Date:
September 3rd 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 4843 76 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 2265)
---------------------------------------
Vector Time (GMT): 2007/243/11:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3413763
21 A = 6722715
11 meter
Y = -5253581
02 meter E =
0006937
Z = 2435777
06 I = 51
95593
XDOT = 3126
252248 Wp = 69
89307
YDOT = -4533
832661 meter/sec RA = 74
69582 deg
ZDOT = -5382
658721 TA = 82
71282
MA = 82
63398
Ha = 186
518 n
mi
Hp = 181
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11200010
53 X = -3366595
75
Y = -17236158
22 feet Y = -5291491
81 meter
Z = 7991394
56 Z = 2419307
79
XDOT = 10256
733097 XDOT = 3202
865912
YDOT = -14874
779073 feet/sec YDOT = -4498
445020 meter/sec
ZDOT = -17659
641473 ZDOT = -5367
285065
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -310868
21 X = -94752
63
Y = 20577514
24 feet Y = 6272026
34 meter
Z = 7928243
29 Z = 2416528
56
XDOT = -15400
930703 XDOT = -4694
203678
YDOT = 6567
725928 feet/sec YDOT = 2001
842863 meter/sec
ZDOT = -17601
852559 ZDOT = -5365
044660
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 07243
50179537
00020000 00000-0 20000-3 0 9002
2 25544 51
6337 75
2002 0009224 311
7821 48
2555 15
76434621 22667
Satellite: ISS
Catalog Number: 25544
Epoch time: 07243
50179537 = yrday
fracday
Element set: 900
Inclination: 51
6337 deg
RA of node: 75
2002 deg
Eccentricity:
0009224
Arg of perigee: 311
7821 deg
Mean anomaly: 48
2555 deg
Mean motion: 15
76434621 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2266
Checksum: 271
Coasting Arc #2 (Orbit 2281)
---------------------------------------
Vector Time (GMT): 2007/244/11:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2935599
87 A = 6714547
50 meter
Y = 3370877
54 meter E =
0003634
Z = 5010943
77 I = 51
91800
XDOT = -3964
253033 Wp = 332
70443
YDOT = -6317
626851 meter/sec RA = 69
59835 deg
ZDOT = 1931
186633 TA = 98
74691
MA = 98
70575
Ha = 186
839 n
mi
Hp = 181
756
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9631233
18 X = -2997417
73
Y = 11059309
51 feet Y = 3337704
48 meter
Z = 16440104
25 Z = 4996532
33
XDOT = -13006
079504 XDOT = -3902
695160
YDOT = -20727
122214 feet/sec YDOT = -6361
613134 meter/sec
ZDOT = 6335
914149 ZDOT = 1912
077867
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14178016
66 X = 4321459
48
Y = -3979295
21 feet Y = -1212889
18 meter
Z = 16385818
88 Z = 4994397
60
XDOT = -641
462834 XDOT = -195
517872
YDOT = 23452
274997 feet/sec YDOT = 7148
253419 meter/sec
ZDOT = 6262
623241 ZDOT = 1908
847564
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 07244
51608162
00020000 00000-0 20000-3 0 9016
2 25544 51
6328 69
9707 0009061 315
8002 44
2438 15
76373187 22827
Satellite: ISS
Catalog Number: 25544
Epoch time: 07244
51608162 = yrday
fracday
Element set: 901
Inclination: 51
6328 deg
RA of node: 69
9707 deg
Eccentricity:
0009061
Arg of perigee: 315
8002 deg
Mean anomaly: 44
2438 deg
Mean motion: 15
76373187 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2282
Checksum: 285
Coasting Arc #3 (Orbit 2296)
---------------------------------------
Vector Time (GMT): 2007/245/11:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3485567
79 A = 6724961
86 meter
Y = 5670068
48 meter E =
0014807
Z = -891538
27 I = 51
94169
XDOT = -3666
590408 Wp = 1
21262
YDOT = 3192
326814 meter/sec RA = 64
43952 deg
ZDOT = 5984
110252 TA = 349
08009
MA = 349
11220
Ha = 186
868 n
mi
Hp = 181
488
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11435589
87 X = 3426236
14
Y = 18602586
86 feet Y = 5708714
33 meter
Z = -2924994
32 Z = -874749
38
XDOT = -12029
496088 XDOT = -3731
084864
YDOT = 10473
513168 feet/sec YDOT = 3150
964300 meter/sec
ZDOT = 19632
907651 ZDOT = 5966
141209
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 151614
93 X = 46212
23
Y = -21844417
12 feet Y = -6658178
34 meter
Z = -2860594
21 Z = -871909
12
XDOT = 14252
696087 XDOT = 4344
221767
YDOT = -2456
040731 feet/sec YDOT = -748
601215 meter/sec
ZDOT = 19565
091762 ZDOT = 5963
439969
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 07245
46695722
00020000 00000-0 20000-3 0 9020
2 25544 51
6323 65
0683 0009130 318
5848 41
4623 15
76422448 22973
Satellite: ISS
Catalog Number: 25544
Epoch time: 07245
46695722 = yrday
fracday
Element set: 902
Inclination: 51
6323 deg
RA of node: 65
0683 deg
Eccentricity:
0009130
Arg of perigee: 318
5848 deg
Mean anomaly: 41
4623 deg
Mean motion: 15
76422448 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2297
Checksum: 295
Coasting Arc #4 (Orbit 2312)
---------------------------------------
Vector Time (GMT): 2007/246/11:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3522791
20 A = 6713089
98 meter
Y = -2189738
03 meter E =
0012078
Z = -5286589
62 I = 51
88792
XDOT = 3977
325410 Wp = 52
73782
YDOT = 6590
688913 meter/sec RA = 59
31341 deg
ZDOT = -72
516651 TA = 216
53496
MA = 216
61741
Ha = 186
956 n
mi
Hp = 181
291
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11557713
90 X = 3572696
74
Y = -7184179
87 feet Y = -2150065
00 meter
Z = -17344454
14 Z = -5269354
68
XDOT = 13048
967881 XDOT = 3903
684016
YDOT = 21622
995120 feet/sec YDOT = 6634
753862 meter/sec
ZDOT = -237
915522 ZDOT = -53
373428
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13690402
78 X = -4172834
77
Y = 148350
95 feet Y = 45217
37 meter
Z = -17279298
14 Z = -5266730
07
XDOT = -25
993596 XDOT = -7
922848
YDOT = -24257
524479 feet/sec YDOT = -7393
693461 meter/sec
ZDOT = -164
475996 ZDOT = -50
132284
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 07246
48121152
00020000 00000-0 20000-3 0 9035
2 25544 51
6318 59
8395 0008992 322
9015 37
1527 15
76463493 23137
Satellite: ISS
Catalog Number: 25544
Epoch time: 07246
48121152 = yrday
fracday
Element set: 903
Inclination: 51
6318 deg
RA of node: 59
8395 deg
Eccentricity:
0008992
Arg of perigee: 322
9015 deg
Mean anomaly: 37
1527 deg
Mean motion: 15
76463493 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2313
Checksum: 294
Coasting Arc #5 (Orbit 2328)
---------------------------------------
Vector Time (GMT): 2007/247/11:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3395140
43 A = 6724727
73 meter
Y = -5751813
49 meter E =
0001619
Z = -781723
44 I = 51
91250
XDOT = 4473
730892 Wp = 100
57619
YDOT = -1827
630413 meter/sec RA = 54
18465 deg
ZDOT = -5993
335463 TA = 87
91722
MA = 87
89868
Ha = 187
070 n
mi
Hp = 180
853
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11138912
18 X = -3326773
00
Y = -18870779
17 feet Y = -5789397
57 meter
Z = -2564709
44 Z = -798051
19
XDOT = 14677
594790 XDOT = 4522
949752
YDOT = -5996
162773 feet/sec YDOT = -1777
327185 meter/sec
ZDOT = -19663
174090 ZDOT = -5971
482614
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 182105
47 X = 55505
75
Y = 21904867
51 feet Y = 6676603
62 meter
Z = -2627360
37 Z = -800819
44
XDOT = -14205
672875 XDOT = -4329
889092
YDOT = -2226
344975 feet/sec YDOT = -678
589948 meter/sec
ZDOT = -19580
441028 ZDOT = -5968
118425
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 07247
49544881
00020000 00000-0 20000-3 0 9046
2 25544 51
6324 54
6111 0009219 327
4041 32
6553 15
76521512 23298
Satellite: ISS
Catalog Number: 25544
Epoch time: 07247
49544881 = yrday
fracday
Element set: 904
Inclination: 51
6324 deg
RA of node: 54
6111 deg
Eccentricity:
0009219
Arg of perigee: 327
4041 deg
Mean anomaly: 32
6553 deg
Mean motion: 15
76521512 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2329
Checksum: 276
Coasting Arc #6 (Orbit 2344)
---------------------------------------
Vector Time (GMT): 2007/248/11:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4327015
54 A = 6714197
54 meter
Y = 1041881
88 meter E =
0011022
Z = 5030022
36 I = 51
85788
XDOT = -3718
220894 Wp =
59967
YDOT = -6488
757502 meter/sec RA = 49
02347 deg
ZDOT = -1843
686791 TA = 107
17952
MA = 107
05882
Ha = 187
270 n
mi
Hp = 180
765
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14196245
21 X = -4362779
22
Y = 3418247
64 feet Y = 993294
57 meter
Z = 16502698
02 Z = 5008915
01
XDOT = -12198
887448 XDOT = -3636
430050
YDOT = -21288
574483 feet/sec YDOT = -6529
879353 meter/sec
ZDOT = -6048
841178 ZDOT = -1861
551410
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14150410
58 X = 4313045
14
Y = 3951928
68 feet Y = 1204547
86 meter
Z = 16422697
01 Z = 5005638
05
XDOT = 582
202805 XDOT = 177
455415
YDOT = 23485
386040 feet/sec YDOT = 7158
345665 meter/sec
ZDOT = -6117
411810 ZDOT = -1864
587120
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 07248
50967237
00020000 00000-0 20000-3 0 9054
2 25544 51
6319 49
3816 0008993 330
6488 29
4170 15
76482079 23455
Satellite: ISS
Catalog Number: 25544
Epoch time: 07248
50967237 = yrday
fracday
Element set: 905
Inclination: 51
6319 deg
RA of node: 49
3816 deg
Eccentricity:
0008993
Arg of perigee: 330
6488 deg
Mean anomaly: 29
4170 deg
Mean motion: 15
76482079 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2345
Checksum: 321
Coasting Arc #7 (Orbit 2360)
---------------------------------------
Vector Time (GMT): 2007/249/11:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3006949
77 A = 6722437
57 meter
Y = 5503551
16 meter E =
0015225
Z = 2392827
94 I = 51
86639
XDOT = -5463
002186 Wp = 38
51802
YDOT = 631
378132 meter/sec RA = 43
91993 deg
ZDOT = 5406
310165 TA = 348
43143
MA = 348
46638
Ha = 187
252 n
mi
Hp = 180
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9865320
76 X = 2933560
95
Y = 18056270
21 feet Y = 5536766
16 meter
Z = 7850485
36 Z = 2407257
45
XDOT = -17923
235520 XDOT = -5495
918931
YDOT = 2071
450564 feet/sec YDOT = 570
103548 meter/sec
ZDOT = 17737
238075 ZDOT = 5379
691245
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -168822
85 X = -51457
21
Y = -20553631
28 feet Y = -6264746
81 meter
Z = 7905903
35 Z = 2409719
34
XDOT = 15378
339193 XDOT = 4687
317786
YDOT = 6665
694896 feet/sec YDOT = 2031
703804 meter/sec
ZDOT = 17636
261867 ZDOT = 5375
532617
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 07249
52387762
00020000 00000-0 20000-3 0 9067
2 25544 51
6319 44
1520 0008971 334
6641 25
4083 15
76538146 23615
Satellite: ISS
Catalog Number: 25544
Epoch time: 07249
52387762 = yrday
fracday
Element set: 906
Inclination: 51
6319 deg
RA of node: 44
1520 deg
Eccentricity:
0008971
Arg of perigee: 334
6641 deg
Mean anomaly: 25
4083 deg
Mean motion: 15
76538146 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2361
Checksum: 294
Coasting Arc #8 (Orbit 2375)
---------------------------------------
Vector Time (GMT): 2007/250/11:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5193423
41 A = 6717089
61 meter
Y = -126190
91 meter E =
0007105
Z = -4258664
59 I = 51
82745
XDOT = 3080
004421 Wp = 40
31906
YDOT = 6082
832980 meter/sec RA = 38
73320 deg
ZDOT = 3584
419997 TA = 265
93293
MA = 266
01415
Ha = 187
467 n
mi
Hp = 180
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17038790
71 X = 5215136
05
Y = -414012
19 feet Y = -67993
68 meter
Z = -13971996
68 Z = -4233382
55
XDOT = 10105
001382 XDOT = 2994
344139
YDOT = 19956
801115 feet/sec YDOT = 6116
796345 meter/sec
ZDOT = 11759
908125 ZDOT = 3599
174441
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15428150
09 X = -4702500
15
Y = -7425387
48 feet Y = -2263258
10 meter
Z = -13876033
01 Z = -4229414
86
XDOT = -392
285178 XDOT = -119
568522
YDOT = -21213
837833 feet/sec YDOT = -6465
977771 meter/sec
ZDOT = 11816
630353 ZDOT = 3601
708932
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 07250
47468082
00020000 00000-0 20000-3 0 9079
2 25544 51
6327 39
2498 0008912 338
8629 21
2166 15
76560772 23762
Satellite: ISS
Catalog Number: 25544
Epoch time: 07250
47468082 = yrday
fracday
Element set: 907
Inclination: 51
6327 deg
RA of node: 39
2498 deg
Eccentricity:
0008912
Arg of perigee: 338
8629 deg
Mean anomaly: 21
2166 deg
Mean motion: 15
76560772 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2376
Checksum: 313
Coasting Arc #9 (Orbit 2391)
---------------------------------------
Vector Time (GMT): 2007/251/11:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2251179
41 A = 6718490
28 meter
Y = -5078895
10 meter E =
0010802
Z = -3789659
77 I = 51
80975
XDOT = 6431
931413 Wp = 18
14794
YDOT = 298
427001 meter/sec RA = 33
64170 deg
ZDOT = -4213
870901 TA = 207
65840
MA = 207
71590
Ha = 187
509 n
mi
Hp = 179
806
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7385759
21 X = -2175809
92
Y = -16663041
68 feet Y = -5103647
71 meter
Z = -12433266
96 Z = -3800412
68
XDOT = 21102
137183 XDOT = 6448
586250
YDOT = 979
091209 feet/sec YDOT = 370
445542 meter/sec
ZDOT = -13825
035763 ZDOT = -4182
584586
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -761117
81 X = -231988
71
Y = 18182284
90 feet Y = 5541960
44 meter
Z = -12474683
96 Z = -3802283
67
XDOT = -17263
008098 XDOT = -5261
764868
YDOT = -10141
717895 feet/sec YDOT = -3091
195614 meter/sec
ZDOT = -13706
226171 ZDOT = -4177
657737
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 07251
48885392
00020000 00000-0 20000-3 0 9089
2 25544 51
6330 34
0209 0009049 343
3090 16
7775 15
76601924 23922
Satellite: ISS
Catalog Number: 25544
Epoch time: 07251
48885392 = yrday
fracday
Element set: 908
Inclination: 51
6330 deg
RA of node: 34
0209 deg
Eccentricity:
0009049
Arg of perigee: 343
3090 deg
Mean anomaly: 16
7775 deg
Mean motion: 15
76601924 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2392
Checksum: 293
Coasting Arc #10 (Orbit 2407)
---------------------------------------
Vector Time (GMT): 2007/252/11:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5993129
68 A = 6720996
18 meter
Y = -572685
36 meter E =
0013161
Z = 2987042
97 I = 51
79261
XDOT = -1968
045987 Wp = 57
30680
YDOT = -5529
746193 meter/sec RA = 28
44630 deg
ZDOT = -4986
026550 TA = 88
24767
MA = 88
09693
Ha = 187
637 n
mi
Hp = 179
742
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19662498
94 X = -6000790
73
Y = -1878888
98 feet Y = -639746
63 meter
Z = 9800009
76 Z = 2957910
15
XDOT = -6456
843788 XDOT = -1881
844373
YDOT = -18142
211920 feet/sec YDOT = -5551
272223 meter/sec
ZDOT = -16358
354824 ZDOT = -4995
377583
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17055650
05 X = 5198562
13
Y = 10070039
73 feet Y = 3069348
11 meter
Z = 9689343
68 Z = 2953311
95
XDOT = -1202
783284 XDOT = -366
608345
YDOT = 17884
645930 feet/sec YDOT = 5451
240079 meter/sec
ZDOT = -16394
505173 ZDOT = -4997
045177
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 07252
50301053
00020000 00000-0 20000-3 0 9091
2 25544 51
6325 28
7908 0008986 346
5390 13
5534 15
76598369 24083
Satellite: ISS
Catalog Number: 25544
Epoch time: 07252
50301053 = yrday
fracday
Element set: 909
Inclination: 51
6325 deg
RA of node: 28
7908 deg
Eccentricity:
0008986
Arg of perigee: 346
5390 deg
Mean anomaly: 13
5534 deg
Mean motion: 15
76598369 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2408
Checksum: 306
Coasting Arc #11 (Orbit 2423)
---------------------------------------
Vector Time (GMT): 2007/253/11:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1094896
26 A = 6714575
58 meter
Y = 4578667
63 meter E =
0007007
Z = 4781739
87 I = 51
74697
XDOT = -7217
780976 Wp = 40
67857
YDOT = -929
139038 meter/sec RA = 23
34371 deg
ZDOT = 2545
506300 TA = 24
47528
MA = 24
44203
Ha = 187
646 n
mi
Hp = 179
371
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3592179
32 X = 1020386
94
Y = 15021875
44 feet Y = 4590495
07 meter
Z = 15688122
94 Z = 4786877
57
XDOT = -23680
383780 XDOT = -7219
220254
YDOT = -3048
356425 feet/sec YDOT = -1009
860236 meter/sec
ZDOT = 8351
398622 ZDOT = 2510
439228
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2943079
62 X = 897050
67
Y = -15141646
16 feet Y = -4615173
75 meter
Z = 15708167
59 Z = 4787849
48
XDOT = 19303
459027 XDOT = 5883
694311
YDOT = 12266
986747 feet/sec YDOT = 3738
977561 meter/sec
ZDOT = 8218
164734 ZDOT = 2504
896611
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 07253
51714851
00020000 00000-0 20000-3 0 9109
2 25544 51
6337 23
5614 0009056 349
9324 10
1658 15
76667439 24249
Satellite: ISS
Catalog Number: 25544
Epoch time: 07253
51714851 = yrday
fracday
Element set: 910
Inclination: 51
6337 deg
RA of node: 23
5614 deg
Eccentricity:
0009056
Arg of perigee: 349
9324 deg
Mean anomaly: 10
1658 deg
Mean motion: 15
76667439 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2424
Checksum: 290
Coasting Arc #12 (Orbit 2438)
---------------------------------------
Vector Time (GMT): 2007/254/11:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 511203
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6495937
19 A = 6723822
85 meter
Y = 982511
10 meter E =
0016699
Z = -1384542
17 I = 51
75216
XDOT = 481
701946 Wp = 15
09826
YDOT = 5006
532211 meter/sec RA = 18
16330 deg
ZDOT = 5844
286503 TA = 329
67863
MA = 329
77514
Ha = 187
876 n
mi
Hp = 179
128
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21312129
90 X = 6491193
64
Y = 3223461
60 feet Y = 1055125
71 meter
Z = -4542461
19 Z = -1352996
67
XDOT = 1580
386961 XDOT = 397
292014
YDOT = 16425
630613 feet/sec YDOT = 5011
447339 meter/sec
ZDOT = 19174
168318 ZDOT = 5846
421204
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18353164
16 X = -5594044
43
Y = -11350487
47 feet Y = -3459628
58 meter
Z = -4422594
15 Z = -1348006
70
XDOT = 4274
090405 XDOT = 1302
742756
YDOT = -14344
052795 feet/sec YDOT = -4372
067292 meter/sec
ZDOT = 19182
864066 ZDOT = 5846
936967
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 07254
46788906
00020000 00000-0 20000-3 0 9117
2 25544 51
6351 18
6596 0009109 354
4922 5
6141 15
76660451 24392
Satellite: ISS
Catalog Number: 25544
Epoch time: 07254
46788906 = yrday
fracday
Element set: 911
Inclination: 51
6351 deg
RA of node: 18
6596 deg
Eccentricity:
0009109
Arg of perigee: 354
4922 deg
Mean anomaly: 5
6141 deg
Mean motion: 15
76660451 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2439
Checksum: 301
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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