[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 29th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19375 04 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 120 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 031 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
There are no maneuvers
Coasting Arc #1 (Orbit 2952)
---------------------------------------
Vector Time (GMT): 2014/027/16:06:44
022
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3281946
33 A = 6799523
70 meter
Y = -5491059
56 meter E =
0016954
Z = 2284664
38 I = 52
00632
XDOT = 3294
167868 Wp = 100
12675
YDOT = -4253
146055 meter/sec RA = 75
33217 deg
ZDOT = -5458
618149 TA = 54
61000
MA = 54
45173
Ha = 229
046 n
mi
Hp = 220
057
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10767540
45 X = -3231398
17
Y = -18015287
26 feet Y = -5527477
84 meter
Z = 7495618
05 Z = 2268843
91
XDOT = 10807
637362 XDOT = 3367
998527
YDOT = -13953
891258 feet/sec YDOT = -4215
895529 meter/sec
ZDOT = -17908
852196 ZDOT = -5442
436607
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13135896
45 X = -4003821
24
Y = -16398843
71 feet Y = -4998367
56 meter
Z = 7429733
63 Z = 2264582
81
XDOT = 7749
991141 XDOT = 2362
197300
YDOT = -14337
724489 feet/sec YDOT = -4370
138424 meter/sec
ZDOT = -17839
838855 ZDOT = -5437
582883
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 14027
70814029
00016717 00000-0 10270-3 0 9002
2 25544 51
6462 75
9225 0003768 70
3781 289
7776 15
49888301 29538
Satellite: ISS
Catalog Number: 25544
Epoch time: 14027
70814029 = yrday
fracday
Element set: 900
Inclination: 51
6462 deg
RA of node: 75
9225 deg
Eccentricity:
0003768
Arg of perigee: 70
3781 deg
Mean anomaly: 289
7776 deg
Mean motion: 15
49888301 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2953
Checksum: 334
Coasting Arc #2 (Orbit 2967)
---------------------------------------
Vector Time (GMT): 2014/028/16:06:44
022
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3606404
47 A = 6799971
07 meter
Y = 5391861
08 meter E =
0010133
Z = -2034076
09 I = 51
99879
XDOT = -3138
023819 Wp = 53
01157
YDOT = 4196
355512 meter/sec RA = 70
40484 deg
ZDOT = 5584
944781 TA = 284
67298
MA = 284
78528
Ha = 229
111 n
mi
Hp = 219
985
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11832035
67 X = 3555724
15
Y = 17689832
93 feet Y = 5431906
91 meter
Z = -6673478
00 Z = -2016679
90
XDOT = -10295
353738 XDOT = -3211
844539
YDOT = 13767
570578 feet/sec YDOT = 4160
851152 meter/sec
ZDOT = 18323
309650 ZDOT = 5569
521850
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14413929
27 X = 4393365
64
Y = 15688498
01 feet Y = 4781854
19 meter
Z = -6600927
12 Z = -2011962
59
XDOT = -7061
750631 XDOT = -2152
421592
YDOT = 14134
866398 feet/sec YDOT = 4308
307278 meter/sec
ZDOT = 18257
499297 ZDOT = 5564
885786
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 14028
67531875
00016717 00000-0 10270-3 0 9015
2 25544 51
6458 71
1328 0003894 75
6953 284
4630 15
49887987 29680
Satellite: ISS
Catalog Number: 25544
Epoch time: 14028
67531875 = yrday
fracday
Element set: 901
Inclination: 51
6458 deg
RA of node: 71
1328 deg
Eccentricity:
0003894
Arg of perigee: 75
6953 deg
Mean anomaly: 284
4630 deg
Mean motion: 15
49887987 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2968
Checksum: 359
Coasting Arc #3 (Orbit 2983)
---------------------------------------
Vector Time (GMT): 2014/029/16:06:44
022
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3893921
05 A = 6800380
53 meter
Y = -5294120
68 meter E =
0016996
Z = 1721072
66 I = 51
98931
XDOT = 3036
757632 Wp = 107
34597
YDOT = -4104
936813 meter/sec RA = 65
47582 deg
ZDOT = -5714
874652 TA = 53
89804
MA = 53
74080
Ha = 229
019 n
mi
Hp = 219
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12775331
53 X = -3842791
83
Y = -17369162
32 feet Y = -5337379
15 meter
Z = 5646563
85 Z = 1702281
05
XDOT = 9963
115592 XDOT = 3110
194622
YDOT = -13467
640461 feet/sec YDOT = -4070
567102 meter/sec
ZDOT = -18749
588753 ZDOT = -5699
944589
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15551194
80 X = -4740004
18
Y = -14964528
67 feet Y = -4561188
34 meter
Z = 5568105
65 Z = 1697158
60
XDOT = 6577
733547 XDOT = 2004
893185
YDOT = -13839
746407 feet/sec YDOT = -4218
354705 meter/sec
ZDOT = -18685
868094 ZDOT = -5695
452595
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 14029
70696153
00016717 00000-0 10270-3 0 9022
2 25544 51
6460 66
0219 0003789 76
1972 283
9600 15
49919596 29846
Satellite: ISS
Catalog Number: 25544
Epoch time: 14029
70696153 = yrday
fracday
Element set: 902
Inclination: 51
6460 deg
RA of node: 66
0219 deg
Eccentricity:
0003789
Arg of perigee: 76
1972 deg
Mean anomaly: 283
9600 deg
Mean motion: 15
49919596 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2984
Checksum: 342
Coasting Arc #4 (Orbit 2998)
---------------------------------------
Vector Time (GMT): 2014/030/16:06:44
022
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4202930
03 A = 6800700
52 meter
Y = 5142983
82 meter E =
0011640
Z = -1446214
14 I = 51
97647
XDOT = -2943
504968 Wp = 50
79503
YDOT = 4028
816852 meter/sec RA = 60
54679 deg
ZDOT = 5811
261548 TA = 293
53609
MA = 293
65833
Ha = 229
054 n
mi
Hp = 219
887
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13789140
51 X = 4152132
72
Y = 16873306
49 feet Y = 5189699
64 meter
Z = -4744797
06 Z = -1425920
83
XDOT = -9657
168529 XDOT = -3016
565819
YDOT = 13217
903059 feet/sec YDOT = 3995
492197 meter/sec
ZDOT = 19065
818726 ZDOT = 5796
785339
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16705163
35 X = 5091733
79
Y = 14020846
40 feet Y = 4273553
98 meter
Z = -4659973
22 Z = -1420359
84
XDOT = -6135
409622 XDOT = -1870
072853
YDOT = 13583
594698 feet/sec YDOT = 4140
279664 meter/sec
ZDOT = 19004
023335 ZDOT = 5792
426313
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 14030
67411446
00016717 00000-0 10270-3 0 9031
2 25544 51
6456 61
2316 0003883 81
3116 278
8474 15
49931532 29991
Satellite: ISS
Catalog Number: 25544
Epoch time: 14030
67411446 = yrday
fracday
Element set: 903
Inclination: 51
6456 deg
RA of node: 61
2316 deg
Eccentricity:
0003883
Arg of perigee: 81
3116 deg
Mean anomaly: 278
8474 deg
Mean motion: 15
49931532 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2999
Checksum: 316
Coasting Arc #5 (Orbit 3014)
---------------------------------------
Vector Time (GMT): 2014/031/16:06:44
022
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4469334
92 A = 6801012
66 meter
Y = -4995902
66 meter E =
0016652
Z = 1108277
44 I = 51
96228
XDOT = 2909
334104 Wp = 114
42991
YDOT = -3926
166901 meter/sec RA = 55
61610 deg
ZDOT = -5903
059431 TA = 53
61718
MA = 53
46368
Ha = 228
979 n
mi
Hp = 219
892
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14663172
30 X = -4418520
96
Y = -16390756
76 feet Y = -5045597
47 meter
Z = 3636080
85 Z = 1086690
19
XDOT = 9545
059397 XDOT = 2981
695553
YDOT = -12881
125004 feet/sec YDOT = -3893
228438 meter/sec
ZDOT = -19366
992883 ZDOT = -5888
750807
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17695539
12 X = -5393600
32
Y = -13083654
69 feet Y = -3987897
95 meter
Z = 3545770
45 Z = 1080750
83
XDOT = 5908
207207 XDOT = 1800
821557
YDOT = -13280
223538 feet/sec YDOT = -4047
812134 meter/sec
ZDOT = -19305
920681 ZDOT = -5884
444624
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 14031
70573041
00016717 00000-0 10270-3 0 9047
2 25544 51
6462 56
1205 0003797 82
7060 277
4522 15
49950152 30153
Satellite: ISS
Catalog Number: 25544
Epoch time: 14031
70573041 = yrday
fracday
Element set: 904
Inclination: 51
6462 deg
RA of node: 56
1205 deg
Eccentricity:
0003797
Arg of perigee: 82
7060 deg
Mean anomaly: 277
4522 deg
Mean motion: 15
49950152 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3015
Checksum: 284
Coasting Arc #6 (Orbit 3029)
---------------------------------------
Vector Time (GMT): 2014/032/16:06:44
022
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4747968
08 A = 6801171
78 meter
Y = 4795212
91 meter E =
0013212
Z = -811402
76 I = 51
94472
XDOT = -2881
437192 Wp = 51
77611
YDOT = 3849
637710 meter/sec RA = 50
68487 deg
ZDOT = 5963
364987 TA = 299
50358
MA = 299
63528
Ha = 228
971 n
mi
Hp = 219
817
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15577323
09 X = 4697935
49
Y = 15732325
82 feet Y = 4848027
93 meter
Z = -2662082
55 Z = -788460
13
XDOT = -9453
534094 XDOT = -2953
237960
YDOT = 12630
044981 feet/sec YDOT = 3817
014480 meter/sec
ZDOT = 19564
845757 ZDOT = 5949
193119
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18659846
88 X = 5687521
33
Y = 11936138
85 feet Y = 3638135
12 meter
Z = -2566019
75 Z = -782122
82
XDOT = -5707
114491 XDOT = -1739
528497
YDOT = 13061
045919 feet/sec YDOT = 3981
006796 meter/sec
ZDOT = 19504
363396 ZDOT = 5944
929963
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 14032
67285738
00016717 00000-0 10270-3 0 9058
2 25544 51
6461 51
3298 0003825 86
9319 273
2269 15
49973649 30301
Satellite: ISS
Catalog Number: 25544
Epoch time: 14032
67285738 = yrday
fracday
Element set: 905
Inclination: 51
6461 deg
RA of node: 51
3298 deg
Eccentricity:
0003825
Arg of perigee: 86
9319 deg
Mean anomaly: 273
2269 deg
Mean motion: 15
49973649 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3030
Checksum: 333
Coasting Arc #7 (Orbit 3045)
---------------------------------------
Vector Time (GMT): 2014/033/16:06:44
022
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4978019
76 A = 6801328
32 meter
Y = -4602921
79 meter E =
0015860
Z = 452088
26 I = 51
92619
XDOT = 2913
699671 Wp = 121
03399
YDOT = -3755
940617 meter/sec RA = 45
75219 deg
ZDOT = -6009
892717 TA = 54
11781
MA = 53
97066
Ha = 228
915 n
mi
Hp = 219
826
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16332085
84 X = -4928374
94
Y = -15101449
44 feet Y = -4658311
58 meter
Z = 1483229
19 Z = 428027
10
XDOT = 9559
382123 XDOT = 2984
676427
YDOT = -12322
639820 feet/sec YDOT = -3722
961293 meter/sec
ZDOT = -19717
495792 ZDOT = -5995
566029
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19440053
87 X = -5925328
42
Y = -10824231
95 feet Y = -3299225
90 meter
Z = 1382418
25 Z = 421361
08
XDOT = 5715
396248 XDOT = 1742
052776
YDOT = -12841
599387 feet/sec YDOT = -3914
119493 meter/sec
ZDOT = -19656
375326 ZDOT = -5991
263199
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 14033
70444609
00016717 00000-0 10270-3 0 9068
2 25544 51
6472 46
2188 0003788 89
4916 270
6669 15
49984541 30468
Satellite: ISS
Catalog Number: 25544
Epoch time: 14033
70444609 = yrday
fracday
Element set: 906
Inclination: 51
6472 deg
RA of node: 46
2188 deg
Eccentricity:
0003788
Arg of perigee: 89
4916 deg
Mean anomaly: 270
6669 deg
Mean motion: 15
49984541 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3046
Checksum: 340
Coasting Arc #8 (Orbit 3060)
---------------------------------------
Vector Time (GMT): 2014/034/16:06:44
022
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5211359
46 A = 6801313
77 meter
Y = 4359660
74 meter E =
0014665
Z = -136681
70 I = 51
90419
XDOT = -2947
927586 Wp = 55
39727
YDOT = 3698
156879 meter/sec RA = 40
81845 deg
ZDOT = 6027
768815 TA = 303
13828
MA = 303
27892
Ha = 228
882 n
mi
Hp = 219
761
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17097636
01 X = 5162885
38
Y = 14303348
89 feet Y = 4417666
45 meter
Z = -448430
79 Z = -111484
09
XDOT = -9671
678432 XDOT = -3018
342597
YDOT = 12133
060628 feet/sec YDOT = 3664
797949 meter/sec
ZDOT = 19776
144406 ZDOT = 6013
277160
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20156459
61 X = 6143688
89
Y = 9524477
31 feet Y = 2903060
69 meter
Z = -342789
39 Z = -104482
21
XDOT = -5720
797399 XDOT = -1743
699047
YDOT = 12744
134194 feet/sec YDOT = 3884
412102 meter/sec
ZDOT = 19714
336631 ZDOT = 6008
929805
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 14034
67154696
00016717 00000-0 10270-3 0 9070
2 25544 51
6472 41
4282 0003769 92
7605 267
3977 15
50012518 30611
Satellite: ISS
Catalog Number: 25544
Epoch time: 14034
67154696 = yrday
fracday
Element set: 907
Inclination: 51
6472 deg
RA of node: 41
4282 deg
Eccentricity:
0003769
Arg of perigee: 92
7605 deg
Mean anomaly: 267
3977 deg
Mean motion: 15
50012518 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3061
Checksum: 315
Coasting Arc #9 (Orbit 3076)
---------------------------------------
Vector Time (GMT): 2014/035/16:06:44
022
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5390434
29 A = 6801252
92 meter
Y = -4131251
92 meter E =
0014603
Z = -239196
70 I = 51
88136
XDOT = 3039
767733 Wp = 126
64235
YDOT = -3632
828724 meter/sec RA = 35
88316 deg
ZDOT = -6022
081731 TA = 55
92191
MA = 55
78339
Ha = 228
830 n
mi
Hp = 219
765
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17685151
87 X = -5342675
15
Y = -13553976
10 feet Y = -4191264
18 meter
Z = -784766
08 Z = -265266
08
XDOT = 9972
991251 XDOT = 3109
417865
YDOT = -11918
729409 feet/sec YDOT = -3598
447011 meter/sec
ZDOT = -19757
485995 ZDOT = -6007
145781
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20674193
74 X = -6301494
25
Y = -8298734
25 feet Y = -2529454
20 meter
Z = -894117
20 Z = -272526
92
XDOT = 5912
476718 XDOT = 1802
122904
YDOT = -12689
215374 feet/sec YDOT = -3867
672846 meter/sec
ZDOT = -19693
812428 ZDOT = -6002
674028
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 14035
70310782
00016717 00000-0 10270-3 0 9086
2 25544 51
6485 36
3175 0003777 96
3147 263
8433 15
50024523 30773
Satellite: ISS
Catalog Number: 25544
Epoch time: 14035
70310782 = yrday
fracday
Element set: 908
Inclination: 51
6485 deg
RA of node: 36
3175 deg
Eccentricity:
0003777
Arg of perigee: 96
3147 deg
Mean anomaly: 263
8433 deg
Mean motion: 15
50024523 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3077
Checksum: 303
Coasting Arc #10 (Orbit 3092)
---------------------------------------
Vector Time (GMT): 2014/036/16:06:44
022
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5564997
94 A = 6801057
33 meter
Y = 3857201
24 meter E =
0015843
Z = 568430
12 I = 51
85516
XDOT = -3127
151583 Wp = 61
16174
YDOT = 3611
281892 meter/sec RA = 30
94620 deg
ZDOT = 5991
231698 TA = 304
94442
MA = 305
09314
Ha = 228
795 n
mi
Hp = 219
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18257867
26 X = 5518691
03
Y = 12654859
71 feet Y = 3919173
72 meter
Z = 1864928
21 Z = 595351
12
XDOT = -10259
683670 XDOT = -3196
404466
YDOT = 11848
037704 feet/sec YDOT = 3575
925143 meter/sec
ZDOT = 19656
271976 ZDOT = 5975
872241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21099591
47 X = 6431155
48
Y = 6918688
51 feet Y = 2108816
26 meter
Z = 1977912
40 Z = 602867
70
XDOT = -6062
278866 XDOT = -1847
782598
YDOT = 12782
125518 feet/sec YDOT = 3895
991858 meter/sec
ZDOT = 19590
812593 ZDOT = 5971
279678
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 14036
73465367
00016717 00000-0 10270-3 0 9091
2 25544 51
6483 31
2074 0003749 99
1989 260
9586 15
50050915 30936
Satellite: ISS
Catalog Number: 25544
Epoch time: 14036
73465367 = yrday
fracday
Element set: 909
Inclination: 51
6483 deg
RA of node: 31
2074 deg
Eccentricity:
0003749
Arg of perigee: 99
1989 deg
Mean anomaly: 260
9586 deg
Mean motion: 15
50050915 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3093
Checksum: 331
Coasting Arc #11 (Orbit 3107)
---------------------------------------
Vector Time (GMT): 2014/037/16:06:44
022
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5680708
71 A = 6800743
57 meter
Y = -3606654
74 meter E =
0012930
Z = -954729
62 I = 51
82832
XDOT = 3265
721456 Wp = 130
45909
YDOT = -3590
916043 meter/sec RA = 26
00725 deg
ZDOT = -5926
894186 TA = 59
83424
MA = 59
70621
Ha = 228
730 n
mi
Hp = 219
709
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18637495
77 X = -5635318
37
Y = -11832856
77 feet Y = -3669926
30 meter
Z = -3132315
04 Z = -982215
02
XDOT = 10714
309240 XDOT = 3334
423780
YDOT = -11781
220615 feet/sec YDOT = -3554
012716 meter/sec
ZDOT = -19445
190899 ZDOT = -5910
862968
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21321649
53 X = -6498838
78
Y = -5658952
19 feet Y = -1724848
63 meter
Z = -3247717
17 Z = -989904
19
XDOT = 6359
156153 XDOT = 1938
270795
YDOT = -12949
938515 feet/sec YDOT = -3947
141259 meter/sec
ZDOT = -19376
897481 ZDOT = -5906
078352
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 14037
70171437
00016717 00000-0 10270-3 0 9103
2 25544 51
6493 26
4161 0003768 103
2456 256
9115 15
50067381 31082
Satellite: ISS
Catalog Number: 25544
Epoch time: 14037
70171437 = yrday
fracday
Element set: 910
Inclination: 51
6493 deg
RA of node: 26
4161 deg
Eccentricity:
0003768
Arg of perigee: 103
2456 deg
Mean anomaly: 256
9115 deg
Mean motion: 15
50067381 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3108
Checksum: 289
Coasting Arc #12 (Orbit 3123)
---------------------------------------
Vector Time (GMT): 2014/038/16:06:44
022
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5785970
50 A = 6800352
30 meter
Y = 3318073
12 meter E =
0016605
Z = 1291772
37 I = 51
79866
XDOT = -3391
998273 Wp = 68
62101
YDOT = 3619
551522 meter/sec RA = 21
06614 deg
ZDOT = 5841
312704 TA = 305
38105
MA = 305
53608
Ha = 228
700 n
mi
Hp = 219
659
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18982842
83 X = 5742162
10
Y = 10886066
68 feet Y = 3382530
63 meter
Z = 4238098
34 Z = 1319772
96
XDOT = -11128
603259 XDOT = -3460
595660
YDOT = 11875
169034 feet/sec YDOT = 3581
236609 meter/sec
ZDOT = 19164
411758 ZDOT = 5824
668371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21435314
23 X = 6533483
78
Y = 4286170
96 feet Y = 1306424
91 meter
Z = 4355719
22 Z = 1327623
22
XDOT = -6569
938669 XDOT = -2002
517306
YDOT = 13276
345932 feet/sec YDOT = 4046
630240 meter/sec
ZDOT = 19093
523765 ZDOT = 5819
706044
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 14038
73323140
00016717 00000-0 10270-3 0 9118
2 25544 51
6489 21
3057 0003759 105
7663 254
3903 15
50090789 31245
Satellite: ISS
Catalog Number: 25544
Epoch time: 14038
73323140 = yrday
fracday
Element set: 911
Inclination: 51
6489 deg
RA of node: 21
3057 deg
Eccentricity:
0003759
Arg of perigee: 105
7663 deg
Mean anomaly: 254
3903 deg
Mean motion: 15
50090789 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3124
Checksum: 297
Coasting Arc #13 (Orbit 3138)
---------------------------------------
Vector Time (GMT): 2014/039/16:06:44
022
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5829874
73 A = 6799788
44 meter
Y = -3063542
10 meter E =
0010984
Z = -1680775
00 I = 51
76863
XDOT = 3559
159924 Wp = 131
11374
YDOT = -3655
997492 meter/sec RA = 16
12263 deg
ZDOT = -5712
757375 TA = 67
23536
MA = 67
11934
Ha = 228
616 n
mi
Hp = 219
673
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19126885
61 X = -5787019
69
Y = -10050991
15 feet Y = -3128495
90 meter
Z = -5514353
66 Z = -1708991
13
XDOT = 11677
033873 XDOT = 3627
527896
YDOT = -11994
742429 feet/sec YDOT = -3615
814520 meter/sec
ZDOT = -18742
642306 ZDOT = -5695
301623
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21354732
93 X = -6508922
60
Y = -3084447
62 feet Y = -940139
63 meter
Z = -5632924
38 Z = -1716915
35
XDOT = 6875
634754 XDOT = 2095
693473
YDOT = -13693
672239 feet/sec YDOT = -4173
831298 meter/sec
ZDOT = -18668
322007 ZDOT = -5690
104548
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 14039
70026416
00016717 00000-0 10270-3 0 9123
2 25544 51
6497 16
5142 0003745 110
5239 249
6314 15
50109712 31399
Satellite: ISS
Catalog Number: 25544
Epoch time: 14039
70026416 = yrday
fracday
Element set: 912
Inclination: 51
6497 deg
RA of node: 16
5142 deg
Eccentricity:
0003745
Arg of perigee: 110
5239 deg
Mean anomaly: 249
6314 deg
Mean motion: 15
50109712 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3139
Checksum: 286
Coasting Arc #14 (Orbit 3154)
---------------------------------------
Vector Time (GMT): 2014/040/16:06:44
022
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5859803
28 A = 6799189
11 meter
Y = 2780268
90 meter E =
0016831
Z = 2018105
98 I = 51
73660
XDOT = -3705
696625 Wp = 77
39629
YDOT = 3743
508356 meter/sec RA = 11
17660 deg
ZDOT = 5567
024061 TA = 304
83775
MA = 304
99594
Ha = 228
581 n
mi
Hp = 219
629
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19225076
38 X = 5818475
05
Y = 9121617
14 feet Y = 2845565
93 meter
Z = 6621082
63 Z = 2046471
14
XDOT = -12157
797327 XDOT = -3774
324282
YDOT = 12281
851563 feet/sec YDOT = 3701
685264 meter/sec
ZDOT = 18264
514637 ZDOT = 5548
855884
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21164170
58 X = 6450839
19
Y = 1814400
00 feet Y = 553029
12 meter
Z = 6740328
84 Z = 2054452
23
XDOT = -7051
598531 XDOT = -2149
327232
YDOT = 14263
855590 feet/sec YDOT = 4347
623184 meter/sec
ZDOT = 18187
172121 ZDOT = 5543
450062
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 14040
73175145
00016717 00000-0 10270-3 0 9133
2 25544 51
6494 11
4033 0003759 112
5919 247
5630 15
50134125 31553
Satellite: ISS
Catalog Number: 25544
Epoch time: 14040
73175145 = yrday
fracday
Element set: 913
Inclination: 51
6494 deg
RA of node: 11
4033 deg
Eccentricity:
0003759
Arg of perigee: 112
5919 deg
Mean anomaly: 247
5630 deg
Mean motion: 15
50134125 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3155
Checksum: 280
Coasting Arc #15 (Orbit 3169)
---------------------------------------
Vector Time (GMT): 2014/041/16:06:44
022
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5828985
16 A = 6798404
73 meter
Y = -2542760
26 meter E =
0009098
Z = -2400359
99 I = 51
70442
XDOT = 3879
399564 Wp = 126
19037
YDOT = -3842
143235 meter/sec RA = 6
22805 deg
ZDOT = -5370
037574 TA = 80
54997
MA = 80
44714
Ha = 228
477 n
mi
Hp = 219
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19123967
08 X = -5788458
29
Y = -8342389
31 feet Y = -2607717
16 meter
Z = -7875196
82 Z = -2428577
29
XDOT = 12727
688858 XDOT = 3948
160319
YDOT = -12605
456809 feet/sec YDOT = -3798
376969 meter/sec
ZDOT = -17618
233509 ZDOT = -5351
025290
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20805118
86 X = -6341400
23
Y = -765218
55 feet Y = -233238
62 meter
Z = -7993858
32 Z = -2436528
02
XDOT = 7262
872853 XDOT = 2213
723646
YDOT = -14919
820442 feet/sec YDOT = -4547
561271 meter/sec
ZDOT = -17537
312502 ZDOT = -5345
372851
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 14041
69875569
00016717 00000-0 10270-3 0 9147
2 25544 51
6502 6
6116 0003682 118
2101 241
9422 15
50151854 31704
Satellite: ISS
Catalog Number: 25544
Epoch time: 14041
69875569 = yrday
fracday
Element set: 914
Inclination: 51
6502 deg
RA of node: 6
6116 deg
Eccentricity:
0003682
Arg of perigee: 118
2101 deg
Mean anomaly: 241
9422 deg
Mean motion: 15
50151854 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3170
Checksum: 285
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