[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 8th 2011
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 29708 39 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 114 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 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
343/19:50:40
741 3
2 4
3 4
3
N/A 1
3 -0
4 223
2
000/00:01:21
483 2
5 -0
0 201
2
Coasting Arc #1 (Orbit 2765)
---------------------------------------
Vector Time (GMT): 2011/339/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5598147
18 A = 6770848
19 meter
Y = 1134191
56 meter E =
0038053
Z = 3590555
76 I = 51
75463
XDOT = -3866
309313 Wp = 116
96582
YDOT = -4961
219320 meter/sec RA = 18
24790 deg
ZDOT = -4441
823163 TA = 20
37471
MA = 20
22330
Ha = 224
091 n
mi
Hp = 198
129
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18366624
61 X = -5627856
35
Y = 3721100
93 feet Y = 1071423
35 meter
Z = 11780038
58 Z = 3563287
51
XDOT = -12684
741841 XDOT = -3788
966774
YDOT = -16276
966273 feet/sec YDOT = -5004
022087 meter/sec
ZDOT = -14572
910639 ZDOT = -4460
418321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1783432
80 X = 543590
32
Y = -18724661
29 feet Y = -5707276
76 meter
Z = 11668557
23 Z = 3556576
24
XDOT = 17865
161112 XDOT = 5445
301107
YDOT = -7466
252221 feet/sec YDOT = -2275
713677 meter/sec
ZDOT = -14648
439141 ZDOT = -4464
844250
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 11339
53966918
00016717 00000-0 10270-3 0 9001
2 25544 51
6418 18
6083 0028290 129
9777 230
3869 15
58631332 27665
Satellite: ISS
Catalog Number: 25544
Epoch time: 11339
53966918 = yrday
fracday
Element set: 900
Inclination: 51
6418 deg
RA of node: 18
6083 deg
Eccentricity:
0028290
Arg of perigee: 129
9777 deg
Mean anomaly: 230
3869 deg
Mean motion: 15
58631332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2766
Checksum: 340
Coasting Arc #2 (Orbit 2780)
---------------------------------------
Vector Time (GMT): 2011/340/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6675195
75 A = 6775951
91 meter
Y = 950962
94 meter E =
0029631
Z = -767023
02 I = 51
74323
XDOT = -22
170526 Wp = 112
16779
YDOT = 4817
538820 meter/sec RA = 13
25434 deg
ZDOT = 5953
234303 TA = 239
55624
MA = 239
84930
Ha = 223
914 n
mi
Hp = 198
250
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21900248
53 X = 6667791
89
Y = 3119957
15 feet Y = 1025567
73 meter
Z = -2516479
74 Z = -734612
38
XDOT = -72
737946 XDOT = -104
959696
YDOT = 15805
573555 feet/sec YDOT = 4816
827597 meter/sec
ZDOT = 19531
608605 ZDOT = 5952
925821
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8992771
37 X = -2740996
71
Y = 20227047
44 feet Y = 6165204
06 meter
Z = -2384177
70 Z = -726697
36
XDOT = -13677
230652 XDOT = -4168
819903
YDOT = -3849
526465 feet/sec YDOT = -1173
335667 meter/sec
ZDOT = 19529
927556 ZDOT = 5952
721919
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 11340
50140691
00016717 00000-0 10270-3 0 9013
2 25544 51
6420 13
7816 0028318 133
3318 227
0204 15
58656906 27816
Satellite: ISS
Catalog Number: 25544
Epoch time: 11340
50140691 = yrday
fracday
Element set: 901
Inclination: 51
6420 deg
RA of node: 13
7816 deg
Eccentricity:
0028318
Arg of perigee: 133
3318 deg
Mean anomaly: 227
0204 deg
Mean motion: 15
58656906 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2781
Checksum: 283
Coasting Arc #3 (Orbit 2796)
---------------------------------------
Vector Time (GMT): 2011/341/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5665862
29 A = 6773393
18 meter
Y = -2774528
82 meter E =
0033682
Z = -2445682
68 I = 51
70608
XDOT = 4086
751047 Wp = 135
63571
YDOT = -3681
809403 meter/sec RA = 8
26664 deg
ZDOT = -5358
730072 TA = 71
78667
MA = 71
42032
Ha = 223
683 n
mi
Hp = 198
254
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18588787
04 X = -5622535
00
Y = -9102784
86 feet Y = -2837645
51 meter
Z = -8023893
32 Z = -2473102
83
XDOT = 13407
975875 XDOT = 4153
650146
YDOT = -12079
427176 feet/sec YDOT = -3635
734340 meter/sec
ZDOT = -17581
135408 ZDOT = -5338
714158
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13559411
58 X = 4132908
65
Y = -15580121
07 feet Y = -4748820
90 meter
Z = -8135646
54 Z = -2479745
06
XDOT = 7068
347478 XDOT = 2154
432311
YDOT = 15174
540237 feet/sec YDOT = 4625
199864 meter/sec
ZDOT = -17499
053616 ZDOT = -5333
711542
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 11341
52722342
00016717 00000-0 10270-3 0 9026
2 25544 51
6425 8
6313 0028339 137
1155 223
2217 15
58715637 27976
Satellite: ISS
Catalog Number: 25544
Epoch time: 11341
52722342 = yrday
fracday
Element set: 902
Inclination: 51
6425 deg
RA of node: 8
6313 deg
Eccentricity:
0028339
Arg of perigee: 137
1155 deg
Mean anomaly: 223
2217 deg
Mean motion: 15
58715637 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2797
Checksum: 296
Coasting Arc #4 (Orbit 2812)
---------------------------------------
Vector Time (GMT): 2011/342/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2971355
63 A = 6766457
11 meter
Y = 3873288
62 meter E =
0035767
Z = 4675137
24 I = 51
65169
XDOT = -6904
143610 Wp = 134
88776
YDOT = 1844
227472 meter/sec RA = 3
24997 deg
ZDOT = 2822
159165 TA = 286
98871
MA = 287
38037
Ha = 223
557 n
mi
Hp = 198
344
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9748542
10 X = 2905111
64
Y = 12707639
82 feet Y = 3906145
27 meter
Z = 15338376
77 Z = 4689411
77
XDOT = -22651
389798 XDOT = -6937
962711
YDOT = 6050
615065 feet/sec YDOT = 1766
831720 meter/sec
ZDOT = 9259
052378 ZDOT = 2788
536428
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14655477
65 X = -4466989
59
Y = 6320905
07 feet Y = 1926611
87 meter
Z = 15396334
60 Z = 4692802
79
XDOT = 40
257013 XDOT = 12
270338
YDOT = -22426
959094 feet/sec YDOT = -6835
737132 meter/sec
ZDOT = 9121
554744 ZDOT = 2780
249886
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 11342
55300352
00016717 00000-0 10270-3 0 9034
2 25544 51
6410 3
4823 0028372 140
6081 219
7144 15
58770868 28138
Satellite: ISS
Catalog Number: 25544
Epoch time: 11342
55300352 = yrday
fracday
Element set: 903
Inclination: 51
6410 deg
RA of node: 3
4823 deg
Eccentricity:
0028372
Arg of perigee: 140
6081 deg
Mean anomaly: 219
7144 deg
Mean motion: 15
58770868 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2813
Checksum: 286
Coasting Arc #5 (Orbit 2827)
---------------------------------------
Vector Time (GMT): 2011/343/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 872020
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 799342
63 A = 6764047
98 meter
Y = -4201789
57 meter E =
0039464
Z = -5269776
09 I = 51
61432
XDOT = 7596
647194 Wp = 128
11235
YDOT = 403
902112 meter/sec RA = 358
20131 deg
ZDOT = 810
602120 TA = 149
77048
MA = 149
54222
Ha = 223
419 n
mi
Hp = 198
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2622515
19 X = 871868
35
Y = -13785398
86 feet Y = -4192444
69 meter
Z = -17289291
64 Z = -5265717
18
XDOT = 24923
383182 XDOT = 7587
628274
YDOT = 1325
138164 feet/sec YDOT = 488
801956 meter/sec
ZDOT = 2659
455773 ZDOT = 847
485172
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12828562
69 X = 3910145
91
Y = 5738369
70 feet Y = 1749055
08 meter
Z = -17272333
53 Z = -5264607
26
XDOT = -6438
254302 XDOT = -1962
379911
YDOT = 23045
620290 feet/sec YDOT = 7024
305064 meter/sec
ZDOT = 2810
069282 ZDOT = 856
509117
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 11343
51463845
00016717 00000-0 10270-3 0 9049
2 25544 51
6420 358
6541 0028198 144
3812 215
9232 15
58802631 28286
Satellite: ISS
Catalog Number: 25544
Epoch time: 11343
51463845 = yrday
fracday
Element set: 904
Inclination: 51
6420 deg
RA of node: 358
6541 deg
Eccentricity:
0028198
Arg of perigee: 144
3812 deg
Mean anomaly: 215
9232 deg
Mean motion: 15
58802631 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2828
Checksum: 309
Coasting Arc #6 (Orbit 2832)
---------------------------------------
Vector Time (GMT): 2011/343/19:51:21
483
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4682130
35 A = 6772164
58 meter
Y = -3228303
92 meter E =
0028829
Z = -3712474
52 I = 51
62583
XDOT = 5530
322428 Wp = 138
38521
YDOT = 3075
540731 meter/sec RA = 356
53886 deg
ZDOT = 4298
512437 TA = 177
40837
MA = 177
39340
Ha = 223
237 n
mi
Hp = 201
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15361320
03 X = 4735916
59
Y = -10591548
30 feet Y = -3175644
27 meter
Z = -12180034
50 Z = -3689598
26
XDOT = 18144
102453 XDOT = 5474
638497
YDOT = 10090
356730 feet/sec YDOT = 3137
072310 meter/sec
ZDOT = 14102
731093 ZDOT = 4325
244128
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12104715
50 X = 3689517
28
Y = -14279405
61 feet Y = -4352362
83 meter
Z = -12086303
28 Z = -3683905
24
XDOT = 19035
749141 XDOT = 5802
096338
YDOT = 4102
623769 feet/sec YDOT = 1250
479725 meter/sec
ZDOT = 14211
639598 ZDOT = 4331
707749
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 11343
83517616
00016717 00000-0 10270-3 0 9051
2 25544 51
6435 357
0445 0024683 147
0088 213
2613 15
58063311 28332
Satellite: ISS
Catalog Number: 25544
Epoch time: 11343
83517616 = yrday
fracday
Element set: 905
Inclination: 51
6435 deg
RA of node: 357
0445 deg
Eccentricity:
0024683
Arg of perigee: 147
0088 deg
Mean anomaly: 213
2613 deg
Mean motion: 15
58063311 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2833
Checksum: 297
Coasting Arc #7 (Orbit 2848)
---------------------------------------
Vector Time (GMT): 2011/344/19:51:21
483
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6434939
68 A = 6777507
64 meter
Y = 1779749
60 meter E =
0037478
Z = 1026719
82 I = 51
61351
XDOT = -2178
317774 Wp = 141
07599
YDOT = -4413
121770 meter/sec RA = 351
53733 deg
ZDOT = -5914
674633 TA = 27
74299
MA = 27
54357
Ha = 223
181 n
mi
Hp = 201
247
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21112006
83 X = -6459350
58
Y = 5839073
49 feet Y = 1707653
53 meter
Z = 3368503
33 Z = 995399
64
XDOT = -7146
711857 XDOT = -2100
074894
YDOT = -14478
745964 feet/sec YDOT = -4437
042793 meter/sec
ZDOT = -19405
100502 ZDOT = -5925
067492
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18656340
86 X = -5686452
69
Y = 11515168
66 feet Y = 3509823
41 meter
Z = 3240410
87 Z = 987677
23
XDOT = -9957
913389 XDOT = -3035
172001
YDOT = -10576
366722 feet/sec YDOT = -3223
676577 meter/sec
ZDOT = -19447
150446 ZDOT = -5927
491456
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 11344
86139511
00016717 00000-0 10270-3 0 9060
2 25544 51
6434 351
8976 0024831 150
9502 209
3040 15
58067343 28497
Satellite: ISS
Catalog Number: 25544
Epoch time: 11344
86139511 = yrday
fracday
Element set: 906
Inclination: 51
6434 deg
RA of node: 351
8976 deg
Eccentricity:
0024831
Arg of perigee: 150
9502 deg
Mean anomaly: 209
3040 deg
Mean motion: 15
58067343 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2849
Checksum: 311
Coasting Arc #8 (Orbit 2864)
---------------------------------------
Vector Time (GMT): 2011/345/19:51:21
483
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6499218
90 A = 6775998
38 meter
Y = 21569
80 meter E =
0029001
Z = 1933097
38 I = 51
57976
XDOT = -1700
806239 Wp = 125
18446
YDOT = 4963
493315 meter/sec RA = 346
54464 deg
ZDOT = 5587
101577 TA = 256
15420
MA = 256
47703
Ha = 222
854 n
mi
Hp = 201
343
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21322896
67 X = 6489104
02
Y = 70767
06 feet Y = 94191
24 meter
Z = 6342183
01 Z = 1964646
07
XDOT = -5580
072961 XDOT = -1783
323760
YDOT = 16284
426885 feet/sec YDOT = 4944
011738 meter/sec
ZDOT = 18330
385751 ZDOT = 5578
639268
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20350830
84 X = 6202933
24
Y = -6234054
69 feet Y = -1900139
87 meter
Z = 6471047
96 Z = 1972375
42
XDOT = -1068
324472 XDOT = -325
625299
YDOT = 15756
226503 feet/sec YDOT = 4802
497838 meter/sec
ZDOT = 18295
369170 ZDOT = 5576
428523
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 11345
88757679
00016717 00000-0 10270-3 0 9075
2 25544 51
6435 346
7507 0024555 154
6151 205
6216 15
58154608 28658
Satellite: ISS
Catalog Number: 25544
Epoch time: 11345
88757679 = yrday
fracday
Element set: 907
Inclination: 51
6435 deg
RA of node: 346
7507 deg
Eccentricity:
0024555
Arg of perigee: 154
6151 deg
Mean anomaly: 205
6216 deg
Mean motion: 15
58154608 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2865
Checksum: 337
Coasting Arc #9 (Orbit 2879)
---------------------------------------
Vector Time (GMT): 2011/346/19:51:21
483
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4763462
50 A = 6769304
44 meter
Y = -2054783
21 meter E =
0026204
Z = -4352016
83 I = 51
52892
XDOT = 5095
213953 Wp = 138
02461
YDOT = -4586
185268 meter/sec RA = 341
52821 deg
ZDOT = -3442
621254 TA = 97
15017
MA = 96
85215
Ha = 222
560 n
mi
Hp = 201
484
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15628157
80 X = -4718990
21
Y = -6741414
74 feet Y = -2107801
98 meter
Z = -14278270
43 Z = -4375049
90
XDOT = 16716
581209 XDOT = 5162
842483
YDOT = -15046
539594 feet/sec YDOT = -4528
828906 meter/sec
ZDOT = -11294
689154 ZDOT = -3417
705059
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16870048
21 X = -5141990
69
Y = -1548289
43 feet Y = -471918
62 meter
Z = -14372169
94 Z = -4380637
40
XDOT = 11129
357243 XDOT = 3392
228088
YDOT = -18308
292107 feet/sec YDOT = -5580
367434 meter/sec
ZDOT = -11192
497707 ZDOT = -3411
473301
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 11346
84959020
00016717 00000-0 10270-3 0 9087
2 25544 51
6437 341
9247 0024477 158
5137 201
7051 15
58210282 28800
Satellite: ISS
Catalog Number: 25544
Epoch time: 11346
84959020 = yrday
fracday
Element set: 908
Inclination: 51
6437 deg
RA of node: 341
9247 deg
Eccentricity:
0024477
Arg of perigee: 158
5137 deg
Mean anomaly: 201
7051 deg
Mean motion: 15
58210282 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2880
Checksum: 311
Coasting Arc #10 (Orbit 2895)
---------------------------------------
Vector Time (GMT): 2011/347/19:51:21
483
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1896717
78 A = 6765298
98 meter
Y = 3761653
34 meter E =
0025698
Z = 5285425
94 I = 51
48782
XDOT = -6978
356037 Wp = 156
67225
YDOT = 3208
239447 meter/sec RA = 336
48189 deg
ZDOT = 197
425268 TA = 291
30879
MA = 291
58295
Ha = 222
390 n
mi
Hp = 201
650
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6222827
36 X = 1828837
76
Y = 12341382
36 feet Y = 3782483
50 meter
Z = 17340636
30 Z = 5294475
67
XDOT = -22894
868889 XDOT = -7014
671609
YDOT = 10525
719971 feet/sec YDOT = 3130
000116 meter/sec
ZDOT = 647
720696 ZDOT = 163
436731
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9835503
70 X = 2997861
53
Y = 9644918
39 feet Y = 2939771
12 meter
Z = 17377266
26 Z = 5296590
76
XDOT = -17461
598625 XDOT = -5322
295261
YDOT = 16751
683499 feet/sec YDOT = 5105
913130 meter/sec
ZDOT = 508
595815 ZDOT = 155
020005
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 11347
87570461
00016717 00000-0 10270-3 0 9090
2 25544 51
6439 336
7780 0024542 162
1531 198
0491 15
58275707 28964
Satellite: ISS
Catalog Number: 25544
Epoch time: 11347
87570461 = yrday
fracday
Element set: 909
Inclination: 51
6439 deg
RA of node: 336
7780 deg
Eccentricity:
0024542
Arg of perigee: 162
1531 deg
Mean anomaly: 198
0491 deg
Mean motion: 15
58275707 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2896
Checksum: 338
Coasting Arc #11 (Orbit 2910)
---------------------------------------
Vector Time (GMT): 2011/348/19:51:21
483
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1443484
63 A = 6768606
55 meter
Y = -4868603
21 meter E =
0030884
Z = -4502817
70 I = 51
47129
XDOT = 6910
652319 Wp = 150
72819
YDOT = -893
919690 meter/sec RA = 331
42902 deg
ZDOT = 3164
737237 TA = 151
26762
MA = 151
09715
Ha = 222
222 n
mi
Hp = 201
848
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4735841
97 X = 1519692
76
Y = -15973107
65 feet Y = -4852034
78 meter
Z = -14773023
93 Z = -4495620
61
XDOT = 22672
743830 XDOT = 6904
761076
YDOT = -2932
807382 feet/sec YDOT = -816
673753 meter/sec
ZDOT = 10382
996185 ZDOT = 3198
294567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -981509
61 X = -299164
13
Y = -16657895
10 feet Y = -5077326
43 meter
Z = -14743194
12 Z = -4493725
57
XDOT = 18995
406971 XDOT = 5789
800045
YDOT = -10480
144461 feet/sec YDOT = -3194
348032 meter/sec
ZDOT = 10520
152064 ZDOT = 3206
542349
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 11348
83765465
00016717 00000-0 10270-3 0 9109
2 25544 51
6434 331
9511 0024449 165
8719 194
3125 15
58325021 29118
Satellite: ISS
Catalog Number: 25544
Epoch time: 11348
83765465 = yrday
fracday
Element set: 910
Inclination: 51
6434 deg
RA of node: 331
9511 deg
Eccentricity:
0024449
Arg of perigee: 165
8719 deg
Mean anomaly: 194
3125 deg
Mean motion: 15
58325021 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2911
Checksum: 311
Coasting Arc #12 (Orbit 2926)
---------------------------------------
Vector Time (GMT): 2011/349/19:51:21
483
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4165345
42 A = 6775063
80 meter
Y = 4848296
26 meter E =
0033708
Z = 2176977
45 I = 51
46743
XDOT = -5061
164842 Wp = 147
98106
YDOT = -1880
990418 meter/sec RA = 326
40452 deg
ZDOT = -5484
012154 TA = 7
67953
MA = 7
62804
Ha = 222
039 n
mi
Hp = 201
985
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13665831
42 X = -4229825
74
Y = 15906483
80 feet Y = 4801356
13 meter
Z = 7142314
47 Z = 2156586
05
XDOT = -16604
871528 XDOT = -5013
114911
YDOT = -6171
228405 feet/sec YDOT = -1937
318429 meter/sec
ZDOT = -17992
165859 ZDOT = -5508
482550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7040701
36 X = -2146005
77
Y = 19783543
24 feet Y = 6030023
98 meter
Z = 7058595
63 Z = 2151459
95
XDOT = -16168
859234 XDOT = -4928
268295
YDOT = 713
463472 feet/sec YDOT = 217
463666 meter/sec
ZDOT = -18091
958724 ZDOT = -5514
429019
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 11349
86370114
00016717 00000-0 10270-3 0 9117
2 25544 51
6437 326
8041 0024465 169
3969 190
7707 15
58368447 29278
Satellite: ISS
Catalog Number: 25544
Epoch time: 11349
86370114 = yrday
fracday
Element set: 911
Inclination: 51
6437 deg
RA of node: 326
8041 deg
Eccentricity:
0024465
Arg of perigee: 169
3969 deg
Mean anomaly: 190
7707 deg
Mean motion: 15
58368447 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2927
Checksum: 339
Coasting Arc #13 (Orbit 2942)
---------------------------------------
Vector Time (GMT): 2011/350/19:51:21
483
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5663682
62 A = 6776436
38 meter
Y = -3635462
78 meter E =
0021586
Z = 868640
96 I = 51
44727
XDOT = 1947
494734 Wp = 139
82317
YDOT = 4468
938730 meter/sec RA = 321
40011 deg
ZDOT = 5907
061201 TA = 229
59763
MA = 229
78620
Ha = 221
787 n
mi
Hp = 202
060
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18581635
88 X = 5699694
46
Y = -11927371
31 feet Y = -3571926
69 meter
Z = 2849871
92 Z = 896242
29
XDOT = 6389
418420 XDOT = 1868
682120
YDOT = 14661
872475 feet/sec YDOT = 4490
275824 meter/sec
ZDOT = 19380
122052 ZDOT = 5916
330900
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12696790
96 X = 3869981
88
Y = -18046431
56 feet Y = -5500552
34 meter
Z = 2962930
23 Z = 903101
13
XDOT = 10021
787547 XDOT = 3054
640844
YDOT = 10290
035565 feet/sec YDOT = 3136
402840 meter/sec
ZDOT = 19417
600719 ZDOT = 5918
484699
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 11350
88970947
00016717 00000-0 10270-3 0 9122
2 25544 51
6426 321
6555 0024533 173
6526 186
4945 15
58450361 29433
Satellite: ISS
Catalog Number: 25544
Epoch time: 11350
88970947 = yrday
fracday
Element set: 912
Inclination: 51
6426 deg
RA of node: 321
6555 deg
Eccentricity:
0024533
Arg of perigee: 173
6526 deg
Mean anomaly: 186
4945 deg
Mean motion: 15
58450361 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2943
Checksum: 329
Coasting Arc #14 (Orbit 2957)
---------------------------------------
Vector Time (GMT): 2011/351/19:51:21
483
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5542766
65 A = 6770876
61 meter
Y = 1230887
56 meter E =
0024278
Z = -3674011
63 I = 51
40471
XDOT = 1475
873293 Wp = 163
26922
YDOT = -6174
567593 meter/sec RA = 316
38345 deg
ZDOT = -4325
122417 TA = 60
76554
MA = 60
52299
Ha = 221
478 n
mi
Hp = 202
280
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18184929
94 X = -5538271
05
Y = 4038345
01 feet Y = 1168930
26 meter
Z = -12053843
92 Z = -3700927
39
XDOT = 4842
103979 XDOT = 1565
819489
YDOT = -20257
767693 feet/sec YDOT = -6157
560343 meter/sec
ZDOT = -14190
034178 ZDOT = -4317
734453
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15068468
89 X = -4592869
32
Y = 10829407
51 feet Y = 3300803
41 meter
Z = -12163890
77 Z = -3707553
91
XDOT = -2638
834743 XDOT = -804
316830
YDOT = -19466
665485 feet/sec YDOT = -5933
439640 meter/sec
ZDOT = -14159
329261 ZDOT = -4315
763559
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 11351
85156268
00016717 00000-0 10270-3 0 9133
2 25544 51
6415 316
8287 0024467 177
2744 182
8548 15
58462851 29589
Satellite: ISS
Catalog Number: 25544
Epoch time: 11351
85156268 = yrday
fracday
Element set: 913
Inclination: 51
6415 deg
RA of node: 316
8287 deg
Eccentricity:
0024467
Arg of perigee: 177
2744 deg
Mean anomaly: 182
8548 deg
Mean motion: 15
58462851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2958
Checksum: 346
Coasting Arc #15 (Orbit 2973)
---------------------------------------
Vector Time (GMT): 2011/352/19:51:21
483
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4043130
12 A = 6765179
96 meter
Y = 1656618
78 meter E =
0026961
Z = 5167008
47 I = 51
36446
XDOT = -4208
303047 Wp = 173
00749
YDOT = 6294
836199 meter/sec RA = 311
33262 deg
ZDOT = 1247
743807 TA = 264
82475
MA = 265
13250
Ha = 221
325 n
mi
Hp = 202
441
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13264862
60 X = 3999204
51
Y = 5435101
00 feet Y = 1701585
66 meter
Z = 16952127
53 Z = 5186543
45
XDOT = -13806
768526 XDOT = -4284
441715
YDOT = 20652
349735 feet/sec YDOT = 6247
350588 meter/sec
ZDOT = 4093
647661 ZDOT = 1227
115210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14234308
24 X = 4338617
15
Y = -417733
92 feet Y = -127325
30 meter
Z = 17031779
05 Z = 5191286
25
XDOT = -4213
591658 XDOT = -1284
302737
YDOT = 23463
749776 feet/sec YDOT = 7151
750932 meter/sec
ZDOT = 4008
854434 ZDOT = 1221
898831
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 11352
87750479
00016717 00000-0 10270-3 0 9141
2 25544 51
6414 311
6801 0024466 180
7620 179
3502 15
58493379 29742
Satellite: ISS
Catalog Number: 25544
Epoch time: 11352
87750479 = yrday
fracday
Element set: 914
Inclination: 51
6414 deg
RA of node: 311
6801 deg
Eccentricity:
0024466
Arg of perigee: 180
7620 deg
Mean anomaly: 179
3502 deg
Mean motion: 15
58493379 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2974
Checksum: 327
Coasting Arc #16 (Orbit 2988)
---------------------------------------
Vector Time (GMT): 2011/353/19:51:21
483
Vector Time (MET): N/A
Weight (LBS) : 871622
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1582728
34 A = 6766277
41 meter
Y = -4436020
61 meter E =
0029591
Z = -4876532
22 I = 51
34830
XDOT = 5671
754461 Wp = 160
83006
YDOT = -4597
393751 meter/sec RA = 306
26410 deg
ZDOT = 2317
840101 TA = 132
09225
MA = 131
84025
Ha = 221
120 n
mi
Hp = 202
489
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5192678
28 X = -1509316
79
Y = -14553873
41 feet Y = -4453308
84 meter
Z = -15999121
47 Z = -4884043
17
XDOT = 18608
118312 XDOT = 5711
482177
YDOT = -15083
312832 feet/sec YDOT = -4533
746747 meter/sec
ZDOT = 7604
462274 ZDOT = 2345
489818
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10790186
24 X = -3288848
77
Y = -11017279
05 feet Y = -3358066
65 meter
Z = -16029425
13 Z = -4885768
78
XDOT = 9604
498597 XDOT = 2927
451172
YDOT = -20747
042795 feet/sec YDOT = -6323
698644 meter/sec
ZDOT = 7717
787279 ZDOT = 2352
381563
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 11353
83929046
00016717 00000-0 10270-3 0 9157
2 25544 51
6400 306
8511 0024546 184
4311 175
6631 15
58584364 29891
Satellite: ISS
Catalog Number: 25544
Epoch time: 11353
83929046 = yrday
fracday
Element set: 915
Inclination: 51
6400 deg
RA of node: 306
8511 deg
Eccentricity:
0024546
Arg of perigee: 184
4311 deg
Mean anomaly: 175
6631 deg
Mean motion: 15
58584364 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2989
Checksum: 322
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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