Date:
June 28th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 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 2477)
---------------------------------------
Vector Time (GMT): 2010/176/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5630239
71 A = 6733418
67 meter
Y = 1853373
61 meter E =
0011735
Z = -3187589
04 I = 51
60595
XDOT = -4145
778111 Wp = 28
68238
YDOT = -4350
040417 meter/sec RA = 187
00215 deg
ZDOT = 4810
823009 TA = 294
13902
MA = 294
26169
Ha = 195
485 n
mi
Hp = 185
542
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18471915
07 X = -5635061
34
Y = 6080622
09 feet Y = 1790386
62 meter
Z = -10457969
29 Z = -3214951
99
XDOT = -13601
634222 XDOT = -4120
197070
YDOT = -14271
786146 feet/sec YDOT = -4396
258945 meter/sec
ZDOT = 15783
540057 ZDOT = 4790
744117
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6954562
91 X = 2119750
78
Y = 18097635
79 feet Y = 5516159
39 meter
Z = -10567136
16 Z = -3220863
10
XDOT = -12279
649538 XDOT = -3742
837179
YDOT = 13854
979019 feet/sec YDOT = 4222
997605 meter/sec
ZDOT = 15703
370298 ZDOT = 4786
387267
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 10176
50663790
00016717 00000-0 10270-3 0 9008
2 25544 51
6447 188
0340 0009743 5
8236 354
3038 15
71981411 24785
Satellite: ISS
Catalog Number: 25544
Epoch time: 10176
50663790 = yrday
fracday
Element set: 900
Inclination: 51
6447 deg
RA of node: 188
0340 deg
Eccentricity:
0009743
Arg of perigee: 5
8236 deg
Mean anomaly: 354
3038 deg
Mean motion: 15
71981411 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2478
Checksum: 307
Coasting Arc #2 (Orbit 2493)
---------------------------------------
Vector Time (GMT): 2010/177/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4585003
09 A = 6731764
74 meter
Y = 3162198
88 meter E =
0013318
Z = -3796481
05 I = 51
62892
XDOT = -5630
871572 Wp = 34
45486
YDOT = 3129
609412 meter/sec RA = 181
93066 deg
ZDOT = -4190
033426 TA = 191
46763
MA = 191
49801
Ha = 195
653 n
mi
Hp = 185
512
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15042661
07 X = 4567744
52
Y = 10374668
24 feet Y = 3213375
39 meter
Z = -12455646
47 Z = -3774248
55
XDOT = -18473
988098 XDOT = -5645
094670
YDOT = 10267
747415 feet/sec YDOT = 3066
562976 meter/sec
ZDOT = -13746
828824 ZDOT = -4217
421905
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9369086
26 X = 2855697
49
Y = -15758774
07 feet Y = -4803274
34 meter
Z = -12366882
58 Z = -3769425
81
XDOT = 10292
709203 XDOT = 3137
217765
YDOT = 17002
456028 feet/sec YDOT = 5182
348597 meter/sec
ZDOT = -13856
099394 ZDOT = -4223
339095
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 10177
52377472
00016717 00000-0 10270-3 0 9011
2 25544 51
6433 182
8258 0009735 9
2876 350
8464 15
71987107 24949
Satellite: ISS
Catalog Number: 25544
Epoch time: 10177
52377472 = yrday
fracday
Element set: 901
Inclination: 51
6433 deg
RA of node: 182
8258 deg
Eccentricity:
0009735
Arg of perigee: 9
2876 deg
Mean anomaly: 350
8464 deg
Mean motion: 15
71987107 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2494
Checksum: 334
Coasting Arc #3 (Orbit 2509)
---------------------------------------
Vector Time (GMT): 2010/178/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4056745
65 A = 6730435
33 meter
Y = -3473280
91 meter E =
0017291
Z = 4093900
90 I = 51
65497
XDOT = 6139
634371 Wp = 45
58197
YDOT = 2664
419708 meter/sec RA = 176
75930 deg
ZDOT = -3801
674828 TA = 83
54788
MA = 83
35102
Ha = 195
655 n
mi
Hp = 185
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13309532
98 X = 4075395
80
Y = -11395278
57 feet Y = -3427812
47 meter
Z = 13431433
41 Z = 4113652
99
XDOT = 20143
157384 XDOT = 6127
851670
YDOT = 8741
534474 feet/sec YDOT = 2733
011608 meter/sec
ZDOT = -12472
686444 ZDOT = -3771
876926
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12443756
01 X = -3792856
83
Y = -12248508
34 feet Y = -3733345
34 meter
Z = 13510234
08 Z = 4117919
35
XDOT = 6156
589712 XDOT = 1876
528544
YDOT = -19959
201707 feet/sec YDOT = -6083
564680 meter/sec
ZDOT = -12353
717023 ZDOT = -3765
412949
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 10178
54089924
00016717 00000-0 10270-3 0 9027
2 25544 51
6429 177
6177 0009842 12
5555 347
5850 15
72030141 25105
Satellite: ISS
Catalog Number: 25544
Epoch time: 10178
54089924 = yrday
fracday
Element set: 902
Inclination: 51
6429 deg
RA of node: 177
6177 deg
Eccentricity:
0009842
Arg of perigee: 12
5555 deg
Mean anomaly: 347
5850 deg
Mean motion: 15
72030141 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2510
Checksum: 306
Coasting Arc #4 (Orbit 2525)
---------------------------------------
Vector Time (GMT): 2010/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5961182
68 A = 6734419
43 meter
Y = -1358940
24 meter E =
0019914
Z = 2793322
06 I = 51
69841
XDOT = 3457
995350 Wp = 54
00111
YDOT = -4598
586410 meter/sec RA = 171
69077 deg
ZDOT = 5128
629109 TA = 337
97231
MA = 338
05778
Ha = 195
807 n
mi
Hp = 185
019
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19557685
95 X = -5959112
98
Y = -4458465
35 feet Y = -1425590
66 meter
Z = 9164442
47 Z = 2764367
82
XDOT = 11345
129101 XDOT = 3484
246965
YDOT = -15087
225754 feet/sec YDOT = -4559
771164 meter/sec
ZDOT = 16826
210987 ZDOT = 5145
490780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2488107
01 X = -758375
02
Y = 19957350
11 feet Y = 6083000
31 meter
Z = 9048839
65 Z = 2758086
33
XDOT = -14673
757513 XDOT = -4472
561290
YDOT = -9509
875903 feet/sec YDOT = -2898
610175 meter/sec
ZDOT = 16893
468508 ZDOT = 5149
129201
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 10179
55801240
00016717 00000-0 10270-3 0 9033
2 25544 51
6429 172
4106 0009745 16
1728 343
9744 15
72054104 25268
Satellite: ISS
Catalog Number: 25544
Epoch time: 10179
55801240 = yrday
fracday
Element set: 903
Inclination: 51
6429 deg
RA of node: 172
4106 deg
Eccentricity:
0009745
Arg of perigee: 16
1728 deg
Mean anomaly: 343
9744 deg
Mean motion: 15
72054104 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2526
Checksum: 295
Coasting Arc #5 (Orbit 2540)
---------------------------------------
Vector Time (GMT): 2010/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1891435
53 A = 6727836
54 meter
Y = 4341396
63 meter E =
0015613
Z = -4789203
96 I = 51
70593
XDOT = -7241
917237 Wp = 68
93953
YDOT = -344
277369 meter/sec RA = 166
53183 deg
ZDOT = 2560
194774 TA = 226
09965
MA = 226
22866
Ha = 195
920 n
mi
Hp = 184
785
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6205497
13 X = -1916576
49
Y = 14243427
26 feet Y = 4320105
65 meter
Z = -15712611
42 Z = -4798452
81
XDOT = -23759
570989 XDOT = -7249
966012
YDOT = -1129
518927 feet/sec YDOT = -425
306209 meter/sec
ZDOT = 8399
589155 ZDOT = 2524
994440
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14857728
79 X = 4528635
74
Y = 4412620
89 feet Y = 1344966
85 meter
Z = -15749483
94 Z = -4800442
70
XDOT = 1972
303086 XDOT = 601
157981
YDOT = 22694
909241 feet/sec YDOT = 6917
408337 meter/sec
ZDOT = 8259
046899 ZDOT = 2517
357495
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 10180
51154675
00016717 00000-0 10270-3 0 9045
2 25544 51
6429 167
5281 0009922 19
8328 340
3218 15
72019641 25411
Satellite: ISS
Catalog Number: 25544
Epoch time: 10180
51154675 = yrday
fracday
Element set: 904
Inclination: 51
6429 deg
RA of node: 167
5281 deg
Eccentricity:
0009922
Arg of perigee: 19
8328 deg
Mean anomaly: 340
3218 deg
Mean motion: 15
72019641 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2541
Checksum: 300
Coasting Arc #6 (Orbit 2556)
---------------------------------------
Vector Time (GMT): 2010/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6481065
53 A = 6736497
85 meter
Y = -779057
56 meter E =
0009299
Z = -1679056
79 I = 51
76481
XDOT = -870
690641 Wp = 72
15430
YDOT = 5052
934039 meter/sec RA = 161
45264 deg
ZDOT = -5728
434455 TA = 126
33610
MA = 126
25023
Ha = 195
987 n
mi
Hp = 184
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21263338
36 X = 6497451
85
Y = -2555963
14 feet Y = -706490
57 meter
Z = -5508716
49 Z = -1647532
50
XDOT = -2856
596590 XDOT = -899
301438
YDOT = 16577
867581 feet/sec YDOT = 5043
038273 meter/sec
ZDOT = -18794
076296 ZDOT = -5732
733013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5376184
56 X = -1638661
05
Y = -20763670
37 feet Y = -6328766
73 meter
Z = -5382851
99 Z = -1640693
29
XDOT = 15281
272355 XDOT = 4657
731814
YDOT = 899
879250 feet/sec YDOT = 274
283195 meter/sec
ZDOT = -18811
176054 ZDOT = -5733
646461
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 10181
52863743
00016717 00000-0 10270-3 0 9051
2 25544 51
6432 162
3197 0010019 23
7667 336
3956 15
72070495 25578
Satellite: ISS
Catalog Number: 25544
Epoch time: 10181
52863743 = yrday
fracday
Element set: 905
Inclination: 51
6432 deg
RA of node: 162
3197 deg
Eccentricity:
0010019
Arg of perigee: 23
7667 deg
Mean anomaly: 336
3956 deg
Mean motion: 15
72070495 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2557
Checksum: 313
Coasting Arc #7 (Orbit 2572)
---------------------------------------
Vector Time (GMT): 2010/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -377725
80 A = 6726045
55 meter
Y = -4282139
97 meter E =
0013608
Z = 5168291
49 I = 51
75795
XDOT = 7295
612904 Wp = 35
20852
YDOT = -2142
304276 meter/sec RA = 156
31533 deg
ZDOT = -1229
280534 TA = 66
58742
MA = 66
44438
Ha = 196
019 n
mi
Hp = 184
457
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1239257
86 X = -354920
39
Y = -14049015
66 feet Y = -4286237
05 meter
Z = 16956336
91 Z = 5166511
39
XDOT = 23935
737875 XDOT = 7324
997867
YDOT = -7028
557337 feet/sec YDOT = -2060
555930 meter/sec
ZDOT = -4033
072617 ZDOT = -1193
767733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13686769
47 X = -4171727
34
Y = 3438867
57 feet Y = 1048166
84 meter
Z = 16949173
84 Z = 5166108
19
XDOT = -10304
316977 XDOT = -3140
755815
YDOT = -21630
112120 feet/sec YDOT = -6592
858174 meter/sec
ZDOT = -3891
286844 ZDOT = -1186
064230
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 10182
54571595
00016717 00000-0 10270-3 0 9066
2 25544 51
6430 157
1119 0009967 26
8247 333
3429 15
72078320 25735
Satellite: ISS
Catalog Number: 25544
Epoch time: 10182
54571595 = yrday
fracday
Element set: 906
Inclination: 51
6430 deg
RA of node: 157
1119 deg
Eccentricity:
0009967
Arg of perigee: 26
8247 deg
Mean anomaly: 333
3429 deg
Mean motion: 15
72078320 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2573
Checksum: 315
Coasting Arc #8 (Orbit 2588)
---------------------------------------
Vector Time (GMT): 2010/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6042484
25 A = 6737443
45 meter
Y = 2918639
31 meter E =
0022595
Z = 446425
03 I = 51
82403
XDOT = -1705
066370 Wp = 41
87453
YDOT = -4477
247079 meter/sec RA = 151
22024 deg
ZDOT = 6035
150675 TA = 322
96933
MA = 323
12505
Ha = 196
007 n
mi
Hp = 184
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19824423
38 X = -6076840
54
Y = 9575588
28 feet Y = 2850876
50 meter
Z = 1464649
06 Z = 416987
76
XDOT = -5594
049770 XDOT = -1684
191681
YDOT = -14689
130836 feet/sec YDOT = -4496
198112 meter/sec
ZDOT = 19800
363108 ZDOT = 6026
917730
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12762501
99 X = 3890010
61
Y = 17948499
89 feet Y = 5470702
77 meter
Z = 1347124
57 Z = 410603
57
XDOT = -12215
475158 XDOT = -3723
276828
YDOT = 7160
106103 feet/sec YDOT = 2182
400340 meter/sec
ZDOT = 19767
427691 ZDOT = 6025
111960
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 10183
56278104
00016717 00000-0 10270-3 0 9070
2 25544 51
6431 151
9046 0009897 31
4359 328
7393 15
72129381 25894
Satellite: ISS
Catalog Number: 25544
Epoch time: 10183
56278104 = yrday
fracday
Element set: 907
Inclination: 51
6431 deg
RA of node: 151
9046 deg
Eccentricity:
0009897
Arg of perigee: 31
4359 deg
Mean anomaly: 328
7393 deg
Mean motion: 15
72129381 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2589
Checksum: 328
Coasting Arc #9 (Orbit 2603)
---------------------------------------
Vector Time (GMT): 2010/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2488000
56 A = 6725520
11 meter
Y = 3346215
86 meter E =
0022379
Z = -5294763
85 I = 51
81022
XDOT = -6298
309795 Wp = 67
35467
YDOT = 4395
546839 meter/sec RA = 146
10903 deg
ZDOT = -173
800515 TA = 200
94997
MA = 201
04181
Ha = 196
143 n
mi
Hp = 184
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8162731
50 X = 2476118
54
Y = 10978398
50 feet Y = 3373972
32 meter
Z = -17371272
47 Z = -5282705
69
XDOT = -20663
746048 XDOT = -6346
149206
YDOT = 14421
085430 feet/sec YDOT = 4324
847915 meter/sec
ZDOT = -570
211663 ZDOT = -204
513281
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9265018
85 X = 2823977
74
Y = -10148255
27 feet Y = -3093188
21 meter
Z = -17323073
26 Z = -5280072
73
XDOT = 17244
213954 XDOT = 5256
036413
YDOT = 16970
077231 feet/sec YDOT = 5172
479540 meter/sec
ZDOT = -692
822926 ZDOT = -211
172428
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 10184
51627033
00016717 00000-0 10270-3 0 9086
2 25544 51
6437 147
0217 0010015 34
0045 326
1757 15
72108553 26043
Satellite: ISS
Catalog Number: 25544
Epoch time: 10184
51627033 = yrday
fracday
Element set: 908
Inclination: 51
6437 deg
RA of node: 147
0217 deg
Eccentricity:
0010015
Arg of perigee: 34
0045 deg
Mean anomaly: 326
1757 deg
Mean motion: 15
72108553 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2604
Checksum: 273
Coasting Arc #10 (Orbit 2619)
---------------------------------------
Vector Time (GMT): 2010/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4821327
65 A = 6737217
04 meter
Y = -4645849
56 meter E =
0016854
Z = 733391
25 I = 51
87476
XDOT = 3797
610582 Wp = 90
63771
YDOT = 2976
454130 meter/sec RA = 140
99339 deg
ZDOT = -5992
745759 TA = 81
40626
MA = 81
21533
Ha = 196
161 n
mi
Hp = 183
916
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15818004
10 X = 4869357
37
Y = -15242288
59 feet Y = -4591666
13 meter
Z = 2406139
26 Z = 756929
36
XDOT = 12459
352303 XDOT = 3793
156719
YDOT = 9765
269454 feet/sec YDOT = 3018
897059 meter/sec
ZDOT = -19661
239366 ZDOT = -5974
307466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18111714
91 X = -5520450
71
Y = -12411341
02 feet Y = -3782976
74 meter
Z = 2500103
66 Z = 762031
60
XDOT = 6127
957080 XDOT = 1867
801318
YDOT = -12962
990324 feet/sec YDOT = -3951
119451 meter/sec
ZDOT = -19587
560304 ZDOT = -5970
288381
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 10185
53331212
00016717 00000-0 10270-3 0 9091
2 25544 51
6440 141
8136 0010056 37
4383 322
7478 15
72141510 26206
Satellite: ISS
Catalog Number: 25544
Epoch time: 10185
53331212 = yrday
fracday
Element set: 909
Inclination: 51
6440 deg
RA of node: 141
8136 deg
Eccentricity:
0010056
Arg of perigee: 37
4383 deg
Mean anomaly: 322
7478 deg
Mean motion: 15
72141510 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2620
Checksum: 271
Coasting Arc #11 (Orbit 2635)
---------------------------------------
Vector Time (GMT): 2010/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4008427
84 A = 6726039
63 meter
Y = -1707768
71 meter E =
0011388
Z = 5114109
61 I = 51
86069
XDOT = 4522
914787 Wp = 65
75510
YDOT = -6050
494544 meter/sec RA = 135
90904 deg
ZDOT = 1526
526854 TA = 9
66950
MA = 9
64760
Ha = 196
211 n
mi
Hp = 183
784
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13151009
98 X = -4013876
80
Y = -5602915
71 feet Y = -1752624
45 meter
Z = 16778574
85 Z = 5094623
19
XDOT = 14838
959275 XDOT = 4582
820760
YDOT = -19850
703884 feet/sec YDOT = -5999
581851 meter/sec
ZDOT = 5008
290205 ZDOT = 1548
643963
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2577084
07 X = -785495
22
Y = 14152982
00 feet Y = 4313828
91 meter
Z = 16700719
74 Z = 5090379
38
XDOT = -21570
901524 XDOT = -6574
810784
YDOT = -9934
305536 feet/sec YDOT = -3027
976327 meter/sec
ZDOT = 5096
577467 ZDOT = 1553
436812
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 10186
55033999
00016717 00000-0 10270-3 0 9107
2 25544 51
6444 136
6063 0009919 40
6897 319
5005 15
72191973 26368
Satellite: ISS
Catalog Number: 25544
Epoch time: 10186
55033999 = yrday
fracday
Element set: 910
Inclination: 51
6444 deg
RA of node: 136
6063 deg
Eccentricity:
0009919
Arg of perigee: 40
6897 deg
Mean anomaly: 319
5005 deg
Mean motion: 15
72191973 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2636
Checksum: 329
Coasting Arc #12 (Orbit 2650)
---------------------------------------
Vector Time (GMT): 2010/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2961419
77 A = 6735770
57 meter
Y = 5732588
97 meter E =
0017005
Z = -1915571
57 I = 51
91387
XDOT = -5165
658320 Wp = 42
47872
YDOT = -793
445969 meter/sec RA = 130
77480 deg
ZDOT = 5652
671796 TA = 296
32330
MA = 296
49785
Ha = 196
215 n
mi
Hp = 183
648
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9715944
12 X = -3015996
99
Y = 18807706
61 feet Y = 5699167
73 meter
Z = -6284683
63 Z = -1930089
94
XDOT = -16947
697901 XDOT = -5183
861669
YDOT = -2603
169190 feet/sec YDOT = -851
314026 meter/sec
ZDOT = 18545
511141 ZDOT = 5627
532625
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20554742
00 X = 6265085
36
Y = 4990011
62 feet Y = 1520955
54 meter
Z = -6342634
42 Z = -1933234
97
XDOT = 1840
764608 XDOT = 561
065053
YDOT = 15692
251463 feet/sec YDOT = 4782
998246 meter/sec
ZDOT = 18445
077850 ZDOT = 5622
059729
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 10187
50379413
00016717 00000-0 10270-3 0 9118
2 25544 51
6441 131
7235 0010054 44
2776 315
9189 15
72166727 26519
Satellite: ISS
Catalog Number: 25544
Epoch time: 10187
50379413 = yrday
fracday
Element set: 911
Inclination: 51
6441 deg
RA of node: 131
7235 deg
Eccentricity:
0010054
Arg of perigee: 44
2776 deg
Mean anomaly: 315
9189 deg
Mean motion: 15
72166727 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2651
Checksum: 301
Coasting Arc #13 (Orbit 2666)
---------------------------------------
Vector Time (GMT): 2010/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4806917
36 A = 6727799
95 meter
Y = -356798
64 meter E =
0020617
Z = -4713404
19 I = 51
90703
XDOT = -2216
692893 Wp = 60
12465
YDOT = 6810
842909 meter/sec RA = 125
71046 deg
ZDOT = -2775
236736 TA = 182
54282
MA = 182
55331
Ha = 196
226 n
mi
Hp = 183
605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15770726
24 X = 4833446
80
Y = -1170599
20 feet Y = -302895
72 meter
Z = -15463924
52 Z = -4689987
75
XDOT = -7272
614479 XDOT = -2279
206598
YDOT = 22345
285133 feet/sec YDOT = 6785
705445 meter/sec
ZDOT = -9105
107402 ZDOT = -2786
156196
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5123992
67 X = -1561792
97
Y = -15057071
23 feet Y = -4589395
31 meter
Z = -15370373
29 Z = -4684889
78
XDOT = 22344
381006 XDOT = 6810
567331
YDOT = 1738
544598 feet/sec YDOT = 529
908393 meter/sec
ZDOT = -9148
687569 ZDOT = -2788
519971
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 10188
52079831
00016717 00000-0 10270-3 0 9123
2 25544 51
6450 126
5148 0010061 48
1492 312
0527 15
72207977 26674
Satellite: ISS
Catalog Number: 25544
Epoch time: 10188
52079831 = yrday
fracday
Element set: 912
Inclination: 51
6450 deg
RA of node: 126
5148 deg
Eccentricity:
0010061
Arg of perigee: 48
1492 deg
Mean anomaly: 312
0527 deg
Mean motion: 15
72207977 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2667
Checksum: 301
Coasting Arc #14 (Orbit 2682)
---------------------------------------
Vector Time (GMT): 2010/189/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 890678
82 A = 6733532
44 meter
Y = -5997572
60 meter E =
0021561
Z = 2916052
90 I = 51
94388
XDOT = 5569
509409 Wp = 78
39293
YDOT = -1648
085474 meter/sec RA = 120
56435 deg
ZDOT = -5055
299001 TA = 68
21052
MA = 67
98124
Ha = 196
240 n
mi
Hp = 183
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2922174
60 X = 943512
91
Y = -19677075
46 feet Y = -5987317
62 meter
Z = 9567102
69 Z = 2920507
06
XDOT = 18272
668665 XDOT = 5612
082382
YDOT = -5407
104573 feet/sec YDOT = -1585
564937 meter/sec
ZDOT = -16585
626645 ZDOT = -5028
139213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19724426
15 X = -6012005
09
Y = 2516573
22 feet Y = 767051
52 meter
Z = 9584869
82 Z = 2921468
32
XDOT = -9952
836001 XDOT = -3033
624413
YDOT = -14808
806916 feet/sec YDOT = -4513
724348 meter/sec
ZDOT = -16477
113934 ZDOT = -5022
224327
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 10189
53778955
00016717 00000-0 10270-3 0 9139
2 25544 51
6455 121
3066 0010044 51
6872 308
5192 15
72225639 26834
Satellite: ISS
Catalog Number: 25544
Epoch time: 10189
53778955 = yrday
fracday
Element set: 913
Inclination: 51
6455 deg
RA of node: 121
3066 deg
Eccentricity:
0010044
Arg of perigee: 51
6872 deg
Mean anomaly: 308
5192 deg
Mean motion: 15
72225639 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2683
Checksum: 317
Coasting Arc #15 (Orbit 2698)
---------------------------------------
Vector Time (GMT): 2010/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4723819
41 A = 6730109
77 meter
Y = 2519808
94 meter E =
0019035
Z = 4059712
85 I = 51
94712
XDOT = -197
050056 Wp = 80
17430
YDOT = -6653
236255 meter/sec RA = 115
51344 deg
ZDOT = 3888
144359 TA = 329
93866
MA = 330
04779
Ha = 196
374 n
mi
Hp = 183
262
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15498095
18 X = -4771366
54
Y = 8267089
68 feet Y = 2466717
72 meter
Z = 13319267
89 Z = 4036649
64
XDOT = -646
489684 XDOT = -141
525526
YDOT = -21828
202935 feet/sec YDOT = -6655
130095 meter/sec
ZDOT = 12756
379131 ZDOT = 3887
320657
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12360357
35 X = 3767436
92
Y = 12577903
73 feet Y = 3833745
06 meter
Z = 13227113
33 Z = 4031624
14
XDOT = -19801
576935 XDOT = -6035
520650
YDOT = 6005
581587 feet/sec YDOT = 1830
501268 meter/sec
ZDOT = 12753
063664 ZDOT = 3887
133805
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 10190
55476795
00016717 00000-0 10270-3 0 9141
2 25544 51
6459 116
0986 0010005 55
7841 304
4268 15
72242290 26996
Satellite: ISS
Catalog Number: 25544
Epoch time: 10190
55476795 = yrday
fracday
Element set: 914
Inclination: 51
6459 deg
RA of node: 116
0986 deg
Eccentricity:
0010005
Arg of perigee: 55
7841 deg
Mean anomaly: 304
4268 deg
Mean motion: 15
72242290 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2699
Checksum: 321
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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