Date:
May 4th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 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 2068)
---------------------------------------
Vector Time (GMT): 2008/119/11:52:46
026
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3266541
92 A = 6720326
08 meter
Y = 4388451
95 meter E =
0010977
Z = -3908581
12 I = 51
31005
XDOT = -3037
195349 Wp = 112
36775
YDOT = -5824
087749 meter/sec RA = 271
75974 deg
ZDOT = -4013
934208 TA = 115
77227
MA = 115
65896
Ha = 189
352 n
mi
Hp = 179
293
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10717001
05 X = -3296384
26
Y = 14397808
24 feet Y = 4351756
92 meter
Z = -12823428
87 Z = -3924522
33
XDOT = -9964
551669 XDOT = -2952
344725
YDOT = -19107
899438 feet/sec YDOT = -5857
576806 meter/sec
ZDOT = -13169
075485 ZDOT = -4028
483102
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -689364
86 X = -210118
41
Y = 17891753
68 feet Y = 5453406
52 meter
Z = -12884147
16 Z = -3927088
06
XDOT = -17627
154662 XDOT = -5372
756741
YDOT = -10172
272544 feet/sec YDOT = -3100
508671 meter/sec
ZDOT = -13225
492784 ZDOT = -4031
130200
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 08119
51825482
00020000 00000-0 20000-3 0 9003
2 25544 51
6379 272
3532 0007188 149
5687 210
5896 15
75805196 20696
Satellite: ISS
Catalog Number: 25544
Epoch time: 08119
51825482 = yrday
fracday
Element set: 900
Inclination: 51
6379 deg
RA of node: 272
3532 deg
Eccentricity:
0007188
Arg of perigee: 149
5687 deg
Mean anomaly: 210
5896 deg
Mean motion: 15
75805196 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2069
Checksum: 321
Coasting Arc #2 (Orbit 2084)
---------------------------------------
Vector Time (GMT): 2008/120/11:52:46
026
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2740908
53 A = 6723029
13 meter
Y = 5334382
35 meter E =
0018095
Z = 3014639
88 I = 51
31881
XDOT = -3664
300026 Wp = 115
75280
YDOT = 4672
439596 meter/sec RA = 266
53566 deg
ZDOT = -4921
167366 TA = 29
12516
MA = 29
02435
Ha = 189
247 n
mi
Hp = 179
485
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8992482
05 X = 2666410
29
Y = 17501254
44 feet Y = 5364616
14 meter
Z = 9890550
78 Z = 3027774
45
XDOT = -12021
981712 XDOT = -3692
369409
YDOT = 15329
526235 feet/sec YDOT = 4631
306489 meter/sec
ZDOT = -16145
562225 ZDOT = -4939
036653
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17398960
88 X = 5303203
28
Y = 9133693
64 feet Y = 2783949
82 meter
Z = 9941500
68 Z = 3030169
41
XDOT = -227
887234 XDOT = -69
460029
YDOT = 18135
375122 feet/sec YDOT = 5527
662337 meter/sec
ZDOT = -16213
646535 ZDOT = -4941
919464
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 08120
53291778
00020000 00000-0 20000-3 0 9013
2 25544 51
6371 267
1275 0007210 154
1229 206
0297 15
75809633 20857
Satellite: ISS
Catalog Number: 25544
Epoch time: 08120
53291778 = yrday
fracday
Element set: 901
Inclination: 51
6371 deg
RA of node: 267
1275 deg
Eccentricity:
0007210
Arg of perigee: 154
1229 deg
Mean anomaly: 206
0297 deg
Mean motion: 15
75809633 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2085
Checksum: 282
Coasting Arc #3 (Orbit 2100)
---------------------------------------
Vector Time (GMT): 2008/121/11:52:46
026
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3173076
76 A = 6717458
44 meter
Y = -3711783
52 meter E =
0014243
Z = 4609070
29 I = 51
30475
XDOT = 3274
769936 Wp = 135
86742
YDOT = 6364
420928 meter/sec RA = 261
40911 deg
ZDOT = 2855
529442 TA = 285
70928
MA = 285
86635
Ha = 189
004 n
mi
Hp = 179
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10410356
83 X = 3191956
51
Y = -12177767
45 feet Y = -3676194
85 meter
Z = 15121621
68 Z = 4624531
00
XDOT = 10743
995852 XDOT = 3189
486870
YDOT = 20880
646088 feet/sec YDOT = 6400
564402 meter/sec
ZDOT = 9368
534914 ZDOT = 2871
231288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1128057
74 X = 343832
00
Y = -15925296
05 feet Y = -4854030
23 meter
Z = 15180560
70 Z = 4627034
90
XDOT = 19805
026699 XDOT = 6036
572138
YDOT = 10439
301232 feet/sec YDOT = 3181
899016 meter/sec
ZDOT = 9429
451960 ZDOT = 2874
096957
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 08121
54755611
00020000 00000-0 20000-3 0 9027
2 25544 51
6380 261
9022 0007093 158
7289 201
4171 15
75893081 21013
Satellite: ISS
Catalog Number: 25544
Epoch time: 08121
54755611 = yrday
fracday
Element set: 902
Inclination: 51
6380 deg
RA of node: 261
9022 deg
Eccentricity:
0007093
Arg of perigee: 158
7289 deg
Mean anomaly: 201
4171 deg
Mean motion: 15
75893081 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2101
Checksum: 272
Coasting Arc #4 (Orbit 2115)
---------------------------------------
Vector Time (GMT): 2008/122/11:52:46
026
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2979360
67 A = 6725154
89 meter
Y = -5721451
55 meter E =
0006798
Z = -1910113
99 I = 51
33745
XDOT = 3683
773181 Wp = 100
53037
YDOT = -3782
350362 meter/sec RA = 256
19670 deg
ZDOT = 5599
221098 TA = 238
14735
MA = 238
21353
Ha = 188
976 n
mi
Hp = 179
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9774805
34 X = -2905881
99
Y = -18771166
50 feet Y = -5754357
62 meter
Z = -6266778
20 Z = -1924409
39
XDOT = 12085
870016 XDOT = 3698
593956
YDOT = -12409
285963 feet/sec YDOT = -3741
073438 meter/sec
ZDOT = 18370
147958 ZDOT = 5617
153041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19110396
91 X = -5824848
98
Y = -9055277
75 feet Y = -2760048
66 meter
Z = -6322238
12 Z = -1927018
18
XDOT = 1373
005396 XDOT = 418
492045
YDOT = -15735
547196 feet/sec YDOT = -4796
194785 meter/sec
ZDOT = 18438
560314 ZDOT = 5620
073184
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 08122
49876121
00020000 00000-0 20000-3 0 9033
2 25544 51
6389 257
0037 0007042 161
1203 199
0223 15
75898030 21167
Satellite: ISS
Catalog Number: 25544
Epoch time: 08122
49876121 = yrday
fracday
Element set: 903
Inclination: 51
6389 deg
RA of node: 257
0037 deg
Eccentricity:
0007042
Arg of perigee: 161
1203 deg
Mean anomaly: 199
0223 deg
Mean motion: 15
75898030 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2116
Checksum: 272
Coasting Arc #5 (Orbit 2131)
---------------------------------------
Vector Time (GMT): 2008/123/11:52:46
026
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3330663
92 A = 6715296
76 meter
Y = 2860484
00 meter E =
0015944
Z = -5093726
29 I = 51
31301
XDOT = -3525
360278 Wp = 104
42755
YDOT = -6681
778045 meter/sec RA = 251
05446 deg
ZDOT = -1454
853149 TA = 151
59611
MA = 151
50910
Ha = 188
740 n
mi
Hp = 179
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10927375
06 X = -3337657
97
Y = 9384790
02 feet Y = 2823199
50 meter
Z = -16711700
43 Z = -5109923
89
XDOT = -11566
142645 XDOT = -3443
314054
YDOT = -21921
843980 feet/sec YDOT = -6720
741899 meter/sec
ZDOT = -4773
140252 ZDOT = -1471
780308
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2706336
43 X = -824891
34
Y = 14074315
41 feet Y = 4289851
34 meter
Z = -16773554
47 Z = -5112579
40
XDOT = -21600
057583 XDOT = -6583
697551
YDOT = -9890
216385 feet/sec YDOT = -3014
537954 meter/sec
ZDOT = -4838
805541 ZDOT = -1474
867929
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 08123
51335687
00020000 00000-0 20000-3 0 9045
2 25544 51
6392 251
7787 0006882 165
0813 195
0556 15
75939184 21324
Satellite: ISS
Catalog Number: 25544
Epoch time: 08123
51335687 = yrday
fracday
Element set: 904
Inclination: 51
6392 deg
RA of node: 251
7787 deg
Eccentricity:
0006882
Arg of perigee: 165
0813 deg
Mean anomaly: 195
0556 deg
Mean motion: 15
75939184 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2132
Checksum: 311
Coasting Arc #6 (Orbit 2147)
---------------------------------------
Vector Time (GMT): 2008/124/11:52:46
026
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3172386
66 A = 6726430
15 meter
Y = 5887369
50 meter E =
0019074
Z = 609938
47 I = 51
36181
XDOT = -3993
531342 Wp = 142
17206
YDOT = 2780
223047 meter/sec RA = 245
86309 deg
ZDOT = -5981
206706 TA = 31
15052
MA = 31
03760
Ha = 188
608 n
mi
Hp = 179
858
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10408092
71 X = 3103354
36
Y = 19315516
75 feet Y = 5922458
96 meter
Z = 2001110
45 Z = 625182
62
XDOT = -13102
136948 XDOT = -3995
267190
YDOT = 9121
466689 feet/sec YDOT = 2735
555455 meter/sec
ZDOT = -19623
381582 ZDOT = -6000
611874
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20264158
08 X = 6176515
38
Y = 8398889
98 feet Y = 2559981
67 meter
Z = 2060235
01 Z = 627959
63
XDOT = -3690
355607 XDOT = -1124
820389
YDOT = 13800
939678 feet/sec YDOT = 4206
526414 meter/sec
ZDOT = -19697
554752 ZDOT = -6003
814688
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 08124
52793049
00020000 00000-0 20000-3 0 9058
2 25544 51
6394 246
5523 0006875 169
1577 190
9737 15
75964609 21482
Satellite: ISS
Catalog Number: 25544
Epoch time: 08124
52793049 = yrday
fracday
Element set: 905
Inclination: 51
6394 deg
RA of node: 246
5523 deg
Eccentricity:
0006875
Arg of perigee: 169
1577 deg
Mean anomaly: 190
9737 deg
Mean motion: 15
75964609 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2148
Checksum: 332
Coasting Arc #7 (Orbit 2163)
---------------------------------------
Vector Time (GMT): 2008/125/11:52:46
026
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3688238
42 A = 6714320
45 meter
Y = -1996109
82 meter E =
0007268
Z = 5240763
47 I = 51
33588
XDOT = 3728
928640 Wp = 154
37586
YDOT = 6745
010244 meter/sec RA = 240
69756 deg
ZDOT = -61
657292 TA = 296
17380
MA = 296
24853
Ha = 188
290 n
mi
Hp = 179
964
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12100519
75 X = 3684825
79
Y = -6548916
75 feet Y = -1954885
11 meter
Z = 17194105
87 Z = 5258673
02
XDOT = 12234
017848 XDOT = 3653
527262
YDOT = 22129
298702 feet/sec YDOT = 6786
287669 meter/sec
ZDOT = -202
287705 ZDOT = -43
724598
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4944536
99 X = 1507094
87
Y = -12747605
21 feet Y = -3885470
07 meter
Z = 17262626
71 Z = 5261648
62
XDOT = 22696
111074 XDOT = 6917
774655
YDOT = 8652
071011 feet/sec YDOT = 2637
151244 meter/sec
ZDOT = -132
754513 ZDOT = -40
463576
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 08125
54248092
00020000 00000-0 20000-3 0 9065
2 25544 51
6405 241
3269 0006665 173
3021 186
8233 15
76027982 21641
Satellite: ISS
Catalog Number: 25544
Epoch time: 08125
54248092 = yrday
fracday
Element set: 906
Inclination: 51
6405 deg
RA of node: 241
3269 deg
Eccentricity:
0006665
Arg of perigee: 173
3021 deg
Mean anomaly: 186
8233 deg
Mean motion: 15
76027982 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2164
Checksum: 288
Coasting Arc #8 (Orbit 2179)
---------------------------------------
Vector Time (GMT): 2008/126/11:52:46
026
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3284048
66 A = 6726173
71 meter
Y = -5821375
64 meter E =
0011249
Z = 734798
36 I = 51
39175
XDOT = 4536
170704 Wp = 82
07486
YDOT = -1797
436924 meter/sec RA = 235
53475 deg
ZDOT = 5957
375348 TA = 285
96397
MA = 286
08787
Ha = 188
286 n
mi
Hp = 180
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10774437
86 X = -3222278
65
Y = -19099001
46 feet Y = -5857754
43 meter
Z = 2410755
79 Z = 718993
65
XDOT = 14882
449816 XDOT = 4526
992177
YDOT = -5897
102768 feet/sec YDOT = -1746
762632 meter/sec
ZDOT = 19545
194712 ZDOT = 5979
390214
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20693199
20 X = -6307287
12
Y = -7276230
61 feet Y = -2217795
09 meter
Z = 2349486
37 Z = 716123
45
XDOT = 6707
117516 XDOT = 2044
329419
YDOT = -12653
517799 feet/sec YDOT = -3856
792225 meter/sec
ZDOT = 19629
498946 ZDOT = 5983
071279
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 08126
55701087
00020000 00000-0 20000-3 0 9076
2 25544 51
6409 236
1015 0006592 176
1644 183
9572 15
76035194 21803
Satellite: ISS
Catalog Number: 25544
Epoch time: 08126
55701087 = yrday
fracday
Element set: 907
Inclination: 51
6409 deg
RA of node: 236
1015 deg
Eccentricity:
0006592
Arg of perigee: 176
1644 deg
Mean anomaly: 183
9572 deg
Mean motion: 15
76035194 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2180
Checksum: 291
Coasting Arc #9 (Orbit 2194)
---------------------------------------
Vector Time (GMT): 2008/127/11:52:46
026
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4282009
94 A = 6715010
70 meter
Y = 1162537
17 meter E =
0016393
Z = -5054079
20 I = 51
37228
XDOT = -3714
822778 Wp = 125
34330
YDOT = -6533
822026 meter/sec RA = 230
34533 deg
ZDOT = 1638
826914 TA = 160
51310
MA = 160
45036
Ha = 188
049 n
mi
Hp = 180
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14048589
05 X = -4270139
00
Y = 3814098
34 feet Y = 1114720
22 meter
Z = -16581624
68 Z = -5074852
73
XDOT = -12187
738772 XDOT = -3649
445769
YDOT = -21436
423970 feet/sec YDOT = -6574
997936 meter/sec
ZDOT = 5376
728721 ZDOT = 1620
937973
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7785264
93 X = -2372948
75
Y = 12192341
58 feet Y = 3716225
71 meter
Z = -16661240
48 Z = -5078346
10
XDOT = -22555
132668 XDOT = -6874
804437
YDOT = -7124
562413 feet/sec YDOT = -2171
566623 meter/sec
ZDOT = 5307
382611 ZDOT = 1617
690220
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 08127
50811197
00020000 00000-0 20000-3 0 9087
2 25544 51
6408 231
2033 0006514 179
7510 180
3658 15
76094738 21954
Satellite: ISS
Catalog Number: 25544
Epoch time: 08127
50811197 = yrday
fracday
Element set: 908
Inclination: 51
6408 deg
RA of node: 231
2033 deg
Eccentricity:
0006514
Arg of perigee: 179
7510 deg
Mean anomaly: 180
3658 deg
Mean motion: 15
76094738 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2195
Checksum: 293
Coasting Arc #10 (Orbit 2210)
---------------------------------------
Vector Time (GMT): 2008/128/11:52:46
026
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3140673
76 A = 6724302
02 meter
Y = 5551809
22 meter E =
0011974
Z = -2109264
13 I = 51
42283
XDOT = -5300
592961 Wp = 161
94235
YDOT = 909
133968 meter/sec RA = 225
20965 deg
ZDOT = -5519
140803 TA = 41
73590
MA = 41
64462
Ha = 187
945 n
mi
Hp = 180
325
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10304047
77 X = 3088605
74
Y = 18214597
19 feet Y = 5586639
19 meter
Z = -6920157
90 Z = -2094132
20
XDOT = -17390
396853 XDOT = -5283
553639
YDOT = 2982
722993 feet/sec YDOT = 849
955718 meter/sec
ZDOT = -18107
417333 ZDOT = -5544
850020
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20001979
18 X = 6096603
25
Y = 6218866
53 feet Y = 1895510
52 meter
Z = -6861491
41 Z = -2091382
58
XDOT = -10121
519140 XDOT = -3085
039034
YDOT = 12538
263171 feet/sec YDOT = 3821
662614 meter/sec
ZDOT = -18206
017796 ZDOT = -5549
194224
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 08128
52259936
00020000 00000-0 20000-3 0 9098
2 25544 51
6404 225
9775 0006491 184
1634 175
9477 15
76099134 22117
Satellite: ISS
Catalog Number: 25544
Epoch time: 08128
52259936 = yrday
fracday
Element set: 909
Inclination: 51
6404 deg
RA of node: 225
9775 deg
Eccentricity:
0006491
Arg of perigee: 184
1634 deg
Mean anomaly: 175
9477 deg
Mean motion: 15
76099134 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2211
Checksum: 317
Coasting Arc #11 (Orbit 2226)
---------------------------------------
Vector Time (GMT): 2008/129/11:52:46
026
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4977840
19 A = 6717218
88 meter
Y = -484437
60 meter E =
0007767
Z = 4476446
80 I = 51
42096
XDOT = 3426
711036 Wp = 110
89080
YDOT = 6148
744988 meter/sec RA = 220
00041 deg
ZDOT = -3143
470612 TA = 10
55689
MA = 10
54059
Ha = 187
589 n
mi
Hp = 180
409
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16331496
69 X = 4961141
29
Y = -1589362
21 feet Y = -428866
54 meter
Z = 14686505
24 Z = 4500588
77
XDOT = 11242
490277 XDOT = 3372
970693
YDOT = 20173
047860 feet/sec YDOT = 6186
764394 meter/sec
ZDOT = -10313
223792 ZDOT = -3126
953147
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10556611
78 X = 3217655
27
Y = -12452793
55 feet Y = -3795611
47 meter
Z = 14779146
57 Z = 4504683
87
XDOT = 21248
907142 XDOT = 6476
666897
YDOT = 5843
132663 feet/sec YDOT = 1780
986836 meter/sec
ZDOT = -10249
166977 ZDOT = -3123
946095
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 08129
53706524
00020000 00000-0 20000-3 0 9102
2 25544 51
6403 220
7517 0006264 187
5662 172
5409 15
76143725 22270
Satellite: ISS
Catalog Number: 25544
Epoch time: 08129
53706524 = yrday
fracday
Element set: 910
Inclination: 51
6403 deg
RA of node: 220
7517 deg
Eccentricity:
0006264
Arg of perigee: 187
5662 deg
Mean anomaly: 172
5409 deg
Mean motion: 15
76143725 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2227
Checksum: 284
Coasting Arc #12 (Orbit 2242)
---------------------------------------
Vector Time (GMT): 2008/130/11:52:46
026
Vector Time (MET): N/A
Weight (LBS) : 615213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2746498
29 A = 6721186
50 meter
Y = -5149252
35 meter E =
0012852
Z = 3330565
26 I = 51
45727
XDOT = 6131
809318 Wp = 117
65349
YDOT = -246
541495 meter/sec RA = 214
88305 deg
ZDOT = 4655
777748 TA = 281
67180
MA = 281
81600
Ha = 187
551 n
mi
Hp = 180
542
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9010821
15 X = -2704893
77
Y = -16893872
55 feet Y = -5179733
08 meter
Z = 10927051
38 Z = 3317323
09
XDOT = 20117
484639 XDOT = 6111
493428
YDOT = -808
863173 feet/sec YDOT = -178
086304 meter/sec
ZDOT = 15274
861378 ZDOT = 4685
516835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18371776
22 X = -5599717
39
Y = -5495093
30 feet Y = -1674904
44 meter
Z = 10875663
99 Z = 3314902
38
XDOT = 13162
641465 XDOT = 4011
973118
YDOT = -13421
814094 feet/sec YDOT = -4090
968936 meter/sec
ZDOT = 15389
033107 ZDOT = 4690
577291
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 08130
55150928
00020000 00000-0 20000-3 0 9118
2 25544 51
6399 215
5253 0006283 192
0478 168
0537 15
76184484 22437
Satellite: ISS
Catalog Number: 25544
Epoch time: 08130
55150928 = yrday
fracday
Element set: 911
Inclination: 51
6399 deg
RA of node: 215
5253 deg
Eccentricity:
0006283
Arg of perigee: 192
0478 deg
Mean anomaly: 168
0537 deg
Mean motion: 15
76184484 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2243
Checksum: 297
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 normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! 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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