Date:
March 20th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9472 24 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
080/02:40:34
719 0
0 0
6 0
6
N/A -0
5 -0
0 186
6
000/00:05:09
439 0
3 -0
1 180
6
Coasting Arc #1 (Orbit 1404)
---------------------------------------
Vector Time (GMT): 2008/077/09:07:03
812
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5258533
35 A = 6722664
35 meter
Y = 3235494
26 meter E =
0012587
Z = 2645106
30 I = 51
90312
XDOT = -789
259210 Wp = 77
44187
YDOT = -5588
104263 meter/sec RA = 128
77050 deg
ZDOT = 5248
182094 TA = 312
58440
MA = 312
69053
Ha = 186
212 n
mi
Hp = 180
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17252406
01 X = -5307171
51
Y = 10615138
64 feet Y = 3176418
50 meter
Z = 8678170
28 Z = 2619442
59
XDOT = -2589
433105 XDOT = -752
207702
YDOT = -18333
675404 feet/sec YDOT = -5596
722820 meter/sec
ZDOT = 17218
445190 ZDOT = 5244
438187
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19397149
72 X = -5912251
24
Y = -5980712
53 feet Y = -1822921
18 meter
Z = 8580150
43 Z = 2615229
85
XDOT = 11555
698512 XDOT = 3522
176906
YDOT = -12711
471112 feet/sec YDOT = -3874
456395 meter/sec
ZDOT = 17203
428446 ZDOT = 5243
604990
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 08077
43806303
00020000 00000-0 20000-3 0 9008
2 25544 51
6394 129
3546 0001171 259
8037 100
2995 15
76300411 14058
Satellite: ISS
Catalog Number: 25544
Epoch time: 08077
43806303 = yrday
fracday
Element set: 900
Inclination: 51
6394 deg
RA of node: 129
3546 deg
Eccentricity:
0001171
Arg of perigee: 259
8037 deg
Mean anomaly: 100
2995 deg
Mean motion: 15
76300411 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1405
Checksum: 268
Coasting Arc #2 (Orbit 1419)
---------------------------------------
Vector Time (GMT): 2008/078/09:07:03
812
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 382610
93 A = 6718073
45 meter
Y = 5285381
82 meter E =
0006795
Z = -4136451
77 I = 51
90522
XDOT = -5796
249952 Wp = 113
99080
YDOT = 3374
445223 meter/sec RA = 123
58925 deg
ZDOT = 3777
725345 TA = 194
57820
MA = 194
59780
Ha = 186
085 n
mi
Hp = 180
610
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1255285
21 X = 343574
27
Y = 17340491
53 feet Y = 5289441
84 meter
Z = -13571035
99 Z = -4134688
26
XDOT = -19016
568084 XDOT = -5851
903876
YDOT = 11071
014510 feet/sec YDOT = 3309
317328 meter/sec
ZDOT = 12394
112025 ZDOT = 3749
432316
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11924822
77 X = -3634685
98
Y = 12659679
09 feet Y = 3858670
19 meter
Z = -13563647
46 Z = -4134199
74
XDOT = -20112
977606 XDOT = -6130
435574
YDOT = -5789
702253 feet/sec YDOT = -1764
701247 meter/sec
ZDOT = 12286
020053 ZDOT = 3744
778912
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 08078
38901334
00020000 00000-0 20000-3 0 9014
2 25544 51
6392 124
4552 0001161 265
8306 94
2725 15
76341814 14206
Satellite: ISS
Catalog Number: 25544
Epoch time: 08078
38901334 = yrday
fracday
Element set: 901
Inclination: 51
6392 deg
RA of node: 124
4552 deg
Eccentricity:
0001161
Arg of perigee: 265
8306 deg
Mean anomaly: 94
2725 deg
Mean motion: 15
76341814 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1420
Checksum: 272
Coasting Arc #3 (Orbit 1435)
---------------------------------------
Vector Time (GMT): 2008/079/09:07:03
812
Vector Time (MET): N/A
Weight (LBS) : 567227
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4853153
64 A = 6719032
06 meter
Y = -2554585
72 meter E =
0005385
Z = -3887301
38 I = 51
92255
XDOT = 132
945468 Wp = 70
38235
YDOT = 6506
456081 meter/sec RA = 118
50663 deg
ZDOT = -4112
631553 TA = 156
89146
MA = 156
86723
Ha = 186
095 n
mi
Hp = 180
699
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15922420
09 X = 4900242
21
Y = -8381186
76 feet Y = -2500052
05 meter
Z = -12753613
45 Z = -3863610
56
XDOT = 436
172794 XDOT = 80
157466
YDOT = 21346
640686 feet/sec YDOT = 6507
647229 meter/sec
ZDOT = -13492
885671 ZDOT = -4112
114521
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17069366
75 X = 5202742
99
Y = 5891166
34 feet Y = 1795627
50 meter
Z = -12663067
83 Z = -3859703
07
XDOT = -14753
167396 XDOT = -4496
765422
YDOT = 13769
524436 feet/sec YDOT = 4196
951048 meter/sec
ZDOT = -13490
132148 ZDOT = -4111
792279
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 08079
40333919
00020000 00000-0 20000-3 0 9027
2 25544 51
6384 119
2279 0001183 271
9495 88
1534 15
76341091 14360
Satellite: ISS
Catalog Number: 25544
Epoch time: 08079
40333919 = yrday
fracday
Element set: 902
Inclination: 51
6384 deg
RA of node: 119
2279 deg
Eccentricity:
0001183
Arg of perigee: 271
9495 deg
Mean anomaly: 88
1534 deg
Mean motion: 15
76341091 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1436
Checksum: 299
Coasting Arc #4 (Orbit 1447)
---------------------------------------
Vector Time (GMT): 2008/080/02:43:09
439
Vector Time (MET): N/A
Weight (LBS) : 567143
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4445769
83 A = 6714889
06 meter
Y = 240876
77 meter E =
0004752
Z = 5023908
01 I = 51
91353
XDOT = 1730
355401 Wp = 122
59293
YDOT = -7272
042213 meter/sec RA = 114
72847 deg
ZDOT = 1876
114564 TA = 309
36985
MA = 309
41194
Ha = 186
583 n
mi
Hp = 180
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14585859
03 X = -4472537
84
Y = 790278
12 feet Y = 191012
47 meter
Z = 16482637
83 Z = 5002245
72
XDOT = 5677
019032 XDOT = 1802
430203
YDOT = -23858
406209 feet/sec YDOT = -7252
289209 meter/sec
ZDOT = 6155
231509 ZDOT = 1884
696316
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11072294
82 X = 3374835
46
Y = -9669888
01 feet Y = -2947381
86 meter
Z = 16399595
31 Z = 4998596
65
XDOT = 9557
283920 XDOT = 2913
060139
YDOT = 21457
796837 feet/sec YDOT = 6540
336476 meter/sec
ZDOT = 6187
280912 ZDOT = 1885
883222
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 08080
16407427
00020000 00000-0 20000-3 0 9039
2 25544 51
6347 115
3043 0000915 317
1792 42
9301 15
76244056 14486
Satellite: ISS
Catalog Number: 25544
Epoch time: 08080
16407427 = yrday
fracday
Element set: 903
Inclination: 51
6347 deg
RA of node: 115
3043 deg
Eccentricity:
0000915
Arg of perigee: 317
1792 deg
Mean anomaly: 42
9301 deg
Mean motion: 15
76244056 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1448
Checksum: 267
Coasting Arc #5 (Orbit 1462)
---------------------------------------
Vector Time (GMT): 2008/081/02:43:09
439
Vector Time (MET): N/A
Weight (LBS) : 567143
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1564363
91 A = 6725271
77 meter
Y = 6475068
69 meter E =
0010256
Z = -888408
14 I = 51
96053
XDOT = -4841
563528 Wp = 34
77470
YDOT = -354
633257 meter/sec RA = 109
57176 deg
ZDOT = 5982
432619 TA = 315
56243
MA = 315
64467
Ha = 186
386 n
mi
Hp = 180
421
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5132427
51 X = -1632337
17
Y = 21243663
68 feet Y = 6457194
92 meter
Z = -2914724
86 Z = -896173
56
XDOT = -15884
394778 XDOT = -4866
299454
YDOT = -1163
494937 feet/sec YDOT = -408
912044 meter/sec
ZDOT = 19627
403605 ZDOT = 5958
852469
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9405814
32 X = -2866892
21
Y = -19722974
36 feet Y = -6011562
59 meter
Z = -2943742
30 Z = -897252
65
XDOT = 11719
096865 XDOT = 3571
980724
YDOT = -8484
495074 feet/sec YDOT = -2586
074099 meter/sec
ZDOT = 19536
934762 ZDOT = 5954
857716
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 08081
11503342
00020000 00000-0 20000-3 0 9049
2 25544 51
6350 110
4031 0000732 315
6618 44
4487 15
76304435 14637
Satellite: ISS
Catalog Number: 25544
Epoch time: 08081
11503342 = yrday
fracday
Element set: 904
Inclination: 51
6350 deg
RA of node: 110
4031 deg
Eccentricity:
0000732
Arg of perigee: 315
6618 deg
Mean anomaly: 44
4487 deg
Mean motion: 15
76304435 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1463
Checksum: 248
Coasting Arc #6 (Orbit 1478)
---------------------------------------
Vector Time (GMT): 2008/082/02:43:09
439
Vector Time (MET): N/A
Weight (LBS) : 567143
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4043937
65 A = 6713431
25 meter
Y = 918241
42 meter E =
0014761
Z = -5292129
76 I = 51
92962
XDOT = -1837
924850 Wp = 87
06126
YDOT = 7470
549618 meter/sec RA = 104
45001 deg
ZDOT = -107
731218 TA = 181
91680
MA = 181
92247
Ha = 186
390 n
mi
Hp = 180
399
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13267511
96 X = 4059077
30
Y = 3012603
10 feet Y = 963547
13 meter
Z = -17362630
45 Z = -5272447
71
XDOT = -6029
937171 XDOT = -1920
801761
YDOT = 24509
677226 feet/sec YDOT = 7449
533493 meter/sec
ZDOT = -353
448878 ZDOT = -116
861924
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12172928
89 X = -3710308
73
Y = 6288202
25 feet Y = 1916644
05 meter
Z = -17287044
34 Z = -5269091
11
XDOT = -10687
008365 XDOT = -3257
400150
YDOT = -21758
214312 feet/sec YDOT = -6631
903722 meter/sec
ZDOT = -387
592433 ZDOT = -118
138174
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 08082
12936960
00020000 00000-0 20000-3 0 9058
2 25544 51
6351 105
1758 0000628 329
0583 31
0544 15
76345808 14791
Satellite: ISS
Catalog Number: 25544
Epoch time: 08082
12936960 = yrday
fracday
Element set: 905
Inclination: 51
6351 deg
RA of node: 105
1758 deg
Eccentricity:
0000628
Arg of perigee: 329
0583 deg
Mean anomaly: 31
0544 deg
Mean motion: 15
76345808 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1479
Checksum: 291
Coasting Arc #7 (Orbit 1494)
---------------------------------------
Vector Time (GMT): 2008/083/02:43:09
439
Vector Time (MET): N/A
Weight (LBS) : 567143
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1630021
43 A = 6725122
35 meter
Y = -6480841
31 meter E =
0009835
Z = -714304
34 I = 51
97526
XDOT = 4472
999184 Wp = 139
07405
YDOT = 1781
940199 meter/sec RA = 99
32318 deg
ZDOT = -6013
688368 TA = 48
68000
MA = 48
59541
Ha = 186
305 n
mi
Hp = 180
217
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5347839
33 X = 1705840
02
Y = -21262602
72 feet Y = -6462189
62 meter
Z = -2343518
16 Z = -706200
90
XDOT = 14675
194172 XDOT = 4481
954252
YDOT = 5846
260497 feet/sec YDOT = 1832
009329 meter/sec
ZDOT = -19729
948715 ZDOT = -5991
936938
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9906015
36 X = 3019353
48
Y = 19562968
85 feet Y = 5962792
90 meter
Z = -2313189
79 Z = -705060
25
XDOT = -13568
128142 XDOT = -4135
565458
YDOT = 4568
415040 feet/sec YDOT = 1392
452904 meter/sec
ZDOT = -19646
327475 ZDOT = -5988
200614
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 08083
14368207
00020000 00000-0 20000-3 0 9065
2 25544 51
6347 99
9468 0000850 334
3457 25
7665 15
76406062 14952
Satellite: ISS
Catalog Number: 25544
Epoch time: 08083
14368207 = yrday
fracday
Element set: 906
Inclination: 51
6347 deg
RA of node: 99
9468 deg
Eccentricity:
0000850
Arg of perigee: 334
3457 deg
Mean anomaly: 25
7665 deg
Mean motion: 15
76406062 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1495
Checksum: 309
Coasting Arc #8 (Orbit 1510)
---------------------------------------
Vector Time (GMT): 2008/084/02:43:09
439
Vector Time (MET): N/A
Weight (LBS) : 567143
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3818216
68 A = 6714339
34 meter
Y = -2190370
83 meter E =
0005430
Z = 5067496
41 I = 51
94220
XDOT = 1881
555577 Wp = 49
01340
YDOT = -7273
037562 meter/sec RA = 94
17053 deg
ZDOT = -1721
318975 TA = 57
49080
MA = 57
43834
Ha = 186
546 n
mi
Hp = 180
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12526957
62 X = -3818056
93
Y = -7186256
00 feet Y = -2233067
02 meter
Z = 16625644
37 Z = 5048947
99
XDOT = 6173
082603 XDOT = 1971
105865
YDOT = -23861
671790 feet/sec YDOT = -7251
496366 meter/sec
ZDOT = -5647
371966 ZDOT = -1711
960251
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14188265
32 X = 4324583
27
Y = -3102987
98 feet Y = -945790
74 meter
Z = 16554261
87 Z = 5045739
02
XDOT = 11126
393164 XDOT = 3391
324636
YDOT = 20851
400285 feet/sec YDOT = 6355
506807 meter/sec
ZDOT = -5612
309058 ZDOT = -1710
631801
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 08084
15797568
00020000 00000-0 20000-3 0 9074
2 25544 51
6350 94
7186 0000565 344
4989 15
6157 15
76363751 15111
Satellite: ISS
Catalog Number: 25544
Epoch time: 08084
15797568 = yrday
fracday
Element set: 907
Inclination: 51
6350 deg
RA of node: 94
7186 deg
Eccentricity:
0000565
Arg of perigee: 344
4989 deg
Mean anomaly: 15
6157 deg
Mean motion: 15
76363751 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1511
Checksum: 317
Coasting Arc #9 (Orbit 1526)
---------------------------------------
Vector Time (GMT): 2008/085/02:43:09
439
Vector Time (MET): N/A
Weight (LBS) : 567143
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1669423
50 A = 6722956
80 meter
Y = 6100038
31 meter E =
0013951
Z = 2260694
93 I = 51
97448
XDOT = -4343
548357 Wp = 69
81227
YDOT = -3230
451981 meter/sec RA = 89
07322 deg
ZDOT = 5486
842502 TA = 315
48410
MA = 315
59609
Ha = 186
256 n
mi
Hp = 180
083
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5477111
22 X = -1748493
11
Y = 20013249
03 feet Y = 6080927
89 meter
Z = 7416978
10 Z = 2252392
40
XDOT = -14250
486735 XDOT = -4333
756369
YDOT = -10598
595739 feet/sec YDOT = -3278
968952 meter/sec
ZDOT = 18001
451778 ZDOT = 5465
765392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9605706
03 X = -2927819
20
Y = -18404361
09 feet Y = -5609649
26 meter
Z = 7385821
07 Z = 2251198
26
XDOT = 16383
644424 XDOT = 4993
734820
YDOT = -1329
913036 feet/sec YDOT = -405
357493 meter/sec
ZDOT = 17920
256864 ZDOT = 5462
094292
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 08085
17224161
00020000 00000-0 20000-3 0 9082
2 25544 51
6364 89
4906 0000534 331
9505 28
1630 15
76469851 15278
Satellite: ISS
Catalog Number: 25544
Epoch time: 08085
17224161 = yrday
fracday
Element set: 908
Inclination: 51
6364 deg
RA of node: 89
4906 deg
Eccentricity:
0000534
Arg of perigee: 331
9505 deg
Mean anomaly: 28
1630 deg
Mean motion: 15
76469851 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1527
Checksum: 292
Coasting Arc #10 (Orbit 1541)
---------------------------------------
Vector Time (GMT): 2008/086/02:43:09
439
Vector Time (MET): N/A
Weight (LBS) : 567143
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3803044
69 A = 6716935
64 meter
Y = 3412584
82 meter E =
0008635
Z = -4368394
95 I = 51
95298
XDOT = -1990
513101 Wp = 107
37847
YDOT = 6599
195540 meter/sec RA = 83
89796 deg
ZDOT = 3425
375093 TA = 197
01669
MA = 197
04567
Ha = 186
272 n
mi
Hp = 180
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12477180
73 X = 3785822
99
Y = 11196144
41 feet Y = 3455016
18 meter
Z = -14332004
44 Z = -4349961
61
XDOT = -6530
554792 XDOT = -2080
798347
YDOT = 21650
904001 feet/sec YDOT = 6576
431804 meter/sec
ZDOT = 11238
107259 ZDOT = 3415
485569
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16811634
43 X = -5124186
17
Y = 659405
18 feet Y = 200986
70 meter
Z = -14260931
69 Z = -4346731
98
XDOT = -10235
811539 XDOT = -3119
875357
YDOT = -18935
574247 feet/sec YDOT = -5771
563030 meter/sec
ZDOT = 11200
907291 ZDOT = 3414
036542
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 08086
12309831
00020000 00000-0 20000-3 0 9097
2 25544 51
6370 84
5900 0000633 342
3558 17
7585 15
76466384 15427
Satellite: ISS
Catalog Number: 25544
Epoch time: 08086
12309831 = yrday
fracday
Element set: 909
Inclination: 51
6370 deg
RA of node: 84
5900 deg
Eccentricity:
0000633
Arg of perigee: 342
3558 deg
Mean anomaly: 17
7585 deg
Mean motion: 15
76466384 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1542
Checksum: 296
Coasting Arc #11 (Orbit 1557)
---------------------------------------
Vector Time (GMT): 2008/087/02:43:09
439
Vector Time (MET): N/A
Weight (LBS) : 567143
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1864018
14 A = 6719259
62 meter
Y = -5324139
52 meter E =
0005624
Z = -3656716
32 I = 51
95727
XDOT = 4397
507984 Wp = 73
30627
YDOT = 4548
965126 meter/sec RA = 78
81550 deg
ZDOT = -4385
542145 TA = 150
37792
MA = 150
34606
Ha = 186
212 n
mi
Hp = 180
021
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6115545
08 X = 1941178
71
Y = -17467649
33 feet Y = -5302863
65 meter
Z = -11997100
78 Z = -3647473
34
XDOT = 14427
519631 XDOT = 4367
618190
YDOT = 14924
426265 feet/sec YDOT = 4597
973357 meter/sec
ZDOT = -14388
261631 ZDOT = -4364
251647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7964417
87 X = 2427554
57
Y = 16730875
64 feet Y = 5099570
90 meter
Z = -11962229
74 Z = -3646087
63
XDOT = -19592
264124 XDOT = -5971
722105
YDOT = -892
784121 feet/sec YDOT = -272
120600 meter/sec
ZDOT = -14306
109247 ZDOT = -4360
502098
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 08087
13732164
00020000 00000-0 20000-3 0 9100
2 25544 51
6375 79
3615 0000609 344
7042 15
4104 15
76506583 15589
Satellite: ISS
Catalog Number: 25544
Epoch time: 08087
13732164 = yrday
fracday
Element set: 910
Inclination: 51
6375 deg
RA of node: 79
3615 deg
Eccentricity:
0000609
Arg of perigee: 344
7042 deg
Mean anomaly: 15
4104 deg
Mean motion: 15
76506583 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1558
Checksum: 281
Coasting Arc #12 (Orbit 1573)
---------------------------------------
Vector Time (GMT): 2008/088/02:43:09
439
Vector Time (MET): N/A
Weight (LBS) : 567143
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3899523
42 A = 6720628
24 meter
Y = -4447163
59 meter E =
0012925
Z = 3179757
03 I = 51
95560
XDOT = 2331
137512 Wp = 91
35001
YDOT = -5521
126959 meter/sec RA = 73
63224 deg
ZDOT = -4846
464941 TA = 51
68967
MA = 51
57352
Ha = 186
259 n
mi
Hp = 179
921
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12793712
02 X = -3864951
45
Y = -14590431
74 feet Y = -4490576
96 meter
Z = 10432273
71 Z = 3160897
11
XDOT = 7648
088950 XDOT = 2416
245667
YDOT = -18113
933594 feet/sec YDOT = -5494
583033 meter/sec
ZDOT = -15900
475529 ZDOT = -4834
933464
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19422729
39 X = 5920047
92
Y = 911772
87 feet Y = 277908
37 meter
Z = 10359457
20 Z = 3157562
56
XDOT = 7700
678654 XDOT = 2347
166854
YDOT = 16741
666678 feet/sec YDOT = 5102
860003 meter/sec
ZDOT = -15856
838889 ZDOT = -4833
164493
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 08088
15152168
00020000 00000-0 20000-3 0 9114
2 25544 51
6380 74
1335 0000545 354
0524 6
0634 15
76534265 15745
Satellite: ISS
Catalog Number: 25544
Epoch time: 08088
15152168 = yrday
fracday
Element set: 911
Inclination: 51
6380 deg
RA of node: 74
1335 deg
Eccentricity:
0000545
Arg of perigee: 354
0524 deg
Mean anomaly: 6
0634 deg
Mean motion: 15
76534265 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1574
Checksum: 271
Coasting Arc #13 (Orbit 1589)
---------------------------------------
Vector Time (GMT): 2008/089/02:43:09
439
Vector Time (MET): N/A
Weight (LBS) : 567143
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2272554
06 A = 6715212
40 meter
Y = 4240242
50 meter E =
0007589
Z = 4680485
69 I = 51
92985
XDOT = -4548
896217 Wp = 113
47884
YDOT = -5550
480207 meter/sec RA = 68
54498 deg
ZDOT = 2813
215107 TA = 308
86785
MA = 308
93554
Ha = 186
129 n
mi
Hp = 179
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7455886
03 X = -2342537
16
Y = 13911556
74 feet Y = 4214438
23 meter
Z = 15355924
18 Z = 4669275
61
XDOT = -14924
200186 XDOT = -4500
157884
YDOT = -18210
236900 feet/sec YDOT = -5601
076036 meter/sec
ZDOT = 9229
708357 ZDOT = 2791
234999
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5009311
46 X = -1526838
13
Y = -15011108
22 feet Y = -4575385
79 meter
Z = 15313375
97 Z = 4667517
00
XDOT = 22435
316041 XDOT = 6838
284329
YDOT = 1864
038981 feet/sec YDOT = 568
159082 meter/sec
ZDOT = 9144
807152 ZDOT = 2787
337220
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 08089
16569537
00020000 00000-0 20000-3 0 9129
2 25544 51
6391 68
9052 0000605 350
3532 9
7620 15
76621463 15909
Satellite: ISS
Catalog Number: 25544
Epoch time: 08089
16569537 = yrday
fracday
Element set: 912
Inclination: 51
6391 deg
RA of node: 68
9052 deg
Eccentricity:
0000605
Arg of perigee: 350
3532 deg
Mean anomaly: 9
7620 deg
Mean motion: 15
76621463 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1590
Checksum: 290
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data may contain past, current and future orbital data These sources include:
NASA Orbital Flight Dynamics 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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