Date:
July 3rd 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12916 69 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 2556)
---------------------------------------
Vector Time (GMT): 2010/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6475962
15 A = 6736306
23 meter
Y = -750502
87 meter E =
0009314
Z = -1710921
49 I = 51
76473
XDOT = -917
998727 Wp = 71
91025
YDOT = 5058
497163 meter/sec RA = 161
45567 deg
ZDOT = -5716
180976 TA = 126
94456
MA = 126
85922
Ha = 195
909 n
mi
Hp = 184
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21246594
97 X = 6492184
33
Y = -2462279
74 feet Y = -677993
86 meter
Z = -5613259
49 Z = -1679422
39
XDOT = -3011
806846 XDOT = -946
727740
YDOT = 16596
119301 feet/sec YDOT = 5048
071708 meter/sec
ZDOT = -18753
874594 ZDOT = -5720
709640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5281190
44 X = -1609706
84
Y = -20760195
70 feet Y = -6327707
65 meter
Z = -5487495
19 Z = -1672588
53
XDOT = 15320
367083 XDOT = 4669
647887
YDOT = 1044
569196 feet/sec YDOT = 318
384691 meter/sec
ZDOT = -18771
893077 ZDOT = -5721
673010
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
52857223
00016717 00000-0 10270-3 0 9002
2 25544 51
6433 162
3230 0009998 24
1493 336
0136 15
72121637 25575
Satellite: ISS
Catalog Number: 25544
Epoch time: 10181
52857223 = yrday
fracday
Element set: 900
Inclination: 51
6433 deg
RA of node: 162
3230 deg
Eccentricity:
0009998
Arg of perigee: 24
1493 deg
Mean anomaly: 336
0136 deg
Mean motion: 15
72121637 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2557
Checksum: 291
Coasting Arc #2 (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 = -316032
67 A = 6725939
49 meter
Y = -4299871
76 meter E =
0013721
Z = 5157557
72 I = 51
75820
XDOT = 7299
665536 Wp = 35
57533
YDOT = -2094
668565 meter/sec RA = 156
31725 deg
ZDOT = -1286
388400 TA = 66
77413
MA = 66
62970
Ha = 195
935 n
mi
Hp = 184
366
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1036852
58 X = -292981
43
Y = -14107190
81 feet Y = -4303277
57 meter
Z = 16921121
13 Z = 5156077
92
XDOT = 23949
033911 XDOT = 7328
794943
YDOT = -6872
272195 feet/sec YDOT = -2012
876322 meter/sec
ZDOT = -4220
434384 ZDOT = -1250
856527
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13774781
00 X = -4198553
25
Y = 3247323
26 feet Y = 989784
13 meter
Z = 16915157
00 Z = 5155739
85
XDOT = -10165
954299 XDOT = -3098
582870
YDOT = -21661
457525 feet/sec YDOT = -6602
412254 meter/sec
ZDOT = -4078
571844 ZDOT = -1243
148698
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
54561695
00016717 00000-0 10270-3 0 9011
2 25544 51
6431 157
1151 0009943 27
1971 332
9710 15
72131648 25735
Satellite: ISS
Catalog Number: 25544
Epoch time: 10182
54561695 = yrday
fracday
Element set: 901
Inclination: 51
6431 deg
RA of node: 157
1151 deg
Eccentricity:
0009943
Arg of perigee: 27
1971 deg
Mean anomaly: 332
9710 deg
Mean motion: 15
72131648 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2573
Checksum: 300
Coasting Arc #3 (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 = -6061400
47 A = 6737258
97 meter
Y = 2867099
39 meter E =
0022660
Z = 515069
62 I = 51
82406
XDOT = -1614
430174 Wp = 42
48993
YDOT = -4520
569594 meter/sec RA = 151
22289 deg
ZDOT = 6027
994851 TA = 323
10116
MA = 323
25686
Ha = 195
921 n
mi
Hp = 184
137
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19886484
49 X = -6095512
49
Y = 9406494
07 feet Y = 2799126
41 meter
Z = 1689860
95 Z = 485541
04
XDOT = -5296
686921 XDOT = -1593
043019
YDOT = -14831
265072 feet/sec YDOT = -4538
504213 meter/sec
ZDOT = 19776
885994 ZDOT = 6020
203453
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12606422
86 X = 3842437
69
Y = 18039319
15 feet Y = 5498384
48 meter
Z = 1571971
18 Z = 479136
82
XDOT = -12398
812598 XDOT = -3779
158080
YDOT = 6902
003556 feet/sec YDOT = 2103
730684 meter/sec
ZDOT = 19745
713401 ZDOT = 6018
493445
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
56264710
00016717 00000-0 10270-3 0 9023
2 25544 51
6433 151
9074 0009868 31
8142 328
3614 15
72184844 25896
Satellite: ISS
Catalog Number: 25544
Epoch time: 10183
56264710 = yrday
fracday
Element set: 902
Inclination: 51
6433 deg
RA of node: 151
9074 deg
Eccentricity:
0009868
Arg of perigee: 31
8142 deg
Mean anomaly: 328
3614 deg
Mean motion: 15
72184844 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2589
Checksum: 313
Coasting Arc #4 (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 = 2396394
20 A = 6725347
67 meter
Y = 3409344
24 meter E =
0022336
Z = -5296457
61 I = 51
81030
XDOT = -6344
374780 Wp = 68
03497
YDOT = 4331
926822 meter/sec RA = 146
10976 deg
ZDOT = -74
135784 TA = 201
21515
MA = 201
30791
Ha = 196
054 n
mi
Hp = 184
066
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7862185
69 X = 2383821
30
Y = 11185512
61 feet Y = 3436072
44 meter
Z = -17376829
43 Z = -5284846
15
XDOT = -20814
877886 XDOT = -6391
983506
YDOT = 14212
358340 feet/sec YDOT = 4260
714051 meter/sec
ZDOT = -243
227638 ZDOT = -105
071780
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9524005
83 X = 2902916
98
Y = -9891103
97 feet Y = -3014808
49 meter
Z = -17330413
51 Z = -5282310
04
XDOT = 17086
061369 XDOT = 5207
831505
YDOT = 17140
123947 feet/sec YDOT = 5224
309779 meter/sec
ZDOT = -366
731218 ZDOT = -111
779675
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
51610261
00016717 00000-0 10270-3 0 9036
2 25544 51
6438 147
0244 0009988 34
3831 325
7976 15
72165008 26043
Satellite: ISS
Catalog Number: 25544
Epoch time: 10184
51610261 = yrday
fracday
Element set: 903
Inclination: 51
6438 deg
RA of node: 147
0244 deg
Eccentricity:
0009988
Arg of perigee: 34
3831 deg
Mean anomaly: 325
7976 deg
Mean motion: 15
72165008 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2604
Checksum: 303
Coasting Arc #5 (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 = 4887247
99 A = 6737114
44 meter
Y = -4592161
33 meter E =
0016622
Z = 627692
18 I = 51
87511
XDOT = 3685
901038 Wp = 91
32376
YDOT = 3082
889411 meter/sec RA = 140
99554 deg
ZDOT = -6008
573082 TA = 81
87280
MA = 81
68427
Ha = 196
067 n
mi
Hp = 183
823
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16034278
18 X = 4935185
93
Y = -15066146
10 feet Y = -4537241
25 meter
Z = 2059357
55 Z = 651550
32
XDOT = 12092
851176 XDOT = 3680
342186
YDOT = 10114
466571 feet/sec YDOT = 3124
076961 meter/sec
ZDOT = -19713
166278 ZDOT = -5990
680145
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17983142
60 X = -5481261
86
Y = -12660650
31 feet Y = -3858966
22 meter
Z = 2154600
78 Z = 656722
32
XDOT = 6525
544366 XDOT = 1988
985923
YDOT = -12683
976481 feet/sec YDOT = -3866
076031 meter/sec
ZDOT = -19641
664297 ZDOT = -5986
779278
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
53310719
00016717 00000-0 10270-3 0 9045
2 25544 51
6442 141
8160 0010026 37
8116 322
3749 15
72200025 26204
Satellite: ISS
Catalog Number: 25544
Epoch time: 10185
53310719 = yrday
fracday
Element set: 904
Inclination: 51
6442 deg
RA of node: 141
8160 deg
Eccentricity:
0010026
Arg of perigee: 37
8116 deg
Mean anomaly: 322
3749 deg
Mean motion: 15
72200025 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2620
Checksum: 263
Coasting Arc #6 (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 = -3912819
82 A = 6725734
84 meter
Y = -1833496
61 meter E =
0011240
Z = 5144344
30 I = 51
86036
XDOT = 4631
459854 Wp = 64
63971
YDOT = -6002
016518 meter/sec RA = 135
90865 deg
ZDOT = 1385
916839 TA = 12
15665
MA = 12
12955
Ha = 196
115 n
mi
Hp = 183
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12837335
37 X = -3917016
84
Y = -6015408
82 feet Y = -1877276
21 meter
Z = 16877770
03 Z = 5125325
37
XDOT = 15195
078262 XDOT = 4691
498729
YDOT = -19691
655243 feet/sec YDOT = -5949
889249 meter/sec
ZDOT = 4546
971257 ZDOT = 1408
561589
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3047936
20 X = -929010
95
Y = 13937420
18 feet Y = 4248125
67 meter
Z = 16801781
07 Z = 5121182
87
XDOT = -21509
694677 XDOT = -6556
154938
YDOT = -10284
860334 feet/sec YDOT = -3134
825430 meter/sec
ZDOT = 4637
366655 ZDOT = 1413
469356
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
55009676
00016717 00000-0 10270-3 0 9056
2 25544 51
6445 136
6085 0009894 41
0639 319
1267 15
72250561 26369
Satellite: ISS
Catalog Number: 25544
Epoch time: 10186
55009676 = yrday
fracday
Element set: 905
Inclination: 51
6445 deg
RA of node: 136
6085 deg
Eccentricity:
0009894
Arg of perigee: 41
0639 deg
Mean anomaly: 319
1267 deg
Mean motion: 15
72250561 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2636
Checksum: 319
Coasting Arc #7 (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 = -3085489
12 A = 6735812
99 meter
Y = 5710975
27 meter E =
0017392
Z = -1777918
65 I = 51
91475
XDOT = -5069
824597 Wp = 42
21351
YDOT = -974
935360 meter/sec RA = 130
77613 deg
ZDOT = 5711
414164 TA = 298
17600
MA = 298
35157
Ha = 196
111 n
mi
Hp = 183
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10122995
81 X = -3140484
13
Y = 18736795
50 feet Y = 5676164
25 meter
Z = -5833066
42 Z = -1793040
77
XDOT = -16633
282799 XDOT = -5086
290982
YDOT = -3198
606823 feet/sec YDOT = -1031
722043 meter/sec
ZDOT = 18738
235447 ZDOT = 5686
744748
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20582069
62 X = 6273414
82
Y = 5404915
82 feet Y = 1647418
34 meter
Z = -5893429
27 Z = -1796317
24
XDOT = 1218
662631 XDOT = 371
448370
YDOT = 15525
617998 feet/sec YDOT = 4732
208366 meter/sec
ZDOT = 18639
677237 ZDOT = 5681
373622
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
50351375
00016717 00000-0 10270-3 0 9069
2 25544 51
6442 131
7254 0010017 44
6865 315
5103 15
72229699 26513
Satellite: ISS
Catalog Number: 25544
Epoch time: 10187
50351375 = yrday
fracday
Element set: 906
Inclination: 51
6442 deg
RA of node: 131
7254 deg
Eccentricity:
0010017
Arg of perigee: 44
6865 deg
Mean anomaly: 315
5103 deg
Mean motion: 15
72229699 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2651
Checksum: 296
Coasting Arc #8 (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 = 4743016
94 A = 6727315
63 meter
Y = -167954
27 meter E =
0021032
Z = -4787751
81 I = 51
90615
XDOT = -2388
505523 Wp = 60
99451
YDOT = 6820
317778 meter/sec RA = 125
70928 deg
ZDOT = -2604
060419 TA = 183
48211
MA = 183
49677
Ha = 196
120 n
mi
Hp = 183
511
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15561079
20 X = 4767800
61
Y = -551031
06 feet Y = -114775
67 meter
Z = -15707847
16 Z = -4764650
01
XDOT = -7836
304208 XDOT = -2451
943953
YDOT = 22376
370664 feet/sec YDOT = 6793
253805 meter/sec
ZDOT = -8543
505311 ZDOT = -2615
816791
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4471980
56 X = -1363059
67
Y = -15011436
23 feet Y = -4575485
76 meter
Z = -15615551
72 Z = -4759620
16
XDOT = 22520
459011 XDOT = 6864
235907
YDOT = 2231
937306 feet/sec YDOT = 680
294491 meter/sec
ZDOT = -8590
429059 ZDOT = -2618
362777
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
52047722
00016717 00000-0 10270-3 0 9071
2 25544 51
6451 126
5164 0010018 48
5335 311
6686 15
72270949 26675
Satellite: ISS
Catalog Number: 25544
Epoch time: 10188
52047722 = yrday
fracday
Element set: 907
Inclination: 51
6451 deg
RA of node: 126
5164 deg
Eccentricity:
0010018
Arg of perigee: 48
5335 deg
Mean anomaly: 311
6686 deg
Mean motion: 15
72270949 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2667
Checksum: 310
Coasting Arc #9 (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 = 1064083
27 A = 6733738
41 meter
Y = -6044963
22 meter E =
0021551
Z = 2756267
36 I = 51
94536
XDOT = 5529
687750 Wp = 80
27974
YDOT = -1401
868413 meter/sec RA = 120
56443 deg
ZDOT = -5171
698195 TA = 68
37191
MA = 68
14248
Ha = 196
130 n
mi
Hp = 183
269
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3491086
84 X = 1118210
62
Y = -19832556
50 feet Y = -6032761
87 meter
Z = 9042871
91 Z = 2761567
05
XDOT = 18142
020178 XDOT = 5570
075885
YDOT = -4599
305816 feet/sec YDOT = -1339
805380 meter/sec
ZDOT = -16967
513762 ZDOT = -5144
737122
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20027634
34 X = -6104422
95
Y = 2007229
73 feet Y = 611803
62 meter
Z = 9064017
25 Z = 2762712
46
XDOT = -9177
352094 XDOT = -2797
256918
YDOT = -14879
653693 feet/sec YDOT = -4535
318446 meter/sec
ZDOT = -16859
793810 ZDOT = -5138
865153
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
53742656
00016717 00000-0 10270-3 0 9082
2 25544 51
6457 121
3080 0010006 52
0868 308
1198 15
72290805 26839
Satellite: ISS
Catalog Number: 25544
Epoch time: 10189
53742656 = yrday
fracday
Element set: 908
Inclination: 51
6457 deg
RA of node: 121
3080 deg
Eccentricity:
0010006
Arg of perigee: 52
0868 deg
Mean anomaly: 308
1198 deg
Mean motion: 15
72290805 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2683
Checksum: 305
Coasting Arc #10 (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 = -4726832
77 A = 6729435
44 meter
Y = 2285667
87 meter E =
0018370
Z = 4191955
35 I = 51
94569
XDOT = 19
457714 Wp = 81
32503
YDOT = -6763
325763 meter/sec RA = 115
51183 deg
ZDOT = 3698
693641 TA = 331
08235
MA = 331
18401
Ha = 196
255 n
mi
Hp = 183
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15507981
53 X = -4772403
88
Y = 7498910
34 feet Y = 2232553
98 meter
Z = 13753134
34 Z = 4168882
25
XDOT = 63
837645 XDOT = 77
117507
YDOT = -22189
388985 feet/sec YDOT = -6762
786508 meter/sec
ZDOT = 12134
821657 ZDOT = 3698
926894
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11627532
44 X = 3544071
89
Y = 12808554
74 feet Y = 3904047
48 meter
Z = 13660939
44 Z = 4163854
34
XDOT = -20334
303729 XDOT = -6197
895776
YDOT = 5477
426018 feet/sec YDOT = 1669
519450 meter/sec
ZDOT = 12135
729530 ZDOT = 3698
970361
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
55436168
00016717 00000-0 10270-3 0 9095
2 25544 51
6460 116
0997 0009948 56
1972 304
0136 15
72312601 26998
Satellite: ISS
Catalog Number: 25544
Epoch time: 10190
55436168 = yrday
fracday
Element set: 909
Inclination: 51
6460 deg
RA of node: 116
0997 deg
Eccentricity:
0009948
Arg of perigee: 56
1972 deg
Mean anomaly: 304
0136 deg
Mean motion: 15
72312601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2699
Checksum: 317
Coasting Arc #11 (Orbit 2713)
---------------------------------------
Vector Time (GMT): 2010/191/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 983528
13 A = 6731143
87 meter
Y = 5570768
72 meter E =
0014694
Z = -3656375
45 I = 51
96441
XDOT = -5064
180169 Wp = 74
04226
YDOT = 3766
035876 meter/sec RA = 110
36096 deg
ZDOT = 4394
090030 TA = 242
39087
MA = 242
54015
Ha = 196
152 n
mi
Hp = 183
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3226798
31 X = 938923
50
Y = 18276800
26 feet Y = 5581518
45 meter
Z = -11995982
43 Z = -3651704
75
XDOT = -16614
764335 XDOT = -5127
261754
YDOT = 12355
760747 feet/sec YDOT = 3709
051613 meter/sec
ZDOT = 14416
305872 ZDOT = 4369
336017
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16434663
55 X = 5009285
45
Y = -8648891
81 feet Y = -2636182
22 meter
Z = -11977301
63 Z = -3650681
54
XDOT = 16181
326486 XDOT = 4932
068313
YDOT = 11004
591677 feet/sec YDOT = 3354
199543 meter/sec
ZDOT = 14317
382441 ZDOT = 4363
938168
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
50772609
00016717 00000-0 10270-3 0 9106
2 25544 51
6467 111
2167 0009969 59
3653 300
8491 15
72332388 27145
Satellite: ISS
Catalog Number: 25544
Epoch time: 10191
50772609 = yrday
fracday
Element set: 910
Inclination: 51
6467 deg
RA of node: 111
2167 deg
Eccentricity:
0009969
Arg of perigee: 59
3653 deg
Mean anomaly: 300
8491 deg
Mean motion: 15
72332388 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2714
Checksum: 315
Coasting Arc #12 (Orbit 2729)
---------------------------------------
Vector Time (GMT): 2010/192/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3967528
52 A = 6731683
35 meter
Y = -4195290
65 meter E =
0014709
Z = -3476943
47 I = 51
97680
XDOT = 2125
112187 Wp = 71
03396
YDOT = 5795
136575 meter/sec RA = 105
31272 deg
ZDOT = -4578
483884 TA = 149
87266
MA = 149
78798
Ha = 196
143 n
mi
Hp = 183
007
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13016825
85 X = 4031036
23
Y = -13764076
94 feet Y = -4150567
64 meter
Z = -11407294
85 Z = -3457516
05
XDOT = 6972
152843 XDOT = 2082
393052
YDOT = 19012
915272 feet/sec YDOT = 5818
662846 meter/sec
ZDOT = -15021
272584 ZDOT = -4568
262937
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17206694
46 X = -5244600
47
Y = -8036334
42 feet Y = -2449474
73 meter
Z = -11329648
71 Z = -3453276
93
XDOT = 15200
445671 XDOT = 4633
095841
YDOT = -11477
723024 feet/sec YDOT = -3498
409978 meter/sec
ZDOT = -14980
407971 ZDOT = -4566
028350
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
52463406
00016717 00000-0 10270-3 0 9112
2 25544 51
6476 106
0079 0009985 62
9275 297
2905 15
72359338 27308
Satellite: ISS
Catalog Number: 25544
Epoch time: 10192
52463406 = yrday
fracday
Element set: 911
Inclination: 51
6476 deg
RA of node: 106
0079 deg
Eccentricity:
0009985
Arg of perigee: 62
9275 deg
Mean anomaly: 297
2905 deg
Mean motion: 15
72359338 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2730
Checksum: 324
Coasting Arc #13 (Orbit 2745)
---------------------------------------
Vector Time (GMT): 2010/193/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2644623
80 A = 6728734
34 meter
Y = -4413677
42 meter E =
0019650
Z = 4324619
96 I = 51
97339
XDOT = 3801
065356 Wp = 68
94560
YDOT = -5719
743028 meter/sec RA = 100
16419 deg
ZDOT = -3493
520959 TA = 56
28878
MA = 56
10162
Ha = 196
204 n
mi
Hp = 182
863
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8676587
28 X = -2616080
49
Y = -14480568
97 feet Y = -4443092
29 meter
Z = 14188385
68 Z = 4311841
25
XDOT = 12470
686864 XDOT = 3881
712600
YDOT = -18765
561114 feet/sec YDOT = -5676
785755 meter/sec
ZDOT = -11461
682937 ZDOT = -3474
860805
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10725466
49 X = -3269122
19
Y = 13091277
90 feet Y = 3990221
50 meter
Z = 14137296
22 Z = 4309047
89
XDOT = -20920
198823 XDOT = -6376
476601
YDOT = -4773
095012 feet/sec YDOT = -1454
839360 meter/sec
ZDOT = -11387
096559 ZDOT = -3470
787031
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
54152835
00016717 00000-0 10270-3 0 9127
2 25544 51
6471 100
7995 0009966 66
5534 293
6676 15
72373703 27462
Satellite: ISS
Catalog Number: 25544
Epoch time: 10193
54152835 = yrday
fracday
Element set: 912
Inclination: 51
6471 deg
RA of node: 100
7995 deg
Eccentricity:
0009966
Arg of perigee: 66
5534 deg
Mean anomaly: 293
6676 deg
Mean motion: 15
72373703 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2746
Checksum: 333
Coasting Arc #14 (Orbit 2761)
---------------------------------------
Vector Time (GMT): 2010/194/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2536715
84 A = 6733923
35 meter
Y = 5662237
41 meter E =
0023696
Z = 2587829
93 I = 51
99552
XDOT = -3783
647988 Wp = 73
89548
YDOT = -4129
686747 meter/sec RA = 95
11145 deg
ZDOT = 5293
661487 TA = 315
34887
MA = 315
53946
Ha = 196
198 n
mi
Hp = 182
799
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8322558
53 X = -2612414
41
Y = 18576894
38 feet Y = 5633446
74 meter
Z = 8490255
68 Z = 2575323
72
XDOT = -12413
543268 XDOT = -3762
902951
YDOT = -13548
841035 feet/sec YDOT = -4171
882471 meter/sec
ZDOT = 17367
655796 ZDOT = 5275
330766
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20332523
51 X = 6197353
17
Y = 1341955
12 feet Y = 409027
92 meter
Z = 8440264
87 Z = 2572592
73
XDOT = -8213
591002 XDOT = -2503
502537
YDOT = 14983
272758 feet/sec YDOT = 4566
901537 meter/sec
ZDOT = 17294
367481 ZDOT = 5271
323208
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
55840866
00016717 00000-0 10270-3 0 9138
2 25544 51
6476 95
5904 0009965 70
1246 290
0989 15
72380045 27621
Satellite: ISS
Catalog Number: 25544
Epoch time: 10194
55840866 = yrday
fracday
Element set: 913
Inclination: 51
6476 deg
RA of node: 95
5904 deg
Eccentricity:
0009965
Arg of perigee: 70
1246 deg
Mean anomaly: 290
0989 deg
Mean motion: 15
72380045 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2762
Checksum: 333
Coasting Arc #15 (Orbit 2776)
---------------------------------------
Vector Time (GMT): 2010/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3802023
90 A = 6726571
67 meter
Y = 2710752
60 meter E =
0020841
Z = -4859903
93 I = 51
97293
XDOT = -1904
821961 Wp = 92
13362
YDOT = 7031
764142 meter/sec RA = 89
97143 deg
ZDOT = 2440
171232 TA = 201
60055
MA = 201
68860
Ha = 196
081 n
mi
Hp = 182
829
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12473831
69 X = 3795037
25
Y = 8893545
26 feet Y = 2753230
55 meter
Z = -15944566
70 Z = -4841450
76
XDOT = -6249
415881 XDOT = -1995
164525
YDOT = 23070
092331 feet/sec YDOT = 7009
957895 meter/sec
ZDOT = 8005
811128 ZDOT = 2430
699101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3675792
07 X = 1120381
42
Y = -14950835
37 feet Y = -4557014
62 meter
Z = -15870787
82 Z = -4837416
13
XDOT = 22683
904075 XDOT = 6914
053962
YDOT = -2852
539935 feet/sec YDOT = -869
454172 meter/sec
ZDOT = 7967
947918 ZDOT = 2428
630525
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
51171992
00016717 00000-0 10270-3 0 9143
2 25544 51
6479 90
7069 0009830 73
3725 286
8516 15
72415368 27773
Satellite: ISS
Catalog Number: 25544
Epoch time: 10195
51171992 = yrday
fracday
Element set: 914
Inclination: 51
6479 deg
RA of node: 90
7069 deg
Eccentricity:
0009830
Arg of perigee: 73
3725 deg
Mean anomaly: 286
8516 deg
Mean motion: 15
72415368 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2777
Checksum: 340
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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