Date:
April 20th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5059 04 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
115/10:22:18
142 -2
9 3
1 3
1
N/A 0
0 0
0 189
2
000/00:00:32
284 1
0 0
0 170
6
Coasting Arc #1 (Orbit 102)
---------------------------------------
Vector Time (GMT): 2007/106/10:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 480296
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1621893
30 A = 6716775
85 meter
Y = 6234609
81 meter E =
0029561
Z = 1854969
50 I = 51
92824
XDOT = -5209
894599 Wp = 70
14761
YDOT = -354
366465 meter/sec RA = 62
38299 deg
ZDOT = 5683
664433 TA = 310
43046
MA = 310
68794
Ha = 188
148 n
mi
Hp = 170
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5321172
23 X = 1543045
23
Y = 20454756
58 feet Y = 6252305
97 meter
Z = 6085857
94 Z = 1862656
87
XDOT = -17092
830049 XDOT = -5233
155370
YDOT = -1162
619636 feet/sec YDOT = -412
756157 meter/sec
ZDOT = 18647
193023 ZDOT = 5658
297972
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5628503
53 X = 1715567
87
Y = 20363421
42 feet Y = 6206770
85 meter
Z = 6115604
93 Z = 1864036
38
XDOT = -15728
611177 XDOT = -4794
080687
YDOT = -1285
476529 feet/sec YDOT = -391
813246 meter/sec
ZDOT = 18551
626312 ZDOT = 5654
535700
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 07106
49714911
00020000 00000-0 20000-3 0 9009
2 25544 51
6303 62
6738 0015447 73
9784 286
3081 15
78896700 1034
Satellite: ISS
Catalog Number: 25544
Epoch time: 07106
49714911 = yrday
fracday
Element set: 900
Inclination: 51
6303 deg
RA of node: 62
6738 deg
Eccentricity:
0015447
Arg of perigee: 73
9784 deg
Mean anomaly: 286
3081 deg
Mean motion: 15
78896700 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 103
Checksum: 295
Coasting Arc #2 (Orbit 117)
---------------------------------------
Vector Time (GMT): 2007/107/10:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 480296
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4994876
59 A = 6710986
07 meter
Y = 1745191
72 meter E =
0022459
Z = -4146707
70 I = 51
89415
XDOT = 782
679439 Wp = 87
26108
YDOT = 6663
501443 meter/sec RA = 57
18595 deg
ZDOT = 3765
635326 TA = 221
11668
MA = 221
28614
Ha = 188
277 n
mi
Hp = 170
855
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16387390
38 X = 4995134
68
Y = 5725694
61 feet Y = 1801048
53 meter
Z = -13604684
04 Z = -4122441
59
XDOT = 2567
845929 XDOT = 689
815931
YDOT = 21861
881376 feet/sec YDOT = 6671
734702 meter/sec
ZDOT = 12354
446608 ZDOT = 3769
211860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16647707
95 X = 5074221
38
Y = 5164095
82 feet Y = 1574016
40 meter
Z = -13513086
42 Z = -4118788
74
XDOT = 3615
630153 XDOT = 1102
044071
YDOT = 20550
459246 feet/sec YDOT = 6263
779978 meter/sec
ZDOT = 12368
757424 ZDOT = 3769
997263
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 07107
44655445
00020000 00000-0 20000-3 0 9012
2 25544 51
6307 57
7615 0015549 76
6389 283
6509 15
78857244 1182
Satellite: ISS
Catalog Number: 25544
Epoch time: 07107
44655445 = yrday
fracday
Element set: 901
Inclination: 51
6307 deg
RA of node: 57
7615 deg
Eccentricity:
0015549
Arg of perigee: 76
6389 deg
Mean anomaly: 283
6509 deg
Mean motion: 15
78857244 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 118
Checksum: 316
Coasting Arc #3 (Orbit 133)
---------------------------------------
Vector Time (GMT): 2007/108/10:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 480296
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 455394
00 A = 6709749
25 meter
Y = -5053104
51 meter E =
0024782
Z = -4414751
62 I = 51
87482
XDOT = 6007
696292 Wp = 76
04386
YDOT = 3449
071985 meter/sec RA = 52
07914 deg
ZDOT = -3337
787767 TA = 160
51422
MA = 160
41933
Ha = 188
163 n
mi
Hp = 170
665
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1494074
81 X = 533311
19
Y = -16578426
88 feet Y = -5047576
38 meter
Z = -14484093
24 Z = -4412350
02
XDOT = 19710
289671 XDOT = 5984
896453
YDOT = 11315
852969 feet/sec YDOT = 3516
125936 meter/sec
ZDOT = -10950
747267 ZDOT = -3308
657177
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 725469
06 X = 221122
97
Y = -16637123
05 feet Y = -5070995
10 meter
Z = -14475679
11 Z = -4412186
99
XDOT = 19110
301963 XDOT = 5824
820038
YDOT = 10237
830422 feet/sec YDOT = 3120
490713 meter/sec
ZDOT = -10840
621789 ZDOT = -3304
221521
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 07108
45922991
00020000 00000-0 20000-3 0 9028
2 25544 51
6316 52
5214 0015506 80
6491 279
6427 15
78914947 1348
Satellite: ISS
Catalog Number: 25544
Epoch time: 07108
45922991 = yrday
fracday
Element set: 902
Inclination: 51
6316 deg
RA of node: 52
5214 deg
Eccentricity:
0015506
Arg of perigee: 80
6491 deg
Mean anomaly: 279
6427 deg
Mean motion: 15
78914947 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 134
Checksum: 298
Coasting Arc #4 (Orbit 149)
---------------------------------------
Vector Time (GMT): 2007/109/10:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 480296
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5219925
00 A = 6717313
80 meter
Y = -3978400
05 meter E =
0028034
Z = 1391070
97 I = 51
88228
XDOT = 1948
225569 Wp = 100
85497
YDOT = -4634
175526 meter/sec RA = 46
88564 deg
ZDOT = -5849
411311 TA = 63
86434
MA = 63
57621
Ha = 188
099 n
mi
Hp = 170
634
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17125738
19 X = -5181807
69
Y = -13052493
60 feet Y = -4036559
10 meter
Z = 4563881
14 Z = 1365804
56
XDOT = 6391
816171 XDOT = 2028
316688
YDOT = -15203
987947 feet/sec YDOT = -4611
941351 meter/sec
ZDOT = -19190
981992 ZDOT = -5839
752285
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18002082
92 X = -5487034
87
Y = -11851046
53 feet Y = -3612198
98 meter
Z = 4468245
25 Z = 1361921
15
XDOT = 4581
250887 XDOT = 1396
365270
YDOT = -14299
337064 feet/sec YDOT = -4358
437937 meter/sec
ZDOT = -19155
176476 ZDOT = -5838
497790
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 07109
47188258
00020000 00000-0 20000-3 0 9032
2 25544 51
6320 47
2821 0015415 84
2097 276
0826 15
78954597 1506
Satellite: ISS
Catalog Number: 25544
Epoch time: 07109
47188258 = yrday
fracday
Element set: 903
Inclination: 51
6320 deg
RA of node: 47
2821 deg
Eccentricity:
0015415
Arg of perigee: 84
2097 deg
Mean anomaly: 276
0826 deg
Mean motion: 15
78954597 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 150
Checksum: 300
Coasting Arc #5 (Orbit 165)
---------------------------------------
Vector Time (GMT): 2007/110/10:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 480296
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2977407
84 A = 6705912
68 meter
Y = 2882734
61 meter E =
0017761
Z = 5256962
02 I = 51
82419
XDOT = -5614
246986 Wp = 85
85078
YDOT = -5296
777869 meter/sec RA = 41
73897 deg
ZDOT = -273
150268 TA = 6
73970
MA = 6
71584
Ha = 188
097 n
mi
Hp = 170
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9768398
43 X = -3034959
43
Y = 9457790
73 feet Y = 2849117
46 meter
Z = 17247250
73 Z = 5242357
96
XDOT = -18419
445493 XDOT = -5553
273453
YDOT = -17377
880146 feet/sec YDOT = -5359
218584 meter/sec
ZDOT = -896
162298 ZDOT = -300
276874
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9020375
79 X = -2749410
54
Y = 10265786
27 feet Y = 3129011
65 meter
Z = 17192600
85 Z = 5240304
74
XDOT = -19082
822375 XDOT = -5816
444260
YDOT = -15083
470218 feet/sec YDOT = -4597
441723 meter/sec
ZDOT = -998
961975 ZDOT = -304
483610
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 07110
48451258
00020000 00000-0 20000-3 0 9049
2 25544 51
6326 42
0436 0015310 88
0374 272
2545 15
78996010 1660
Satellite: ISS
Catalog Number: 25544
Epoch time: 07110
48451258 = yrday
fracday
Element set: 904
Inclination: 51
6326 deg
RA of node: 42
0436 deg
Eccentricity:
0015310
Arg of perigee: 88
0374 deg
Mean anomaly: 272
2545 deg
Mean motion: 15
78996010 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 166
Checksum: 271
Coasting Arc #6 (Orbit 181)
---------------------------------------
Vector Time (GMT): 2007/111/10:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 480296
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4173655
13 A = 6716367
72 meter
Y = 4911972
64 meter E =
0028744
Z = 1851633
03 I = 51
83759
XDOT = -4848
077115 Wp = 79
51466
YDOT = 1954
338501 meter/sec RA = 36
59868 deg
ZDOT = 5674
617440 TA = 301
04336
MA = 301
32525
Ha = 187
907 n
mi
Hp = 170
496
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13693094
25 X = 4109423
57
Y = 16115395
80 feet Y = 4958285
52 meter
Z = 6074911
52 Z = 1871753
15
XDOT = -15905
764813 XDOT = -4897
136981
YDOT = 6411
871724 feet/sec YDOT = 1899
849874 meter/sec
ZDOT = 18617
511286 ZDOT = 5650
946259
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15239696
19 X = 4645059
40
Y = 14629586
71 feet Y = 4459098
03 meter
Z = 6151277
47 Z = 1874909
37
XDOT = -14200
542086 XDOT = -4328
325228
YDOT = 6908
456888 feet/sec YDOT = 2105
697660 meter/sec
ZDOT = 18528
594477 ZDOT = 5647
515597
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 07111
49711977
00020000 00000-0 20000-3 0 9059
2 25544 51
6327 36
8039 0015280 92
1892 268
1023 15
79034240 1820
Satellite: ISS
Catalog Number: 25544
Epoch time: 07111
49711977 = yrday
fracday
Element set: 905
Inclination: 51
6327 deg
RA of node: 36
8039 deg
Eccentricity:
0015280
Arg of perigee: 92
1892 deg
Mean anomaly: 268
1023 deg
Mean motion: 15
79034240 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 182
Checksum: 281
Coasting Arc #7 (Orbit 196)
---------------------------------------
Vector Time (GMT): 2007/112/10:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 480296
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5298585
21 A = 6710615
10 meter
Y = -549497
70 meter E =
0022562
Z = -4102742
50 I = 51
79444
XDOT = 3530
261172 Wp = 99
65621
YDOT = 5670
845899 meter/sec RA = 31
39387 deg
ZDOT = 3813
710054 TA = 209
40128
MA = 209
52839
Ha = 187
868 n
mi
Hp = 170
635
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17383809
76 X = 5324266
42
Y = -1802813
97 feet Y = -490102
08 meter
Z = -13460441
28 Z = -4076939
55
XDOT = 11582
221692 XDOT = 3448
060204
YDOT = 18605
137464 feet/sec YDOT = 5709
863385 meter/sec
ZDOT = 12512
172093 ZDOT = 3830
660841
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17117474
11 X = 5217406
11
Y = -3878683
52 feet Y = -1182222
74 meter
Z = -13363321
20 Z = -4073140
30
XDOT = 13372
831318 XDOT = 4076
038986
YDOT = 15845
718575 feet/sec YDOT = 4829
775022 meter/sec
ZDOT = 12576
692927 ZDOT = 3833
376004
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 07112
44641898
00020000 00000-0 20000-3 0 9060
2 25544 51
6329 31
8915 0015184 95
4801 264
8097 15
79047274 1970
Satellite: ISS
Catalog Number: 25544
Epoch time: 07112
44641898 = yrday
fracday
Element set: 906
Inclination: 51
6329 deg
RA of node: 31
8915 deg
Eccentricity:
0015184
Arg of perigee: 95
4801 deg
Mean anomaly: 264
8097 deg
Mean motion: 15
79047274 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 197
Checksum: 312
Coasting Arc #8 (Orbit 212)
---------------------------------------
Vector Time (GMT): 2007/113/10:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 480296
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1645806
63 A = 6708943
34 meter
Y = -4742446
48 meter E =
0024209
Z = -4472183
37 I = 51
76492
XDOT = 6959
299709 Wp = 87
24790
YDOT = 607
508796 meter/sec RA = 26
27809 deg
ZDOT = -3219
071534 TA = 150
62495
MA = 150
48865
Ha = 187
759 n
mi
Hp = 170
433
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5399628
06 X = -1570928
55
Y = -15559207
61 feet Y = -4760431
90 meter
Z = -14672517
62 Z = -4479997
08
XDOT = 22832
348127 XDOT = 6967
626885
YDOT = 1993
139095 feet/sec YDOT = 685
378322 meter/sec
ZDOT = -10561
258314 ZDOT = -3185
243016
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7394887
08 X = -2253961
58
Y = -14686028
32 feet Y = -4476301
43 meter
Z = -14702513
91 Z = -4481326
24
XDOT = 21877
533276 XDOT = 6668
272143
YDOT = -615
666032 feet/sec YDOT = -187
655007 meter/sec
ZDOT = -10433
766397 ZDOT = -3180
211998
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 07113
45898264
00020000 00000-0 20000-3 0 9074
2 25544 51
6336 26
6509 0015199 99
3445 260
9440 15
79102225 2138
Satellite: ISS
Catalog Number: 25544
Epoch time: 07113
45898264 = yrday
fracday
Element set: 907
Inclination: 51
6336 deg
RA of node: 26
6509 deg
Eccentricity:
0015199
Arg of perigee: 99
3445 deg
Mean anomaly: 260
9440 deg
Mean motion: 15
79102225 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 213
Checksum: 294
Coasting Arc #9 (Orbit 228)
---------------------------------------
Vector Time (GMT): 2007/114/10:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 480296
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6432763
18 A = 6717050
98 meter
Y = -1449314
25 meter E =
0028707
Z = 1219763
01 I = 51
76625
XDOT = -13
952083 Wp = 111
89306
YDOT = -4981
192912 meter/sec RA = 21
07709 deg
ZDOT = -5892
954363 TA = 54
71756
MA = 54
44936
Ha = 187
729 n
mi
Hp = 170
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21104866
06 X = -6422004
01
Y = -4754968
01 feet Y = -1521188
90 meter
Z = 4001847
13 Z = 1188538
81
XDOT = -45
774551 XDOT = 70
376201
YDOT = -16342
496430 feet/sec YDOT = -4980
877204 meter/sec
ZDOT = -19333
839773 ZDOT = -5892
817499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21606701
58 X = -6585722
64
Y = -1450651
68 feet Y = -442158
63 meter
Z = 3884060
95 Z = 1183861
78
XDOT = -2556
785379 XDOT = -779
308183
YDOT = -14582
039386 feet/sec YDOT = -4444
605605 meter/sec
ZDOT = -19333
918115 ZDOT = -5892
978241
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 07114
47152431
00020000 00000-0 20000-3 0 9087
2 25544 51
6340 21
4107 0015166 103
3944 256
8913 15
79118145 2298
Satellite: ISS
Catalog Number: 25544
Epoch time: 07114
47152431 = yrday
fracday
Element set: 908
Inclination: 51
6340 deg
RA of node: 21
4107 deg
Eccentricity:
0015166
Arg of perigee: 103
3944 deg
Mean anomaly: 256
8913 deg
Mean motion: 15
79118145 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 229
Checksum: 267
Coasting Arc #10 (Orbit 244)
---------------------------------------
Vector Time (GMT): 2007/115/10:22:34
284
Vector Time (MET): N/A
Weight (LBS) : 480125
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1619645
28 A = 6709095
11 meter
Y = 4394607
11 meter E =
0023836
Z = 4786899
88 I = 51
70699
XDOT = -7307
648240 Wp = 106
72523
YDOT = -42
328848 meter/sec RA = 15
96717 deg
ZDOT = 2494
495346 TA = 318
87963
MA = 319
05902
Ha = 189
214 n
mi
Hp = 170
643
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5313796
86 X = 1547129
95
Y = 14418002
34 feet Y = 4412313
35 meter
Z = 15705052
10 Z = 4794592
04
XDOT = -23975
223886 XDOT = -7318
749567
YDOT = -138
874173 feet/sec YDOT = -124
109182 meter/sec
ZDOT = 8184
039850 ZDOT = 2458
967925
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7173931
02 X = 2186614
17
Y = 13554426
77 feet Y = 4131389
28 meter
Z = 15734551
75 Z = 4795891
37
XDOT = -22819
526198 XDOT = -6955
391585
YDOT = 2668
372364 feet/sec YDOT = 813
319897 meter/sec
ZDOT = 8050
211132 ZDOT = 2453
704353
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 07115
48406687
00020000 00000-0 20000-3 0 9095
2 25544 51
6339 16
1711 0017033 101
7165 258
5913 15
78571828 2457
Satellite: ISS
Catalog Number: 25544
Epoch time: 07115
48406687 = yrday
fracday
Element set: 909
Inclination: 51
6339 deg
RA of node: 16
1711 deg
Eccentricity:
0017033
Arg of perigee: 101
7165 deg
Mean anomaly: 258
5913 deg
Mean motion: 15
78571828 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 245
Checksum: 294
Coasting Arc #11 (Orbit 259)
---------------------------------------
Vector Time (GMT): 2007/116/10:22:34
284
Vector Time (MET): N/A
Weight (LBS) : 480125
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6644398
08 A = 6719002
58 meter
Y = 685549
47 meter E =
0023639
Z = -720443
71 I = 51
71238
XDOT = 131
902700 Wp = 80
14763
YDOT = 4839
557074 meter/sec RA = 10
77495 deg
ZDOT = 5991
336878 TA = 272
00007
MA = 272
27078
Ha = 189
239 n
mi
Hp = 170
709
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21799206
28 X = 6639738
12
Y = 2249178
06 feet Y = 759824
80 meter
Z = -2363660
47 Z = -688176
57
XDOT = 432
751640 XDOT = 48
671461
YDOT = 15877
811924 feet/sec YDOT = 4840
566701 meter/sec
ZDOT = 19656
617053 ZDOT = 5991
775504
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21896345
55 X = 6674006
12
Y = -1172352
53 feet Y = -357333
05 meter
Z = -2242036
66 Z = -683372
77
XDOT = 2704
404577 XDOT = 824
302515
YDOT = 14037
261021 feet/sec YDOT = 4278
557159 meter/sec
ZDOT = 19658
848490 ZDOT = 5992
017020
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 07116
43365667
00020000 00000-0 20000-3 0 9105
2 25544 51
6340 11
2606 0016996 104
8342 255
4707 15
78564919 2603
Satellite: ISS
Catalog Number: 25544
Epoch time: 07116
43365667 = yrday
fracday
Element set: 910
Inclination: 51
6340 deg
RA of node: 11
2606 deg
Eccentricity:
0016996
Arg of perigee: 104
8342 deg
Mean anomaly: 255
4707 deg
Mean motion: 15
78564919 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 260
Checksum: 290
Coasting Arc #12 (Orbit 275)
---------------------------------------
Vector Time (GMT): 2007/117/10:22:34
284
Vector Time (MET): N/A
Weight (LBS) : 480125
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1475598
93 A = 6707353
99 meter
Y = -3996108
68 meter E =
0031356
Z = -5208088
96 I = 51
64568
XDOT = 7474
988729 Wp = 103
25263
YDOT = 1500
405979 meter/sec RA = 5
60501 deg
ZDOT = 964
435763 TA = 175
96902
MA = 175
94371
Ha = 189
112 n
mi
Hp = 170
727
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4841203
85 X = 1545474
36
Y = -13110592
79 feet Y = -3979217
06 meter
Z = -17086906
04 Z = -5200750
72
XDOT = 24524
241238 XDOT = 7452
970347
YDOT = 4922
591796 feet/sec YDOT = 1583
872389 meter/sec
ZDOT = 3164
159329 ZDOT = 1000
695862
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2599780
85 X = 792413
20
Y = -13765664
61 feet Y = -4195774
57 meter
Z = -17059744
24 Z = -5199810
04
XDOT = 23984
237160 XDOT = 7310
395486
YDOT = 429
901672 feet/sec YDOT = 131
034030 meter/sec
ZDOT = 3300
917997 ZDOT = 1006
119805
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 07117
44653036
00020000 00000-0 20000-3 0 9118
2 25544 51
6349 6
0224 0016948 108
7675 251
5331 15
78606954 2762
Satellite: ISS
Catalog Number: 25544
Epoch time: 07117
44653036 = yrday
fracday
Element set: 911
Inclination: 51
6349 deg
RA of node: 6
0224 deg
Eccentricity:
0016948
Arg of perigee: 108
7675 deg
Mean anomaly: 251
5331 deg
Mean motion: 15
78606954 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 276
Checksum: 292
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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