Date:
December 11th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9526 06 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 86 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 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 3860)
---------------------------------------
Vector Time (GMT): 2007/344/13:31:02
895
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1019165
37 A = 6722729
95 meter
Y = -6598619
26 meter E =
0013190
Z = 723418
14 I = 51
33700
XDOT = 4687
254552 Wp = 47
97230
YDOT = 1384
043878 meter/sec RA = 273
80696 deg
ZDOT = 5960
326939 TA = 319
95699
MA = 320
05415
Ha = 184
794 n
mi
Hp = 179
100
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3343718
40 X = 1089362
11
Y = -21649013
31 feet Y = -6586830
01 meter
Z = 2373419
09 Z = 728538
68
XDOT = 15378
131733 XDOT = 4642
475078
YDOT = 4540
826371 feet/sec YDOT = 1436
208022 meter/sec
ZDOT = 19554
878409 ZDOT = 5982
989352
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21887886
81 X = 6671427
90
Y = -831157
03 feet Y = -253336
66 meter
Z = 2392266
12 Z = 729162
71
XDOT = -1626
991854 XDOT = -495
907117
YDOT = 14255
179561 feet/sec YDOT = 4344
978730 meter/sec
ZDOT = 19641
359678 ZDOT = 5986
686430
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 07344
62518908
00020000 00000-0 20000-3 0 9006
2 25544 51
6402 274
2052 0001120 306
3942 53
7120 15
77247577 38611
Satellite: ISS
Catalog Number: 25544
Epoch time: 07344
62518908 = yrday
fracday
Element set: 900
Inclination: 51
6402 deg
RA of node: 274
2052 deg
Eccentricity:
0001120
Arg of perigee: 306
3942 deg
Mean anomaly: 53
7120 deg
Mean motion: 15
77247577 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3861
Checksum: 269
Coasting Arc #2 (Orbit 3875)
---------------------------------------
Vector Time (GMT): 2007/345/13:31:02
895
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4001469
33 A = 6712123
67 meter
Y = -2209184
86 meter E =
0011790
Z = -4926042
80 I = 51
30164
XDOT = 1475
078707 Wp = 103
27949
YDOT = -7267
496996 meter/sec RA = 268
59935 deg
ZDOT = 2062
504132 TA = 186
79280
MA = 186
80880
Ha = 184
711 n
mi
Hp = 178
896
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13128180
23 X = -3952538
51
Y = -7247981
82 feet Y = -2253657
13 meter
Z = -16161557
75 Z = -4945363
60
XDOT = 4839
497069 XDOT = 1546
215992
YDOT = -23843
494083 feet/sec YDOT = -7250
604433 meter/sec
ZDOT = 6766
745840 ZDOT = 2069
841670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4402614
29 X = 1341916
84
Y = -14251564
81 feet Y = -4343876
95 meter
Z = -16235399
39 Z = -4948549
73
XDOT = 23281
839954 XDOT = 7096
304818
YDOT = -541
983645 feet/sec YDOT = -165
196615 meter/sec
ZDOT = 6793
969500 ZDOT = 2070
801904
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 07345
57554964
00020000 00000-0 20000-3 0 9014
2 25544 51
6407 269
3011 0001135 307
1469 52
9592 15
77301870 38762
Satellite: ISS
Catalog Number: 25544
Epoch time: 07345
57554964 = yrday
fracday
Element set: 901
Inclination: 51
6407 deg
RA of node: 269
3011 deg
Eccentricity:
0001135
Arg of perigee: 307
1469 deg
Mean anomaly: 52
9592 deg
Mean motion: 15
77301870 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3876
Checksum: 298
Coasting Arc #3 (Orbit 3891)
---------------------------------------
Vector Time (GMT): 2007/346/13:31:02
895
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1588275
98 A = 6719250
29 meter
Y = 5893131
26 meter E =
0003493
Z = -2810709
76 I = 51
32804
XDOT = -4507
982253 Wp = 116
22052
YDOT = -3634
018612 meter/sec RA = 263
45600 deg
ZDOT = -5078
361100 TA = 96
17531
MA = 96
13552
Ha = 184
647 n
mi
Hp = 178
982
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5210879
19 X = -1640401
87
Y = 19334420
15 feet Y = 5875079
26 meter
Z = -9221488
73 Z = -2818551
30
XDOT = -14789
968023 XDOT = -4442
341239
YDOT = -11922
633242 feet/sec YDOT = -3684
061589 meter/sec
ZDOT = -16661
289698 ZDOT = -5100
102083
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19998016
73 X = -6095395
50
Y = -715215
33 feet Y = -217997
63 meter
Z = -9250768
23 Z = -2819634
16
XDOT = 8291
384570 XDOT = 2527
214017
YDOT = -15526
941285 feet/sec YDOT = -4732
611704 meter/sec
ZDOT = -16744
509031 ZDOT = -5103
726353
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 07346
58924185
00020000 00000-0 20000-3 0 9023
2 25544 51
6408 264
0697 0001185 304
8935 55
2118 15
77328481 38927
Satellite: ISS
Catalog Number: 25544
Epoch time: 07346
58924185 = yrday
fracday
Element set: 902
Inclination: 51
6408 deg
RA of node: 264
0697 deg
Eccentricity:
0001185
Arg of perigee: 304
8935 deg
Mean anomaly: 55
2118 deg
Mean motion: 15
77328481 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3892
Checksum: 312
Coasting Arc #4 (Orbit 3907)
---------------------------------------
Vector Time (GMT): 2007/347/13:31:02
895
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3879249
82 A = 6716436
80 meter
Y = 4022488
08 meter E =
0011005
Z = 3718389
01 I = 51
32310
XDOT = -2202
269825 Wp = 78
47614
YDOT = 6051
696772 meter/sec RA = 258
22232 deg
ZDOT = -4236
341722 TA = 56
32237
MA = 56
21747
Ha = 184
561 n
mi
Hp = 178
839
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12727197
59 X = 3815918
18
Y = 13197139
36 feet Y = 4065513
41 meter
Z = 12199439
00 Z = 3737081
15
XDOT = -7225
294700 XDOT = -2249
197767
YDOT = 19854
648201 feet/sec YDOT = 6026
807965 meter/sec
ZDOT = -13898
758930 ZDOT = -4247
153464
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9776116
24 X = -2979760
23
Y = 15453809
10 feet Y = 4710321
01 meter
Z = 12271091
77 Z = 3740228
77
XDOT = -19862
279443 XDOT = -6054
022774
YDOT = -1463
414722 feet/sec YDOT = -446
048807 meter/sec
ZDOT = -13939
336440 ZDOT = -4248
709747
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 07347
60290724
00020000 00000-0 20000-3 0 9033
2 25544 51
6401 258
8382 0001165 315
8236 44
2836 15
77390404 39083
Satellite: ISS
Catalog Number: 25544
Epoch time: 07347
60290724 = yrday
fracday
Element set: 903
Inclination: 51
6401 deg
RA of node: 258
8382 deg
Eccentricity:
0001165
Arg of perigee: 315
8236 deg
Mean anomaly: 44
2836 deg
Mean motion: 15
77390404 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3908
Checksum: 288
Coasting Arc #5 (Orbit 3923)
---------------------------------------
Vector Time (GMT): 2007/348/13:31:02
895
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2314801
77 A = 6713948
71 meter
Y = -4503710
40 meter E =
0008180
Z = 4403224
87 I = 51
32225
XDOT = 4380
557388 Wp = 107
62164
YDOT = 5443
449779 meter/sec RA = 253
08787 deg
ZDOT = 3257
385256 TA = 309
57386
MA = 309
64608
Ha = 184
532 n
mi
Hp = 178
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7594493
98 X = 2343600
86
Y = -14775952
75 feet Y = -4477664
49 meter
Z = 14446275
81 Z = 4414539
56
XDOT = 14371
907442 XDOT = 4303
538570
YDOT = 17859
087201 feet/sec YDOT = 5492
004622 meter/sec
ZDOT = 10686
959501 ZDOT = 3278
479562
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16208638
03 X = 4940392
87
Y = 3471461
13 feet Y = 1058101
35 meter
Z = 14488927
30 Z = 4416225
04
XDOT = -13337
631796 XDOT = -4065
310171
YDOT = 17231
422505 feet/sec YDOT = 5252
137580 meter/sec
ZDOT = 10767
928476 ZDOT = 3282
064600
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 07348
61654575
00020000 00000-0 20000-3 0 9044
2 25544 51
6402 253
6059 0001192 318
3800 41
7274 15
77416501 39246
Satellite: ISS
Catalog Number: 25544
Epoch time: 07348
61654575 = yrday
fracday
Element set: 904
Inclination: 51
6402 deg
RA of node: 253
6059 deg
Eccentricity:
0001192
Arg of perigee: 318
3800 deg
Mean anomaly: 41
7274 deg
Mean motion: 15
77416501 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3924
Checksum: 282
Coasting Arc #6 (Orbit 3938)
---------------------------------------
Vector Time (GMT): 2007/349/13:31:02
895
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3715287
31 A = 6720852
16 meter
Y = -5296423
44 meter E =
0007631
Z = -1808002
13 I = 51
35571
XDOT = 3185
886445 Wp = 28
53600
YDOT = -4158
084223 meter/sec RA = 247
86294 deg
ZDOT = 5650
515727 TA = 311
30632
MA = 311
37198
Ha = 184
450 n
mi
Hp = 178
732
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12189262
84 X = -3647002
83
Y = -17376717
33 feet Y = -5337587
91 meter
Z = -5931765
52 Z = -1825885
66
XDOT = 10452
383350 XDOT = 3204
696829
YDOT = -13642
008605 feet/sec YDOT = -4122
353231 meter/sec
ZDOT = 18538
437425 ZDOT = 5666
038025
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13396701
85 X = 4083314
72
Y = -16438878
58 feet Y = -5010570
19 meter
Z = -6000493
84 Z = -1828950
52
XDOT = 14750
497842 XDOT = 4495
951742
YDOT = 5251
882739 feet/sec YDOT = 1600
773859 meter/sec
ZDOT = 18597
159936 ZDOT = 5668
414348
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 07349
56680703
00020000 00000-0 20000-3 0 9052
2 25544 51
6400 248
7005 0001330 317
4651 42
6411 15
77470641 39392
Satellite: ISS
Catalog Number: 25544
Epoch time: 07349
56680703 = yrday
fracday
Element set: 905
Inclination: 51
6400 deg
RA of node: 248
7005 deg
Eccentricity:
0001330
Arg of perigee: 317
4651 deg
Mean anomaly: 42
6411 deg
Mean motion: 15
77470641 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3939
Checksum: 276
Coasting Arc #7 (Orbit 3954)
---------------------------------------
Vector Time (GMT): 2007/350/13:31:02
895
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3311422
07 A = 6710275
38 meter
Y = 2664916
58 meter E =
0014028
Z = -5204488
71 I = 51
33202
XDOT = -4041
250840 Wp = 79
38658
YDOT = -6505
942992 meter/sec RA = 242
70272 deg
ZDOT = -759
202696 TA = 183
35061
MA = 183
36002
Ha = 184
407 n
mi
Hp = 178
554
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10864245
64 X = -3315692
94
Y = 8743164
62 feet Y = 2627862
94 meter
Z = -17075094
20 Z = -5220585
79
XDOT = -13258
696982 XDOT = -3964
511963
YDOT = -21344
957323 feet/sec YDOT = -6550
705418 meter/sec
ZDOT = -2490
822494 ZDOT = -778
649289
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11486760
06 X = -3501164
47
Y = -7774299
71 feet Y = -2369606
55 meter
Z = -17136166
73 Z = -5223103
62
XDOT = 16027
915744 XDOT = 4885
308719
YDOT = -18020
622907 feet/sec YDOT = -5492
685862 meter/sec
ZDOT = -2565
649226 ZDOT = -782
009884
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 07350
58039420
00020000 00000-0 20000-3 0 9061
2 25544 51
6394 243
4676 0001399 319
9145 40
1917 15
77525397 39551
Satellite: ISS
Catalog Number: 25544
Epoch time: 07350
58039420 = yrday
fracday
Element set: 906
Inclination: 51
6394 deg
RA of node: 243
4676 deg
Eccentricity:
0001399
Arg of perigee: 319
9145 deg
Mean anomaly: 40
1917 deg
Mean motion: 15
77525397 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3955
Checksum: 314
Coasting Arc #8 (Orbit 3970)
---------------------------------------
Vector Time (GMT): 2007/351/13:31:02
895
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3232710
16 A = 6722110
34 meter
Y = 5864704
96 meter E =
0009880
Z = -528950
85 I = 51
38636
XDOT = -4450
336609 Wp = 139
55827
YDOT = 1919
057568 meter/sec RA = 237
51887 deg
ZDOT = -5990
813980 TA = 46
22548
MA = 46
14377
Ha = 184
437 n
mi
Hp = 178
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10606004
47 X = 3169459
44
Y = 19241157
99 feet Y = 5900501
34 meter
Z = -1735403
04 Z = -513399
43
XDOT = -14600
841893 XDOT = -4442
362564
YDOT = 6296
120630 feet/sec YDOT = 1869
336425 meter/sec
ZDOT = -19654
901508 ZDOT = -6012
414340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15069558
40 X = -4593201
40
Y = 15994445
11 feet Y = 4875106
87 meter
Z = -1675485
16 Z = -510687
88
XDOT = -9261
780718 XDOT = -2822
990763
YDOT = -10768
915020 feet/sec YDOT = -3282
365298 meter/sec
ZDOT = -19737
034322 ZDOT = -6015
848061
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 07351
59395725
00020000 00000-0 20000-3 0 9077
2 25544 51
6395 238
2353 0001276 315
9364 44
1699 15
77504315 39715
Satellite: ISS
Catalog Number: 25544
Epoch time: 07351
59395725 = yrday
fracday
Element set: 907
Inclination: 51
6395 deg
RA of node: 238
2353 deg
Eccentricity:
0001276
Arg of perigee: 315
9364 deg
Mean anomaly: 44
1699 deg
Mean motion: 15
77504315 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3971
Checksum: 314
Coasting Arc #9 (Orbit 3986)
---------------------------------------
Vector Time (GMT): 2007/352/13:31:02
895
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4462257
40 A = 6711057
57 meter
Y = -708513
71 meter E =
0005836
Z = 4960332
61 I = 51
36674
XDOT = 3232
345962 Wp = 40
77985
YDOT = 6723
230270 meter/sec RA = 232
31531 deg
ZDOT = -1941
818836 TA = 68
06406
MA = 68
00204
Ha = 184
158 n
mi
Hp = 178
554
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14639952
10 X = 4445751
80
Y = -2324520
05 feet Y = -658706
91 meter
Z = 16274057
10 Z = 4981970
34
XDOT = 10604
809586 XDOT = 3166
358650
YDOT = 22057
842093 feet/sec YDOT = 6759
007402 meter/sec
ZDOT = -6370
796707 ZDOT = -1926
275659
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6889866
32 X = 2100031
26
Y = 13021990
24 feet Y = 3969102
62 meter
Z = 16356467
77 Z = 4985451
38
XDOT = -16500
907136 XDOT = -5029
476495
YDOT = 16680
471042 feet/sec YDOT = 5084
207574 meter/sec
ZDOT = -6310
811687 ZDOT = -1923
535402
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 07352
60749198
00020000 00000-0 20000-3 0 9088
2 25544 51
6393 233
0018 0001500 321
9844 38
1215 15
77608936 39872
Satellite: ISS
Catalog Number: 25544
Epoch time: 07352
60749198 = yrday
fracday
Element set: 908
Inclination: 51
6393 deg
RA of node: 233
0018 deg
Eccentricity:
0001500
Arg of perigee: 321
9844 deg
Mean anomaly: 38
1215 deg
Mean motion: 15
77608936 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3987
Checksum: 302
Coasting Arc #10 (Orbit 4002)
---------------------------------------
Vector Time (GMT): 2007/353/13:31:02
895
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2246800
67 A = 6718538
15 meter
Y = -5682973
70 meter E =
0012997
Z = 2776143
72 I = 51
40984
XDOT = 5768
382205 Wp = 73
76052
YDOT = 223
902070 meter/sec RA = 227
17300 deg
ZDOT = 5110
700183 TA = 318
18832
MA = 318
28754
Ha = 184
271 n
mi
Hp = 178
532
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7371393
29 X = -2196572
01
Y = -18644926
85 feet Y = -5707818
14 meter
Z = 9108083
08 Z = 2765350
04
XDOT = 18925
138467 XDOT = 5740
622556
YDOT = 734
586844 feet/sec YDOT = 288
251667 meter/sec
ZDOT = 16767
389052 ZDOT = 5138
655992
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15030515
86 X = 4581301
23
Y = -13297121
27 feet Y = -4052962
56 meter
Z = 9066315
26 Z = 2763412
89
XDOT = 4714
685035 XDOT = 1437
035999
YDOT = 16870
665131 feet/sec YDOT = 5142
178732 meter/sec
ZDOT = 16873
993853 ZDOT = 5143
193326
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 07353
62100392
00020000 00000-0 20000-3 0 9099
2 25544 51
6383 227
7681 0001568 324
1492 35
9568 15
77630163 40038
Satellite: ISS
Catalog Number: 25544
Epoch time: 07353
62100392 = yrday
fracday
Element set: 909
Inclination: 51
6383 deg
RA of node: 227
7681 deg
Eccentricity:
0001568
Arg of perigee: 324
1492 deg
Mean anomaly: 35
9568 deg
Mean motion: 15
77630163 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4003
Checksum: 289
Coasting Arc #11 (Orbit 4017)
---------------------------------------
Vector Time (GMT): 2007/354/13:31:02
895
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5522388
56 A = 6715715
50 meter
Y = -1003121
76 meter E =
0004971
Z = -3691846
21 I = 51
42071
XDOT = -1741
592831 Wp = 90
73990
YDOT = -6158
766699 meter/sec RA = 221
94295 deg
ZDOT = 4283
441681 TA = 224
59494
MA = 224
63494
Ha = 184
200 n
mi
Hp = 178
334
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18118072
71 X = -5492826
45
Y = -3291081
89 feet Y = -1064710
47 meter
Z = -12112356
32 Z = -3718602
73
XDOT = -5713
887242 XDOT = -1693
403644
YDOT = -20205
927491 feet/sec YDOT = -6177
973295 meter/sec
ZDOT = 14053
286356 ZDOT = 4275
097140
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3325326
44 X = -1013559
50
Y = -18043103
53 feet Y = -5499537
96 meter
Z = -12214482
11 Z = -3722974
15
XDOT = 15521
357565 XDOT = 4730
909786
YDOT = -12341
336738 feet/sec YDOT = -3761
639438 meter/sec
ZDOT = 14020
804120 ZDOT = 4273
541096
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 07354
57114861
00020000 00000-0 20000-3 0 9102
2 25544 51
6373 222
8613 0001516 327
0346 33
0725 15
77664153 40187
Satellite: ISS
Catalog Number: 25544
Epoch time: 07354
57114861 = yrday
fracday
Element set: 910
Inclination: 51
6373 deg
RA of node: 222
8613 deg
Eccentricity:
0001516
Arg of perigee: 327
0346 deg
Mean anomaly: 33
0725 deg
Mean motion: 15
77664153 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4018
Checksum: 271
Coasting Arc #12 (Orbit 4033)
---------------------------------------
Vector Time (GMT): 2007/355/13:31:02
895
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 626835
29 A = 6712870
35 meter
Y = 4950805
66 meter E =
0009815
Z = -4499741
68 I = 51
43236
XDOT = -6762
979916 Wp = 60
93729
YDOT = -1967
343327 meter/sec RA = 216
81386 deg
ZDOT = -3107
066051 TA = 177
98639
MA = 177
98244
Ha = 184
235 n
mi
Hp = 178
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2056546
23 X = 593287
28
Y = 16242800
72 feet Y = 4957628
44 meter
Z = -14762932
03 Z = -4496777
16
XDOT = -22188
254317 XDOT = -6725
384361
YDOT = -6454
538475 feet/sec YDOT = -2042
760091 meter/sec
ZDOT = -10193
786255 ZDOT = -3139
830084
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14291873
11 X = -4356162
92
Y = 8009349
53 feet Y = 2441249
74 meter
Z = -14751094
96 Z = -4496133
74
XDOT = -1626
134053 XDOT = -495
645659
YDOT = -21904
010125 feet/sec YDOT = -6676
342286 meter/sec
ZDOT = -10318
935158 ZDOT = -3145
211436
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 07355
58461230
00020000 00000-0 20000-3 0 9110
2 25544 51
6360 217
6281 0001531 331
4014 28
7067 15
77693912 40347
Satellite: ISS
Catalog Number: 25544
Epoch time: 07355
58461230 = yrday
fracday
Element set: 911
Inclination: 51
6360 deg
RA of node: 217
6281 deg
Eccentricity:
0001531
Arg of perigee: 331
4014 deg
Mean anomaly: 28
7067 deg
Mean motion: 15
77693912 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4034
Checksum: 269
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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