Date:
July 8th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6458 35 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
197/08:06:48
655 1
6 6
2 6
2
N/A 6
0 0
0 196
4
000/00:18:37
309 -0
7 -0
3 186
8
Coasting Arc #1 (Orbit 2666)
---------------------------------------
Vector Time (GMT): 2010/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4737520
96 A = 6727304
61 meter
Y = -151653
16 meter E =
0021179
Z = -4793867
75 I = 51
90592
XDOT = -2403
260755 Wp = 61
67204
YDOT = 6820
512032 meter/sec RA = 125
71378 deg
ZDOT = -2589
596028 TA = 182
95697
MA = 182
96951
Ha = 196
168 n
mi
Hp = 183
459
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15543047
76 X = 4762152
46
Y = -497549
73 feet Y = -98536
87 meter
Z = -15727912
55 Z = -4770793
01
XDOT = -7884
713763 XDOT = -2466
770526
YDOT = 22377
007980 feet/sec YDOT = 6793
282656 meter/sec
ZDOT = -8496
049962 ZDOT = -2601
424255
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4415713
59 X = -1345909
50
Y = -15007554
61 feet Y = -4574302
64 meter
Z = -15635725
15 Z = -4765769
02
XDOT = 22533
609705 XDOT = 6868
244238
YDOT = 2274
796772 feet/sec YDOT = 693
358056 meter/sec
ZDOT = -8543
260775 ZDOT = -2603
985884
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
52045118
00016717 00000-0 10270-3 0 9001
2 25544 51
6448 126
5215 0010080 49
9383 310
2662 15
72266087 26672
Satellite: ISS
Catalog Number: 25544
Epoch time: 10188
52045118 = yrday
fracday
Element set: 900
Inclination: 51
6448 deg
RA of node: 126
5215 deg
Eccentricity:
0010080
Arg of perigee: 49
9383 deg
Mean anomaly: 310
2662 deg
Mean motion: 15
72266087 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2667
Checksum: 297
Coasting Arc #2 (Orbit 2682)
---------------------------------------
Vector Time (GMT): 2010/189/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1074252
86 A = 6733804
84 meter
Y = -6047220
96 meter E =
0021731
Z = 2747144
30 I = 51
94530
XDOT = 5527
483733 Wp = 80
84937
YDOT = -1387
628382 meter/sec RA = 120
56912 deg
ZDOT = -5178
094068 TA = 67
91727
MA = 67
68666
Ha = 196
199 n
mi
Hp = 183
232
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3524451
64 X = 1128449
02
Y = -19839963
78 feet Y = -6034905
50 meter
Z = 9012940
61 Z = 2752493
56
XDOT = 18134
789151 XDOT = 5567
743867
YDOT = -4552
586555 feet/sec YDOT = -1325
590710 meter/sec
ZDOT = -16988
497600 ZDOT = -5151
144011
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20043766
70 X = -6109340
09
Y = 1976904
14 feet Y = 602560
38 meter
Z = 9034284
00 Z = 2753649
76
XDOT = -9132
650429 XDOT = -2783
631851
YDOT = -14884
160379 feet/sec YDOT = -4536
692083 meter/sec
ZDOT = -16880
821594 ZDOT = -5145
274422
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
53740729
00016717 00000-0 10270-3 0 9014
2 25544 51
6454 121
3131 0010083 53
4763 306
7326 15
72275131 26839
Satellite: ISS
Catalog Number: 25544
Epoch time: 10189
53740729 = yrday
fracday
Element set: 901
Inclination: 51
6454 deg
RA of node: 121
3131 deg
Eccentricity:
0010083
Arg of perigee: 53
4763 deg
Mean anomaly: 306
7326 deg
Mean motion: 15
72275131 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2683
Checksum: 287
Coasting Arc #3 (Orbit 2698)
---------------------------------------
Vector Time (GMT): 2010/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4727039
57 A = 6729503
28 meter
Y = 2281610
81 meter E =
0018543
Z = 4193966
91 I = 51
94554
XDOT = 23
513791 Wp = 81
89227
YDOT = -6765
026704 meter/sec RA = 115
51662 deg
ZDOT = 3695
586575 TA = 330
55074
MA = 330
65509
Ha = 196
343 n
mi
Hp = 183
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15508659
99 X = -4772575
06
Y = 7485599
76 feet Y = 2228494
81 meter
Z = 13759733
94 Z = 4170892
89
XDOT = 77
144985 XDOT = 81
207396
YDOT = -22194
969500 feet/sec YDOT = -6764
441901 meter/sec
ZDOT = 12124
627872 ZDOT = 3695
839615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11614977
28 X = 3540245
08
Y = 12813032
30 feet Y = 3905412
24 meter
Z = 13667535
36 Z = 4165864
78
XDOT = -20343
133090 XDOT = -6200
586966
YDOT = 5467
116449 feet/sec YDOT = 1666
377094 meter/sec
ZDOT = 12125
614800 ZDOT = 3695
887391
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
55435625
00016717 00000-0 10270-3 0 9025
2 25544 51
6457 116
1048 0010040 57
5685 302
6447 15
72286330 26991
Satellite: ISS
Catalog Number: 25544
Epoch time: 10190
55435625 = yrday
fracday
Element set: 902
Inclination: 51
6457 deg
RA of node: 116
1048 deg
Eccentricity:
0010040
Arg of perigee: 57
5685 deg
Mean anomaly: 302
6447 deg
Mean motion: 15
72286330 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2699
Checksum: 300
Coasting Arc #4 (Orbit 2713)
---------------------------------------
Vector Time (GMT): 2010/191/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 989010
43 A = 6731233
47 meter
Y = 5566681
12 meter E =
0014863
Z = -3661651
17 I = 51
96425
XDOT = -5062
848140 Wp = 74
91874
YDOT = 3773
920678 meter/sec RA = 110
36598 deg
ZDOT = 4388
367787 TA = 241
43792
MA = 241
58759
Ha = 196
260 n
mi
Hp = 183
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3244784
88 X = 944476
74
Y = 18263389
52 feet Y = 5577492
55 meter
Z = -12013291
25 Z = -3656953
68
XDOT = -16610
394161 XDOT = -5125
990196
YDOT = 12381
629520 feet/sec YDOT = 3716
950974 meter/sec
ZDOT = 14397
532110 ZDOT = 4363
620100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16416427
15 X = 5003726
99
Y = -8662101
47 feet Y = -2640208
53 meter
Z = -11994503
33 Z = -3655924
61
XDOT = 16203
680732 XDOT = 4938
881887
YDOT = 10993
857701 feet/sec YDOT = 3350
927827 meter/sec
ZDOT = 14298
633986 ZDOT = 4358
223639
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 10191
50774014
00016717 00000-0 10270-3 0 9030
2 25544 51
6464 111
2219 0010073 60
7221 299
4947 15
72295350 27141
Satellite: ISS
Catalog Number: 25544
Epoch time: 10191
50774014 = yrday
fracday
Element set: 903
Inclination: 51
6464 deg
RA of node: 111
2219 deg
Eccentricity:
0010073
Arg of perigee: 60
7221 deg
Mean anomaly: 299
4947 deg
Mean motion: 15
72295350 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2714
Checksum: 285
Coasting Arc #5 (Orbit 2729)
---------------------------------------
Vector Time (GMT): 2010/192/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3960628
33 A = 6731867
53 meter
Y = -4215008
71 meter E =
0014804
Z = -3461176
66 I = 51
97686
XDOT = 2142
508110 Wp = 72
05383
YDOT = 5776
239729 meter/sec RA = 105
31801 deg
ZDOT = -4594
159025 TA = 148
62707
MA = 148
53867
Ha = 196
272 n
mi
Hp = 183
015
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12994187
43 X = 4024280
45
Y = -13828768
72 feet Y = -4170362
05 meter
Z = -11355566
46 Z = -3441782
41
XDOT = 7029
226083 XDOT = 2100
075136
YDOT = 18950
917745 feet/sec YDOT = 5799
962134 meter/sec
ZDOT = -15072
700214 ZDOT = -4583
852879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17260751
34 X = -5261077
01
Y = -7994036
86 feet Y = -2436582
44 meter
Z = -11278052
96 Z = -3437550
54
XDOT = 15126
520704 XDOT = 4610
563511
YDOT = -11508
501681 feet/sec YDOT = -3507
791312 meter/sec
ZDOT = -15031
495077 ZDOT = -4581
599699
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 10192
52467575
00016717 00000-0 10270-3 0 9045
2 25544 51
6474 106
0133 0010102 64
2665 295
9539 15
72311212 27305
Satellite: ISS
Catalog Number: 25544
Epoch time: 10192
52467575 = yrday
fracday
Element set: 904
Inclination: 51
6474 deg
RA of node: 106
0133 deg
Eccentricity:
0010102
Arg of perigee: 64
2665 deg
Mean anomaly: 295
9539 deg
Mean motion: 15
72311212 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2730
Checksum: 284
Coasting Arc #6 (Orbit 2745)
---------------------------------------
Vector Time (GMT): 2010/193/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2668601
45 A = 6728816
44 meter
Y = -4377001
10 meter E =
0019699
Z = 4346965
15 I = 51
97302
XDOT = 3779
260537 Wp = 69
34122
YDOT = -5756
527776 meter/sec RA = 100
17003 deg
ZDOT = -3456
903077 TA = 55
47026
MA = 55
28446
Ha = 196
353 n
mi
Hp = 182
885
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8755254
11 X = -2640575
03
Y = -14360239
81 feet Y = -4406686
99 meter
Z = 14261696
68 Z = 4334068
71
XDOT = 12399
148744 XDOT = 3860
142856
YDOT = -18886
245985 feet/sec YDOT = -5713
813030 meter/sec
ZDOT = -11341
545529 ZDOT = -3438
348283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10585633
64 X = -3226501
13
Y = 13125674
52 feet Y = 4000705
59 meter
Z = 14210136
64 Z = 4331249
65
XDOT = -21007
334287 XDOT = -6403
035491
YDOT = -4674
905515 feet/sec YDOT = -1424
911201 meter/sec
ZDOT = -11267
380394 ZDOT = -3434
297544
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 10193
54160476
00016717 00000-0 10270-3 0 9059
2 25544 51
6469 100
8051 0010098 67
8608 292
3625 15
72315561 27465
Satellite: ISS
Catalog Number: 25544
Epoch time: 10193
54160476 = yrday
fracday
Element set: 905
Inclination: 51
6469 deg
RA of node: 100
8051 deg
Eccentricity:
0010098
Arg of perigee: 67
8608 deg
Mean anomaly: 292
3625 deg
Mean motion: 15
72315561 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2746
Checksum: 308
Coasting Arc #7 (Orbit 2761)
---------------------------------------
Vector Time (GMT): 2010/194/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2499348
54 A = 6734239
25 meter
Y = 5703122
15 meter E =
0023909
Z = 2534792
28 I = 51
99582
XDOT = -3816
164710 Wp = 73
96415
YDOT = -4055
548427 meter/sec RA = 95
11732 deg
ZDOT = 5327
199842 TA = 314
62303
MA = 314
81778
Ha = 196
364 n
mi
Hp = 182
837
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8199962
41 X = -2575249
43
Y = 18711030
69 feet Y = 5674748
22 meter
Z = 8316247
64 Z = 2522467
11
XDOT = -12520
225425 XDOT = -3796
409204
YDOT = -13305
605075 feet/sec YDOT = -4098
113309 meter/sec
ZDOT = 17477
689769 ZDOT = 5308
708765
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20414909
38 X = 6222464
38
Y = 1179208
98 feet Y = 359422
90 meter
Z = 8266980
66 Z = 2519775
70
XDOT = -7960
038823 XDOT = -2426
219833
YDOT = 14992
685456 feet/sec YDOT = 4569
770527 meter/sec
ZDOT = 17403
760461 ZDOT = 5304
666188
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 10194
55852692
00016717 00000-0 10270-3 0 9060
2 25544 51
6474 95
5963 0010110 71
4253 288
8006 15
72310465 27624
Satellite: ISS
Catalog Number: 25544
Epoch time: 10194
55852692 = yrday
fracday
Element set: 906
Inclination: 51
6474 deg
RA of node: 95
5963 deg
Eccentricity:
0010110
Arg of perigee: 71
4253 deg
Mean anomaly: 288
8006 deg
Mean motion: 15
72310465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2762
Checksum: 308
Coasting Arc #8 (Orbit 2776)
---------------------------------------
Vector Time (GMT): 2010/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3828281
45 A = 6726660
15 meter
Y = 2612109
81 meter E =
0021304
Z = -4893871
99 I = 51
97239
XDOT = -1835
769084 Wp = 92
46158
YDOT = 7079
887401 meter/sec RA = 89
97873 deg
ZDOT = 2350
704534 TA = 200
35355
MA = 200
43858
Ha = 196
267 n
mi
Hp = 182
882
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12559978
53 X = 3822560
90
Y = 8569914
07 feet Y = 2654888
47 meter
Z = -16056010
48 Z = -4875288
20
XDOT = -6022
864448 XDOT = -1926
220299
YDOT = 23227
977038 feet/sec YDOT = 7058
852747 meter/sec
ZDOT = 7712
285217 ZDOT = 2341
567596
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3342843
05 X = 1018898
56
Y = -14913159
40 feet Y = -4545530
99 meter
Z = -15981709
46 Z = -4871225
04
XDOT = 22750
014630 XDOT = 6934
204459
YDOT = -3098
488948 feet/sec YDOT = -944
419431 meter/sec
ZDOT = 7675
762177 ZDOT = 2339
572312
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 10195
51188383
00016717 00000-0 10270-3 0 9077
2 25544 51
6477 90
7131 0009988 74
6986 285
5279 15
72335496 27773
Satellite: ISS
Catalog Number: 25544
Epoch time: 10195
51188383 = yrday
fracday
Element set: 907
Inclination: 51
6477 deg
RA of node: 90
7131 deg
Eccentricity:
0009988
Arg of perigee: 74
6986 deg
Mean anomaly: 285
5279 deg
Mean motion: 15
72335496 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2777
Checksum: 364
Coasting Arc #9 (Orbit 2792)
---------------------------------------
Vector Time (GMT): 2010/196/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 657773
54 A = 6735899
57 meter
Y = -6515276
42 meter E =
0015316
Z = -1578152
86 I = 52
00211
XDOT = 4707
789504 Wp = 107
32533
YDOT = 1865
742752 meter/sec RA = 84
91288 deg
ZDOT = -5790
652262 TA = 89
97081
MA = 89
79529
Ha = 196
276 n
mi
Hp = 182
842
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2158049
68 X = 738245
92
Y = -21375578
80 feet Y = -6507470
72 meter
Z = -5177666
85 Z = -1574762
55
XDOT = 15445
503622 XDOT = 4714
706013
YDOT = 6121
203253 feet/sec YDOT = 1918
427245 meter/sec
ZDOT = -18998
202959 ZDOT = -5767
765231
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20590895
02 X = -6276104
80
Y = 6142291
59 feet Y = 1872170
48 meter
Z = -5164114
40 Z = -1574022
07
XDOT = 161
781527 XDOT = 49
311010
YDOT = -15214
330168 feet/sec YDOT = -4637
327835 meter/sec
ZDOT = -18906
696954 ZDOT = -5762
761232
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 10196
52879232
00016717 00000-0 10270-3 0 9080
2 25544 51
6476 85
5037 0009874 79
1810 281
0463 15
72312941 27933
Satellite: ISS
Catalog Number: 25544
Epoch time: 10196
52879232 = yrday
fracday
Element set: 908
Inclination: 51
6476 deg
RA of node: 85
5037 deg
Eccentricity:
0009874
Arg of perigee: 79
1810 deg
Mean anomaly: 281
0463 deg
Mean motion: 15
72312941 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2793
Checksum: 327
Coasting Arc #10 (Orbit 2805)
---------------------------------------
Vector Time (GMT): 2010/197/08:16:07
309
Vector Time (MET): N/A
Weight (LBS) : 828051
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4088450
68 A = 6731733
18 meter
Y = 2799238
23 meter E =
0014331
Z = -4570235
48 I = 51
97017
XDOT = -1295
803927 Wp = 100
43365
YDOT = 6918
368786 meter/sec RA = 80
56875 deg
ZDOT = 3083
858427 TA = 200
16646
MA = 200
22313
Ha = 196
399 n
mi
Hp = 186
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13413552
10 X = 4079046
33
Y = 9183852
46 feet Y = 2844905
52 meter
Z = -14994210
90 Z = -4550396
65
XDOT = -4251
325220 XDOT = -1388
050719
YDOT = 22698
060323 feet/sec YDOT = 6903
362300 meter/sec
ZDOT = 10117
645759 ZDOT = 3077
339994
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15020135
20 X = 4578137
21
Y = -6405808
55 feet Y = -1952490
45 meter
Z = -14914893
29 Z = -4546059
47
XDOT = 16310
008055 XDOT = 4971
290455
YDOT = 14789
627700 feet/sec YDOT = 4507
878523 meter/sec
ZDOT = 10091
580902 ZDOT = 3075
913859
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 10197
35502895
00016717 00000-0 10270-3 0 9091
2 25544 51
6453 81
2707 0004702 79
1210 281
0480 15
71021750 28062
Satellite: ISS
Catalog Number: 25544
Epoch time: 10197
35502895 = yrday
fracday
Element set: 909
Inclination: 51
6453 deg
RA of node: 81
2707 deg
Eccentricity:
0004702
Arg of perigee: 79
1210 deg
Mean anomaly: 281
0480 deg
Mean motion: 15
71021750 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2806
Checksum: 287
Coasting Arc #11 (Orbit 2821)
---------------------------------------
Vector Time (GMT): 2010/198/08:16:07
309
Vector Time (MET): N/A
Weight (LBS) : 828051
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -186799
18 A = 6739139
90 meter
Y = -6478881
57 meter E =
0010488
Z = -1841520
54 I = 51
99007
XDOT = 4968
399630 Wp = 118
69324
YDOT = 1464
717987 meter/sec RA = 75
51873 deg
ZDOT = -5686
383994 TA = 81
60271
MA = 81
48383
Ha = 196
375 n
mi
Hp = 186
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -612858
19 X = -105391
56
Y = -21256173
12 feet Y = -6480515
13 meter
Z = -6041734
04 Z = -1842230
83
XDOT = 16300
523721 XDOT = 4979
274824
YDOT = 4805
505207 feet/sec YDOT = 1520
338901 meter/sec
ZDOT = -18656
115466 ZDOT = -5662
221159
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18389235
74 X = -5605039
05
Y = -10677186
72 feet Y = -3254406
51 meter
Z = -6044562
34 Z = -1842382
60
XDOT = 11931
893330 XDOT = 3636
841087
YDOT = -10097
510857 feet/sec YDOT = -3077
721309 meter/sec
ZDOT = -18559
510476 ZDOT = -5656
938793
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 10198
37278248
00016717 00000-0 10270-3 0 9108
2 25544 51
6461 76
0673 0004717 82
5022 277
6676 15
71039191 28224
Satellite: ISS
Catalog Number: 25544
Epoch time: 10198
37278248 = yrday
fracday
Element set: 910
Inclination: 51
6461 deg
RA of node: 76
0673 deg
Eccentricity:
0004717
Arg of perigee: 82
5022 deg
Mean anomaly: 277
6676 deg
Mean motion: 15
71039191 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2822
Checksum: 316
Coasting Arc #12 (Orbit 2837)
---------------------------------------
Vector Time (GMT): 2010/199/08:16:07
309
Vector Time (MET): N/A
Weight (LBS) : 828051
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4229127
79 A = 6728819
94 meter
Y = 301092
67 meter E =
0008043
Z = 5218804
93 I = 51
94693
XDOT = -1793
096360 Wp = 72
77411
YDOT = -7420
548628 meter/sec RA = 70
40425 deg
ZDOT = -1021
326262 TA = 26
94142
MA = 26
89968
Ha = 196
451 n
mi
Hp = 186
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13875091
18 X = -4257532
23
Y = 987836
86 feet Y = 253640
70 meter
Z = 17122063
40 Z = 5198190
96
XDOT = -5882
862073 XDOT = -1705
023773
YDOT = -24345
631980 feet/sec YDOT = -7440
107558 meter/sec
ZDOT = -3350
807947 ZDOT = -1029
823906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6287723
09 X = -1916498
00
Y = 12520947
89 feet Y = 3816384
92 meter
Z = 17039643
02 Z = 5193683
19
XDOT = -23012
697491 XDOT = -7014
270195
YDOT = -6933
932909 feet/sec YDOT = -2113
462751 meter/sec
ZDOT = -3384
757991 ZDOT = -1031
674236
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 10199
39052934
00016717 00000-0 10270-3 0 9114
2 25544 51
6462 70
8647 0004633 85
6655 274
5036 15
71065071 28380
Satellite: ISS
Catalog Number: 25544
Epoch time: 10199
39052934 = yrday
fracday
Element set: 911
Inclination: 51
6462 deg
RA of node: 70
8647 deg
Eccentricity:
0004633
Arg of perigee: 85
6655 deg
Mean anomaly: 274
5036 deg
Mean motion: 15
71065071 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2838
Checksum: 318
Coasting Arc #13 (Orbit 2852)
---------------------------------------
Vector Time (GMT): 2010/200/08:16:07
309
Vector Time (MET): N/A
Weight (LBS) : 828051
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2871980
90 A = 6740598
36 meter
Y = 6091179
16 meter E =
0015808
Z = -84951
49 I = 51
97532
XDOT = -4260
354290 Wp = 56
39353
YDOT = 2081
985144 meter/sec RA = 65
32140 deg
ZDOT = 6062
202688 TA = 302
68898
MA = 302
84134
Ha = 196
369 n
mi
Hp = 186
629
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9422509
52 X = 2804067
45
Y = 19984183
60 feet Y = 6122915
65 meter
Z = -278712
25 Z = -71163
69
XDOT = -13977
540320 XDOT = -4312
767756
YDOT = 6830
659921 feet/sec YDOT = 2034
049531 meter/sec
ZDOT = 19889
116431 ZDOT = 6041
378902
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22027354
19 X = 6713937
56
Y = 1724709
81 feet Y = 525691
55 meter
Z = -223616
03 Z = -68158
17
XDOT = -930
451522 XDOT = -283
601624
YDOT = 14021
260068 feet/sec YDOT = 4273
680069 meter/sec
ZDOT = 19805
845526 ZDOT = 6036
821716
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 10200
34466259
00016717 00000-0 10270-3 0 9122
2 25544 51
6464 65
9865 0004668 88
6178 271
5519 15
71043838 28537
Satellite: ISS
Catalog Number: 25544
Epoch time: 10200
34466259 = yrday
fracday
Element set: 912
Inclination: 51
6464 deg
RA of node: 65
9865 deg
Eccentricity:
0004668
Arg of perigee: 88
6178 deg
Mean anomaly: 271
5519 deg
Mean motion: 15
71043838 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2853
Checksum: 333
Coasting Arc #14 (Orbit 2868)
---------------------------------------
Vector Time (GMT): 2010/201/08:16:07
309
Vector Time (MET): N/A
Weight (LBS) : 828051
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2894115
82 A = 6728884
63 meter
Y = -3156442
15 meter E =
0018991
Z = -5206761
11 I = 51
92356
XDOT = 4536
924001 Wp = 83
74759
YDOT = 6087
708834 meter/sec RA = 60
24037 deg
ZDOT = -1170
310888 TA = 175
10289
MA = 175
08429
Ha = 196
319 n
mi
Hp = 186
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9495130
66 X = 2954490
02
Y = -10355781
34 feet Y = -3123740
13 meter
Z = -17082549
56 Z = -5192555
35
XDOT = 14884
921263 XDOT = 4474
198067
YDOT = 19972
798011 feet/sec YDOT = 6138
092869 meter/sec
ZDOT = -3839
602651 ZDOT = -1148
422133
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4466734
08 X = -1361460
55
Y = -13393510
53 feet Y = -4082342
01 meter
Z = -17025726
86 Z = -5189441
55
XDOT = 23703
507022 XDOT = 7224
828940
YDOT = -3142
206227 feet/sec YDOT = -957
744458 meter/sec
ZDOT = -3752
123878 ZDOT = -1143
647358
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 10201
36239826
00016717 00000-0 10270-3 0 9134
2 25544 51
6474 60
7832 0004710 92
4349 267
7352 15
71076308 28693
Satellite: ISS
Catalog Number: 25544
Epoch time: 10201
36239826 = yrday
fracday
Element set: 913
Inclination: 51
6474 deg
RA of node: 60
7832 deg
Eccentricity:
0004710
Arg of perigee: 92
4349 deg
Mean anomaly: 267
7352 deg
Mean motion: 15
71076308 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2869
Checksum: 311
Coasting Arc #15 (Orbit 2884)
---------------------------------------
Vector Time (GMT): 2010/202/08:16:07
309
Vector Time (MET): N/A
Weight (LBS) : 828051
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4825878
30 A = 6738985
54 meter
Y = -4274892
85 meter E =
0018632
Z = 1934250
36 I = 51
94128
XDOT = 2010
589893 Wp = 108
54572
YDOT = -4839
608552 meter/sec RA = 55
12108 deg
ZDOT = -5641
465156 TA = 50
04866
MA = 49
88513
Ha = 196
365 n
mi
Hp = 186
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15832934
04 X = -4787113
16
Y = -14025239
01 feet Y = -4328642
25 meter
Z = 6345965
75 Z = 1910899
93
XDOT = 6596
423535 XDOT = 2091
962845
YDOT = -15877
980813 feet/sec YDOT = -4816
669099 meter/sec
ZDOT = -18508
743951 ZDOT = -5631
500867
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19801785
98 X = -6035584
37
Y = 7513605
62 feet Y = 2290146
99 meter
Z = 6252632
55 Z = 1905802
40
XDOT = -10381
404451 XDOT = -3164
252077
YDOT = -11884
503495 feet/sec YDOT = -3622
396665 meter/sec
ZDOT = -18468
859958 ZDOT = -5629
308515
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 10202
38012831
00016717 00000-0 10270-3 0 9143
2 25544 51
6474 55
5802 0004681 96
5474 263
6220 15
71060756 28850
Satellite: ISS
Catalog Number: 25544
Epoch time: 10202
38012831 = yrday
fracday
Element set: 914
Inclination: 51
6474 deg
RA of node: 55
5802 deg
Eccentricity:
0004681
Arg of perigee: 96
5474 deg
Mean anomaly: 263
6220 deg
Mean motion: 15
71060756 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2885
Checksum: 297
Coasting Arc #16 (Orbit 2900)
---------------------------------------
Vector Time (GMT): 2010/203/08:16:07
309
Vector Time (MET): N/A
Weight (LBS) : 828051
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -411673
91 A = 6731757
64 meter
Y = 4991813
09 meter E =
0013486
Z = 4488855
36 I = 51
89933
XDOT = -6122
851126 Wp = 107
73970
YDOT = -3398
395475 meter/sec RA = 50
06821 deg
ZDOT = 3205
778809 TA = 310
26684
MA = 310
38468
Ha = 196
307 n
mi
Hp = 186
595
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1350636
20 X = -489268
46
Y = 16377339
54 feet Y = 4986774
95 meter
Z = 14727215
76 Z = 4486667
79
XDOT = -20088
094245 XDOT = -6099
967490
YDOT = -11149
591455 feet/sec YDOT = -3466
737407 meter/sec
ZDOT = 10517
647011 ZDOT = 3176
089398
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13975277
61 X = 4259664
62
Y = 8659796
06 feet Y = 2639505
84 meter
Z = 14718420
45 Z = 4486174
55
XDOT = -18397
996108 XDOT = -5607
709214
YDOT = 11950
349486 feet/sec YDOT = 3642
466523 meter/sec
ZDOT = 10398
957787 ZDOT = 3169
602334
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 10203
39785148
00016717 00000-0 10270-3 0 9154
2 25544 51
6476 50
3771 0004653 99
3633 260
8055 15
71081568 29015
Satellite: ISS
Catalog Number: 25544
Epoch time: 10203
39785148 = yrday
fracday
Element set: 915
Inclination: 51
6476 deg
RA of node: 50
3771 deg
Eccentricity:
0004653
Arg of perigee: 99
3633 deg
Mean anomaly: 260
8055 deg
Mean motion: 15
71081568 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2901
Checksum: 313
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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