Date:
November 7th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16684 06 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 45 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 569)
---------------------------------------
Vector Time (GMT): 2010/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 487693
93 A = 6729490
54 meter
Y = 5302943
68 meter E =
0010493
Z = -4119022
46 I = 51
39200
XDOT = -6307
496998 Wp = 117
01553
YDOT = -2318
854852 meter/sec RA = 226
60173 deg
ZDOT = -3744
177529 TA = 114
51550
MA = 114
40606
Ha = 194
529 n
mi
Hp = 185
053
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1600045
71 X = 448369
30
Y = 17398109
20 feet Y = 5308177
51 meter
Z = -13513853
21 Z = -4116748
67
XDOT = -20693
887790 XDOT = -6262
909208
YDOT = -7607
791509 feet/sec YDOT = -2389
139764 meter/sec
ZDOT = -12284
047011 ZDOT = -3774
712045
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13260430
27 X = -4041779
15
Y = -11386914
57 feet Y = -3470731
56 meter
Z = -13504730
44 Z = -4116241
84
XDOT = 19314
095453 XDOT = 5886
936294
YDOT = -7824
691414 feet/sec YDOT = -2384
965943 meter/sec
ZDOT = -12406
510329 ZDOT = -3781
504348
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 10309
52278073
00016717 00000-0 10270-3 0 9004
2 25544 51
6457 227
4237 0007598 163
9414 196
1990 15
72361970 5702
Satellite: ISS
Catalog Number: 25544
Epoch time: 10309
52278073 = yrday
fracday
Element set: 900
Inclination: 51
6457 deg
RA of node: 227
4237 deg
Eccentricity:
0007598
Arg of perigee: 163
9414 deg
Mean anomaly: 196
1990 deg
Mean motion: 15
72361970 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 570
Checksum: 320
Coasting Arc #2 (Orbit 585)
---------------------------------------
Vector Time (GMT): 2010/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5547370
56 A = 6730837
68 meter
Y = 997105
12 meter E =
0014719
Z = 3662180
82 I = 51
41822
XDOT = 1751
849457 Wp = 115
57343
YDOT = 6137
841971 meter/sec RA = 221
41156 deg
ZDOT = -4317
616068 TA = 20
24135
MA = 20
18305
Ha = 194
298 n
mi
Hp = 185
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18200034
66 X = 5518017
67
Y = 3271342
25 feet Y = 1058974
92 meter
Z = 12015028
93 Z = 3689059
54
XDOT = 5747
537589 XDOT = 1704
059635
YDOT = 20137
276808 feet/sec YDOT = 6157
165126 meter/sec
ZDOT = -14165
407047 ZDOT = -4309
221213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15165852
92 X = -4622551
97
Y = 10456459
41 feet Y = 3187128
83 meter
Z = 12122838
93 Z = 3695041
31
XDOT = -17567
298841 XDOT = -5354
512687
YDOT = -9068
346552 feet/sec YDOT = -2764
032029 meter/sec
ZDOT = -14131
734450 ZDOT = -4307
352660
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 10310
53966519
00016717 00000-0 10270-3 0 9017
2 25544 51
6452 222
2153 0007640 168
1465 191
9878 15
72385104 5868
Satellite: ISS
Catalog Number: 25544
Epoch time: 10310
53966519 = yrday
fracday
Element set: 901
Inclination: 51
6452 deg
RA of node: 222
2153 deg
Eccentricity:
0007640
Arg of perigee: 168
1465 deg
Mean anomaly: 191
9878 deg
Mean motion: 15
72385104 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 586
Checksum: 309
Coasting Arc #3 (Orbit 601)
---------------------------------------
Vector Time (GMT): 2010/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2539867
01 A = 6731676
73 meter
Y = -5225974
43 meter E =
0015526
Z = 3395085
40 I = 51
44500
XDOT = 6176
533161 Wp = 119
14280
YDOT = -2
668692 meter/sec RA = 216
32483 deg
ZDOT = 4593
319569 TA = 281
03238
MA = 281
20697
Ha = 194
245 n
mi
Hp = 185
293
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8332897
03 X = -2497733
61
Y = -17145585
39 feet Y = -5254141
34 meter
Z = 11138731
63 Z = 3382848
44
XDOT = 20264
216408 XDOT = 6153
789779
YDOT = -8
755552 feet/sec YDOT = 66
273609 meter/sec
ZDOT = 15069
946092 ZDOT = 4623
270794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18147154
60 X = 5531252
72
Y = 5931286
58 feet Y = 1807856
15 meter
Z = 11089645
29 Z = 3380123
89
XDOT = -13626
072891 XDOT = -4153
227017
YDOT = 13145
930209 feet/sec YDOT = 4006
879528 meter/sec
ZDOT = 15190
093382 ZDOT = 4629
940463
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 10311
55651761
00016717 00000-0 10270-3 0 9021
2 25544 51
6453 217
0058 0007568 172
2650 187
8630 15
72436698 6020
Satellite: ISS
Catalog Number: 25544
Epoch time: 10311
55651761 = yrday
fracday
Element set: 902
Inclination: 51
6453 deg
RA of node: 217
0058 deg
Eccentricity:
0007568
Arg of perigee: 172
2650 deg
Mean anomaly: 187
8630 deg
Mean motion: 15
72436698 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 602
Checksum: 305
Coasting Arc #4 (Orbit 616)
---------------------------------------
Vector Time (GMT): 2010/312/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5089766
93 A = 6728301
81 meter
Y = 939124
75 meter E =
0013825
Z = -4313109
71 I = 51
45985
XDOT = -3964
226503 Wp = 140
79892
YDOT = -5608
055628 meter/sec RA = 211
13794 deg
ZDOT = 3452
471281 TA = 164
26865
MA = 164
22565
Ha = 193
994 n
mi
Hp = 185
257
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16698710
42 X = -5078937
29
Y = 3081117
94 feet Y = 882268
75 meter
Z = -14150622
40 Z = -4337810
04
XDOT = -13005
992464 XDOT = -3917
993441
YDOT = -18399
132639 feet/sec YDOT = -5652
127718 meter/sec
ZDOT = 11327
005514 ZDOT = 3433
324525
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9130850
91 X = 2783083
36
Y = -14218065
54 feet Y = -4333666
38 meter
Z = -14249719
49 Z = -4343314
50
XDOT = 21323
732170 XDOT = 6499
473565
YDOT = 2404
160358 feet/sec YDOT = 732
788077 meter/sec
ZDOT = 11250
192226 ZDOT = 3429
058591
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 10312
50978788
00016717 00000-0 10270-3 0 9039
2 25544 51
6455 212
1219 0007519 176
5396 183
5819 15
72493416 6176
Satellite: ISS
Catalog Number: 25544
Epoch time: 10312
50978788 = yrday
fracday
Element set: 903
Inclination: 51
6455 deg
RA of node: 212
1219 deg
Eccentricity:
0007519
Arg of perigee: 176
5396 deg
Mean anomaly: 183
5819 deg
Mean motion: 15
72493416 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 617
Checksum: 329
Coasting Arc #5 (Orbit 632)
---------------------------------------
Vector Time (GMT): 2010/313/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4311595
88 A = 6733435
12 meter
Y = 4441811
65 meter E =
0011296
Z = -2636855
35 I = 51
50375
XDOT = -5281
383239 Wp = 160
56976
YDOT = 2038
445345 meter/sec RA = 206
04946 deg
ZDOT = -5218
811597 TA = 49
47842
MA = 49
38008
Ha = 193
886 n
mi
Hp = 185
582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14145655
76 X = 4274415
88
Y = 14572872
85 feet Y = 4489818
80 meter
Z = -8651100
22 Z = -2615999
20
XDOT = -17327
372830 XDOT = -5278
432443
YDOT = 6687
812811 feet/sec YDOT = 1979
402611 meter/sec
ZDOT = -17122
085291 ZDOT = -5244
461752
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20332058
82 X = -6197211
53
Y = 718673
22 feet Y = 219051
60 meter
Z = -8567416
66 Z = -2611348
60
XDOT = 6677
348262 XDOT = 2035
255750
YDOT = -15766
703703 feet/sec YDOT = -4805
691289 meter/sec
ZDOT = -17225
007429 ZDOT = -5250
182264
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 10313
52657999
00016717 00000-0 10270-3 0 9041
2 25544 51
6455 206
9122 0007603 181
6247 178
4892 15
72517106 6331
Satellite: ISS
Catalog Number: 25544
Epoch time: 10313
52657999 = yrday
fracday
Element set: 904
Inclination: 51
6455 deg
RA of node: 206
9122 deg
Eccentricity:
0007603
Arg of perigee: 181
6247 deg
Mean anomaly: 178
4892 deg
Mean motion: 15
72517106 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 633
Checksum: 316
Coasting Arc #6 (Orbit 648)
---------------------------------------
Vector Time (GMT): 2010/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4000927
98 A = 6726092
06 meter
Y = -2533916
58 meter E =
0006662
Z = 4769988
07 I = 51
50769
XDOT = 5804
717295 Wp = 124
82376
YDOT = 4378
690421 meter/sec RA = 200
87362 deg
ZDOT = -2544
016965 TA = 350
12719
MA = 350
14027
Ha = 193
413 n
mi
Hp = 185
605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13126404
14 X = 4005793
25
Y = -8313374
60 feet Y = -2489148
90 meter
Z = 15649567
17 Z = 4789436
54
XDOT = 19044
348082 XDOT = 5767
681108
YDOT = 14365
782222 feet/sec YDOT = 4443
395345 meter/sec
ZDOT = -8346
512354 ZDOT = -2515
906885
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2341269
93 X = -713619
07
Y = 15280190
35 feet Y = 4657402
02 meter
Z = 15727614
99 Z = 4793777
05
XDOT = -22274
883632 XDOT = -6789
384531
YDOT = 5057
621070 feet/sec YDOT = 1541
562902 meter/sec
ZDOT = -8233
705695 ZDOT = -2509
633496
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 10314
54333986
00016717 00000-0 10270-3 0 9052
2 25544 51
6451 201
7023 0007418 185
8198 174
2879 15
72625170 6492
Satellite: ISS
Catalog Number: 25544
Epoch time: 10314
54333986 = yrday
fracday
Element set: 905
Inclination: 51
6451 deg
RA of node: 201
7023 deg
Eccentricity:
0007418
Arg of perigee: 185
8198 deg
Mean anomaly: 174
2879 deg
Mean motion: 15
72625170 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 649
Checksum: 318
Coasting Arc #7 (Orbit 664)
---------------------------------------
Vector Time (GMT): 2010/315/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5694590
80 A = 6734719
26 meter
Y = -3102398
65 meter E =
0011704
Z = 1811003
17 I = 51
56532
XDOT = 3771
811121 Wp = 97
37549
YDOT = -3600
904152 meter/sec RA = 195
77726 deg
ZDOT = 5658
930980 TA = 282
70742
MA = 282
83822
Ha = 193
393 n
mi
Hp = 185
827
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18683040
69 X = -5668273
60
Y = -10178473
25 feet Y = -3165931
93 meter
Z = 5941611
46 Z = 1783402
26
XDOT = 12374
708403 XDOT = 3784
306355
YDOT = -11813
989999 feet/sec YDOT = -3558
655924 meter/sec
ZDOT = 18566
046523 ZDOT = 5677
284836
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19863368
75 X = 6054354
79
Y = -7707661
62 feet Y = -2349295
26 meter
Z = 5830832
53 Z = 1777237
76
XDOT = 528
271102 XDOT = 161
017032
YDOT = 15544
900334 feet/sec YDOT = 4738
085622 meter/sec
ZDOT = 18639
709274 ZDOT = 5681
383387
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 10315
56007126
00016717 00000-0 10270-3 0 9060
2 25544 51
6450 196
4915 0007392 189
6800 170
4222 15
72626850 6658
Satellite: ISS
Catalog Number: 25544
Epoch time: 10315
56007126 = yrday
fracday
Element set: 906
Inclination: 51
6450 deg
RA of node: 196
4915 deg
Eccentricity:
0007392
Arg of perigee: 189
6800 deg
Mean anomaly: 170
4222 deg
Mean motion: 15
72626850 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 665
Checksum: 302
Coasting Arc #8 (Orbit 679)
---------------------------------------
Vector Time (GMT): 2010/316/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2527857
08 A = 6724659
40 meter
Y = 3627539
89 meter E =
0015358
Z = -5079096
21 I = 51
56178
XDOT = -7041
092848 Wp = 131
27538
YDOT = -2628
282215 meter/sec RA = 190
61646 deg
ZDOT = 1620
414119 TA = 154
37210
MA = 154
29590
Ha = 193
114 n
mi
Hp = 185
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8293494
37 X = -2543559
41
Y = 11901377
60 feet Y = 3599184
26 meter
Z = -16663701
49 Z = -5091414
70
XDOT = -23100
698321 XDOT = -7019
051364
YDOT = -8622
973147 feet/sec YDOT = -2706
896767 meter/sec
ZDOT = 5316
319287 ZDOT = 1586
261537
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4026316
27 X = -1227221
20
Y = -13876719
71 feet Y = -4229624
17 meter
Z = -16713144
89 Z = -5094166
56
XDOT = 20305
645067 XDOT = 6189
160616
YDOT = -12156
246887 feet/sec YDOT = -3705
224051 meter/sec
ZDOT = 5179
227960 ZDOT = 1578
628682
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 10316
51322727
00016717 00000-0 10270-3 0 9074
2 25544 51
6449 191
6063 0007420 194
2299 165
8656 15
72693338 6804
Satellite: ISS
Catalog Number: 25544
Epoch time: 10316
51322727 = yrday
fracday
Element set: 907
Inclination: 51
6449 deg
RA of node: 191
6063 deg
Eccentricity:
0007420
Arg of perigee: 194
2299 deg
Mean anomaly: 165
8656 deg
Mean motion: 15
72693338 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 680
Checksum: 322
Coasting Arc #9 (Orbit 695)
---------------------------------------
Vector Time (GMT): 2010/317/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6489297
31 A = 6735504
11 meter
Y = 1441594
29 meter E =
0015423
Z = -1025125
04 I = 51
62826
XDOT = -1936
377596 Wp = 166
39109
YDOT = 4526
394545 meter/sec RA = 185
51133 deg
ZDOT = -5925
132280 TA = 24
81867
MA = 24
74456
Ha = 193
101 n
mi
Hp = 186
089
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21290345
49 X = 6477674
76
Y = 4729640
06 feet Y = 1514096
55 meter
Z = -3363271
12 Z = -993627
85
XDOT = -6352
944869 XDOT = -1958
065092
YDOT = 14850
375805 feet/sec YDOT = 4504
619661 meter/sec
ZDOT = -19439
410368 ZDOT = -5934
591908
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16915451
66 X = -5155829
67
Y = 13796751
46 feet Y = 4205249
84 meter
Z = -3236826
13 Z = -986584
60
XDOT = -6785
564732 XDOT = -2068
240130
YDOT = -12862
827507 feet/sec YDOT = -3920
589824 meter/sec
ZDOT = -19477
379438 ZDOT = -5936
705253
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 10317
52989924
00016717 00000-0 10270-3 0 9085
2 25544 51
6450 186
3961 0007602 198
3665 161
7225 15
72684246 6960
Satellite: ISS
Catalog Number: 25544
Epoch time: 10317
52989924 = yrday
fracday
Element set: 908
Inclination: 51
6450 deg
RA of node: 186
3961 deg
Eccentricity:
0007602
Arg of perigee: 198
3665 deg
Mean anomaly: 161
7225 deg
Mean motion: 15
72684246 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 696
Checksum: 339
Coasting Arc #10 (Orbit 711)
---------------------------------------
Vector Time (GMT): 2010/318/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 819153
00 A = 6723708
83 meter
Y = -4140128
33 meter E =
0005509
Z = 5233817
31 I = 51
61991
XDOT = 7641
877847 Wp = 182
49159
YDOT = 615
281476 meter/sec RA = 180
36855 deg
ZDOT = -714
767361 TA = 274
27772
MA = 274
34067
Ha = 192
710 n
mi
Hp = 186
165
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2687509
86 X = 839962
51
Y = -13583098
20 feet Y = -4130851
76 meter
Z = 17171316
64 Z = 5237847
33
XDOT = 25071
777713 XDOT = 7637
901948
YDOT = 2018
640014 feet/sec YDOT = 700
715326 meter/sec
ZDOT = -2345
037273 ZDOT = -677
652243
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9237902
86 X = 2815712
79
Y = 10287308
39 feet Y = 3135571
60 meter
Z = 17187490
15 Z = 5238747
00
XDOT = -16056
705218 XDOT = -4894
083750
YDOT = 18058
014178 feet/sec YDOT = 5504
082721 meter/sec
ZDOT = -2196
026916 ZDOT = -669
349004
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 10318
54653871
00016717 00000-0 10270-3 0 9098
2 25544 51
6449 181
1849 0007412 202
8934 157
1899 15
72783348 7123
Satellite: ISS
Catalog Number: 25544
Epoch time: 10318
54653871 = yrday
fracday
Element set: 909
Inclination: 51
6449 deg
RA of node: 181
1849 deg
Eccentricity:
0007412
Arg of perigee: 202
8934 deg
Mean anomaly: 157
1899 deg
Mean motion: 15
72783348 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 712
Checksum: 335
Coasting Arc #11 (Orbit 727)
---------------------------------------
Vector Time (GMT): 2010/319/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6719663
20 A = 6735471
88 meter
Y = 365009
00 meter E =
0006217
Z = 243784
19 I = 51
68959
XDOT = -36
267745 Wp = 71
85912
YDOT = -4778
187244 meter/sec RA = 175
25074 deg
ZDOT = 6031
010527 TA = 290
78528
MA = 290
85187
Ha = 192
469 n
mi
Hp = 186
343
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22046139
11 X = -6724429
65
Y = 1197536
09 feet Y = 289839
03 meter
Z = 799816
90 Z = 211127
93
XDOT = -118
988665 XDOT = -12
132538
YDOT = -15676
467335 feet/sec YDOT = -4778
457866 meter/sec
ZDOT = 19786
779944 ZDOT = 6030
892959
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12093455
98 X = 3686085
38
Y = -18477207
97 feet Y = -5631852
99 meter
Z = 668698
63 Z = 203819
34
XDOT = 11424
048197 XDOT = 3482
049890
YDOT = 8210
731318 feet/sec YDOT = 2502
630906 meter/sec
ZDOT = 19786
301105 ZDOT = 6030
864577
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 10319
56314853
00016717 00000-0 10270-3 0 9107
2 25544 51
6440 175
9729 0007413 207
4230 152
6543 15
72835819 7287
Satellite: ISS
Catalog Number: 25544
Epoch time: 10319
56314853 = yrday
fracday
Element set: 910
Inclination: 51
6440 deg
RA of node: 175
9729 deg
Eccentricity:
0007413
Arg of perigee: 207
4230 deg
Mean anomaly: 152
6543 deg
Mean motion: 15
72835819 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 728
Checksum: 308
Coasting Arc #12 (Orbit 742)
---------------------------------------
Vector Time (GMT): 2010/320/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 852418
05 A = 6723309
08 meter
Y = 4087057
94 meter E =
0012665
Z = -5279386
55 I = 51
67805
XDOT = -7558
242652 Wp = 118
29720
YDOT = 1418
571302 meter/sec RA = 170
12558 deg
ZDOT = -128
291544 TA = 150
52029
MA = 150
44881
Ha = 192
223 n
mi
Hp = 186
485
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2796647
14 X = 832299
29
Y = 13408982
74 feet Y = 4096477
70 meter
Z = -17320822
01 Z = -5275294
29
XDOT = -24797
384029 XDOT = -7572
920398
YDOT = 4654
105322 feet/sec YDOT = 1333
968417 meter/sec
ZDOT = -420
904016 ZDOT = -165
045909
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12615951
76 X = -3845342
10
Y = -5387849
16 feet Y = -1642216
42 meter
Z = -17304385
89 Z = -5274376
82
XDOT = 10147
629734 XDOT = 3092
997543
YDOT = -21999
943362 feet/sec YDOT = -6705
582737 meter/sec
ZDOT = -568
487050 ZDOT = -173
274853
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 10320
51619364
00016717 00000-0 10270-3 0 9110
2 25544 51
6428 171
0865 0007349 211
5036 148
5688 15
72877994 7430
Satellite: ISS
Catalog Number: 25544
Epoch time: 10320
51619364 = yrday
fracday
Element set: 911
Inclination: 51
6428 deg
RA of node: 171
0865 deg
Eccentricity:
0007349
Arg of perigee: 211
5036 deg
Mean anomaly: 148
5688 deg
Mean motion: 15
72877994 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 743
Checksum: 324
Coasting Arc #13 (Orbit 758)
---------------------------------------
Vector Time (GMT): 2010/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6376985
41 A = 6735186
00 meter
Y = -2085461
80 meter E =
0015503
Z = 461435
57 I = 51
74836
XDOT = 1883
352759 Wp = 158
39978
YDOT = 4414
461518 meter/sec RA = 164
99890 deg
ZDOT = -6026
897029 TA = 16
58778
MA = 16
53712
Ha = 192
022 n
mi
Hp = 186
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20921868
15 X = 6397589
85
Y = -6842066
26 feet Y = -2014035
30 meter
Z = 1513896
22 Z = 492465
76
XDOT = 6178
978868 XDOT = 1863
127748
YDOT = 14483
141464 feet/sec YDOT = 4435
409248 meter/sec
ZDOT = -19773
284215 ZDOT = -6017
796582
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6148228
31 X = -1873979
99
Y = 21126876
49 feet Y = 6439471
96 meter
Z = 1638504
72 Z = 499416
24
XDOT = -13969
296922 XDOT = -4257
841702
YDOT = -2522
910579 feet/sec YDOT = -768
983145 meter/sec
ZDOT = -19736
738488 ZDOT = -6015
757891
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 10321
53274569
00016717 00000-0 10270-3 0 9128
2 25544 51
6430 165
8758 0007347 215
6211 144
4462 15
72907151 7594
Satellite: ISS
Catalog Number: 25544
Epoch time: 10321
53274569 = yrday
fracday
Element set: 912
Inclination: 51
6430 deg
RA of node: 165
8758 deg
Eccentricity:
0007347
Arg of perigee: 215
6211 deg
Mean anomaly: 144
4462 deg
Mean motion: 15
72907151 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 759
Checksum: 306
Coasting Arc #14 (Orbit 774)
---------------------------------------
Vector Time (GMT): 2010/322/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2378106
98 A = 6723483
48 meter
Y = -3512667
39 meter E =
0007712
Z = 5218867
34 I = 51
73694
XDOT = 6895
784859 Wp = 192
78333
YDOT = -3295
170221 meter/sec RA = 159
89065 deg
ZDOT = 917
236438 TA = 248
44647
MA = 248
52867
Ha = 191
910 n
mi
Hp = 186
788
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7802188
25 X = -2364003
94
Y = -11524499
31 feet Y = -3539182
05 meter
Z = 17122268
17 Z = 5207348
37
XDOT = 22623
966073 XDOT = 6927
663657
YDOT = -10810
925922 feet/sec YDOT = -3217
879179 meter/sec
ZDOT = 3009
305898 ZDOT = 950
814462
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13971389
46 X = 4258479
51
Y = -265366
19 feet Y = -80883
61 meter
Z = 17076010
96 Z = 5204768
14
XDOT = -3419
264666 XDOT = -1042
191870
YDOT = 23807
199237 feet/sec YDOT = 7256
434327 meter/sec
ZDOT = 3144
160122 ZDOT = 958
340005
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 10322
54926772
00016717 00000-0 10270-3 0 9131
2 25544 51
6418 160
6629 0007311 219
5259 140
5371 15
72920178 7754
Satellite: ISS
Catalog Number: 25544
Epoch time: 10322
54926772 = yrday
fracday
Element set: 913
Inclination: 51
6418 deg
RA of node: 160
6629 deg
Eccentricity:
0007311
Arg of perigee: 219
5259 deg
Mean anomaly: 140
5371 deg
Mean motion: 15
72920178 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 775
Checksum: 309
Coasting Arc #15 (Orbit 789)
---------------------------------------
Vector Time (GMT): 2010/323/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5577618
11 A = 6734459
40 meter
Y = 3602387
08 meter E =
0002196
Z = -1117351
59 I = 51
80166
XDOT = -3452
823652 Wp = 16
61708
YDOT = -3514
161769 meter/sec RA = 154
75223 deg
ZDOT = 5910
979206 TA = 331
19241
MA = 331
20454
Ha = 191
566 n
mi
Hp = 186
907
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18299272
03 X = -5612058
08
Y = 11818855
24 feet Y = 3539822
28 meter
Z = -3665851
68 Z = -1144531
98
XDOT = -11328
161589 XDOT = -3441
986333
YDOT = -11529
402130 feet/sec YDOT = -3552
712952 meter/sec
ZDOT = 19392
976397 ZDOT = 5894
231083
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -196405
69 X = -59864
45
Y = -21764598
63 feet Y = -6633849
66 meter
Z = -3775027
89 Z = -1150628
50
XDOT = 14276
736145 XDOT = 4351
549177
YDOT = -3478
132437 feet/sec YDOT = -1060
134767 meter/sec
ZDOT = 19325
717807 ZDOT = 5890
478788
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 10323
50222711
00016717 00000-0 10270-3 0 9141
2 25544 51
6406 155
7754 0007402 223
9639 136
0936 15
72994169 7902
Satellite: ISS
Catalog Number: 25544
Epoch time: 10323
50222711 = yrday
fracday
Element set: 914
Inclination: 51
6406 deg
RA of node: 155
7754 deg
Eccentricity:
0007402
Arg of perigee: 223
9639 deg
Mean anomaly: 136
0936 deg
Mean motion: 15
72994169 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 790
Checksum: 307
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