ISS TRAJECTORY DATA
Lift off time (UTC) : N/A
Area (sq ft) : 10225.71
Drag Coefficient (Cd) : 2.00
Monthly MSFC 50% solar flux (F10.7-jansky) : 71.3
Monthly MSFC 50% earth geomagnetic index (Kp) : 2.07
ET - UTC (sec) : 65.18
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
------------------------------------------------------------------------
There are no maneuvers.
Coasting Arc #1 (Orbit 117)
---------------------------------------
Vector Time (GMT): 2008/249/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 643009.1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5684041.13 A = 6737942.86 meter
Y = -3551807.36 meter E = .0019113
Z = 612604.61 I = 51.46816
XDOT = 2078.646331 Wp = 61.18588
YDOT = 4380.835296 meter/sec RA = 323.82585 deg
ZDOT = 5981.376402 TA = 305.49589
MA = 305.67405
Ha = 195.625 n.mi
Hp = 184.647
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18648428.92 X = 5720359.62
Y = -11652911.29 feet Y = -3488042.06 meter
Z = 2009857.66 Z = 640306.10
XDOT = 6819.705812 XDOT = 2000.448035
YDOT = 14372.819214 feet/sec YDOT = 4403.642765 meter/sec
ZDOT = 19623.938326 ZDOT = 5991.284519
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21104180.29 X = -6432554.15
Y = 6142255.62 feet Y = 1872159.51 meter
Z = 2116610.65 Z = 645142.93
XDOT = -2095.463419 XDOT = -638.697250
YDOT = -14116.670912 feet/sec YDOT = -4302.761294 meter/sec
ZDOT = 19662.613950 ZDOT = 5993.164732
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 08249.56233711 .00020000 00000-0 20000-3 0 9000
2 25544 51.6425 324.0421 0006399 82.3294 277.8595 15.71916473 1183
Satellite: ISS
Catalog Number: 25544
Epoch time: 08249.56233711 = yrday.fracday
Element set: 900
Inclination: 51.6425 deg
RA of node: 324.0421 deg
Eccentricity: .0006399
Arg of perigee: 82.3294 deg
Mean anomaly: 277.8595 deg
Mean motion: 15.71916473 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 118
Checksum: 295
Coasting Arc #2 (Orbit 132)
---------------------------------------
Vector Time (GMT): 2008/250/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 643009.1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2803261.08 A = 6726008.94 meter
Y = -3134100.84 meter E = .0021312
Z = -5267951.97 I = 51.40430
XDOT = 5752.784979 Wp = 88.38438
YDOT = -5090.679087 meter/sec RA = 318.68553 deg
ZDOT = -32.144567 TA = 181.30606
MA = 181.31164
Ha = 195.568 n.mi
Hp = 184.560
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9197050.79 X = -2742415.85
Y = -10282483.08 feet Y = -3165108.31 meter
Z = -17283306.97 Z = -5281422.48
XDOT = 18873.966465 XDOT = 5809.438362
YDOT = -16701.703041 feet/sec YDOT = -5026.031365 meter/sec
ZDOT = -105.461179 ZDOT = -4.059819
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6168735.07 X = 1880230.45
Y = 12265810.18 feet Y = 3738618.94 meter
Z = -17335642.75 Z = -5283903.91
XDOT = -21620.714613 XDOT = -6589.993814
YDOT = 10875.033301 feet/sec YDOT = 3314.710150 meter/sec
ZDOT = 2.639939 ZDOT = .804653
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 08250.51592465 .00020000 00000-0 20000-3 0 9012
2 25544 51.6415 319.1600 0006291 85.6567 274.5314 15.71932703 1330
Satellite: ISS
Catalog Number: 25544
Epoch time: 08250.51592465 = yrday.fracday
Element set: 901
Inclination: 51.6415 deg
RA of node: 319.1600 deg
Eccentricity: .0006291
Arg of perigee: 85.6567 deg
Mean anomaly: 274.5314 deg
Mean motion: 15.71932703 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 133
Checksum: 274
Coasting Arc #3 (Orbit 148)
---------------------------------------
Vector Time (GMT): 2008/251/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 643009.1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4218453.14 A = 6737735.70 meter
Y = 5203295.99 meter E = .0018738
Z = 660403.71 I = 51.42334
XDOT = -4125.788717 Wp = 115.17981
YDOT = -2571.394577 meter/sec RA = 313.54288 deg
ZDOT = -5970.293784 TA = 57.61043
MA = 57.42925
Ha = 195.545 n.mi
Hp = 184.523
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13840069.37 X = -4279531.84
Y = 17071181.07 feet Y = 5155781.30 meter
Z = 2166678.82 Z = 639762.12
XDOT = -13536.052221 XDOT = -4067.725659
YDOT = -8436.333915 feet/sec YDOT = -2617.206801 meter/sec
ZDOT = -19587.578031 ZDOT = -5990.195907
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17528588.88 X = 5342713.89
Y = -13268713.75 feet Y = -4044303.95 meter
Z = 2087354.25 Z = 636225.58
XDOT = 10052.711804 XDOT = 3064.066558
YDOT = 10120.112673 feet/sec YDOT = 3084.610343 meter/sec
ZDOT = -19664.724792 ZDOT = -5993.808116
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 08251.53307237 .00020000 00000-0 20000-3 0 9027
2 25544 51.6417 313.9521 0006484 88.4779 271.7126 15.71989013 1499
Satellite: ISS
Catalog Number: 25544
Epoch time: 08251.53307237 = yrday.fracday
Element set: 902
Inclination: 51.6417 deg
RA of node: 313.9521 deg
Eccentricity: .0006484
Arg of perigee: 88.4779 deg
Mean anomaly: 271.7126 deg
Mean motion: 15.71989013 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 149
Checksum: 298
Coasting Arc #4 (Orbit 164)
---------------------------------------
Vector Time (GMT): 2008/252/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 643009.1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4224606.79 A = 6726481.45 meter
Y = 1212523.58 meter E = .0010586
Z = 5083839.79 I = 51.36649
XDOT = -3700.201227 Wp = 105.96019
YDOT = 6590.345555 meter/sec RA = 308.42416 deg
ZDOT = 1497.536595 TA = 329.60202
MA = 329.66336
Ha = 195.360 n.mi
Hp = 184.507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13860258.51 X = 4186037.81
Y = 3978095.74 feet Y = 1259549.83 meter
Z = 16679264.41 Z = 5104269.26
XDOT = -12139.767804 XDOT = -3780.895281
YDOT = 21621.868618 feet/sec YDOT = 6548.516565 meter/sec
ZDOT = 4913.177804 ZDOT = 1479.365128
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12537217.96 X = -3821344.03
Y = -6935869.49 feet Y = -2114053.02 meter
Z = 16758333.84 Z = 5107940.15
XDOT = 16160.209901 XDOT = 4925.631978
YDOT = -17465.211917 feet/sec YDOT = -5323.396592 meter/sec
ZDOT = 4843.523173 ZDOT = 1476.305863
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 08252.55020541 .00020000 00000-0 20000-3 0 9031
2 25544 51.6416 308.7444 0006389 92.4338 267.7556 15.72014438 1655
Satellite: ISS
Catalog Number: 25544
Epoch time: 08252.55020541 = yrday.fracday
Element set: 903
Inclination: 51.6416 deg
RA of node: 308.7444 deg
Eccentricity: .0006389
Arg of perigee: 92.4338 deg
Mean anomaly: 267.7556 deg
Mean motion: 15.72014438 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 165
Checksum: 288
Coasting Arc #5 (Orbit 179)
---------------------------------------
Vector Time (GMT): 2008/253/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 643009.1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2150884.09 A = 6736256.74 meter
Y = -6085655.99 meter E = .0011948
Z = -1925993.05 I = 51.38161
XDOT = 5277.442863 Wp = 65.32642
YDOT = 104.278385 meter/sec RA = 303.25496 deg
ZDOT = 5596.268872 TA = 273.20675
MA = 273.34344
Ha = 195.524 n.mi
Hp = 184.492
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7056706.33 X = 2228131.11
Y = -19966062.97 feet Y = -6061171.63 meter
Z = -6318874.83 Z = -1915356.53
XDOT = 17314.445089 XDOT = 5248.699006
YDOT = 342.120686 feet/sec YDOT = 163.133006 meter/sec
ZDOT = 18360.462179 ZDOT = 5621.836783
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11040605.53 X = -3365176.57
Y = 18084714.24 feet Y = 5512220.90 meter
Z = -6278303.47 Z = -1913626.90
XDOT = -15453.483718 XDOT = -4710.221837
YDOT = -3062.699822 feet/sec YDOT = -933.510906 meter/sec
ZDOT = 18459.298518 ZDOT = 5626.394188
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 08253.50375691 .00020000 00000-0 20000-3 0 9047
2 25544 51.6411 303.8621 0006471 94.6125 265.5776 15.72007569 1807
Satellite: ISS
Catalog Number: 25544
Epoch time: 08253.50375691 = yrday.fracday
Element set: 904
Inclination: 51.6411 deg
RA of node: 303.8621 deg
Eccentricity: .0006471
Arg of perigee: 94.6125 deg
Mean anomaly: 265.5776 deg
Mean motion: 15.72007569 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 180
Checksum: 286
Coasting Arc #6 (Orbit 195)
---------------------------------------
Vector Time (GMT): 2008/254/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 643009.1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4771674.30 A = 6728367.33 meter
Y = 1044717.50 meter E = .0016967
Z = -4642844.87 I = 51.34076
XDOT = 1203.408129 Wp = 80.86283
YDOT = -7043.247899 meter/sec RA = 298.15326 deg
ZDOT = -2827.803294 TA = 161.05339
MA = 160.99018
Ha = 195.503 n.mi
Hp = 184.305
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15655099.42 X = -4760447.90
Y = 3427550.87 feet Y = 991420.67 meter
Z = -15232430.66 Z = -4665998.25
XDOT = 3948.189399 XDOT = 1295.814292
YDOT = -23107.768699 feet/sec YDOT = -7029.274024 meter/sec
ZDOT = -9277.569863 ZDOT = -2821.732728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15934595.57 X = 4856864.73
Y = -432729.10 feet Y = -131895.83 meter
Z = -15321833.97 Z = -4670094.99
XDOT = -8315.289932 XDOT = -2534.500371
YDOT = 20777.948793 feet/sec YDOT = 6333.118792 meter/sec
ZDOT = -9254.740319 ZDOT = -2820.844849
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 08254.52086464 .00020000 00000-0 20000-3 0 9058
2 25544 51.6416 298.6537 0006575 98.6952 261.4955 15.72026799 1963
Satellite: ISS
Catalog Number: 25544
Epoch time: 08254.52086464 = yrday.fracday
Element set: 905
Inclination: 51.6416 deg
RA of node: 298.6537 deg
Eccentricity: .0006575
Arg of perigee: 98.6952 deg
Mean anomaly: 261.4955 deg
Mean motion: 15.72026799 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 196
Checksum: 333
Coasting Arc #7 (Orbit 211)
---------------------------------------
Vector Time (GMT): 2008/255/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 643009.1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 51757.79 A = 6733738.86 meter
Y = 6020036.85 meter E = .0019799
Z = 2996341.97 I = 51.34598
XDOT = -5353.768893 Wp = 97.81333
YDOT = 2515.332932 meter/sec RA = 292.96595 deg
ZDOT = -4935.984385 TA = 47.39702
MA = 47.23019
Ha = 195.404 n.mi
Hp = 184.363
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 169809.02 X = -30118.65
Y = 19750777.08 feet Y = 6020157.90 meter
Z = 9830518.28 Z = 2996394.42
XDOT = -17564.858572 XDOT = -5357.519917
YDOT = 8252.404631 feet/sec YDOT = 2455.442940 meter/sec
ZDOT = -16194.174491 ZDOT = -4962.001942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3275572.59 X = 998394.53
Y = -19477623.16 feet Y = -5936779.54 meter
Z = 9831273.57 Z = 2996572.18
XDOT = 17207.961538 XDOT = 5244.986677
YDOT = -5372.396689 feet/sec YDOT = -1637.506511 meter/sec
ZDOT = -16294.515648 ZDOT = -4966.568369
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 08255.53795697 .00020000 00000-0 20000-3 0 9066
2 25544 51.6409 293.4458 0006565 100.8707 259.3194 15.72085068 2127
Satellite: ISS
Catalog Number: 25544
Epoch time: 08255.53795697 = yrday.fracday
Element set: 906
Inclination: 51.6409 deg
RA of node: 293.4458 deg
Eccentricity: .0006565
Arg of perigee: 100.8707 deg
Mean anomaly: 259.3194 deg
Mean motion: 15.72085068 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 212
Checksum: 315
Coasting Arc #8 (Orbit 227)
---------------------------------------
Vector Time (GMT): 2008/256/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 643009.1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4357109.26 A = 6730917.71 meter
Y = -3301157.54 meter E = .0017825
Z = 3914999.14 I = 51.32554
XDOT = 1281.543388 Wp = 101.82442
YDOT = 6457.757886 meter/sec RA = 287.87348 deg
ZDOT = 4000.005446 TA = 306.40438
MA = 306.56865
Ha = 195.414 n.mi
Hp = 184.308
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14294977.87 X = 4374681.30
Y = -10830569.35 feet Y = -3252335.41 meter
Z = 12844485.36 Z = 3936208.62
XDOT = 4204.538674 XDOT = 1189.805308
YDOT = 21186.869705 feet/sec YDOT = 6471.576077 meter/sec
ZDOT = 13123.377446 ZDOT = 4006.008030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15724052.56 X = -4792691.22
Y = 8502756.01 feet Y = 2591640.03 meter
Z = 12926164.94 Z = 3939895.07
XDOT = -185.557926 XDOT = -56.558056
YDOT = -20423.900715 feet/sec YDOT = -6225.204938 meter/sec
ZDOT = 13147.184628 ZDOT = 4007.261875
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 08256.55503733 .00020000 00000-0 20000-3 0 9078
2 25544 51.6402 288.2375 0006767 104.3094 255.8820 15.72076600 2288
Satellite: ISS
Catalog Number: 25544
Epoch time: 08256.55503733 = yrday.fracday
Element set: 907
Inclination: 51.6402 deg
RA of node: 288.2375 deg
Eccentricity: .0006767
Arg of perigee: 104.3094 deg
Mean anomaly: 255.8820 deg
Mean motion: 15.72076600 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 228
Checksum: 288
Coasting Arc #9 (Orbit 242)
---------------------------------------
Vector Time (GMT): 2008/257/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 643009.1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2086231.07 A = 6730839.38 meter
Y = -5061592.61 meter E = .0013504
Z = -3929820.71 I = 51.31874
XDOT = 4377.162732 Wp = 107.16316
YDOT = -4897.325553 meter/sec RA = 282.67836 deg
ZDOT = 3991.413873 TA = 204.50540
MA = 204.56964
Ha = 195.393 n.mi
Hp = 184.276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6844590.14 X = -2010386.24
Y = -16606274.96 feet Y = -5084498.24 meter
Z = -12893112.56 Z = -3939770.99
XDOT = 14360.770117 XDOT = 4412.210648
YDOT = -16067.341052 feet/sec YDOT = -4848.181366 meter/sec
ZDOT = 13095.189872 ZDOT = 4012.763449
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4422655.02 X = 1348025.25
Y = 17379617.92 feet Y = 5297307.54 meter
Z = -12932058.50 Z = -3941691.43
XDOT = -15092.017020 XDOT = -4600.046788
YDOT = 13627.638591 feet/sec YDOT = 4153.704243 meter/sec
ZDOT = 13177.254506 ZDOT = 4016.427173
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 08257.50853589 .00020000 00000-0 20000-3 0 9082
2 25544 51.6412 283.3548 0006682 107.3049 252.8844 15.72108074 2437
Satellite: ISS
Catalog Number: 25544
Epoch time: 08257.50853589 = yrday.fracday
Element set: 908
Inclination: 51.6412 deg
RA of node: 283.3548 deg
Eccentricity: .0006682
Arg of perigee: 107.3049 deg
Mean anomaly: 252.8844 deg
Mean motion: 15.72108074 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 243
Checksum: 301
Coasting Arc #10 (Orbit 258)
---------------------------------------
Vector Time (GMT): 2008/258/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 643009.1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3139815.00 A = 6733448.70 meter
Y = 5123233.92 meter E = .0011159
Z = -3043226.90 I = 51.32179
XDOT = -3302.005557 Wp = 109.32133
YDOT = -4923.712944 meter/sec RA = 277.58403 deg
ZDOT = -4900.464145 TA = 106.04189
MA = 105.91897
Ha = 195.307 n.mi
Hp = 184.314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10301230.32 X = -3182087.06
Y = 16808510.22 feet Y = 5087886.08 meter
Z = -9984340.23 Z = -3058583.20
XDOT = -10833.351565 XDOT = -3222.896879
YDOT = -16153.913858 feet/sec YDOT = -4960.195977 meter/sec
ZDOT = -16077.638272 ZDOT = -4916.312670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12194030.78 X = 3716740.58
Y = -15452119.74 feet Y = -4709806.10 meter
Z = -10043207.68 Z = -3061169.70
XDOT = 7590.203439 XDOT = 2313.494008
YDOT = 16440.985465 feet/sec YDOT = 5011.212370 meter/sec
ZDOT = -16139.379050 ZDOT = -4919.282734
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 08258.52558729 .00020000 00000-0 20000-3 0 9094
2 25544 51.6404 278.1457 0006652 111.4202 248.7671 15.72126145 2591
Satellite: ISS
Catalog Number: 25544
Epoch time: 08258.52558729 = yrday.fracday
Element set: 909
Inclination: 51.6404 deg
RA of node: 278.1457 deg
Eccentricity: .0006652
Arg of perigee: 111.4202 deg
Mean anomaly: 248.7671 deg
Mean motion: 15.72126145 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 259
Checksum: 297
Coasting Arc #11 (Orbit 274)
---------------------------------------
Vector Time (GMT): 2008/259/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 643009.1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3542713.55 A = 6728125.63 meter
Y = 3391215.50 meter E = .0013501
Z = 4594934.90 I = 51.30040
XDOT = -2599.878769 Wp = 86.33371
YDOT = 6650.841741 meter/sec RA = 272.39237 deg
ZDOT = -2895.861537 TA = 32.49325
MA = 32.41021
Ha = 195.147 n.mi
Hp = 184.331
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11623075.96 X = 3482207.70
Y = 11126035.11 feet Y = 3430494.30 meter
Z = 15075245.74 Z = 4611998.16
XDOT = -8529.785989 XDOT = -2659.988705
YDOT = 21820.346918 feet/sec YDOT = 6621.432027 meter/sec
ZDOT = -9500.858062 ZDOT = -2908.638431
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10324703.12 X = -3146969.51
Y = -12258952.84 feet Y = -3736528.83 meter
Z = 15141537.80 Z = 4615140.72
XDOT = 9791.371432 XDOT = 2984.410012
YDOT = -20074.507219 feet/sec YDOT = -6118.709800 meter/sec
ZDOT = -9549.598627 ZDOT = -2910.717662
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 08259.54262382 .00020000 00000-0 20000-3 0 9106
2 25544 51.6391 272.9366 0006640 114.4080 245.7776 15.72169181 2759
Satellite: ISS
Catalog Number: 25544
Epoch time: 08259.54262382 = yrday.fracday
Element set: 910
Inclination: 51.6391 deg
RA of node: 272.9366 deg
Eccentricity: .0006640
Arg of perigee: 114.4080 deg
Mean anomaly: 245.7776 deg
Mean motion: 15.72169181 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 275
Checksum: 297
Coasting Arc #12 (Orbit 290)
---------------------------------------
Vector Time (GMT): 2008/260/12:00:00.000
Vector Time (MET): N/A
Weight (LBS) : 643009.1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1293052.23 A = 6735646.92 meter
Y = -6298412.82 meter E = .0019036
Z = 1986025.07 I = 51.32583
XDOT = 4584.727242 Wp = 83.70336
YDOT = 2708.620515 meter/sec RA = 267.28782 deg
ZDOT = 5561.420072 TA = 298.50749
MA = 298.69905
Ha = 195.179 n.mi
Hp = 184.371
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4242297.36 X = 1353738.16
Y = -20664084.07 feet Y = -6283613.67 meter
Z = 6515830.28 Z = 1992454.77
XDOT = 15041.756042 XDOT = 4527.081637
YDOT = 8886.550247 feet/sec YDOT = 2759.567786 meter/sec
ZDOT = 18246.128844 ZDOT = 5583.552603
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5971338.09 X = -1820063.85
Y = 20224445.08 feet Y = 6164410.86 meter
Z = 6540064.55 Z = 1993411.67
XDOT = -12640.186620 XDOT = -3852.728882
YDOT = -9706.229998 feet/sec YDOT = -2958.458903 meter/sec
ZDOT = 18331.951655 ZDOT = 5587.578865
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 08260.55964621 .00020000 00000-0 20000-3 0 9115
2 25544 51.6391 267.7280 0006601 118.3539 241.8289 15.72180452 2913
Satellite: ISS
Catalog Number: 25544
Epoch time: 08260.55964621 = yrday.fracday
Element set: 911
Inclination: 51.6391 deg
RA of node: 267.7280 deg
Eccentricity: .0006601
Arg of perigee: 118.3539 deg
Mean anomaly: 241.8289 deg
Mean motion: 15.72180452 rev/day
Decay rate: 2.00000E-04 rev/day^2
Epoch rev: 291
Checksum: 290
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