Date:
February 13th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 23142 41 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
046/05:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 188
6
000/00:00:00
000 0
0 0
0 181
0
046/05:56:31
000 -0
1 0
2 0
3
N/A 0
2 0
1 188
6
000/00:04:58
000 -0
2 0
2 181
3
046/07:41:31
000 -0
2 0
4 0
4
N/A 0
4 -0
1 188
6
000/00:04:58
000 -0
0 0
1 181
6
046/07:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 188
6
000/00:00:00
000 0
0 0
0 181
6
049/06:36:31
000 0
3 0
7 0
8
N/A -0
7 0
0 189
2
000/00:04:58
000 0
1 -0
3 180
8
049/07:03:31
000 0
9 1
8 2
0
N/A 1
6 -0
8 189
3
000/00:24:58
000 -0
7 0
1 182
0
049/07:27:01
000 -0
3 0
3 0
4
N/A 0
2 0
2 189
4
000/00:05:58
000 -0
0 -0
1 182
1
Coasting Arc #1 (Orbit 384)
---------------------------------------
Vector Time (GMT): 2010/043/13:54:18
929
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5142457
34 A = 6726087
21 meter
Y = -4159304
37 meter E =
0004416
Z = 1222893
03 I = 51
83366
XDOT = 3891
370733 Wp = 76
74948
YDOT = 3074
601146 meter/sec RA = 149
38945 deg
ZDOT = -5887
791139 TA = 89
87983
MA = 89
82922
Ha = 188
112 n
mi
Hp = 182
047
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16871579
18 X = 5182644
81
Y = -13646011
71 feet Y = -4101573
65 meter
Z = 4012116
24 Z = 1247971
94
XDOT = 12766
964347 XDOT = 3885
301704
YDOT = 10087
274102 feet/sec YDOT = 3118
082781 meter/sec
ZDOT = -19316
900063 ZDOT = -5868
902225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18903370
51 X = 5761747
33
Y = -10616925
64 feet Y = -3236038
94 meter
Z = 4111492
36 Z = 1253182
87
XDOT = 10225
419141 XDOT = 3116
707754
YDOT = 10731
564823 feet/sec YDOT = 3270
980958 meter/sec
ZDOT = -19241
801506 ZDOT = -5864
901099
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 10043
61352491
00016717 00000-0 10270-3 0 9006
2 25544 51
6459 150
2251 0011255 317
4630 42
5661 15
75900006 3859
Satellite: ISS
Catalog Number: 25544
Epoch time: 10043
61352491 = yrday
fracday
Element set: 900
Inclination: 51
6459 deg
RA of node: 150
2251 deg
Eccentricity:
0011255
Arg of perigee: 317
4630 deg
Mean anomaly: 42
5661 deg
Mean motion: 15
75900006 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 385
Checksum: 269
Coasting Arc #2 (Orbit 400)
---------------------------------------
Vector Time (GMT): 2010/044/13:54:18
929
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2999465
40 A = 6714678
96 meter
Y = -2926965
43 meter E =
0008685
Z = 5249352
06 I = 51
82160
XDOT = 5912
621579 Wp = 329
07466
YDOT = -4891
462100 meter/sec RA = 144
27023 deg
ZDOT = 658
822095 TA = 114
72342
MA = 114
63300
Ha = 188
275 n
mi
Hp = 181
785
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9840765
75 X = -2992012
25
Y = -9602904
94 feet Y = -2960465
41 meter
Z = 17222283
68 Z = 5234799
29
XDOT = 19398
364762 XDOT = 5963
678999
YDOT = -16048
104004 feet/sec YDOT = -4825
058164 meter/sec
ZDOT = 2161
489812 ZDOT = 687
668870
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8374915
73 X = -2552674
31
Y = -10995807
50 feet Y = -3351522
13 meter
Z = 17164396
67 Z = 5231708
10
XDOT = 20787
884827 XDOT = 6336
147295
YDOT = -12320
467574 feet/sec YDOT = -3755
278517 meter/sec
ZDOT = 2275
800258 ZDOT = 693
663919
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 10044
62812066
00016717 00000-0 10270-3 0 9018
2 25544 51
6465 145
0001 0011367 320
9537 39
0806 15
75956628 4012
Satellite: ISS
Catalog Number: 25544
Epoch time: 10044
62812066 = yrday
fracday
Element set: 901
Inclination: 51
6465 deg
RA of node: 145
0001 deg
Eccentricity:
0011367
Arg of perigee: 320
9537 deg
Mean anomaly: 39
0806 deg
Mean motion: 15
75956628 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 401
Checksum: 284
Coasting Arc #3 (Orbit 416)
---------------------------------------
Vector Time (GMT): 2010/045/13:54:18
929
Vector Time (MET): N/A
Weight (LBS) : 764580
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5120433
98 A = 6726708
46 meter
Y = 4342532
39 meter E =
0018387
Z = 84959
15 I = 51
88510
XDOT = -3019
163695 Wp = 8
06503
YDOT = -3681
415992 meter/sec RA = 139
13061 deg
ZDOT = 6066
700877 TA = 352
85646
MA = 352
88262
Ha = 188
593 n
mi
Hp = 181
427
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16799324
07 X = -5169025
09
Y = 14247153
51 feet Y = 4285000
98 meter
Z = 278737
36 Z = 59966
57
XDOT = -9905
392701 XDOT = -3007
243157
YDOT = -12078
136457 feet/sec YDOT = -3715
111147 meter/sec
ZDOT = 19903
874267 ZDOT = 6052
063319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18561075
73 X = -5657415
88
Y = 11862990
49 feet Y = 3615839
50 meter
Z = 179697
75 Z = 54771
87
XDOT = -7445
159438 XDOT = -2269
284597
YDOT = -11960
187399 feet/sec YDOT = -3645
465119 meter/sec
ZDOT = 19845
615649 ZDOT = 6048
943650
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 10045
64269586
00016717 00000-0 10270-3 0 9025
2 25544 51
6459 139
7757 0011526 326
4931 33
5503 15
75927042 4177
Satellite: ISS
Catalog Number: 25544
Epoch time: 10045
64269586 = yrday
fracday
Element set: 902
Inclination: 51
6459 deg
RA of node: 139
7757 deg
Eccentricity:
0011526
Arg of perigee: 326
4931 deg
Mean anomaly: 33
5503 deg
Mean motion: 15
75927042 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 417
Checksum: 316
Coasting Arc #4 (Orbit 426)
---------------------------------------
Vector Time (GMT): 2010/046/05:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 1010385
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4166803
03 A = 6725866
78 meter
Y = -5181503
27 meter E =
0005873
Z = 1019368
34 I = 51
89593
XDOT = 4318
530681 Wp = 65
75570
YDOT = 2297
957412 meter/sec RA = 135
71040 deg
ZDOT = -5942
872326 TA = 103
14093
MA = 103
07538
Ha = 188
586 n
mi
Hp = 181
028
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13670613
63 X = 4219482
06
Y = -16999682
64 feet Y = -5134613
01 meter
Z = 3344384
32 Z = 1039738
38
XDOT = 14168
407745 XDOT = 4321
382195
YDOT = 7539
230355 feet/sec YDOT = 2346
265399 meter/sec
ZDOT = -19497
612619 ZDOT = -5921
886658
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4940107
19 X = 1505744
67
Y = 21234976
30 feet Y = 6472420
78 meter
Z = 3425042
46 Z = 1043952
94
XDOT = -13201
491561 XDOT = -4023
814628
YDOT = 6217
575085 feet/sec YDOT = 1895
116886 meter/sec
ZDOT = -19414
206446 ZDOT = -5917
450125
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 10046
27678718
00016717 00000-0 10270-3 0 9037
2 25544 51
6434 136
5078 0011807 328
9224 31
1241 15
76050887 4274
Satellite: ISS
Catalog Number: 25544
Epoch time: 10046
27678718 = yrday
fracday
Element set: 903
Inclination: 51
6434 deg
RA of node: 136
5078 deg
Eccentricity:
0011807
Arg of perigee: 328
9224 deg
Mean anomaly: 31
1241 deg
Mean motion: 15
76050887 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 427
Checksum: 305
Coasting Arc #5 (Orbit 426)
---------------------------------------
Vector Time (GMT): 2010/046/05:59:00
000
Vector Time (MET): N/A
Weight (LBS) : 1010305
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5581642
45 A = 6724538
62 meter
Y = -3058875
32 meter E =
0005418
Z = -2177907
16 I = 51
89064
XDOT = 754
056179 Wp = 340
41725
YDOT = 5311
278791 meter/sec RA = 135
70764 deg
ZDOT = -5518
241997 TA = 223
87912
MA = 223
92216
Ha = 188
595 n
mi
Hp = 181
308
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18312475
21 X = 5626012
10
Y = -10035680
18 feet Y = -2996210
12 meter
Z = -7145364
68 Z = -2150684
31
XDOT = 2473
937596 XDOT = 721
414395
YDOT = 17425
455352 feet/sec YDOT = 5319
528279 meter/sec
ZDOT = -18104
468493 ZDOT = -5514
658467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2626726
97 X = -800626
38
Y = 20753143
40 feet Y = 6325558
11 meter
Z = -7037414
73 Z = -2145004
01
XDOT = -14117
077533 XDOT = -4302
885232
YDOT = -7931
235630 feet/sec YDOT = -2417
440620 meter/sec
ZDOT = -18090
026067 ZDOT = -5513
839945
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 10046
27678897
00016717 00000-0 10270-3 0 9046
2 25544 51
6433 136
5078 0011514 328
5446 31
5029 15
75980732 4278
Satellite: ISS
Catalog Number: 25544
Epoch time: 10046
27678897 = yrday
fracday
Element set: 904
Inclination: 51
6433 deg
RA of node: 136
5078 deg
Eccentricity:
0011514
Arg of perigee: 328
5446 deg
Mean anomaly: 31
5029 deg
Mean motion: 15
75980732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 427
Checksum: 318
Coasting Arc #6 (Orbit 427)
---------------------------------------
Vector Time (GMT): 2010/046/07:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 1010226
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3835964
99 A = 6715214
64 meter
Y = 1921406
34 meter E =
0014174
Z = -5174933
96 I = 51
86092
XDOT = -4676
724206 Wp = 34
40635
YDOT = 5986
826189 meter/sec RA = 135
32346 deg
ZDOT = -1233
994371 TA = 223
77520
MA = 223
88765
Ha = 188
592 n
mi
Hp = 181
585
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12585186
96 X = 3839332
63
Y = 6303826
56 feet Y = 1964320
91 meter
Z = -16978129
78 Z = -5156291
25
XDOT = -15343
583353 XDOT = -4737
328009
YDOT = 19641
818204 feet/sec YDOT = 5934
189360 meter/sec
ZDOT = -4048
537962 ZDOT = -1256
860845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8322788
77 X = -2536786
02
Y = 11461529
62 feet Y = 3493474
23 meter
Z = -16904040
25 Z = -5152351
47
XDOT = -15988
540023 XDOT = -4873
306999
YDOT = -17762
286484 feet/sec YDOT = -5413
944920 meter/sec
ZDOT = -4139
074655 ZDOT = -1261
589955
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 10046
34020130
00016717 00000-0 10270-3 0 9056
2 25544 51
6442 136
1802 0011147 326
9879 33
0588 15
75902100 4284
Satellite: ISS
Catalog Number: 25544
Epoch time: 10046
34020130 = yrday
fracday
Element set: 905
Inclination: 51
6442 deg
RA of node: 136
1802 deg
Eccentricity:
0011147
Arg of perigee: 326
9879 deg
Mean anomaly: 33
0588 deg
Mean motion: 15
75902100 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 428
Checksum: 274
Coasting Arc #7 (Orbit 443)
---------------------------------------
Vector Time (GMT): 2010/047/07:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4513207
79 A = 6726598
38 meter
Y = -4980006
91 meter E =
0002732
Z = -300793
52 I = 51
91969
XDOT = 3340
455819 Wp = 61
88830
YDOT = 3390
262790 meter/sec RA = 130
17527 deg
ZDOT = -6048
802826 TA = 121
36791
MA = 121
34117
Ha = 188
685 n
mi
Hp = 181
209
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14807112
17 X = 4570020
85
Y = -16338605
33 feet Y = -4929219
90 meter
Z = -986855
37 Z = -278730
51
XDOT = 10959
500720 XDOT = 3331
680380
YDOT = 11122
909415 feet/sec YDOT = 3427
568277 meter/sec
ZDOT = -19845
153628 ZDOT = -6032
596791
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14096178
70 X = 4296515
27
Y = 16960636
60 feet Y = 5169602
04 meter
Z = -899461
49 Z = -274155
86
XDOT = -11331
058016 XDOT = -3453
706483
YDOT = 8376
023336 feet/sec YDOT = 2553
011913 meter/sec
ZDOT = -19780
676320 ZDOT = -6029
150142
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 10047
35480652
00016717 00000-0 10270-3 0 9068
2 25544 51
6434 130
9542 0011326 330
6971 29
3556 15
75948081 4441
Satellite: ISS
Catalog Number: 25544
Epoch time: 10047
35480652 = yrday
fracday
Element set: 906
Inclination: 51
6434 deg
RA of node: 130
9542 deg
Eccentricity:
0011326
Arg of perigee: 330
6971 deg
Mean anomaly: 29
3556 deg
Mean motion: 15
75948081 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 444
Checksum: 303
Coasting Arc #8 (Orbit 459)
---------------------------------------
Vector Time (GMT): 2010/048/07:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2631222
30 A = 6715000
39 meter
Y = -3345599
33 meter E =
0012316
Z = 5196981
88 I = 51
89955
XDOT = 5054
818308 Wp = 352
78488
YDOT = -5705
259865 meter/sec RA = 125
03225 deg
ZDOT = -1101
881739 TA = 107
75749
MA = 107
62305
Ha = 188
907 n
mi
Hp = 181
010
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8632619
09 X = -2618861
21
Y = -10976375
74 feet Y = -3374953
74 meter
Z = 17050465
49 Z = 5184229
89
XDOT = 16584
049568 XDOT = 5123
592501
YDOT = -18718
044176 feet/sec YDOT = -5648
349427 meter/sec
ZDOT = -3615
097568 ZDOT = -1077
158415
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11969715
73 X = 3648369
36
Y = -7311449
04 feet Y = -2228529
67 meter
Z = 16999703
78 Z = 5181509
71
XDOT = 15992
812594 XDOT = 4874
609279
YDOT = 17915
092912 feet/sec YDOT = 5460
520319 meter/sec
ZDOT = -3517
162746 ZDOT = -1072
031205
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 10048
36939010
00016717 00000-0 10270-3 0 9078
2 25544 51
6440 125
7292 0011180 335
1466 24
9159 15
75924978 4606
Satellite: ISS
Catalog Number: 25544
Epoch time: 10048
36939010 = yrday
fracday
Element set: 907
Inclination: 51
6440 deg
RA of node: 125
7292 deg
Eccentricity:
0011180
Arg of perigee: 335
1466 deg
Mean anomaly: 24
9159 deg
Mean motion: 15
75924978 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 460
Checksum: 308
Coasting Arc #9 (Orbit 474)
---------------------------------------
Vector Time (GMT): 2010/049/06:39:00
000
Vector Time (MET): N/A
Weight (LBS) : 1010305
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1924130
15 A = 6716802
76 meter
Y = -4242656
44 meter E =
0014248
Z = 4841800
29 I = 51
91906
XDOT = 5188
798634 Wp = 10
15382
YDOT = -5144
827810 meter/sec RA = 120
13080 deg
ZDOT = -2431
353200 TA = 103
57252
MA = 103
41377
Ha = 189
248 n
mi
Hp = 180
793
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6312762
96 X = -1900065
28
Y = -13919476
49 feet Y = -4264038
33 meter
Z = 15885171
54 Z = 4832511
72
XDOT = 17023
617566 XDOT = 5257
754283
YDOT = -16879
356333 feet/sec YDOT = -5086
418193 meter/sec
ZDOT = -7976
880576 ZDOT = -2405
978535
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15314793
25 X = 4667948
98
Y = -485187
40 feet Y = -147885
12 meter
Z = 15848128
53 Z = 4830509
57
XDOT = 8871
883129 XDOT = 2704
149978
YDOT = 21176
072990 feet/sec YDOT = 6454
467047 meter/sec
ZDOT = -7876
328541 ZDOT = -2400
704939
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 10049
32054241
00016717 00000-0 10270-3 0 9080
2 25544 51
6427 120
8305 0011015 341
6488 18
4277 15
75832015 4750
Satellite: ISS
Catalog Number: 25544
Epoch time: 10049
32054241 = yrday
fracday
Element set: 908
Inclination: 51
6427 deg
RA of node: 120
8305 deg
Eccentricity:
0011015
Arg of perigee: 341
6488 deg
Mean anomaly: 18
4277 deg
Mean motion: 15
75832015 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 475
Checksum: 284
Coasting Arc #10 (Orbit 474)
---------------------------------------
Vector Time (GMT): 2010/049/07:16:00
000
Vector Time (MET): N/A
Weight (LBS) : 1009908
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4151662
50 A = 6716353
31 meter
Y = 962764
40 meter E =
0015032
Z = -5201271
72 I = 51
91428
XDOT = -3028
217500 Wp = 41
46687
YDOT = 6985
268811 meter/sec RA = 120
02775 deg
ZDOT = -1114
951224 TA = 217
87175
MA = 217
97759
Ha = 189
284 n
mi
Hp = 181
999
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13620939
95 X = 4165854
63
Y = 3158675
84 feet Y = 1009269
76 meter
Z = -17064539
77 Z = -5181068
81
XDOT = -9935
096785 XDOT = -3100
686794
YDOT = 22917
548591 feet/sec YDOT = 6951
000215 meter/sec
ZDOT = -3657
976457 ZDOT = -1129
838585
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6301245
93 X = -1920619
76
Y = 12591029
90 feet Y = 3837745
91 meter
Z = -16984287
49 Z = -5176810
83
XDOT = -19019
526539 XDOT = -5797
151689
YDOT = -14572
977172 feet/sec YDOT = -4441
843442 meter/sec
ZDOT = -3716
818408 ZDOT = -1132
886251
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 10049
32054663
00016717 00000-0 10270-3 0 9099
2 25544 51
6426 120
8308 0010085 334
7487 25
3183 15
75466408 4752
Satellite: ISS
Catalog Number: 25544
Epoch time: 10049
32054663 = yrday
fracday
Element set: 909
Inclination: 51
6426 deg
RA of node: 120
8308 deg
Eccentricity:
0010085
Arg of perigee: 334
7487 deg
Mean anomaly: 25
3183 deg
Mean motion: 15
75466408 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 475
Checksum: 305
Coasting Arc #11 (Orbit 474)
---------------------------------------
Vector Time (GMT): 2010/049/07:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 208503
84 A = 6722051
74 meter
Y = 5556495
61 meter E =
0007828
Z = -3771951
97 I = 51
93304
XDOT = -5627
846234 Wp = 9
87405
YDOT = 3093
743900 meter/sec RA = 119
94233 deg
ZDOT = 4255
162185 TA = 304
64198
MA = 304
71575
Ha = 189
406 n
mi
Hp = 182
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 684067
71 X = 164677
84
Y = 18229972
47 feet Y = 5558581
93 meter
Z = -12375170
51 Z = -3771045
89
XDOT = -18464
062448 XDOT = -5682
693284
YDOT = 10150
078413 feet/sec YDOT = 3030
503595 meter/sec
ZDOT = 13960
505857 ZDOT = 4227
689058
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18079304
17 X = -5510571
91
Y = -2456198
04 feet Y = -748649
16 meter
Z = -12371359
75 Z = -3770790
45
XDOT = -6915
068472 XDOT = -2107
712870
YDOT = -18721
671907 feet/sec YDOT = -5706
365597 meter/sec
ZDOT = 13851
542823 ZDOT = 4221
950253
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 10049
32054673
00016717 00000-0 10270-3 0 9102
2 25544 51
6427 120
8306 0010299 333
2638 26
7993 15
75378665 4751
Satellite: ISS
Catalog Number: 25544
Epoch time: 10049
32054673 = yrday
fracday
Element set: 910
Inclination: 51
6427 deg
RA of node: 120
8306 deg
Eccentricity:
0010299
Arg of perigee: 333
2638 deg
Mean anomaly: 26
7993 deg
Mean motion: 15
75378665 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 475
Checksum: 317
Coasting Arc #12 (Orbit 490)
---------------------------------------
Vector Time (GMT): 2010/050/07:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4700124
93 A = 6721116
49 meter
Y = -2605755
18 meter E =
0012130
Z = -4047315
63 I = 51
94411
XDOT = 300
387697 Wp = 13
67040
YDOT = 6621
806350 meter/sec RA = 114
86874 deg
ZDOT = -3905
273479 TA = 216
14873
MA = 216
23078
Ha = 189
481 n
mi
Hp = 181
914
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15420357
38 X = 4748574
55
Y = -8549065
55 feet Y = -2552924
91 meter
Z = -13278594
57 Z = -4024364
84
XDOT = 985
523941 XDOT = 245
290073
YDOT = 21725
086451 feet/sec YDOT = 6624
857189 meter/sec
ZDOT = -12812
577032 ZDOT = -3903
948395
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5982419
81 X = 1823441
56
Y = 16658148
11 feet Y = 5077403
55 meter
Z = -13187561
27 Z = -4019568
67
XDOT = -20403
219064 XDOT = -6218
901171
YDOT = -2835
396199 feet/sec YDOT = -864
228761 meter/sec
ZDOT = -12807
070799 ZDOT = -3903
595180
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 10050
33547193
00016717 00000-0 10270-3 0 9110
2 25544 51
6427 115
6077 0010315 337
0970 22
9732 15
75419868 4916
Satellite: ISS
Catalog Number: 25544
Epoch time: 10050
33547193 = yrday
fracday
Element set: 911
Inclination: 51
6427 deg
RA of node: 115
6077 deg
Eccentricity:
0010315
Arg of perigee: 337
0970 deg
Mean anomaly: 22
9732 deg
Mean motion: 15
75419868 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 491
Checksum: 300
Coasting Arc #13 (Orbit 506)
---------------------------------------
Vector Time (GMT): 2010/051/07:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -349745
39 A = 6724128
38 meter
Y = -6004535
01 meter E =
0012837
Z = 3007867
51 I = 51
96643
XDOT = 5148
591205 Wp = 50
32109
YDOT = -2808
943403 meter/sec RA = 109
69449 deg
ZDOT = -4986
754880 TA = 95
07782
MA = 94
93129
Ha = 189
572 n
mi
Hp = 181
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1147458
63 X = -297187
17
Y = -19699918
01 feet Y = -6008152
09 meter
Z = 9868331
71 Z = 3006296
34
XDOT = 16891
703427 XDOT = 5203
843191
YDOT = -9215
693581 feet/sec YDOT = -2751
060056 meter/sec
ZDOT = -16360
744356 ZDOT = -4961
608940
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19671820
37 X = 5995970
85
Y = 1596933
35 feet Y = 486745
29 meter
Z = 9861880
60 Z = 3005901
21
XDOT = 6833
549223 XDOT = 2082
865803
YDOT = 16687
133596 feet/sec YDOT = 5086
238320 meter/sec
ZDOT = -16260
992681 ZDOT = -4956
350569
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 10051
35037396
00016717 00000-0 10270-3 0 9123
2 25544 51
6429 110
3845 0010263 341
2887 18
7898 15
75448289 5072
Satellite: ISS
Catalog Number: 25544
Epoch time: 10051
35037396 = yrday
fracday
Element set: 912
Inclination: 51
6429 deg
RA of node: 110
3845 deg
Eccentricity:
0010263
Arg of perigee: 341
2887 deg
Mean anomaly: 18
7898 deg
Mean motion: 15
75448289 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 507
Checksum: 319
Coasting Arc #14 (Orbit 522)
---------------------------------------
Vector Time (GMT): 2010/052/07:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4321531
69 A = 6718616
16 meter
Y = 2252118
49 meter E =
0008021
Z = 4617988
16 I = 51
95868
XDOT = -541
232779 Wp = 37
19459
YDOT = -7097
216501 meter/sec RA = 104
61685 deg
ZDOT = 2958
315061 TA = 23
65965
MA = 23
62278
Ha = 189
739 n
mi
Hp = 181
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14178253
59 X = -4368827
24
Y = 7388840
19 feet Y = 2203528
20 meter
Z = 15150879
78 Z = 4596879
43
XDOT = -1775
698093 XDOT = -476
201042
YDOT = -23284
831039 feet/sec YDOT = -7102
905218 meter/sec
ZDOT = 9705
758075 ZDOT = 2955
843876
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5554119
49 X = -1692895
62
Y = -15076482
46 feet Y = -4595311
85 meter
Z = 15067130
63 Z = 4592461
42
XDOT = 22232
119497 XDOT = 6776
350023
YDOT = 1487
577769 feet/sec YDOT = 453
413704 meter/sec
ZDOT = 9695
705725 ZDOT = 2955
251105
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 10052
36525045
00016717 00000-0 10270-3 0 9139
2 25544 51
6440 105
1614 0010348 345
0212 15
0644 15
75529714 5239
Satellite: ISS
Catalog Number: 25544
Epoch time: 10052
36525045 = yrday
fracday
Element set: 913
Inclination: 51
6440 deg
RA of node: 105
1614 deg
Eccentricity:
0010348
Arg of perigee: 345
0212 deg
Mean anomaly: 15
0644 deg
Mean motion: 15
75529714 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 523
Checksum: 262
Coasting Arc #15 (Orbit 537)
---------------------------------------
Vector Time (GMT): 2010/053/07:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 626815
18 A = 6725918
98 meter
Y = 6341726
27 meter E =
0015307
Z = -2123739
41 I = 51
98992
XDOT = -4797
373369 Wp = 8
42283
YDOT = 2331
143015 meter/sec RA = 99
45290 deg
ZDOT = 5564
921959 TA = 327
91932
MA = 328
01239
Ha = 189
892 n
mi
Hp = 180
897
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2056480
26 X = 566170
91
Y = 20806188
54 feet Y = 6348396
60 meter
Z = -6967648
98 Z = -2120841
70
XDOT = -15739
413939 XDOT = -4850
117135
YDOT = 7648
107003 feet/sec YDOT = 2277
201053 meter/sec
ZDOT = 18257
617975 ZDOT = 5541
488477
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20910923
39 X = -6373649
45
Y = -151462
17 feet Y = -46165
67 meter
Z = -6955937
54 Z = -2120169
76
XDOT = -5911
728707 XDOT = -1801
894910
YDOT = -15051
987452 feet/sec YDOT = -4587
845776 meter/sec
ZDOT = 18164
628856 ZDOT = 5536
578875
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 10053
31667819
00016717 00000-0 10270-3 0 9142
2 25544 51
6443 100
2654 0010542 349
1547 10
9388 15
75510303 5383
Satellite: ISS
Catalog Number: 25544
Epoch time: 10053
31667819 = yrday
fracday
Element set: 914
Inclination: 51
6443 deg
RA of node: 100
2654 deg
Eccentricity:
0010542
Arg of perigee: 349
1547 deg
Mean anomaly: 10
9388 deg
Mean motion: 15
75510303 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 538
Checksum: 289
Coasting Arc #16 (Orbit 553)
---------------------------------------
Vector Time (GMT): 2010/054/07:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4090730
24 A = 6716800
30 meter
Y = -1756685
25 meter E =
0017803
Z = -5043027
96 I = 51
96372
XDOT = 887
662797 Wp = 40
47406
YDOT = 7412
488006 meter/sec RA = 94
36425 deg
ZDOT = -1852
415950 TA = 211
66796
MA = 211
77519
Ha = 189
902 n
mi
Hp = 180
768
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13421030
97 X = 4134567
50
Y = -5763403
04 feet Y = -1710695
13 meter
Z = -16545367
34 Z = -5023049
05
XDOT = 2912
279517 XDOT = 813
707624
YDOT = 24319
186371 feet/sec YDOT = 7422
000885 meter/sec
ZDOT = -6077
480150 ZDOT = -1848
283335
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4518377
52 X = 1377201
47
Y = 13983664
03 feet Y = 4262220
80 meter
Z = -16466070
33 Z = -5018858
24
XDOT = -23466
247016 XDOT = -7152
512091
YDOT = 408
321621 feet/sec YDOT = 124
456430 meter/sec
ZDOT = -6060
838495 ZDOT = -1847
343573
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 10054
33151031
00016717 00000-0 10270-3 0 9150
2 25544 51
6447 95
0427 0010452 352
7370 7
3641 15
75559221 5542
Satellite: ISS
Catalog Number: 25544
Epoch time: 10054
33151031 = yrday
fracday
Element set: 915
Inclination: 51
6447 deg
RA of node: 95
0427 deg
Eccentricity:
0010452
Arg of perigee: 352
7370 deg
Mean anomaly: 7
3641 deg
Mean motion: 15
75559221 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 554
Checksum: 276
Coasting Arc #17 (Orbit 569)
---------------------------------------
Vector Time (GMT): 2010/055/07:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -931943
32 A = 6727124
74 meter
Y = -6574873
26 meter E =
0011371
Z = 1077524
34 I = 51
99980
XDOT = 4616
912091 Wp = 75
79714
YDOT = -1636
423438 meter/sec RA = 89
21572 deg
ZDOT = -5937
451003 TA = 92
47537
MA = 92
34519
Ha = 189
954 n
mi
Hp = 180
379
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3057556
81 X = -863586
96
Y = -21571106
50 feet Y = -6584912
61 meter
Z = 3535184
84 Z = 1073163
04
XDOT = 15147
349380 XDOT = 4663
710187
YDOT = -5368
843299 feet/sec YDOT = -1584
532682 meter/sec
ZDOT = -19479
826124 ZDOT = -5914
908858
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21738544
84 X = 6625908
47
Y = -1490140
69 feet Y = -454194
88 meter
Z = 3517665
44 Z = 1072184
43
XDOT = 4128
454146 XDOT = 1258
352824
YDOT = 14028
641013 feet/sec YDOT = 4275
929781 meter/sec
ZDOT = -19390
335612 ZDOT = -5910
174295
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 10055
34631887
00016717 00000-0 10270-3 0 9165
2 25544 51
6445 89
8196 0010404 357
3701 2
7407 15
75599448 5702
Satellite: ISS
Catalog Number: 25544
Epoch time: 10055
34631887 = yrday
fracday
Element set: 916
Inclination: 51
6445 deg
RA of node: 89
8196 deg
Eccentricity:
0010404
Arg of perigee: 357
3701 deg
Mean anomaly: 2
7407 deg
Mean motion: 15
75599448 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 570
Checksum: 321
Coasting Arc #18 (Orbit 585)
---------------------------------------
Vector Time (GMT): 2010/056/07:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4026100
54 A = 6715417
72 meter
Y = 1084880
97 meter E =
0009690
Z = 5260945
17 I = 51
96006
XDOT = -1260
077549 Wp = 16
33076
YDOT = -7579
084546 meter/sec RA = 84
10695 deg
ZDOT = 607
431696 TA = 67
97739
MA = 67
87448
Ha = 190
091 n
mi
Hp = 180
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13208991
29 X = -4063488
71
Y = 3559320
75 feet Y = 1039649
70 meter
Z = 17260318
80 Z = 5241296
06
XDOT = -4134
112692 XDOT = -1178
183944
YDOT = -24865
762947 feet/sec YDOT = -7592
717586 meter/sec
ZDOT = 1992
886142 ZDOT = 601
509356
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2807760
12 X = -855805
29
Y = -13488883
71 feet Y = -4111411
75 meter
Z = 17182296
69 Z = 5237164
03
XDOT = 24075
438931 XDOT = 7338
193786
YDOT = -2540
152389 feet/sec YDOT = -774
238448 meter/sec
ZDOT = 1969
138375 ZDOT = 600
193377
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 10056
36110138
00016717 00000-0 10270-3 0 9170
2 25544 51
6450 84
5956 0010498
9056 359
2125 15
75680996 5864
Satellite: ISS
Catalog Number: 25544
Epoch time: 10056
36110138 = yrday
fracday
Element set: 917
Inclination: 51
6450 deg
RA of node: 84
5956 deg
Eccentricity:
0010498
Arg of perigee:
9056 deg
Mean anomaly: 359
2125 deg
Mean motion: 15
75680996 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 586
Checksum: 318
Coasting Arc #19 (Orbit 601)
---------------------------------------
Vector Time (GMT): 2010/057/07:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1264168
20 A = 6727470
04 meter
Y = 6594331
95 meter E =
0021603
Z = 25373
15 I = 51
99590
XDOT = -4669
419241 Wp = 26
79954
YDOT = 864
208727 meter/sec RA = 78
97858 deg
ZDOT = 6076
921470 TA = 333
47524
MA = 333
58563
Ha = 190
221 n
mi
Hp = 179
766
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4147533
47 X = 1190212
00
Y = 21634947
34 feet Y = 6608055
12 meter
Z = 83245
23 Z = 31334
46
XDOT = -15319
616934 XDOT = -4708
255661
YDOT = 2835
330470 feet/sec YDOT = 811
775555 meter/sec
ZDOT = 19937
406398 ZDOT = 6054
143739
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21779865
38 X = -6638502
97
Y = 3302408
13 feet Y = 1006574
00 meter
Z = 107119
11 Z = 32649
90
XDOT = -1992
474029 XDOT = -607
306084
YDOT = -13946
945939 feet/sec YDOT = -4251
029122 meter/sec
ZDOT = 19846
944225 ZDOT = 6049
348600
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 10057
37586323
00016717 00000-0 10270-3 0 9186
2 25544 51
6448 79
3725 0010675 5
3289 354
7987 15
75659507 6020
Satellite: ISS
Catalog Number: 25544
Epoch time: 10057
37586323 = yrday
fracday
Element set: 918
Inclination: 51
6448 deg
RA of node: 79
3725 deg
Eccentricity:
0010675
Arg of perigee: 5
3289 deg
Mean anomaly: 354
7987 deg
Mean motion: 15
75659507 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 602
Checksum: 340
Coasting Arc #20 (Orbit 616)
---------------------------------------
Vector Time (GMT): 2010/058/07:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 764580
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4169873
53 A = 6715384
63 meter
Y = -406067
81 meter E =
0018701
Z = -5261213
81 I = 51
94780
XDOT = 1599
305578 Wp = 60
72860
YDOT = 7491
920239 meter/sec RA = 73
84772 deg
ZDOT = 700
108115 TA = 215
84539
MA = 215
97102
Ha = 190
241 n
mi
Hp = 179
630
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13680687
44 X = 4199661
61
Y = -1332243
49 feet Y = -359271
59 meter
Z = -17261200
18 Z = -5240884
79
XDOT = 5247
065544 XDOT = 1512
009832
YDOT = 24579
790812 feet/sec YDOT = 7509
316572 meter/sec
ZDOT = 2296
942634 ZDOT = 707
664801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1033286
40 X = 314945
69
Y = 13807590
94 feet Y = 4208553
72 meter
Z = -17180450
08 Z = -5236601
18
XDOT = -23680
747844 XDOT = -7217
891943
YDOT = 4623
559762 feet/sec YDOT = 1409
261016 meter/sec
ZDOT = 2327
180962 ZDOT = 709
324757
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 10058
32717690
00016717 00000-0 10270-3 0 9196
2 25544 51
6439 74
4755 0010638 8
6191 351
5154 15
75713217 6172
Satellite: ISS
Catalog Number: 25544
Epoch time: 10058
32717690 = yrday
fracday
Element set: 919
Inclination: 51
6439 deg
RA of node: 74
4755 deg
Eccentricity:
0010638
Arg of perigee: 8
6191 deg
Mean anomaly: 351
5154 deg
Mean motion: 15
75713217 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 617
Checksum: 312
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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