[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 12th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 126 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 347 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
053/10:35:16
651 -1
7 2
5 2
5
N/A -0
6 -0
1 223
8
000/00:06:33
302 -1
8 -0
0 219
9
Coasting Arc #1 (Orbit 1524)
---------------------------------------
Vector Time (GMT): 2013/042/21:29:09
492
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4681020
63 A = 6789315
96 meter
Y = -3557012
09 meter E =
0007827
Z = -3387667
70 I = 51
71430
XDOT = 5450
127962 Wp = 260
78010
YDOT = -2744
144597 meter/sec RA = 10
17606 deg
ZDOT = -4641
647665 TA = 318
71864
MA = 318
77778
Ha = 222
036 n
mi
Hp = 219
045
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15357679
22 X = -4624441
47
Y = -11669987
17 feet Y = -3609042
13 meter
Z = -11114395
35 Z = -3410269
43
XDOT = 17880
997252 XDOT = 5502
955847
YDOT = -9003
099070 feet/sec YDOT = -2682
902845 meter/sec
ZDOT = -15228
502839 ZDOT = -4615
043520
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7754036
63 X = -2363430
36
Y = 17602068
78 feet Y = 5365110
57 meter
Z = -11207978
68 Z = -3416191
90
XDOT = -11689
834069 XDOT = -3563
061424
YDOT = -14791
902304 feet/sec YDOT = -4508
571822 meter/sec
ZDOT = -15117
419203 ZDOT = -4607
789373
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 13042
92028105
00016717 00000-0 10270-3 0 9004
2 25544 51
6453 10
5609 0012669 264
6190 95
3516 15
52435150 15252
Satellite: ISS
Catalog Number: 25544
Epoch time: 13042
92028105 = yrday
fracday
Element set: 900
Inclination: 51
6453 deg
RA of node: 10
5609 deg
Eccentricity:
0012669
Arg of perigee: 264
6190 deg
Mean anomaly: 95
3516 deg
Mean motion: 15
52435150 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1525
Checksum: 280
Coasting Arc #2 (Orbit 1540)
---------------------------------------
Vector Time (GMT): 2013/043/21:29:09
492
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3860175
12 A = 6786650
44 meter
Y = 3684049
81 meter E =
0004465
Z = 4198337
10 I = 51
67523
XDOT = -6278
535818 Wp = 222
63419
YDOT = 2363
271446 meter/sec RA = 5
20597 deg
ZDOT = 3698
142919 TA = 189
38285
MA = 189
39119
Ha = 222
005 n
mi
Hp = 218
861
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12664616
52 X = 3798298
40
Y = 12086777
59 feet Y = 3726871
13 meter
Z = 13774071
84 Z = 4216938
48
XDOT = -20598
870795 XDOT = -6322
460020
YDOT = 7753
515242 feet/sec YDOT = 2292
815659 meter/sec
ZDOT = 12133
014827 ZDOT = 3667
536047
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8535149
56 X = 2601513
59
Y = -15215425
57 feet Y = -4637661
71 meter
Z = 13850985
74 Z = 4221780
45
XDOT = 11595
284014 XDOT = 3534
242567
YDOT = 17435
854482 feet/sec YDOT = 5314
448446 meter/sec
ZDOT = 12005
332950 ZDOT = 3659
225483
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 13043
95023552
00016717 00000-0 10270-3 0 9010
2 25544 51
6452 5
4386 0012812 267
8153 92
1531 15
52459814 15413
Satellite: ISS
Catalog Number: 25544
Epoch time: 13043
95023552 = yrday
fracday
Element set: 901
Inclination: 51
6452 deg
RA of node: 5
4386 deg
Eccentricity:
0012812
Arg of perigee: 267
8153 deg
Mean anomaly: 92
1531 deg
Mean motion: 15
52459814 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1541
Checksum: 287
Coasting Arc #3 (Orbit 1555)
---------------------------------------
Vector Time (GMT): 2013/044/21:29:09
492
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2901120
00 A = 6784254
40 meter
Y = -3813444
17 meter E =
0004117
Z = -4803038
61 I = 51
63741
XDOT = 6930
107153 Wp = 337
47686
YDOT = -2015
336194 meter/sec RA =
23058 deg
ZDOT = -2581
349243 TA = 267
06350
MA = 267
11062
Ha = 221
756 n
mi
Hp = 218
985
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9518110
23 X = -2834930
14
Y = -12511299
77 feet Y = -3845516
67 meter
Z = -15758000
68 Z = -4816970
64
XDOT = 22736
572024 XDOT = 6964
667312
YDOT = -6611
995388 feet/sec YDOT = -1937
646382 meter/sec
ZDOT = -8468
993579 ZDOT = -2547
599807
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9528210
34 X = -2904198
51
Y = 12430848
00 feet Y = 3788922
47 meter
Z = -15815462
54 Z = -4820552
98
XDOT = -11574
237386 XDOT = -3527
827555
YDOT = -19486
012730 feet/sec YDOT = -5939
336680 meter/sec
ZDOT = -8328
289980 ZDOT = -2538
462786
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 13044
91580264
00016717 00000-0 10270-3 0 9026
2 25544 51
6456
6380 0012506 271
2264 88
7455 15
52491457 15561
Satellite: ISS
Catalog Number: 25544
Epoch time: 13044
91580264 = yrday
fracday
Element set: 902
Inclination: 51
6456 deg
RA of node:
6380 deg
Eccentricity:
0012506
Arg of perigee: 271
2264 deg
Mean anomaly: 88
7455 deg
Mean motion: 15
52491457 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1556
Checksum: 301
Coasting Arc #4 (Orbit 1571)
---------------------------------------
Vector Time (GMT): 2013/045/21:29:09
492
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1833338
53 A = 6782719
90 meter
Y = 3974693
40 meter E =
0009133
Z = 5189396
65 I = 51
60097
XDOT = -7357
509058 Wp = 261
28604
YDOT = 1665
121282 meter/sec RA = 355
24752 deg
ZDOT = 1324
585546 TA = 175
96886
MA = 175
96150
Ha = 221
977 n
mi
Hp = 218
975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6014890
20 X = 1763548
05
Y = 13040332
66 feet Y = 3994805
15 meter
Z = 17025579
58 Z = 5198132
89
XDOT = -24138
809246 XDOT = -7382
016368
YDOT = 5462
996331 feet/sec YDOT = 1582
708074 meter/sec
ZDOT = 4345
753104 ZDOT = 1288
784229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10819646
62 X = 3297828
29
Y = -9377820
71 feet Y = -2858359
75 meter
Z = 17061396
94 Z = 5200313
79
XDOT = 11432
344465 XDOT = 3484
578593
YDOT = 20821
175674 feet/sec YDOT = 6346
294346 meter/sec
ZDOT = 4196
566862 ZDOT = 1279
113580
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 13045
94572337
00016717 00000-0 10270-3 0 9033
2 25544 51
6452 355
5156 0012548 275
0654 84
9065 15
52472783 15725
Satellite: ISS
Catalog Number: 25544
Epoch time: 13045
94572337 = yrday
fracday
Element set: 903
Inclination: 51
6452 deg
RA of node: 355
5156 deg
Eccentricity:
0012548
Arg of perigee: 275
0654 deg
Mean anomaly: 84
9065 deg
Mean motion: 15
52472783 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1572
Checksum: 322
Coasting Arc #5 (Orbit 1586)
---------------------------------------
Vector Time (GMT): 2013/046/21:29:09
492
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -714776
10 A = 6781969
60 meter
Y = -4155484
33 meter E =
0003028
Z = -5314098
69 I = 51
56951
XDOT = 7553
940914 Wp = 57
46003
YDOT = -1296
748012 meter/sec RA = 350
26182 deg
ZDOT = -
431359 TA = 212
52652
MA = 212
54519
Ha = 221
952 n
mi
Hp = 219
029
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2345065
93 X = -642441
31
Y = -13633478
77 feet Y = -4163073
33 meter
Z = -17434706
99 Z = -5317394
99
XDOT = 24783
270715 XDOT = 7567
882096
YDOT = -4254
422610 feet/sec YDOT = -1212
197149 meter/sec
ZDOT = -1
415220 ZDOT = 36
298532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12328142
61 X = -3757617
87
Y = 6239312
74 feet Y = 1901742
52 meter
Z = -17447864
10 Z = -5318108
98
XDOT = -11064
355710 XDOT = -3372
415621
YDOT = -21452
585802 feet/sec YDOT = -6538
748152 meter/sec
ZDOT = 151
578020 ZDOT = 46
200980
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 13046
91125560
00016717 00000-0 10270-3 0 9044
2 25544 51
6461 350
7150 0012421 277
9270 82
0472 15
52542228 15870
Satellite: ISS
Catalog Number: 25544
Epoch time: 13046
91125560 = yrday
fracday
Element set: 904
Inclination: 51
6461 deg
RA of node: 350
7150 deg
Eccentricity:
0012421
Arg of perigee: 277
9270 deg
Mean anomaly: 82
0472 deg
Mean motion: 15
52542228 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1587
Checksum: 288
Coasting Arc #6 (Orbit 1602)
---------------------------------------
Vector Time (GMT): 2013/047/21:29:09
492
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -419374
34 A = 6782702
73 meter
Y = 4366015
44 meter E =
0009851
Z = 5182055
75 I = 51
54098
XDOT = -7490
682990 Wp = 300
12278
YDOT = 870
972554 meter/sec RA = 345
27195 deg
ZDOT = -1337
094504 TA = 162
77644
MA = 162
74299
Ha = 222
310 n
mi
Hp = 219
159
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1375900
06 X = -493337
62
Y = 14324197
63 feet Y = 4360912
46 meter
Z = 17001495
26 Z = 5179838
60
XDOT = -24575
731594 XDOT = -7493
370497
YDOT = 2857
521502 feet/sec YDOT = 787
191930 meter/sec
ZDOT = -4386
792991 ZDOT = -1373
489721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14054375
99 X = 4283773
80
Y = -3143842
18 feet Y = -958243
10 meter
Z = 16991684
78 Z = 5179065
52
XDOT = 10273
453004 XDOT = 3131
348476
YDOT = 21346
385712 feet/sec YDOT = 6506
378365 meter/sec
ZDOT = -4538
331022 ZDOT = -1383
283295
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 13047
94114108
00016717 00000-0 10270-3 0 9055
2 25544 51
6455 345
5923 0012375 281
6853 78
2910 15
52511026 16035
Satellite: ISS
Catalog Number: 25544
Epoch time: 13047
94114108 = yrday
fracday
Element set: 905
Inclination: 51
6455 deg
RA of node: 345
5923 deg
Eccentricity:
0012375
Arg of perigee: 281
6853 deg
Mean anomaly: 78
2910 deg
Mean motion: 15
52511026 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1603
Checksum: 294
Coasting Arc #7 (Orbit 1617)
---------------------------------------
Vector Time (GMT): 2013/048/21:29:09
492
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1501407
75 A = 6784193
21 meter
Y = -4573773
08 meter E =
0001456
Z = -4779270
24 I = 51
51836
XDOT = 7196
665196 Wp = 255
57124
YDOT = -371
047263 meter/sec RA = 340
28350 deg
ZDOT = 2614
901548 TA = 40
26685
MA = 40
25607
Ha = 222
494 n
mi
Hp = 219
052
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4925878
45 X = 1575657
17
Y = -15005817
21 feet Y = -4556568
46 meter
Z = -15680020
48 Z = -4771796
08
XDOT = 23611
106285 XDOT = 7187
577129
YDOT = -1217
346665 feet/sec YDOT = -290
620329 meter/sec
ZDOT = 8579
073321 ZDOT = 2649
839798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15822680
06 X = -4822752
88
Y = 273865
66 feet Y = 83474
25 meter
Z = -15648311
86 Z = -4769605
45
XDOT = -8989
034945 XDOT = -2739
857851
YDOT = -20647
294276 feet/sec YDOT = -6293
295295 meter/sec
ZDOT = 8724
478693 ZDOT = 2659
221106
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 13048
90663924
00016717 00000-0 10270-3 0 9068
2 25544 51
6466 340
7912 0012456 285
0391 74
9382 15
52581748 16187
Satellite: ISS
Catalog Number: 25544
Epoch time: 13048
90663924 = yrday
fracday
Element set: 906
Inclination: 51
6466 deg
RA of node: 340
7912 deg
Eccentricity:
0012456
Arg of perigee: 285
0391 deg
Mean anomaly: 74
9382 deg
Mean motion: 15
52581748 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1618
Checksum: 329
Coasting Arc #8 (Orbit 1633)
---------------------------------------
Vector Time (GMT): 2013/049/21:33:09
492
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3992196
05 A = 6789818
52 meter
Y = 4542260
03 meter E =
0002851
Z = 3089568
22 I = 51
50828
XDOT = -5668
490470 Wp = 23
41266
YDOT = -1661
150064 meter/sec RA = 335
28291 deg
ZDOT = -4878
235658 TA = 121
04709
MA = 121
01910
Ha = 222
756 n
mi
Hp = 219
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13097756
06 X = -4057699
92
Y = 14902427
91 feet Y = 4497250
65 meter
Z = 10136378
67 Z = 3070015
49
XDOT = -18597
409680 XDOT = -5625
797039
YDOT = -5449
967402 feet/sec YDOT = -1724
300166 meter/sec
ZDOT = -16004
710163 ZDOT = -4905
668506
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18687380
32 X = 5695913
52
Y = 6787493
94 feet Y = 2068828
15 meter
Z = 10054426
23 Z = 3064589
11
XDOT = 2197
452228 XDOT = 669
783439
YDOT = 17846
881710 feet/sec YDOT = 5439
729545 meter/sec
ZDOT = -16118
616525 ZDOT = -4912
954317
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 13049
93648792
00016717 00000-0 10270-3 0 9079
2 25544 51
6462 335
6688 0012465 288
6463 71
3335 15
52595038 16349
Satellite: ISS
Catalog Number: 25544
Epoch time: 13049
93648792 = yrday
fracday
Element set: 907
Inclination: 51
6462 deg
RA of node: 335
6688 deg
Eccentricity:
0012465
Arg of perigee: 288
6463 deg
Mean anomaly: 71
3335 deg
Mean motion: 15
52595038 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1634
Checksum: 342
Coasting Arc #9 (Orbit 1648)
---------------------------------------
Vector Time (GMT): 2013/050/21:33:09
492
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4654000
43 A = 6792000
48 meter
Y = -4503790
16 meter E =
0012272
Z = -2019292
04 I = 51
48993
XDOT = 4723
910062 Wp = 323
80654
YDOT = 2389
797323 meter/sec RA = 330
30482 deg
ZDOT = 5549
807618 TA = 13
83526
MA = 13
80166
Ha = 223
036 n
mi
Hp = 218
928
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15269030
27 X = 4713825
88
Y = -14776214
43 feet Y = -4451411
78 meter
Z = -6624973
88 Z = -1996538
22
XDOT = 15498
392593 XDOT = 4669
876742
YDOT = 7840
542398 feet/sec YDOT = 2442
321153 meter/sec
ZDOT = 18208
030244 ZDOT = 5572
624222
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19506066
51 X = -5945449
07
Y = -8499781
90 feet Y = -2590733
52 meter
Z = -6529713
18 Z = -1990256
58
XDOT = 746
327164 XDOT = 227
480520
YDOT = -15792
526314 feet/sec YDOT = -4813
562021 meter/sec
ZDOT = 18302
634995 ZDOT = 5578
643146
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 13050
90195381
00016717 00000-0 10270-3 0 9080
2 25544 51
6476 330
8670 0012479 292
5034 67
4796 15
52634091 16491
Satellite: ISS
Catalog Number: 25544
Epoch time: 13050
90195381 = yrday
fracday
Element set: 908
Inclination: 51
6476 deg
RA of node: 330
8670 deg
Eccentricity:
0012479
Arg of perigee: 292
5034 deg
Mean anomaly: 67
4796 deg
Mean motion: 15
52634091 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1649
Checksum: 325
Coasting Arc #10 (Orbit 1664)
---------------------------------------
Vector Time (GMT): 2013/051/21:33:09
492
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5133458
29 A = 6793299
31 meter
Y = 4366432
72 meter E =
0002452
Z = 842365
40 I = 51
46818
XDOT = -3679
371084 Wp = 191
32667
YDOT = -3185
077860 meter/sec RA = 325
32860 deg
ZDOT = -5917
773265 TA = 339
55057
MA = 339
56039
Ha = 223
234 n
mi
Hp = 218
774
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16842054
75 X = -5185995
04
Y = 14325566
68 feet Y = 4308733
46 meter
Z = 2763666
02 Z = 817300
21
XDOT = -12071
427442 XDOT = -3614
735024
YDOT = -10449
730512 feet/sec YDOT = -3225
861757 meter/sec
ZDOT = -19415
266618 ZDOT = -5935
489837
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19852355
27 X = 6050997
89
Y = 9763668
55 feet Y = 2975966
18 meter
Z = 2658812
79 Z = 810406
14
XDOT = -4118
488484 XDOT = -1255
315290
YDOT = 13676
224511 feet/sec YDOT = 4168
513231 meter/sec
ZDOT = -19488
551000 ZDOT = -5940
110345
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 13051
93176683
00016717 00000-0 10270-3 0 9099
2 25544 51
6472 325
7451 0012517 296
1614 63
8251 15
52666745 16659
Satellite: ISS
Catalog Number: 25544
Epoch time: 13051
93176683 = yrday
fracday
Element set: 909
Inclination: 51
6472 deg
RA of node: 325
7451 deg
Eccentricity:
0012517
Arg of perigee: 296
1614 deg
Mean anomaly: 63
8251 deg
Mean motion: 15
52666745 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1665
Checksum: 322
Coasting Arc #11 (Orbit 1680)
---------------------------------------
Vector Time (GMT): 2013/052/21:33:09
492
Vector Time (MET): N/A
Weight (LBS) : 906534
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5410529
84 A = 6793447
05 meter
Y = -4072610
35 meter E =
0014614
Z = 397063
25 I = 51
44549
XDOT = 2601
298339 Wp = 355
67730
YDOT = 4036
305833 meter/sec RA = 320
35211 deg
ZDOT = 5982
104511 TA = 8
61521
MA = 8
59015
Ha = 223
440 n
mi
Hp = 218
629
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17751082
15 X = 5453739
73
Y = -13361582
52 feet Y = -4011864
79 meter
Z = 1302700
94 Z = 423451
72
XDOT = 8534
443371 XDOT = 2526
911358
YDOT = 13242
473206 feet/sec YDOT = 4064
979586 meter/sec
ZDOT = 19626
327135 ZDOT = 5994
560214
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19505239
78 X = -5945197
08
Y = -10624445
68 feet Y = -3238331
04 meter
Z = 1413014
46 Z = 430686
81
XDOT = 7801
294880 XDOT = 2377
834680
YDOT = -11716
734597 feet/sec YDOT = -3571
260705 meter/sec
ZDOT = 19677
617876 ZDOT = 5997
737929
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 13052
96156204
00016717 00000-0 10270-3 0 9102
2 25544 51
6484 320
6230 0012492 300
3819 59
6098 15
52687959 16818
Satellite: ISS
Catalog Number: 25544
Epoch time: 13052
96156204 = yrday
fracday
Element set: 910
Inclination: 51
6484 deg
RA of node: 320
6230 deg
Eccentricity:
0012492
Arg of perigee: 300
3819 deg
Mean anomaly: 59
6098 deg
Mean motion: 15
52687959 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1681
Checksum: 314
Coasting Arc #12 (Orbit 1688)
---------------------------------------
Vector Time (GMT): 2013/053/10:38:33
302
Vector Time (MET): N/A
Weight (LBS) : 906265
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4750124
18 A = 6794807
50 meter
Y = 4833484
27 meter E =
0003107
Z = 463363
75 I = 51
43244
XDOT = -3700
458499 Wp = 182
31287
YDOT = -3064
987558 meter/sec RA = 317
62690 deg
ZDOT = -5967
508962 TA = 352
68197
MA = 352
68651
Ha = 223
811 n
mi
Hp = 219
871
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15584396
91 X = -4806071
03
Y = 15857888
03 feet Y = 4780052
61 meter
Z = 1520222
27 Z = 440152
41
XDOT = -12140
611874 XDOT = -3636
922239
YDOT = -10055
733457 feet/sec YDOT = -3106
013528 meter/sec
ZDOT = -19578
441476 ZDOT = -5985
330537
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22205851
16 X = -6768343
43
Y = -1237849
66 feet Y = -377296
58 meter
Z = 1423031
31 Z = 433739
94
XDOT = -475
275773 XDOT = -144
864056
YDOT = -14048
238317 feet/sec YDOT = -4281
903039 meter/sec
ZDOT = -19652
184546 ZDOT = -5989
985850
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 13053
47646551
00016717 00000-0 10270-3 0 9119
2 25544 51
6481 318
0666 0011213 297
7163 62
2851 15
52217029 16892
Satellite: ISS
Catalog Number: 25544
Epoch time: 13053
47646551 = yrday
fracday
Element set: 911
Inclination: 51
6481 deg
RA of node: 318
0666 deg
Eccentricity:
0011213
Arg of perigee: 297
7163 deg
Mean anomaly: 62
2851 deg
Mean motion: 15
52217029 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1689
Checksum: 305
Coasting Arc #13 (Orbit 1704)
---------------------------------------
Vector Time (GMT): 2013/054/10:38:33
302
Vector Time (MET): N/A
Weight (LBS) : 906265
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4934004
61 A = 6794640
87 meter
Y = -4614879
88 meter E =
0014051
Z = 629523
19 I = 51
40981
XDOT = 2877
606775 Wp = 2
79735
YDOT = 3887
512467 meter/sec RA = 312
64967 deg
ZDOT = 5952
754087 TA = 4
01979
MA = 4
00852
Ha = 223
999 n
mi
Hp = 219
640
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16187679
17 X = 4982184
49
Y = -15140682
03 feet Y = -4559435
30 meter
Z = 2065364
81 Z = 653608
98
XDOT = 9440
967108 XDOT = 2805
005719
YDOT = 12754
305995 feet/sec YDOT = 3919
286219 meter/sec
ZDOT = 19530
033095 ZDOT = 5966
556261
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22084549
57 X = 6731370
71
Y = 1768439
71 feet Y = 539020
42 meter
Z = 2166156
14 Z = 660244
39
XDOT = -3029
233605 XDOT = -923
310403
YDOT = 13868
698476 feet/sec YDOT = 4227
179296 meter/sec
ZDOT = 19586
953965 ZDOT = 5970
103569
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 13054
50655094
00016717 00000-0 10270-3 0 9127
2 25544 51
6478 312
9462 0011306 301
9604 58
0448 15
52241456 17051
Satellite: ISS
Catalog Number: 25544
Epoch time: 13054
50655094 = yrday
fracday
Element set: 912
Inclination: 51
6478 deg
RA of node: 312
9462 deg
Eccentricity:
0011306
Arg of perigee: 301
9604 deg
Mean anomaly: 58
0448 deg
Mean motion: 15
52241456 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1705
Checksum: 292
Coasting Arc #14 (Orbit 1719)
---------------------------------------
Vector Time (GMT): 2013/055/10:38:33
302
Vector Time (MET): N/A
Weight (LBS) : 906265
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5006360
19 A = 6793475
73 meter
Y = 4265699
58 meter E =
0004616
Z = -1697708
11 I = 51
38685
XDOT = -2085
365047 Wp = 276
12154
YDOT = -4709
771812 meter/sec RA = 307
67026 deg
ZDOT = -5670
548313 TA = 282
53265
MA = 282
58428
Ha = 224
204 n
mi
Hp = 219
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16425066
24 X = -5045441
25
Y = 13995077
35 feet Y = 4209496
62 meter
Z = -5569908
49 Z = -1722123
36
XDOT = -6841
748841 XDOT = -2004
999021
YDOT = -15452
007257 feet/sec YDOT = -4732
642898 meter/sec
ZDOT = -18604
161133 ZDOT = -5680
482920
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21425750
36 X = -6530568
71
Y = -2331164
54 feet Y = -710538
95 meter
Z = -5672015
96 Z = -1728830
46
XDOT = 6463
378436 XDOT = 1970
037747
YDOT = -13931
323311 feet/sec YDOT = -4246
267345 meter/sec
ZDOT = -18644
895012 ZDOT = -5682
964000
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 13055
47223956
00016717 00000-0 10270-3 0 9133
2 25544 51
6484 308
1464 0011306 305
0031 55
0059 15
52268253 17202
Satellite: ISS
Catalog Number: 25544
Epoch time: 13055
47223956 = yrday
fracday
Element set: 913
Inclination: 51
6484 deg
RA of node: 308
1464 deg
Eccentricity:
0011306
Arg of perigee: 305
0031 deg
Mean anomaly: 55
0059 deg
Mean motion: 15
52268253 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1720
Checksum: 279
Coasting Arc #15 (Orbit 1735)
---------------------------------------
Vector Time (GMT): 2013/056/10:38:33
302
Vector Time (MET): N/A
Weight (LBS) : 906265
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4970742
86 A = 6791496
22 meter
Y = -3740771
17 meter E =
0010711
Z = 2706408
81 I = 51
36209
XDOT = 1350
523781 Wp = 24
18111
YDOT = 5519
331294 meter/sec RA = 302
68612 deg
ZDOT = 5150
655901 TA = 6
53043
MA = 6
51648
Ha = 224
312 n
mi
Hp = 219
159
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16308211
49 X = 4999056
79
Y = -12272871
30 feet Y = -3685026
56 meter
Z = 8879294
00 Z = 2730624
96
XDOT = 4430
852299 XDOT = 1263
685084
YDOT = 18108
042304 feet/sec YDOT = 5533
948775 meter/sec
ZDOT = 16898
477366 ZDOT = 5157
004906
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20133785
20 X = 6136777
73
Y = 3066651
83 feet Y = 934715
48 meter
Z = 8980497
43 Z = 2737255
62
XDOT = -9719
539828 XDOT = -2962
515740
YDOT = 14273
392307 feet/sec YDOT = 4350
529975 meter/sec
ZDOT = 16924
202255 ZDOT = 5158
496847
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 13056
50229149
00016717 00000-0 10270-3 0 9149
2 25544 51
6479 303
0256 0011336 309
4281 50
5867 15
52293678 17360
Satellite: ISS
Catalog Number: 25544
Epoch time: 13056
50229149 = yrday
fracday
Element set: 914
Inclination: 51
6479 deg
RA of node: 303
0256 deg
Eccentricity:
0011336
Arg of perigee: 309
4281 deg
Mean anomaly: 50
5867 deg
Mean motion: 15
52293678 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1736
Checksum: 313
Coasting Arc #16 (Orbit 1750)
---------------------------------------
Vector Time (GMT): 2013/057/10:38:33
302
Vector Time (MET): N/A
Weight (LBS) : 906265
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4867552
73 A = 6788996
90 meter
Y = 3083256
49 meter E =
0009056
Z = -3595699
44 I = 51
33876
XDOT = -696
037037 Wp = 339
89525
YDOT = -6235
513260 meter/sec RA = 297
69731 deg
ZDOT = -4392
963390 TA = 242
79221
MA = 242
88453
Ha = 224
547 n
mi
Hp = 218
780
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15969661
18 X = -4884201
95
Y = 10115670
90 feet Y = 3028730
89 meter
Z = -11796914
18 Z = -3619386
02
XDOT = -2283
586081 XDOT = -604
918998
YDOT = -20457
720668 feet/sec YDOT = -6242
787892 meter/sec
ZDOT = -14412
609546 ZDOT = -4396
122479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18411960
05 X = -5611965
42
Y = -4001642
92 feet Y = -1219700
76 meter
Z = -11895824
53 Z = -3625847
32
XDOT = 12547
184964 XDOT = 3824
381977
YDOT = -14736
450519 feet/sec YDOT = -4491
670118 meter/sec
ZDOT = -14424
985776 ZDOT = -4396
735665
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 13057
46794823
00016717 00000-0 10270-3 0 9152
2 25544 51
6482 298
2256 0011449 312
5472 47
4712 15
52334044 17515
Satellite: ISS
Catalog Number: 25544
Epoch time: 13057
46794823 = yrday
fracday
Element set: 915
Inclination: 51
6482 deg
RA of node: 298
2256 deg
Eccentricity:
0011449
Arg of perigee: 312
5472 deg
Mean anomaly: 47
4712 deg
Mean motion: 15
52334044 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1751
Checksum: 311
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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