Date:
May 8th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19375 04 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 1706)
---------------------------------------
Vector Time (GMT): 2010/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2959333
73 A = 6730629
48 meter
Y = -5585375
30 meter E =
0003841
Z = 2306971
82 I = 51
98723
XDOT = 3525
219770 Wp = 110
55286
YDOT = -4125
342976 meter/sec RA = 78
65932 deg
ZDOT = -5459
780159 TA = 43
65155
MA = 43
62117
Ha = 189
392 n
mi
Hp = 187
262
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9709100
18 X = -2907864
03
Y = -18324722
10 feet Y = -5618180
59 meter
Z = 7568805
20 Z = 2292720
21
XDOT = 11565
681660 XDOT = 3597
610861
YDOT = -13534
589816 feet/sec YDOT = -4085
516994 meter/sec
ZDOT = -17912
664563 ZDOT = -5442
478797
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19794950
85 X = -6033501
02
Y = -6251331
33 feet Y = -1905405
79 meter
Z = 7511967
51 Z = 2289647
70
XDOT = -1602
393448 XDOT = -488
409523
YDOT = -16391
811502 feet/sec YDOT = -4996
224146 meter/sec
ZDOT = -17843
817569 ZDOT = -5438
795595
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10127
53628857
00016717 00000-0 10270-3 0 9002
2 25544 51
6431 79
2154 0010157 286
4773 73
5273 15
73742904 17075
Satellite: ISS
Catalog Number: 25544
Epoch time: 10127
53628857 = yrday
fracday
Element set: 900
Inclination: 51
6431 deg
RA of node: 79
2154 deg
Eccentricity:
0010157
Arg of perigee: 286
4773 deg
Mean anomaly: 73
5273 deg
Mean motion: 15
73742904 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1707
Checksum: 311
Coasting Arc #2 (Orbit 1722)
---------------------------------------
Vector Time (GMT): 2010/128/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2713337
16 A = 6722996
34 meter
Y = 3921326
72 meter E =
0002988
Z = 4741814
46 I = 51
95577
XDOT = -3974
170282 Wp = 265
07265
YDOT = -6014
076650 meter/sec RA = 73
59016 deg
ZDOT = 2700
563323 TA = 158
48028
MA = 158
46772
Ha = 189
597 n
mi
Hp = 186
993
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8902024
82 X = -2780019
56
Y = 12865245
15 feet Y = 3890611
66 meter
Z = 15557134
05 Z = 4728471
04
XDOT = -13038
616411 XDOT = -3919
743387
YDOT = -19731
222606 feet/sec YDOT = -6058
213913 meter/sec
ZDOT = 8860
115888 ZDOT = 2681
388747
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2855105
43 X = 870236
14
Y = 15435609
23 feet Y = 4704773
69 meter
Z = 15504042
67 Z = 4725632
21
XDOT = -22117
710603 XDOT = -6741
478192
YDOT = -4727
572071 feet/sec YDOT = -1440
963967 meter/sec
ZDOT = 8783
672445 ZDOT = 2677
263361
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10128
55227278
00016717 00000-0 10270-3 0 9018
2 25544 51
6437 74
0003 0010275 289
4751 70
5302 15
73814641 17233
Satellite: ISS
Catalog Number: 25544
Epoch time: 10128
55227278 = yrday
fracday
Element set: 901
Inclination: 51
6437 deg
RA of node: 74
0003 deg
Eccentricity:
0010275
Arg of perigee: 289
4751 deg
Mean anomaly: 70
5302 deg
Mean motion: 15
73814641 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1723
Checksum: 285
Coasting Arc #3 (Orbit 1737)
---------------------------------------
Vector Time (GMT): 2010/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3951446
85 A = 6730267
72 meter
Y = 4879303
11 meter E =
0009672
Z = -2405824
74 I = 51
97012
XDOT = -2645
427654 Wp = 326
29076
YDOT = 4808
722557 meter/sec RA = 68
43717 deg
ZDOT = 5405
263113 TA = 6
69262
MA = 6
67972
Ha = 189
921 n
mi
Hp = 186
758
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12964064
46 X = 3908279
13
Y = 16008212
30 feet Y = 4923249
22 meter
Z = -7893125
79 Z = -2386733
15
XDOT = -8679
224587 XDOT = -2725
261167
YDOT = 15776
648810 feet/sec YDOT = 4778
693353 meter/sec
ZDOT = 17733
802865 ZDOT = 5392
217618
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20565297
27 X = 6268302
61
Y = 1610521
00 feet Y = 490886
80 meter
Z = -7817034
83 Z = -2382632
22
XDOT = 5491
483087 XDOT = 1673
804045
YDOT = 15739
534675 feet/sec YDOT = 4797
410169 meter/sec
ZDOT = 17681
903236 ZDOT = 5389
444106
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10129
50473829
00016717 00000-0 10270-3 0 9020
2 25544 51
6435 69
1103 0010288 294
0307 65
9779 15
73802472 17381
Satellite: ISS
Catalog Number: 25544
Epoch time: 10129
50473829 = yrday
fracday
Element set: 902
Inclination: 51
6435 deg
RA of node: 69
1103 deg
Eccentricity:
0010288
Arg of perigee: 294
0307 deg
Mean anomaly: 65
9779 deg
Mean motion: 15
73802472 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1738
Checksum: 315
Coasting Arc #4 (Orbit 1753)
---------------------------------------
Vector Time (GMT): 2010/130/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1898419
53 A = 6723001
06 meter
Y = -4422920
71 meter E =
0008540
Z = -4698799
34 I = 51
93520
XDOT = 5015
947705 Wp = 9
31784
YDOT = 5126
229187 meter/sec RA = 63
36701 deg
ZDOT = -2791
162025 TA = 233
21386
MA = 233
29226
Ha = 189
973 n
mi
Hp = 186
539
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6228410
53 X = 1970562
63
Y = -14510894
73 feet Y = -4401287
98 meter
Z = -15416008
33 Z = -4689401
52
XDOT = 16456
521343 XDOT = 4971
811677
YDOT = 16818
337227 feet/sec YDOT = 5182
073787 meter/sec
ZDOT = -9157
355726 ZDOT = -2766
901231
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6405873
05 X = -1952510
11
Y = -14473256
79 feet Y = -4411448
67 meter
Z = -15378624
93 Z = -4687404
88
XDOT = 22499
619906 XDOT = 6857
884148
YDOT = -304
531530 feet/sec YDOT = -92
821210 meter/sec
ZDOT = -9060
684443 ZDOT = -2761
696618
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10130
52067637
00016717 00000-0 10270-3 0 9031
2 25544 51
6445 63
8946 0010226 297
9986 62
0142 15
73869740 17546
Satellite: ISS
Catalog Number: 25544
Epoch time: 10130
52067637 = yrday
fracday
Element set: 903
Inclination: 51
6445 deg
RA of node: 63
8946 deg
Eccentricity:
0010226
Arg of perigee: 297
9986 deg
Mean anomaly: 62
0142 deg
Mean motion: 15
73869740 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1754
Checksum: 321
Coasting Arc #5 (Orbit 1769)
---------------------------------------
Vector Time (GMT): 2010/131/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4775897
45 A = 6729905
02 meter
Y = -4054308
01 meter E =
0004930
Z = 2457426
36 I = 51
94455
XDOT = 1689
835870 Wp = 70
15113
YDOT = -5250
426245 meter/sec RA = 58
21178 deg
ZDOT = -5367
838054 TA = 82
21859
MA = 82
16263
Ha = 190
135 n
mi
Hp = 186
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15668954
90 X = -4742144
47
Y = -13301535
45 feet Y = -4107526
31 meter
Z = 8062422
46 Z = 2434306
42
XDOT = 5544
080938 XDOT = 1774
498005
YDOT = -17225
807889 feet/sec YDOT = -5231
055917 meter/sec
ZDOT = -17611
017237 ZDOT = -5359
423217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20381538
63 X = -6212292
97
Y = 2918326
18 feet Y = 889505
82 meter
Z = 7970313
94 Z = 2429351
69
XDOT = -8916
879849 XDOT = -2717
864978
YDOT = -14175
550665 feet/sec YDOT = -4320
707843 meter/sec
ZDOT = -17577
547394 ZDOT = -5357
636446
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10131
53658987
00016717 00000-0 10270-3 0 9048
2 25544 51
6451 58
6791 0010267 301
6423 58
3738 15
73896935 17700
Satellite: ISS
Catalog Number: 25544
Epoch time: 10131
53658987 = yrday
fracday
Element set: 904
Inclination: 51
6451 deg
RA of node: 58
6791 deg
Eccentricity:
0010267
Arg of perigee: 301
6423 deg
Mean anomaly: 58
3738 deg
Mean motion: 15
73896935 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1770
Checksum: 332
Coasting Arc #6 (Orbit 1785)
---------------------------------------
Vector Time (GMT): 2010/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1060136
66 A = 6722820
21 meter
Y = 4705936
77 meter E =
0002623
Z = 4682773
71 I = 51
90463
XDOT = -5857
575870 Wp = 327
91815
YDOT = -4124
765979 meter/sec RA = 53
13960 deg
ZDOT = 2821
959033 TA = 94
34175
MA = 94
31178
Ha = 190
290 n
mi
Hp = 185
979
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3478138
64 X = -1135429
08
Y = 15439425
11 feet Y = 4693660
43 meter
Z = 15363430
81 Z = 4677440
85
XDOT = -19217
768601 XDOT = -5824
725515
YDOT = -13532
696781 feet/sec YDOT = -4190
085374 meter/sec
ZDOT = 9258
395779 ZDOT = 2793
581834
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9395513
16 X = 2863752
41
Y = 12761225
79 feet Y = 3889621
62 meter
Z = 15342221
19 Z = 4676309
02
XDOT = -21888
303413 XDOT = -6671
554880
YDOT = 5131
753099 feet/sec YDOT = 1564
158345 meter/sec
ZDOT = 9145
358354 ZDOT = 2787
505226
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10132
55247810
00016717 00000-0 10270-3 0 9051
2 25544 51
6454 53
4631 0010265 305
0259 54
9940 15
73944630 17862
Satellite: ISS
Catalog Number: 25544
Epoch time: 10132
55247810 = yrday
fracday
Element set: 905
Inclination: 51
6454 deg
RA of node: 53
4631 deg
Eccentricity:
0010265
Arg of perigee: 305
0259 deg
Mean anomaly: 54
9940 deg
Mean motion: 15
73944630 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1786
Checksum: 297
Coasting Arc #7 (Orbit 1800)
---------------------------------------
Vector Time (GMT): 2010/133/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5417409
76 A = 6729675
54 meter
Y = 3122680
25 meter E =
0010919
Z = -2467947
13 I = 51
90926
XDOT = -718
437473 Wp = 338
18910
YDOT = 5483
748422 meter/sec RA = 47
98106 deg
ZDOT = 5363
900145 TA = 354
00578
MA = 354
01884
Ha = 190
516 n
mi
Hp = 185
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17773654
06 X = 5394077
86
Y = 10245013
93 feet Y = 3183130
70 meter
Z = -8096939
41 Z = -2441685
16
XDOT = -2357
078323 XDOT = -805
761787
YDOT = 17991
300597 feet/sec YDOT = 5475
225708 meter/sec
ZDOT = 17598
097590 ZDOT = 5360
198254
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19258035
28 X = 5869849
15
Y = -7188472
26 feet Y = -2191046
35 meter
Z = -7992337
62 Z = -2436064
51
XDOT = 11761
421914 XDOT = 3584
881400
YDOT = 11968
203190 feet/sec YDOT = 3647
908332 meter/sec
ZDOT = 17583
376441 ZDOT = 5359
413139
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10133
50485196
00016717 00000-0 10270-3 0 9069
2 25544 51
6459 48
5733 0010330 308
8729 51
1512 15
73970655 18019
Satellite: ISS
Catalog Number: 25544
Epoch time: 10133
50485196 = yrday
fracday
Element set: 906
Inclination: 51
6459 deg
RA of node: 48
5733 deg
Eccentricity:
0010330
Arg of perigee: 308
8729 deg
Mean anomaly: 51
1512 deg
Mean motion: 15
73970655 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1801
Checksum: 302
Coasting Arc #8 (Orbit 1816)
---------------------------------------
Vector Time (GMT): 2010/134/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 214064
82 A = 6722569
65 meter
Y = -4822959
11 meter E =
0011062
Z = -4685464
43 I = 51
86573
XDOT = 6493
444943 Wp = 14
71142
YDOT = 3025
326266 meter/sec RA = 42
90626 deg
ZDOT = -2808
407437 TA = 227
59419
MA = 227
68784
Ha = 190
545 n
mi
Hp = 185
393
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 702312
40 X = 290741
72
Y = -15823356
67 feet Y = -4820136
07 meter
Z = -15372258
61 Z = -4684238
76
XDOT = 21303
953226 XDOT = 6472
775607
YDOT = 9925
611110 feet/sec YDOT = 3097
824575 meter/sec
ZDOT = -9213
935160 ZDOT = -2776
911490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11862429
15 X = -3615668
40
Y = -10502589
50 feet Y = -3201189
28 meter
Z = -15367386
98 Z = -4683979
55
XDOT = 20325
266312 XDOT = 6195
141172
YDOT = -9615
266206 feet/sec YDOT = -2930
733140 meter/sec
ZDOT = -9088
492256 ZDOT = -2770
172440
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10134
52069283
00016717 00000-0 10270-3 0 9078
2 25544 51
6467 43
3575 0010331 313
1158 46
9141 15
74027666 18174
Satellite: ISS
Catalog Number: 25544
Epoch time: 10134
52069283 = yrday
fracday
Element set: 907
Inclination: 51
6467 deg
RA of node: 43
3575 deg
Eccentricity:
0010331
Arg of perigee: 313
1158 deg
Mean anomaly: 46
9141 deg
Mean motion: 15
74027666 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1817
Checksum: 296
Coasting Arc #9 (Orbit 1832)
---------------------------------------
Vector Time (GMT): 2010/135/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5895743
45 A = 6729611
25 meter
Y = -2156706
43 meter E =
0007234
Z = 2424820
99 I = 51
86591
XDOT = -206
598509 Wp = 59
84142
YDOT = -5500
141467 meter/sec RA = 37
74466 deg
ZDOT = -5378
880052 TA = 92
89553
MA = 92
81274
Ha = 190
706 n
mi
Hp = 185
262
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19342990
33 X = -5882968
13
Y = -7075808
49 feet Y = -2222565
02 meter
Z = 7955449
45 Z = 2396209
73
XDOT = -677
816629 XDOT = -118
949512
YDOT = -18045
083554 feet/sec YDOT = -5501
961002 meter/sec
ZDOT = -17647
244266 ZDOT = -5379
671538
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17449124
86 X = -5318493
26
Y = 11024812
53 feet Y = 3360362
86 meter
Z = 7841496
48 Z = 2390088
13
XDOT = -13831
258594 XDOT = -4215
767619
YDOT = -9300
387196 feet/sec YDOT = -2834
758017 meter/sec
ZDOT = -17650
398367 ZDOT = -5379
841422
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10135
53651000
00016717 00000-0 10270-3 0 9085
2 25544 51
6463 38
1413 0010300 316
4705 43
5644 15
74029156 18338
Satellite: ISS
Catalog Number: 25544
Epoch time: 10135
53651000 = yrday
fracday
Element set: 908
Inclination: 51
6463 deg
RA of node: 38
1413 deg
Eccentricity:
0010300
Arg of perigee: 316
4705 deg
Mean anomaly: 43
5644 deg
Mean motion: 15
74029156 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1833
Checksum: 267
Coasting Arc #10 (Orbit 1848)
---------------------------------------
Vector Time (GMT): 2010/136/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 553225
47 A = 6722260
15 meter
Y = 4758378
26 meter E =
0004347
Z = 4714031
88 I = 51
81763
XDOT = -6945
352963 Wp = 1
17955
YDOT = -1897
834466 meter/sec RA = 32
66455 deg
ZDOT = 2734
987930 TA = 61
98584
MA = 61
94187
Ha = 190
849 n
mi
Hp = 184
829
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1815044
20 X = 477075
13
Y = 15611477
24 feet Y = 4764138
32 meter
Z = 15465983
86 Z = 4716535
18
XDOT = -22786
591086 XDOT = -6936
901072
YDOT = -6226
491030 feet/sec YDOT = -1975
454662 meter/sec
ZDOT = 8973
057512 ZDOT = 2701
267260
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13550150
43 X = 4130085
85
Y = 7943403
41 feet Y = 2421149
36 meter
Z = 15475950
02 Z = 4717069
57
XDOT = -18057
106403 XDOT = -5503
806032
YDOT = 13609
053401 feet/sec YDOT = 4148
039477 meter/sec
ZDOT = 8838
751498 ZDOT = 2694
051457
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10136
55230142
00016717 00000-0 10270-3 0 9099
2 25544 51
6468 32
9244 0010391 320
4547 39
5857 15
74080114 18495
Satellite: ISS
Catalog Number: 25544
Epoch time: 10136
55230142 = yrday
fracday
Element set: 909
Inclination: 51
6468 deg
RA of node: 32
9244 deg
Eccentricity:
0010391
Arg of perigee: 320
4547 deg
Mean anomaly: 39
5857 deg
Mean motion: 15
74080114 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1849
Checksum: 298
Coasting Arc #11 (Orbit 1863)
---------------------------------------
Vector Time (GMT): 2010/137/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6193330
09 A = 6729480
56 meter
Y = 1142163
33 meter E =
0012774
Z = -2347992
67 I = 51
81637
XDOT = 1064
821914 Wp = 349
95478
YDOT = 5365
923195 meter/sec RA = 27
49954 deg
ZDOT = 5426
825359 TA = 343
65812
MA = 343
69927
Ha = 191
031 n
mi
Hp = 184
546
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20319324
43 X = 6191504
10
Y = 3747255
02 feet Y = 1211410
95 meter
Z = -7703388
03 Z = -2317909
55
XDOT = 3493
510217 XDOT = 978
377344
YDOT = 17604
734892 feet/sec YDOT = 5377
346578 meter/sec
ZDOT = 17804
545141 ZDOT = 5431
789068
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14925139
69 X = 4549182
58
Y = -14352309
74 feet Y = -4374584
01 meter
Z = -7583565
32 Z = -2311470
71
XDOT = 15228
315732 XDOT = 4641
590635
YDOT = 6431
930824 feet/sec YDOT = 1960
452515 meter/sec
ZDOT = 17824
307138 ZDOT = 5432
848816
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10137
50458362
00016717 00000-0 10270-3 0 9103
2 25544 51
6470 28
0337 0010510 323
6795 36
3654 15
74129326 18646
Satellite: ISS
Catalog Number: 25544
Epoch time: 10137
50458362 = yrday
fracday
Element set: 910
Inclination: 51
6470 deg
RA of node: 28
0337 deg
Eccentricity:
0010510
Arg of perigee: 323
6795 deg
Mean anomaly: 36
3654 deg
Mean motion: 15
74129326 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1864
Checksum: 293
Coasting Arc #12 (Orbit 1879)
---------------------------------------
Vector Time (GMT): 2010/138/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1267695
47 A = 6721805
03 meter
Y = -4581648
76 meter E =
0013625
Z = -4761874
59 I = 51
76361
XDOT = 7196
514437 Wp = 22
20347
YDOT = 738
333532 meter/sec RA = 22
41451 deg
ZDOT = -2616
292153 TA = 222
08701
MA = 222
19174
Ha = 191
054 n
mi
Hp = 184
219
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4159105
89 X = -1193236
05
Y = -15031656
03 feet Y = -4595407
96 meter
Z = -15622948
12 Z = -4767852
78
XDOT = 23610
611670 XDOT = 7200
432899
YDOT = 2422
354108 feet/sec YDOT = 818
831477 meter/sec
ZDOT = -8583
635672 ZDOT = -2581
321784
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14672915
67 X = -4472304
70
Y = -5216326
30 feet Y = -1589936
26 meter
Z = -15646751
69 Z = -4769129
91
XDOT = 15083
553658 XDOT = 4597
467155
YDOT = -17001
210559 feet/sec YDOT = -5181
968978 meter/sec
ZDOT = -8444
341602 ZDOT = -2573
835320
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10138
52032769
00016717 00000-0 10270-3 0 9116
2 25544 51
6469 22
8169 0010636 327
3096 32
7408 15
74174989 18803
Satellite: ISS
Catalog Number: 25544
Epoch time: 10138
52032769 = yrday
fracday
Element set: 911
Inclination: 51
6469 deg
RA of node: 22
8169 deg
Eccentricity:
0010636
Arg of perigee: 327
3096 deg
Mean anomaly: 32
7408 deg
Mean motion: 15
74174989 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1880
Checksum: 323
Coasting Arc #13 (Orbit 1895)
---------------------------------------
Vector Time (GMT): 2010/139/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6355787
70 A = 6729612
95 meter
Y = -151108
32 meter E =
0009404
Z = 2208187
87 I = 51
76131
XDOT = -1793
879107 Wp = 60
35592
YDOT = -5086
268250 meter/sec RA = 17
24667 deg
ZDOT = -5489
371743 TA = 94
95255
MA = 94
84518
Ha = 191
208 n
mi
Hp = 184
084
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20852321
85 X = -6364352
58
Y = -495762
22 feet Y = -222230
64 meter
Z = 7244710
86 Z = 2177290
62
XDOT = -5885
430140 XDOT = -1710
203830
YDOT = -16687
231791 feet/sec YDOT = -5105
860051 meter/sec
ZDOT = -18009
749812 ZDOT = -5497
883692
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12012707
51 X = -3661473
25
Y = 17103451
98 feet Y = 5213132
16 meter
Z = 7121638
23 Z = 2170675
33
XDOT = -15840
913267 XDOT = -4828
310364
YDOT = -3582
293814 feet/sec YDOT = -1091
883154 meter/sec
ZDOT = -18043
645416 ZDOT = -5499
703123
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 10139
53604912
00016717 00000-0 10270-3 0 9124
2 25544 51
6468 17
5997 0010519 331
3516 28
7068 15
74181233 18968
Satellite: ISS
Catalog Number: 25544
Epoch time: 10139
53604912 = yrday
fracday
Element set: 912
Inclination: 51
6468 deg
RA of node: 17
5997 deg
Eccentricity:
0010519
Arg of perigee: 331
3516 deg
Mean anomaly: 28
7068 deg
Mean motion: 15
74181233 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1896
Checksum: 316
Coasting Arc #14 (Orbit 1911)
---------------------------------------
Vector Time (GMT): 2010/140/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1840429
54 A = 6721358
77 meter
Y = 4295594
17 meter E =
0006216
Z = 4827450
03 I = 51
70492
XDOT = -7297
823421 Wp = 12
33552
YDOT = 395
572123 meter/sec RA = 12
15417 deg
ZDOT = 2435
636324 TA = 53
93713
MA = 53
87956
Ha = 191
322 n
mi
Hp = 183
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6038154
66 X = 1768807
75
Y = 14093156
71 feet Y = 4315774
10 meter
Z = 15838090
64 Z = 4836217
22
XDOT = -23942
990226 XDOT = -7313
536277
YDOT = 1297
808803 feet/sec YDOT = 313
875466 meter/sec
ZDOT = 7990
932820 ZDOT = 2400
145331
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15069731
15 X = 4593254
05
Y = 2621528
51 feet Y = 799041
89 meter
Z = 15873004
89 Z = 4838091
89
XDOT = -11690
677322 XDOT = -3563
318448
YDOT = 19782
005355 feet/sec YDOT = 6029
555232 meter/sec
ZDOT = 7849
562015 ZDOT = 2392
546502
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 10140
55174491
00016717 00000-0 10270-3 0 9133
2 25544 51
6469 12
3817 0010656 335
0689 24
9958 15
74217258 19129
Satellite: ISS
Catalog Number: 25544
Epoch time: 10140
55174491 = yrday
fracday
Element set: 913
Inclination: 51
6469 deg
RA of node: 12
3817 deg
Eccentricity:
0010656
Arg of perigee: 335
0689 deg
Mean anomaly: 24
9958 deg
Mean motion: 15
74217258 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1912
Checksum: 316
Coasting Arc #15 (Orbit 1926)
---------------------------------------
Vector Time (GMT): 2010/141/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 808518
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6346523
80 A = 6729693
28 meter
Y = -846597
80 meter E =
0015208
Z = -2041329
24 I = 51
70292
XDOT = 2420
979510 Wp =
32775
YDOT = 4734
588955 meter/sec RA = 6
98374 deg
ZDOT = 5578
409398 TA = 336
90143
MA = 336
96973
Ha = 191
514 n
mi
Hp = 183
442
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20821928
48 X = 6365435
37
Y = -2777551
83 feet Y = -775521
32 meter
Z = -6697274
42 Z = -2010451
83
XDOT = 7942
846160 XDOT = 2340
757542
YDOT = 15533
428330 feet/sec YDOT = 4761
212899 meter/sec
ZDOT = 18301
868105 ZDOT = 5589
975996
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8616215
31 X = 2626222
43
Y = -19200536
89 feet Y = -5852323
64 meter
Z = -6574283
35 Z = -2003841
56
XDOT = 15931
919918 XDOT = 4856
049191
YDOT = 884
377044 feet/sec YDOT = 269
558123 meter/sec
ZDOT = 18347
931272 ZDOT = 5592
449452
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 10141
50393724
00016717 00000-0 10270-3 0 9142
2 25544 51
6465 7
4901 0010847 337
6923 22
3767 15
74257795 19271
Satellite: ISS
Catalog Number: 25544
Epoch time: 10141
50393724 = yrday
fracday
Element set: 914
Inclination: 51
6465 deg
RA of node: 7
4901 deg
Eccentricity:
0010847
Arg of perigee: 337
6923 deg
Mean anomaly: 22
3767 deg
Mean motion: 15
74257795 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1927
Checksum: 317
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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