Date:
October 18th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5112 86 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 3007)
---------------------------------------
Vector Time (GMT): 2007/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 645252
77 A = 6715101
34 meter
Y = -4127729
55 meter E =
0004948
Z = 5253066
39 I = 51
54818
XDOT = 7567
279160 Wp = 101
52044
YDOT = 1451
920778 meter/sec RA = 192
10265 deg
ZDOT = 210
228720 TA = 346
47713
MA = 346
49039
Ha = 188
272 n
mi
Hp = 180
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2116971
03 X = 665842
74
Y = -13542419
78 feet Y = -4120398
97 meter
Z = 17234469
80 Z = 5256251
02
XDOT = 24827
031364 XDOT = 7549
459869
YDOT = 4763
519614 feet/sec YDOT = 1536
442737 meter/sec
ZDOT = 689
726773 ZDOT = 246
948066
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3863385
72 X = 1177559
97
Y = 13135976
27 feet Y = 4003845
57 meter
Z = 17246043
82 Z = 5256594
16
XDOT = -23565
994117 XDOT = -7182
915007
YDOT = 5837
053851 feet/sec YDOT = 1779
134014 meter/sec
ZDOT = 829
449554 ZDOT = 252
816224
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 07290
54801102
00020000 00000-0 20000-3 0 9008
2 25544 51
6365 192
8436 0002483 100
2968 259
8476 15
75760891 30085
Satellite: ISS
Catalog Number: 25544
Epoch time: 07290
54801102 = yrday
fracday
Element set: 900
Inclination: 51
6365 deg
RA of node: 192
8436 deg
Eccentricity:
0002483
Arg of perigee: 100
2968 deg
Mean anomaly: 259
8476 deg
Mean motion: 15
75760891 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3008
Checksum: 295
Coasting Arc #2 (Orbit 3023)
---------------------------------------
Vector Time (GMT): 2007/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6613656
35 A = 6727149
55 meter
Y = -1127722
80 meter E =
0014599
Z = 402741
87 I = 51
61758
XDOT = 1170
662154 Wp = 57
09825
YDOT = -4661
873134 meter/sec RA = 186
95133 deg
ZDOT = 6021
135836 TA = 307
28579
MA = 307
41880
Ha = 188
306 n
mi
Hp = 180
209
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21698347
62 X = -6602510
92
Y = -3699877
97 feet Y = -1201618
14 meter
Z = 1321331
61 Z = 370639
24
XDOT = 3840
755097 XDOT = 1193
454828
YDOT = -15294
859362 feet/sec YDOT = -4648
654808 meter/sec
ZDOT = 19754
382664 ZDOT = 6026
878280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21145907
11 X = 6445272
49
Y = -6137253
76 feet Y = -1870634
95 meter
Z = 1199179
85 Z = 365510
02
XDOT = 2867
154454 XDOT = 873
908677
YDOT = 13848
202164 feet/sec YDOT = 4220
932019 meter/sec
ZDOT = 19775
610228 ZDOT = 6027
605998
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 07291
56272121
00020000 00000-0 20000-3 0 9015
2 25544 51
6368 187
6184 0002512 101
6599 258
4847 15
75751133 30242
Satellite: ISS
Catalog Number: 25544
Epoch time: 07291
56272121 = yrday
fracday
Element set: 901
Inclination: 51
6368 deg
RA of node: 187
6184 deg
Eccentricity:
0002512
Arg of perigee: 101
6599 deg
Mean anomaly: 258
4847 deg
Mean motion: 15
75751133 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3024
Checksum: 289
Coasting Arc #3 (Orbit 3038)
---------------------------------------
Vector Time (GMT): 2007/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1424189
24 A = 6715399
21 meter
Y = 4056733
76 meter E =
0016837
Z = -5173311
02 I = 51
60783
XDOT = -7514
575885 Wp = 100
06422
YDOT = -1156
008868 meter/sec RA = 181
78667 deg
ZDOT = 1162
536219 TA = 181
05294
MA = 181
05649
Ha = 188
200 n
mi
Hp = 180
095
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4672536
89 X = -1444315
04
Y = 13309493
97 feet Y = 4040695
19 meter
Z = -16972805
19 Z = -5180278
68
XDOT = -24654
120359 XDOT = -7506
738188
YDOT = -3792
680012 feet/sec YDOT = -1239
997295 meter/sec
ZDOT = 3814
095206 ZDOT = 1126
048925
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1926317
21 X = -587141
49
Y = -13942113
37 feet Y = -4249556
16 meter
Z = -16998768
29 Z = -5181224
57
XDOT = 22712
185381 XDOT = 6922
674104
YDOT = -7617
819611 feet/sec YDOT = -2321
911417 meter/sec
ZDOT = 3675
259867 ZDOT = 1120
219208
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 07292
51399150
00020000 00000-0 20000-3 0 9024
2 25544 51
6373 182
7198 0002445 105
8936 254
2498 15
75798711 30390
Satellite: ISS
Catalog Number: 25544
Epoch time: 07292
51399150 = yrday
fracday
Element set: 902
Inclination: 51
6373 deg
RA of node: 182
7198 deg
Eccentricity:
0002445
Arg of perigee: 105
8936 deg
Mean anomaly: 254
2498 deg
Mean motion: 15
75798711 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3039
Checksum: 316
Coasting Arc #4 (Orbit 3054)
---------------------------------------
Vector Time (GMT): 2007/293/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6458913
96 A = 6725996
88 meter
Y = 911485
57 meter E =
0010203
Z = -1626746
41 I = 51
67255
XDOT = -2100
549388 Wp = 136
63758
YDOT = 4675
073251 meter/sec RA = 176
66222 deg
ZDOT = -5749
105587 TA = 61
32869
MA = 61
22614
Ha = 188
207 n
mi
Hp = 180
257
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21190662
60 X = 6456144
09
Y = 2990438
23 feet Y = 983697
30 meter
Z = -5337094
53 Z = -1595375
35
XDOT = -6891
566232 XDOT = -2124
742174
YDOT = 15338
166835 feet/sec YDOT = 4651
448399 meter/sec
ZDOT = -18861
894970 ZDOT = -5759
368991
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20162131
00 X = -6145417
53
Y = 7261907
56 feet Y = 2213429
42 meter
Z = -5217724
85 Z = -1590362
53
XDOT = -630
435591 XDOT = -192
156768
YDOT = -15261
668467 feet/sec YDOT = -4651
756549 meter/sec
ZDOT = -18900
307265 ZDOT = -5760
813654
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 07293
52866141
00020000 00000-0 20000-3 0 9036
2 25544 51
6375 177
4946 0002374 113
8747 246
2666 15
75785497 30557
Satellite: ISS
Catalog Number: 25544
Epoch time: 07293
52866141 = yrday
fracday
Element set: 903
Inclination: 51
6375 deg
RA of node: 177
4946 deg
Eccentricity:
0002374
Arg of perigee: 113
8747 deg
Mean anomaly: 246
2666 deg
Mean motion: 15
75785497 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3055
Checksum: 325
Coasting Arc #5 (Orbit 3070)
---------------------------------------
Vector Time (GMT): 2007/294/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2217085
29 A = 6716745
37 meter
Y = -4155383
67 meter E =
0008665
Z = 4782765
90 I = 51
67157
XDOT = 7221
938022 Wp = 71
66908
YDOT = 937
809150 meter/sec RA = 171
48003 deg
ZDOT = -2526
592552 TA = 43
06217
MA = 42
99441
Ha = 187
899 n
mi
Hp = 180
114
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7273901
86 X = 2240152
52
Y = -13633148
51 feet Y = -4130461
84 meter
Z = 15691489
16 Z = 4793592
79
XDOT = 23694
022383 XDOT = 7223
188437
YDOT = 3076
801673 feet/sec YDOT = 1018
575863 meter/sec
ZDOT = -8289
345643 ZDOT = -2491
504913
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 275205
15 X = 83882
53
Y = 15408443
65 feet Y = 4696493
63 meter
Z = 15732111
90 Z = 4795147
71
XDOT = -21160
187740 XDOT = -6449
625223
YDOT = 8726
461570 feet/sec YDOT = 2659
825487 meter/sec
ZDOT = -8155
832958 ZDOT = -2485
897886
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 07294
54330875
00020000 00000-0 20000-3 0 9040
2 25544 51
6377 172
2692 0002197 112
4025 247
7372 15
75896155 30719
Satellite: ISS
Catalog Number: 25544
Epoch time: 07294
54330875 = yrday
fracday
Element set: 904
Inclination: 51
6377 deg
RA of node: 172
2692 deg
Eccentricity:
0002197
Arg of perigee: 112
4025 deg
Mean anomaly: 247
7372 deg
Mean motion: 15
75896155 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3071
Checksum: 301
Coasting Arc #6 (Orbit 3086)
---------------------------------------
Vector Time (GMT): 2007/295/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6078511
78 A = 6723645
33 meter
Y = -763863
86 meter E =
0015497
Z = 2755086
86 I = 51
72245
XDOT = 2963
057386 Wp = 84
14388
YDOT = -4903
524465 meter/sec RA = 166
37675 deg
ZDOT = 5154
698699 TA = 307
35404
MA = 307
49510
Ha = 188
043 n
mi
Hp = 180
200
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19942623
95 X = -6082902
30
Y = -2506115
02 feet Y = -831861
63 meter
Z = 9038998
90 Z = 2725546
36
XDOT = 9721
316882 XDOT = 2992
628119
YDOT = -16087
678691 feet/sec YDOT = -4870
224276 meter/sec
ZDOT = 16911
741137 ZDOT = 5169
165538
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18594819
70 X = 5667701
04
Y = -7761510
33 feet Y = -2365708
35 meter
Z = 8926589
57 Z = 2720824
50
XDOT = -923
680709 XDOT = -281
537880
YDOT = 17388
314361 feet/sec YDOT = 5299
958217 meter/sec
ZDOT = 16966
106980 ZDOT = 5171
269407
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 07295
55793949
00020000 00000-0 20000-3 0 9058
2 25544 51
6374 167
0434 0002209 114
5555 245
5839 15
75869121 30871
Satellite: ISS
Catalog Number: 25544
Epoch time: 07295
55793949 = yrday
fracday
Element set: 905
Inclination: 51
6374 deg
RA of node: 167
0434 deg
Eccentricity:
0002209
Arg of perigee: 114
5555 deg
Mean anomaly: 245
5839 deg
Mean motion: 15
75869121 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3087
Checksum: 321
Coasting Arc #7 (Orbit 3101)
---------------------------------------
Vector Time (GMT): 2007/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2923120
83 A = 6719254
67 meter
Y = 4434341
64 meter E =
0009925
Z = -4126322
38 I = 51
73579
XDOT = -6649
476603 Wp = 112
59615
YDOT = -876
986708 meter/sec RA = 161
18423 deg
ZDOT = 3771
530260 TA = 196
01581
MA = 196
04721
Ha = 187
825 n
mi
Hp = 180
115
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9590291
43 X = -2952443
70
Y = 14548364
96 feet Y = 4401489
43 meter
Z = -13537803
09 Z = -4140594
71
XDOT = -21815
868120 XDOT = -6657
497594
YDOT = -2877
252979 feet/sec YDOT = -951
389528 meter/sec
ZDOT = 12373
786942 ZDOT = 3739
207006
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 726861
61 X = 221547
42
Y = -17367892
90 feet Y = -5293733
76 meter
Z = -13591493
42 Z = -4142687
20
XDOT = 19007
418335 XDOT = 5793
461108
YDOT = -8782
752808 feet/sec YDOT = -2676
983056 meter/sec
ZDOT = 12250
777158 ZDOT = 3734
036878
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 07296
50913503
00020000 00000-0 20000-3 0 9065
2 25544 51
6369 162
1442 0002086 121
2489 238
8880 15
75918046 31024
Satellite: ISS
Catalog Number: 25544
Epoch time: 07296
50913503 = yrday
fracday
Element set: 906
Inclination: 51
6369 deg
RA of node: 162
1442 deg
Eccentricity:
0002086
Arg of perigee: 121
2489 deg
Mean anomaly: 238
8880 deg
Mean motion: 15
75918046 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3102
Checksum: 291
Coasting Arc #8 (Orbit 3117)
---------------------------------------
Vector Time (GMT): 2007/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5489051
43 A = 6720531
70 meter
Y = 835752
34 meter E =
0007507
Z = -3793044
38 I = 51
76595
XDOT = -3706
721423 Wp = 88
62279
YDOT = 5271
101888 meter/sec RA = 156
09325 deg
ZDOT = -4209
658901 TA = 137
27774
MA = 137
21936
Ha = 187
790 n
mi
Hp = 180
311
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18008698
90 X = 5497724
38
Y = 2741969
63 feet Y = 897182
29 meter
Z = -12444371
32 Z = -3766356
83
XDOT = -12161
159525 XDOT = -3744
937865
YDOT = 17293
641366 feet/sec YDOT = 5229
437294 meter/sec
ZDOT = -13811
216868 ZDOT = -4227
759794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16813226
27 X = -5124671
37
Y = 7187833
61 feet Y = 2190851
68 meter
Z = -12342790
67 Z = -3762082
60
XDOT = 1690
944187 XDOT = 515
399788
YDOT = -19838
514298 feet/sec YDOT = -6046
779158 meter/sec
ZDOT = -13879
361794 ZDOT = -4230
429475
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 07297
52372500
00020000 00000-0 20000-3 0 9075
2 25544 51
6360 156
9184 0002004 127
2453 232
8894 15
75928121 31187
Satellite: ISS
Catalog Number: 25544
Epoch time: 07297
52372500 = yrday
fracday
Element set: 907
Inclination: 51
6360 deg
RA of node: 156
9184 deg
Eccentricity:
0002004
Arg of perigee: 127
2453 deg
Mean anomaly: 232
8894 deg
Mean motion: 15
75928121 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3118
Checksum: 284
Coasting Arc #9 (Orbit 3133)
---------------------------------------
Vector Time (GMT): 2007/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3486607
06 A = 6722032
88 meter
Y = -4788979
68 meter E =
0014569
Z = 3162663
49 I = 51
79803
XDOT = 5896
734498 Wp = 97
79784
YDOT = 1082
050231 meter/sec RA = 150
90138 deg
ZDOT = -4845
300633 TA = 45
38026
MA = 45
26152
Ha = 187
555 n
mi
Hp = 180
104
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11438999
53 X = 3524534
86
Y = -15711875
58 feet Y = -4749778
27 meter
Z = 10376192
57 Z = 3179694
31
XDOT = 19346
241792 XDOT = 5907
734958
YDOT = 3550
033565 feet/sec YDOT = 1148
052167 meter/sec
ZDOT = -15896
655621 ZDOT = -4816
626678
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1069120
67 X = -325867
98
Y = 19370993
64 feet Y = 5904278
86 meter
Z = 10440340
17 Z = 3182215
68
XDOT = -16852
938244 XDOT = -5136
775577
YDOT = 7608
598328 feet/sec YDOT = 2319
100770 meter/sec
ZDOT = -15787
486484 ZDOT = -4812
025880
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 07298
53829369
00020000 00000-0 20000-3 0 9088
2 25544 51
6360 151
6920 0001879 126
3933 233
7404 15
76015928 31347
Satellite: ISS
Catalog Number: 25544
Epoch time: 07298
53829369 = yrday
fracday
Element set: 908
Inclination: 51
6360 deg
RA of node: 151
6920 deg
Eccentricity:
0001879
Arg of perigee: 126
3933 deg
Mean anomaly: 233
7404 deg
Mean motion: 15
76015928 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3134
Checksum: 307
Coasting Arc #10 (Orbit 3149)
---------------------------------------
Vector Time (GMT): 2007/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4773199
94 A = 6717501
44 meter
Y = -1119803
32 meter E =
0010419
Z = 4586573
30 I = 51
80516
XDOT = 4222
656245 Wp = 117
72980
YDOT = -5712
655516 meter/sec RA = 145
80856 deg
ZDOT = 2989
849024 TA = 302
64321
MA = 302
74369
Ha = 187
776 n
mi
Hp = 180
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15660104
78 X = -4782604
92
Y = -3673895
40 feet Y = -1173232
50 meter
Z = 15047812
67 Z = 4563361
42
XDOT = 13853
859073 XDOT = 4271
697509
YDOT = -18742
308123 feet/sec YDOT = -5665
161162 meter/sec
ZDOT = 9809
215958 ZDOT = 3010
482586
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15132966
53 X = 4612528
20
Y = -5690571
99 feet Y = -1734486
34 meter
Z = 14959404
05 Z = 4559626
35
XDOT = -1478
078796 XDOT = -450
518417
YDOT = 22146
046845 feet/sec YDOT = 6750
115078 meter/sec
ZDOT = 9886
960030 ZDOT = 3013
545417
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 07299
55284522
00020000 00000-0 20000-3 0 9098
2 25544 51
6344 146
4649 0001945 129
8567 230
2768 15
75971175 31501
Satellite: ISS
Catalog Number: 25544
Epoch time: 07299
55284522 = yrday
fracday
Element set: 909
Inclination: 51
6344 deg
RA of node: 146
4649 deg
Eccentricity:
0001945
Arg of perigee: 129
8567 deg
Mean anomaly: 230
2768 deg
Mean motion: 15
75971175 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3150
Checksum: 321
Coasting Arc #11 (Orbit 3164)
---------------------------------------
Vector Time (GMT): 2007/300/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3820502
67 A = 6724634
62 meter
Y = 5161005
64 meter E =
0006681
Z = -1994083
72 I = 51
85207
XDOT = -5036
274778 Wp = 56
30910
YDOT = -1567
232777 meter/sec RA = 140
62911 deg
ZDOT = 5609
839583 TA = 281
53552
MA = 281
61053
Ha = 187
475 n
mi
Hp = 180
183
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12534457
58 X = -3868242
62
Y = 16932433
20 feet Y = 5118015
75 meter
Z = -6542269
44 Z = -2012760
18
XDOT = -16523
211215 XDOT = -5045
627979
YDOT = -5141
839820 feet/sec YDOT = -1623
603726 meter/sec
ZDOT = 18404
985510 ZDOT = 5585
349730
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 624879
52 X = 190463
28
Y = -21035767
20 feet Y = -6411701
84 meter
Z = -6612657
15 Z = -2015537
90
XDOT = 15060
045069 XDOT = 4590
301737
YDOT = -5291
617816 feet/sec YDOT = -1612
885110 meter/sec
ZDOT = 18311
655209 ZDOT = 5581
392508
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 07300
50396522
00020000 00000-0 20000-3 0 9102
2 25544 51
6333 141
5641 0001873 138
8645 221
2661 15
76028020 31655
Satellite: ISS
Catalog Number: 25544
Epoch time: 07300
50396522 = yrday
fracday
Element set: 910
Inclination: 51
6333 deg
RA of node: 141
5641 deg
Eccentricity:
0001873
Arg of perigee: 138
8645 deg
Mean anomaly: 221
2661 deg
Mean motion: 15
76028020 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3165
Checksum: 259
Coasting Arc #12 (Orbit 3180)
---------------------------------------
Vector Time (GMT): 2007/301/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 524298
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4015135
28 A = 6715006
90 meter
Y = 1696819
57 meter E =
0014810
Z = -5120795
48 I = 51
84031
XDOT = -4484
955912 Wp = 85
27626
YDOT = 6065
829118 meter/sec RA = 135
52272 deg
ZDOT = -1509
145826 TA = 170
29133
MA = 170
26268
Ha = 187
437 n
mi
Hp = 180
252
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13173016
01 X = 4020739
43
Y = 5566993
35 feet Y = 1741750
73 meter
Z = -16800510
11 Z = -5101275
64
XDOT = -14714
422284 XDOT = -4545
120209
YDOT = 19901
014166 feet/sec YDOT = 6015
339499 meter/sec
ZDOT = -4951
265832 ZDOT = -1531
080190
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14022038
62 X = -4273917
37
Y = 3224635
58 feet Y = 982868
93 meter
Z = -16726059
42 Z = -5098102
91
XDOT = 542
445069 XDOT = 165
337257
YDOT = -23708
944724 feet/sec YDOT = -7226
486352 meter/sec
ZDOT = -5033
951822 ZDOT = -1534
348515
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 07301
51847514
00020000 00000-0 20000-3 0 9117
2 25544 51
6323 136
3368 0001925 141
3246 218
8056 15
76064256 31815
Satellite: ISS
Catalog Number: 25544
Epoch time: 07301
51847514 = yrday
fracday
Element set: 911
Inclination: 51
6323 deg
RA of node: 136
3368 deg
Eccentricity:
0001925
Arg of perigee: 141
3246 deg
Mean anomaly: 218
8056 deg
Mean motion: 15
76064256 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3181
Checksum: 274
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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