Date:
March 25th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5812 51 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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 3723)
---------------------------------------
Vector Time (GMT): 2007/082/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3060429
60 A = 6711095
19 meter
Y = -3528420
74 meter E =
0017558
Z = 4824531
23 I = 51
58619
XDOT = 6833
149592 Wp = 3
73979
YDOT = 2622
438410 meter/sec RA = 185
93101 deg
ZDOT = -2398
948233 TA = 109
77721
MA = 109
58779
Ha = 187
284 n
mi
Hp = 176
793
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10040779
53 X = 3076220
71
Y = -11576183
54 feet Y = -3494108
94 meter
Z = 15828514
53 Z = 4839437
23
XDOT = 22418
469789 XDOT = 6814
970932
YDOT = 8603
800559 feet/sec YDOT = 2698
748834 meter/sec
ZDOT = -7870
565068 ZDOT = -2365
796929
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12635907
88 X = 3851424
72
Y = -8567226
59 feet Y = -2611290
67 meter
Z = 15884067
85 Z = 4841463
88
XDOT = 18801
533582 XDOT = 5730
707436
YDOT = 13262
576493 feet/sec YDOT = 4042
433315 meter/sec
ZDOT = -7745
532496 ZDOT = -2360
838305
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 07082
50181021
00020000 00000-0 20000-3 0 9004
2 25544 51
6334 186
7098 0014767 341
0568 19
0046 15
77822401 37248
Satellite: ISS
Catalog Number: 25544
Epoch time: 07082
50181021 = yrday
fracday
Element set: 900
Inclination: 51
6334 deg
RA of node: 186
7098 deg
Eccentricity:
0014767
Arg of perigee: 341
0568 deg
Mean anomaly: 19
0046 deg
Mean motion: 15
77822401 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3724
Checksum: 274
Coasting Arc #2 (Orbit 3739)
---------------------------------------
Vector Time (GMT): 2007/083/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5280707
63 A = 6716685
37 meter
Y = -2610122
28 meter E =
0017526
Z = 3202842
26 I = 51
63463
XDOT = 4753
381816 Wp = 31
24638
YDOT = -3732
113892 meter/sec RA = 180
80804 deg
ZDOT = 4798
819160 TA = 6
28771
MA = 6
26575
Ha = 187
444 n
mi
Hp = 176
478
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17325156
28 X = -5266687
19
Y = -8563393
31 feet Y = -2669095
71 meter
Z = 10508012
65 Z = 3177222
69
XDOT = 15595
084699 XDOT = 4771
449826
YDOT = -12244
468148 feet/sec YDOT = -3678
857895 meter/sec
ZDOT = 15744
157349 ZDOT = 4821
954922
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14753693
20 X = -4496925
69
Y = -12563620
67 feet Y = -3829391
58 meter
Z = 10411294
23 Z = 3173362
48
XDOT = 17119
532771 XDOT = 5218
033588
YDOT = -6993
651927 feet/sec YDOT = -2131
665107 meter/sec
ZDOT = 15830
641449 ZDOT = 4825
179514
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 07083
51515448
00020000 00000-0 20000-3 0 9011
2 25544 51
6337 181
4750 0014799 344
6710 15
4005 15
77903996 37403
Satellite: ISS
Catalog Number: 25544
Epoch time: 07083
51515448 = yrday
fracday
Element set: 901
Inclination: 51
6337 deg
RA of node: 181
4750 deg
Eccentricity:
0014799
Arg of perigee: 344
6710 deg
Mean anomaly: 15
4005 deg
Mean motion: 15
77903996 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3740
Checksum: 296
Coasting Arc #3 (Orbit 3754)
---------------------------------------
Vector Time (GMT): 2007/084/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5044228
26 A = 6716381
02 meter
Y = 2981057
26 meter E =
0015121
Z = -3268358
50 I = 51
66246
XDOT = -5057
402717 Wp = 6
51781
YDOT = -3373
812046 meter/sec RA = 175
59335 deg
ZDOT = 4744
995559 TA = 315
08803
MA = 315
21027
Ha = 187
557 n
mi
Hp = 176
172
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16549305
31 X = -5061310
99
Y = 9780371
58 feet Y = 2924554
37 meter
Z = -10722960
96 Z = -3292904
68
XDOT = -16592
528599 XDOT = -5042
350560
YDOT = -11068
937158 feet/sec YDOT = -3430
282603 meter/sec
ZDOT = 15567
570732 ZDOT = 4720
463421
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18287518
69 X = -5574035
70
Y = 5755203
72 feet Y = 1754186
09 meter
Z = -10814867
40 Z = -3296371
58
XDOT = -13289
781178 XDOT = -4050
725303
YDOT = -13252
859314 feet/sec YDOT = -4039
471519 meter/sec
ZDOT = 15474
823696 ZDOT = 4716
726262
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 07084
46514806
00020000 00000-0 20000-3 0 9024
2 25544 51
6337 176
5684 0015051 348
0832 11
9975 15
77885118 37557
Satellite: ISS
Catalog Number: 25544
Epoch time: 07084
46514806 = yrday
fracday
Element set: 902
Inclination: 51
6337 deg
RA of node: 176
5684 deg
Eccentricity:
0015051
Arg of perigee: 348
0832 deg
Mean anomaly: 11
9975 deg
Mean motion: 15
77885118 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3755
Checksum: 313
Coasting Arc #4 (Orbit 3770)
---------------------------------------
Vector Time (GMT): 2007/085/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3326926
22 A = 6710998
24 meter
Y = 3302930
51 meter E =
0020605
Z = -4817006
61 I = 51
67308
XDOT = -6615
863241 Wp = 26
81969
YDOT = 3072
665183 meter/sec RA = 170
47519 deg
ZDOT = -2448
462783 TA = 219
17521
MA = 219
32455
Ha = 187
724 n
mi
Hp = 175
982
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10915112
26 X = 3313144
99
Y = 10836386
20 feet Y = 3340056
98 meter
Z = -15803827
45 Z = -4800878
07
XDOT = -21705
588061 XDOT = -6637
836465
YDOT = 10080
922517 feet/sec YDOT = 2998
560028 meter/sec
ZDOT = -8033
014381 ZDOT = -2480
655674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8460135
01 X = 2578649
15
Y = 12919817
67 feet Y = 3937960
42 meter
Z = -15742691
34 Z = -4798372
32
XDOT = -22361
323147 XDOT = -6815
731295
YDOT = 4651
234354 feet/sec YDOT = 1417
696231 meter/sec
ZDOT = -8153
683693 ZDOT = -2485
242790
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 07085
47845282
00020000 00000-0 20000-3 0 9032
2 25544 51
6339 171
3338 0014973 352
0823 8
0104 15
77927360 37710
Satellite: ISS
Catalog Number: 25544
Epoch time: 07085
47845282 = yrday
fracday
Element set: 903
Inclination: 51
6339 deg
RA of node: 171
3338 deg
Eccentricity:
0014973
Arg of perigee: 352
0823 deg
Mean anomaly: 8
0104 deg
Mean motion: 15
77927360 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3771
Checksum: 294
Coasting Arc #5 (Orbit 3786)
---------------------------------------
Vector Time (GMT): 2007/086/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6248583
66 A = 6720560
75 meter
Y = -2333776
36 meter E =
0012363
Z = 849574
98 I = 51
73369
XDOT = 2401
108952 Wp = 55
70814
YDOT = 4233
045163 meter/sec RA = 165
28605 deg
ZDOT = -5963
619560 TA = 115
03130
MA = 114
90289
Ha = 187
822 n
mi
Hp = 175
562
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20500602
55 X = 6270088
85
Y = -7656746
58 feet Y = -2263780
94 meter
Z = 2787319
50 Z = 879982
46
XDOT = 7877
654042 XDOT = 2382
565752
YDOT = 13887
943449 feet/sec YDOT = 4259
791897 meter/sec
ZDOT = -19565
680971 ZDOT = -5952
000272
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21583899
86 X = 6578772
68
Y = -3519493
98 feet Y = -1072741
77 meter
Z = 2901387
93 Z = 884343
04
XDOT = 4871
339878 XDOT = 1484
784395
YDOT = 13603
960315 feet/sec YDOT = 4146
487104 meter/sec
ZDOT = -19521
370519 ZDOT = -5950
113734
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 07086
49173646
00020000 00000-0 20000-3 0 9044
2 25544 51
6335 166
0990 0015008 356
5917 3
5144 15
77968657 37879
Satellite: ISS
Catalog Number: 25544
Epoch time: 07086
49173646 = yrday
fracday
Element set: 904
Inclination: 51
6335 deg
RA of node: 166
0990 deg
Eccentricity:
0015008
Arg of perigee: 356
5917 deg
Mean anomaly: 3
5144 deg
Mean motion: 15
77968657 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3787
Checksum: 325
Coasting Arc #6 (Orbit 3802)
---------------------------------------
Vector Time (GMT): 2007/087/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -811369
55 A = 6708680
94 meter
Y = -4105500
09 meter E =
0016406
Z = 5242402
45 I = 51
72254
XDOT = 7369
249885 Wp = 9
26299
YDOT = -2192
917856 meter/sec RA = 160
12943 deg
ZDOT = -560
659683 TA = 86
14654
MA = 85
95898
Ha = 187
880 n
mi
Hp = 175
225
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2661973
60 X = -790867
21
Y = -13469488
49 feet Y = -4114458
42 meter
Z = 17199483
09 Z = 5238510
85
XDOT = 24177
329018 XDOT = 7395
947254
YDOT = -7194
612388 feet/sec YDOT = -2110
361531 meter/sec
ZDOT = -1839
434656 ZDOT = -524
795480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -317395
05 X = -96742
01
Y = -13745395
61 feet Y = -4189596
58 meter
Z = 17184260
30 Z = 5237762
54
XDOT = 24078
987657 XDOT = 7339
275438
YDOT = -2753
605508 feet/sec YDOT = -839
298959 meter/sec
ZDOT = -1704
806207 ZDOT = -519
624932
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 07087
50499688
00020000 00000-0 20000-3 0 9055
2 25544 51
6343 160
8632 0015149
1059
0107 15
78046928 38037
Satellite: ISS
Catalog Number: 25544
Epoch time: 07087
50499688 = yrday
fracday
Element set: 905
Inclination: 51
6343 deg
RA of node: 160
8632 deg
Eccentricity:
0015149
Arg of perigee:
1059 deg
Mean anomaly:
0107 deg
Mean motion: 15
78046928 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3803
Checksum: 284
Coasting Arc #7 (Orbit 3818)
---------------------------------------
Vector Time (GMT): 2007/088/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6308476
85 A = 6719378
30 meter
Y = 1385846
64 meter E =
0025352
Z = 1791842
50 I = 51
78484
XDOT = 486
581239 Wp = 33
88996
YDOT = -5181
810338 meter/sec RA = 154
99332 deg
ZDOT = 5703
135780 TA = 346
00164
MA = 346
07179
Ha = 188
124 n
mi
Hp = 174
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20697102
52 X = -6332209
05
Y = 4546740
96 feet Y = 1315169
14 meter
Z = 5878748
37 Z = 1761138
63
XDOT = 1596
395140 XDOT = 516
784416
YDOT = -17000
690086 feet/sec YDOT = -5176
199882 meter/sec
ZDOT = 18711
075393 ZDOT = 5705
573245
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21191060
78 X = -6459035
33
Y = 1150909
31 feet Y = 350797
16 meter
Z = 5763413
88 Z = 1756688
55
XDOT = 4292
970936 XDOT = 1308
497541
YDOT = -14993
771003 feet/sec YDOT = -4570
101402 meter/sec
ZDOT = 18719
511927 ZDOT = 5705
707235
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 07088
51823916
00020000 00000-0 20000-3 0 9063
2 25544 51
6341 155
6287 0015235 4
5693 355
5608 15
78037695 38193
Satellite: ISS
Catalog Number: 25544
Epoch time: 07088
51823916 = yrday
fracday
Element set: 906
Inclination: 51
6341 deg
RA of node: 155
6287 deg
Eccentricity:
0015235
Arg of perigee: 4
5693 deg
Mean anomaly: 355
5608 deg
Mean motion: 15
78037695 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3819
Checksum: 318
Coasting Arc #8 (Orbit 3833)
---------------------------------------
Vector Time (GMT): 2007/089/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1572919
50 A = 6712253
00 meter
Y = 4872060
09 meter E =
0016012
Z = -4343122
87 I = 51
78632
XDOT = -6840
114807 Wp = 42
40546
YDOT = 844
553994 meter/sec RA = 149
79687 deg
ZDOT = 3443
544546 TA = 262
17415
MA = 262
35595
Ha = 188
110 n
mi
Hp = 174
557
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5160497
04 X = -1606184
81
Y = 15984449
12 feet Y = 4854284
48 meter
Z = -14249090
78 Z = -4350845
21
XDOT = -22441
321546 XDOT = -6865
778289
YDOT = 2770
846436 feet/sec YDOT = 767
920781 meter/sec
ZDOT = 11297
718326 ZDOT = 3410
253249
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7329151
47 X = -2233925
37
Y = 15086672
23 feet Y = 4598417
69 meter
Z = -14277457
45 Z = -4351769
03
XDOT = -21568
234906 XDOT = -6573
997999
YDOT = 36
825274 feet/sec YDOT = 11
224344 meter/sec
ZDOT = 11172
564769 ZDOT = 3405
397742
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 07089
46813299
00020000 00000-0 20000-3 0 9072
2 25544 51
6333 150
7213 0015271 8
4299 351
7119 15
78098862 38349
Satellite: ISS
Catalog Number: 25544
Epoch time: 07089
46813299 = yrday
fracday
Element set: 907
Inclination: 51
6333 deg
RA of node: 150
7213 deg
Eccentricity:
0015271
Arg of perigee: 8
4299 deg
Mean anomaly: 351
7119 deg
Mean motion: 15
78098862 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3834
Checksum: 313
Coasting Arc #9 (Orbit 3849)
---------------------------------------
Vector Time (GMT): 2007/090/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5384134
55 A = 6713591
81 meter
Y = 71631
44 meter E =
0019900
Z = -4030853
44 I = 51
81396
XDOT = -3010
962891 Wp = 30
44994
YDOT = 5899
725052 meter/sec RA = 144
69138 deg
ZDOT = -3908
565765 TA = 199
22901
MA = 199
30422
Ha = 188
261 n
mi
Hp = 174
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17664483
44 X = 5402514
42
Y = 235011
29 feet Y = 131942
26 meter
Z = -13224584
77 Z = -4004652
87
XDOT = -9878
487175 XDOT = -3057
723714
YDOT = 19356
053320 feet/sec YDOT = 5865
792981 meter/sec
ZDOT = -12823
378493 ZDOT = -3923
307017
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17564610
63 X = 5353693
32
Y = 2484344
51 feet Y = 757228
21 meter
Z = -13125979
34 Z = -4000798
50
XDOT = -12002
927936 XDOT = -3658
492435
YDOT = 16674
253546 feet/sec YDOT = 5082
312481 meter/sec
ZDOT = -12878
013496 ZDOT = -3925
218514
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 07090
48133311
00020000 00000-0 20000-3 0 9087
2 25544 51
6326 145
4853 0015303 12
1647 347
9885 15
78092013 38504
Satellite: ISS
Catalog Number: 25544
Epoch time: 07090
48133311 = yrday
fracday
Element set: 908
Inclination: 51
6326 deg
RA of node: 145
4853 deg
Eccentricity:
0015303
Arg of perigee: 12
1647 deg
Mean anomaly: 347
9885 deg
Mean motion: 15
78092013 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3850
Checksum: 283
Coasting Arc #10 (Orbit 3865)
---------------------------------------
Vector Time (GMT): 2007/091/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3492120
93 A = 6718127
74 meter
Y = -5289136
34 meter E =
0020535
Z = 2232004
24 I = 51
85318
XDOT = 5281
988727 Wp = 59
17909
YDOT = 1152
990201 meter/sec RA = 139
49174 deg
ZDOT = -5484
435394 TA = 95
83633
MA = 95
60219
Ha = 188
324 n
mi
Hp = 173
973
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11457089
67 X = 3540162
62
Y = -17352809
52 feet Y = -5249816
67 meter
Z = 7322848
56 Z = 2249086
09
XDOT = 17329
359341 XDOT = 5295
345596
YDOT = 3782
776250 feet/sec YDOT = 1212
130549 meter/sec
ZDOT = -17993
554443 ZDOT = -5458
743213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13252899
16 X = 4039483
66
Y = -15994093
70 feet Y = -4874999
76 meter
Z = 7386382
29 Z = 2251369
32
XDOT = 15742
100458 XDOT = 4798
192220
YDOT = 4707
888042 feet/sec YDOT = 1434
964275 meter/sec
ZDOT = -17896
706162 ZDOT = -5454
916038
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 07091
49451030
00020000 00000-0 20000-3 0 9091
2 25544 51
6329 140
2492 0015552 15
8807 344
2843 15
78170507 38669
Satellite: ISS
Catalog Number: 25544
Epoch time: 07091
49451030 = yrday
fracday
Element set: 909
Inclination: 51
6329 deg
RA of node: 140
2492 deg
Eccentricity:
0015552
Arg of perigee: 15
8807 deg
Mean anomaly: 344
2843 deg
Mean motion: 15
78170507 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3866
Checksum: 292
Coasting Arc #11 (Orbit 3881)
---------------------------------------
Vector Time (GMT): 2007/092/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3720371
20 A = 6708553
06 meter
Y = -2029982
04 meter E =
0014994
Z = 5191255
14 I = 51
84137
XDOT = 4725
971916 Wp = 33
97332
YDOT = -6008
951858 meter/sec RA = 134
36805 deg
ZDOT = 1047
946069 TA = 46
14256
MA = 46
01877
Ha = 188
476 n
mi
Hp = 173
782
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12205942
25 X = -3722613
39
Y = -6660046
05 feet Y = -2071597
41 meter
Z = 17031676
98 Z = 5173176
26
XDOT = 15505
157205 XDOT = 4787
722889
YDOT = -19714
408983 feet/sec YDOT = -5955
758039 meter/sec
ZDOT = 3438
143270 ZDOT = 1071
055395
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11630142
73 X = -3544867
51
Y = -7771977
57 feet Y = -2368898
76 meter
Z = 16963354
77 Z = 5170430
53
XDOT = 16680
143764 XDOT = 5084
107819
YDOT = -17345
683543 feet/sec YDOT = -5286
964344 meter/sec
ZDOT = 3524
264737 ZDOT = 1074
195892
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 07092
50766676
00020000 00000-0 20000-3 0 9101
2 25544 51
6323 135
0131 0015453 19
8836 340
2928 15
78189021 38820
Satellite: ISS
Catalog Number: 25544
Epoch time: 07092
50766676 = yrday
fracday
Element set: 910
Inclination: 51
6323 deg
RA of node: 135
0131 deg
Eccentricity:
0015453
Arg of perigee: 19
8836 deg
Mean anomaly: 340
2928 deg
Mean motion: 15
78189021 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3882
Checksum: 293
Coasting Arc #12 (Orbit 3897)
---------------------------------------
Vector Time (GMT): 2007/093/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4507582
11 A = 6720315
14 meter
Y = 4939968
88 meter E =
0028181
Z = 471228
74 I = 51
89918
XDOT = -3232
838817 Wp = 35
73734
YDOT = -3542
003826 meter/sec RA = 129
21218 deg
ZDOT = 6050
157444 TA = 329
38732
MA = 329
55147
Ha = 188
675 n
mi
Hp = 173
500
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14788655
22 X = -4564775
70
Y = 16207246
99 feet Y = 4889242
82 meter
Z = 1546026
05 Z = 449191
48
XDOT = -10606
426564 XDOT = -3222
382134
YDOT = -11620
747460 feet/sec YDOT = -3578
096343 meter/sec
ZDOT = 19849
597914 ZDOT = 6034
477853
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15979565
49 X = -4870571
56
Y = 15042613
06 feet Y = 4584988
46 meter
Z = 1463780
64 Z = 446160
34
XDOT = -8711
020263 XDOT = -2655
118976
YDOT = -11232
371528 feet/sec YDOT = -3423
626842 meter/sec
ZDOT = 19790
094286 ZDOT = 6032
020738
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 07093
52080465
00020000 00000-0 20000-3 0 9110
2 25544 51
6317 129
7767 0015818 24
0490 336
1410 15
78154840 38985
Satellite: ISS
Catalog Number: 25544
Epoch time: 07093
52080465 = yrday
fracday
Element set: 911
Inclination: 51
6317 deg
RA of node: 129
7767 deg
Eccentricity:
0015818
Arg of perigee: 24
0490 deg
Mean anomaly: 336
1410 deg
Mean motion: 15
78154840 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3898
Checksum: 297
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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