ISS TRAJECTORY DATA
Lift off time (UTC) : N/A
Area (sq ft) : 12916.69
Drag Coefficient (Cd) : 2.00
Monthly MSFC 50% solar flux (F10.7-jansky) : 72.7
Monthly MSFC 50% earth geomagnetic index (Kp) : 1.25
ET - UTC (sec) : 66.18
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 3121)
---------------------------------------
Vector Time (GMT): 2009/328/12:11:21.825
Vector Time (MET): N/A
Weight (LBS) : 731798.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1243135.65 A = 6714572.23 meter
Y = -3998519.93 meter E = .0008004
Z = 5245240.93 I = 51.49757
XDOT = 7228.621248 Wp = 30.04315
YDOT = 2657.190528 meter/sec RA = 202.07147 deg
ZDOT = 319.026735 TA = 56.96367
MA = 56.88680
Ha = 188.917 n.mi
Hp = 179.682
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4078529.05 X = 1262274.63
Y = -13118503.71 feet Y = -3984511.72 meter
Z = 17208795.70 Z = 5251326.44
XDOT = 23715.948978 XDOT = 7196.821033
YDOT = 8717.816692 feet/sec YDOT = 2737.847414 meter/sec
ZDOT = 1046.675641 ZDOT = 354.066756
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10312196.25 X = 3143157.42
Y = 9031429.02 feet Y = 2752779.56 meter
Z = 17232645.95 Z = 5252510.49
XDOT = -17057.160045 XDOT = -5199.022382
YDOT = 17256.076295 feet/sec YDOT = 5259.652055 meter/sec
ZDOT = 1185.149240 ZDOT = 361.233488
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 09328.55608418 .00016717 00000-0 10270-3 0 9006
2 25544 51.6457 202.8335 0007833 11.2964 348.8375 15.75951685 31225
Satellite: ISS
Catalog Number: 25544
Epoch time: 09328.55608418 = yrday.fracday
Element set: 900
Inclination: 51.6457 deg
RA of node: 202.8335 deg
Eccentricity: .0007833
Arg of perigee: 11.2964 deg
Mean anomaly: 348.8375 deg
Mean motion: 15.75951685 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3122
Checksum: 325
Coasting Arc #2 (Orbit 3137)
---------------------------------------
Vector Time (GMT): 2009/329/12:11:21.825
Vector Time (MET): N/A
Weight (LBS) : 731798.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6321397.76 A = 6726479.55 meter
Y = -2234164.38 meter E = .0019868
Z = 376061.70 I = 51.56599
XDOT = 1925.981027 Wp = 36.03877
YDOT = -4411.073900 meter/sec RA = 196.91376 deg
ZDOT = 6024.263692 TA = 328.06096
MA = 328.18126
Ha = 188.969 n.mi
Hp = 179.509
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20739493.95 X = -6297771.99
Y = -7329935.64 feet Y = -2304721.90 meter
Z = 1233798.22 Z = 345409.14
XDOT = 6318.835392 XDOT = 1945.898026
YDOT = -14472.027232 feet/sec YDOT = -4389.425338 meter/sec
ZDOT = 19764.644658 ZDOT = 6033.668451
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14954416.06 X = 4558106.02
Y = -16140144.36 feet Y = -4919516.00 meter
Z = 1112656.40 Z = 339137.67
XDOT = 9649.355576 XDOT = 2941.123580
YDOT = 10341.770796 feet/sec YDOT = 3152.171739 meter/sec
ZDOT = 19801.583439 ZDOT = 6035.522632
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 09329.57065440 .00016717 00000-0 10270-3 0 9012
2 25544 51.6453 197.6080 0007850 14.2944 345.8441 15.75990185 31385
Satellite: ISS
Catalog Number: 25544
Epoch time: 09329.57065440 = yrday.fracday
Element set: 901
Inclination: 51.6453 deg
RA of node: 197.6080 deg
Eccentricity: .0007850
Arg of perigee: 14.2944 deg
Mean anomaly: 345.8441 deg
Mean motion: 15.75990185 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3138
Checksum: 321
Coasting Arc #3 (Orbit 3152)
---------------------------------------
Vector Time (GMT): 2009/330/12:11:21.825
Vector Time (MET): N/A
Weight (LBS) : 731798.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2146998.88 A = 6714809.23 meter
Y = 3738631.18 meter E = .0017382
Z = -5161303.72 I = 51.55533
XDOT = -7184.398136 Wp = 72.67483
YDOT = -2471.785127 meter/sec RA = 191.74343 deg
ZDOT = 1206.522498 TA = 208.82850
MA = 208.92465
Ha = 189.028 n.mi
Hp = 179.233
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7043959.59 X = -2163572.17
Y = 12265850.32 feet Y = 3714529.69 meter
Z = -16933411.15 Z = -5171774.16
XDOT = -23570.860025 XDOT = -7162.085420
YDOT = -8109.531258 feet/sec YDOT = -2552.000595 meter/sec
ZDOT = 3958.407145 ZDOT = 1171.674113
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8699004.14 X = -2651456.46
Y = -11090511.52 feet Y = -3380387.91 meter
Z = -16974591.17 Z = -5173855.39
XDOT = 15670.404971 XDOT = 4776.339435
YDOT = -18096.899436 feet/sec YDOT = -5515.934948 meter/sec
ZDOT = 3820.675263 ZDOT = 1164.541820
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 09330.52179795 .00016717 00000-0 10270-3 0 9029
2 25544 51.6445 192.7089 0007885 17.4480 342.6953 15.76014395 31530
Satellite: ISS
Catalog Number: 25544
Epoch time: 09330.52179795 = yrday.fracday
Element set: 902
Inclination: 51.6445 deg
RA of node: 192.7089 deg
Eccentricity: .0007885
Arg of perigee: 17.4480 deg
Mean anomaly: 342.6953 deg
Mean motion: 15.76014395 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3153
Checksum: 333
Coasting Arc #4 (Orbit 3168)
---------------------------------------
Vector Time (GMT): 2009/331/12:11:21.825
Vector Time (MET): N/A
Weight (LBS) : 731798.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6153370.17 A = 6725214.82 meter
Y = 2095697.08 meter E = .0007568
Z = -1733261.65 I = 51.61960
XDOT = -3027.699885 Wp = 81.67071
YDOT = 4192.993400 meter/sec RA = 186.61584 deg
ZDOT = -5699.126147 TA = 117.51655
MA = 117.43962
Ha = 189.104 n.mi
Hp = 179.266
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20188222.33 X = 6137898.45
Y = 6875646.60 feet Y = 2164421.26 meter
Z = -5686553.96 Z = -1703405.37
XDOT = -9933.398574 XDOT = -3046.675669
YDOT = 13756.540026 feet/sec YDOT = 4159.030000 meter/sec
ZDOT = -18697.920430 ZDOT = -5713.880986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13775759.82 X = -4198851.59
Y = 16321626.12 feet Y = 4974831.64 meter
Z = -5568545.14 Z = -1697292.56
XDOT = -8036.449224 XDOT = -2449.509723
YDOT = -13159.085399 feet/sec YDOT = -4010.889230 meter/sec
ZDOT = -18756.004898 ZDOT = -5716.830293
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 09331.53633312 .00016717 00000-0 10270-3 0 9032
2 25544 51.6442 187.4842 0007776 20.9157 339.2324 15.76004948 31698
Satellite: ISS
Catalog Number: 25544
Epoch time: 09331.53633312 = yrday.fracday
Element set: 903
Inclination: 51.6442 deg
RA of node: 187.4842 deg
Eccentricity: .0007776
Arg of perigee: 20.9157 deg
Mean anomaly: 339.2324 deg
Mean motion: 15.76004948 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3169
Checksum: 314
Coasting Arc #5 (Orbit 3184)
---------------------------------------
Vector Time (GMT): 2009/332/12:11:21.825
Vector Time (MET): N/A
Weight (LBS) : 731798.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3121788.53 A = 6716564.79 meter
Y = -3643085.61 meter E = .0014678
Z = 4696566.04 I = 51.62110
XDOT = 6826.365477 Wp = 42.91885
YDOT = 2324.108888 meter/sec RA = 181.42583 deg
ZDOT = -2719.135624 TA = 73.91042
MA = 73.74886
Ha = 189.006 n.mi
Hp = 178.976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10242088.37 X = 3139478.45
Y = -11952380.60 feet Y = -3608077.26 meter
Z = 15408681.22 Z = 4711774.87
XDOT = 22396.212194 XDOT = 6813.078954
YDOT = 7625.029161 feet/sec YDOT = 2400.371190 meter/sec
ZDOT = -8921.048635 ZDOT = -2686.004394
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7663669.01 X = 2335886.31
Y = 13681305.04 feet Y = 4170061.78 meter
Z = 15468590.84 Z = 4714826.49
XDOT = -13973.864673 XDOT = -4259.233952
YDOT = 17823.333502 feet/sec YDOT = 5432.552051 meter/sec
ZDOT = -8790.086377 ZDOT = -2679.218328
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 09332.55084798 .00016717 00000-0 10270-3 0 9044
2 25544 51.6439 182.2579 0007849 23.9849 336.1680 15.76078380 31856
Satellite: ISS
Catalog Number: 25544
Epoch time: 09332.55084798 = yrday.fracday
Element set: 904
Inclination: 51.6439 deg
RA of node: 182.2579 deg
Eccentricity: .0007849
Arg of perigee: 23.9849 deg
Mean anomaly: 336.1680 deg
Mean motion: 15.76078380 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3185
Checksum: 354
Coasting Arc #6 (Orbit 3200)
---------------------------------------
Vector Time (GMT): 2009/333/12:11:21.825
Vector Time (MET): N/A
Weight (LBS) : 731798.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5684121.00 A = 6722453.08 meter
Y = -1984034.79 meter E = .0018941
Z = 2965792.47 I = 51.66953
XDOT = 4088.374491 Wp = 63.18587
YDOT = -4221.000562 meter/sec RA = 176.31969 deg
ZDOT = 4995.932816 TA = 331.10123
MA = 331.20599
Ha = 189.167 n.mi
Hp = 178.855
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18648690.94 X = -5675920.42
Y = -6509300.48 feet Y = -2047552.36 meter
Z = 9730290.26 Z = 2938197.97
XDOT = 13413.302135 XDOT = 4111.000546
YDOT = -13848.427040 feet/sec YDOT = -4175.155816 meter/sec
ZDOT = 16390.855696 ZDOT = 5015.849365
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12356699.40 X = 3766321.98
Y = -15477972.62 feet Y = -4717686.05 meter
Z = 9621203.60 Z = 2932542.86
XDOT = 7505.202015 XDOT = 2287.585574
YDOT = 16262.053742 feet/sec YDOT = 4956.673981 meter/sec
ZDOT = 16469.345658 ZDOT = 5019.856557
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 09333.56534573 .00016717 00000-0 10270-3 0 9058
2 25544 51.6424 177.0316 0007788 27.6842 332.4735 15.76101164 32013
Satellite: ISS
Catalog Number: 25544
Epoch time: 09333.56534573 = yrday.fracday
Element set: 905
Inclination: 51.6424 deg
RA of node: 177.0316 deg
Eccentricity: .0007788
Arg of perigee: 27.6842 deg
Mean anomaly: 332.4735 deg
Mean motion: 15.76101164 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3201
Checksum: 305
Coasting Arc #7 (Orbit 3215)
---------------------------------------
Vector Time (GMT): 2009/334/12:11:21.825
Vector Time (MET): N/A
Weight (LBS) : 731798.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3967609.50 A = 6719388.88 meter
Y = 3753999.17 meter E = .0011647
Z = -3919271.68 I = 51.68838
XDOT = -6139.397187 Wp = 67.36319
YDOT = -2277.498180 meter/sec RA = 171.12005 deg
ZDOT = 4047.563653 TA = 244.65003
MA = 244.77068
Ha = 189.127 n.mi
Hp = 178.587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13017091.54 X = -3990252.81
Y = 12316270.23 feet Y = 3709504.82 meter
Z = -12858502.88 Z = -3938601.51
XDOT = -20142.379224 XDOT = -6133.136419
YDOT = -7472.106890 feet/sec YDOT = -2346.117962 meter/sec
ZDOT = 13279.408309 ZDOT = 4017.752542
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7593041.99 X = -2314359.20
Y = -16171434.69 feet Y = -4929053.29 meter
Z = -12934708.90 Z = -3942499.27
XDOT = 12301.497377 XDOT = 3749.496401
YDOT = -16266.949400 feet/sec YDOT = -4958.166177 meter/sec
ZDOT = 13161.542984 ZDOT = 4011.638302
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 09334.51642119 .00016717 00000-0 10270-3 0 9061
2 25544 51.6412 172.1315 0007818 32.0982 328.0656 15.76114502 32163
Satellite: ISS
Catalog Number: 25544
Epoch time: 09334.51642119 = yrday.fracday
Element set: 906
Inclination: 51.6412 deg
RA of node: 172.1315 deg
Eccentricity: .0007818
Arg of perigee: 32.0982 deg
Mean anomaly: 328.0656 deg
Mean motion: 15.76114502 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3216
Checksum: 288
Coasting Arc #8 (Orbit 3231)
---------------------------------------
Vector Time (GMT): 2009/335/12:11:21.825
Vector Time (MET): N/A
Weight (LBS) : 731798.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4962994.20 A = 6719038.73 meter
Y = 2059204.01 meter E = .0014437
Z = -4050195.49 I = 51.71589
XDOT = -4984.155612 Wp = 53.33313
YDOT = 4392.464119 meter/sec RA = 166.02476 deg
ZDOT = -3875.273155 TA = 176.73744
MA = 176.72802
Ha = 189.218 n.mi
Hp = 178.552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16282789.37 X = 4959274.60
Y = 6755918.67 feet Y = 2114682.89 meter
Z = -13288042.94 Z = -4026093.36
XDOT = -16352.216574 XDOT = -5014.076590
YDOT = 14410.971520 feet/sec YDOT = 4336.561577 meter/sec
ZDOT = -12714.150772 ZDOT = -3899.558933
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11349203.53 X = -3459237.24
Y = 13582753.42 feet Y = 4140023.24 meter
Z = -13192730.60 Z = -4021144.29
XDOT = -7877.990373 XDOT = -2401.211466
YDOT = -19021.254016 feet/sec YDOT = -5797.678224 meter/sec
ZDOT = -12809.927436 ZDOT = -3904.465882
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 09335.53088319 .00016717 00000-0 10270-3 0 9071
2 25544 51.6403 166.9055 0007913 36.1173 324.0524 15.76148530 32324
Satellite: ISS
Catalog Number: 25544
Epoch time: 09335.53088319 = yrday.fracday
Element set: 907
Inclination: 51.6403 deg
RA of node: 166.9055 deg
Eccentricity: .0007913
Arg of perigee: 36.1173 deg
Mean anomaly: 324.0524 deg
Mean motion: 15.76148530 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3232
Checksum: 299
Coasting Arc #9 (Orbit 3247)
---------------------------------------
Vector Time (GMT): 2009/336/12:11:21.825
Vector Time (MET): N/A
Weight (LBS) : 731798.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4673664.09 A = 6722493.38 meter
Y = -3944688.60 meter E = .0018576
Z = 2780318.42 I = 51.75751
XDOT = 5175.380893 Wp = 78.33379
YDOT = 2487.683574 meter/sec RA = 160.82987 deg
ZDOT = -5137.768176 TA = 69.86791
MA = 69.66815
Ha = 189.106 n.mi
Hp = 178.315
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15333543.60 X = 4703920.35
Y = -12941891.75 feet Y = -3892256.20 meter
Z = 9121779.58 Z = 2803096.46
XDOT = 16979.596106 XDOT = 5172.137425
YDOT = 8161.691516 feet/sec YDOT = 2545.540401 meter/sec
ZDOT = -16856.194802 ZDOT = -5112.633108
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8082413.45 X = 2463519.62
Y = 18320407.85 feet Y = 5584060.31 meter
Z = 9211635.74 Z = 2807706.57
XDOT = -11329.353935 XDOT = -3453.187079
YDOT = 13476.608088 feet/sec YDOT = 4107.670145 meter/sec
ZDOT = -16756.771844 ZDOT = -5107.464058
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 09336.54532513 .00016717 00000-0 10270-3 0 9084
2 25544 51.6406 161.6784 0007809 38.2115 321.9602 15.76198983 32488
Satellite: ISS
Catalog Number: 25544
Epoch time: 09336.54532513 = yrday.fracday
Element set: 908
Inclination: 51.6406 deg
RA of node: 161.6784 deg
Eccentricity: .0007809
Arg of perigee: 38.2115 deg
Mean anomaly: 321.9602 deg
Mean motion: 15.76198983 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3248
Checksum: 326
Coasting Arc #10 (Orbit 3263)
---------------------------------------
Vector Time (GMT): 2009/337/12:11:21.825
Vector Time (MET): N/A
Weight (LBS) : 731798.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4039308.68 A = 6715933.48 meter
Y = -2342056.02 meter E = .0011764
Z = 4816594.00 I = 51.76221
XDOT = 5633.164797 Wp = 80.01476
YDOT = -4661.624003 meter/sec RA = 155.72864 deg
ZDOT = 2454.363029 TA = 346.06889
MA = 346.10132
Ha = 189.387 n.mi
Hp = 178.210
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13252325.08 X = -4036217.69
Y = -7683910.83 feet Y = -2387209.46 meter
Z = 15802473.77 Z = 4796977.86
XDOT = 18481.511801 XDOT = 5672.950187
YDOT = -15294.042005 feet/sec YDOT = -4598.408583 meter/sec
ZDOT = 8052.372144 ZDOT = 2481.825244
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10965060.94 X = 3342150.57
Y = -10811158.83 feet Y = -3295241.21 meter
Z = 15724855.04 Z = 4792935.82
XDOT = 9033.467955 XDOT = 2753.401033
YDOT = 21046.439943 feet/sec YDOT = 6414.954894 meter/sec
ZDOT = 8160.732182 ZDOT = 2487.391169
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 09337.55975235 .00016717 00000-0 10270-3 0 9099
2 25544 51.6398 156.4513 0007882 43.4696 316.7089 15.76178130 32644
Satellite: ISS
Catalog Number: 25544
Epoch time: 09337.55975235 = yrday.fracday
Element set: 909
Inclination: 51.6398 deg
RA of node: 156.4513 deg
Eccentricity: .0007882
Arg of perigee: 43.4696 deg
Mean anomaly: 316.7089 deg
Mean motion: 15.76178130 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3264
Checksum: 347
Coasting Arc #11 (Orbit 3278)
---------------------------------------
Vector Time (GMT): 2009/338/12:11:21.825
Vector Time (MET): N/A
Weight (LBS) : 731798.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5068277.99 A = 6724905.10 meter
Y = 4167523.39 meter E = .0016188
Z = -1446590.80 I = 51.82059
XDOT = -4081.612409 Wp = 42.88503
YDOT = -2958.129364 meter/sec RA = 150.55341 deg
ZDOT = 5827.691800 TA = 301.21975
MA = 301.37829
Ha = 189.226 n.mi
Hp = 178.016
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16628208.62 X = -5107475.94
Y = 13672976.99 feet Y = 4110627.97 meter
Z = -4746032.80 Z = -1471307.27
XDOT = -13391.116829 XDOT = -4076.540848
YDOT = -9705.148833 feet/sec YDOT = -3003.744914 meter/sec
ZDOT = 19119.723752 ZDOT = 5807.875009
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9085482.83 X = -2769255.17
Y = -19492721.88 feet Y = -5941381.63 meter
Z = -4843577.67 Z = -1476322.47
XDOT = 11352.512697 XDOT = 3460.245870
YDOT = -9983.220238 feet/sec YDOT = -3042.885529 meter/sec
ZDOT = 19041.277175 ZDOT = 5803.781283
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 09338.51075874 .00016717 00000-0 10270-3 0 9108
2 25544 51.6404 151.5510 0007838 48.2358 311.9475 15.76221975 32792
Satellite: ISS
Catalog Number: 25544
Epoch time: 09338.51075874 = yrday.fracday
Element set: 910
Inclination: 51.6404 deg
RA of node: 151.5510 deg
Eccentricity: .0007838
Arg of perigee: 48.2358 deg
Mean anomaly: 311.9475 deg
Mean motion: 15.76221975 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3279
Checksum: 324
Coasting Arc #12 (Orbit 3294)
---------------------------------------
Vector Time (GMT): 2009/339/12:11:21.825
Vector Time (MET): N/A
Weight (LBS) : 731798.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3061761.45 A = 6713896.85 meter
Y = 2899259.49 meter E = .0021923
Z = -5243240.44 I = 51.80990
XDOT = -5927.345313 Wp = 73.22142
YDOT = 4833.581988 meter/sec RA = 145.43476 deg
ZDOT = -785.001743 TA = 189.29415
MA = 189.33479
Ha = 189.300 n.mi
Hp = 177.903
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10045149.12 X = 3054584.68
Y = 9512006.21 feet Y = 2933458.50 meter
Z = -17202232.42 Z = -5228383.38
XDOT = -19446.670973 XDOT = -5977.141326
YDOT = 15858.208621 feet/sec YDOT = 4767.020598 meter/sec
ZDOT = -2575.465036 ZDOT = -813.917201
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11617401.14 X = -3540983.87
Y = 7644632.45 feet Y = 2330083.97 meter
Z = -17143385.57 Z = -5225303.92
XDOT = -10325.909111 XDOT = -3147.337097
YDOT = -21749.465790 feet/sec YDOT = -6629.237173 meter/sec
ZDOT = -2689.600642 ZDOT = -819.790276
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 09339.52514853 .00016717 00000-0 10270-3 0 9116
2 25544 51.6410 146.3250 0007955 52.7034 307.4855 15.76260136 32955
Satellite: ISS
Catalog Number: 25544
Epoch time: 09339.52514853 = yrday.fracday
Element set: 911
Inclination: 51.6410 deg
RA of node: 146.3250 deg
Eccentricity: .0007955
Arg of perigee: 52.7034 deg
Mean anomaly: 307.4855 deg
Mean motion: 15.76260136 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3295
Checksum: 305
Coasting Arc #13 (Orbit 3310)
---------------------------------------
Vector Time (GMT): 2009/340/12:11:21.825
Vector Time (MET): N/A
Weight (LBS) : 731798.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5221838.09 A = 6725572.76 meter
Y = -4233334.25 meter E = .0015532
Z = -101492.93 I = 51.87400
XDOT = 2932.628094 Wp = 105.15222
YDOT = 3744.214164 meter/sec RA = 140.28944 deg
ZDOT = -6057.389181 TA = 75.94738
MA = 75.77478
Ha = 189.244 n.mi
Hp = 177.692
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17132014.75 X = 5269280.91
Y = -13888891.91 feet Y = -4174675.30 meter
Z = -332982.04 Z = -76010.41
XDOT = 9621.483248 XDOT = 2919.967429
YDOT = 12284.167204 feet/sec YDOT = 3776.938416 meter/sec
ZDOT = -19873.324085 ZDOT = -6043.172788
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9845896.82 X = 3001029.35
Y = 19736322.82 feet Y = 6015631.20 meter
Z = -232383.35 Z = -70830.44
XDOT = -12662.795178 XDOT = -3859.619970
YDOT = 6126.309551 feet/sec YDOT = 1867.299151 meter/sec
ZDOT = -19816.971438 ZDOT = -6040.212894
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 09340.53951804 .00016717 00000-0 10270-3 0 9121
2 25544 51.6410 141.0973 0007982 54.3943 305.7964 15.76321506 33116
Satellite: ISS
Catalog Number: 25544
Epoch time: 09340.53951804 = yrday.fracday
Element set: 912
Inclination: 51.6410 deg
RA of node: 141.0973 deg
Eccentricity: .0007982
Arg of perigee: 54.3943 deg
Mean anomaly: 305.7964 deg
Mean motion: 15.76321506 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3311
Checksum: 301
Coasting Arc #14 (Orbit 3326)
---------------------------------------
Vector Time (GMT): 2009/341/12:11:21.825
Vector Time (MET): N/A
Weight (LBS) : 731798.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2099529.10 A = 6713943.88 meter
Y = -3675733.71 meter E = .0011552
Z = 5203651.12 I = 51.85692
XDOT = 5943.534611 Wp = 59.66735
YDOT = -4812.566546 meter/sec RA = 135.14346 deg
ZDOT = -994.083506 TA = 39.80823
MA = 39.72354
Ha = 189.467 n.mi
Hp = 177.648
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6888218.84 X = -2083548.82
Y = -12059493.81 feet Y = -3699122.98 meter
Z = 17072346.20 Z = 5193490.08
XDOT = 19499.785470 XDOT = 6001.736925
YDOT = -15789.260320 feet/sec YDOT = -4745.776923 meter/sec
ZDOT = -3261.428827 ZDOT = -965.068773
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13212508.56 X = 4027172.61
Y = -4436620.62 feet Y = -1352281.96 meter
Z = 17032027.76 Z = 5191362.06
XDOT = 11245.805542 XDOT = 3427.721529
YDOT = 21317.172851 feet/sec YDOT = 6497.474285 meter/sec
ZDOT = -3146.873566 ZDOT = -959.167063
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 09341.55387333 .00016717 00000-0 10270-3 0 9135
2 25544 51.6412 135.8705 0008038 60.2666 299.9298 15.76265361 33270
Satellite: ISS
Catalog Number: 25544
Epoch time: 09341.55387333 = yrday.fracday
Element set: 913
Inclination: 51.6412 deg
RA of node: 135.8705 deg
Eccentricity: .0008038
Arg of perigee: 60.2666 deg
Mean anomaly: 299.9298 deg
Mean motion: 15.76265361 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3327
Checksum: 329
Coasting Arc #15 (Orbit 3342)
---------------------------------------
Vector Time (GMT): 2009/342/12:11:21.825
Vector Time (MET): N/A
Weight (LBS) : 731798.0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5081294.35 A = 6724384.53 meter
Y = 4080220.04 meter E = .0022008
Z = 1615760.09 I = 51.91457
XDOT = -1941.880777 Wp = 63.58589
YDOT = -4725.462120 meter/sec RA = 130.03162 deg
ZDOT = 5775.684920 TA = 314.21743
MA = 314.39797
Ha = 189.272 n.mi
Hp = 177.510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16670913.23 X = -5134391.55
Y = 13386548.69 feet Y = 4023101.01 meter
Z = 5301050.15 Z = 1590946.32
XDOT = -6370.999923 XDOT = -1916.952894
YDOT = -15503.484646 feet/sec YDOT = -4747.038394 meter/sec
ZDOT = 18949.097507 ZDOT = 5766.311437
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10104265.30 X = -3079780.06
Y = -18869341.46 feet Y = -5751375.28 meter
Z = 5203070.47 Z = 1585895.88
XDOT = 15051.417894 XDOT = 4587.672174
YDOT = -2798.516573 feet/sec YDOT = -852.987851 meter/sec
ZDOT = 18911.853364 ZDOT = 5764.332905
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 09342.56820488 .00016717 00000-0 10270-3 0 9141
2 25544 51.6424 130.6440 0007895 64.2128 295.9850 15.76359037 33431
Satellite: ISS
Catalog Number: 25544
Epoch time: 09342.56820488 = yrday.fracday
Element set: 914
Inclination: 51.6424 deg
RA of node: 130.6440 deg
Eccentricity: .0007895
Arg of perigee: 64.2128 deg
Mean anomaly: 295.9850 deg
Mean motion: 15.76359037 rev/day
Decay rate: 1.67170E-04 rev/day^2
Epoch rev: 3343
Checksum: 326
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