[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 20th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 25295 19 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 124 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 3 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
099/21:16:36
000 0
0 0
0 0
0
N/A 0
0 0
0 226
7
000/00:00:00
000 0
0 0
0 220
1
102/15:22:48
548 3
6 5
5 5
6
N/A 4
0 -0
4 226
7
000/00:13:37
097 -1
2 -0
0 223
2
106/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 226
8
000/00:00:00
000 0
0 0
0 222
8
Coasting Arc #1 (Orbit 39)
---------------------------------------
Vector Time (GMT): 2014/097/17:01:59
341
Vector Time (MET): N/A
Weight (LBS) : 888709
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3693920
11 A = 6789790
79 meter
Y = 2975442
53 meter E =
0006081
Z = 4853486
36 I = 51
99365
XDOT = -2214
843543 Wp = 98
91659
YDOT = -6887
827804 meter/sec RA = 88
05407 deg
ZDOT = 2533
297027 TA = 326
26719
MA = 326
30587
Ha = 226
859 n
mi
Hp = 220
294
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12119160
46 X = -3750494
34
Y = 9761950
55 feet Y = 2933818
81 meter
Z = 15923511
68 Z = 4835404
14
XDOT = -7266
547058 XDOT = -2149
963643
YDOT = -22597
860249 feet/sec YDOT = -6912
232637 meter/sec
ZDOT = 8311
341951 ZDOT = 2522
695762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9883031
22 X = 3012347
92
Y = 12121907
05 feet Y = 3694757
27 meter
Z = 15846545
87 Z = 4830027
18
XDOT = -21640
117816 XDOT = -6595
907910
YDOT = 6819
776895 feet/sec YDOT = 2078
667998 meter/sec
ZDOT = 8267
559728 ZDOT = 2519
952205
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 14097
76250877
00016717 00000-0 10270-3 0 9000
2 25544 51
6480 88
5903 0002624 354
6196 5
4926 15
50582954 401
Satellite: ISS
Catalog Number: 25544
Epoch time: 14097
76250877 = yrday
fracday
Element set: 900
Inclination: 51
6480 deg
RA of node: 88
5903 deg
Eccentricity:
0002624
Arg of perigee: 354
6196 deg
Mean anomaly: 5
4926 deg
Mean motion: 15
50582954 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 40
Checksum: 315
Coasting Arc #2 (Orbit 54)
---------------------------------------
Vector Time (GMT): 2014/098/17:01:59
341
Vector Time (MET): N/A
Weight (LBS) : 888709
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3664006
40 A = 6788813
54 meter
Y = -2672934
87 meter E =
0013775
Z = -5064060
27 I = 51
98958
XDOT = 2390
419362 Wp = 64
48906
YDOT = 6998
998874 meter/sec RA = 83
11619 deg
ZDOT = -1963
095481 TA = 186
49965
MA = 186
51754
Ha = 226
737 n
mi
Hp = 220
241
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12021018
36 X = 3718223
03
Y = -8769471
36 feet Y = -2631658
92 meter
Z = -16614370
97 Z = -5046129
10
XDOT = 7842
583208 XDOT = 2321
513408
YDOT = 22962
594732 feet/sec YDOT = 7025
344624 meter/sec
ZDOT = -6440
601971 ZDOT = -1951
651157
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9095485
01 X = -2772303
83
Y = -11883169
46 feet Y = -3621990
05 meter
Z = -16538085
41 Z = -5040808
43
XDOT = 21873
984544 XDOT = 6667
190489
YDOT = -7837
512099 feet/sec YDOT = -2388
873688 meter/sec
ZDOT = -6393
278405 ZDOT = -1948
671258
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 14098
72924083
00016717 00000-0 10270-3 0 9015
2 25544 51
6487 83
7969 0002698 359
5081
6067 15
50632406 552
Satellite: ISS
Catalog Number: 25544
Epoch time: 14098
72924083 = yrday
fracday
Element set: 901
Inclination: 51
6487 deg
RA of node: 83
7969 deg
Eccentricity:
0002698
Arg of perigee: 359
5081 deg
Mean anomaly:
6067 deg
Mean motion: 15
50632406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 55
Checksum: 321
Coasting Arc #3 (Orbit 70)
---------------------------------------
Vector Time (GMT): 2014/099/17:01:59
341
Vector Time (MET): N/A
Weight (LBS) : 888709
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3670633
53 A = 6788013
94 meter
Y = 2334960
16 meter E =
0003621
Z = 5207570
23 I = 51
98245
XDOT = -2573
959126 Wp = 87
90130
YDOT = -7090
590709 meter/sec RA = 78
17700 deg
ZDOT = 1364
284211 TA = 349
03869
MA = 349
04658
Ha = 226
814 n
mi
Hp = 220
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12042760
93 X = -3721767
50
Y = 7660630
44 feet Y = 2293627
40 meter
Z = 17085204
15 Z = 5189614
35
XDOT = -8444
747789 XDOT = -2501
106499
YDOT = -23263
092877 feet/sec YDOT = -7118
966891 meter/sec
ZDOT = 4475
998067 ZDOT = 1351
957941
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8191919
71 X = 2496897
13
Y = 11798668
60 feet Y = 3596234
19 meter
Z = 17008863
02 Z = 5184301
45
XDOT = -22004
833167 XDOT = -6707
073149
YDOT = 8895
889168 feet/sec YDOT = 2711
467018 meter/sec
ZDOT = 4424
965993 ZDOT = 1348
729635
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 14099
76039187
00016717 00000-0 10270-3 0 9023
2 25544 51
6484 78
6836 0002609 1
1659 358
9497 15
50676759 711
Satellite: ISS
Catalog Number: 25544
Epoch time: 14099
76039187 = yrday
fracday
Element set: 902
Inclination: 51
6484 deg
RA of node: 78
6836 deg
Eccentricity:
0002609
Arg of perigee: 1
1659 deg
Mean anomaly: 358
9497 deg
Mean motion: 15
50676759 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 71
Checksum: 348
Coasting Arc #4 (Orbit 72)
---------------------------------------
Vector Time (GMT): 2014/099/21:16:36
000
Vector Time (MET): N/A
Weight (LBS) : 904195
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2529385
52 A = 6798595
34 meter
Y = 6141136
13 meter E =
0010681
Z = -1427721
61 I = 52
01382
XDOT = -3986
082897 Wp = 28
43754
YDOT = 2989
050158 meter/sec RA = 77
27818 deg
ZDOT = 5822
108749 TA = 316
09732
MA = 316
18214
Ha = 226
693 n
mi
Hp = 220
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8298508
91 X = 2467461
38
Y = 20148084
41 feet Y = 6169074
95 meter
Z = -4684126
03 Z = -1415585
25
XDOT = -13077
699793 XDOT = -4047
492848
YDOT = 9806
595007 feet/sec YDOT = 2944
132460 meter/sec
ZDOT = 19101
406656 ZDOT = 5802
595427
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 449360
22 X = 136964
99
Y = -21796285
00 feet Y = -6643507
67 meter
Z = -4633748
76 Z = -1412366
62
XDOT = 14432
961985 XDOT = 4399
166813
YDOT = -3726
600963 feet/sec YDOT = -1135
867973 meter/sec
ZDOT = 19018
371654 ZDOT = 5796
799680
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 14099
88928247
00016717 00000-0 10270-3 0 9031
2 25544 51
6458 78
0423 0002630 357
3834 2
7303 15
50656548 739
Satellite: ISS
Catalog Number: 25544
Epoch time: 14099
88928247 = yrday
fracday
Element set: 903
Inclination: 51
6458 deg
RA of node: 78
0423 deg
Eccentricity:
0002630
Arg of perigee: 357
3834 deg
Mean anomaly: 2
7303 deg
Mean motion: 15
50656548 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 73
Checksum: 314
Coasting Arc #5 (Orbit 88)
---------------------------------------
Vector Time (GMT): 2014/100/21:16:36
000
Vector Time (MET): N/A
Weight (LBS) : 904195
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2666626
80 A = 6798880
91 meter
Y = -6191080
30 meter E =
0011997
Z = 849719
14 I = 52
00819
XDOT = 4065
633978 Wp = 115
05349
YDOT = -2577
627504 meter/sec RA = 72
34764 deg
ZDOT = -5960
960530 TA = 55
81562
MA = 55
70196
Ha = 226
597 n
mi
Hp = 219
935
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8748775
58 X = -2601326
22
Y = -20311943
25 feet Y = -6220535
02 meter
Z = 2787792
45 Z = 836924
32
XDOT = 13338
694152 XDOT = 4123
111944
YDOT = -8456
783150 feet/sec YDOT = -2531
842275 meter/sec
ZDOT = -19556
957121 ZDOT = -5941
070293
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 267034
21 X = 81392
03
Y = 22120992
41 feet Y = 6742478
49 meter
Z = 2734645
64 Z = 833519
99
XDOT = -14067
015237 XDOT = -4287
626244
YDOT = 2602
151793 feet/sec YDOT = 793
135866 meter/sec
ZDOT = -19472
389585 ZDOT = -5935
184345
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 14100
92039954
00016717 00000-0 10270-3 0 9048
2 25544 51
6461 72
9287 0002747 1
3394 358
7764 15
50747802 896
Satellite: ISS
Catalog Number: 25544
Epoch time: 14100
92039954 = yrday
fracday
Element set: 904
Inclination: 51
6461 deg
RA of node: 72
9287 deg
Eccentricity:
0002747
Arg of perigee: 1
3394 deg
Mean anomaly: 358
7764 deg
Mean motion: 15
50747802 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 89
Checksum: 318
Coasting Arc #6 (Orbit 103)
---------------------------------------
Vector Time (GMT): 2014/101/21:16:36
000
Vector Time (MET): N/A
Weight (LBS) : 904195
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2810326
08 A = 6799158
02 meter
Y = 6176822
52 meter E =
0013587
Z = -284861
68 I = 51
99777
XDOT = -4197
094140 Wp = 36
88896
YDOT = 2180
401413 meter/sec RA = 67
41502 deg
ZDOT = 6031
385330 TA = 320
06005
MA = 320
15993
Ha = 226
649 n
mi
Hp = 219
854
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9220229
92 X = 2742430
36
Y = 20265165
75 feet Y = 6207869
73 meter
Z = -934585
58 Z = -271375
11
XDOT = -13769
993898 XDOT = -4250
462646
YDOT = 7153
547943 feet/sec YDOT = 2133
169144 meter/sec
ZDOT = 19788
009612 ZDOT = 6010
866430
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1092075
81 X = -332864
71
Y = -22239572
99 feet Y = -6778621
85 meter
Z = -878519
49 Z = -267772
74
XDOT = 13931
962212 XDOT = 4246
462082
YDOT = -1440
408561 feet/sec YDOT = -439
036529 meter/sec
ZDOT = 19700
844282 ZDOT = 6004
817337
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 14101
88704635
00016717 00000-0 10270-3 0 9050
2 25544 51
6451 68
1333 0002467 6
2464 353
8717 15
50742964 1041
Satellite: ISS
Catalog Number: 25544
Epoch time: 14101
88704635 = yrday
fracday
Element set: 905
Inclination: 51
6451 deg
RA of node: 68
1333 deg
Eccentricity:
0002467
Arg of perigee: 6
2464 deg
Mean anomaly: 353
8717 deg
Mean motion: 15
50742964 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 104
Checksum: 295
Coasting Arc #7 (Orbit 115)
---------------------------------------
Vector Time (GMT): 2014/102/15:29:37
097
Vector Time (MET): N/A
Weight (LBS) : 903571
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4109081
79 A = 6790485
86 meter
Y = -1065324
06 meter E =
0010685
Z = -5309373
51 I = 51
95254
XDOT = 2827
099260 Wp = 92
33654
YDOT = 7070
310185 meter/sec RA = 63
66523 deg
ZDOT = 770
234213 TA = 185
00034
MA = 185
01102
Ha = 226
694 n
mi
Hp = 223
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13481239
47 X = 4146480
54
Y = -3495157
67 feet Y = -1019165
21 meter
Z = -17419204
42 Z = -5289321
03
XDOT = 9275
260041 XDOT = 2744
085756
YDOT = 23196
555724 feet/sec YDOT = 7101
460564 meter/sec
ZDOT = 2527
015136 ZDOT = 783
765465
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 791940
29 X = 241383
40
Y = -14010253
91 feet Y = -4270325
39 meter
Z = -17334192
90 Z = -5283462
00
XDOT = 23891
027700 XDOT = 7281
985243
YDOT = -1841
777197 feet/sec YDOT = -561
373690 meter/sec
ZDOT = 2583
116775 ZDOT = 787
333993
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 14102
66035009
00016717 00000-0 10270-3 0 9060
2 25544 51
6485 64
2998 0003913 285
8468 74
2251 15
49698906 1162
Satellite: ISS
Catalog Number: 25544
Epoch time: 14102
66035009 = yrday
fracday
Element set: 906
Inclination: 51
6485 deg
RA of node: 64
2998 deg
Eccentricity:
0003913
Arg of perigee: 285
8468 deg
Mean anomaly: 74
2251 deg
Mean motion: 15
49698906 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 116
Checksum: 326
Coasting Arc #8 (Orbit 131)
---------------------------------------
Vector Time (GMT): 2014/103/15:29:37
097
Vector Time (MET): N/A
Weight (LBS) : 903571
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4136533
54 A = 6790442
68 meter
Y = 1131978
56 meter E =
0003403
Z = 5265887
64 I = 51
93861
XDOT = -3216
089636 Wp = 348
00259
YDOT = -6873
772858 meter/sec RA = 58
73274 deg
ZDOT = -1045
613430 TA = 111
99848
MA = 111
96232
Ha = 226
721 n
mi
Hp = 222
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13571304
25 X = -4174464
44
Y = 3713840
42 feet Y = 1085509
73 meter
Z = 17276534
26 Z = 5245700
43
XDOT = -10551
475184 XDOT = -3133
907210
YDOT = -22551
748222 feet/sec YDOT = -6909
277854 meter/sec
ZDOT = -3430
490256 ZDOT = -1061
036486
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -366946
68 X = -111845
35
Y = 14169981
26 feet Y = 4319010
29 meter
Z = 17190943
16 Z = 5239799
48
XDOT = -23592
039179 XDOT = -7190
853542
YDOT = 3641
175390 feet/sec YDOT = 1109
830259 meter/sec
ZDOT = -3494
613619 ZDOT = -1065
158231
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 14103
69211542
00016717 00000-0 10270-3 0 9073
2 25544 51
6485 59
1907 0004055 288
9004 71
1707 15
49770414 1328
Satellite: ISS
Catalog Number: 25544
Epoch time: 14103
69211542 = yrday
fracday
Element set: 907
Inclination: 51
6485 deg
RA of node: 59
1907 deg
Eccentricity:
0004055
Arg of perigee: 288
9004 deg
Mean anomaly: 71
1707 deg
Mean motion: 15
49770414 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 132
Checksum: 295
Coasting Arc #9 (Orbit 146)
---------------------------------------
Vector Time (GMT): 2014/104/15:29:37
097
Vector Time (MET): N/A
Weight (LBS) : 903571
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4183817
91 A = 6790626
24 meter
Y = -1207220
98 meter E =
0010034
Z = -5219452
62 I = 51
92341
XDOT = 3570
174148 Wp = 95
24373
YDOT = 6638
775738 meter/sec RA = 53
79864 deg
ZDOT = 1327
589418 TA = 187
47810
MA = 187
49307
Ha = 226
680 n
mi
Hp = 223
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13726436
73 X = 4222361
21
Y = -3960698
76 feet Y = -1160219
90 meter
Z = -17124188
40 Z = -5199034
16
XDOT = 11713
169777 XDOT = 3489
223407
YDOT = 21780
760296 feet/sec YDOT = 6678
247240 meter/sec
ZDOT = 4355
608328 ZDOT = 1344
735748
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -72796
13 X = -22188
26
Y = -14389393
67 feet Y = -4385887
19 meter
Z = -17037607
78 Z = -5193062
85
XDOT = 23080
688327 XDOT = 7034
993802
YDOT = -5353
473961 feet/sec YDOT = -1631
738863 meter/sec
ZDOT = 4427
045430 ZDOT = 1349
363447
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 14104
65937126
00016717 00000-0 10270-3 0 9084
2 25544 51
6495 54
4006 0003990 292
4264 67
6464 15
49786420 1472
Satellite: ISS
Catalog Number: 25544
Epoch time: 14104
65937126 = yrday
fracday
Element set: 908
Inclination: 51
6495 deg
RA of node: 54
4006 deg
Eccentricity:
0003990
Arg of perigee: 292
4264 deg
Mean anomaly: 67
6464 deg
Mean motion: 15
49786420 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 147
Checksum: 320
Coasting Arc #10 (Orbit 162)
---------------------------------------
Vector Time (GMT): 2014/105/15:29:37
097
Vector Time (MET): N/A
Weight (LBS) : 903571
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4247700
18 A = 6790715
32 meter
Y = 1268111
54 meter E =
0004687
Z = 5144981
96 I = 51
90565
XDOT = -3889
484079 Wp = 4
90416
YDOT = -6395
469088 meter/sec RA = 48
86339 deg
ZDOT = -1630
178265 TA = 100
80966
MA = 100
75690
Ha = 226
712 n
mi
Hp = 222
771
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13936024
23 X = -4286557
93
Y = 4160470
92 feet Y = 1220394
23 meter
Z = 16879862
07 Z = 5124252
35
XDOT = -12760
774537 XDOT = -3809
760392
YDOT = -20982
510132 feet/sec YDOT = -6438
518182 meter/sec
ZDOT = -5348
353888 ZDOT = -1648
878955
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 460692
17 X = 140418
97
Y = 14637964
90 feet Y = 4461651
70 meter
Z = 16791955
79 Z = 5118188
12
XDOT = -22459
179323 XDOT = -6845
557858
YDOT = 6949
350737 feet/sec YDOT = 2118
162105 meter/sec
ZDOT = -5426
391149 ZDOT = -1653
964022
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 14105
69108058
00016717 00000-0 10270-3 0 9094
2 25544 51
6497 49
2914 0004124 295
5585 64
5139 15
49858912 1633
Satellite: ISS
Catalog Number: 25544
Epoch time: 14105
69108058 = yrday
fracday
Element set: 909
Inclination: 51
6497 deg
RA of node: 49
2914 deg
Eccentricity:
0004124
Arg of perigee: 295
5585 deg
Mean anomaly: 64
5139 deg
Mean motion: 15
49858912 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 163
Checksum: 331
Coasting Arc #11 (Orbit 174)
---------------------------------------
Vector Time (GMT): 2014/106/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925957
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5631122
99 A = 6797632
88 meter
Y = 2069828
91 meter E =
0003066
Z = -3193297
30 I = 51
90873
XDOT = 567
681024 Wp = 16
67602
YDOT = 5911
340173 meter/sec RA = 44
84085 deg
ZDOT = 4836
676119 TA = 306
66902
MA = 306
69720
Ha = 226
813 n
mi
Hp = 222
816
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18474812
96 X = 5623071
49
Y = 6790777
26 feet Y = 2132754
49 meter
Z = -10476697
17 Z = -3165961
27
XDOT = 1862
470550 XDOT = 478
041409
YDOT = 19394
160672 feet/sec YDOT = 5917
187497 meter/sec
ZDOT = 15868
359970 ZDOT = 4839
215721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19353030
94 X = 5898803
83
Y = 3911001
34 feet Y = 1192073
21 meter
Z = -10361409
92 Z = -3158157
74
XDOT = 4958
283745 XDOT = 1511
284885
YDOT = 17495
241855 feet/sec YDOT = 5332
549717 meter/sec
ZDOT = 15878
101123 ZDOT = 4839
645222
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 14106
46484592
00016717 00000-0 10270-3 0 9102
2 25544 51
6470 45
4583 0004024 298
8099 61
2647 15
49834133 1759
Satellite: ISS
Catalog Number: 25544
Epoch time: 14106
46484592 = yrday
fracday
Element set: 910
Inclination: 51
6470 deg
RA of node: 45
4583 deg
Eccentricity:
0004024
Arg of perigee: 298
8099 deg
Mean anomaly: 61
2647 deg
Mean motion: 15
49834133 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 175
Checksum: 315
Coasting Arc #12 (Orbit 190)
---------------------------------------
Vector Time (GMT): 2014/107/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925957
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5833062
08 A = 6798105
58 meter
Y = -1874617
04 meter E =
0009683
Z = 2937343
27 I = 51
88919
XDOT = -699
852979 Wp = 88
65099
YDOT = -5732
753768 meter/sec RA = 39
90597 deg
ZDOT = -5033
891799 TA = 58
02084
MA = 57
92675
Ha = 226
756 n
mi
Hp = 222
626
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19137342
78 X = -5825935
11
Y = -6150318
36 feet Y = -1939806
08 meter
Z = 9636953
00 Z = 2909023
94
XDOT = -2296
105573 XDOT = -611
242509
YDOT = -18808
247271 feet/sec YDOT = -5740
084787 meter/sec
ZDOT = -16515
393040 ZDOT = -5037
076119
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19957732
58 X = -6083116
89
Y = -2835782
67 feet Y = -864346
56 meter
Z = 9517479
44 Z = 2900927
73
XDOT = -5529
407520 XDOT = -1685
363412
YDOT = -16718
249488 feet/sec YDOT = -5095
722444 meter/sec
ZDOT = -16527
879938 ZDOT = -5037
697805
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 14107
49650616
00016717 00000-0 10270-3 0 9119
2 25544 51
6479 40
3488 0004044 302
2300 57
8458 15
49898488 1915
Satellite: ISS
Catalog Number: 25544
Epoch time: 14107
49650616 = yrday
fracday
Element set: 911
Inclination: 51
6479 deg
RA of node: 40
3488 deg
Eccentricity:
0004044
Arg of perigee: 302
2300 deg
Mean anomaly: 57
8458 deg
Mean motion: 15
49898488 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 191
Checksum: 318
Coasting Arc #13 (Orbit 205)
---------------------------------------
Vector Time (GMT): 2014/108/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925957
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6024033
19 A = 6798640
72 meter
Y = 1645099
14 meter E =
0005360
Z = -2680781
62 I = 51
86667
XDOT = 800
508277 Wp = 6
84833
YDOT = 5554
723116 meter/sec RA = 34
96943 deg
ZDOT = 5213
823864 TA = 323
05133
MA = 323
08823
Ha = 226
844 n
mi
Hp = 222
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19763888
42 X = 6018212
20
Y = 5397306
89 feet Y = 1712431
11 meter
Z = -8795215
29 Z = -2651531
40
XDOT = 2626
339493 XDOT = 713
007087
YDOT = 18224
157204 feet/sec YDOT = 5563
185843 meter/sec
ZDOT = 17105
721340 ZDOT = 5217
499962
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20474815
24 X = 6240723
69
Y = 1637187
20 feet Y = 499014
66 meter
Z = -8671769
03 Z = -2643155
20
XDOT = 5966
676772 XDOT = 1818
643080
YDOT = 15951
937226 feet/sec YDOT = 4862
150466 meter/sec
ZDOT = 17120
308844 ZDOT = 5218
270136
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 14108
46366157
00016717 00000-0 10270-3 0 9122
2 25544 51
6477 35
5585 0004116 305
1758 54
9006 15
49919981 2062
Satellite: ISS
Catalog Number: 25544
Epoch time: 14108
46366157 = yrday
fracday
Element set: 912
Inclination: 51
6477 deg
RA of node: 35
5585 deg
Eccentricity:
0004116
Arg of perigee: 305
1758 deg
Mean anomaly: 54
9006 deg
Mean motion: 15
49919981 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 206
Checksum: 318
Coasting Arc #14 (Orbit 221)
---------------------------------------
Vector Time (GMT): 2014/109/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925957
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6202896
99 A = 6799106
70 meter
Y = -1425219
63 meter E =
0010092
Z = 2380705
55 I = 51
84366
XDOT = -840
319532 Wp = 98
05116
YDOT = -5378
147092 meter/sec RA = 30
03129 deg
ZDOT = -5390
918107 TA = 55
49015
MA = 55
39490
Ha = 226
786 n
mi
Hp = 222
407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20350711
91 X = -6198063
71
Y = -4675917
42 feet Y = -1494557
33 meter
Z = 7810713
76 Z = 2350584
10
XDOT = -2756
953846 XDOT = -753
929705
YDOT = -17644
839540 feet/sec YDOT = -5387
061166 meter/sec
ZDOT = -17686
739197 ZDOT = -5394
790366
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20923036
25 X = -6377341
45
Y = -461077
21 feet Y = -140536
33 meter
Z = 7683546
73 Z = 2341945
04
XDOT = -6187
544418 XDOT = -1885
963539
YDOT = -15223
118737 feet/sec YDOT = -4640
006591 meter/sec
ZDOT = -17702
179107 ZDOT = -5395
624192
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 14109
49526683
00016717 00000-0 10270-3 0 9139
2 25544 51
6485 30
4485 0004084 308
6358 51
4426 15
49978863 2222
Satellite: ISS
Catalog Number: 25544
Epoch time: 14109
49526683 = yrday
fracday
Element set: 913
Inclination: 51
6485 deg
RA of node: 30
4485 deg
Eccentricity:
0004084
Arg of perigee: 308
6358 deg
Mean anomaly: 51
4426 deg
Mean motion: 15
49978863 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 222
Checksum: 325
Coasting Arc #15 (Orbit 236)
---------------------------------------
Vector Time (GMT): 2014/110/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925957
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6361390
12 A = 6799580
42 meter
Y = 1171034
67 meter E =
0007869
Z = -2081682
52 I = 51
81780
XDOT = 851
760619 Wp = 8
18319
YDOT = 5215
762389 meter/sec RA = 25
09112 deg
ZDOT = 5547
137777 TA = 328
87846
MA = 328
92504
Ha = 226
881 n
mi
Hp = 222
328
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20870702
49 X = 6357934
79
Y = 3841977
27 feet Y = 1242152
46 meter
Z = -6829667
07 Z = -2050787
89
XDOT = 2794
490219 XDOT = 766
426999
YDOT = 17112
081330 feet/sec YDOT = 5224
810292 meter/sec
ZDOT = 18199
270922 ZDOT = 5551
068189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21246922
94 X = 6476062
11
Y = -824940
00 feet Y = -251441
71 meter
Z = -6699186
79 Z = -2041912
13
XDOT = 6297
951351 XDOT = 1919
615572
YDOT = 14563
841913 feet/sec YDOT = 4439
059015 meter/sec
ZDOT = 18214
979688 ZDOT = 5551
925809
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 14110
46237077
00016717 00000-0 10270-3 0 9145
2 25544 51
6481 25
6577 0004174 311
4849 48
5943 15
50005000 2376
Satellite: ISS
Catalog Number: 25544
Epoch time: 14110
46237077 = yrday
fracday
Element set: 914
Inclination: 51
6481 deg
RA of node: 25
6577 deg
Eccentricity:
0004174
Arg of perigee: 311
4849 deg
Mean anomaly: 48
5943 deg
Mean motion: 15
50005000 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 237
Checksum: 285
Coasting Arc #16 (Orbit 252)
---------------------------------------
Vector Time (GMT): 2014/111/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925957
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6503941
27 A = 6799984
43 meter
Y = -929781
20 meter E =
0010107
Z = 1737292
87 I = 51
79189
XDOT = -802
337215 Wp = 107
68032
YDOT = -5065
775852 meter/sec RA = 20
14924 deg
ZDOT = -5690
599147 TA = 53
33372
MA = 53
24087
Ha = 226
827 n
mi
Hp = 222
170
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21338390
01 X = -6501500
12
Y = -3050463
24 feet Y = -1002498
75 meter
Z = 5699779
76 Z = 1705703
39
XDOT = -2632
339944 XDOT = -717
987657
YDOT = -16619
999513 feet/sec YDOT = -5074
276612 meter/sec
ZDOT = -18669
944708 ZDOT = -5694
291811
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21490917
55 X = -6550431
67
Y = 2067909
63 feet Y = 630298
85 meter
Z = 5566319
77 Z = 1696614
26
XDOT = -6207
235293 XDOT = -1891
965317
YDOT = -13994
957840 feet/sec YDOT = -4265
663150 meter/sec
ZDOT = -18684
670890 ZDOT = -5695
087687
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 14111
49392149
00016717 00000-0 10270-3 0 9152
2 25544 51
6488 20
5470 0004111 314
8600 45
2216 15
50054435 2533
Satellite: ISS
Catalog Number: 25544
Epoch time: 14111
49392149 = yrday
fracday
Element set: 915
Inclination: 51
6488 deg
RA of node: 20
5470 deg
Eccentricity:
0004111
Arg of perigee: 314
8600 deg
Mean anomaly: 45
2216 deg
Mean motion: 15
50054435 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 253
Checksum: 269
Coasting Arc #17 (Orbit 267)
---------------------------------------
Vector Time (GMT): 2014/112/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 925957
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6616421
31 A = 6800320
27 meter
Y = 657786
51 meter E =
0010322
Z = -1396766
51 I = 51
76383
XDOT = 731
220913 Wp = 13
57907
YDOT = 4942
751031 meter/sec RA = 15
20521 deg
ZDOT = 5809
967648 TA = 331
24796
MA = 331
30482
Ha = 226
917 n
mi
Hp = 222
038
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21707419
01 X = 6615359
12
Y = 2158092
23 feet Y = 731769
59 meter
Z = -4582567
30 Z = -1364627
35
XDOT = 2399
018743 XDOT = 647
672535
YDOT = 16216
374773 feet/sec YDOT = 4950
461091 meter/sec
ZDOT = 19061
573648 ZDOT = 5813
316705
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21577538
38 X = 6576833
70
Y = -3392003
77 feet Y = -1033882
75 meter
Z = -4446737
38 Z = -1355365
55
XDOT = 6047
516790 XDOT = 1843
283118
YDOT = 13545
860710 feet/sec YDOT = 4128
778344 meter/sec
ZDOT = 19074
866494 ZDOT = 5814
019307
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 14112
46097449
00016717 00000-0 10270-3 0 9166
2 25544 51
6487 15
7556 0004220 317
8982 42
1844 15
50088959 2687
Satellite: ISS
Catalog Number: 25544
Epoch time: 14112
46097449 = yrday
fracday
Element set: 916
Inclination: 51
6487 deg
RA of node: 15
7556 deg
Eccentricity:
0004220
Arg of perigee: 317
8982 deg
Mean anomaly: 42
1844 deg
Mean motion: 15
50088959 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 268
Checksum: 327
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