Date:
August 20th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 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 3333)
---------------------------------------
Vector Time (GMT): 2010/230/22:03:25
906
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3978627
95 A = 6729901
80 meter
Y = -2339970
88 meter E =
0005331
Z = -4902088
70 I = 51
29217
XDOT = 1578
593406 Wp = 135
89671
YDOT = -7212
290974 meter/sec RA = 268
79204 deg
ZDOT = 2159
146486 TA = 155
19791
MA = 155
17228
Ha = 192
062 n
mi
Hp = 191
572
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13053241
31 X = -3928353
11
Y = -7677069
81 feet Y = -2384180
89 meter
Z = -16082968
18 Z = -4921294
65
XDOT = 5179
112226 XDOT = 1648
636629
YDOT = -23662
371961 feet/sec YDOT = -7194
246691 meter/sec
ZDOT = 7083
813929 ZDOT = 2166
984908
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 895716
34 X = 273014
34
Y = -15034806
79 feet Y = -4582609
11 meter
Z = -16159785
02 Z = -4925502
48
XDOT = 22293
151283 XDOT = 6794
952511
YDOT = -6327
683812 feet/sec YDOT = -1928
678026 meter/sec
ZDOT = 7115
139062 ZDOT = 2168
694386
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 10230
93123099
00016717 00000-0 10270-3 0 9009
2 25544 51
6468 269
5282 0008390 267
4753 92
5448 15
71110928 33340
Satellite: ISS
Catalog Number: 25544
Epoch time: 10230
93123099 = yrday
fracday
Element set: 900
Inclination: 51
6468 deg
RA of node: 269
5282 deg
Eccentricity:
0008390
Arg of perigee: 267
4753 deg
Mean anomaly: 92
5448 deg
Mean motion: 15
71110928 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3334
Checksum: 313
Coasting Arc #2 (Orbit 3349)
---------------------------------------
Vector Time (GMT): 2010/231/22:03:25
906
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -65341
69 A = 6740047
58 meter
Y = 6660168
04 meter E =
0008025
Z = -996827
66 I = 51
32777
XDOT = -4853
825784 Wp = 197
05301
YDOT = -931
296668 meter/sec RA = 263
68249 deg
ZDOT = -5899
716783 TA = 353
87548
MA = 353
88528
Ha = 191
637 n
mi
Hp = 191
430
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -214375
63 X = -134969
73
Y = 21850945
03 feet Y = 6659048
10 meter
Z = -3270431
94 Z = -997313
85
XDOT = -15924
625274 XDOT = -4814
391818
YDOT = -3055
435263 feet/sec YDOT = -985
354256 meter/sec
ZDOT = -19356
026192 ZDOT = -5923
200550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19345217
18 X = -5896422
20
Y = 10161683
06 feet Y = 3097281
00 meter
Z = -3272346
28 Z = -997411
15
XDOT = -4042
820025 XDOT = -1232
251544
YDOT = -13964
610806 feet/sec YDOT = -4256
413374 meter/sec
ZDOT = -19449
954902 ZDOT = -5928
346254
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 10231
94893381
00016717 00000-0 10270-3 0 9010
2 25544 51
6467 264
3251 0008442 270
3788 89
6406 15
71087249 33505
Satellite: ISS
Catalog Number: 25544
Epoch time: 10231
94893381 = yrday
fracday
Element set: 901
Inclination: 51
6467 deg
RA of node: 264
3251 deg
Eccentricity:
0008442
Arg of perigee: 270
3788 deg
Mean anomaly: 89
6406 deg
Mean motion: 15
71087249 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3350
Checksum: 319
Coasting Arc #3 (Orbit 3365)
---------------------------------------
Vector Time (GMT): 2010/232/22:03:25
906
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4145763
67 A = 6728203
69 meter
Y = -736631
28 meter E =
0006082
Z = 5252927
52 I = 51
29288
XDOT = 1457
748634 Wp = 279
15717
YDOT = 7552
400503 meter/sec RA = 258
53477 deg
ZDOT = -90
540762 TA = 171
71210
MA = 171
70204
Ha = 192
577 n
mi
Hp = 192
000
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13601586
85 X = 4128175
42
Y = -2416769
29 feet Y = -690369
42 meter
Z = 17234014
16 Z = 5273024
50
XDOT = 4782
639875 XDOT = 1373
627786
YDOT = 24778
216872 feet/sec YDOT = 7568
231579 meter/sec
ZDOT = -297
049745 ZDOT = -83
663184
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8696557
52 X = 2650710
73
Y = 10603622
67 feet Y = 3231984
19 meter
Z = 17314394
48 Z = 5277427
44
XDOT = -18519
585450 XDOT = -5644
769645
YDOT = 15633
492712 feet/sec YDOT = 4765
088579 meter/sec
ZDOT = -269
493625 ZDOT = -82
141657
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 10232
96661961
00016717 00000-0 10270-3 0 9021
2 25544 51
6464 259
1212 0008425 275
5752 84
4449 15
71161251 33663
Satellite: ISS
Catalog Number: 25544
Epoch time: 10232
96661961 = yrday
fracday
Element set: 902
Inclination: 51
6464 deg
RA of node: 259
1212 deg
Eccentricity:
0008425
Arg of perigee: 275
5752 deg
Mean anomaly: 84
4449 deg
Mean motion: 15
71161251 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3366
Checksum: 308
Coasting Arc #4 (Orbit 3380)
---------------------------------------
Vector Time (GMT): 2010/233/22:03:25
906
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2540043
14 A = 6739901
52 meter
Y = -6179923
21 meter E =
0009582
Z = -834301
03 I = 51
33895
XDOT = 4200
497639 Wp = 348
59977
YDOT = -2527
963441 meter/sec RA = 253
38985 deg
ZDOT = 5934
559862 TA = 2
27010
MA = 2
26575
Ha = 192
787 n
mi
Hp = 191
768
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8333474
86 X = -2466696
52
Y = -20275338
62 feet Y = -6207917
37 meter
Z = -2737208
10 Z = -846462
27
XDOT = 13781
160234 XDOT = 4199
625185
YDOT = -8293
843310 feet/sec YDOT = -2480
995964 meter/sec
ZDOT = 19470
340756 ZDOT = 5954
963280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13341503
96 X = 4066490
41
Y = -17385956
31 feet Y = -5299239
48 meter
Z = -2785904
30 Z = -849143
63
XDOT = 12773
133813 XDOT = 3893
251186
YDOT = 6667
555951 feet/sec YDOT = 2032
271054 meter/sec
ZDOT = 19551
936519 ZDOT = 5959
430251
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 10233
92068749
00016717 00000-0 10270-3 0 9034
2 25544 51
6457 254
2422 0008488 279
7244 80
2959 15
71179568 33812
Satellite: ISS
Catalog Number: 25544
Epoch time: 10233
92068749 = yrday
fracday
Element set: 903
Inclination: 51
6457 deg
RA of node: 254
2422 deg
Eccentricity:
0008488
Arg of perigee: 279
7244 deg
Mean anomaly: 80
2959 deg
Mean motion: 15
71179568 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3381
Checksum: 340
Coasting Arc #5 (Orbit 3396)
---------------------------------------
Vector Time (GMT): 2010/234/22:03:25
906
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2881778
08 A = 6729382
59 meter
Y = 3514926
35 meter E =
0006817
Z = -4967626
49 I = 51
31238
XDOT = -4148
143916 Wp = 38
43801
YDOT = -6174
295607 meter/sec RA = 248
27733 deg
ZDOT = -1958
517056 TA = 212
50259
MA = 212
54458
Ha = 193
000 n
mi
Hp = 191
411
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9454652
48 X = -2896737
12
Y = 11531910
59 feet Y = 3482616
94 meter
Z = -16297987
16 Z = -4981662
20
XDOT = -13609
396051 XDOT = -4069
279589
YDOT = -20256
875351 feet/sec YDOT = -6220
241681 meter/sec
ZDOT = -6425
580891 ZDOT = -1978
476763
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14710482
07 X = -4483754
94
Y = -2035909
00 feet Y = -620545
06 meter
Z = -16354100
18 Z = -4984729
73
XDOT = 10156
165100 XDOT = 3095
599122
YDOT = -21025
666914 feet/sec YDOT = -6408
623276 meter/sec
ZDOT = -6505
488451 ZDOT = -1982
872880
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 10234
93834447
00016717 00000-0 10270-3 0 9043
2 25544 51
6446 249
0379 0008572 283
8961 76
1247 15
71204305 33978
Satellite: ISS
Catalog Number: 25544
Epoch time: 10234
93834447 = yrday
fracday
Element set: 904
Inclination: 51
6446 deg
RA of node: 249
0379 deg
Eccentricity:
0008572
Arg of perigee: 283
8961 deg
Mean anomaly: 76
1247 deg
Mean motion: 15
71204305 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3397
Checksum: 325
Coasting Arc #6 (Orbit 3412)
---------------------------------------
Vector Time (GMT): 2010/235/22:03:25
906
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4477909
34 A = 6737183
94 meter
Y = 4345061
93 meter E =
0005294
Z = 2535909
14 I = 51
35178
XDOT = -2074
305499 Wp = 96
17520
YDOT = 5214
783860 meter/sec RA = 243
10345 deg
ZDOT = -5263
414177 TA = 55
00202
MA = 54
95234
Ha = 193
207 n
mi
Hp = 191
144
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14691303
60 X = 4416670
50
Y = 14255452
53 feet Y = 4394794
24 meter
Z = 8319911
89 Z = 2557513
58
XDOT = -6805
464236 XDOT = -2106
895784
YDOT = 17108
870933 feet/sec YDOT = 5191
405414 meter/sec
ZDOT = -17268
419216 ZDOT = -5273
570213
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4272771
45 X = -1302340
74
Y = 19983724
32 feet Y = 6091039
17 meter
Z = 8406393
31 Z = 2562268
68
XDOT = -16593
632460 XDOT = -5057
739174
YDOT = 3745
407346 feet/sec YDOT = 1141
600159 meter/sec
ZDOT = -17308
987539 ZDOT = -5275
779402
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 10235
95598621
00016717 00000-0 10270-3 0 9058
2 25544 51
6449 243
8339 0008551 288
3066 71
7165 15
71245082 34138
Satellite: ISS
Catalog Number: 25544
Epoch time: 10235
95598621 = yrday
fracday
Element set: 905
Inclination: 51
6449 deg
RA of node: 243
8339 deg
Eccentricity:
0008551
Arg of perigee: 288
3066 deg
Mean anomaly: 71
7165 deg
Mean motion: 15
71245082 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3413
Checksum: 320
Coasting Arc #7 (Orbit 3428)
---------------------------------------
Vector Time (GMT): 2010/236/22:03:25
906
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 564351
48 A = 6732780
57 meter
Y = -5301105
14 meter E =
0002307
Z = 4109846
52 I = 51
35015
XDOT = 5729
106824 Wp = 74
19816
YDOT = 3516
059411 meter/sec RA = 238
01432 deg
ZDOT = 3747
377011 TA = 337
22578
MA = 337
23601
Ha = 193
405 n
mi
Hp = 191
060
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1851546
85 X = 603622
90
Y = -17392077
23 feet Y = -5294574
50 meter
Z = 13483748
42 Z = 4112683
67
XDOT = 18796
282231 XDOT = 5671
160023
YDOT = 11535
627989 feet/sec YDOT = 3579
801851 meter/sec
ZDOT = 12294
544000 ZDOT = 3775
067675
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15529585
62 X = 4733417
70
Y = -8027468
32 feet Y = -2446772
34 meter
Z = 13495027
62 Z = 4113284
42
XDOT = -4
853173 XDOT = -1
479247
YDOT = 20851
568542 feet/sec YDOT = 6355
558092 meter/sec
ZDOT = 12405
374852 ZDOT = 3781
158255
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 10236
97361358
00016717 00000-0 10270-3 0 9067
2 25544 51
6437 238
6283 0008572 292
1647 67
8605 15
71214608 34298
Satellite: ISS
Catalog Number: 25544
Epoch time: 10236
97361358 = yrday
fracday
Element set: 906
Inclination: 51
6437 deg
RA of node: 238
6283 deg
Eccentricity:
0008572
Arg of perigee: 292
1647 deg
Mean anomaly: 67
8605 deg
Mean motion: 15
71214608 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3429
Checksum: 329
Coasting Arc #8 (Orbit 3443)
---------------------------------------
Vector Time (GMT): 2010/237/22:03:25
906
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5206755
39 A = 6733167
17 meter
Y = -1676150
82 meter E =
0001921
Z = -3924103
70 I = 51
36844
XDOT = -920
877329 Wp = 321
37610
YDOT = -6508
166898 meter/sec RA = 232
82780 deg
ZDOT = 4002
217838 TA = 350
36180
MA = 350
36549
Ha = 193
363 n
mi
Hp = 190
749
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17082530
80 X = -5168563
04
Y = -5499182
47 feet Y = -1734162
52 meter
Z = -12874355
97 Z = -3949304
94
XDOT = -3021
251078 XDOT = -867
475176
YDOT = -21352
253603 feet/sec YDOT = -6518
165920 meter/sec
ZDOT = 13130
635951 ZDOT = 3997
874299
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4991298
89 X = -1521347
90
Y = -17161986
97 feet Y = -5230973
63 meter
Z = -12975208
92 Z = -3954843
68
XDOT = 14682
303982 XDOT = 4475
166254
YDOT = -14183
196792 feet/sec YDOT = -4323
038382 meter/sec
ZDOT = 13113
160633 ZDOT = 3996
891361
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 10237
92762221
00016717 00000-0 10270-3 0 9078
2 25544 51
6429 233
7482 0008569 294
6617 65
3652 15
71272202 34442
Satellite: ISS
Catalog Number: 25544
Epoch time: 10237
92762221 = yrday
fracday
Element set: 907
Inclination: 51
6429 deg
RA of node: 233
7482 deg
Eccentricity:
0008569
Arg of perigee: 294
6617 deg
Mean anomaly: 65
3652 deg
Mean motion: 15
71272202 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3444
Checksum: 314
Coasting Arc #9 (Orbit 3459)
---------------------------------------
Vector Time (GMT): 2010/238/22:03:25
906
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2177453
46 A = 6736529
34 meter
Y = 5725111
44 meter E =
0003869
Z = -2803528
69 I = 51
39855
XDOT = -5762
243832 Wp = 297
54444
YDOT = -303
010231 meter/sec RA = 227
74438 deg
ZDOT = -5087
089189 TA = 274
63268
MA = 274
67687
Ha = 193
675 n
mi
Hp = 190
561
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7143876
17 X = 2126891
30
Y = 18783174
02 feet Y = 5749178
17 meter
Z = -9197928
76 Z = -2793073
84
XDOT = -18904
999449 XDOT = -5733
715297
YDOT = -994
128056 feet/sec YDOT = -367
287868 meter/sec
ZDOT = -16689
925160 ZDOT = -5115
012621
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11221567
89 X = -3420333
89
Y = 16693964
42 feet Y = 5088320
35 meter
Z = -9156006
37 Z = -2790750
74
XDOT = -8788
602550 XDOT = -2678
766057
YDOT = -15135
593502 feet/sec YDOT = -4613
328899 meter/sec
ZDOT = -16801
653503 ZDOT = -5121
143988
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 10238
94521709
00016717 00000-0 10270-3 0 9086
2 25544 51
6425 228
5442 0008582 298
7802 61
2497 15
71288661 34608
Satellite: ISS
Catalog Number: 25544
Epoch time: 10238
94521709 = yrday
fracday
Element set: 908
Inclination: 51
6425 deg
RA of node: 228
5442 deg
Eccentricity:
0008582
Arg of perigee: 298
7802 deg
Mean anomaly: 61
2497 deg
Mean motion: 15
71288661 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3460
Checksum: 328
Coasting Arc #10 (Orbit 3475)
---------------------------------------
Vector Time (GMT): 2010/239/22:03:25
906
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4540506
71 A = 6729543
13 meter
Y = -1087696
94 meter E =
0008204
Z = 4850634
06 I = 51
39695
XDOT = 3968
745934 Wp = 349
09846
YDOT = 6166
108470 meter/sec RA = 222
56973 deg
ZDOT = -2325
034898 TA = 123
69301
MA = 123
61477
Ha = 193
737 n
mi
Hp = 190
289
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14896675
55 X = 4528768
67
Y = -3568559
50 feet Y = -1036987
63 meter
Z = 15914153
75 Z = 4872663
30
XDOT = 13020
819992 XDOT = 3910
794963
YDOT = 20230
014664 feet/sec YDOT = 6210
165214 meter/sec
ZDOT = -7628
067250 ZDOT = -2305
895919
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11605721
83 X = 3537424
01
Y = 9855968
31 feet Y = 3004099
14 meter
Z = 16002279
79 Z = 4877494
88
XDOT = -7925
173101 XDOT = -2415
592761
YDOT = 21631
298887 feet/sec YDOT = 6593
219901 meter/sec
ZDOT = -7551
383834 ZDOT = -2301
661793
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 10239
96279521
00016717 00000-0 10270-3 0 9092
2 25544 51
6428 223
3386 0008562 301
9893 58
0437 15
71308328 34764
Satellite: ISS
Catalog Number: 25544
Epoch time: 10239
96279521 = yrday
fracday
Element set: 909
Inclination: 51
6428 deg
RA of node: 223
3386 deg
Eccentricity:
0008562
Arg of perigee: 301
9893 deg
Mean anomaly: 58
0437 deg
Mean motion: 15
71308328 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3476
Checksum: 330
Coasting Arc #11 (Orbit 3491)
---------------------------------------
Vector Time (GMT): 2010/240/22:03:25
906
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4609564
59 A = 6739163
33 meter
Y = -4751456
50 meter E =
0013234
Z = 1213717
10 I = 51
45177
XDOT = 4250
982340 Wp = 21
92421
YDOT = -2624
976406 meter/sec RA = 217
46811 deg
ZDOT = 5860
081638 TA = 351
40718
MA = 351
42981
Ha = 193
911 n
mi
Hp = 190
079
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15123243
40 X = -4561986
35
Y = -15588768
05 feet Y = -4802737
33 meter
Z = 3982011
49 Z = 1191439
65
XDOT = 13946
792455 XDOT = 4251
552161
YDOT = -8612
127315 feet/sec YDOT = -2577
435901 meter/sec
ZDOT = 19225
989626 ZDOT = 5880
734410
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3299002
59 X = 1005535
99
Y = -21483514
26 feet Y = -6548175
15 meter
Z = 3892787
29 Z = 1186521
57
XDOT = 13645
120866 XDOT = 4159
032840
YDOT = 5599
161922 feet/sec YDOT = 1706
624554 meter/sec
ZDOT = 19308
585354 ZDOT = 5885
256816
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 10240
98035689
00016717 00000-0 10270-3 0 9103
2 25544 51
6420 218
1327 0008477 305
9825 54
0550 15
71336297 34923
Satellite: ISS
Catalog Number: 25544
Epoch time: 10240
98035689 = yrday
fracday
Element set: 910
Inclination: 51
6420 deg
RA of node: 218
1327 deg
Eccentricity:
0008477
Arg of perigee: 305
9825 deg
Mean anomaly: 54
0550 deg
Mean motion: 15
71336297 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3492
Checksum: 310
Coasting Arc #12 (Orbit 3506)
---------------------------------------
Vector Time (GMT): 2010/241/22:03:25
906
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2634813
13 A = 6727652
99 meter
Y = 3287651
88 meter E =
0009671
Z = -5252145
33 I = 51
43794
XDOT = -6303
451536 Wp = 62
43799
YDOT = -4386
266159 meter/sec RA = 212
32393 deg
ZDOT = 421
566664 TA = 211
55271
MA = 211
61074
Ha = 193
957 n
mi
Hp = 189
692
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8644400
04 X = -2645866
41
Y = 10786259
45 feet Y = 3258125
83 meter
Z = -17231447
95 Z = -5264972
25
XDOT = -20680
615274 XDOT = -6255
982911
YDOT = -14390
637003 feet/sec YDOT = -4456
489706 meter/sec
ZDOT = 1383
092730 ZDOT = 391
059897
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13758425
11 X = -4193567
97
Y = -71829
77 feet Y = -21893
71 meter
Z = -17282720
34 Z = -5267773
16
XDOT = -1437
292919 XDOT = -438
086882
YDOT = -24157
214307 feet/sec YDOT = -7363
118921 meter/sec
ZDOT = 1260
936761 ZDOT = 384
333525
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 10241
93430513
00016717 00000-0 10270-3 0 9115
2 25544 51
6417 213
2529 0008307 309
7265 50
3164 15
71370130 35072
Satellite: ISS
Catalog Number: 25544
Epoch time: 10241
93430513 = yrday
fracday
Element set: 911
Inclination: 51
6417 deg
RA of node: 213
2529 deg
Eccentricity:
0008307
Arg of perigee: 309
7265 deg
Mean anomaly: 50
3164 deg
Mean motion: 15
71370130 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3507
Checksum: 271
Coasting Arc #13 (Orbit 3522)
---------------------------------------
Vector Time (GMT): 2010/242/22:03:25
906
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6139491
66 A = 6739340
82 meter
Y = 2734958
97 meter E =
0004591
Z = 469366
17 I = 51
50460
XDOT = -1568
101293 Wp = 121
79512
YDOT = 4556
194965 meter/sec RA = 207
19537 deg
ZDOT = -5996
676369 TA = 53
09819
MA = 53
05612
Ha = 194
149 n
mi
Hp = 189
389
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20142689
18 X = 6106172
44
Y = 8972962
51 feet Y = 2803428
16 meter
Z = 1539915
26 Z = 499110
92
XDOT = -5144
689280 XDOT = -1589
802104
YDOT = 14948
146210 feet/sec YDOT = 4538
538067 meter/sec
ZDOT = -19674
135068 ZDOT = -6004
347023
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5721096
03 X = 1743790
07
Y = 21286852
57 feet Y = 6488232
66 meter
Z = 1659002
90 Z = 505664
08
XDOT = -13222
098733 XDOT = -4030
095694
YDOT = 5098
918116 feet/sec YDOT = 1554
150242 meter/sec
ZDOT = -19704
753936 ZDOT = -6006
009000
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 10242
95183094
00016717 00000-0 10270-3 0 9128
2 25544 51
6421 208
0480 0008590 314
2412 45
8044 15
71445787 35239
Satellite: ISS
Catalog Number: 25544
Epoch time: 10242
95183094 = yrday
fracday
Element set: 912
Inclination: 51
6421 deg
RA of node: 208
0480 deg
Eccentricity:
0008590
Arg of perigee: 314
2412 deg
Mean anomaly: 45
8044 deg
Mean motion: 15
71445787 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3523
Checksum: 291
Coasting Arc #14 (Orbit 3538)
---------------------------------------
Vector Time (GMT): 2010/243/22:03:25
906
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1889
33 A = 6728302
15 meter
Y = -4383880
27 meter E =
0003776
Z = 5104807
54 I = 51
49363
XDOT = 7355
579597 Wp = 333
24889
YDOT = 1714
779628 meter/sec RA = 202
08633 deg
ZDOT = 1479
071250 TA = 102
55580
MA = 102
51356
Ha = 194
281 n
mi
Hp = 189
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6198
58 X = 22333
89
Y = -14382809
27 feet Y = -4383765
94 meter
Z = 16748056
24 Z = 5104857
22
XDOT = 24132
478993 XDOT = 7328
672856
YDOT = 5625
917416 feet/sec YDOT = 1796
883688 meter/sec
ZDOT = 4852
595965 ZDOT = 1514
739358
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10941404
00 X = 3334939
94
Y = -9335245
54 feet Y = -2845382
84 meter
Z = 16748178
95 Z = 5104844
94
XDOT = 10522
285200 XDOT = 3207
192529
YDOT = 21272
790314 feet/sec YDOT = 6483
946488 meter/sec
ZDOT = 4995
385679 ZDOT = 1522
593555
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 10243
96934315
00016717 00000-0 10270-3 0 9131
2 25544 51
6414 202
8422 0008293 317
8234 42
2289 15
71392691 35394
Satellite: ISS
Catalog Number: 25544
Epoch time: 10243
96934315 = yrday
fracday
Element set: 913
Inclination: 51
6414 deg
RA of node: 202
8422 deg
Eccentricity:
0008293
Arg of perigee: 317
8234 deg
Mean anomaly: 42
2289 deg
Mean motion: 15
71392691 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3539
Checksum: 309
Coasting Arc #15 (Orbit 3553)
---------------------------------------
Vector Time (GMT): 2010/244/22:03:25
906
Vector Time (MET): N/A
Weight (LBS) : 826788
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6395333
82 A = 6737495
60 meter
Y = -215717
68 meter E =
0011121
Z = -2086029
80 I = 51
55448
XDOT = -1631
996894 Wp = 355
56441
YDOT = -5093
355816 meter/sec RA = 196
93088 deg
ZDOT = 5538
999434 TA = 341
12364
MA = 341
16484
Ha = 194
229 n
mi
Hp = 189
033
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20982066
35 X = -6382312
76
Y = -707735
16 feet Y = -287161
31 meter
Z = -6843929
81 Z = -2117066
68
XDOT = -5354
320520 XDOT = -1601
828196
YDOT = -16710
484962 feet/sec YDOT = -5111
437153 meter/sec
ZDOT = 18172
570321 ZDOT = 5531
144432
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13214633
00 X = -4027820
14
Y = -16260548
22 feet Y = -4956215
10 meter
Z = -6968171
83 Z = -2123898
77
XDOT = 7832
453658 XDOT = 2387
331875
YDOT = -14126
976756 feet/sec YDOT = -4305
902515 meter/sec
ZDOT = 18141
038828 ZDOT = 5529
388635
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 10244
92324078
00016717 00000-0 10270-3 0 9148
2 25544 51
6421 197
9622 0008140 320
7825 39
2746 15
71446140 35548
Satellite: ISS
Catalog Number: 25544
Epoch time: 10244
92324078 = yrday
fracday
Element set: 914
Inclination: 51
6421 deg
RA of node: 197
9622 deg
Eccentricity:
0008140
Arg of perigee: 320
7825 deg
Mean anomaly: 39
2746 deg
Mean motion: 15
71446140 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3554
Checksum: 300
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