[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 11th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 152 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
166/13:46:01
000 0
0 0
0 0
0
N/A 0
0 0
0 230
2
000/00:00:00
000 0
0 0
0 216
2
170/12:56:11
071 0
2 3
3 3
3
N/A 3
2 0
0 230
0
000/00:02:22
141 -0
7 -0
0 217
9
Coasting Arc #1 (Orbit 3367)
---------------------------------------
Vector Time (GMT): 2013/161/13:05:45
790
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5231169
49 A = 6791353
59 meter
Y = -56480
28 meter E =
0018044
Z = 4313136
59 I = 51
86220
XDOT = 2997
030469 Wp = 78
78553
YDOT = -6109
832111 meter/sec RA = 140
27744 deg
ZDOT = 3545
810382 TA = 335
19221
MA = 335
27885
Ha = 230
032 n
mi
Hp = 216
634
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17162629
58 X = -5251101
21
Y = -185302
76 feet Y = -115090
58 meter
Z = 14150710
58 Z = 4287675
56
XDOT = 9832
777129 XDOT = 3047
904567
YDOT = -20045
380941 feet/sec YDOT = -6076
033478 meter/sec
ZDOT = 11633
236163 ZDOT = 3560
492416
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1222767
18 X = 372699
44
Y = 17207435
13 feet Y = 5244826
23 meter
Z = 14044280
61 Z = 4280696
73
XDOT = -19518
721498 XDOT = -5949
306313
YDOT = -8183
095734 feet/sec YDOT = -2494
207580 meter/sec
ZDOT = 11695
412286 ZDOT = 3564
761665
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 13161
60053692
00016717 00000-0 10270-3 0 9000
2 25544 51
6455 141
0113 0010500 51
9336 308
2761 15
50767394 33686
Satellite: ISS
Catalog Number: 25544
Epoch time: 13161
60053692 = yrday
fracday
Element set: 900
Inclination: 51
6455 deg
RA of node: 141
0113 deg
Eccentricity:
0010500
Arg of perigee: 51
9336 deg
Mean anomaly: 308
2761 deg
Mean motion: 15
50767394 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3368
Checksum: 280
Coasting Arc #2 (Orbit 3382)
---------------------------------------
Vector Time (GMT): 2013/162/13:05:45
790
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4957355
99 A = 6790191
36 meter
Y = 235041
13 meter E =
0020717
Z = -4654798
53 I = 51
88167
XDOT = -3089
128841 Wp = 62
75046
YDOT = 6331
619411 meter/sec RA = 135
33090 deg
ZDOT = -2971
157434 TA = 177
65509
MA = 177
64536
Ha = 230
037 n
mi
Hp = 216
632
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16264291
29 X = 4976971
00
Y = 771132
32 feet Y = 290587
71 meter
Z = -15271648
73 Z = -4630668
48
XDOT = -10134
937142 XDOT = -3145
267717
YDOT = 20773
029564 feet/sec YDOT = 6296
761334 meter/sec
ZDOT = -9747
891844 ZDOT = -2986
299643
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -847748
70 X = -258393
80
Y = -16354614
02 feet Y = -4984886
35 meter
Z = -15170794
10 Z = -4624058
04
XDOT = 20472
269803 XDOT = 6239
947836
YDOT = 8037
697198 feet/sec YDOT = 2449
890106 meter/sec
ZDOT = -9812
033506 ZDOT = -2990
707813
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 13162
56717913
00016717 00000-0 10270-3 0 9010
2 25544 51
6461 136
2165 0010687 55
2330 304
9825 15
50746646 33831
Satellite: ISS
Catalog Number: 25544
Epoch time: 13162
56717913 = yrday
fracday
Element set: 901
Inclination: 51
6461 deg
RA of node: 136
2165 deg
Eccentricity:
0010687
Arg of perigee: 55
2330 deg
Mean anomaly: 304
9825 deg
Mean motion: 15
50746646 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3383
Checksum: 305
Coasting Arc #3 (Orbit 3398)
---------------------------------------
Vector Time (GMT): 2013/163/13:05:45
790
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4662605
44 A = 6788972
01 meter
Y = -449217
98 meter E =
0015019
Z = 4900560
46 I = 51
90000
XDOT = 3144
315073 Wp = 82
77903
YDOT = -6581
242167 meter/sec RA = 130
38652 deg
ZDOT = 2383
954223 TA = 343
94438
MA = 343
99193
Ha = 230
078 n
mi
Hp = 216
417
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15297261
94 X = -4681041
19
Y = -1473812
26 feet Y = -501461
85 meter
Z = 16077954
28 Z = 4877865
16
XDOT = 10315
994334 XDOT = 3206
093674
YDOT = -21592
001860 feet/sec YDOT = -6545
735320 meter/sec
ZDOT = 7821
372124 ZDOT = 2399
378242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 319684
23 X = 97439
75
Y = 15463400
38 feet Y = 4713244
44 meter
Z = 15983116
40 Z = 4871653
88
XDOT = -21507
203806 XDOT = -6555
395720
YDOT = -7722
193312 feet/sec YDOT = -2353
724522 meter/sec
ZDOT = 7886
736896 ZDOT = 2403
877406
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 13163
59825232
00016717 00000-0 10270-3 0 9029
2 25544 51
6468 131
1038 0010502 58
7049 301
5129 15
50795780 33992
Satellite: ISS
Catalog Number: 25544
Epoch time: 13163
59825232 = yrday
fracday
Element set: 902
Inclination: 51
6468 deg
RA of node: 131
1038 deg
Eccentricity:
0010502
Arg of perigee: 58
7049 deg
Mean anomaly: 301
5129 deg
Mean motion: 15
50795780 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3399
Checksum: 305
Coasting Arc #4 (Orbit 3413)
---------------------------------------
Vector Time (GMT): 2013/164/13:05:45
790
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4414759
78 A = 6788183
79 meter
Y = 725290
25 meter E =
0023679
Z = -5126550
19 I = 51
91654
XDOT = -3132
082580 Wp = 70
42666
YDOT = 6752
986474 meter/sec RA = 125
44080 deg
ZDOT = -1740
661525 TA = 182
75220
MA = 182
76526
Ha = 230
054 n
mi
Hp = 216
450
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14484120
01 X = 4431224
63
Y = 2379561
20 feet Y = 774751
50 meter
Z = -16819390
40 Z = -5105063
67
XDOT = -10275
861482 XDOT = -3198
907511
YDOT = 22155
467434 feet/sec YDOT = 6717
588099 meter/sec
ZDOT = -5710
831776 ZDOT = -1756
038443
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 419437
63 X = 127844
59
Y = -14774549
22 feet Y = -4503282
60 meter
Z = -16729635
52 Z = -5099192
91
XDOT = 22241
557814 XDOT = 6779
226822
YDOT = 7176
103608 feet/sec YDOT = 2187
276380 meter/sec
ZDOT = -5776
033694 ZDOT = -1760
535070
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 13164
56487780
00016717 00000-0 10270-3 0 9030
2 25544 51
6471 126
3092 0010645 62
0242 298
1985 15
50771686 34141
Satellite: ISS
Catalog Number: 25544
Epoch time: 13164
56487780 = yrday
fracday
Element set: 903
Inclination: 51
6471 deg
RA of node: 126
3092 deg
Eccentricity:
0010645
Arg of perigee: 62
0242 deg
Mean anomaly: 298
1985 deg
Mean motion: 15
50771686 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3414
Checksum: 315
Coasting Arc #5 (Orbit 3429)
---------------------------------------
Vector Time (GMT): 2013/165/13:05:45
790
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4160521
43 A = 6787382
51 meter
Y = -1038087
42 meter E =
0012939
Z = 5249939
40 I = 51
93191
XDOT = 3098
996026 Wp = 80
04160
YDOT = -6935
342923 meter/sec RA = 120
49700 deg
ZDOT = 1084
488076 TA = 359
61601
MA = 359
61700
Ha = 230
100 n
mi
Hp = 216
237
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13650004
70 X = -4174106
82
Y = -3405798
63 feet Y = -1084689
46 meter
Z = 17224210
62 Z = 5229694
90
XDOT = 10167
309797 XDOT = 3171
050065
YDOT = -22753
749748 feet/sec YDOT = -6900
285220 meter/sec
ZDOT = 3558
031744 ZDOT = 1099
717050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1304474
85 X = -397603
93
Y = 14111167
61 feet Y = 4301083
89 meter
Z = 17139685
47 Z = 5224176
13
XDOT = -22987
868104 XDOT = -7006
702198
YDOT = -6525
543204 feet/sec YDOT = -1988
985569 meter/sec
ZDOT = 3622
650460 ZDOT = 1104
183860
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 13165
59593304
00016717 00000-0 10270-3 0 9045
2 25544 51
6475 121
1963 0010503 65
5252 294
6993 15
50822179 34309
Satellite: ISS
Catalog Number: 25544
Epoch time: 13165
59593304 = yrday
fracday
Element set: 904
Inclination: 51
6475 deg
RA of node: 121
1963 deg
Eccentricity:
0010503
Arg of perigee: 65
5252 deg
Mean anomaly: 294
6993 deg
Mean motion: 15
50822179 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3430
Checksum: 308
Coasting Arc #6 (Orbit 3444)
---------------------------------------
Vector Time (GMT): 2013/166/13:05:45
790
Vector Time (MET): N/A
Weight (LBS) : 894481
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3972871
05 A = 6787140
92 meter
Y = 1391631
90 meter E =
0025074
Z = -5345527
13 I = 51
94567
XDOT = -3004
875090 Wp = 79
46539
YDOT = 7017
471836 meter/sec RA = 115
55214 deg
ZDOT = -403
523986 TA = 186
67405
MA = 186
70750
Ha = 230
062 n
mi
Hp = 216
287
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13034353
84 X = 3982981
37
Y = 4565721
47 feet Y = 1436116
04 meter
Z = -17537818
68 Z = -5326202
61
XDOT = -9858
514075 XDOT = -3081
162436
YDOT = 23023
201562 feet/sec YDOT = 6983
442914 meter/sec
ZDOT = -1323
897593 ZDOT = -418
306108
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2307584
32 X = 703351
70
Y = -13719950
30 feet Y = -4181840
85 meter
Z = -17457184
63 Z = -5320949
87
XDOT = 23343
360026 XDOT = 7115
056136
YDOT = 5702
475934 feet/sec YDOT = 1738
114665 meter/sec
ZDOT = -1386
670085 ZDOT = -422
657042
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 13166
56254133
00016717 00000-0 10270-3 0 9058
2 25544 51
6476 116
4015 0010618 68
9629 291
2656 15
50797207 34455
Satellite: ISS
Catalog Number: 25544
Epoch time: 13166
56254133 = yrday
fracday
Element set: 905
Inclination: 51
6476 deg
RA of node: 116
4015 deg
Eccentricity:
0010618
Arg of perigee: 68
9629 deg
Mean anomaly: 291
2656 deg
Mean motion: 15
50797207 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3445
Checksum: 317
Coasting Arc #7 (Orbit 3445)
---------------------------------------
Vector Time (GMT): 2013/166/13:46:01
000
Vector Time (MET): N/A
Weight (LBS) : 922037
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4694530
42 A = 6789620
43 meter
Y = 1261260
73 meter E =
0017027
Z = 4725485
99 I = 51
95477
XDOT = 933
287846 Wp = 89
65997
YDOT = -7080
093662 meter/sec RA = 115
43215 deg
ZDOT = 2808
281545 TA = 332
60434
MA = 332
69402
Ha = 230
169 n
mi
Hp = 216
152
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15402002
68 X = -4731240
33
Y = 4137994
53 feet Y = 1208557
88 meter
Z = 15503562
97 Z = 4702591
32
XDOT = 3061
967999 XDOT = 998
747747
YDOT = -23228
653747 feet/sec YDOT = -7069
291277 meter/sec
ZDOT = 9213
522130 ZDOT = 2812
973779
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9120059
29 X = 2779794
07
Y = 13195997
20 feet Y = 4022139
95 meter
Z = 15407638
57 Z = 4696248
24
XDOT = -21919
484009 XDOT = -6681
058726
YDOT = 4334
132429 feet/sec YDOT = 1321
043564 meter/sec
ZDOT = 9234
103764 ZDOT = 2814
554827
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 13166
62698081
00016717 00000-0 10270-3 0 9060
2 25544 51
6479 116
0825 0010588 69
6756 290
5532 15
50818123 34465
Satellite: ISS
Catalog Number: 25544
Epoch time: 13166
62698081 = yrday
fracday
Element set: 906
Inclination: 51
6479 deg
RA of node: 116
0825 deg
Eccentricity:
0010588
Arg of perigee: 69
6756 deg
Mean anomaly: 290
5532 deg
Mean motion: 15
50818123 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3446
Checksum: 329
Coasting Arc #8 (Orbit 3460)
---------------------------------------
Vector Time (GMT): 2013/167/13:46:01
000
Vector Time (MET): N/A
Weight (LBS) : 922037
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4520742
97 A = 6788549
85 meter
Y = -920921
46 meter E =
0023087
Z = -5001152
59 I = 51
96416
XDOT = -910
729808 Wp = 73
58411
YDOT = 7275
357191 meter/sec RA = 110
48998 deg
ZDOT = -2164
892002 TA = 175
35529
MA = 175
33383
Ha = 230
064 n
mi
Hp = 216
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14831833
88 X = 4554999
23
Y = -3021395
87 feet Y = -870175
73 meter
Z = -16407980
95 Z = -4979108
03
XDOT = -2987
958688 XDOT = -981
500245
YDOT = 23869
282123 feet/sec YDOT = 7264
777307 meter/sec
ZDOT = -7102
664048 ZDOT = -2169
487582
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8101736
28 X = -2469409
22
Y = -12903307
29 feet Y = -3932928
06 meter
Z = -16315651
94 Z = -4973010
71
XDOT = 22429
425693 XDOT = 6836
488951
YDOT = -5084
572516 feet/sec YDOT = -1549
777703 meter/sec
ZDOT = -7122
878667 ZDOT = -2171
053418
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 13167
59357959
00016717 00000-0 10270-3 0 9074
2 25544 51
6484 111
2878 0010693 72
7529 287
4791 15
50828238 34613
Satellite: ISS
Catalog Number: 25544
Epoch time: 13167
59357959 = yrday
fracday
Element set: 907
Inclination: 51
6484 deg
RA of node: 111
2878 deg
Eccentricity:
0010693
Arg of perigee: 72
7529 deg
Mean anomaly: 287
4791 deg
Mean motion: 15
50828238 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3461
Checksum: 351
Coasting Arc #9 (Orbit 3476)
---------------------------------------
Vector Time (GMT): 2013/168/13:46:01
000
Vector Time (MET): N/A
Weight (LBS) : 922037
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4350064
60 A = 6787653
08 meter
Y = 553015
53 meter E =
0014126
Z = 5168956
23 I = 51
97104
XDOT = 851
710230 Wp = 91
17876
YDOT = -7474
679861 meter/sec RA = 105
54817 deg
ZDOT = 1512
638426 TA = 344
30705
MA = 344
35079
Ha = 230
145 n
mi
Hp = 216
022
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14271865
48 X = -4381034
78
Y = 1814355
40 feet Y = 504196
77 meter
Z = 16958517
82 Z = 5147748
69
XDOT = 2794
324900 XDOT = 927
882379
YDOT = -24523
227891 feet/sec YDOT = -7464
729721 meter/sec
ZDOT = 4962
724496 ZDOT = 1516
960394
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6995291
90 X = 2132164
97
Y = 12690440
79 feet Y = 3868046
35 meter
Z = 16869735
04 Z = 5141895
24
XDOT = -22885
163749 XDOT = -6975
397911
YDOT = 5975
563332 feet/sec YDOT = 1821
351704 meter/sec
ZDOT = 4981
835186 ZDOT = 1518
463365
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 13168
62460759
00016717 00000-0 10270-3 0 9083
2 25544 51
6481 106
1739 0010541 76
6697 283
5628 15
50853339 34773
Satellite: ISS
Catalog Number: 25544
Epoch time: 13168
62460759 = yrday
fracday
Element set: 908
Inclination: 51
6481 deg
RA of node: 106
1739 deg
Eccentricity:
0010541
Arg of perigee: 76
6697 deg
Mean anomaly: 283
5628 deg
Mean motion: 15
50853339 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3477
Checksum: 340
Coasting Arc #10 (Orbit 3491)
---------------------------------------
Vector Time (GMT): 2013/169/13:46:01
000
Vector Time (MET): N/A
Weight (LBS) : 922037
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4251585
96 A = 6787136
56 meter
Y = -144991
29 meter E =
0025108
Z = -5310351
21 I = 51
97742
XDOT = -764
678288 Wp = 82
05626
YDOT = 7561
731481 meter/sec RA = 100
60558 deg
ZDOT = -818
624353 TA = 180
13036
MA = 180
13102
Ha = 230
029 n
mi
Hp = 216
081
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13948772
82 X = 4278687
78
Y = -475693
22 feet Y = -97295
35 meter
Z = -17422412
09 Z = -5289631
37
XDOT = -2508
787034 XDOT = -845
201678
YDOT = 24808
830317 feet/sec YDOT = 7552
730210 meter/sec
ZDOT = -2685
775435 ZDOT = -822
534013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5853862
76 X = -1784257
37
Y = -12788277
45 feet Y = -3897866
97 meter
Z = -17335721
53 Z = -5283927
92
XDOT = 22922
136247 XDOT = 6986
667128
YDOT = -6827
979501 feet/sec YDOT = -2081
168152 meter/sec
ZDOT = -2703
189305 ZDOT = -823
932100
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 13169
59118963
00016717 00000-0 10270-3 0 9098
2 25544 51
6490 101
3792 0010628 79
7706 280
4643 15
50855158 34921
Satellite: ISS
Catalog Number: 25544
Epoch time: 13169
59118963 = yrday
fracday
Element set: 909
Inclination: 51
6490 deg
RA of node: 101
3792 deg
Eccentricity:
0010628
Arg of perigee: 79
7706 deg
Mean anomaly: 280
4643 deg
Mean motion: 15
50855158 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3492
Checksum: 333
Coasting Arc #11 (Orbit 3506)
---------------------------------------
Vector Time (GMT): 2013/170/12:57:22
141
Vector Time (MET): N/A
Weight (LBS) : 921723
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4225899
77 A = 6788987
84 meter
Y = -735248
47 meter E =
0022346
Z = -5281800
99 I = 51
98240
XDOT = 33
903206 Wp = 83
41528
YDOT = 7575
754718 meter/sec RA = 95
83733 deg
ZDOT = -1028
698123 TA = 176
75822
MA = 176
74371
Ha = 230
037 n
mi
Hp = 217
922
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13864500
55 X = 4259465
23
Y = -2412232
52 feet Y = -687803
53 meter
Z = -17328743
41 Z = -5261190
27
XDOT = 111
230991 XDOT = -45
815849
YDOT = 24854
838315 feet/sec YDOT = 7575
688226 meter/sec
ZDOT = -3374
993843 ZDOT = -1028
726214
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5137374
30 X = -1565871
69
Y = -13214949
84 feet Y = -4027916
71 meter
Z = -17242420
81 Z = -5255489
86
XDOT = 23370
697628 XDOT = 7123
388637
YDOT = -4685
697273 feet/sec YDOT = -1428
200529 meter/sec
ZDOT = -3376
189623 ZDOT = -1029
062597
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 13170
55776508
00016717 00000-0 10270-3 0 9103
2 25544 51
6489 96
5846 0008062 85
7127 274
4944 15
50263945 35078
Satellite: ISS
Catalog Number: 25544
Epoch time: 13170
55776508 = yrday
fracday
Element set: 910
Inclination: 51
6489 deg
RA of node: 96
5846 deg
Eccentricity:
0008062
Arg of perigee: 85
7127 deg
Mean anomaly: 274
4944 deg
Mean motion: 15
50263945 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3507
Checksum: 335
Coasting Arc #12 (Orbit 3522)
---------------------------------------
Vector Time (GMT): 2013/171/12:57:22
141
Vector Time (MET): N/A
Weight (LBS) : 921723
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4168225
30 A = 6788617
91 meter
Y = 559229
55 meter E =
0010546
Z = 5320064
19 I = 51
98384
XDOT = -314
013473 Wp = 95
59764
YDOT = -7643
987167 meter/sec RA = 90
90186 deg
ZDOT = 555
541609 TA = 349
11638
MA = 349
13918
Ha = 230
080 n
mi
Hp = 217
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13675279
87 X = -4200012
64
Y = 1834742
62 feet Y = 512439
37 meter
Z = 17454278
85 Z = 5299737
98
XDOT = -1030
227930 XDOT = -231
212118
YDOT = -25078
698054 feet/sec YDOT = -7647
035771 meter/sec
ZDOT = 1822
643075 ZDOT = 554
216228
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4759431
28 X = 1450674
65
Y = 13064889
27 feet Y = 3982178
25 meter
Z = 17369164
98 Z = 5294121
49
XDOT = -23314
015447 XDOT = -7106
111908
YDOT = 6067
359502 feet/sec YDOT = 1849
331176 meter/sec
ZDOT = 1818
204492 ZDOT = 554
188729
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 13171
58916772
00016717 00000-0 10270-3 0 9117
2 25544 51
6490 91
4734 0007891 89
6511 270
5544 15
50297030 35232
Satellite: ISS
Catalog Number: 25544
Epoch time: 13171
58916772 = yrday
fracday
Element set: 911
Inclination: 51
6490 deg
RA of node: 91
4734 deg
Eccentricity:
0007891
Arg of perigee: 89
6511 deg
Mean anomaly: 270
5544 deg
Mean motion: 15
50297030 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3523
Checksum: 313
Coasting Arc #13 (Orbit 3537)
---------------------------------------
Vector Time (GMT): 2013/172/12:57:22
141
Vector Time (MET): N/A
Weight (LBS) : 921723
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4174525
00 A = 6788561
08 meter
Y = -369965
73 meter E =
0022798
Z = -5360162
96 I = 51
98413
XDOT = 590
059077 Wp = 90
53764
YDOT = 7622
125708 meter/sec RA = 85
96589 deg
ZDOT = -67
001836 TA = 178
82767
MA = 178
82231
Ha = 229
960 n
mi
Hp = 217
913
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13695948
15 X = 4204390
19
Y = -1213798
32 feet Y = -323115
72 meter
Z = -17585836
48 Z = -5339810
85
XDOT = 1935
889359 XDOT = 505
108444
YDOT = 25006
974109 feet/sec YDOT = 7628
249146 meter/sec
ZDOT = -219
822298 ZDOT = -64
340489
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4384454
90 X = -1336381
85
Y = -13146037
01 feet Y = -4006912
08 meter
Z = -17500634
64 Z = -5334193
44
XDOT = 22916
733285 XDOT = 6985
020305
YDOT = -7365
853419 feet/sec YDOT = -2245
112122 meter/sec
ZDOT = -209
808273 ZDOT = -63
949562
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 13172
55610190
00016717 00000-0 10270-3 0 9121
2 25544 51
6501 86
6814 0007962 92
6031 267
6031 15
50290480 35386
Satellite: ISS
Catalog Number: 25544
Epoch time: 13172
55610190 = yrday
fracday
Element set: 912
Inclination: 51
6501 deg
RA of node: 86
6814 deg
Eccentricity:
0007962
Arg of perigee: 92
6031 deg
Mean anomaly: 267
6031 deg
Mean motion: 15
50290480 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3538
Checksum: 291
Coasting Arc #14 (Orbit 3553)
---------------------------------------
Vector Time (GMT): 2013/173/12:57:22
141
Vector Time (MET): N/A
Weight (LBS) : 921723
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4189971
97 A = 6788489
31 meter
Y = 178113
04 meter E =
0010283
Z = 5329308
05 I = 51
98138
XDOT = -864
865107 Wp = 89
87628
YDOT = -7609
806315 meter/sec RA = 81
03010 deg
ZDOT = -424
910443 TA = 4
16007
MA = 4
15153
Ha = 229
995 n
mi
Hp = 217
800
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13746627
21 X = -4217540
66
Y = 584360
36 feet Y = 131103
05 meter
Z = 17484606
46 Z = 5308886
55
XDOT = -2837
483947 XDOT = -777
642224
YDOT = -24966
556150 feet/sec YDOT = -7618
990017 meter/sec
ZDOT = -1394
063134 ZDOT = -428
901355
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4012714
99 X = 1223075
53
Y = 13273692
51 feet Y = 4045821
48 meter
Z = 17399135
19 Z = 5303256
41
XDOT = -22510
944259 XDOT = -6861
335810
YDOT = 8656
071260 feet/sec YDOT = 2638
370520 meter/sec
ZDOT = -1409
627632 ZDOT = -429
654502
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 13173
58748770
00016717 00000-0 10270-3 0 9132
2 25544 51
6502 81
5702 0007803 96
3960 263
8080 15
50326876 35542
Satellite: ISS
Catalog Number: 25544
Epoch time: 13173
58748770 = yrday
fracday
Element set: 913
Inclination: 51
6502 deg
RA of node: 81
5702 deg
Eccentricity:
0007803
Arg of perigee: 96
3960 deg
Mean anomaly: 263
8080 deg
Mean motion: 15
50326876 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3554
Checksum: 318
Coasting Arc #15 (Orbit 3568)
---------------------------------------
Vector Time (GMT): 2013/174/12:57:22
141
Vector Time (MET): N/A
Weight (LBS) : 921723
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4269399
24 A = 6788766
67 meter
Y = 7825
52 meter E =
0022218
Z = -5297595
49 I = 51
97685
XDOT = 1121
467774 Wp = 97
82984
YDOT = 7507
268741 meter/sec RA = 76
09370 deg
ZDOT = 915
241455 TA = 180
90872
MA = 180
91277
Ha = 229
855 n
mi
Hp = 217
952
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14007215
37 X = 4294728
61
Y = 25674
27 feet Y = 55711
19 meter
Z = -17380562
64 Z = -5276793
69
XDOT = 3679
356215 XDOT = 1032
990545
YDOT = 24630
146788 feet/sec YDOT = 7519
314836 meter/sec
ZDOT = 3002
760679 ZDOT = 920
475835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3721231
26 X = -1134231
29
Y = -13615185
62 feet Y = -4149908
58 meter
Z = -17293520
69 Z = -5271065
10
XDOT = 21783
701328 XDOT = 6639
672165
YDOT = -9792
738324 feet/sec YDOT = -2984
826641 meter/sec
ZDOT = 3023
533192 ZDOT = 921
572917
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 13174
55440603
00016717 00000-0 10270-3 0 9145
2 25544 51
6507 76
7782 0007818 99
5024 260
7010 15
50315717 35690
Satellite: ISS
Catalog Number: 25544
Epoch time: 13174
55440603 = yrday
fracday
Element set: 914
Inclination: 51
6507 deg
RA of node: 76
7782 deg
Eccentricity:
0007818
Arg of perigee: 99
5024 deg
Mean anomaly: 260
7010 deg
Mean motion: 15
50315717 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3569
Checksum: 309
Coasting Arc #16 (Orbit 3584)
---------------------------------------
Vector Time (GMT): 2013/175/12:57:22
141
Vector Time (MET): N/A
Weight (LBS) : 921723
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4357126
61 A = 6789013
72 meter
Y = -190977
17 meter E =
0011218
Z = 5193401
12 I = 51
96982
XDOT = -1363
010011 Wp = 85
46974
YDOT = -7415
145969 meter/sec RA = 71
15709 deg
ZDOT = -1412
724875 TA = 18
07205
MA = 18
03220
Ha = 229
885 n
mi
Hp = 217
838
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14295034
80 X = -4379895
12
Y = -626565
51 feet Y = -239829
46 meter
Z = 17038717
57 Z = 5172179
45
XDOT = -4471
817621 XDOT = -1273
128375
YDOT = -24327
906721 feet/sec YDOT = -7429
885220 meter/sec
ZDOT = -4634
924129 ZDOT = -1419
129085
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3458849
61 X = 1054257
36
Y = 13992654
72 feet Y = 4264961
16 meter
Z = 16949940
23 Z = 5166341
78
XDOT = -21069
323739 XDOT = -6421
929876
YDOT = 10867
641200 feet/sec YDOT = 3312
457038 meter/sec
ZDOT = -4660
599105 ZDOT = -1420
550607
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 13175
58577508
00016717 00000-0 10270-3 0 9155
2 25544 51
6506 71
6669 0007685 103
1550 257
0459 15
50355615 35850
Satellite: ISS
Catalog Number: 25544
Epoch time: 13175
58577508 = yrday
fracday
Element set: 915
Inclination: 51
6506 deg
RA of node: 71
6669 deg
Eccentricity:
0007685
Arg of perigee: 103
1550 deg
Mean anomaly: 257
0459 deg
Mean motion: 15
50355615 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3585
Checksum: 329
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