Date:
December 1st 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6996 54 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 3701)
---------------------------------------
Vector Time (GMT): 2007/334/12:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5170404
33 A = 6716069
31 meter
Y = -584050
02 meter E =
0007826
Z = -4254373
74 I = 51
44831
XDOT = 3566
896169 Wp = 68
75915
YDOT = -5833
621692 meter/sec RA = 325
78406 deg
ZDOT = -3536
470424 TA = 165
27753
MA = 165
25472
Ha = 185
413 n
mi
Hp = 179
558
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16963268
81 X = -5142822
04
Y = -1916174
60 feet Y = -641713
83 meter
Z = -13957919
11 Z = -4279424
75
XDOT = 11702
415252 XDOT = 3649
043129
YDOT = -19139
178778 feet/sec YDOT = -5793
275030 meter/sec
ZDOT = -11602
593254 ZDOT = -3518
943313
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5309616
17 X = 1618371
01
Y = -16141806
92 feet Y = -4920022
75 meter
Z = -14053389
81 Z = -4283473
22
XDOT = 15169
168773 XDOT = 4623
562642
YDOT = 15026
650312 feet/sec YDOT = 4580
123015 meter/sec
ZDOT = -11536
410568 ZDOT = -3516
297941
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 07334
54991906
00020000 00000-0 20000-3 0 9009
2 25544 51
6372 326
1750 0000833 252
0944 108
0130 15
76854572 37025
Satellite: ISS
Catalog Number: 25544
Epoch time: 07334
54991906 = yrday
fracday
Element set: 900
Inclination: 51
6372 deg
RA of node: 326
1750 deg
Eccentricity:
0000833
Arg of perigee: 252
0944 deg
Mean anomaly: 108
0130 deg
Mean motion: 15
76854572 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3702
Checksum: 276
Coasting Arc #2 (Orbit 3717)
---------------------------------------
Vector Time (GMT): 2007/335/12:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3554997
86 A = 6721748
82 meter
Y = 5237477
52 meter E =
0013198
Z = 2242478
82 I = 51
44442
XDOT = -5305
173301 Wp = 109
48060
YDOT = -1259
090025 meter/sec RA = 320
56786 deg
ZDOT = -5447
971161 TA = 45
24124
MA = 45
13392
Ha = 185
312 n
mi
Hp = 179
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11663378
79 X = -3624193
55
Y = 17183325
21 feet Y = 5197336
47 meter
Z = 7357213
97 Z = 2225040
80
XDOT = -17405
424217 XDOT = -5264
234216
YDOT = -4130
872785 feet/sec YDOT = -1318
186197 meter/sec
ZDOT = -17873
921132 ZDOT = -5473
644534
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14699171
46 X = -4480307
46
Y = -14703765
99 feet Y = -4481707
87 meter
Z = 7291316
19 Z = 2222393
17
XDOT = 6213
130971 XDOT = 1893
762320
YDOT = -15158
554284 feet/sec YDOT = -4620
327346 meter/sec
ZDOT = -17971
829939 ZDOT = -5477
813765
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 07335
56389216
00020000 00000-0 20000-3 0 9018
2 25544 51
6371 320
9454 0000910 268
5144 91
5916 15
76913434 37185
Satellite: ISS
Catalog Number: 25544
Epoch time: 07335
56389216 = yrday
fracday
Element set: 901
Inclination: 51
6371 deg
RA of node: 320
9454 deg
Eccentricity:
0000910
Arg of perigee: 268
5144 deg
Mean anomaly: 91
5916 deg
Mean motion: 15
76913434 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3718
Checksum: 295
Coasting Arc #3 (Orbit 3733)
---------------------------------------
Vector Time (GMT): 2007/336/12:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4052108
95 A = 6712494
44 meter
Y = 1695497
71 meter E =
0003961
Z = 5073898
04 I = 51
39184
XDOT = -4460
471077 Wp = 133
51501
YDOT = 6099
043401 meter/sec RA = 315
42757 deg
ZDOT = 1520
723773 TA = 301
84090
MA = 301
87945
Ha = 185
133 n
mi
Hp = 179
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13294320
69 X = 4008200
12
Y = 5562656
51 feet Y = 1740564
86 meter
Z = 16646647
10 Z = 5093476
85
XDOT = -14634
091459 XDOT = -4535
727475
YDOT = 20009
984913 feet/sec YDOT = 6048
743009 meter/sec
ZDOT = 4989
251224 ZDOT = 1498
872147
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7720261
81 X = -2353135
80
Y = 12065891
60 feet Y = 3677683
76 meter
Z = 16721387
12 Z = 5096678
79
XDOT = -16354
368557 XDOT = -4984
811536
YDOT = -17279
538505 feet/sec YDOT = -5266
803336 meter/sec
ZDOT = 4906
632656 ZDOT = 1495
541633
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 07336
57784616
00020000 00000-0 20000-3 0 9024
2 25544 51
6370 315
7158 0000956 270
1217 89
9838 15
76932314 37347
Satellite: ISS
Catalog Number: 25544
Epoch time: 07336
57784616 = yrday
fracday
Element set: 902
Inclination: 51
6370 deg
RA of node: 315
7158 deg
Eccentricity:
0000956
Arg of perigee: 270
1217 deg
Mean anomaly: 89
9838 deg
Mean motion: 15
76932314 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3734
Checksum: 313
Coasting Arc #4 (Orbit 3748)
---------------------------------------
Vector Time (GMT): 2007/337/12:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4115871
74 A = 6723673
51 meter
Y = -5298228
82 meter E =
0011016
Z = -351297
64 I = 51
40989
XDOT = 3990
378158 Wp = 39
26735
YDOT = 2708
750448 meter/sec RA = 310
23626 deg
ZDOT = 6009
844317 TA = 316
89676
MA = 316
98297
Ha = 185
241 n
mi
Hp = 179
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13503516
22 X = 4176518
01
Y = -17382640
48 feet Y = -5251863
69 meter
Z = -1152551
32 Z = -331155
47
XDOT = 13091
791856 XDOT = 3930
596746
YDOT = 8886
976534 feet/sec YDOT = 2753
038473 meter/sec
ZDOT = 19717
336998 ZDOT = 6029
084833
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15117814
62 X = 4607909
90
Y = 16003831
80 feet Y = 4877967
93 meter
Z = -1076366
02 Z = -328076
36
XDOT = -9596
403371 XDOT = -2924
983747
YDOT = 10370
000989 feet/sec YDOT = 3160
776301 meter/sec
ZDOT = 19790
890068 ZDOT = 6032
263293
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 07337
52840931
00020000 00000-0 20000-3 0 9034
2 25544 51
6367 310
8126 0000815 266
4510 93
6562 15
76975076 37496
Satellite: ISS
Catalog Number: 25544
Epoch time: 07337
52840931 = yrday
fracday
Element set: 903
Inclination: 51
6367 deg
RA of node: 310
8126 deg
Eccentricity:
0000815
Arg of perigee: 266
4510 deg
Mean anomaly: 93
6562 deg
Mean motion: 15
76975076 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3749
Checksum: 302
Coasting Arc #5 (Orbit 3764)
---------------------------------------
Vector Time (GMT): 2007/338/12:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2923292
32 A = 6711827
34 meter
Y = -3083679
34 meter E =
0013840
Z = -5207556
02 I = 51
35277
XDOT = 4880
002577 Wp = 95
55721
YDOT = -5902
340362 meter/sec RA = 305
05574 deg
ZDOT = 756
081469 TA = 181
66720
MA = 181
67182
Ha = 185
196 n
mi
Hp = 179
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9590854
06 X = -2863295
04
Y = -10117058
19 feet Y = -3116033
40 meter
Z = -17085157
53 Z = -5221612
13
XDOT = 16010
507141 XDOT = 4941
967772
YDOT = -19364
633735 feet/sec YDOT = -5847
422999 meter/sec
ZDOT = 2480
582247 ZDOT = 779
939040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11310669
34 X = 3447492
01
Y = -8035253
97 feet Y = -2449145
41 meter
Z = -17139002
56 Z = -5223967
98
XDOT = 16431
574289 XDOT = 5008
343843
YDOT = 17648
804064 feet/sec YDOT = 5379
355479 meter/sec
ZDOT = 2570
857305 ZDOT = 783
597306
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 07338
54232361
00020000 00000-0 20000-3 0 9040
2 25544 51
6374 305
5818 0000919 280
1234 79
9827 15
76979250 37651
Satellite: ISS
Catalog Number: 25544
Epoch time: 07338
54232361 = yrday
fracday
Element set: 904
Inclination: 51
6374 deg
RA of node: 305
5818 deg
Eccentricity:
0000919
Arg of perigee: 280
1234 deg
Mean anomaly: 79
9827 deg
Mean motion: 15
76979250 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3765
Checksum: 313
Coasting Arc #6 (Orbit 3780)
---------------------------------------
Vector Time (GMT): 2007/339/12:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4326400
42 A = 6722346
02 meter
Y = 4866706
98 meter E =
0007012
Z = -1657703
12 I = 51
37378
XDOT = -2745
578164 Wp = 146
80023
YDOT = -4380
362517 meter/sec RA = 299
89981 deg
ZDOT = -5711
462137 TA = 51
60807
MA = 51
54511
Ha = 185
101 n
mi
Hp = 179
432
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14194227
09 X = -4372446
13
Y = 15966886
41 feet Y = 4818069
41 meter
Z = -5438658
54 Z = -1678832
63
XDOT = -9007
802375 XDOT = -2668
646391
YDOT = -14371
268102 feet/sec YDOT = -4410
634462 meter/sec
ZDOT = -18738
392839 ZDOT = -5724
613967
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14176148
34 X = -4320890
01
Y = -15955497
16 feet Y = -4863235
53 meter
Z = -5518648
33 Z = -1682084
01
XDOT = 14161
335038 XDOT = 4316
374920
YDOT = -6102
588321 feet/sec YDOT = -1860
068920 meter/sec
ZDOT = -18788
923821 ZDOT = -5726
863981
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 07339
55621734
00020000 00000-0 20000-3 0 9059
2 25544 51
6380 300
3514 0000957 287
0872 73
0188 15
77025139 37812
Satellite: ISS
Catalog Number: 25544
Epoch time: 07339
55621734 = yrday
fracday
Element set: 905
Inclination: 51
6380 deg
RA of node: 300
3514 deg
Eccentricity:
0000957
Arg of perigee: 287
0872 deg
Mean anomaly: 73
0188 deg
Mean motion: 15
77025139 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3781
Checksum: 293
Coasting Arc #7 (Orbit 3796)
---------------------------------------
Vector Time (GMT): 2007/340/12:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1928486
56 A = 6714385
65 meter
Y = 4534969
19 meter E =
0007822
Z = 4556555
68 I = 51
33402
XDOT = -4958
618997 Wp = 60
04330
YDOT = 5099
768754 meter/sec RA = 294
68252 deg
ZDOT = -2969
301949 TA = 59
55785
MA = 59
48060
Ha = 185
031 n
mi
Hp = 179
407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6327055
64 X = 1855497
10
Y = 14878507
85 feet Y = 4556126
01 meter
Z = 14949329
66 Z = 4565747
68
XDOT = -16268
435029 XDOT = -5000
852195
YDOT = 16731
524784 feet/sec YDOT = 5044
082856 meter/sec
ZDOT = -9741
804294 ZDOT = -2993
493483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15434794
40 X = -4704525
33
Y = 4701824
12 feet Y = 1433115
99 meter
Z = 14984794
22 Z = 4567365
28
XDOT = -14658
492014 XDOT = -4467
908366
YDOT = -16700
624617 feet/sec YDOT = -5090
350383 meter/sec
ZDOT = -9833
436711 ZDOT = -2997
231510
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 07340
57009089
00020000 00000-0 20000-3 0 9067
2 25544 51
6383 295
1213 0000964 289
5649 70
5411 15
77054116 37974
Satellite: ISS
Catalog Number: 25544
Epoch time: 07340
57009089 = yrday
fracday
Element set: 906
Inclination: 51
6383 deg
RA of node: 295
1213 deg
Eccentricity:
0000964
Arg of perigee: 289
5649 deg
Mean anomaly: 70
5411 deg
Mean motion: 15
77054116 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3797
Checksum: 303
Coasting Arc #8 (Orbit 3812)
---------------------------------------
Vector Time (GMT): 2007/341/12:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4282777
18 A = 6718186
62 meter
Y = -3872391
13 meter E =
0011508
Z = 3424627
43 I = 51
33681
XDOT = 1746
196254 Wp = 89
66675
YDOT = 5969
780498 meter/sec RA = 289
55028 deg
ZDOT = 4553
468324 TA = 311
12643
MA = 311
22570
Ha = 184
947 n
mi
Hp = 179
323
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14051106
23 X = 4309123
96
Y = -12704695
32 feet Y = -3824351
82 meter
Z = 11235654
29 Z = 3445497
11
XDOT = 5728
990334 XDOT = 1657
191076
YDOT = 19585
894023 feet/sec YDOT = 5988
809209 meter/sec
ZDOT = 14939
200538 ZDOT = 4561
736109
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11480815
50 X = 3499352
57
Y = 15008326
02 feet Y = 4574537
77 meter
Z = 11314761
26 Z = 3448739
23
XDOT = -18897
463175 XDOT = -5759
946776
YDOT = 3136
876178 feet/sec YDOT = 956
119859 meter/sec
ZDOT = 14971
288594 ZDOT = 4563
248763
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 07341
58394327
00020000 00000-0 20000-3 0 9072
2 25544 51
6387 289
8907 0000963 289
7015 70
4046 15
77098154 38138
Satellite: ISS
Catalog Number: 25544
Epoch time: 07341
58394327 = yrday
fracday
Element set: 907
Inclination: 51
6387 deg
RA of node: 289
8907 deg
Eccentricity:
0000963
Arg of perigee: 289
7015 deg
Mean anomaly: 70
4046 deg
Mean motion: 15
77098154 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3813
Checksum: 322
Coasting Arc #9 (Orbit 3827)
---------------------------------------
Vector Time (GMT): 2007/342/12:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1176943
22 A = 6718830
90 meter
Y = -5783693
32 meter E =
0003817
Z = -3212219
20 I = 51
33050
XDOT = 4852
989760 Wp = 72
58525
YDOT = -3625
496491 meter/sec RA = 284
31750 deg
ZDOT = 4755
463590 TA = 249
66179
MA = 249
70281
Ha = 184
993 n
mi
Hp = 179
307
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3861362
26 X = -1096576
92
Y = -18975371
79 feet Y = -5796404
74 meter
Z = -10538776
91 Z = -3217742
55
XDOT = 15921
882416 XDOT = 4870
068294
YDOT = -11894
673526 feet/sec YDOT = -3571
132823 meter/sec
ZDOT = 15601
914665 ZDOT = 4779
080826
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19187749
58 X = 5848426
07
Y = -2519726
80 feet Y = -768012
73 meter
Z = -10560393
67 Z = -3218807
99
XDOT = 10621
438277 XDOT = 3237
414387
YDOT = 15197
002660 feet/sec YDOT = 4632
046411 meter/sec
ZDOT = 15691
517716 ZDOT = 4782
774600
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 07342
53441239
00020000 00000-0 20000-3 0 9084
2 25544 51
6386 284
9869 0001054 298
2990 61
8068 15
77104748 38280
Satellite: ISS
Catalog Number: 25544
Epoch time: 07342
53441239 = yrday
fracday
Element set: 908
Inclination: 51
6386 deg
RA of node: 284
9869 deg
Eccentricity:
0001054
Arg of perigee: 298
2990 deg
Mean anomaly: 61
8068 deg
Mean motion: 15
77104748 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3828
Checksum: 326
Coasting Arc #10 (Orbit 3843)
---------------------------------------
Vector Time (GMT): 2007/343/12:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4196172
35 A = 6713432
97 meter
Y = 2318207
50 meter E =
0010850
Z = -4710194
79 I = 51
30774
XDOT = -988
223490 Wp = 67
09870
YDOT = -7160
652827 meter/sec RA = 279
18109 deg
ZDOT = -2644
534067 TA = 176
78868
MA = 176
78171
Ha = 184
964 n
mi
Hp = 179
082
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13766969
65 X = -4198901
39
Y = 7605667
66 feet Y = 2271269
03 meter
Z = -15453394
97 Z = -4730586
38
XDOT = -3242
203052 XDOT = -895
231663
YDOT = -23492
955468 feet/sec YDOT = -7171
183329 meter/sec
ZDOT = -8676
292871 ZDOT = -2649
110216
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6912979
58 X = -2107076
18
Y = -14042313
15 feet Y = -4280097
05 meter
Z = -15530846
88 Z = -4733802
13
XDOT = 22599
136527 XDOT = 6888
216814
YDOT = -1511
803265 feet/sec YDOT = -460
797635 meter/sec
ZDOT = -8694
441175 ZDOT = -2650
065670
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 07343
54822598
00020000 00000-0 20000-3 0 9098
2 25544 51
6395 279
7560 0000976 304
9302 55
1771 15
77160713 38443
Satellite: ISS
Catalog Number: 25544
Epoch time: 07343
54822598 = yrday
fracday
Element set: 909
Inclination: 51
6395 deg
RA of node: 279
7560 deg
Eccentricity:
0000976
Arg of perigee: 304
9302 deg
Mean anomaly: 55
1771 deg
Mean motion: 15
77160713 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3844
Checksum: 313
Coasting Arc #11 (Orbit 3859)
---------------------------------------
Vector Time (GMT): 2007/344/12:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 589439
16 A = 6722429
20 meter
Y = 6562431
71 meter E =
0013025
Z = 1302078
77 I = 51
33511
XDOT = -4785
014604 Wp = 120
22188
YDOT = 1593
485328 meter/sec RA = 273
96545 deg
ZDOT = -5828
141271 TA = 45
40169
MA = 45
29549
Ha = 184
948 n
mi
Hp = 179
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1933855
53 X = 509687
91
Y = 21530287
76 feet Y = 6568577
02 meter
Z = 4271911
96 Z = 1304749
70
XDOT = -15698
866811 XDOT = -4774
165184
YDOT = 5227
970235 feet/sec YDOT = 1540
038239 meter/sec
ZDOT = -19121
198396 ZDOT = -5851
360521
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21581290
25 X = -6577977
27
Y = 1203460
21 feet Y = 366814
67 meter
Z = 4282746
21 Z = 1305381
04
XDOT = -4626
719808 XDOT = -1410
224197
YDOT = -14179
839960 feet/sec YDOT = -4322
015220 meter/sec
ZDOT = -19209
502218 ZDOT = -5855
056276
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
56201970
00020000 00000-0 20000-3 0 9108
2 25544 51
6397 274
5254 0000969 305
5495 54
5579 15
77171264 38600
Satellite: ISS
Catalog Number: 25544
Epoch time: 07344
56201970 = yrday
fracday
Element set: 910
Inclination: 51
6397 deg
RA of node: 274
5254 deg
Eccentricity:
0000969
Arg of perigee: 305
5495 deg
Mean anomaly: 54
5579 deg
Mean motion: 15
77171264 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3860
Checksum: 310
Coasting Arc #12 (Orbit 3875)
---------------------------------------
Vector Time (GMT): 2007/345/12:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4183509
22 A = 6710881
82 meter
Y = -403110
54 meter E =
0001495
Z = 5230509
12 I = 51
29588
XDOT = 387
927850 Wp = 88
27379
YDOT = 7693
086022 meter/sec RA = 268
79782 deg
ZDOT = 282
598474 TA = 359
03330
MA = 359
03358
Ha = 184
660 n
mi
Hp = 179
120
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13725423
93 X = 4162296
89
Y = -1322541
14 feet Y = -356447
66 meter
Z = 17160463
00 Z = 5250781
16
XDOT = 1272
729167 XDOT = 300
500940
YDOT = 25239
783538 feet/sec YDOT = 7696
935175 meter/sec
ZDOT = 927
160347 ZDOT = 284
271992
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1110337
55 X = 338430
88
Y = 13647268
17 feet Y = 4159687
34 meter
Z = 17237664
85 Z = 5254040
25
XDOT = -24261
274345 XDOT = -7394
836420
YDOT = 793
668144 feet/sec YDOT = 241
910050 meter/sec
ZDOT = 934
314374 ZDOT = 284
779021
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
57579129
00020000 00000-0 20000-3 0 9115
2 25544 51
6394 269
2949 0001118 304
3459 55
7600 15
77247580 38763
Satellite: ISS
Catalog Number: 25544
Epoch time: 07345
57579129 = yrday
fracday
Element set: 911
Inclination: 51
6394 deg
RA of node: 269
2949 deg
Eccentricity:
0001118
Arg of perigee: 304
3459 deg
Mean anomaly: 55
7600 deg
Mean motion: 15
77247580 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3876
Checksum: 320
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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