Date:
October 10th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 3390 63 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 2865)
---------------------------------------
Vector Time (GMT): 2007/281/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4930762
34 A = 6719655
13 meter
Y = 1418216
94 meter E =
0012235
Z = 4331843
11 I = 51
35008
XDOT = 1016
880505 Wp = 70
39019
YDOT = 6847
931094 meter/sec RA = 238
51664 deg
ZDOT = -3387
636582 TA = 53
91571
MA = 53
80246
Ha = 188
670 n
mi
Hp = 180
520
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16177041
81 X = 4893493
64
Y = 4652942
73 feet Y = 1473147
49 meter
Z = 14212083
70 Z = 4355706
35
XDOT = 3336
222130 XDOT = 956
687025
YDOT = 22466
965533 feet/sec YDOT = 6858
965594 meter/sec
ZDOT = -11114
293248 ZDOT = -3382
843296
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16755769
15 X = -5107158
44
Y = -35140
20 feet Y = -10710
73 meter
Z = 14302896
42 Z = 4359522
83
XDOT = -9463
065856 XDOT = -2884
342473
YDOT = -19437
718340 feet/sec YDOT = -5924
616550 meter/sec
ZDOT = -11095
203700 ZDOT = -3381
818088
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 07281
54160763
00020000 00000-0 20000-3 0 9009
2 25544 51
6326 239
2005 0002757 70
4427 289
7034 15
75488250 28661
Satellite: ISS
Catalog Number: 25544
Epoch time: 07281
54160763 = yrday
fracday
Element set: 900
Inclination: 51
6326 deg
RA of node: 239
2005 deg
Eccentricity:
0002757
Arg of perigee: 70
4427 deg
Mean anomaly: 289
7034 deg
Mean motion: 15
75488250 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2866
Checksum: 292
Coasting Arc #2 (Orbit 2881)
---------------------------------------
Vector Time (GMT): 2007/282/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -926954
37 A = 6722938
11 meter
Y = -5743669
44 meter E =
0015257
Z = 3355011
82 I = 51
37848
XDOT = 5909
340895 Wp = 87
48896
YDOT = 1758
558433 meter/sec RA = 233
40010 deg
ZDOT = 4625
877712 TA = 312
25797
MA = 312
38726
Ha = 188
709 n
mi
Hp = 180
471
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3041188
89 X = -878957
19
Y = -18844059
84 feet Y = -5753766
52 meter
Z = 11007256
63 Z = 3350625
68
XDOT = 19387
601363 XDOT = 5866
765219
YDOT = 5769
548664 feet/sec YDOT = 1824
402363 meter/sec
ZDOT = 15176
764148 ZDOT = 4654
482148
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8473259
27 X = 2582649
42
Y = 17115319
12 feet Y = 5216749
27 meter
Z = 10989852
07 Z = 3349706
91
XDOT = -18897
294143 XDOT = -5759
895255
YDOT = -496
262402 feet/sec YDOT = -151
260780 meter/sec
ZDOT = 15285
630846 ZDOT = 4659
060282
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 07282
55647504
00020000 00000-0 20000-3 0 9015
2 25544 51
6335 233
9766 0002685 76
8019 283
3444 15
75531040 28822
Satellite: ISS
Catalog Number: 25544
Epoch time: 07282
55647504 = yrday
fracday
Element set: 901
Inclination: 51
6335 deg
RA of node: 233
9766 deg
Eccentricity:
0002685
Arg of perigee: 76
8019 deg
Mean anomaly: 283
3444 deg
Mean motion: 15
75531040 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2882
Checksum: 299
Coasting Arc #3 (Orbit 2896)
---------------------------------------
Vector Time (GMT): 2007/283/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5390841
80 A = 6721878
74 meter
Y = -1612664
67 meter E =
0008413
Z = -3684991
68 I = 51
39336
XDOT = -1042
075900 Wp = 94
49179
YDOT = -6303
041028 meter/sec RA = 228
18256 deg
ZDOT = 4290
631717 TA = 220
99417
MA = 221
05744
Ha = 188
720 n
mi
Hp = 180
395
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17686488
85 X = -5354506
70
Y = -5290894
59 feet Y = -1672745
25 meter
Z = -12089867
71 Z = -3711092
52
XDOT = -3418
884186 XDOT = -992
360427
YDOT = -20679
268464 feet/sec YDOT = -6314
415800 meter/sec
ZDOT = 14076
875713 ZDOT = 4285
690469
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18391041
82 X = 5605589
55
Y = -403853
57 feet Y = -123094
57 meter
Z = -12189209
89 Z = -3715271
17
XDOT = 9678
947164 XDOT = 2950
143096
YDOT = 17249
736034 feet/sec YDOT = 5257
719543 meter/sec
ZDOT = 14057
287941 ZDOT = 4284
661364
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 07283
50790204
00020000 00000-0 20000-3 0 9028
2 25544 51
6336 229
0787 0002714 76
3032 283
8434 15
75507980 28971
Satellite: ISS
Catalog Number: 25544
Epoch time: 07283
50790204 = yrday
fracday
Element set: 902
Inclination: 51
6336 deg
RA of node: 229
0787 deg
Eccentricity:
0002714
Arg of perigee: 76
3032 deg
Mean anomaly: 283
8434 deg
Mean motion: 15
75507980 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2897
Checksum: 301
Coasting Arc #4 (Orbit 2912)
---------------------------------------
Vector Time (GMT): 2007/284/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 823384
50 A = 6720410
86 meter
Y = 5260476
14 meter E =
0010404
Z = -4111036
54 I = 51
40991
XDOT = -6437
419214 Wp = 73
26232
YDOT = -1920
036901 meter/sec RA = 223
06955 deg
ZDOT = -3751
079079 TA = 158
17003
MA = 158
12567
Ha = 188
696 n
mi
Hp = 180
388
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2701392
70 X = 784471
02
Y = 17258779
98 feet Y = 5269465
84 meter
Z = -13487652
69 Z = -4107131
32
XDOT = -21120
141778 XDOT = -6397
248124
YDOT = -6299
333666 feet/sec YDOT = -1991
799410 meter/sec
ZDOT = -12306
689892 ZDOT = -3782
255101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8233775
24 X = -2509654
69
Y = -15420320
93 feet Y = -4700113
82 meter
Z = -13472135
37 Z = -4106306
86
XDOT = 20830
716677 XDOT = 6349
202443
YDOT = -281
133428 feet/sec YDOT = -85
689469 meter/sec
ZDOT = -12425
351688 ZDOT = -3787
247195
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 07284
52274238
00020000 00000-0 20000-3 0 9036
2 25544 51
6346 223
8542 0002758 80
0156 280
1319 15
75558934 29136
Satellite: ISS
Catalog Number: 25544
Epoch time: 07284
52274238 = yrday
fracday
Element set: 903
Inclination: 51
6346 deg
RA of node: 223
8542 deg
Eccentricity:
0002758
Arg of perigee: 80
0156 deg
Mean anomaly: 280
1319 deg
Mean motion: 15
75558934 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2913
Checksum: 294
Coasting Arc #5 (Orbit 2928)
---------------------------------------
Vector Time (GMT): 2007/285/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5851792
91 A = 6724117
06 meter
Y = 1688652
44 meter E =
0016095
Z = 2833170
93 I = 51
44524
XDOT = 807
858109 Wp = 96
45202
YDOT = 5747
139603 meter/sec RA = 217
85795 deg
ZDOT = -5071
255535 TA = 50
90903
MA = 50
76600
Ha = 188
596 n
mi
Hp = 180
334
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19198795
64 X = 5818711
82
Y = 5540198
30 feet Y = 1753905
68 meter
Z = 9295180
22 Z = 2861519
26
XDOT = 2650
453114 XDOT = 768
168596
YDOT = 18855
444892 feet/sec YDOT = 5755
951354 meter/sec
ZDOT = -16637
977477 ZDOT = -5067
427559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19887674
07 X = -6061763
06
Y = 1323065
14 feet Y = 403270
25 meter
Z = 9403076
36 Z = 2866057
67
XDOT = -8914
746882 XDOT = -2717
214850
YDOT = -15338
422772 feet/sec YDOT = -4675
151261 meter/sec
ZDOT = -16622
691310 ZDOT = -5066
596311
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 07285
53756821
00020000 00000-0 20000-3 0 9042
2 25544 51
6350 218
6303 0002722 83
4798 276
6676 15
75577371 29297
Satellite: ISS
Catalog Number: 25544
Epoch time: 07285
53756821 = yrday
fracday
Element set: 904
Inclination: 51
6350 deg
RA of node: 218
6303 deg
Eccentricity:
0002722
Arg of perigee: 83
4798 deg
Mean anomaly: 276
6676 deg
Mean motion: 15
75577371 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2929
Checksum: 321
Coasting Arc #6 (Orbit 2944)
---------------------------------------
Vector Time (GMT): 2007/286/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -534406
39 A = 6718016
20 meter
Y = -4780505
60 meter E =
0010256
Z = 4683026
15 I = 51
44854
XDOT = 6958
093672 Wp = 110
95039
YDOT = 1896
070259 meter/sec RA = 212
74191 deg
ZDOT = 2721
171147 TA = 312
17170
MA = 312
25876
Ha = 188
575 n
mi
Hp = 180
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1753301
80 X = -503660
28
Y = -15684073
49 feet Y = -4786309
57 meter
Z = 15364259
03 Z = 4680504
77
XDOT = 22828
391313 XDOT = 6923
155051
YDOT = 6220
702951 feet/sec YDOT = 1973
684339 meter/sec
ZDOT = 8927
726861 ZDOT = 2754
889592
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7321142
04 X = 2231484
09
Y = 13992080
32 feet Y = 4264786
08 meter
Z = 15354063
03 Z = 4679918
41
XDOT = -22476
732304 XDOT = -6850
908006
YDOT = 1792
800081 feet/sec YDOT = 546
445465 meter/sec
ZDOT = 9056
054600 ZDOT = 2760
285442
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 07286
55237823
00020000 00000-0 20000-3 0 9052
2 25544 51
6350 213
4064 0002625 89
5761 270
5704 15
75618711 29450
Satellite: ISS
Catalog Number: 25544
Epoch time: 07286
55237823 = yrday
fracday
Element set: 905
Inclination: 51
6350 deg
RA of node: 213
4064 deg
Eccentricity:
0002625
Arg of perigee: 89
5761 deg
Mean anomaly: 270
5704 deg
Mean motion: 15
75618711 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2945
Checksum: 294
Coasting Arc #7 (Orbit 2959)
---------------------------------------
Vector Time (GMT): 2007/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6260444
54 A = 6726010
88 meter
Y = -1581385
74 meter E =
0008932
Z = -1876752
62 I = 51
50045
XDOT = -357
870458 Wp = 52
56342
YDOT = -5238
981155 meter/sec RA = 207
54348 deg
ZDOT = 5631
856475 TA = 286
54344
MA = 286
64154
Ha = 188
553 n
mi
Hp = 180
309
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20539516
21 X = -6233178
77
Y = -5188273
44 feet Y = -1651241
15 meter
Z = -6157324
87 Z = -1907100
47
XDOT = -1174
115677 XDOT = -326
620101
YDOT = -17188
258384 feet/sec YDOT = -5242
808259 meter/sec
ZDOT = 18477
219407 ZDOT = 5630
193872
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20959238
22 X = 6388375
81
Y = -2839834
57 feet Y = -865581
58 meter
Z = -6272816
73 Z = -1911954
54
XDOT = 7394
015542 XDOT = 2253
695937
YDOT = 13940
834907 feet/sec YDOT = 4249
166480 meter/sec
ZDOT = 18470
228501 ZDOT = 5629
725647
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 07287
50375106
00020000 00000-0 20000-3 0 9066
2 25544 51
6348 208
5084 0002635 90
0401 270
1065 15
75606075 29606
Satellite: ISS
Catalog Number: 25544
Epoch time: 07287
50375106 = yrday
fracday
Element set: 906
Inclination: 51
6348 deg
RA of node: 208
5084 deg
Eccentricity:
0002635
Arg of perigee: 90
0401 deg
Mean anomaly: 270
1065 deg
Mean motion: 15
75606075 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2960
Checksum: 274
Coasting Arc #8 (Orbit 2975)
---------------------------------------
Vector Time (GMT): 2007/288/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 26546
37 A = 6716208
47 meter
Y = 4394451
99 meter E =
0016410
Z = -5093424
12 I = 51
49447
XDOT = -7340
783655 Wp = 81
07985
YDOT = -1717
992378 meter/sec RA = 202
41559 deg
ZDOT = -1522
155214 TA = 174
28030
MA = 174
26154
Ha = 188
542 n
mi
Hp = 180
227
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 87094
39 X = 2148
57
Y = 14417493
42 feet Y = 4394612
46 meter
Z = -16710709
04 Z = -5093354
39
XDOT = -24083
935875 XDOT = -7313
632665
YDOT = -5636
457934 feet/sec YDOT = -1799
929359 meter/sec
ZDOT = -4993
947552 ZDOT = -1557
751748
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5777359
61 X = -1760939
21
Y = -13210659
20 feet Y = -4026608
92 meter
Z = -16709880
25 Z = -5093171
50
XDOT = 23389
376791 XDOT = 7129
082046
YDOT = -3747
600832 feet/sec YDOT = -1142
268734 meter/sec
ZDOT = -5129
408221 ZDOT = -1563
443626
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 07288
51853316
00020000 00000-0 20000-3 0 9073
2 25544 51
6354 203
2837 0002713 93
9613 266
1861 15
75652840 29762
Satellite: ISS
Catalog Number: 25544
Epoch time: 07288
51853316 = yrday
fracday
Element set: 907
Inclination: 51
6354 deg
RA of node: 203
2837 deg
Eccentricity:
0002713
Arg of perigee: 93
9613 deg
Mean anomaly: 266
1861 deg
Mean motion: 15
75652840 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2976
Checksum: 307
Coasting Arc #9 (Orbit 2991)
---------------------------------------
Vector Time (GMT): 2007/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6530077
31 A = 6727225
12 meter
Y = 1390981
05 meter E =
0015954
Z = 764359
26 I = 51
55876
XDOT = -326
940391 Wp = 122
52118
YDOT = 4860
474273 meter/sec RA = 197
23876 deg
ZDOT = -5970
325299 TA = 49
12897
MA = 48
99083
Ha = 188
528 n
mi
Hp = 180
258
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21424138
16 X = 6510324
61
Y = 4563586
13 feet Y = 1463893
61 meter
Z = 2507740
36 Z = 796035
18
XDOT = -1072
639079 XDOT = -352
263189
YDOT = 15946
437904 feet/sec YDOT = 4856
676758 meter/sec
ZDOT = -19587
681428 ZDOT = -5971
975040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21423815
78 X = -6529979
05
Y = 4496783
06 feet Y = 1370619
48 meter
Z = 2628276
15 Z = 801098
57
XDOT = -5249
384356 XDOT = -1600
012352
YDOT = -13408
121085 feet/sec YDOT = -4086
795307 meter/sec
ZDOT = -19593
327722 ZDOT = -5972
046290
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 07289
53330082
00020000 00000-0 20000-3 0 9087
2 25544 51
6352 198
0590 0002671 99
3537 260
7929 15
75645397 29927
Satellite: ISS
Catalog Number: 25544
Epoch time: 07289
53330082 = yrday
fracday
Element set: 908
Inclination: 51
6352 deg
RA of node: 198
0590 deg
Eccentricity:
0002671
Arg of perigee: 99
3537 deg
Mean anomaly: 260
7929 deg
Mean motion: 15
75645397 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2992
Checksum: 326
Coasting Arc #10 (Orbit 3007)
---------------------------------------
Vector Time (GMT): 2007/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 618972
90 A = 6715220
36 meter
Y = -4132920
86 meter E =
0004984
Z = 5252301
97 I = 51
54676
XDOT = 7570
246789 Wp = 103
10288
YDOT = 1432
360220 meter/sec RA = 192
09421 deg
ZDOT = 233
657516 TA = 344
67119
MA = 344
68628
Ha = 188
336 n
mi
Hp = 180
241
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2030750
97 X = 639626
58
Y = -13559451
65 feet Y = -4125883
80 meter
Z = 17231961
84 Z = 5255359
07
XDOT = 24836
767680 XDOT = 7552
532191
YDOT = 4699
344553 feet/sec YDOT = 1516
915949 meter/sec
ZDOT = 766
592901 ZDOT = 270
391533
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3948758
09 X = 1203581
46
Y = 13115170
68 feet Y = 3997504
02 meter
Z = 17243050
63 Z = 5255681
83
XDOT = -23548
959744 XDOT = -7177
722930
YDOT = 5892
964413 feet/sec YDOT = 1796
175553 meter/sec
ZDOT = 906
368942 ZDOT = 276
261253
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
54805129
00020000 00000-0 20000-3 0 9090
2 25544 51
6350 192
8343 0002499 102
4327 257
7117 15
75720701 30081
Satellite: ISS
Catalog Number: 25544
Epoch time: 07290
54805129 = yrday
fracday
Element set: 909
Inclination: 51
6350 deg
RA of node: 192
8343 deg
Eccentricity:
0002499
Arg of perigee: 102
4327 deg
Mean anomaly: 257
7117 deg
Mean motion: 15
75720701 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3008
Checksum: 283
Coasting Arc #11 (Orbit 3023)
---------------------------------------
Vector Time (GMT): 2007/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6620649
08 A = 6727296
11 meter
Y = -1099728
60 meter E =
0014479
Z = 367875
38 I = 51
61619
XDOT = 1119
574057 Wp = 57
10015
YDOT = -4670
587269 meter/sec RA = 186
94251 deg
ZDOT = 6023
843432 TA = 306
90364
MA = 307
03623
Ha = 188
380 n
mi
Hp = 180
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21721289
62 X = -6609646
78
Y = -3608033
47 feet Y = -1173702
94 meter
Z = 1206940
22 Z = 335738
42
XDOT = 3673
143233 XDOT = 1142
454819
YDOT = -15323
449044 feet/sec YDOT = -4657
939746 meter/sec
ZDOT = 19763
265852 ZDOT = 6029
337899
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21125914
79 X = 6439178
83
Y = -6229628
09 feet Y = -1898790
64 meter
Z = 1084661
61 Z = 330604
86
XDOT = 3023
760296 XDOT = 921
642138
YDOT = 13802
263729 feet/sec YDOT = 4206
929985 meter/sec
ZDOT = 19783
549859 ZDOT = 6030
025997
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
56279009
00020000 00000-0 20000-3 0 9107
2 25544 51
6353 187
6092 0002527 103
6320 256
5125 15
75703198 30240
Satellite: ISS
Catalog Number: 25544
Epoch time: 07291
56279009 = yrday
fracday
Element set: 910
Inclination: 51
6353 deg
RA of node: 187
6092 deg
Eccentricity:
0002527
Arg of perigee: 103
6320 deg
Mean anomaly: 256
5125 deg
Mean motion: 15
75703198 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3024
Checksum: 279
Coasting Arc #12 (Orbit 3038)
---------------------------------------
Vector Time (GMT): 2007/292/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509113
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1358545
48 A = 6715517
76 meter
Y = 4066973
12 meter E =
0016913
Z = -5183139
56 I = 51
60625
XDOT = -7530
375760 Wp = 99
95270
YDOT = -1108
962493 meter/sec RA = 181
77890 deg
ZDOT = 1103
800297 TA = 180
59725
MA = 180
59927
Ha = 188
289 n
mi
Hp = 180
183
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4457170
21 X = -1378742
91
Y = 13343087
67 feet Y = 4051668
21 meter
Z = -17005051
06 Z = -5189788
49
XDOT = -24705
957217 XDOT = -7522
777635
YDOT = -3638
328390 feet/sec YDOT = -1193
128943 meter/sec
ZDOT = 3621
392050 ZDOT = 1067
235665
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2133804
78 X = -650383
70
Y = -13874756
16 feet Y = -4229025
68 meter
Z = -17029801
38 Z = -5190683
46
XDOT = 22692
680528 XDOT = 6916
729025
YDOT = -7763
326419 feet/sec YDOT = -2366
261892 meter/sec
ZDOT = 3482
268781 ZDOT = 1061
395524
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
51409224
00020000 00000-0 20000-3 0 9118
2 25544 51
6358 182
7107 0002467 107
7041 252
4393 15
75742342 30398
Satellite: ISS
Catalog Number: 25544
Epoch time: 07292
51409224 = yrday
fracday
Element set: 911
Inclination: 51
6358 deg
RA of node: 182
7107 deg
Eccentricity:
0002467
Arg of perigee: 107
7041 deg
Mean anomaly: 252
4393 deg
Mean motion: 15
75742342 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3039
Checksum: 278
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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