Date:
September 28th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 3982 65 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 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 2676)
---------------------------------------
Vector Time (GMT): 2007/269/12:45:08
773
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4833265
85 A = 6719513
42 meter
Y = 1013871
72 meter E =
0012722
Z = -4569264
53 I = 51
34585
XDOT = 1341
020779 Wp = 64
18232
YDOT = -6969
537371 meter/sec RA = 300
41782 deg
ZDOT = -2965
916021 TA = 176
23582
MA = 176
22624
Ha = 188
902 n
mi
Hp = 181
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15857171
42 X = -4822047
01
Y = 3326350
80 feet Y = 959885
67 meter
Z = -14991025
35 Z = -4592717
61
XDOT = 4399
674472 XDOT = 1433
263548
YDOT = -22865
936257 feet/sec YDOT = -6954
025869 meter/sec
ZDOT = -9730
695607 ZDOT = -2959
176500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14311054
18 X = 4362009
31
Y = -7418551
99 feet Y = -2261174
65 meter
Z = -15079925
43 Z = -4596361
27
XDOT = 1274
142701 XDOT = 388
358695
YDOT = 22181
282765 feet/sec YDOT = 6760
854987 meter/sec
ZDOT = -9705
967160 ZDOT = -2958
378790
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 07269
55241681
00020000 00000-0 20000-3 0 9005
2 25544 51
6347 300
8975 0002511 40
2562 319
8787 15
75225537 26775
Satellite: ISS
Catalog Number: 25544
Epoch time: 07269
55241681 = yrday
fracday
Element set: 900
Inclination: 51
6347 deg
RA of node: 300
8975 deg
Eccentricity:
0002511
Arg of perigee: 40
2562 deg
Mean anomaly: 319
8787 deg
Mean motion: 15
75225537 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2677
Checksum: 302
Coasting Arc #2 (Orbit 2692)
---------------------------------------
Vector Time (GMT): 2007/270/12:45:08
773
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1007895
28 A = 6726508
88 meter
Y = 6270075
07 meter E =
0015360
Z = 2199461
93 I = 51
35465
XDOT = -5329
178223 Wp = 99
60417
YDOT = 1069
304957 meter/sec RA = 295
20903 deg
ZDOT = -5460
557700 TA = 55
62287
MA = 55
47769
Ha = 188
934 n
mi
Hp = 181
143
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3306743
05 X = -1088618
06
Y = 20571112
42 feet Y = 6258353
07 meter
Z = 7216082
46 Z = 2194368
83
XDOT = -17484
180522 XDOT = -5314
212430
YDOT = 3508
218364 feet/sec YDOT = 1009
794241 meter/sec
ZDOT = -17915
215551 ZDOT = -5486
411018
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2625025
39 X = -800107
74
Y = -20675637
98 feet Y = -6301934
46 meter
Z = 7197520
25 Z = 2193804
17
XDOT = 14166
442453 XDOT = 4317
931660
YDOT = -8103
437450 feet/sec YDOT = -2469
927735 meter/sec
ZDOT = -18013
216954 ZDOT = -5490
428528
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 07270
56745246
00020000 00000-0 20000-3 0 9015
2 25544 51
6332 295
6738 0002672 43
6985 316
4390 15
75258251 26931
Satellite: ISS
Catalog Number: 25544
Epoch time: 07270
56745246 = yrday
fracday
Element set: 901
Inclination: 51
6332 deg
RA of node: 295
6738 deg
Eccentricity:
0002672
Arg of perigee: 43
6985 deg
Mean anomaly: 316
4390 deg
Mean motion: 15
75258251 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2693
Checksum: 308
Coasting Arc #3 (Orbit 2708)
---------------------------------------
Vector Time (GMT): 2007/271/12:45:08
773
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4494102
55 A = 6717920
23 meter
Y = -819018
54 meter E =
0007166
Z = 4920175
56 I = 51
31408
XDOT = -927
887031 Wp = 102
31180
YDOT = 7366
219561 meter/sec RA = 290
07779 deg
ZDOT = 2069
682690 TA = 327
54486
MA = 327
58891
Ha = 188
827 n
mi
Hp = 181
104
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14744430
95 X = 4479025
09
Y = -2687068
69 feet Y = -768846
91 meter
Z = 16142308
26 Z = 4941971
80
XDOT = -3044
248790 XDOT = -1020
242597
YDOT = 24167
387010 feet/sec YDOT = 7355
327158 meter/sec
ZDOT = 6790
297538 ZDOT = 2064
950082
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13171636
66 X = -4014714
85
Y = 6960746
94 feet Y = 2121635
67 meter
Z = 16224940
31 Z = 4945361
81
XDOT = -3804
600248 XDOT = -1159
642156
YDOT = -23017
968092 feet/sec YDOT = -7015
876675 meter/sec
ZDOT = 6773
237227 ZDOT = 2064
482707
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 07271
58247465
00020000 00000-0 20000-3 0 9029
2 25544 51
6325 290
4499 0002670 46
7533 313
3854 15
75260295 27091
Satellite: ISS
Catalog Number: 25544
Epoch time: 07271
58247465 = yrday
fracday
Element set: 902
Inclination: 51
6325 deg
RA of node: 290
4499 deg
Eccentricity:
0002670
Arg of perigee: 46
7533 deg
Mean anomaly: 313
3854 deg
Mean motion: 15
75260295 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2709
Checksum: 302
Coasting Arc #4 (Orbit 2723)
---------------------------------------
Vector Time (GMT): 2007/272/12:45:08
773
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 589125
38 A = 6727556
91 meter
Y = -6551367
31 meter E =
0011262
Z = -1391214
25 I = 51
33909
XDOT = 5007
533158 Wp = 40
63607
YDOT = -774
149753 meter/sec RA = 284
88021 deg
ZDOT = 5800
777321 TA = 303
99722
MA = 304
10416
Ha = 188
876 n
mi
Hp = 180
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1932826
05 X = 669098
39
Y = -21493987
24 feet Y = -6544332
28 meter
Z = -4564351
21 Z = -1388157
72
XDOT = 16428
914562 XDOT = 4987
637874
YDOT = -2539
861393 feet/sec YDOT = -718
263717 meter/sec
ZDOT = 19031
421657 ZDOT = 5825
056169
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4944150
69 X = 1506977
13
Y = 21009073
32 feet Y = 6403565
55 meter
Z = -4553550
08 Z = -1387922
06
XDOT = -13147
001409 XDOT = -4007
206030
YDOT = 7214
044532 feet/sec YDOT = 2198
840773 meter/sec
ZDOT = 19123
484501 ZDOT = 5828
838076
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 07272
53404466
00020000 00000-0 20000-3 0 9032
2 25544 51
6331 285
5538 0002637 52
4820 307
6584 15
75327670 27247
Satellite: ISS
Catalog Number: 25544
Epoch time: 07272
53404466 = yrday
fracday
Element set: 903
Inclination: 51
6331 deg
RA of node: 285
5538 deg
Eccentricity:
0002637
Arg of perigee: 52
4820 deg
Mean anomaly: 307
6584 deg
Mean motion: 15
75327670 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2724
Checksum: 291
Coasting Arc #5 (Orbit 2739)
---------------------------------------
Vector Time (GMT): 2007/273/12:45:08
773
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4283142
65 A = 6716799
53 meter
Y = 486692
23 meter E =
0016820
Z = -5165748
62 I = 51
29548
XDOT = 431
503913 Wp = 77
13547
YDOT = -7603
056184 meter/sec RA = 279
73297 deg
ZDOT = -1073
348932 TA = 182
55775
MA = 182
56636
Ha = 188
940 n
mi
Hp = 180
848
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14052305
28 X = -4263171
79
Y = 1596759
28 feet Y = 438907
33 meter
Z = -16947994
17 Z = -5186508
05
XDOT = 1415
695254 XDOT = 521
704599
YDOT = -24944
410053 feet/sec YDOT = -7597
726533 meter/sec
ZDOT = -3521
485997 ZDOT = -1071
033487
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12630229
40 X = 3849693
92
Y = -6149711
82 feet Y = -1874432
16 meter
Z = -17026737
21 Z = -5189749
50
XDOT = 6497
606539 XDOT = 1980
470473
YDOT = 23079
728320 feet/sec YDOT = 7034
701192 meter/sec
ZDOT = -3513
623322 ZDOT = -1070
952389
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 07273
54903950
00020000 00000-0 20000-3 0 9047
2 25544 51
6323 280
3294 0002666 51
8662 308
2742 15
75295150 27407
Satellite: ISS
Catalog Number: 25544
Epoch time: 07273
54903950 = yrday
fracday
Element set: 904
Inclination: 51
6323 deg
RA of node: 280
3294 deg
Eccentricity:
0002666
Arg of perigee: 51
8662 deg
Mean anomaly: 308
2742 deg
Mean motion: 15
75295150 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2740
Checksum: 286
Coasting Arc #6 (Orbit 2755)
---------------------------------------
Vector Time (GMT): 2007/274/12:45:08
773
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -154861
98 A = 6728272
35 meter
Y = 6704639
32 meter E =
0014008
Z = 471624
24 I = 51
33078
XDOT = -4833
524527 Wp = 118
86216
YDOT = 318
620491 meter/sec RA = 274
54938 deg
ZDOT = -5989
261503 TA = 55
98292
MA = 55
84995
Ha = 188
922 n
mi
Hp = 180
866
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -508077
36 X = -232113
85
Y = 21996848
18 feet Y = 6702475
63 meter
Z = 1547323
62 Z = 470684
33
XDOT = -15858
020101 XDOT = -4807
632916
YDOT = 1045
342818 feet/sec YDOT = 264
714120 meter/sec
ZDOT = -19649
808082 ZDOT = -6012
680260
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7190435
25 X = -2191644
66
Y = -20794845
99 feet Y = -6338269
06 meter
Z = 1544572
37 Z = 470785
66
XDOT = 12876
548958 XDOT = 3924
772122
YDOT = -5949
673104 feet/sec YDOT = -1813
460362 meter/sec
ZDOT = -19738
672696 ZDOT = -6016
347438
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 07274
56401968
00020000 00000-0 20000-3 0 9053
2 25544 51
6320 275
1055 0002799 53
6439 306
4978 15
75340305 27561
Satellite: ISS
Catalog Number: 25544
Epoch time: 07274
56401968 = yrday
fracday
Element set: 905
Inclination: 51
6320 deg
RA of node: 275
1055 deg
Eccentricity:
0002799
Arg of perigee: 53
6439 deg
Mean anomaly: 306
4978 deg
Mean motion: 15
75340305 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2756
Checksum: 306
Coasting Arc #7 (Orbit 2771)
---------------------------------------
Vector Time (GMT): 2007/275/12:45:08
773
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4197920
20 A = 6716264
71 meter
Y = -64127
63 meter E =
0004839
Z = 5238317
02 I = 51
28879
XDOT = 97
160199 Wp = 72
21229
YDOT = 7706
722349 meter/sec RA = 269
38453 deg
ZDOT = 17
929594 TA = 17
62529
MA = 17
60850
Ha = 188
772 n
mi
Hp = 180
876
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13772704
06 X = 4172878
19
Y = -210392
49 feet Y = -17324
21 meter
Z = 17186079
47 Z = 5258649
93
XDOT = 318
767056 XDOT = 10
888154
YDOT = 25284
522143 feet/sec YDOT = 7707
326478 meter/sec
ZDOT = 58
824127 ZDOT = 18
192164
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12655634
09 X = -3857437
27
Y = 5187244
73 feet Y = 1581072
19 meter
Z = 17263267
00 Z = 5261843
78
XDOT = -9146
306619 XDOT = -2787
794257
YDOT = -22501
292369 feet/sec YDOT = -6858
393914 meter/sec
ZDOT = 60
762971 ZDOT = 18
520554
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 07275
57898551
00020000 00000-0 20000-3 0 9064
2 25544 51
6314 269
8818 0002702 56
0062 304
1358 15
75345278 27723
Satellite: ISS
Catalog Number: 25544
Epoch time: 07275
57898551 = yrday
fracday
Element set: 906
Inclination: 51
6314 deg
RA of node: 269
8818 deg
Eccentricity:
0002702
Arg of perigee: 56
0062 deg
Mean anomaly: 304
1358 deg
Mean motion: 15
75345278 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2772
Checksum: 309
Coasting Arc #8 (Orbit 2787)
---------------------------------------
Vector Time (GMT): 2007/276/12:45:08
773
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -319000
40 A = 6728058
03 meter
Y = -6698454
91 meter E =
0015665
Z = 446423
67 I = 51
33072
XDOT = 4839
019994 Wp = 52
08762
YDOT = 177
876415 meter/sec RA = 264
21963 deg
ZDOT = 5993
593233 TA = 312
79269
MA = 312
92431
Ha = 188
811 n
mi
Hp = 180
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1046589
25 X = -246242
23
Y = -21976558
11 feet Y = -6701615
35 meter
Z = 1464644
58 Z = 445050
64
XDOT = 15876
049849 XDOT = 4807
555316
YDOT = 583
584038 feet/sec YDOT = 231
813100 meter/sec
ZDOT = 19664
019792 ZDOT = 6017
024923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9346839
97 X = 2848916
82
Y = 19917798
26 feet Y = 6070944
91 meter
Z = 1458606
92 Z = 444583
39
XDOT = -13346
386260 XDOT = -4067
978532
YDOT = 4784
393712 feet/sec YDOT = 1458
283204 meter/sec
ZDOT = 19753
009459 ZDOT = 6020
717283
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 07276
59393407
00020000 00000-0 20000-3 0 9078
2 25544 51
6312 264
6587 0002676 64
0963 296
0476 15
75422010 27883
Satellite: ISS
Catalog Number: 25544
Epoch time: 07276
59393407 = yrday
fracday
Element set: 907
Inclination: 51
6312 deg
RA of node: 264
6587 deg
Eccentricity:
0002676
Arg of perigee: 64
0963 deg
Mean anomaly: 296
0476 deg
Mean motion: 15
75422010 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2788
Checksum: 313
Coasting Arc #9 (Orbit 2802)
---------------------------------------
Vector Time (GMT): 2007/277/12:45:08
773
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4291796
44 A = 6716548
74 meter
Y = -387481
89 meter E =
0016773
Z = -5166480
37 I = 51
29578
XDOT = -598
565211 Wp = 92
72286
YDOT = -7592
644028 meter/sec RA = 259
03572 deg
ZDOT = 1068
873467 TA = 187
52317
MA = 187
54837
Ha = 188
897 n
mi
Hp = 180
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14080696
99 X = -4262046
68
Y = -1271266
03 feet Y = -435308
89 meter
Z = -16950394
90 Z = -5187257
72
XDOT = -1963
796625 XDOT = -518
811052
YDOT = -24910
249437 feet/sec YDOT = -7598
891585 meter/sec
ZDOT = 3506
802712 ZDOT = 1066
159421
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13341517
55 X = 4066494
55
Y = -4382186
85 feet Y = -1335690
55 meter
Z = -17029338
81 Z = -5190542
47
XDOT = 11384
997144 XDOT = 3470
147130
YDOT = 21105
601104 feet/sec YDOT = 6432
987216 meter/sec
ZDOT = 3495
553398 ZDOT = 1065
444676
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 07277
54543805
00020000 00000-0 20000-3 0 9084
2 25544 51
6312 259
7609 0002756 62
2243 297
9200 15
75381147 28031
Satellite: ISS
Catalog Number: 25544
Epoch time: 07277
54543805 = yrday
fracday
Element set: 908
Inclination: 51
6312 deg
RA of node: 259
7609 deg
Eccentricity:
0002756
Arg of perigee: 62
2243 deg
Mean anomaly: 297
9200 deg
Mean motion: 15
75381147 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2803
Checksum: 297
Coasting Arc #10 (Orbit 2818)
---------------------------------------
Vector Time (GMT): 2007/278/12:45:08
773
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 700631
93 A = 6727231
18 meter
Y = 6534739
44 meter E =
0009519
Z = -1425359
47 I = 51
33942
XDOT = -5027
151126 Wp = 126
28201
YDOT = -716
517662 meter/sec RA = 253
88856 deg
ZDOT = -5788
422718 TA = 69
46745
MA = 69
36533
Ha = 188
846 n
mi
Hp = 180
650
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2298661
20 X = 634431
58
Y = 21439433
87 feet Y = 6542204
12 meter
Z = -4676376
21 Z = -1422116
79
XDOT = -16493
277973 XDOT = -4990
646124
YDOT = -2350
779732 feet/sec YDOT = -772
530176 meter/sec
ZDOT = -18990
888184 ZDOT = -5812
755969
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10961891
90 X = -3341184
65
Y = -18571288
86 feet Y = -5660528
84 meter
Z = -4663241
18 Z = -1421355
91
XDOT = 14542
480580 XDOT = 4432
548081
YDOT = -3818
764486 feet/sec YDOT = -1163
959415 meter/sec
ZDOT = -19083
382393 ZDOT = -5816
614953
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 07278
56035821
00020000 00000-0 20000-3 0 9092
2 25544 51
6315 254
5366 0002781 63
9010 296
2440 15
75428984 28191
Satellite: ISS
Catalog Number: 25544
Epoch time: 07278
56035821 = yrday
fracday
Element set: 909
Inclination: 51
6315 deg
RA of node: 254
5366 deg
Eccentricity:
0002781
Arg of perigee: 63
9010 deg
Mean anomaly: 296
2440 deg
Mean motion: 15
75428984 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2819
Checksum: 305
Coasting Arc #11 (Orbit 2834)
---------------------------------------
Vector Time (GMT): 2007/279/12:45:08
773
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4526254
20 A = 6717526
14 meter
Y = 833836
46 meter E =
0009015
Z = 4887908
12 I = 51
31611
XDOT = 997
289699 Wp = 60
16050
YDOT = 7329
191007 meter/sec RA = 248
68858 deg
ZDOT = -2166
388364 TA = 50
98443
MA = 50
90419
Ha = 188
691 n
mi
Hp = 180
624
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14849915
35 X = 4492849
07
Y = 2735683
94 feet Y = 884265
08 meter
Z = 16036443
96 Z = 4909815
53
XDOT = 3271
947830 XDOT = 925
783417
YDOT = 24045
902255 feet/sec YDOT = 7339
943340 meter/sec
ZDOT = -7107
573373 ZDOT = -2161
717590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14509617
82 X = -4422531
51
Y = 3846590
47 feet Y = 1172440
78 meter
Z = 16119746
27 Z = 4913298
66
XDOT = -13007
035197 XDOT = -3964
544328
YDOT = -19254
931919 feet/sec YDOT = -5868
903249 meter/sec
ZDOT = -7088
904204 ZDOT = -2160
698001
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 07279
57526271
00020000 00000-0 20000-3 0 9100
2 25544 51
6314 249
3128 0002718 67
3144 292
8307 15
75447081 28355
Satellite: ISS
Catalog Number: 25544
Epoch time: 07279
57526271 = yrday
fracday
Element set: 910
Inclination: 51
6314 deg
RA of node: 249
3128 deg
Eccentricity:
0002718
Arg of perigee: 67
3144 deg
Mean anomaly: 292
8307 deg
Mean motion: 15
75447081 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2835
Checksum: 297
Coasting Arc #12 (Orbit 2850)
---------------------------------------
Vector Time (GMT): 2007/280/12:45:08
773
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1001718
58 A = 6725559
24 meter
Y = -6216809
23 meter E =
0016645
Z = 2340471
35 I = 51
35570
XDOT = 5389
317556 Wp = 73
27562
YDOT = 1168
777164 meter/sec RA = 243
55829 deg
ZDOT = 5384
346410 TA = 313
21592
MA = 313
35481
Ha = 188
737 n
mi
Hp = 180
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3286478
28 X = -943496
49
Y = -20396355
75 feet Y = -6227685
31 meter
Z = 7678711
79 Z = 2335746
84
XDOT = 17681
488044 XDOT = 5349
691236
YDOT = 3834
570748 feet/sec YDOT = 1228
822380 meter/sec
ZDOT = 17665
178509 ZDOT = 5410
431524
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12031942
43 X = 3667336
05
Y = 16802740
28 feet Y = 5121475
24 meter
Z = 7659971
44 Z = 2334759
29
XDOT = -16232
962039 XDOT = -4947
806830
YDOT = 3485
385965 feet/sec YDOT = 1062
345642 meter/sec
ZDOT = 17764
393706 ZDOT = 5414
587201
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 07280
59014983
00020000 00000-0 20000-3 0 9117
2 25544 51
6318 244
0886 0002665 72
8389 287
3066 15
75495666 28516
Satellite: ISS
Catalog Number: 25544
Epoch time: 07280
59014983 = yrday
fracday
Element set: 911
Inclination: 51
6318 deg
RA of node: 244
0886 deg
Eccentricity:
0002665
Arg of perigee: 72
8389 deg
Mean anomaly: 287
3066 deg
Mean motion: 15
75495666 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2851
Checksum: 325
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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