[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 16th 2012
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13454 89 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 129 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 331 ET - UTC (sec) : 67 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
351/13:37:55
332 -0
8 1
4 1
4
N/A 1
1 0
1 230
5
000/00:07:50
665 -0
5 0
3 212
7
Coasting Arc #1 (Orbit 600)
---------------------------------------
Vector Time (GMT): 2012/349/08:59:06
294
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4246599
24 A = 6783929
38 meter
Y = 1152529
54 meter E =
0017404
Z = 5149121
54 I = 51
34552
XDOT = -3478
683398 Wp = 52
81298
YDOT = 6704
542714 meter/sec RA = 305
79747 deg
ZDOT = 1375
398515 TA = 23
96554
MA = 23
88463
Ha = 229
713 n
mi
Hp = 212
984
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13932412
22 X = 4208382
57
Y = 3781264
91 feet Y = 1199803
30 meter
Z = 16893443
37 Z = 5169658
63
XDOT = -11413
003273 XDOT = -3560
077823
YDOT = 21996
531214 feet/sec YDOT = 6665
186616 meter/sec
ZDOT = 4512
462318 ZDOT = 1358
302443
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13282477
78 X = -4048499
23
Y = 5395097
57 feet Y = 1644425
74 meter
Z = 16978433
67 Z = 5175026
58
XDOT = -3880
164660 XDOT = -1182
674188
YDOT = -23454
431845 feet/sec YDOT = -7148
910826 meter/sec
ZDOT = 4440
681677 ZDOT = 1353
519775
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 12349
42504399
00016717 00000-0 10270-3 0 9002
2 25544 51
6470 306
1748 0016569 38
8375 321
3964 15
52071556 6017
Satellite: ISS
Catalog Number: 25544
Epoch time: 12349
42504399 = yrday
fracday
Element set: 900
Inclination: 51
6470 deg
RA of node: 306
1748 deg
Eccentricity:
0016569
Arg of perigee: 38
8375 deg
Mean anomaly: 321
3964 deg
Mean motion: 15
52071556 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 601
Checksum: 313
Coasting Arc #2 (Orbit 615)
---------------------------------------
Vector Time (GMT): 2012/350/08:59:06
294
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3781479
19 A = 6783354
42 meter
Y = -1950353
82 meter E =
0028847
Z = -5305937
44 I = 51
32665
XDOT = 3759
395531 Wp = 63
70951
YDOT = -6653
626310 meter/sec RA = 300
79918 deg
ZDOT = -221
970024 TA = 204
09168
MA = 204
22688
Ha = 229
850 n
mi
Hp = 212
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12406427
79 X = -3733614
00
Y = -6398798
63 feet Y = -1992372
43 meter
Z = -17407931
24 Z = -5324191
55
XDOT = 12333
974840 XDOT = 3834
596644
YDOT = -21829
482643 feet/sec YDOT = -6611
165899 meter/sec
ZDOT = -728
248109 ZDOT = -203
525289
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13614700
49 X = 4149760
71
Y = -2621514
13 feet Y = -799037
51 meter
Z = -17483356
04 Z = -5328926
92
XDOT = 3694
355719 XDOT = 1126
039623
YDOT = 23779
416150 feet/sec YDOT = 7247
966043 meter/sec
ZDOT = -650
888607 ZDOT = -198
390847
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 12350
39084591
00016717 00000-0 10270-3 0 9018
2 25544 51
6471 301
3761 0016530 42
1759 318
0661 15
52078618 6161
Satellite: ISS
Catalog Number: 25544
Epoch time: 12350
39084591 = yrday
fracday
Element set: 901
Inclination: 51
6471 deg
RA of node: 301
3761 deg
Eccentricity:
0016530
Arg of perigee: 42
1759 deg
Mean anomaly: 318
0661 deg
Mean motion: 15
52078618 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 616
Checksum: 293
Coasting Arc #3 (Orbit 631)
---------------------------------------
Vector Time (GMT): 2012/351/08:59:06
294
Vector Time (MET): N/A
Weight (LBS) : 891020
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3277259
84 A = 6783510
33 meter
Y = 2819195
10 meter E =
0020089
Z = 5216654
06 I = 51
31205
XDOT = -3997
878586 Wp = 47
54810
YDOT = 6478
792941 meter/sec RA = 295
79730 deg
ZDOT = -973
956657 TA = 51
89869
MA = 51
71771
Ha = 229
775 n
mi
Hp = 212
617
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10752164
84 X = 3220150
34
Y = 9249327
75 feet Y = 2855523
65 meter
Z = 17115006
76 Z = 5232436
25
XDOT = -13116
399561 XDOT = -4065
297460
YDOT = 21255
882353 feet/sec YDOT = 6433
709296 meter/sec
ZDOT = -3195
395856 ZDOT = -993
541139
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14098596
76 X = -4297252
29
Y = -396447
03 feet Y = -120837
05 meter
Z = 17180074
74 Z = 5236486
78
XDOT = -3389
724011 XDOT = -1033
187879
YDOT = -23711
078914 feet/sec YDOT = -7227
136853 meter/sec
ZDOT = -3277
449543 ZDOT = -998
966621
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 12351
42101783
00016717 00000-0 10270-3 0 9027
2 25544 51
6463 296
2557 0016542 45
7282 314
5224 15
52126163 6323
Satellite: ISS
Catalog Number: 25544
Epoch time: 12351
42101783 = yrday
fracday
Element set: 902
Inclination: 51
6463 deg
RA of node: 296
2557 deg
Eccentricity:
0016542
Arg of perigee: 45
7282 deg
Mean anomaly: 314
5224 deg
Mean motion: 15
52126163 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 632
Checksum: 284
Coasting Arc #4 (Orbit 634)
---------------------------------------
Vector Time (GMT): 2012/351/13:41:50
665
Vector Time (MET): N/A
Weight (LBS) : 890855
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2108985
54 A = 6786482
92 meter
Y = 4406344
03 meter E =
0024877
Z = 4700222
91 I = 51
31896
XDOT = -4853
547706 Wp = 53
27415
YDOT = 5272
333509 meter/sec RA = 294
80545 deg
ZDOT = -2740
169585 TA = 64
08090
MA = 63
82471
Ha = 230
506 n
mi
Hp = 212
661
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6919243
89 X = 2036723
72
Y = 14456509
29 feet Y = 4429523
56 meter
Z = 15420678
83 Z = 4710293
05
XDOT = -15923
712947 XDOT = -4898
832318
YDOT = 17297
682115 feet/sec YDOT = 5217
805151 meter/sec
ZDOT = -8990
057693 ZDOT = -2763
857204
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11201250
97 X = -3414141
30
Y = 11407318
06 feet Y = 3476950
54 meter
Z = 15461856
41 Z = 4712773
83
XDOT = -20888
906838 XDOT = -6366
938804
YDOT = -8082
387564 feet/sec YDOT = -2463
511730 meter/sec
ZDOT = -9088
964637 ZDOT = -2770
316421
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 12351
61418416
00016717 00000-0 10270-3 0 9033
2 25544 51
6484 295
2966 0017179 49
2428 311
0212 15
51872064 6356
Satellite: ISS
Catalog Number: 25544
Epoch time: 12351
61418416 = yrday
fracday
Element set: 903
Inclination: 51
6484 deg
RA of node: 295
2966 deg
Eccentricity:
0017179
Arg of perigee: 49
2428 deg
Mean anomaly: 311
0212 deg
Mean motion: 15
51872064 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 635
Checksum: 303
Coasting Arc #5 (Orbit 649)
---------------------------------------
Vector Time (GMT): 2012/352/13:41:50
665
Vector Time (MET): N/A
Weight (LBS) : 890855
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1776769
18 A = 6788283
56 meter
Y = -5026746
06 meter E =
0022540
Z = -4215119
01 I = 51
31365
XDOT = 4797
790151 Wp = 69
94450
YDOT = -4725
710364 meter/sec RA = 289
81140 deg
ZDOT = 3636
748331 TA = 237
44502
MA = 237
66293
Ha = 230
526 n
mi
Hp = 212
461
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5829295
19 X = -1699951
07
Y = -16491949
01 feet Y = -5046185
20 meter
Z = -13829130
60 Z = -4223564
16
XDOT = 15740
781335 XDOT = 4832
611107
YDOT = -15504
299094 feet/sec YDOT = -4671
864031 meter/sec
ZDOT = 11931
589012 ZDOT = 3660
139828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13291748
29 X = 4051324
88
Y = -11328845
16 feet Y = -3453032
01 meter
Z = -13863499
29 Z = -4225594
58
XDOT = 19299
912666 XDOT = 5882
613380
YDOT = 8017
407056 feet/sec YDOT = 2443
705671 meter/sec
ZDOT = 12029
190322 ZDOT = 3666
497210
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 12352
58011362
00016717 00000-0 10270-3 0 9040
2 25544 51
6487 290
4981 0017178 52
7731 307
4985 15
51897674 6505
Satellite: ISS
Catalog Number: 25544
Epoch time: 12352
58011362 = yrday
fracday
Element set: 904
Inclination: 51
6487 deg
RA of node: 290
4981 deg
Eccentricity:
0017178
Arg of perigee: 52
7731 deg
Mean anomaly: 307
4985 deg
Mean motion: 15
51897674 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 650
Checksum: 329
Coasting Arc #6 (Orbit 665)
---------------------------------------
Vector Time (GMT): 2012/353/13:41:50
665
Vector Time (MET): N/A
Weight (LBS) : 890855
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1416130
31 A = 6790560
93 meter
Y = 5630872
49 meter E =
0028276
Z = 3507934
92 I = 51
31141
XDOT = -4766
889775 Wp = 69
48900
YDOT = 4010
235268 meter/sec RA = 284
81927 deg
ZDOT = -4473
677336 TA = 69
02024
MA = 68
71793
Ha = 230
566 n
mi
Hp = 212
356
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4646096
83 X = 1336018
82
Y = 18473991
11 feet Y = 5646260
43 meter
Z = 11508972
84 Z = 3514620
09
XDOT = -15639
402150 XDOT = -4789
646817
YDOT = 13156
939857 feet/sec YDOT = 3956
801926 meter/sec
ZDOT = -14677
419081 ZDOT = -4496
889573
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15371680
90 X = -4685288
34
Y = 11223355
35 feet Y = 3420878
71 meter
Z = 11535975
90 Z = 3516165
45
XDOT = -17241
335540 XDOT = -5255
159073
YDOT = -8296
693071 feet/sec YDOT = -2528
832048 meter/sec
ZDOT = -14774
179446 ZDOT = -4503
169895
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 12353
61042262
00016717 00000-0 10270-3 0 9059
2 25544 51
6483 285
3792 0017171 56
7144 303
5649 15
51909785 6667
Satellite: ISS
Catalog Number: 25544
Epoch time: 12353
61042262 = yrday
fracday
Element set: 905
Inclination: 51
6483 deg
RA of node: 285
3792 deg
Eccentricity:
0017171
Arg of perigee: 56
7144 deg
Mean anomaly: 303
5649 deg
Mean motion: 15
51909785 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 666
Checksum: 320
Coasting Arc #7 (Orbit 680)
---------------------------------------
Vector Time (GMT): 2012/354/13:41:50
665
Vector Time (MET): N/A
Weight (LBS) : 890855
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1186486
43 A = 6792419
23 meter
Y = -6092753
85 meter E =
0021905
Z = -2758756
59 I = 51
31177
XDOT = 4712
409289 Wp = 59
67297
YDOT = -3214
075652 meter/sec RA = 279
82995 deg
ZDOT = 5112
928330 TA = 268
97349
MA = 269
22446
Ha = 230
513 n
mi
Hp = 212
198
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3892672
03 X = -1104866
44
Y = -19989349
89 feet Y = -6105565
39 meter
Z = -9051038
69 Z = -2764322
50
XDOT = 15460
660397 XDOT = 4723
162173
YDOT = -10544
867625 feet/sec YDOT = -3161
318662 meter/sec
ZDOT = 16774
699245 ZDOT = 5135
846874
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16859873
34 X = 5138889
39
Y = -11404704
10 feet Y = -3476153
81 meter
Z = -9073351
17 Z = -2765557
44
XDOT = 14911
115367 XDOT = 4544
907964
YDOT = 8729
513968 feet/sec YDOT = 2660
755857 meter/sec
ZDOT = 16870
136898 ZDOT = 5142
017727
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 12354
57632138
00016717 00000-0 10270-3 0 9063
2 25544 51
6488 280
5804 0017126 60
0980 300
1871 15
51952499 6816
Satellite: ISS
Catalog Number: 25544
Epoch time: 12354
57632138 = yrday
fracday
Element set: 906
Inclination: 51
6488 deg
RA of node: 280
5804 deg
Eccentricity:
0017126
Arg of perigee: 60
0980 deg
Mean anomaly: 300
1871 deg
Mean motion: 15
51952499 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 681
Checksum: 313
Coasting Arc #8 (Orbit 696)
---------------------------------------
Vector Time (GMT): 2012/355/13:41:50
665
Vector Time (MET): N/A
Weight (LBS) : 890855
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 908548
21 A = 6794291
69 meter
Y = 6478746
50 meter E =
0028163
Z = 1813606
69 I = 51
31336
XDOT = -4704
718314 Wp = 86
28514
YDOT = 2253
744742 meter/sec RA = 274
84302 deg
ZDOT = -5616
664232 TA = 73
70148
MA = 73
39191
Ha = 230
579 n
mi
Hp = 212
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2980801
20 X = 827223
89
Y = 21255729
97 feet Y = 6488451
65 meter
Z = 5950153
19 Z = 1817823
15
XDOT = -15435
427539 XDOT = -4702
286046
YDOT = 7394
175664 feet/sec YDOT = 2201
147510 meter/sec
ZDOT = -18427
376088 ZDOT = -5639
513494
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18182050
33 X = -5541888
94
Y = 11397611
36 feet Y = 3473991
94 meter
Z = 5966829
70 Z = 1818689
69
XDOT = -12192
099731 XDOT = -3716
151998
YDOT = -9619
944494 feet/sec YDOT = -2932
159082 meter/sec
ZDOT = -18522
404381 ZDOT = -5645
628855
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 12355
60659865
00016717 00000-0 10270-3 0 9075
2 25544 51
6485 275
4608 0017112 64
1399 296
1515 15
51945044 6976
Satellite: ISS
Catalog Number: 25544
Epoch time: 12355
60659865 = yrday
fracday
Element set: 907
Inclination: 51
6485 deg
RA of node: 275
4608 deg
Eccentricity:
0017112
Arg of perigee: 64
1399 deg
Mean anomaly: 296
1515 deg
Mean motion: 15
51945044 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 697
Checksum: 335
Coasting Arc #9 (Orbit 711)
---------------------------------------
Vector Time (GMT): 2012/356/13:41:50
665
Vector Time (MET): N/A
Weight (LBS) : 890855
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -733824
38 A = 6795182
39 meter
Y = -6688546
48 meter E =
0026309
Z = -895786
63 I = 51
31579
XDOT = 4721
861659 Wp = 56
88302
YDOT = -1289
613448 meter/sec RA = 269
85808 deg
ZDOT = 5901
147022 TA = 293
38407
MA = 293
66057
Ha = 230
480 n
mi
Hp = 211
995
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2407560
30 X = -654625
57
Y = -21944050
13 feet Y = -6696309
69 meter
Z = -2938932
52 Z = -899159
53
XDOT = 15491
672111 XDOT = 4707
264980
YDOT = -4231
015249 feet/sec YDOT = -1236
892584 meter/sec
ZDOT = 19360
718576 ZDOT = 5924
050109
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18842046
18 X = 5743055
67
Y = -11499454
60 feet Y = -3505033
76 meter
Z = -2952091
97 Z = -899797
63
XDOT = 9529
913238 XDOT = 2904
717555
YDOT = 10737
811271 feet/sec YDOT = 3272
884875 meter/sec
ZDOT = 19455
851028 ZDOT = 5930
143393
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 12356
57246739
00016717 00000-0 10270-3 0 9085
2 25544 51
6490 270
6619 0017047 67
1843 293
1107 15
51998572 7121
Satellite: ISS
Catalog Number: 25544
Epoch time: 12356
57246739 = yrday
fracday
Element set: 908
Inclination: 51
6490 deg
RA of node: 270
6619 deg
Eccentricity:
0017047
Arg of perigee: 67
1843 deg
Mean anomaly: 293
1107 deg
Mean motion: 15
51998572 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 712
Checksum: 330
Coasting Arc #10 (Orbit 727)
---------------------------------------
Vector Time (GMT): 2012/357/13:41:50
665
Vector Time (MET): N/A
Weight (LBS) : 890855
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 475727
44 A = 6795565
29 meter
Y = 6775325
58 meter E =
0024466
Z = -164206
41 I = 51
31798
XDOT = -4786
229681 Wp = 97
06724
YDOT = 209
901284 meter/sec RA = 264
87447 deg
ZDOT = -5977
551367 TA = 84
70701
MA = 84
42789
Ha = 230
532 n
mi
Hp = 211
977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1560785
57 X = 400726
65
Y = 22228758
47 feet Y = 6780226
12 meter
Z = -538734
94 Z = -162077
05
XDOT = -15702
853283 XDOT = -4759
183454
YDOT = 688
652508 feet/sec YDOT = 156
530305 meter/sec
ZDOT = -19611
389000 ZDOT = -6000
737002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19260748
09 X = -5870676
02
Y = 11206511
12 feet Y = 3415744
59 meter
Z = -530736
79 Z = -161768
57
XDOT = -6671
202498 XDOT = -2033
382521
YDOT = -12277
454976 feet/sec YDOT = -3742
168277 meter/sec
ZDOT = -19707
563183 ZDOT = -6006
865258
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 12357
60271349
00016717 00000-0 10270-3 0 9096
2 25544 51
6491 265
5422 0016965 71
4090 288
8902 15
51979972 7281
Satellite: ISS
Catalog Number: 25544
Epoch time: 12357
60271349 = yrday
fracday
Element set: 909
Inclination: 51
6491 deg
RA of node: 265
5422 deg
Eccentricity:
0016965
Arg of perigee: 71
4090 deg
Mean anomaly: 288
8902 deg
Mean motion: 15
51979972 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 728
Checksum: 341
Coasting Arc #11 (Orbit 743)
---------------------------------------
Vector Time (GMT): 2012/358/13:41:50
665
Vector Time (MET): N/A
Weight (LBS) : 890855
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -278330
64 A = 6794890
73 meter
Y = -6683467
99 meter E =
0030281
Z = 1123114
48 I = 51
31989
XDOT = 4899
739936 Wp = 66
70760
YDOT = 798
194072 meter/sec RA = 259
89046 deg
ZDOT = 5850
198862 TA = 305
53824
MA = 305
82022
Ha = 230
438 n
mi
Hp = 211
844
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -913158
27 X = -209029
86
Y = -21927388
41 feet Y = -6686193
07 meter
Z = 3684758
80 Z = 1121930
13
XDOT = 16075
262257 XDOT = 4862
031187
YDOT = 2618
746955 feet/sec YDOT = 852
774700 meter/sec
ZDOT = 19193
565821 ZDOT = 5873
910111
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19083499
74 X = 5816650
72
Y = -10839484
60 feet Y = -3303874
90 meter
Z = 3680662
90 Z = 1121866
05
XDOT = 4160
456589 XDOT = 1268
107168
YDOT = 14002
563503 feet/sec YDOT = 4267
981356 meter/sec
ZDOT = 19291
801886 ZDOT = 5880
141215
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 12358
63294225
00016717 00000-0 10270-3 0 9100
2 25544 51
6491 260
4231 0016963 74
3855 285
9167 15
52038268 7446
Satellite: ISS
Catalog Number: 25544
Epoch time: 12358
63294225 = yrday
fracday
Element set: 910
Inclination: 51
6491 deg
RA of node: 260
4231 deg
Eccentricity:
0016963
Arg of perigee: 74
3855 deg
Mean anomaly: 285
9167 deg
Mean motion: 15
52038268 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 744
Checksum: 320
Coasting Arc #12 (Orbit 758)
---------------------------------------
Vector Time (GMT): 2012/359/13:41:50
665
Vector Time (MET): N/A
Weight (LBS) : 890855
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -40499
08 A = 6793473
63 meter
Y = 6450241
59 meter E =
0020695
Z = -2147070
26 I = 51
32135
XDOT = -5030
257433 Wp = 93
58427
YDOT = -1836
487893 meter/sec RA = 254
90556 deg
ZDOT = -5469
388060 TA = 110
27916
MA = 110
05659
Ha = 230
427 n
mi
Hp = 211
858
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -132871
01 X = -102194
04
Y = 21162209
93 feet Y = 6449443
96 meter
Z = -7044193
75 Z = -2147416
23
XDOT = -16503
469269 XDOT = -4982
778493
YDOT = -6025
222745 feet/sec YDOT = -1892
473376 meter/sec
ZDOT = -17944
186550 ZDOT = -5493
709712
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18702832
19 X = -5700623
25
Y = 9900990
32 feet Y = 3017821
85 meter
Z = -7046411
02 Z = -2147746
08
XDOT = -1694
733295 XDOT = -516
554708
YDOT = -15933
710399 feet/sec YDOT = -4856
594930 meter/sec
ZDOT = -18044
835926 ZDOT = -5500
065990
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 12359
59876869
00016717 00000-0 10270-3 0 9117
2 25544 51
6489 255
6236 0016800 78
3148 281
9888 15
52031016 7599
Satellite: ISS
Catalog Number: 25544
Epoch time: 12359
59876869 = yrday
fracday
Element set: 911
Inclination: 51
6489 deg
RA of node: 255
6236 deg
Eccentricity:
0016800
Arg of perigee: 78
3148 deg
Mean anomaly: 281
9888 deg
Mean motion: 15
52031016 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 759
Checksum: 350
Coasting Arc #13 (Orbit 774)
---------------------------------------
Vector Time (GMT): 2012/360/13:41:50
665
Vector Time (MET): N/A
Weight (LBS) : 890855
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 341309
20 A = 6791507
57 meter
Y = -6066678
20 meter E =
0030013
Z = 3002764
16 I = 51
32343
XDOT = 5204
782398 Wp = 82
18879
YDOT = 2750
440359 meter/sec RA = 249
91789 deg
ZDOT = 4926
957576 TA = 312
38679
MA = 312
64043
Ha = 230
396 n
mi
Hp = 211
745
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1119780
83 X = 394535
97
Y = -19903799
86 feet Y = -6062564
18 meter
Z = 9851588
46 Z = 3004550
85
XDOT = 17076
057737 XDOT = 5149
705540
YDOT = 9023
754458 feet/sec YDOT = 2808
335003 meter/sec
ZDOT = 16164
558977 ZDOT = 4952
108672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17902195
27 X = 5456589
12
Y = -8761625
47 feet Y = -2670543
44 meter
Z = 9859730
04 Z = 3005245
72
XDOT = -260
310982 XDOT = -79
342787
YDOT = 17917
033944 feet/sec YDOT = 5461
111946 meter/sec
ZDOT = 16268
548951 ZDOT = 4958
653720
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 12360
62896870
00016717 00000-0 10270-3 0 9128
2 25544 51
6484 250
5041 0016896 81
3636 278
9429 15
52067488 7750
Satellite: ISS
Catalog Number: 25544
Epoch time: 12360
62896870 = yrday
fracday
Element set: 912
Inclination: 51
6484 deg
RA of node: 250
5041 deg
Eccentricity:
0016896
Arg of perigee: 81
3636 deg
Mean anomaly: 278
9429 deg
Mean motion: 15
52067488 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 775
Checksum: 342
Coasting Arc #14 (Orbit 789)
---------------------------------------
Vector Time (GMT): 2012/361/13:41:50
665
Vector Time (MET): N/A
Weight (LBS) : 890855
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -787732
78 A = 6789045
17 meter
Y = 5561179
26 meter E =
0022830
Z = -3835758
20 I = 51
32598
XDOT = -5336
060995 Wp = 82
75663
YDOT = -3595
201975 meter/sec RA = 244
92715 deg
ZDOT = -4135
025123 TA = 143
49325
MA = 143
33740
Ha = 230
319 n
mi
Hp = 211
726
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2584425
13 X = -831227
34
Y = 18245338
77 feet Y = 5552127
59 meter
Z = -12584508
52 Z = -3839689
95
XDOT = -17506
761796 XDOT = -5275
375166
YDOT = -11795
282071 feet/sec YDOT = -3654
533353 meter/sec
ZDOT = -13566
355391 ZDOT = -4160
800379
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17040293
00 X = -5193881
31
Y = 6983734
16 feet Y = 2128642
17 meter
Z = -12601482
70 Z = -3840931
93
XDOT = 1973
389682 XDOT = 601
489175
YDOT = -19747
184937 feet/sec YDOT = -6018
941969 meter/sec
ZDOT = -13672
846721 ZDOT = -4167
483681
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 12361
59476648
00016717 00000-0 10270-3 0 9133
2 25544 51
6475 245
7043 0016705 85
2264 275
0795 15
52088339 7906
Satellite: ISS
Catalog Number: 25544
Epoch time: 12361
59476648 = yrday
fracday
Element set: 913
Inclination: 51
6475 deg
RA of node: 245
7043 deg
Eccentricity:
0016705
Arg of perigee: 85
2264 deg
Mean anomaly: 275
0795 deg
Mean motion: 15
52088339 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 790
Checksum: 333
Coasting Arc #15 (Orbit 805)
---------------------------------------
Vector Time (GMT): 2012/362/13:41:50
665
Vector Time (MET): N/A
Weight (LBS) : 890855
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1244261
93 A = 6786811
80 meter
Y = -4954706
56 meter E =
0025503
Z = 4447654
07 I = 51
33193
XDOT = 5479
648481 Wp = 96
53861
YDOT = 4297
499611 meter/sec RA = 239
93344 deg
ZDOT = 3235
614815 TA = 320
70733
MA = 320
89213
Ha = 230
329 n
mi
Hp = 211
687
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4082224
18 X = 1277968
49
Y = -16255598
96 feet Y = -4940604
51 meter
Z = 14592040
92 Z = 4453779
88
XDOT = 17977
849346 XDOT = 5415
467911
YDOT = 14099
408171 feet/sec YDOT = 4358
417231 meter/sec
ZDOT = 10615
534169 ZDOT = 3262
079115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15980855
20 X = 4870964
67
Y = -4976128
18 feet Y = -1516723
87 meter
Z = 14618041
09 Z = 4455578
92
XDOT = -3185
922821 XDOT = -971
069276
YDOT = 21455
324974 feet/sec YDOT = 6539
583052 meter/sec
ZDOT = 10724
816890 ZDOT = 3268
924188
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 12362
62493824
00016717 00000-0 10270-3 0 9144
2 25544 51
6471 240
5845 0016840 88
6240 271
6840 15
52096175 8064
Satellite: ISS
Catalog Number: 25544
Epoch time: 12362
62493824 = yrday
fracday
Element set: 914
Inclination: 51
6471 deg
RA of node: 240
5845 deg
Eccentricity:
0016840
Arg of perigee: 88
6240 deg
Mean anomaly: 271
6840 deg
Mean motion: 15
52096175 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 806
Checksum: 312
Coasting Arc #16 (Orbit 820)
---------------------------------------
Vector Time (GMT): 2012/363/13:41:50
665
Vector Time (MET): N/A
Weight (LBS) : 890855
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1841119
67 A = 6784736
36 meter
Y = 4280311
26 meter E =
0028685
Z = -4957438
84 I = 51
33998
XDOT = -5504
345074 Wp = 84
78699
YDOT = -4848
272511 meter/sec RA = 234
93592 deg
ZDOT = -2150
067341 TA = 164
14418
MA = 164
05418
Ha = 230
229 n
mi
Hp = 211
599
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6040418
85 X = -1864764
33
Y = 14043015
95 feet Y = 4259591
07 meter
Z = -16264563
12 Z = -4966439
76
XDOT = -18058
874916 XDOT = -5439
277152
YDOT = -15906
405876 feet/sec YDOT = -4909
461481 meter/sec
ZDOT = -7054
026709 ZDOT = -2176
649407
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15052623
36 X = -4588039
60
Y = 2424650
77 feet Y = 739033
56 meter
Z = -16302409
92 Z = -4968974
54
XDOT = 4086
529267 XDOT = 1245
574121
YDOT = -22615
015902 feet/sec YDOT = -6893
056847 meter/sec
ZDOT = -7163
751982 ZDOT = -2183
511604
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 12363
59070838
00016717 00000-0 10270-3 0 9158
2 25544 51
6455 235
7839 0016669 92
4232 267
8828 15
52139831 8215
Satellite: ISS
Catalog Number: 25544
Epoch time: 12363
59070838 = yrday
fracday
Element set: 915
Inclination: 51
6455 deg
RA of node: 235
7839 deg
Eccentricity:
0016669
Arg of perigee: 92
4232 deg
Mean anomaly: 267
8828 deg
Mean motion: 15
52139831 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 821
Checksum: 337
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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