Date:
June 20th 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 2359)
---------------------------------------
Vector Time (GMT): 2010/168/23:49:42
916
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4520243
48 A = 6727683
45 meter
Y = 973253
28 meter E =
0009781
Z = -4892135
65 I = 51
38931
XDOT = -3751
265792 Wp = 56
83140
YDOT = -6341
261124 meter/sec RA = 225
51407 deg
ZDOT = 2213
011875 TA = 234
72398
MA = 234
81552
Ha = 194
595 n
mi
Hp = 187
237
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14830195
13 X = -4507025
64
Y = 3193088
19 feet Y = 922779
71 meter
Z = -16050313
80 Z = -4914062
65
XDOT = -12307
302466 XDOT = -3690
828208
YDOT = -20804
662481 feet/sec YDOT = -6382
872351 meter/sec
ZDOT = 7260
537646 ZDOT = 2194
934380
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1313631
25 X = -400394
80
Y = -15019691
27 feet Y = -4578001
90 meter
Z = -16137729
70 Z = -4918780
01
XDOT = 21097
460322 XDOT = 6430
505906
YDOT = -9539
023175 feet/sec YDOT = -2907
494264 meter/sec
ZDOT = 7188
386138 ZDOT = 2191
020095
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 10169
00499183
00016717 00000-0 10270-3 0 9008
2 25544 51
6475 226
4313 0009681 336
3150 23
7565 15
71894561 23602
Satellite: ISS
Catalog Number: 25544
Epoch time: 10169
00499183 = yrday
fracday
Element set: 900
Inclination: 51
6475 deg
RA of node: 226
4313 deg
Eccentricity:
0009681
Arg of perigee: 336
3150 deg
Mean anomaly: 23
7565 deg
Mean motion: 15
71894561 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2360
Checksum: 304
Coasting Arc #2 (Orbit 2375)
---------------------------------------
Vector Time (GMT): 2010/169/23:49:42
916
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4297595
94 A = 6737536
97 meter
Y = 5024312
80 meter E =
0002794
Z = -1304627
25 I = 51
44417
XDOT = -4459
003993 Wp = 49
66463
YDOT = 2302
782071 meter/sec RA = 220
40899 deg
ZDOT = -5826
550674 TA = 144
66849
MA = 144
64997
Ha = 194
820 n
mi
Hp = 187
226
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14099724
22 X = 4247431
39
Y = 16483965
89 feet Y = 5072090
74 meter
Z = -4280273
14 Z = -1283870
85
XDOT = -14629
278191 XDOT = -4456
118421
YDOT = 7555
059288 feet/sec YDOT = 2252
935613 meter/sec
ZDOT = -19115
979903 ZDOT = -5848
205227
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17921640
59 X = -5462516
05
Y = 12249095
41 feet Y = 3733524
28 meter
Z = -4197446
00 Z = -1279381
54
XDOT = -5038
409628 XDOT = -1535
707255
YDOT = -13944
458977 feet/sec YDOT = -4250
271096 meter/sec
ZDOT = -19202
297960 ZDOT = -5852
860418
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 10170
02219117
00016717 00000-0 10270-3 0 9010
2 25544 51
6476 221
2246 0009586 339
6130 20
4648 15
71867183 23762
Satellite: ISS
Catalog Number: 25544
Epoch time: 10170
02219117 = yrday
fracday
Element set: 901
Inclination: 51
6476 deg
RA of node: 221
2246 deg
Eccentricity:
0009586
Arg of perigee: 339
6130 deg
Mean anomaly: 20
4648 deg
Mean motion: 15
71867183 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2376
Checksum: 296
Coasting Arc #3 (Orbit 2391)
---------------------------------------
Vector Time (GMT): 2010/170/23:49:42
916
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3083478
39 A = 6726160
50 meter
Y = -2916811
93 meter E =
0010765
Z = 5218932
36 I = 51
43036
XDOT = 5897
058136 Wp =
19294
YDOT = 4891
135905 meter/sec RA = 215
25613 deg
ZDOT = -739
919499 TA = 96
93072
MA = 96
80826
Ha = 194
840 n
mi
Hp = 186
838
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10116398
91 X = 3090512
83
Y = -9569592
95 feet Y = -2882291
92 meter
Z = 17122481
49 Z = 5233928
69
XDOT = 19347
303596 XDOT = 5845
520690
YDOT = 16047
033810 feet/sec YDOT = 4956
792252 meter/sec
ZDOT = -2427
557410 ZDOT = -711
396098
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8611490
08 X = 2624782
18
Y = 10849454
93 feet Y = 3306913
86 meter
Z = 17182245
92 Z = 5237148
56
XDOT = -16961
736064 XDOT = -5169
937152
YDOT = 17182
147055 feet/sec YDOT = 5237
118422 meter/sec
ZDOT = -2313
751978 ZDOT = -705
231603
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 10171
03937748
00016717 00000-0 10270-3 0 9020
2 25544 51
6476 216
0171 0009745 343
8703 16
2148 15
71932820 23928
Satellite: ISS
Catalog Number: 25544
Epoch time: 10171
03937748 = yrday
fracday
Element set: 902
Inclination: 51
6476 deg
RA of node: 216
0171 deg
Eccentricity:
0009745
Arg of perigee: 343
8703 deg
Mean anomaly: 16
2148 deg
Mean motion: 15
71932820 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2392
Checksum: 302
Coasting Arc #4 (Orbit 2406)
---------------------------------------
Vector Time (GMT): 2010/171/23:49:42
916
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5828411
75 A = 6738041
08 meter
Y = -3356446
60 meter E =
0019271
Z = -28434
49 I = 51
49501
XDOT = 2376
326353 Wp = 19
74170
YDOT = -4167
347809 meter/sec RA = 210
12935 deg
ZDOT = 6029
731715 TA = 339
94877
MA = 340
02438
Ha = 195
017 n
mi
Hp = 186
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19122085
80 X = -5790308
04
Y = -11011963
91 feet Y = -3421410
32 meter
Z = -93289
00 Z = -56657
00
XDOT = 7796
346304 XDOT = 2393
458244
YDOT = -13672
400948 feet/sec YDOT = -4140
679345 meter/sec
ZDOT = 19782
584368 ZDOT = 6041
317030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12405015
79 X = 3781048
81
Y = -18248271
49 feet Y = -5562073
15 meter
Z = -205883
94 Z = -62753
42
XDOT = 11731
387422 XDOT = 3575
726886
YDOT = 7771
341127 feet/sec YDOT = 2368
704775 meter/sec
ZDOT = 19828
734848 ZDOT = 6043
798382
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 10171
99298090
00016717 00000-0 10270-3 0 9036
2 25544 51
6469 211
1352 0009814 347
3474 12
7441 15
71942899 24079
Satellite: ISS
Catalog Number: 25544
Epoch time: 10171
99298090 = yrday
fracday
Element set: 903
Inclination: 51
6469 deg
RA of node: 211
1352 deg
Eccentricity:
0009814
Arg of perigee: 347
3474 deg
Mean anomaly: 12
7441 deg
Mean motion: 15
71942899 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2407
Checksum: 319
Coasting Arc #5 (Orbit 2422)
---------------------------------------
Vector Time (GMT): 2010/172/23:49:42
916
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -959470
25 A = 6726141
45 meter
Y = 4141563
76 meter E =
0017319
Z = -5224849
89 I = 51
48053
XDOT = -7170
271832 Wp = 49
33338
YDOT = -2658
384004 meter/sec RA = 205
00579 deg
ZDOT = -781
093586 TA = 213
15001
MA = 213
25865
Ha = 195
166 n
mi
Hp = 186
310
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3147868
29 X = -980329
10
Y = 13587807
62 feet Y = 4130718
60 meter
Z = -17141895
95 Z = -5229561
03
XDOT = -23524
513886 XDOT = -7136
217947
YDOT = -8721
732295 feet/sec YDOT = -2738
375727 meter/sec
ZDOT = -2562
642999 ZDOT = -815
844744
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13390405
16 X = -4081395
49
Y = -3819924
05 feet Y = -1164312
85 meter
Z = -17160635
70 Z = -5230561
76
XDOT = 9775
706177 XDOT = 2979
635243
YDOT = -21994
265177 feet/sec YDOT = -6703
852026 meter/sec
ZDOT = -2701
278380 ZDOT = -823
349650
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 10173
01014641
00016717 00000-0 10270-3 0 9040
2 25544 51
6456 205
9275 0009859 351
1382 8
9604 15
71963672 24238
Satellite: ISS
Catalog Number: 25544
Epoch time: 10173
01014641 = yrday
fracday
Element set: 904
Inclination: 51
6456 deg
RA of node: 205
9275 deg
Eccentricity:
0009859
Arg of perigee: 351
1382 deg
Mean anomaly: 8
9604 deg
Mean motion: 15
71963672 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2423
Checksum: 302
Coasting Arc #6 (Orbit 2438)
---------------------------------------
Vector Time (GMT): 2010/173/23:49:42
916
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6491258
66 A = 6737122
52 meter
Y = 1235406
08 meter E =
0011589
Z = 1313491
87 I = 51
54591
XDOT = 235
973057 Wp = 76
00312
YDOT = 5009
560650 meter/sec RA = 199
85809 deg
ZDOT = -5832
203793 TA = 89
58068
MA = 89
44788
Ha = 195
283 n
mi
Hp = 186
067
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21296780
39 X = 6470580
93
Y = 4053169
55 feet Y = 1307879
35 meter
Z = 4309356
54 Z = 1344976
61
XDOT = 774
189820 XDOT = 208
269670
YDOT = 16435
566438 feet/sec YDOT = 5012
045605 meter/sec
ZDOT = -19134
526881 ZDOT = -5831
123809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4903139
18 X = -1494476
82
Y = 21091276
40 feet Y = 6428621
05 meter
Z = 4434960
88 Z = 1351776
08
XDOT = -14919
296323 XDOT = -4547
401519
YDOT = 584
910791 feet/sec YDOT = 178
280809 meter/sec
ZDOT = -19130
160195 ZDOT = -5830
872828
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 10174
02730088
00016717 00000-0 10270-3 0 9053
2 25544 51
6457 200
7208 0009916 355
0922 5
0141 15
71985093 24397
Satellite: ISS
Catalog Number: 25544
Epoch time: 10174
02730088 = yrday
fracday
Element set: 905
Inclination: 51
6457 deg
RA of node: 200
7208 deg
Eccentricity:
0009916
Arg of perigee: 355
0922 deg
Mean anomaly: 5
0141 deg
Mean motion: 15
71985093 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2439
Checksum: 294
Coasting Arc #7 (Orbit 2454)
---------------------------------------
Vector Time (GMT): 2010/174/23:49:42
916
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1395754
96 A = 6727632
51 meter
Y = -4389713
91 meter E =
0008341
Z = 4896596
31 I = 51
54086
XDOT = 7376
105024 Wp = 40
47763
YDOT = 122
715007 meter/sec RA = 194
76075 deg
ZDOT = 2216
676594 TA = 27
98343
MA = 27
93861
Ha = 195
478 n
mi
Hp = 185
971
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4579248
57 X = -1370351
50
Y = -14401948
52 feet Y = -4405181
00 meter
Z = 16064948
52 Z = 4889876
54
XDOT = 24199
819632 XDOT = 7363
416345
YDOT = 402
608291 feet/sec YDOT = 205
127623 meter/sec
ZDOT = 7272
561005 ZDOT = 2252
479037
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14504730
17 X = 4421041
76
Y = -4342885
92 feet Y = -1323711
63 meter
Z = 16038090
72 Z = 4888410
05
XDOT = -1272
913373 XDOT = -387
983996
YDOT = 23083
157233 feet/sec YDOT = 7035
746325 meter/sec
ZDOT = 7415
394412 ZDOT = 2260
212217
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 10175
04444536
00016717 00000-0 10270-3 0 9067
2 25544 51
6443 195
5123 0009897 359
1884
9260 15
71946901 24558
Satellite: ISS
Catalog Number: 25544
Epoch time: 10175
04444536 = yrday
fracday
Element set: 906
Inclination: 51
6443 deg
RA of node: 195
5123 deg
Eccentricity:
0009897
Arg of perigee: 359
1884 deg
Mean anomaly:
9260 deg
Mean motion: 15
71946901 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2455
Checksum: 319
Coasting Arc #8 (Orbit 2469)
---------------------------------------
Vector Time (GMT): 2010/175/23:49:42
916
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6152475
84 A = 6734996
19 meter
Y = 998233
98 meter E =
0013667
Z = -2535260
06 I = 51
59475
XDOT = -2944
212217 Wp = 19
14810
YDOT = -4753
879179 meter/sec RA = 189
59519 deg
ZDOT = 5293
812493 TA = 312
11390
MA = 312
22999
Ha = 195
351 n
mi
Hp = 185
710
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20185288
18 X = -6150865
18
Y = 3275045
85 feet Y = 929442
85 meter
Z = -8317782
35 Z = -2565144
64
XDOT = -9659
488901 XDOT = -2916
551008
YDOT = -15596
716468 feet/sec YDOT = -4786
649546 meter/sec
ZDOT = 17368
151224 ZDOT = 5279
575730
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3159696
27 X = -963075
42
Y = -20154166
80 feet Y = -6142990
04 meter
Z = -8437011
76 Z = -2571601
18
XDOT = 14181
981376 XDOT = 4322
667923
YDOT = -9442
287755 feet/sec YDOT = -2878
009308 meter/sec
ZDOT = 17311
293279 ZDOT = 5276
482192
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 10175
99800495
00016717 00000-0 10270-3 0 9072
2 25544 51
6432 190
6295 0009774 2
1123 358
0078 15
72000756 24708
Satellite: ISS
Catalog Number: 25544
Epoch time: 10175
99800495 = yrday
fracday
Element set: 907
Inclination: 51
6432 deg
RA of node: 190
6295 deg
Eccentricity:
0009774
Arg of perigee: 2
1123 deg
Mean anomaly: 358
0078 deg
Mean motion: 15
72000756 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2470
Checksum: 304
Coasting Arc #9 (Orbit 2485)
---------------------------------------
Vector Time (GMT): 2010/176/23:49:42
916
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3641222
52 A = 6729896
55 meter
Y = 3702723
69 meter E =
0015663
Z = -4296227
66 I = 51
60667
XDOT = -6451
220678 Wp = 36
04758
YDOT = 2273
799560 meter/sec RA = 184
51883 deg
ZDOT = -3502
019229 TA = 198
37145
MA = 198
42809
Ha = 195
549 n
mi
Hp = 185
542
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11946268
10 X = 3620417
54
Y = 12148043
60 feet Y = 3743326
57 meter
Z = -14095235
09 Z = -4278588
46
XDOT = -21165
422173 XDOT = -6459
155170
YDOT = 7459
972309 feet/sec YDOT = 2201
614524 meter/sec
ZDOT = -11489
564398 ZDOT = -3533
377894
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12008558
55 X = -3660208
65
Y = 12168129
51 feet Y = 3708845
87 meter
Z = -14024802
42 Z = -4274759
78
XDOT = -6814
183267 XDOT = -2076
963060
YDOT = -20134
379660 feet/sec YDOT = -6136
958920 meter/sec
ZDOT = -11614
680059 ZDOT = -3540
154482
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
01512568
00016717 00000-0 10270-3 0 9089
2 25544 51
6423 185
4219 0009811 6
7477 353
3816 15
72026968 24868
Satellite: ISS
Catalog Number: 25544
Epoch time: 10177
01512568 = yrday
fracday
Element set: 908
Inclination: 51
6423 deg
RA of node: 185
4219 deg
Eccentricity:
0009811
Arg of perigee: 6
7477 deg
Mean anomaly: 353
3816 deg
Mean motion: 15
72026968 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2486
Checksum: 321
Coasting Arc #10 (Orbit 2501)
---------------------------------------
Vector Time (GMT): 2010/177/23:49:42
916
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4949938
89 A = 6732181
63 meter
Y = -2865090
49 meter E =
0017145
Z = 3549168
62 I = 51
64553
XDOT = 5224
345004 Wp = 53
20176
YDOT = 3469
979295 meter/sec RA = 179
34649 deg
ZDOT = -4460
196060 TA = 84
54620
MA = 84
35065
Ha = 195
521 n
mi
Hp = 185
278
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16239957
00 X = 4964367
92
Y = -9399903
17 feet Y = -2809657
35 meter
Z = 11644254
01 Z = 3573249
68
XDOT = 17140
239516 XDOT = 5206
821394
YDOT = 11384
446507 feet/sec YDOT = 3528
303940 meter/sec
ZDOT = -14633
189174 ZDOT = -4434
858308
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9859559
83 X = 3005193
84
Y = 15894548
18 feet Y = 4844658
29 meter
Z = 11740334
44 Z = 3578453
94
XDOT = -9726
030434 XDOT = -2964
494076
YDOT = 16826
942795 feet/sec YDOT = 5128
852164 meter/sec
ZDOT = -14532
021111 ZDOT = -4429
360035
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
03223340
00016717 00000-0 10270-3 0 9090
2 25544 51
6427 180
2132 0009760 9
4186 350
7158 15
72050494 25029
Satellite: ISS
Catalog Number: 25544
Epoch time: 10178
03223340 = yrday
fracday
Element set: 909
Inclination: 51
6427 deg
RA of node: 180
2132 deg
Eccentricity:
0009760
Arg of perigee: 9
4186 deg
Mean anomaly: 350
7158 deg
Mean motion: 15
72050494 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2502
Checksum: 283
Coasting Arc #11 (Orbit 2517)
---------------------------------------
Vector Time (GMT): 2010/178/23:49:42
916
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5340405
11 A = 6732616
36 meter
Y = -2197163
86 meter E =
0017441
Z = 3439504
23 I = 51
67650
XDOT = 4644
250043 Wp = 58
47494
YDOT = -4104
427358 meter/sec RA = 174
27818 deg
ZDOT = 4581
055678 TA = 342
23820
MA = 342
29910
Ha = 195
695 n
mi
Hp = 185
108
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17521014
14 X = -5332147
39
Y = -7208542
84 feet Y = -2256837
91 meter
Z = 11284462
68 Z = 3413580
51
XDOT = 15237
040825 XDOT = 4667
547670
YDOT = -13465
969023 feet/sec YDOT = -4052
363167 meter/sec
ZDOT = 15029
710230 ZDOT = 4603
672995
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6393700
31 X = 1948799
86
Y = -17899579
95 feet Y = -5455791
97 meter
Z = 11180955
17 Z = 3407955
14
XDOT = 12840
994655 XDOT = 3913
935171
YDOT = 14047
988454 feet/sec YDOT = 4281
826881 meter/sec
ZDOT = 15119
945423 ZDOT = 4608
559365
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
04933063
00016717 00000-0 10270-3 0 9104
2 25544 51
6421 175
0046 0009620 14
1426 346
0004 15
72073550 25187
Satellite: ISS
Catalog Number: 25544
Epoch time: 10179
04933063 = yrday
fracday
Element set: 910
Inclination: 51
6421 deg
RA of node: 175
0046 deg
Eccentricity:
0009620
Arg of perigee: 14
1426 deg
Mean anomaly: 346
0004 deg
Mean motion: 15
72073550 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2518
Checksum: 265
Coasting Arc #12 (Orbit 2532)
---------------------------------------
Vector Time (GMT): 2010/179/23:49:42
916
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3027518
86 A = 6729243
77 meter
Y = 4112666
98 meter E =
0013190
Z = -4388976
76 I = 51
69594
XDOT = -6770
820813 Wp = 64
21064
YDOT = -1405
618248 meter/sec RA = 169
11116 deg
ZDOT = 3366
826521 TA = 239
63001
MA = 239
76048
Ha = 195
702 n
mi
Hp = 184
806
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9932804
67 X = -3051961
89
Y = 13493001
89 feet Y = 4078675
52 meter
Z = -14399530
05 Z = -4403742
92
XDOT = -22213
979044 XDOT = -6770
954910
YDOT = -4611
608425 feet/sec YDOT = -1481
334913 meter/sec
ZDOT = 11046
018771 ZDOT = 3333
933779
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14086609
39 X = -4293598
54
Y = -8977159
29 feet Y = -2736238
15 meter
Z = -14458430
79 Z = -4406929
71
XDOT = 2542
656376 XDOT = 775
001664
YDOT = -21498
093653 feet/sec YDOT = -6552
618946 meter/sec
ZDOT = 10914
684434 ZDOT = 3326
795816
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
00284934
00016717 00000-0 10270-3 0 9119
2 25544 51
6426 170
1217 0009637 18
9769 341
1750 15
72073428 25333
Satellite: ISS
Catalog Number: 25544
Epoch time: 10180
00284934 = yrday
fracday
Element set: 911
Inclination: 51
6426 deg
RA of node: 170
1217 deg
Eccentricity:
0009637
Arg of perigee: 18
9769 deg
Mean anomaly: 341
1750 deg
Mean motion: 15
72073428 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2533
Checksum: 296
Coasting Arc #13 (Orbit 2548)
---------------------------------------
Vector Time (GMT): 2010/180/23:49:42
916
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6282926
24 A = 6735041
78 meter
Y = 198695
89 meter E =
0009413
Z = -2433233
64 I = 51
74560
XDOT = -2231
965109 Wp = 56
67591
YDOT = 5035
356024 meter/sec RA = 164
04115 deg
ZDOT = -5361
861925 TA = 150
69144
MA = 150
63860
Ha = 195
818 n
mi
Hp = 184
670
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20613275
07 X = 6292057
47
Y = 651889
39 feet Y = 269006
73 meter
Z = -7983050
01 Z = -2402689
41
XDOT = -7322
720174 XDOT = -2262
058908
YDOT = 16520
196928 feet/sec YDOT = 5010
229383 meter/sec
ZDOT = -17591
410516 ZDOT = -5372
777016
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1007668
99 X = 307137
51
Y = 20645798
18 feet Y = 6292839
28 meter
Z = -7861092
63 Z = -2396061
03
XDOT = -15539
896370 XDOT = -4736
560414
YDOT = -5943
753139 feet/sec YDOT = -1811
655957 meter/sec
ZDOT = -17634
928336 ZDOT = -5375
126157
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
01992247
00016717 00000-0 10270-3 0 9125
2 25544 51
6431 164
9138 0009822 22
7372 337
4223 15
72118948 25498
Satellite: ISS
Catalog Number: 25544
Epoch time: 10181
01992247 = yrday
fracday
Element set: 912
Inclination: 51
6431 deg
RA of node: 164
9138 deg
Eccentricity:
0009822
Arg of perigee: 22
7372 deg
Mean anomaly: 337
4223 deg
Mean motion: 15
72118948 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2549
Checksum: 307
Coasting Arc #14 (Orbit 2564)
---------------------------------------
Vector Time (GMT): 2010/181/23:49:42
916
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 827557
77 A = 6727048
30 meter
Y = -4490683
52 meter E =
0015305
Z = 4935461
92 I = 51
74689
XDOT = 7327
157972 Wp = 38
95491
YDOT = -1019
472238 meter/sec RA = 158
88941 deg
ZDOT = -2140
933874 TA = 71
86100
MA = 71
69440
Ha = 195
886 n
mi
Hp = 184
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2715084
54 X = 853736
63
Y = -14733213
64 feet Y = -4481283
54 meter
Z = 16192460
35 Z = 4939545
15
XDOT = 24039
232193 XDOT = 7348
413462
YDOT = -3344
725190 feet/sec YDOT = -937
416464 meter/sec
ZDOT = -7024
061265 ZDOT = -2105
287490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14917693
75 X = 4546913
05
Y = 1172706
28 feet Y = 357440
88 meter
Z = 16208707
96 Z = 4940414
19
XDOT = 5758
717970 XDOT = 1755
257237
YDOT = 22552
527525 feet/sec YDOT = 6874
010390 meter/sec
ZDOT = -6881
734005 ZDOT = -2097
552525
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
03698528
00016717 00000-0 10270-3 0 9134
2 25544 51
6428 159
7052 0009626 27
2611 332
9055 15
72076932 25656
Satellite: ISS
Catalog Number: 25544
Epoch time: 10182
03698528 = yrday
fracday
Element set: 913
Inclination: 51
6428 deg
RA of node: 159
7052 deg
Eccentricity:
0009626
Arg of perigee: 27
2611 deg
Mean anomaly: 332
9055 deg
Mean motion: 15
72076932 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2565
Checksum: 314
Coasting Arc #15 (Orbit 2580)
---------------------------------------
Vector Time (GMT): 2010/182/23:49:42
916
Vector Time (MET): N/A
Weight (LBS) : 813514
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6298058
43 A = 6736812
73 meter
Y = 1980387
42 meter E =
0022809
Z = 1274831
29 I = 51
80920
XDOT = -363
761441 Wp = 47
78231
YDOT = -4972
774925 meter/sec RA = 153
80745 deg
ZDOT = 5876
356960 TA = 326
17661
MA = 326
32189
Ha = 195
889 n
mi
Hp = 184
321
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20662921
37 X = -6325928
24
Y = 6497334
04 feet Y = 1909802
79 meter
Z = 4182517
35 Z = 1244168
16
XDOT = -1193
443048 XDOT = -336
673926
YDOT = -16314
878363 feet/sec YDOT = -4976
691954 meter/sec
ZDOT = 19279
386353 ZDOT = 5874
655039
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8822468
59 X = -2689088
43
Y = -19807696
30 feet Y = -6037385
83 meter
Z = 4060090
59 Z = 1237515
61
XDOT = 14613
013138 XDOT = 4454
046404
YDOT = -2522
646645 feet/sec YDOT = -768
902697 meter/sec
ZDOT = 19272
526630 ZDOT = 5874
266117
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
05403303
00016717 00000-0 10270-3 0 9143
2 25544 51
6440 154
4974 0009554 31
2159 328
9569 15
72143195 25816
Satellite: ISS
Catalog Number: 25544
Epoch time: 10183
05403303 = yrday
fracday
Element set: 914
Inclination: 51
6440 deg
RA of node: 154
4974 deg
Eccentricity:
0009554
Arg of perigee: 31
2159 deg
Mean anomaly: 328
9569 deg
Mean motion: 15
72143195 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2581
Checksum: 303
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
The following information is a reminder of your current mailing list subscription:
You are subscribed to the following list: [list_name]
using the following email: example@example.com
You may automatically unsubscribe from this list at any time by visiting the following URL:
https://aus-city com/cgi-bin/dada/mail cgi/u/ISSTLE_LIST/example/example com/
If the above URL is inoperable, make sure that you have copied the entire address Some mail readers will wrap a long URL and thus break this automatic unsubscribe mechanism
You may also change your subscription by visiting this list's main screen:
<[program_url]/list/[list]>
If you're still having trouble, please contact the list owner at:
<mailto:[list_owner_email]>
The following physical address is associated with this mailing list:
[physical_address]
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list