Date:
May 15th 2009
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) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 ET - UTC (sec) : 66 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 49)
---------------------------------------
Vector Time (GMT): 2009/133/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4455651
36 A = 6724974
74 meter
Y = -421258
66 meter E =
0007562
Z = 5013980
39 I = 51
89476
XDOT = 2819
672414 Wp = 34
97225
YDOT = -6904
155600 meter/sec RA = 123
92675 deg
ZDOT = 1930
264685 TA = 36
48517
MA = 36
43367
Ha = 194
203 n
mi
Hp = 184
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14618278
74 X = -4474966
83
Y = -1382082
23 feet Y = -471192
97 meter
Z = 16450066
89 Z = 4992287
68
XDOT = 9250
893747 XDOT = 2887
289327
YDOT = -22651
429134 feet/sec YDOT = -6872
246548 meter/sec
ZDOT = 6332
889387 ZDOT = 1944
126167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10404243
56 X = -3171213
44
Y = 10494917
28 feet Y = 3198850
79 meter
Z = 16365126
11 Z = 4988090
44
XDOT = -10894
937093 XDOT = -3320
776826
YDOT = -20735
975374 feet/sec YDOT = -6320
325294 meter/sec
ZDOT = 6386
703950 ZDOT = 1946
667364
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 09133
55100165
00010596 00000-0 82463-4 0 9009
2 25544 51
6361 124
5568 0009493 357
4442 2
6671 15
72725692 502
Satellite: ISS
Catalog Number: 25544
Epoch time: 09133
55100165 = yrday
fracday
Element set: 900
Inclination: 51
6361 deg
RA of node: 124
5568 deg
Eccentricity:
0009493
Arg of perigee: 357
4442 deg
Mean anomaly: 2
6671 deg
Mean motion: 15
72725692 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 50
Checksum: 291
Coasting Arc #2 (Orbit 64)
---------------------------------------
Vector Time (GMT): 2009/134/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1555350
16 A = 6733850
83 meter
Y = 6205862
35 meter E =
0015104
Z = -2075864
24 I = 51
94066
XDOT = -5280
721589 Wp = 17
74113
YDOT = 535
396266 meter/sec RA = 118
78680 deg
ZDOT = 5581
799943 TA = 319
18177
MA = 319
29481
Ha = 194
192 n
mi
Hp = 184
669
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5102854
84 X = -1614545
33
Y = 20360440
77 feet Y = 6188138
77 meter
Z = -6810578
23 Z = -2083563
26
XDOT = -17325
202064 XDOT = -5313
431528
YDOT = 1756
549428 feet/sec YDOT = 476
160634 meter/sec
ZDOT = 18312
991940 ZDOT = 5556
066659
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12811071
51 X = 3904814
60
Y = 16614965
39 feet Y = 5064241
45 meter
Z = -6840323
34 Z = -2084930
55
XDOT = -8238
960296 XDOT = -2511
235098
YDOT = 13817
535895 feet/sec YDOT = 4211
584941 meter/sec
ZDOT = 18212
285782 ZDOT = 5551
104706
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 09134
50410757
00010596 00000-0 82463-4 0 9017
2 25544 51
6363 119
6718 0009499 1
8797 358
2399 15
72747550 655
Satellite: ISS
Catalog Number: 25544
Epoch time: 09134
50410757 = yrday
fracday
Element set: 901
Inclination: 51
6363 deg
RA of node: 119
6718 deg
Eccentricity:
0009499
Arg of perigee: 1
8797 deg
Mean anomaly: 358
2399 deg
Mean motion: 15
72747550 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 65
Checksum: 332
Coasting Arc #3 (Orbit 80)
---------------------------------------
Vector Time (GMT): 2009/135/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4622664
28 A = 6726225
81 meter
Y = -1342980
66 meter E =
0017282
Z = -4713231
64 I = 51
92826
XDOT = -761
463747 Wp = 40
70658
YDOT = 7128
369760 meter/sec RA = 113
72040 deg
ZDOT = -2770
854224 TA = 202
00128
MA = 202
07556
Ha = 194
302 n
mi
Hp = 184
626
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15166221
37 X = 4660234
27
Y = -4406104
53 feet Y = -1291076
80 meter
Z = -15463358
40 Z = -4690683
52
XDOT = -2498
240640 XDOT = -827
657420
YDOT = 23387
039894 feet/sec YDOT = 7119
484796 meter/sec
ZDOT = -9090
729080 ZDOT = -2774
713505
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5769237
71 X = 1758463
65
Y = -14794042
56 feet Y = -4509224
17 meter
Z = -15375164
45 Z = -4686350
12
XDOT = 16010
566740 XDOT = 4880
020742
YDOT = 15731
132241 feet/sec YDOT = 4794
849107 meter/sec
ZDOT = -9105
389665 ZDOT = -2775
322770
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 09135
52074468
00010596 00000-0 82463-4 0 9026
2 25544 51
6365 114
4593 0009546 5
1886 354
9374 15
72752593 817
Satellite: ISS
Catalog Number: 25544
Epoch time: 09135
52074468 = yrday
fracday
Element set: 902
Inclination: 51
6365 deg
RA of node: 114
4593 deg
Eccentricity:
0009546
Arg of perigee: 5
1886 deg
Mean anomaly: 354
9374 deg
Mean motion: 15
72752593 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 81
Checksum: 323
Coasting Arc #4 (Orbit 96)
---------------------------------------
Vector Time (GMT): 2009/136/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -211046
36 A = 6732334
58 meter
Y = -6138268
45 meter E =
0016334
Z = 2754375
89 I = 51
96010
XDOT = 5114
032729 Wp = 64
36549
YDOT = -2511
106182 meter/sec RA = 108
57175 deg
ZDOT = -5173
715408 TA = 84
33198
MA = 84
14574
Ha = 194
366 n
mi
Hp = 184
286
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -692409
32 X = -155771
84
Y = -20138676
03 feet Y = -6140319
67 meter
Z = 9036666
32 Z = 2753484
37
XDOT = 16778
322603 XDOT = 5166
865336
YDOT = -8238
537341 feet/sec YDOT = -2453
622240 meter/sec
ZDOT = -16974
131915 ZDOT = -5148
743209
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16645552
14 X = -5073564
29
Y = -11359634
12 feet Y = -3462416
48 meter
Z = 9032792
89 Z = 2753195
27
XDOT = 2564
489461 XDOT = 781
656388
YDOT = -17257
209658 feet/sec YDOT = -5259
997504 meter/sec
ZDOT = -16876
512621 ZDOT = -5143
961047
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 09136
53737059
00010596 00000-0 82463-4 0 9031
2 25544 51
6365 109
2477 0009686 8
1691 351
9627 15
72790572 976
Satellite: ISS
Catalog Number: 25544
Epoch time: 09136
53737059 = yrday
fracday
Element set: 903
Inclination: 51
6365 deg
RA of node: 109
2477 deg
Eccentricity:
0009686
Arg of perigee: 8
1691 deg
Mean anomaly: 351
9627 deg
Mean motion: 15
72790572 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 97
Checksum: 337
Coasting Arc #5 (Orbit 112)
---------------------------------------
Vector Time (GMT): 2009/137/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4187095
40 A = 6727544
95 meter
Y = 3020106
92 meter E =
0012887
Z = 4300137
82 I = 51
95312
XDOT = -1226
552481 Wp = 60
73619
YDOT = -6737
503087 meter/sec RA = 103
51567 deg
ZDOT = 3535
906587 TA = 353
62398
MA = 353
64037
Ha = 194
466 n
mi
Hp = 184
084
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13737189
62 X = -4241444
96
Y = 9908487
26 feet Y = 2972980
18 meter
Z = 14108063
73 Z = 4279664
99
XDOT = -4024
122313 XDOT = -1168
298322
YDOT = -22104
668921 feet/sec YDOT = -6750
893650 meter/sec
ZDOT = 11600
743396 ZDOT = 3530
088976
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 58988
83 X = 17979
80
Y = 17003977
85 feet Y = 5182812
45 meter
Z = 14028086
76 Z = 4275760
85
XDOT = -19140
828974 XDOT = -5834
124671
YDOT = -9489
628497 feet/sec YDOT = -2892
438766 meter/sec
ZDOT = 11577
548581 ZDOT = 3528
836808
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 09137
55398562
00010596 00000-0 82463-4 0 9047
2 25544 51
6370 104
0366 0009529 11
5332 348
6047 15
72830034 1134
Satellite: ISS
Catalog Number: 25544
Epoch time: 09137
55398562 = yrday
fracday
Element set: 904
Inclination: 51
6370 deg
RA of node: 104
0366 deg
Eccentricity:
0009529
Arg of perigee: 11
5332 deg
Mean anomaly: 348
6047 deg
Mean motion: 15
72830034 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 113
Checksum: 291
Coasting Arc #6 (Orbit 127)
---------------------------------------
Vector Time (GMT): 2009/138/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1881550
45 A = 6730620
48 meter
Y = 5492835
58 meter E =
0011990
Z = -3401230
12 I = 51
96874
XDOT = -4319
274869 Wp = 38
77931
YDOT = 4350
667410 meter/sec RA = 98
36165 deg
ZDOT = 4654
624941 TA = 281
30148
MA = 281
43618
Ha = 194
621 n
mi
Hp = 183
921
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6173065
77 X = 1836511
50
Y = 18021114
10 feet Y = 5513624
56 meter
Z = -11158891
46 Z = -3392198
52
XDOT = -14170
849308 XDOT = -4390
215276
YDOT = 14273
843209 feet/sec YDOT = 4301
969820 meter/sec
ZDOT = 15271
079202 ZDOT = 4633
469666
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18388278
26 X = 5604747
21
Y = 5053114
53 feet Y = 1540189
31 meter
Z = -11123192
41 Z = -3390349
05
XDOT = 4070
203690 XDOT = 1240
598085
YDOT = 18492
611856 feet/sec YDOT = 5636
548094 meter/sec
ZDOT = 15188
505275 ZDOT = 4629
456408
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 09138
50705472
00010596 00000-0 82463-4 0 9056
2 25544 51
6369 99
1503 0009734 15
5529 344
5930 15
72790950 1283
Satellite: ISS
Catalog Number: 25544
Epoch time: 09138
50705472 = yrday
fracday
Element set: 905
Inclination: 51
6369 deg
RA of node: 99
1503 deg
Eccentricity:
0009734
Arg of perigee: 15
5529 deg
Mean anomaly: 344
5930 deg
Mean motion: 15
72790950 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 128
Checksum: 319
Coasting Arc #7 (Orbit 143)
---------------------------------------
Vector Time (GMT): 2009/139/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3260022
32 A = 6729195
41 meter
Y = -4484834
56 meter E =
0014213
Z = -3829984
41 I = 51
96821
XDOT = 2952
224516 Wp = 40
60629
YDOT = 5726
286002 meter/sec RA = 93
30879 deg
ZDOT = -4190
607925 TA = 185
57765
MA = 185
59350
Ha = 194
600 n
mi
Hp = 183
748
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10695611
29 X = 3328535
82
Y = -14714024
14 feet Y = -4447995
78 meter
Z = -12565565
65 Z = -3813980
85
XDOT = 9685
775970 XDOT = 2908
330284
YDOT = 18787
027564 feet/sec YDOT = 5759
054319 meter/sec
ZDOT = -13748
713665 ZDOT = -4176
372115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6334814
86 X = -1930851
57
Y = -17097748
64 feet Y = -5211393
79 meter
Z = -12503165
98 Z = -3810964
99
XDOT = 19810
174983 XDOT = 6038
141335
YDOT = 2677
809955 feet/sec YDOT = 816
196474 meter/sec
ZDOT = -13692
627492 ZDOT = -4173
512860
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 09139
52364991
00010596 00000-0 82463-4 0 9067
2 25544 51
6376 93
9379 0009757 19
2764 340
8766 15
72838458 1441
Satellite: ISS
Catalog Number: 25544
Epoch time: 09139
52364991 = yrday
fracday
Element set: 906
Inclination: 51
6376 deg
RA of node: 93
9379 deg
Eccentricity:
0009757
Arg of perigee: 19
2764 deg
Mean anomaly: 340
8766 deg
Mean motion: 15
72838458 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 144
Checksum: 358
Coasting Arc #8 (Orbit 159)
---------------------------------------
Vector Time (GMT): 2009/140/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3206670
34 A = 6728846
43 meter
Y = -4431126
44 meter E =
0018366
Z = 3914992
59 I = 51
96798
XDOT = 3004
578791 Wp = 53
55934
YDOT = -5798
445208 meter/sec RA = 88
15384 deg
ZDOT = -4078
086723 TA = 78
80017
MA = 78
59378
Ha = 194
694 n
mi
Hp = 183
532
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10520571
98 X = -3175901
07
Y = -14537816
42 feet Y = -4466813
51 meter
Z = 12844463
87 Z = 3899488
76
XDOT = 9857
541966 XDOT = 3089
005632
YDOT = -19023
770369 feet/sec YDOT = -5764
373938 meter/sec
ZDOT = -13379
549617 ZDOT = -4063
285515
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17953249
03 X = -5472150
31
Y = 1128666
73 feet Y = 344017
62 meter
Z = 12783495
37 Z = 3896409
39
XDOT = -10628
616495 XDOT = -3239
602308
YDOT = -17288
940719 feet/sec YDOT = -5269
669131 meter/sec
ZDOT = -13321
926592 ZDOT = -4060
523225
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 09140
54023426
00010596 00000-0 82463-4 0 9077
2 25544 51
6380 88
7261 0009753 22
6030 337
5560 15
72854968 1605
Satellite: ISS
Catalog Number: 25544
Epoch time: 09140
54023426 = yrday
fracday
Element set: 907
Inclination: 51
6380 deg
RA of node: 88
7261 deg
Eccentricity:
0009753
Arg of perigee: 22
6030 deg
Mean anomaly: 337
5560 deg
Mean motion: 15
72854968 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 160
Checksum: 302
Coasting Arc #9 (Orbit 175)
---------------------------------------
Vector Time (GMT): 2009/141/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1904750
00 A = 6730772
96 meter
Y = 5551342
59 meter E =
0019387
Z = 3270625
36 I = 51
97299
XDOT = -4277
278845 Wp = 61
80488
YDOT = -4285
981079 meter/sec RA = 83
10108 deg
ZDOT = 4771
445700 TA = 336
36302
MA = 336
45198
Ha = 194
756 n
mi
Hp = 183
328
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6249179
80 X = -1982572
94
Y = 18213066
25 feet Y = 5529607
17 meter
Z = 10730398
15 Z = 3261183
29
XDOT = -14033
067077 XDOT = -4252
213705
YDOT = -14061
617714 feet/sec YDOT = -4333
672344 meter/sec
ZDOT = 15654
349411 ZDOT = 4750
726768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12231402
25 X = 3728131
41
Y = 14897862
14 feet Y = 4540868
38 meter
Z = 10693735
43 Z = 3259450
56
XDOT = -18282
562642 XDOT = -5572
525093
YDOT = 3802
928128 feet/sec YDOT = 1159
132494 meter/sec
ZDOT = 15572
974130 ZDOT = 4746
642515
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 09141
55680776
00010596 00000-0 82463-4 0 9087
2 25544 51
6385 83
5142 0009685 26
6501 333
5158 15
72869894 1762
Satellite: ISS
Catalog Number: 25544
Epoch time: 09141
55680776 = yrday
fracday
Element set: 908
Inclination: 51
6385 deg
RA of node: 83
5142 deg
Eccentricity:
0009685
Arg of perigee: 26
6501 deg
Mean anomaly: 333
5158 deg
Mean motion: 15
72869894 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 176
Checksum: 339
Coasting Arc #10 (Orbit 190)
---------------------------------------
Vector Time (GMT): 2009/142/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4146161
28 A = 6727124
59 meter
Y = 2983797
54 meter E =
0014303
Z = -4385541
82 I = 51
95634
XDOT = -1282
438468 Wp = 68
29217
YDOT = 6773
750266 meter/sec RA = 77
94781 deg
ZDOT = 3410
224774 TA = 235
90295
MA = 236
03875
Ha = 194
828 n
mi
Hp = 183
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13602891
33 X = 4133792
48
Y = 9789361
99 feet Y = 3030093
64 meter
Z = -14388260
56 Z = -4365429
00
XDOT = -4207
475290 XDOT = -1374
655028
YDOT = 22223
590110 feet/sec YDOT = 6758
893318 meter/sec
ZDOT = 11188
401491 ZDOT = 3403
771257
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15382657
51 X = 4688634
01
Y = -6819754
06 feet Y = -2078661
04 meter
Z = -14309336
29 Z = -4361485
70
XDOT = 16478
946607 XDOT = 5022
782926
YDOT = 13843
385605 feet/sec YDOT = 4219
463932 meter/sec
ZDOT = 11163
494949 ZDOT = 3402
633260
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 09142
50983599
00010596 00000-0 82463-4 0 9093
2 25544 51
6390 78
6280 0009752 29
7395 330
4320 15
72875333 1915
Satellite: ISS
Catalog Number: 25544
Epoch time: 09142
50983599 = yrday
fracday
Element set: 909
Inclination: 51
6390 deg
RA of node: 78
6280 deg
Eccentricity:
0009752
Arg of perigee: 29
7395 deg
Mean anomaly: 330
4320 deg
Mean motion: 15
72875333 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 191
Checksum: 328
Coasting Arc #11 (Orbit 206)
---------------------------------------
Vector Time (GMT): 2009/143/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 314209
99 A = 6732126
85 meter
Y = -6164808
32 meter E =
0010935
Z = -2702674
11 I = 51
96728
XDOT = 5047
711521 Wp = 59
85010
YDOT = 2538
135918 meter/sec RA = 72
88987 deg
ZDOT = -5212
902122 TA = 150
76051
MA = 150
69926
Ha = 194
822 n
mi
Hp = 182
999
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1030872
68 X = 396251
98
Y = -20225749
08 feet Y = -6160835
55 meter
Z = -8867041
06 Z = -2700949
21
XDOT = 16560
733337 XDOT = 5044
278440
YDOT = 8327
217579 feet/sec YDOT = 2594
563899 meter/sec
ZDOT = -17102
697252 ZDOT = -5188
387733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17065094
48 X = -5201440
80
Y = -10910558
00 feet Y = -3325538
08 meter
Z = -8860604
73 Z = -2700712
32
XDOT = 14660
799657 XDOT = 4468
611735
YDOT = -9146
885476 feet/sec YDOT = -2787
970693 meter/sec
ZDOT = -17006
561543 ZDOT = -5183
599958
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 09143
52638865
00010596 00000-0 82463-4 0 9101
2 25544 51
6401 73
4159 0009805 33
6486 326
5297 15
72904915 2076
Satellite: ISS
Catalog Number: 25544
Epoch time: 09143
52638865 = yrday
fracday
Element set: 910
Inclination: 51
6401 deg
RA of node: 73
4159 deg
Eccentricity:
0009805
Arg of perigee: 33
6486 deg
Mean anomaly: 326
5297 deg
Mean motion: 15
72904915 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 207
Checksum: 317
Coasting Arc #12 (Orbit 222)
---------------------------------------
Vector Time (GMT): 2009/144/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 672334
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4572496
95 A = 6725699
97 meter
Y = -1418023
23 meter E =
0017185
Z = 4718040
41 I = 51
93576
XDOT = -618
946817 Wp = 48
20244
YDOT = -7173
438162 meter/sec RA = 67
74180 deg
ZDOT = -2738
291158 TA = 68
72912
MA = 68
54570
Ha = 194
974 n
mi
Hp = 182
859
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15001630
41 X = -4579220
39
Y = -4652307
19 feet Y = -1469193
95 meter
Z = 15479135
19 Z = 4695810
18
XDOT = -2030
665409 XDOT = -525
383822
YDOT = -23534
902107 feet/sec YDOT = -7179
835989 meter/sec
ZDOT = -8983
894876 ZDOT = -2741
072001
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11297700
39 X = -3443539
08
Y = 11033802
62 feet Y = 3363103
04 meter
Z = 15392000
16 Z = 4691481
65
XDOT = -20815
141096 XDOT = -6344
455006
YDOT = -8684
045749 feet/sec YDOT = -2646
897144 meter/sec
ZDOT = -8995
141403 ZDOT = -2741
719100
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 09144
54293075
00010596 00000-0 82463-4 0 9115
2 25544 51
6402 68
2045 0009780 37
3574 322
8266 15
72912101 2233
Satellite: ISS
Catalog Number: 25544
Epoch time: 09144
54293075 = yrday
fracday
Element set: 911
Inclination: 51
6402 deg
RA of node: 68
2045 deg
Eccentricity:
0009780
Arg of perigee: 37
3574 deg
Mean anomaly: 322
8266 deg
Mean motion: 15
72912101 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 223
Checksum: 288
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics 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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