ISS TRAJECTORY DATA
Lift off time (UTC) : N/A
Area (sq ft) : 15069.47
Drag Coefficient (Cd) : 2.00
Monthly MSFC 50% solar flux (F10.7-jansky) : 122.4
Monthly MSFC 50% earth geomagnetic index (Kp) : 2.152
ET - UTC (sec) : 67.18
UT1 - UTC (sec) : 0.00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS)
IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA
DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
------------------------------------------------------------------------
166/13:46:01.000 0.0 0.0 0.0
N/A 0.0 0.0 230.1
000/00:00:00.000 0.0 0.0 216.1
170/12:58:26.030 -0.1 3.2 3.2
N/A 3.1 0.0 229.9
000/00:06:52.060 -0.3 -0.1 217.8
Coasting Arc #1 (Orbit 3319)
---------------------------------------
Vector Time (GMT): 2013/158/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 894481.5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3593302.96 A = 6794296.30 meter
Y = 4631720.15 meter E = .0014438
Z = -3437373.86 I = 51.79078
XDOT = -5987.707983 Wp = 57.65560
YDOT = -1239.923705 meter/sec RA = 155.29349 deg
ZDOT = 4610.245131 TA = 262.27315
MA = 262.43711
Ha = 229.928 n.mi
Hp = 216.923
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11789051.69 X = -3628130.78
Y = 15195932.26 feet Y = 4591343.30 meter
Z = -11277473.29 Z = -3454913.96
XDOT = -19644.711231 XDOT = -5995.793426
YDOT = -4067.991158 feet/sec YDOT = -1306.927862 meter/sec
ZDOT = 15125.476152 ZDOT = 4581.137261
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11706309.53 X = 3568083.15
Y = 15204882.27 feet Y = 4634448.12 meter
Z = -11351359.97 Z = -3459894.52
XDOT = -7854.452516 XDOT = -2394.037127
YDOT = 17195.852369 feet/sec YDOT = 5241.295802 meter/sec
ZDOT = 15004.000765 ZDOT = 4573.219433
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13158.50724933 .00016717 00000-0 10270-3 0 9008
2 25544 51.6443 156.3513 0010730 42.0310 318.1662 15.50686270 33205
Satellite: ISS
Catalog Number: 25544
Epoch time: 13158.50724933 = yrday.fracday
Element set: 900
Inclination: 51.6443 deg
RA of node: 156.3513 deg
Eccentricity: .0010730
Arg of perigee: 42.0310 deg
Mean anomaly: 318.1662 deg
Mean motion: 15.50686270 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3320
Checksum: 267
Coasting Arc #2 (Orbit 3335)
---------------------------------------
Vector Time (GMT): 2013/159/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 894481.5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3780431.52 A = 6795482.22 meter
Y = -4813853.27 meter E = .0021445
Z = 2941493.99 I = 51.82207
XDOT = 5634.337489 Wp = 74.49633
YDOT = 1334.866776 meter/sec RA = 150.34525 deg
ZDOT = -5020.665637 TA = 72.06717
MA = 71.83349
Ha = 229.889 n.mi
Hp = 216.768
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12402990.56 X = 3819691.00
Y = -15793481.86 feet Y = -4771359.01 meter
Z = 9650570.85 Z = 2959953.81
XDOT = 18485.359216 XDOT = 5643.381188
YDOT = 4379.484173 feet/sec YDOT = 1397.924773 meter/sec
ZDOT = -16472.000120 ZDOT = -4993.272151
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12397956.50 X = -3778897.14
Y = -15749661.61 feet Y = -4800496.86 meter
Z = 9728339.82 Z = 2965197.98
XDOT = 7531.174903 XDOT = 2295.502110
YDOT = -16104.888528 feet/sec YDOT = -4908.770023 meter/sec
ZDOT = -16357.687012 ZDOT = -4985.823001
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13159.53835184 .00016717 00000-0 10270-3 0 9014
2 25544 51.6436 151.2363 0010724 44.9759 315.2258 15.50742741 33367
Satellite: ISS
Catalog Number: 25544
Epoch time: 13159.53835184 = yrday.fracday
Element set: 901
Inclination: 51.6436 deg
RA of node: 151.2363 deg
Eccentricity: .0010724
Arg of perigee: 44.9759 deg
Mean anomaly: 315.2258 deg
Mean motion: 15.50742741 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3336
Checksum: 305
Coasting Arc #3 (Orbit 3350)
---------------------------------------
Vector Time (GMT): 2013/160/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 894481.5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3856325.63 A = 6796589.72 meter
Y = 5018183.90 meter E = .0016121
Z = -2471192.33 I = 51.85183
XDOT = -5292.125083 Wp = 49.57011
YDOT = -1450.546733 meter/sec RA = 145.40152 deg
ZDOT = 5345.927111 TA = 282.88075
MA = 283.06079
Ha = 229.990 n.mi
Hp = 216.635
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12651986.98 X = -3900148.99
Y = 16463857.94 feet Y = 4974815.36 meter
Z = -8107586.38 Z = -2490031.82
XDOT = -17362.615101 XDOT = -5301.480623
YDOT = -4759.011590 feet/sec YDOT = -1509.779699 meter/sec
ZDOT = 17539.130940 ZDOT = 5320.195377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13263628.74 X = 4042754.04
Y = 15934672.66 feet Y = 4856888.23 meter
Z = -8186984.17 Z = -2495392.78
XDOT = -7346.664614 XDOT = -2239.263374
YDOT = 15016.115449 feet/sec YDOT = 4576.911989 meter/sec
ZDOT = 17431.764760 ZDOT = 5313.201899
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13160.50500056 .00016717 00000-0 10270-3 0 9021
2 25544 51.6436 146.4428 0010785 49.1956 311.0129 15.50730102 33514
Satellite: ISS
Catalog Number: 25544
Epoch time: 13160.50500056 = yrday.fracday
Element set: 902
Inclination: 51.6436 deg
RA of node: 146.4428 deg
Eccentricity: .0010785
Arg of perigee: 49.1956 deg
Mean anomaly: 311.0129 deg
Mean motion: 15.50730102 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3351
Checksum: 269
Coasting Arc #4 (Orbit 3366)
---------------------------------------
Vector Time (GMT): 2013/161/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 894481.5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3951154.41 A = 6797547.74 meter
Y = -5190539.88 meter E = .0021312
Z = 1895566.92 I = 51.88036
XDOT = 4920.522247 Wp = 86.89991
YDOT = 1668.454677 meter/sec RA = 140.45903 deg
ZDOT = -5632.053233 TA = 72.32571
MA = 72.09313
Ha = 229.967 n.mi
Hp = 216.514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12963105.03 X = 3999694.32
Y = -17029330.32 feet Y = -5146084.45 meter
Z = 6219051.57 Z = 1914878.47
XDOT = 16143.445692 XDOT = 4928.858560
YDOT = 5473.932666 feet/sec YDOT = 1723.526474 meter/sec
ZDOT = -18477.864939 ZDOT = -5608.129243
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14023350.69 X = -4274317.29
Y = -16135880.01 feet Y = -4918216.23 meter
Z = 6300460.10 Z = 1920380.24
XDOT = 7507.199723 XDOT = 2288.194475
YDOT = -13770.763103 feet/sec YDOT = -4197.328594 meter/sec
ZDOT = -18378.071677 ZDOT = -5601.636247
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13161.53607932 .00016717 00000-0 10270-3 0 9037
2 25544 51.6439 141.3278 0010757 51.7644 308.4473 15.50773204 33675
Satellite: ISS
Catalog Number: 25544
Epoch time: 13161.53607932 = yrday.fracday
Element set: 903
Inclination: 51.6439 deg
RA of node: 141.3278 deg
Eccentricity: .0010757
Arg of perigee: 51.7644 deg
Mean anomaly: 308.4473 deg
Mean motion: 15.50773204 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3367
Checksum: 306
Coasting Arc #5 (Orbit 3381)
---------------------------------------
Vector Time (GMT): 2013/162/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 894481.5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3937325.30 A = 6798267.08 meter
Y = 5364260.14 meter E = .0019143
Z = -1363230.49 I = 51.90592
XDOT = -4590.239781 Wp = 48.34979
YDOT = -1902.989022 meter/sec RA = 135.52031 deg
ZDOT = 5834.631054 TA = 296.87544
MA = 297.07098
Ha = 230.010 n.mi
Hp = 216.394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12917733.92 X = -3990394.78
Y = 17599278.68 feet Y = 5319933.94 meter
Z = -4472540.98 Z = -1382485.83
XDOT = -15059.841800 XDOT = -4596.962027
YDOT = -6243.402303 feet/sec YDOT = -1954.358352 meter/sec
ZDOT = 19142.490335 ZDOT = 5812.315507
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14865269.10 X = 4530934.02
Y = 15965375.20 feet Y = 4866246.36 meter
Z = -4553751.38 Z = -1387983.42
XDOT = -7816.901272 XDOT = -2382.591508
YDOT = 12651.806836 feet/sec YDOT = 3856.270724 meter/sec
ZDOT = 19049.441875 ZDOT = 5806.269884
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13162.50270515 .00016717 00000-0 10270-3 0 9049
2 25544 51.6439 136.5344 0010777 56.2487 303.9690 15.50778432 33828
Satellite: ISS
Catalog Number: 25544
Epoch time: 13162.50270515 = yrday.fracday
Element set: 904
Inclination: 51.6439 deg
RA of node: 136.5344 deg
Eccentricity: .0010777
Arg of perigee: 56.2487 deg
Mean anomaly: 303.9690 deg
Mean motion: 15.50778432 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3382
Checksum: 311
Coasting Arc #6 (Orbit 3397)
---------------------------------------
Vector Time (GMT): 2013/163/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 894481.5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3943392.51 A = 6798778.12 meter
Y = -5485326.42 meter E = .0019933
Z = 732285.25 I = 51.92991
XDOT = 4244.628536 Wp = 97.12234
YDOT = 2235.841995 meter/sec RA = 130.58267 deg
ZDOT = -5972.715787 TA = 75.00997
MA = 74.78942
Ha = 230.016 n.mi
Hp = 216.314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12937639.48 X = 4000880.30
Y = -17996477.76 feet Y = -5440907.57 meter
Z = 2402510.66 Z = 751580.82
XDOT = 13925.946641 XDOT = 4248.325166
YDOT = 7335.439615 feet/sec YDOT = 2283.329512 meter/sec
ZDOT = -19595.524235 ZDOT = -5952.086552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15523624.13 X = -4731600.63
Y = -15807435.88 feet Y = -4818106.45 meter
Z = 2483918.18 Z = 757098.26
XDOT = 8473.500093 XDOT = 2582.722828
YDOT = -11455.237470 feet/sec YDOT = -3491.556381 meter/sec
ZDOT = -19509.562116 ZDOT = -5946.514533
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13163.53375965 .00016717 00000-0 10270-3 0 9059
2 25544 51.6448 131.4196 0010743 58.7821 301.4382 15.50800561 33986
Satellite: ISS
Catalog Number: 25544
Epoch time: 13163.53375965 = yrday.fracday
Element set: 905
Inclination: 51.6448 deg
RA of node: 131.4196 deg
Eccentricity: .0010743
Arg of perigee: 58.7821 deg
Mean anomaly: 301.4382 deg
Mean motion: 15.50800561 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3398
Checksum: 309
Coasting Arc #7 (Orbit 3412)
---------------------------------------
Vector Time (GMT): 2013/164/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 894481.5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3852415.44 A = 6798943.36 meter
Y = 5589366.82 meter E = .0022113
Z = -162184.63 I = 51.94983
XDOT = -3965.707382 Wp = 53.36136
YDOT = -2575.087293 meter/sec RA = 125.64765 deg
ZDOT = 6034.721843 TA = 304.90055
MA = 305.10817
Ha = 230.001 n.mi
Hp = 216.217
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12639158.25 X = -3913842.77
Y = 18337817.65 feet Y = 5545943.24 meter
Z = -532101.82 Z = -181047.87
XDOT = -13010.850991 XDOT = -3965.932419
YDOT = -8448.449123 feet/sec YDOT = -2619.436250 meter/sec
ZDOT = 19798.956178 ZDOT = 6015.456018
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16174806.84 X = 4930081.12
Y = 15307136.35 feet Y = 4665615.16 meter
Z = -611727.21 Z = -186454.45
XDOT = -9251.149366 XDOT = -2819.750327
YDOT = 10497.264891 feet/sec YDOT = 3199.566339 meter/sec
ZDOT = 19718.734186 ZDOT = 6010.270180
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13164.50036181 .00016717 00000-0 10270-3 0 9062
2 25544 51.6447 126.6261 0010706 63.0303 297.1940 15.50822467 34135
Satellite: ISS
Catalog Number: 25544
Epoch time: 13164.50036181 = yrday.fracday
Element set: 906
Inclination: 51.6447 deg
RA of node: 126.6261 deg
Eccentricity: .0010706
Arg of perigee: 63.0303 deg
Mean anomaly: 297.1940 deg
Mean motion: 15.50822467 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3413
Checksum: 281
Coasting Arc #8 (Orbit 3428)
---------------------------------------
Vector Time (GMT): 2013/165/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 894481.5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3788923.58 A = 6798829.27 meter
Y = -5621595.14 meter E = .0017559
Z = -493853.62 I = 51.96764
XDOT = 3686.033785 Wp = 102.95238
YDOT = 2996.028702 meter/sec RA = 120.71320 deg
ZDOT = -6007.712239 TA = 82.34019
MA = 82.14081
Ha = 230.021 n.mi
Hp = 216.164
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12430851.64 X = 3853902.87
Y = -18443553.62 feet Y = -5578861.64 meter
Z = -1620254.67 Z = -475290.11
XDOT = 12093.286695 XDOT = 3681.441366
YDOT = 9829.490493 feet/sec YDOT = 3037.223152 meter/sec
ZDOT = -19710.341993 ZDOT = -5989.816725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16567312.28 X = -5049716.78
Y = -14847989.00 feet Y = -4525667.05 meter
Z = -1541867.23 Z = -469961.13
XDOT = 10324.632083 XDOT = 3146.947859
YDOT = -9546.770278 feet/sec YDOT = -2909.855581 meter/sec
ZDOT = -19635.902995 ZDOT = -5985.023233
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13165.53139127 .00016717 00000-0 10270-3 0 9071
2 25544 51.6457 121.5114 0010683 65.8226 294.4041 15.50832026 34296
Satellite: ISS
Catalog Number: 25544
Epoch time: 13165.53139127 = yrday.fracday
Element set: 907
Inclination: 51.6457 deg
RA of node: 121.5114 deg
Eccentricity: .0010683
Arg of perigee: 65.8226 deg
Mean anomaly: 294.4041 deg
Mean motion: 15.50832026 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3429
Checksum: 291
Coasting Arc #9 (Orbit 3444)
---------------------------------------
Vector Time (GMT): 2013/166/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 894481.5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3647377.77 A = 6798398.79 meter
Y = 5623507.47 meter E = .0024045
Z = 1072622.32 I = 51.98105
XDOT = -3490.160147 Wp = 62.43255
YDOT = -3409.440719 meter/sec RA = 115.78002 deg
ZDOT = 5916.476548 TA = 309.13816
MA = 309.35163
Ha = 229.996 n.mi
Hp = 216.085
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11966462.52 X = -3715200.48
Y = 18449827.66 feet Y = 5582340.88 meter
Z = 3519102.09 Z = 1054739.42
XDOT = -11450.656650 XDOT = -3480.516283
YDOT = -11185.829130 feet/sec YDOT = -3448.416471 meter/sec
ZDOT = 19411.012298 ZDOT = 5899.544801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16880873.15 X = 5145290.14
Y = 14112212.13 feet Y = 4301402.26 meter
Z = 3443549.92 Z = 1049594.01
XDOT = -11460.976676 XDOT = -3493.305691
YDOT = 8916.202350 feet/sec YDOT = 2717.658476 meter/sec
ZDOT = 19340.658289 ZDOT = 5895.032647
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13166.56240728 .00016717 00000-0 10270-3 0 9086
2 25544 51.6455 116.3979 0010632 69.8789 290.3505 15.50856992 34453
Satellite: ISS
Catalog Number: 25544
Epoch time: 13166.56240728 = yrday.fracday
Element set: 908
Inclination: 51.6455 deg
RA of node: 116.3979 deg
Eccentricity: .0010632
Arg of perigee: 69.8789 deg
Mean anomaly: 290.3505 deg
Mean motion: 15.50856992 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3445
Checksum: 343
Coasting Arc #10 (Orbit 3445)
---------------------------------------
Vector Time (GMT): 2013/166/13:46:01.000
Vector Time (MET): N/A
Weight (LBS) : 922037.1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4683229.72 A = 6789342.20 meter
Y = 1179432.19 meter E = .0016857
Z = 4757414.95 I = 51.95336
XDOT = 1002.164418 Wp = 89.97038
YDOT = -7098.291414 meter/sec RA = 115.42770 deg
ZDOT = 2737.963832 TA = 333.04517
MA = 333.13263
Ha = 230.095 n.mi
Hp = 216.061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15364926.92 X = -4719180.55
Y = 3869528.20 feet Y = 1126859.95 meter
Z = 15608316.75 Z = 4734577.01
XDOT = 3287.941005 XDOT = 1068.164276
YDOT = -23288.357656 feet/sec YDOT = -7086.715782 meter/sec
ZDOT = 8982.820970 ZDOT = 2742.991972
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8855030.04 X = 2699013.16
Y = 13252177.21 feet Y = 4039263.61 meter
Z = 15512640.70 Z = 4728252.89
XDOT = -22048.252309 XDOT = -6720.307304
YDOT = 4159.493153 feet/sec YDOT = 1267.813513 meter/sec
ZDOT = 9004.809958 ZDOT = 2744.666075
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13166.62684498 .00016717 00000-0 10270-3 0 9090
2 25544 51.6469 116.0789 0010594 70.1514 290.0778 15.50869321 34462
Satellite: ISS
Catalog Number: 25544
Epoch time: 13166.62684498 = yrday.fracday
Element set: 909
Inclination: 51.6469 deg
RA of node: 116.0789 deg
Eccentricity: .0010594
Arg of perigee: 70.1514 deg
Mean anomaly: 290.0778 deg
Mean motion: 15.50869321 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3446
Checksum: 336
Coasting Arc #11 (Orbit 3460)
---------------------------------------
Vector Time (GMT): 2013/167/13:46:01.000
Vector Time (MET): N/A
Weight (LBS) : 922037.1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4506805.97 A = 6788259.89 meter
Y = -815174.88 meter E = .0023292
Z = -5031796.92 I = 51.96275
XDOT = -993.099496 Wp = 74.13297
YDOT = 7291.457720 meter/sec RA = 110.48477 deg
ZDOT = -2072.526445 TA = 175.74414
MA = 175.72430
Ha = 229.981 n.mi
Hp = 216.078
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14786108.82 X = 4540029.65
Y = -2674458.27 feet Y = -764590.77 meter
Z = -16508520.08 Z = -5009822.56
XDOT = -3258.200446 XDOT = -1064.492539
YDOT = 23922.105381 feet/sec YDOT = 7279.953238 meter/sec
ZDOT = -6799.627444 ZDOT = -2077.523682
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7761233.88 X = -2365624.09
Y = -12983635.12 feet Y = -3957411.98 meter
Z = -16416499.15 Z = -5003748.94
XDOT = 22569.109885 XDOT = 6879.064693
YDOT = -4873.488834 feet/sec YDOT = -1485.439397 meter/sec
ZDOT = -6821.524237 ZDOT = -2079.200588
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13167.59341070 .00016717 00000-0 10270-3 0 9105
2 25544 51.6475 111.2839 0010696 73.2548 286.9776 15.50883396 34613
Satellite: ISS
Catalog Number: 25544
Epoch time: 13167.59341070 = yrday.fracday
Element set: 910
Inclination: 51.6475 deg
RA of node: 111.2839 deg
Eccentricity: .0010696
Arg of perigee: 73.2548 deg
Mean anomaly: 286.9776 deg
Mean motion: 15.50883396 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3461
Checksum: 332
Coasting Arc #12 (Orbit 3476)
---------------------------------------
Vector Time (GMT): 2013/168/13:46:01.000
Vector Time (MET): N/A
Weight (LBS) : 922037.1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4334006.71 A = 6787357.60 meter
Y = 420429.06 meter E = .0013924
Z = 5194572.67 I = 51.96967
XDOT = 949.646014 Wp = 90.90863
YDOT = -7485.883209 meter/sec RA = 105.54216 deg
ZDOT = 1394.768652 TA = 345.73040
MA = 345.76969
Ha = 230.046 n.mi
Hp = 215.922
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14219182.12 X = -4363619.91
Y = 1379360.43 feet Y = 371797.46 meter
Z = 17042561.25 Z = 5173446.42
XDOT = 3115.636530 XDOT = 1026.508746
YDOT = -24559.984281 feet/sec YDOT = -7474.834018 meter/sec
ZDOT = 4576.012637 ZDOT = 1399.568062
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6571777.86 X = 2003077.89
Y = 12802564.19 feet Y = 3902221.57 meter
Z = 16954136.82 Z = 5167620.90
XDOT = -23030.686354 XDOT = -7019.753201
YDOT = 5719.199788 feet/sec YDOT = 1743.212096 meter/sec
ZDOT = 4597.121925 ZDOT = 1401.202763
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13168.62439980 .00016717 00000-0 10270-3 0 9119
2 25544 51.6472 106.1697 0010531 77.1911 283.0417 15.50915665 34772
Satellite: ISS
Catalog Number: 25544
Epoch time: 13168.62439980 = yrday.fracday
Element set: 911
Inclination: 51.6472 deg
RA of node: 106.1697 deg
Eccentricity: .0010531
Arg of perigee: 77.1911 deg
Mean anomaly: 283.0417 deg
Mean motion: 15.50915665 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3477
Checksum: 315
Coasting Arc #13 (Orbit 3491)
---------------------------------------
Vector Time (GMT): 2013/169/13:46:01.000
Vector Time (MET): N/A
Weight (LBS) : 922037.1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4234020.75 A = 6786874.55 meter
Y = 16067.93 meter E = .0025204
Z = -5326062.33 I = 51.97619
XDOT = -878.262523 Wp = 82.93492
YDOT = 7563.644386 meter/sec RA = 100.59871 deg
ZDOT = -675.097681 TA = 180.62666
MA = 180.62982
Ha = 229.924 n.mi
Hp = 215.977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13891144.19 X = 4259399.20
Y = 52716.29 feet Y = 63557.81 meter
Z = -17473957.76 Z = -5305432.00
XDOT = -2881.438724 XDOT = -959.496082
YDOT = 24815.106253 feet/sec YDOT = 7553.368960 meter/sec
ZDOT = -2214.887405 ZDOT = -679.560854
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5344147.22 X = -1628896.07
Y = -12938898.38 feet Y = -3943776.23 meter
Z = -17387664.16 Z = -5299760.04
XDOT = 23061.620032 XDOT = 7029.181786
YDOT = -6520.992043 feet/sec YDOT = -1987.598375 meter/sec
ZDOT = -2234.616878 ZDOT = -681.111224
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13169.59094216 .00016717 00000-0 10270-3 0 9126
2 25544 51.6480 101.3746 0010616 80.3335 279.9015 15.50920587 34927
Satellite: ISS
Catalog Number: 25544
Epoch time: 13169.59094216 = yrday.fracday
Element set: 912
Inclination: 51.6480 deg
RA of node: 101.3746 deg
Eccentricity: .0010616
Arg of perigee: 80.3335 deg
Mean anomaly: 279.9015 deg
Mean motion: 15.50920587 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3492
Checksum: 307
Coasting Arc #14 (Orbit 3506)
---------------------------------------
Vector Time (GMT): 2013/170/13:01:52.060
Vector Time (MET): N/A
Weight (LBS) : 921735.5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4005964.86 A = 6788734.00 meter
Y = 1498196.07 meter E = .0022246
Z = -5291350.54 I = 51.98125
XDOT = -1511.475109 Wp = 92.38175
YDOT = 7432.677174 meter/sec RA = 95.79926 deg
ZDOT = 962.783629 TA = 186.80088
MA = 186.83111
Ha = 229.912 n.mi
Hp = 217.825
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13142929.33 X = 4014618.20
Y = 4915341.45 feet Y = 1543042.27 meter
Z = -17360073.94 Z = -5271868.52
XDOT = -4958.907839 XDOT = -1599.153568
YDOT = 24385.423799 feet/sec YDOT = 7415.284560 meter/sec
ZDOT = 3158.738941 ZDOT = 955.228798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1912451.38 X = 582915.18
Y = -14001973.41 feet Y = -4267801.50 meter
Z = -17278790.76 Z = -5266575.42
XDOT = 23863.573713 XDOT = 7273.617268
YDOT = -587.709161 feet/sec YDOT = -179.133752 meter/sec
ZDOT = 3126.077847 ZDOT = 952.828528
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13170.55747388 .00016717 00000-0 10270-3 0 9130
2 25544 51.6479 96.5798 0008027 83.3865 276.8199 15.50333418 35078
Satellite: ISS
Catalog Number: 25544
Epoch time: 13170.55747388 = yrday.fracday
Element set: 913
Inclination: 51.6479 deg
RA of node: 96.5798 deg
Eccentricity: .0008027
Arg of perigee: 83.3865 deg
Mean anomaly: 276.8199 deg
Mean motion: 15.50333418 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3507
Checksum: 352
Coasting Arc #15 (Orbit 3522)
---------------------------------------
Vector Time (GMT): 2013/171/13:01:52.060
Vector Time (MET): N/A
Weight (LBS) : 921735.5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4024478.05 A = 6788970.88 meter
Y = -1719182.76 meter E = .0012064
Z = 5180830.63 I = 51.98487
XDOT = 1264.391569 Wp = 75.00887
YDOT = -7420.548819 meter/sec RA = 90.86289 deg
ZDOT = -1474.325609 TA = 29.14539
MA = 29.07811
Ha = 229.923 n.mi
Hp = 217.672
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13203668.16 X = -4030122.01
Y = -5640363.38 feet Y = -1764219.27 meter
Z = 16997475.82 Z = 5161265.92
XDOT = 4148.266301 XDOT = 1354.437726
YDOT = -24345.632609 feet/sec YDOT = -7405.905918 meter/sec
ZDOT = -4837.026277 ZDOT = -1467.965531
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2362451.22 X = -720075.13
Y = 14259616.19 feet Y = 4346331.02 meter
Z = 16915877.34 Z = 5155959.41
XDOT = -23607.267970 XDOT = -7195.495277
YDOT = 1817.154618 feet/sec YDOT = 553.868728 meter/sec
ZDOT = -4809.345628 ZDOT = -1465.888547
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13171.58882164 .00016717 00000-0 10270-3 0 9147
2 25544 51.6480 91.4680 0007885 86.7335 273.4718 15.50386059 35231
Satellite: ISS
Catalog Number: 25544
Epoch time: 13171.58882164 = yrday.fracday
Element set: 914
Inclination: 51.6480 deg
RA of node: 91.4680 deg
Eccentricity: .0007885
Arg of perigee: 86.7335 deg
Mean anomaly: 273.4718 deg
Mean motion: 15.50386059 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3523
Checksum: 332
Coasting Arc #16 (Orbit 3537)
---------------------------------------
Vector Time (GMT): 2013/172/13:01:52.060
Vector Time (MET): N/A
Weight (LBS) : 921735.5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4109047.50 A = 6789586.68 meter
Y = 1926405.84 meter E = .0020631
Z = -5068602.08 I = 51.98733
XDOT = -1016.201611 Wp = 99.08098
YDOT = 7320.331116 meter/sec RA = 85.92673 deg
ZDOT = 1962.041455 TA = 189.90521
MA = 189.94594
Ha = 229.824 n.mi
Hp = 217.790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13481126.95 X = 4111822.70
Y = 6320229.14 feet Y = 1972372.13 meter
Z = -16629271.93 Z = -5048633.49
XDOT = -3333.994787 XDOT = -1107.514748
YDOT = 24016.834369 feet/sec YDOT = 7308.456435 meter/sec
ZDOT = 6437.143882 ZDOT = 1956.884168
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2705834.92 X = 824738.48
Y = -14735219.86 feet Y = -4491295.01 meter
Z = -16546012.15 Z = -5043224.50
XDOT = 23020.544838 XDOT = 7016.662067
YDOT = -2961.973374 feet/sec YDOT = -902.809484 meter/sec
ZDOT = 6414.491207 ZDOT = 1955.136920
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 13172.55570109 .00016717 00000-0 10270-3 0 9159
2 25544 51.6491 86.6756 0007922 90.3116 269.8943 15.50370947 35387
Satellite: ISS
Catalog Number: 25544
Epoch time: 13172.55570109 = yrday.fracday
Element set: 915
Inclination: 51.6491 deg
RA of node: 86.6756 deg
Eccentricity: .0007922
Arg of perigee: 90.3116 deg
Mean anomaly: 269.8943 deg
Mean motion: 15.50370947 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3538
Checksum: 330
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