[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 15th 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
170/12:58:27
645 -0
1 3
2 3
2
N/A 3
1 0
0 230
0
000/00:06:55
289 -0
4 -0
1 218
0
Coasting Arc #1 (Orbit 3428)
---------------------------------------
Vector Time (GMT): 2013/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 881745
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3757108
91 A = 6798985
82 meter
Y = -5647220
25 meter E =
0017650
Z = -441422
47 I = 51
96863
XDOT = 3727
501850 Wp = 103
22666
YDOT = 2933
839425 meter/sec RA = 120
71813 deg
ZDOT = -6012
964880 TA = 81
50262
MA = 81
30262
Ha = 230
064 n
mi
Hp = 216
264
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12326472
80 X = 3822122
41
Y = -18527625
49 feet Y = -5604842
34 meter
Z = -1448236
46 Z = -423013
43
XDOT = 12229
336777 XDOT = 3723
627278
YDOT = 9625
457430 feet/sec YDOT = 2975
501611 meter/sec
ZDOT = -19727
575065 ZDOT = -5994
866180
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16665011
69 X = -5079495
56
Y = -14755045
41 feet Y = -4497337
84 meter
Z = -1370491
60 Z = -417725
84
XDOT = 10147
931292 XDOT = 3093
089458
YDOT = -9702
445344 feet/sec YDOT = -2957
305341 meter/sec
ZDOT = -19652
277992 ZDOT = -5990
014332
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
53149298
00016717 00000-0 10270-3 0 9004
2 25544 51
6466 121
5167 0010597 65
9845 294
2414 15
50785178 34293
Satellite: ISS
Catalog Number: 25544
Epoch time: 13165
53149298 = yrday
fracday
Element set: 900
Inclination: 51
6466 deg
RA of node: 121
5167 deg
Eccentricity:
0010597
Arg of perigee: 65
9845 deg
Mean anomaly: 294
2414 deg
Mean motion: 15
50785178 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3429
Checksum: 331
Coasting Arc #2 (Orbit 3444)
---------------------------------------
Vector Time (GMT): 2013/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 881745
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3607686
47 A = 6798608
50 meter
Y = 5661941
87 meter E =
0023883
Z = 1004781
13 I = 51
98216
XDOT = -3542
764654 Wp = 62
04618
YDOT = -3327
126843 meter/sec RA = 115
78530 deg
ZDOT = 5931
683456 TA = 308
78281
MA = 308
99591
Ha = 230
049 n
mi
Hp = 216
193
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11836241
69 X = -3675612
35
Y = 18575924
78 feet Y = 5621218
57 meter
Z = 3296526
00 Z = 987090
80
XDOT = -11623
243616 XDOT = -3534
111203
YDOT = -10915
770481 feet/sec YDOT = -3366
696390 meter/sec
ZDOT = 19460
903726 ZDOT = 5914
493762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17021811
60 X = 5188248
18
Y = 13996670
48 feet Y = 4266185
16 meter
Z = 3221774
04 Z = 981996
73
XDOT = -11221
999779 XDOT = -3420
465533
YDOT = 9109
928861 feet/sec YDOT = 2776
706317 meter/sec
ZDOT = 19389
459769 ZDOT = 5909
907338
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
56254202
00016717 00000-0 10270-3 0 9011
2 25544 51
6464 116
4035 0010554 70
0087 290
2199 15
50804926 34453
Satellite: ISS
Catalog Number: 25544
Epoch time: 13166
56254202 = yrday
fracday
Element set: 901
Inclination: 51
6464 deg
RA of node: 116
4035 deg
Eccentricity:
0010554
Arg of perigee: 70
0087 deg
Mean anomaly: 290
2199 deg
Mean motion: 15
50804926 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3445
Checksum: 288
Coasting Arc #3 (Orbit 3445)
---------------------------------------
Vector Time (GMT): 2013/166/13:46:01
000
Vector Time (MET): N/A
Weight (LBS) : 924038
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4694721
68 A = 6789628
38 meter
Y = 1261912
19 meter E =
0017004
Z = 4725211
93 I = 51
95472
XDOT = 932
888289 Wp = 90
09039
YDOT = -7079
837780 meter/sec RA = 115
43400 deg
ZDOT = 2808
878103 TA = 332
16666
MA = 332
25753
Ha = 230
152 n
mi
Hp = 216
171
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15402630
19 X = -4731437
53
Y = 4140131
85 feet Y = 1209207
16 meter
Z = 15502663
81 Z = 4702316
31
XDOT = 3060
657115 XDOT = 998
342460
YDOT = -23227
814238 feet/sec YDOT = -7069
039895 meter/sec
ZDOT = 9215
479339 ZDOT = 2813
568382
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9122281
11 X = 2780471
28
Y = 13195862
45 feet Y = 4022098
88 meter
Z = 15406735
38 Z = 4695972
94
XDOT = -21918
257428 XDOT = -6680
684864
YDOT = 4334
933001 feet/sec YDOT = 1321
287579 meter/sec
ZDOT = 9236
052758 ZDOT = 2815
148881
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
62698195
00016717 00000-0 10270-3 0 9022
2 25544 51
6478 116
0845 0010520 70
2825 289
9460 15
50815871 34466
Satellite: ISS
Catalog Number: 25544
Epoch time: 13166
62698195 = yrday
fracday
Element set: 902
Inclination: 51
6478 deg
RA of node: 116
0845 deg
Eccentricity:
0010520
Arg of perigee: 70
2825 deg
Mean anomaly: 289
9460 deg
Mean motion: 15
50815871 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3446
Checksum: 322
Coasting Arc #4 (Orbit 3460)
---------------------------------------
Vector Time (GMT): 2013/167/13:46:01
000
Vector Time (MET): N/A
Weight (LBS) : 924038
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4520929
79 A = 6788558
27 meter
Y = -922234
43 meter E =
0023017
Z = -5000680
01 I = 51
96412
XDOT = -909
765005 Wp = 73
85776
YDOT = 7275
134973 meter/sec RA = 110
49184 deg
ZDOT = -2166
241309 TA = 175
06865
MA = 175
04594
Ha = 230
047 n
mi
Hp = 216
193
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14832446
82 X = 4555198
43
Y = -3025703
50 feet Y = -871486
53 meter
Z = -16406430
48 Z = -4978634
51
XDOT = -2984
793324 XDOT = -980
526475
YDOT = 23868
553061 feet/sec YDOT = 7264
565928 meter/sec
ZDOT = -7107
090910 ZDOT = -2170
832181
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8105979
28 X = -2470702
49
Y = -12902350
49 feet Y = -3932636
43 meter
Z = -16314097
38 Z = -4972536
88
XDOT = 22427
685512 XDOT = 6835
958544
YDOT = -5086
992473 feet/sec YDOT = -1550
515306 meter/sec
ZDOT = -7127
285800 ZDOT = -2172
396712
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
59358212
00016717 00000-0 10270-3 0 9033
2 25544 51
6483 111
2899 0010625 73
3503 286
8814 15
50825965 34612
Satellite: ISS
Catalog Number: 25544
Epoch time: 13167
59358212 = yrday
fracday
Element set: 903
Inclination: 51
6483 deg
RA of node: 111
2899 deg
Eccentricity:
0010625
Arg of perigee: 73
3503 deg
Mean anomaly: 286
8814 deg
Mean motion: 15
50825965 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3461
Checksum: 319
Coasting Arc #5 (Orbit 3476)
---------------------------------------
Vector Time (GMT): 2013/168/13:46:01
000
Vector Time (MET): N/A
Weight (LBS) : 924038
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4350434
73 A = 6787662
53 meter
Y = 555630
57 meter E =
0014093
Z = 5168437
47 I = 51
97100
XDOT = 849
953430 Wp = 91
69794
YDOT = -7474
342627 meter/sec RA = 105
55006 deg
ZDOT = 1514
998004 TA = 343
76397
MA = 343
80907
Ha = 230
126 n
mi
Hp = 216
045
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14273079
84 X = -4381431
61
Y = 1822934
94 feet Y = 506807
53 meter
Z = 16956815
84 Z = 5147228
07
XDOT = 2788
561121 XDOT = 926
110476
YDOT = -24522
121481 feet/sec YDOT = -7464
412217 meter/sec
ZDOT = 4970
465891 ZDOT = 1519
311400
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7003709
60 X = 2134730
69
Y = 12688391
98 feet Y = 3867421
88 meter
Z = 16868024
90 Z = 5141373
99
XDOT = -22882
138685 XDOT = -6974
475871
YDOT = 5979
941760 feet/sec YDOT = 1822
686249 meter/sec
ZDOT = 4989
540679 ZDOT = 1520
811999
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
62461164
00016717 00000-0 10270-3 0 9040
2 25544 51
6480 106
1760 0010473 77
2765 282
9556 15
50850979 34773
Satellite: ISS
Catalog Number: 25544
Epoch time: 13168
62461164 = yrday
fracday
Element set: 904
Inclination: 51
6480 deg
RA of node: 106
1760 deg
Eccentricity:
0010473
Arg of perigee: 77
2765 deg
Mean anomaly: 282
9556 deg
Mean motion: 15
50850979 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3477
Checksum: 327
Coasting Arc #6 (Orbit 3491)
---------------------------------------
Vector Time (GMT): 2013/169/13:46:01
000
Vector Time (MET): N/A
Weight (LBS) : 924038
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4251922
16 A = 6787145
02 meter
Y = -148324
70 meter E =
0025041
Z = -5309942
49 I = 51
97738
XDOT = -762
409339 Wp = 82
30078
YDOT = 7561
665105 meter/sec RA = 100
60749 deg
ZDOT = -821
781867 TA = 179
85625
MA = 179
85553
Ha = 230
010 n
mi
Hp = 216
105
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13949875
87 X = 4279059
25
Y = -486629
59 feet Y = -100624
80 meter
Z = -17421071
17 Z = -5289220
94
XDOT = -2501
342976 XDOT = -842
916817
YDOT = 24808
612549 feet/sec YDOT = 7552
689296 meter/sec
ZDOT = -2696
134734 ZDOT = -825
680466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5864377
01 X = -1787462
11
Y = -12785075
77 feet Y = -3896891
09 meter
Z = -17334372
95 Z = -5283516
88
XDOT = 22919
276385 XDOT = 6985
795442
YDOT = -6834
057457 feet/sec YDOT = -2083
020713 meter/sec
ZDOT = -2713
502322 ZDOT = -827
075508
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
59119513
00016717 00000-0 10270-3 0 9056
2 25544 51
6489 101
3813 0010559 80
3688 279
8656 15
50852829 34921
Satellite: ISS
Catalog Number: 25544
Epoch time: 13169
59119513 = yrday
fracday
Element set: 905
Inclination: 51
6489 deg
RA of node: 101
3813 deg
Eccentricity:
0010559
Arg of perigee: 80
3688 deg
Mean anomaly: 279
8656 deg
Mean motion: 15
50852829 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3492
Checksum: 341
Coasting Arc #7 (Orbit 3506)
---------------------------------------
Vector Time (GMT): 2013/170/13:01:55
289
Vector Time (MET): N/A
Weight (LBS) : 923737
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4038428
00 A = 6788860
06 meter
Y = 1331702
40 meter E =
0022366
Z = -5311459
17 I = 51
98192
XDOT = -1398
548999 Wp = 91
87397
YDOT = 7472
436807 meter/sec RA = 95
80849 deg
ZDOT = 812
401435 TA = 185
86447
MA = 185
89070
Ha = 230
009 n
mi
Hp = 217
958
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13249435
71 X = 4049038
38
Y = 4369102
38 feet Y = 1376922
57 meter
Z = -17426047
15 Z = -5291814
71
XDOT = -4588
415350 XDOT = -1485
949927
YDOT = 24515
868791 feet/sec YDOT = 7456
308573 meter/sec
ZDOT = 2665
359039 ZDOT = 805
395874
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1352739
13 X = 412314
89
Y = -13987758
03 feet Y = -4263468
65 meter
Z = -17344060
76 Z = -5286469
72
XDOT = 23910
395439 XDOT = 7287
888530
YDOT = -945
730768 feet/sec YDOT = -288
258738 meter/sec
ZDOT = 2634
989989 ZDOT = 803
144949
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
55777139
00016717 00000-0 10270-3 0 9069
2 25544 51
6488 96
5868 0007976 83
8899 276
3160 15
50260565 35075
Satellite: ISS
Catalog Number: 25544
Epoch time: 13170
55777139 = yrday
fracday
Element set: 906
Inclination: 51
6488 deg
RA of node: 96
5868 deg
Eccentricity:
0007976
Arg of perigee: 83
8899 deg
Mean anomaly: 276
3160 deg
Mean motion: 15
50260565 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3507
Checksum: 358
Coasting Arc #8 (Orbit 3522)
---------------------------------------
Vector Time (GMT): 2013/171/13:01:55
289
Vector Time (MET): N/A
Weight (LBS) : 923737
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4056266
09 A = 6789035
83 meter
Y = -1520927
62 meter E =
0011636
Z = 5218079
22 I = 51
98530
XDOT = 1127
866983 Wp = 76
12881
YDOT = -7475
347839 meter/sec RA = 90
87294 deg
ZDOT = -1296
980684 TA = 26
29393
MA = 26
23491
Ha = 230
029 n
mi
Hp = 217
813
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13307959
61 X = -4064305
56
Y = -4989920
00 feet Y = -1566333
00 meter
Z = 17119682
47 Z = 5198354
29
XDOT = 3700
350995 XDOT = 1217
674559
YDOT = -24525
419418 feet/sec YDOT = -7462
232999 meter/sec
ZDOT = -4255
185970 ZDOT = -1291
284424
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1702151
02 X = -518815
63
Y = 14209673
15 feet Y = 4331108
38 meter
Z = 17037385
05 Z = 5192994
96
XDOT = -23679
310911 XDOT = -7217
453966
YDOT = 2255
884244 feet/sec YDOT = 687
593517 meter/sec
ZDOT = -4230
274440 ZDOT = -1289
387649
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
58917002
00016717 00000-0 10270-3 0 9079
2 25544 51
6489 91
4755 0007831 87
2329 272
9717 15
50308401 35231
Satellite: ISS
Catalog Number: 25544
Epoch time: 13171
58917002 = yrday
fracday
Element set: 907
Inclination: 51
6489 deg
RA of node: 91
4755 deg
Eccentricity:
0007831
Arg of perigee: 87
2329 deg
Mean anomaly: 272
9717 deg
Mean motion: 15
50308401 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3523
Checksum: 314
Coasting Arc #9 (Orbit 3537)
---------------------------------------
Vector Time (GMT): 2013/172/13:01:55
289
Vector Time (MET): N/A
Weight (LBS) : 923737
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4138058
89 A = 6789583
60 meter
Y = 1697402
57 meter E =
0021012
Z = -5126942
74 I = 51
98748
XDOT = -854
598337 Wp = 98
50524
YDOT = 7391
506821 meter/sec RA = 85
93755 deg
ZDOT = 1760
526141 TA = 188
46910
MA = 188
50462
Ha = 229
939 n
mi
Hp = 217
937
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13576308
71 X = 4143676
11
Y = 5568906
07 feet Y = 1743709
18 meter
Z = -16820678
27 Z = -5106826
35
XDOT = -2803
800317 XDOT = -945
740472
YDOT = 24250
350461 feet/sec YDOT = 7381
440278 meter/sec
ZDOT = 5776
004398 ZDOT = 1756
154341
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1950922
84 X = 594641
28
Y = -14640308
70 feet Y = -4462366
09 meter
Z = -16736766
47 Z = -5101366
42
XDOT = 23118
516003 XDOT = 7046
523678
YDOT = -3488
399352 feet/sec YDOT = -1063
264122 meter/sec
ZDOT = 5756
627541 ZDOT = 1754
620074
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
55610050
00016717 00000-0 10270-3 0 9081
2 25544 51
6500 86
6835 0007883 90
7429 269
4625 15
50287920 35384
Satellite: ISS
Catalog Number: 25544
Epoch time: 13172
55610050 = yrday
fracday
Element set: 908
Inclination: 51
6500 deg
RA of node: 86
6835 deg
Eccentricity:
0007883
Arg of perigee: 90
7429 deg
Mean anomaly: 269
4625 deg
Mean motion: 15
50287920 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3538
Checksum: 319
Coasting Arc #10 (Orbit 3553)
---------------------------------------
Vector Time (GMT): 2013/173/13:01:55
289
Vector Time (MET): N/A
Weight (LBS) : 923737
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4224554
06 A = 6790059
81 meter
Y = -1879806
16 meter E =
0013553
Z = 4961972
66 I = 51
98662
XDOT = 614
145774 Wp = 77
46554
YDOT = -7310
686997 meter/sec RA = 81
00246 deg
ZDOT = -2238
720646 TA = 34
32151
MA = 34
23401
Ha = 229
953 n
mi
Hp = 217
800
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13860085
51 X = -4227323
66
Y = -6167343
03 feet Y = -1927064
13 meter
Z = 16279437
86 Z = 4941443
05
XDOT = 2014
913956 XDOT = 706
724935
YDOT = -23985
193560 feet/sec YDOT = -7303
301203 meter/sec
ZDOT = -7344
884010 ZDOT = -2235
513575
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2200264
91 X = -670640
74
Y = 15102224
67 feet Y = 4603158
08 meter
Z = 16193820
79 Z = 4935876
58
XDOT = -22559
599470 XDOT = -6876
165918
YDOT = 4601
782781 feet/sec YDOT = 1402
623392 meter/sec
ZDOT = -7330
376209 ZDOT = -2234
298669
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
58748243
00016717 00000-0 10270-3 0 9092
2 25544 51
6501 81
5722 0007760 93
9401 266
2637 15
50336339 35548
Satellite: ISS
Catalog Number: 25544
Epoch time: 13173
58748243 = yrday
fracday
Element set: 909
Inclination: 51
6501 deg
RA of node: 81
5722 deg
Eccentricity:
0007760
Arg of perigee: 93
9401 deg
Mean anomaly: 266
2637 deg
Mean motion: 15
50336339 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3554
Checksum: 314
Coasting Arc #11 (Orbit 3568)
---------------------------------------
Vector Time (GMT): 2013/174/13:01:55
289
Vector Time (MET): N/A
Weight (LBS) : 923737
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4371079
04 A = 6790856
76 meter
Y = 2031415
07 meter E =
0018791
Z = -4801270
81 I = 51
98375
XDOT = -384
540809 Wp = 104
04708
YDOT = 7151
921280 meter/sec RA = 76
06744 deg
ZDOT = 2680
249151 TA = 192
34466
MA = 192
39076
Ha = 229
842 n
mi
Hp = 217
961
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14340810
51 X = 4371361
63
Y = 6664747
61 feet Y = 2080297
66 meter
Z = -15752200
82 Z = -4780035
54
XDOT = -1261
616827 XDOT = -477
506430
YDOT = 23464
308662 feet/sec YDOT = 7147
100832 meter/sec
ZDOT = 8793
468343 ZDOT = 2678
156540
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2281240
17 X = 695322
01
Y = -15737075
92 feet Y = -4796660
74 meter
Z = -15663649
71 Z = -4774280
43
XDOT = 21722
427514 XDOT = 6620
995906
YDOT = -5579
455738 feet/sec YDOT = -1700
618109 meter/sec
ZDOT = 8783
635207 ZDOT = 2677
252011
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
55439698
00016717 00000-0 10270-3 0 9103
2 25544 51
6505 76
7803 0007749 97
6234 262
5797 15
50314638 35690
Satellite: ISS
Catalog Number: 25544
Epoch time: 13174
55439698 = yrday
fracday
Element set: 910
Inclination: 51
6505 deg
RA of node: 76
7803 deg
Eccentricity:
0007749
Arg of perigee: 97
6234 deg
Mean anomaly: 262
5797 deg
Mean motion: 15
50314638 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3569
Checksum: 347
Coasting Arc #12 (Orbit 3584)
---------------------------------------
Vector Time (GMT): 2013/175/13:01:55
289
Vector Time (MET): N/A
Weight (LBS) : 923737
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4517779
93 A = 6791586
66 meter
Y = -2183660
04 meter E =
0015748
Z = 4564383
69 I = 51
97834
XDOT = 201
052197 Wp = 82
59861
YDOT = -6996
655978 meter/sec RA = 71
13226 deg
ZDOT = -3137
072694 TA = 38
73388
MA = 38
62107
Ha = 229
850 n
mi
Hp = 217
828
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14822112
62 X = -4515198
32
Y = -7164238
98 feet Y = -2234167
02 meter
Z = 14975012
11 Z = 4542442
84
XDOT = 659
620070 XDOT = 294
514277
YDOT = -22954
908063 feet/sec YDOT = -6993
884598 meter/sec
ZDOT = -10292
233248 ZDOT = -3135
870137
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2343227
82 X = -714215
84
Y = 16378712
55 feet Y = 4992231
59 meter
Z = 14883527
43 Z = 4536499
16
XDOT = -20915
115992 XDOT = -6374
927355
YDOT = 6388
556224 feet/sec YDOT = 1947
231937 meter/sec
ZDOT = -10286
139604 ZDOT = -3135
215351
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
58576227
00016717 00000-0 10270-3 0 9118
2 25544 51
6505 71
6688 0007657 100
6675 259
5338 15
50363279 35857
Satellite: ISS
Catalog Number: 25544
Epoch time: 13175
58576227 = yrday
fracday
Element set: 911
Inclination: 51
6505 deg
RA of node: 71
6688 deg
Eccentricity:
0007657
Arg of perigee: 100
6675 deg
Mean anomaly: 259
5338 deg
Mean motion: 15
50363279 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3585
Checksum: 339
Coasting Arc #13 (Orbit 3599)
---------------------------------------
Vector Time (GMT): 2013/176/13:01:55
289
Vector Time (MET): N/A
Weight (LBS) : 923737
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4716052
48 A = 6792562
91 meter
Y = 2289260
68 meter E =
0015983
Z = -4335545
08 I = 51
97011
XDOT = -38
718609 Wp = 107
43724
YDOT = 6778
536275 meter/sec RA = 66
19663 deg
ZDOT = 3543
209273 TA = 198
55552
MA = 198
61387
Ha = 229
727 n
mi
Hp = 218
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15472613
11 X = 4711163
59
Y = 7510697
77 feet Y = 2341971
83 meter
Z = -14224229
28 Z = -4312646
77
XDOT = -127
029557 XDOT = -131
726518
YDOT = 22239
292242 feet/sec YDOT = 6777
582763 meter/sec
ZDOT = 11624
702340 ZDOT = 3542
796232
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2184859
62 X = 665945
21
Y = -17139014
62 feet Y = -5223971
66 meter
Z = -14128750
91 Z = -4306443
28
XDOT = 19904
553635 XDOT = 6066
907948
YDOT = -7026
631190 feet/sec YDOT = -2141
717187 meter/sec
ZDOT = 11621
940208 ZDOT = 3542
367375
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 13176
55266099
00016717 00000-0 10270-3 0 9120
2 25544 51
6500 66
8763 0007601 104
6708 255
5286 15
50339587 36003
Satellite: ISS
Catalog Number: 25544
Epoch time: 13176
55266099 = yrday
fracday
Element set: 912
Inclination: 51
6500 deg
RA of node: 66
8763 deg
Eccentricity:
0007601
Arg of perigee: 104
6708 deg
Mean anomaly: 255
5286 deg
Mean motion: 15
50339587 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3600
Checksum: 317
Coasting Arc #14 (Orbit 3615)
---------------------------------------
Vector Time (GMT): 2013/177/13:01:55
289
Vector Time (MET): N/A
Weight (LBS) : 923737
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4906561
05 A = 6793462
13 meter
Y = -2391622
50 meter E =
0017849
Z = 4028897
45 I = 51
96034
XDOT = -65
199606 Wp = 90
34537
YDOT = -6567
044634 meter/sec RA = 61
26084 deg
ZDOT = -3962
695933 TA = 40
71427
MA = 40
58100
Ha = 229
721 n
mi
Hp = 217
899
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16097641
24 X = -4899023
78
Y = -7846530
51 feet Y = -2446449
09 meter
Z = 13218167
48 Z = 4005080
16
XDOT = -213
909467 XDOT = 27
488800
YDOT = -21545
422029 feet/sec YDOT = -6567
255023 meter/sec
ZDOT = -13000
970908 ZDOT = -3962
788299
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2000016
72 X = -609605
10
Y = 17869458
42 feet Y = 5446610
93 meter
Z = 13118857
99 Z = 3998627
92
XDOT = -18965
125846 XDOT = -5780
570358
YDOT = 7458
001003 feet/sec YDOT = 2273
198706 meter/sec
ZDOT = -13000
351824 ZDOT = -3962
507236
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 13177
58400969
00016717 00000-0 10270-3 0 9131
2 25544 51
6500 61
7644 0007526 107
5715 252
6258 15
50387947 36168
Satellite: ISS
Catalog Number: 25544
Epoch time: 13177
58400969 = yrday
fracday
Element set: 913
Inclination: 51
6500 deg
RA of node: 61
7644 deg
Eccentricity:
0007526
Arg of perigee: 107
5715 deg
Mean anomaly: 252
6258 deg
Mean motion: 15
50387947 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3616
Checksum: 323
Coasting Arc #15 (Orbit 3630)
---------------------------------------
Vector Time (GMT): 2013/178/13:01:55
289
Vector Time (MET): N/A
Weight (LBS) : 923737
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5136592
90 A = 6794519
71 meter
Y = 2435265
80 meter E =
0013077
Z = -3735782
54 I = 51
94714
XDOT = 142
657253 Wp = 106
83255
YDOT = 6312
557976 meter/sec RA = 56
32411 deg
ZDOT = 4319
979075 TA = 208
94539
MA = 209
01798
Ha = 229
607 n
mi
Hp = 218
096
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16852338
92 X = 5127126
68
Y = 7989717
20 feet Y = 2492653
86 meter
Z = -12256504
40 Z = -3710852
48
XDOT = 468
035608 XDOT = 51
073217
YDOT = 20710
492047 feet/sec YDOT = 6313
640763 meter/sec
ZDOT = 14173
159696 ZDOT = 4320
450248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1564732
01 X = 476930
32
Y = -18652775
72 feet Y = -5685366
04 meter
Z = -12152546
22 Z = -3704096
09
XDOT = 17910
771393 XDOT = 5459
203121
YDOT = -7713
150021 feet/sec YDOT = -2350
968126 meter/sec
ZDOT = 14174
160427 ZDOT = 4320
284098
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 13178
55089289
00016717 00000-0 10270-3 0 9148
2 25544 51
6491 56
9713 0007472 111
9534 248
2411 15
50362273 36312
Satellite: ISS
Catalog Number: 25544
Epoch time: 13178
55089289 = yrday
fracday
Element set: 914
Inclination: 51
6491 deg
RA of node: 56
9713 deg
Eccentricity:
0007472
Arg of perigee: 111
9534 deg
Mean anomaly: 248
2411 deg
Mean motion: 15
50362273 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3631
Checksum: 314
Coasting Arc #16 (Orbit 3646)
---------------------------------------
Vector Time (GMT): 2013/179/13:01:55
289
Vector Time (MET): N/A
Weight (LBS) : 923737
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5348058
84 A = 6795469
01 meter
Y = -2474242
95 meter E =
0019560
Z = 3364363
11 I = 51
93329
XDOT = -151
773460 Wp = 99
70275
YDOT = -6070
477246 meter/sec RA = 51
38755 deg
ZDOT = -4685
726794 TA = 41
26361
MA = 41
11594
Ha = 229
566 n
mi
Hp = 218
008
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17546124
80 X = -5336336
86
Y = -8117594
98 feet Y = -2533983
07 meter
Z = 11037936
73 Z = 3338411
21
XDOT = -497
944421 XDOT = -61
118994
YDOT = -19916
263931 feet/sec YDOT = -6071
667194 meter/sec
ZDOT = -15373
119404 ZDOT = -4686
244416
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1111759
34 X = -338864
25
Y = 19362419
16 feet Y = 5901665
36 meter
Z = 10929712
08 Z = 3331376
24
XDOT = -16978
129232 XDOT = -5174
933790
YDOT = 7740
934839 feet/sec YDOT = 2359
436939 meter/sec
ZDOT = -15374
346340 ZDOT = -4686
100764
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 13179
58222531
00016717 00000-0 10270-3 0 9152
2 25544 51
6494 51
8591 0007384 114
7879 245
4041 15
50410783 36473
Satellite: ISS
Catalog Number: 25544
Epoch time: 13179
58222531 = yrday
fracday
Element set: 915
Inclination: 51
6494 deg
RA of node: 51
8591 deg
Eccentricity:
0007384
Arg of perigee: 114
7879 deg
Mean anomaly: 245
4041 deg
Mean motion: 15
50410783 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3647
Checksum: 319
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