Date:
May 6th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 22604 21 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 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 1674)
---------------------------------------
Vector Time (GMT): 2010/125/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1807474
56 A = 6731139
32 meter
Y = 6107857
17 meter E =
0008472
Z = -2159306
81 I = 51
99332
XDOT = -4267
815037 Wp = 317
36960
YDOT = 3224
166075 meter/sec RA = 88
87719 deg
ZDOT = 5541
038969 TA = 18
58519
MA = 18
55426
Ha = 188
917 n
mi
Hp = 187
445
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5930034
65 X = 1749530
61
Y = 20038901
48 feet Y = 6127745
55 meter
Z = -7084339
93 Z = -2150666
54
XDOT = -14002
017839 XDOT = -4330
468464
YDOT = 10577
972688 feet/sec YDOT = 3176
090254 meter/sec
ZDOT = 18179
261708 ZDOT = 5520
153848
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17936521
53 X = 5467051
76
Y = 10746711
27 feet Y = 3275597
60 meter
Z = -7049833
19 Z = -2148789
16
XDOT = -2478
590929 XDOT = -755
474515
YDOT = 16021
877999 feet/sec YDOT = 4883
468414 meter/sec
ZDOT = 18096
139567 ZDOT = 5515
703340
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 10125
50424338
00016717 00000-0 10270-3 0 9005
2 25544 51
6421 89
6439 0010040 278
8281 81
1745 15
73658583 16757
Satellite: ISS
Catalog Number: 25544
Epoch time: 10125
50424338 = yrday
fracday
Element set: 900
Inclination: 51
6421 deg
RA of node: 89
6439 deg
Eccentricity:
0010040
Arg of perigee: 278
8281 deg
Mean anomaly: 81
1745 deg
Mean motion: 15
73658583 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1675
Checksum: 306
Coasting Arc #2 (Orbit 1690)
---------------------------------------
Vector Time (GMT): 2010/126/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3425676
01 A = 6723073
66 meter
Y = -3234119
87 meter E =
0005976
Z = -4799699
43 I = 51
96563
XDOT = 2745
417416 Wp = 11
55505
YDOT = 6718
789377 meter/sec RA = 83
80698 deg
ZDOT = -2562
579684 TA = 233
41313
MA = 233
46813
Ha = 189
144 n
mi
Hp = 187
330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11239094
52 X = 3484902
06
Y = -10610629
50 feet Y = -3195480
62 meter
Z = -15747045
36 Z = -4782913
69
XDOT = 9007
274988 XDOT = 2682
531243
YDOT = 22043
272233 feet/sec YDOT = 6749
138735 meter/sec
ZDOT = -8407
413661 ZDOT = -2549
394943
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 925515
35 X = 282097
08
Y = -15496629
29 feet Y = -4723372
61 meter
Z = -15680243
74 Z = -4779338
29
XDOT = 20606
585822 XDOT = 6280
887359
YDOT = 9701
756153 feet/sec YDOT = 2957
095275 meter/sec
ZDOT = -8354
803281 ZDOT = -2546
544040
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 10126
52027681
00016717 00000-0 10270-3 0 9019
2 25544 51
6428 84
4287 0010125 282
7728 77
2303 15
73710167 16913
Satellite: ISS
Catalog Number: 25544
Epoch time: 10126
52027681 = yrday
fracday
Element set: 901
Inclination: 51
6428 deg
RA of node: 84
4287 deg
Eccentricity:
0010125
Arg of perigee: 282
7728 deg
Mean anomaly: 77
2303 deg
Mean motion: 15
73710167 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1691
Checksum: 296
Coasting Arc #3 (Orbit 1706)
---------------------------------------
Vector Time (GMT): 2010/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2957512
27 A = 6730603
46 meter
Y = -5587615
77 meter E =
0003831
Z = 2303892
84 I = 51
98723
XDOT = 3527
261195 Wp = 109
76226
YDOT = -4121
335300 meter/sec RA = 78
65761 deg
ZDOT = -5461
460111 TA = 44
47911
MA = 44
44836
Ha = 189
403 n
mi
Hp = 187
232
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9703124
24 X = -2906002
69
Y = -18332072
73 feet Y = -5620400
48 meter
Z = 7558703
54 Z = 2289650
17
XDOT = 11572
379249 XDOT = 3599
615480
YDOT = -13521
441272 feet/sec YDOT = -4081
486696 meter/sec
ZDOT = -17918
176217 ZDOT = -5444
148922
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19795789
98 X = -6033756
78
Y = -6260805
37 feet Y = -1908293
48 meter
Z = 7501901
45 Z = 2286579
56
XDOT = -1589
072509 XDOT = -484
349301
YDOT = -16387
076769 feet/sec YDOT = -4994
780999 meter/sec
ZDOT = -17849
290024 ZDOT = -5440
463599
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 10127
53628187
00016717 00000-0 10270-3 0 9020
2 25544 51
6431 79
2136 0010165 286
8397 73
1651 15
73754181 17076
Satellite: ISS
Catalog Number: 25544
Epoch time: 10127
53628187 = yrday
fracday
Element set: 902
Inclination: 51
6431 deg
RA of node: 79
2136 deg
Eccentricity:
0010165
Arg of perigee: 286
8397 deg
Mean anomaly: 73
1651 deg
Mean motion: 15
73754181 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1707
Checksum: 310
Coasting Arc #4 (Orbit 1722)
---------------------------------------
Vector Time (GMT): 2010/128/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2718574
62 A = 6722931
27 meter
Y = 3913206
38 meter E =
0002994
Z = 4745416
16 I = 51
95570
XDOT = -3969
582351 Wp = 266
16567
YDOT = -6020
927335 meter/sec RA = 73
58828 deg
ZDOT = 2692
169370 TA = 157
47628
MA = 157
46313
Ha = 189
593 n
mi
Hp = 186
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8919208
07 X = -2785183
32
Y = 12838603
59 feet Y = 3882433
15 meter
Z = 15568950
64 Z = 4732047
47
XDOT = -13023
564144 XDOT = -3915
038415
YDOT = -19753
698607 feet/sec YDOT = -6065
012639 meter/sec
ZDOT = 8832
576673 ZDOT = 2673
017366
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2824018
38 X = 860760
80
Y = 15429205
95 feet Y = 4702821
97 meter
Z = 15515758
53 Z = 4729203
20
XDOT = -22123
514774 XDOT = -6743
247303
YDOT = -4751
917081 feet/sec YDOT = -1448
384326 meter/sec
ZDOT = 8756
223043 ZDOT = 2668
896783
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 10128
55225661
00016717 00000-0 10270-3 0 9034
2 25544 51
6438 73
9984 0010280 289
7981 70
2074 15
73832234 17235
Satellite: ISS
Catalog Number: 25544
Epoch time: 10128
55225661 = yrday
fracday
Element set: 903
Inclination: 51
6438 deg
RA of node: 73
9984 deg
Eccentricity:
0010280
Arg of perigee: 289
7981 deg
Mean anomaly: 70
2074 deg
Mean motion: 15
73832234 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1723
Checksum: 313
Coasting Arc #5 (Orbit 1737)
---------------------------------------
Vector Time (GMT): 2010/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3944978
21 A = 6730227
52 meter
Y = 4891007
98 meter E =
0009741
Z = -2392383
62 I = 51
97019
XDOT = -2658
154370 Wp = 326
71266
YDOT = 4792
943199 meter/sec RA = 68
43526 deg
ZDOT = 5413
142904 TA = 6
43346
MA = 6
42096
Ha = 189
902 n
mi
Hp = 186
706
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12942841
89 X = 3901614
79
Y = 16046614
10 feet Y = 4934880
65 meter
Z = -7849027
64 Z = -2373323
93
XDOT = -8720
978903 XDOT = -2737
848768
YDOT = 15724
879261 feet/sec YDOT = 4762
772455 meter/sec
ZDOT = 17759
655198 ZDOT = 5400
035919
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20578307
85 X = 6272268
23
Y = 1652556
66 feet Y = 503699
27 meter
Z = -7773063
59 Z = -2369229
78
XDOT = 5428
157821 XDOT = 1654
502504
YDOT = 15733
255385 feet/sec YDOT = 4795
496241 meter/sec
ZDOT = 17707
510495 ZDOT = 5397
249199
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 10129
50470949
00016717 00000-0 10270-3 0 9042
2 25544 51
6435 69
1084 0010293 294
3181 65
6907 15
73826306 17380
Satellite: ISS
Catalog Number: 25544
Epoch time: 10129
50470949 = yrday
fracday
Element set: 904
Inclination: 51
6435 deg
RA of node: 69
1084 deg
Eccentricity:
0010293
Arg of perigee: 294
3181 deg
Mean anomaly: 65
6907 deg
Mean motion: 15
73826306 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1738
Checksum: 316
Coasting Arc #6 (Orbit 1753)
---------------------------------------
Vector Time (GMT): 2010/130/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1918118
31 A = 6722870
74 meter
Y = -4402578
42 meter E =
0008598
Z = -4709770
26 I = 51
93502
XDOT = 5006
246386 Wp = 9
86092
YDOT = 5148
951338 meter/sec RA = 63
36468 deg
ZDOT = -2766
707308 TA = 232
93090
MA = 233
00955
Ha = 189
942 n
mi
Hp = 186
479
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6293039
06 X = 1990085
77
Y = -14444154
91 feet Y = -4380726
38 meter
Z = -15452002
16 Z = -4700277
17
XDOT = 16424
692867 XDOT = 4961
738197
YDOT = 16892
884967 feet/sec YDOT = 5204
685371 meter/sec
ZDOT = -9077
123713 ZDOT = -2742
494547
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6312858
72 X = -1924159
34
Y = -14475820
16 feet Y = -4412229
98 meter
Z = -15414239
13 Z = -4698260
09
XDOT = 22532
452644 XDOT = 6867
891566
YDOT = -237
079861 feet/sec YDOT = -72
261942 meter/sec
ZDOT = -8980
643504 ZDOT = -2737
300140
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 10130
52063007
00016717 00000-0 10270-3 0 9050
2 25544 51
6445 63
8925 0010230 298
2461 61
7669 15
73899863 17549
Satellite: ISS
Catalog Number: 25544
Epoch time: 10130
52063007 = yrday
fracday
Element set: 905
Inclination: 51
6445 deg
RA of node: 63
8925 deg
Eccentricity:
0010230
Arg of perigee: 298
2461 deg
Mean anomaly: 61
7669 deg
Mean motion: 15
73899863 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1754
Checksum: 313
Coasting Arc #7 (Orbit 1769)
---------------------------------------
Vector Time (GMT): 2010/131/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4766064
95 A = 6729866
52 meter
Y = -4084484
29 meter E =
0004912
Z = 2426160
29 I = 51
94474
XDOT = 1725
902531 Wp = 71
07396
YDOT = -5219
601619 meter/sec RA = 58
20952 deg
ZDOT = -5386
472105 TA = 81
67648
MA = 81
62078
Ha = 190
090 n
mi
Hp = 186
264
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15636696
02 X = -4731823
37
Y = -13400539
01 feet Y = -4137589
90 meter
Z = 7959843
48 Z = 2403089
30
XDOT = 5662
409880 XDOT = 1810
307822
YDOT = -17124
677227 feet/sec YDOT = -5199
829408 meter/sec
ZDOT = -17672
152575 ZDOT = -5377
882675
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20433743
08 X = -6228204
89
Y = 2828010
39 feet Y = 861977
57 meter
Z = 7867929
68 Z = 2398144
97
XDOT = -8769
038892 XDOT = -2672
803054
YDOT = -14193
332040 feet/sec YDOT = -4326
127606 meter/sec
ZDOT = -17637
987161 ZDOT = -5376
058487
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 10131
53652190
00016717 00000-0 10270-3 0 9060
2 25544 51
6451 58
6769 0010269 301
8519 58
1644 15
73933400 17708
Satellite: ISS
Catalog Number: 25544
Epoch time: 10131
53652190 = yrday
fracday
Element set: 906
Inclination: 51
6451 deg
RA of node: 58
6769 deg
Eccentricity:
0010269
Arg of perigee: 301
8519 deg
Mean anomaly: 58
1644 deg
Mean motion: 15
73933400 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1770
Checksum: 302
Coasting Arc #8 (Orbit 1785)
---------------------------------------
Vector Time (GMT): 2010/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1106684
91 A = 6722605
78 meter
Y = 4672733
12 meter E =
0002710
Z = 4705023
74 I = 51
90429
XDOT = -5846
481334 Wp = 325
71961
YDOT = -4173
617558 meter/sec RA = 53
13657 deg
ZDOT = 2772
761874 TA = 97
06505
MA = 97
03423
Ha = 190
233 n
mi
Hp = 185
903
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3630855
99 X = -1181710
67
Y = 15330489
25 feet Y = 4659937
74 meter
Z = 15436429
61 Z = 4699465
39
XDOT = -19181
369206 XDOT = -5812
846541
YDOT = -13692
970990 feet/sec YDOT = -4238
808498 meter/sec
ZDOT = 9096
987776 ZDOT = 2744
440476
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9213121
73 X = 2808159
50
Y = 12806539
24 feet Y = 3903433
16 meter
Z = 15414321
77 Z = 4698285
27
XDOT = -21982
334072 XDOT = -6700
215425
YDOT = 5012
349723 feet/sec YDOT = 1527
764196 meter/sec
ZDOT = 8984
172287 ZDOT = 2738
375713
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 10132
55238422
00016717 00000-0 10270-3 0 9072
2 25544 51
6454 53
4608 0010268 305
1805 54
8396 15
73988320 17865
Satellite: ISS
Catalog Number: 25544
Epoch time: 10132
55238422 = yrday
fracday
Element set: 907
Inclination: 51
6454 deg
RA of node: 53
4608 deg
Eccentricity:
0010268
Arg of perigee: 305
1805 deg
Mean anomaly: 54
8396 deg
Mean motion: 15
73988320 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1786
Checksum: 311
Coasting Arc #9 (Orbit 1800)
---------------------------------------
Vector Time (GMT): 2010/133/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5409480
60 A = 6729655
51 meter
Y = 3179826
89 meter E =
0011120
Z = -2411295
30 I = 51
90962
XDOT = -792
978441 Wp = 338
75902
YDOT = 5440
323422 meter/sec RA = 47
97831 deg
ZDOT = 5397
751206 TA = 354
12673
MA = 354
13976
Ha = 190
447 n
mi
Hp = 185
613
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17747639
77 X = 5385235
06
Y = 10432502
91 feet Y = 3240183
56 meter
Z = -7911073
83 Z = -2385074
07
XDOT = -2601
635305 XDOT = -879
976075
YDOT = 17848
830124 feet/sec YDOT = 5430
968970 meter/sec
ZDOT = 17709
157500 ZDOT = 5393
687976
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19385129
94 X = 5908587
61
Y = -7047987
36 feet Y = -2148226
55 meter
Z = -7806634
04 Z = -2379462
06
XDOT = 11505
527978 XDOT = 3506
884928
YDOT = 12056
884214 feet/sec YDOT = 3674
938308 meter/sec
ZDOT = 17692
997130 ZDOT = 5392
825525
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 10133
50473005
00016717 00000-0 10270-3 0 9087
2 25544 51
6459 48
5707 0010333 309
0085 51
0158 15
74019378 18013
Satellite: ISS
Catalog Number: 25544
Epoch time: 10133
50473005 = yrday
fracday
Element set: 908
Inclination: 51
6459 deg
RA of node: 48
5707 deg
Eccentricity:
0010333
Arg of perigee: 309
0085 deg
Mean anomaly: 51
0158 deg
Mean motion: 15
74019378 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1801
Checksum: 284
Coasting Arc #10 (Orbit 1816)
---------------------------------------
Vector Time (GMT): 2010/134/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 300868
53 A = 6722260
93 meter
Y = -4781742
53 meter E =
0011150
Z = -4722459
87 I = 51
86518
XDOT = 6489
149254 Wp = 15
97319
YDOT = 3109
167006 meter/sec RA = 42
90228 deg
ZDOT = -2725
796843 TA = 227
21183
MA = 227
30565
Ha = 190
463 n
mi
Hp = 185
303
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 987101
49 X = 377257
81
Y = -15688131
67 feet Y = -4777950
40 meter
Z = -15493634
75 Z = -4720813
20
XDOT = 21289
859757 XDOT = 6467
141399
YDOT = 10200
679153 feet/sec YDOT = 3181
609785 meter/sec
ZDOT = -8942
903027 ZDOT = -2694
325007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11578507
70 X = -3529129
15
Y = -10641093
91 feet Y = -3243405
42 meter
Z = -15487086
32 Z = -4720463
91
XDOT = 20520
187923 XDOT = 6254
553279
YDOT = -9451
907085 feet/sec YDOT = -2880
941280 meter/sec
ZDOT = -8817
555985 ZDOT = -2687
591064
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 10134
52053694
00016717 00000-0 10270-3 0 9099
2 25544 51
6468 43
3547 0010329 313
2097 46
8202 15
74083513 18174
Satellite: ISS
Catalog Number: 25544
Epoch time: 10134
52053694 = yrday
fracday
Element set: 909
Inclination: 51
6468 deg
RA of node: 43
3547 deg
Eccentricity:
0010329
Arg of perigee: 313
2097 deg
Mean anomaly: 46
8202 deg
Mean motion: 15
74083513 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1817
Checksum: 297
Coasting Arc #11 (Orbit 1832)
---------------------------------------
Vector Time (GMT): 2010/135/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5898076
72 A = 6729618
04 meter
Y = -2247513
18 meter E =
0007054
Z = 2334771
62 I = 51
86651
XDOT = -78
424157 Wp = 61
97230
YDOT = -5452
235800 meter/sec RA = 37
74128 deg
ZDOT = -5430
941386 TA = 91
85572
MA = 91
77493
Ha = 190
611 n
mi
Hp = 185
164
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19350645
41 X = -5883848
35
Y = -7373730
90 feet Y = -2313389
73 meter
Z = 7660011
88 Z = 2306152
54
XDOT = -257
297104 XDOT = 8
932532
YDOT = -17887
912731 feet/sec YDOT = -5452
623641 meter/sec
ZDOT = -17818
049168 ZDOT = -5431
110895
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17688575
42 X = -5391477
79
Y = 10847438
97 feet Y = 3306299
40 meter
Z = 7546027
74 Z = 2300029
26
XDOT = -13462
208744 XDOT = -4103
281225
YDOT = -9520
555236 feet/sec YDOT = -2901
865236 meter/sec
ZDOT = -17818
726050 ZDOT = -5431
147700
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 10135
53631591
00016717 00000-0 10270-3 0 9101
2 25544 51
6464 38
1383 0010298 316
5090 43
5260 15
74091106 18337
Satellite: ISS
Catalog Number: 25544
Epoch time: 10135
53631591 = yrday
fracday
Element set: 910
Inclination: 51
6464 deg
RA of node: 38
1383 deg
Eccentricity:
0010298
Arg of perigee: 316
5090 deg
Mean anomaly: 43
5260 deg
Mean motion: 15
74091106 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1833
Checksum: 282
Coasting Arc #12 (Orbit 1848)
---------------------------------------
Vector Time (GMT): 2010/136/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 412800
05 A = 6721842
29 meter
Y = 4718541
96 meter E =
0004357
Z = 4767959
93 I = 51
81684
XDOT = -6958
375843 Wp = 356
36709
YDOT = -2023
097478 meter/sec RA = 32
65936 deg
ZDOT = 2608
959081 TA = 68
12813
MA = 68
08181
Ha = 190
743 n
mi
Hp = 184
723
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1354330
88 X = 336843
62
Y = 15480780
70 feet Y = 4722732
77 meter
Z = 15642913
15 Z = 4769781
50
XDOT = -22829
317071 XDOT = -6947
910038
YDOT = -6637
458918 feet/sec YDOT = -2100
852025 meter/sec
ZDOT = 8559
577038 ZDOT = 2575
180020
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13169511
07 X = 4014066
98
Y = 8235645
57 feet Y = 2510224
77 meter
Z = 15650164
06 Z = 4770170
01
XDOT = -18389
458287 XDOT = -5605
106886
YDOT = 13423
618461 feet/sec YDOT = 4091
518907 meter/sec
ZDOT = 8425
038576 ZDOT = 2567
951758
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 10136
55206490
00016717 00000-0 10270-3 0 9111
2 25544 51
6468 32
9211 0010387 320
4447 39
5957 15
74149716 18498
Satellite: ISS
Catalog Number: 25544
Epoch time: 10136
55206490 = yrday
fracday
Element set: 911
Inclination: 51
6468 deg
RA of node: 32
9211 deg
Eccentricity:
0010387
Arg of perigee: 320
4447 deg
Mean anomaly: 39
5957 deg
Mean motion: 15
74149716 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1849
Checksum: 313
Coasting Arc #13 (Orbit 1863)
---------------------------------------
Vector Time (GMT): 2010/137/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6216579
71 A = 6729524
49 meter
Y = 1271010
01 meter E =
0013209
Z = -2215831
71 I = 51
81721
XDOT = 868
087163 Wp = 350
63051
YDOT = 5327
622870 meter/sec RA = 27
49543 deg
ZDOT = 5499
592722 TA = 344
57087
MA = 344
61110
Ha = 190
908 n
mi
Hp = 184
431
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20395602
71 X = 6212669
19
Y = 4169980
35 feet Y = 1340505
95 meter
Z = -7269789
09 Z = -2185640
69
XDOT = 2848
054998 XDOT = 781
732003
YDOT = 17479
077659 feet/sec YDOT = 5336
846738 meter/sec
ZDOT = 18043
283210 ZDOT = 5503
600899
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15311473
34 X = 4666937
07
Y = -14165524
59 feet Y = -4317651
90 meter
Z = -7149536
81 Z = -2179178
82
XDOT = 14762
471753 XDOT = 4499
601390
YDOT = 6855
775155 feet/sec YDOT = 2089
640267 meter/sec
ZDOT = 18059
239270 ZDOT = 5504
456129
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 10137
50430360
00016717 00000-0 10270-3 0 9123
2 25544 51
6471 28
0301 0010502 323
6531 36
3918 15
74204889 18648
Satellite: ISS
Catalog Number: 25544
Epoch time: 10137
50430360 = yrday
fracday
Element set: 912
Inclination: 51
6471 deg
RA of node: 28
0301 deg
Eccentricity:
0010502
Arg of perigee: 323
6531 deg
Mean anomaly: 36
3918 deg
Mean motion: 15
74204889 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1864
Checksum: 275
Coasting Arc #14 (Orbit 1879)
---------------------------------------
Vector Time (GMT): 2010/138/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1062458
95 A = 6721273
37 meter
Y = -4557979
34 meter E =
0013776
Z = -4833643
88 I = 51
76255
XDOT = 7240
009688 Wp = 24
24279
YDOT = 907
716074 meter/sec RA = 22
40778 deg
ZDOT = -2437
474315 TA = 221
91435
MA = 222
01989
Ha = 190
923 n
mi
Hp = 184
099
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3485757
72 X = -987930
82
Y = -14954000
44 feet Y = -4569443
07 meter
Z = -15858411
68 Z = -4838624
86
XDOT = 23753
312625 XDOT = 7241
162185
YDOT = 2978
071110 feet/sec YDOT = 988
684921 meter/sec
ZDOT = -7996
962975 ZDOT = -2402
299343
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14224885
48 X = -4335745
10
Y = -5726769
13 feet Y = -1745519
23 meter
Z = -15878243
15 Z = -4839688
51
XDOT = 15582
457926 XDOT = 4749
533176
YDOT = -16831
898832 feet/sec YDOT = -5130
362764 meter/sec
ZDOT = -7856
854266 ZDOT = -2394
769180
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 10138
51999716
00016717 00000-0 10270-3 0 9131
2 25544 51
6469 22
8129 0010628 327
2919 32
7585 15
74257897 18809
Satellite: ISS
Catalog Number: 25544
Epoch time: 10138
51999716 = yrday
fracday
Element set: 913
Inclination: 51
6469 deg
RA of node: 22
8129 deg
Eccentricity:
0010628
Arg of perigee: 327
2919 deg
Mean anomaly: 32
7585 deg
Mean motion: 15
74257897 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1880
Checksum: 344
Coasting Arc #15 (Orbit 1895)
---------------------------------------
Vector Time (GMT): 2010/139/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6410385
37 A = 6729705
66 meter
Y = -318850
49 meter E =
0008946
Z = 2024836
05 I = 51
76238
XDOT = -1517
728753 Wp = 63
37259
YDOT = -5076
069722 meter/sec RA = 17
24176 deg
ZDOT = -5581
446919 TA = 94
10511
MA = 94
00286
Ha = 191
065 n
mi
Hp = 183
965
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21031448
06 X = -6416179
78
Y = -1046097
40 feet Y = -390567
84 meter
Z = 6643162
88 Z = 1993680
27
XDOT = -4979
425042 XDOT = -1433
740758
YDOT = -16653
772053 feet/sec YDOT = -5092
571687 meter/sec
ZDOT = -18311
833725 ZDOT = -5588
616569
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12567926
85 X = -3830704
11
Y = 16943931
10 feet Y = 5164510
20 meter
Z = 6519060
81 Z = 1987009
74
XDOT = -15320
737342 XDOT = -4669
760742
YDOT = -4278
248298 feet/sec YDOT = -1304
010081 meter/sec
ZDOT = -18340
382566 ZDOT = -5590
148606
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 10139
53566399
00016717 00000-0 10270-3 0 9142
2 25544 51
6468 17
5953 0010497 331
2061 28
8522 15
74264973 18968
Satellite: ISS
Catalog Number: 25544
Epoch time: 10139
53566399 = yrday
fracday
Element set: 914
Inclination: 51
6468 deg
RA of node: 17
5953 deg
Eccentricity:
0010497
Arg of perigee: 331
2061 deg
Mean anomaly: 28
8522 deg
Mean motion: 15
74264973 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1896
Checksum: 334
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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