[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 29th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21258 72 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 2980)
---------------------------------------
Vector Time (GMT): 2014/029/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4397642
36 A = 6790491
29 meter
Y = -79797
91 meter E =
0017160
Z = -5188654
09 I = 51
96055
XDOT = 1899
297973 Wp = 96
79926
YDOT = 7255
467582 meter/sec RA = 66
32522 deg
ZDOT = 1500
448136 TA = 187
61091
MA = 187
63699
Ha = 229
029 n
mi
Hp = 220
132
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14427960
49 X = 4423412
07
Y = -261804
15 feet Y = -30476
43 meter
Z = -17023143
34 Z = -5167228
86
XDOT = 6231
292561 XDOT = 1810
736027
YDOT = 23804
027499 feet/sec YDOT = 7276
211526 meter/sec
ZDOT = 4922
730104 ZDOT = 1509
459539
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9123544
66 X = 2780856
41
Y = 11316694
97 feet Y = 3449328
63 meter
Z = -16932670
85 Z = -5161078
07
XDOT = -14170
658517 XDOT = -4319
216716
YDOT = 18833
934360 feet/sec YDOT = 5740
583193 meter/sec
ZDOT = 4959
568733 ZDOT = 1511
676550
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
51352827
00016717 00000-0 10270-3 0 9006
2 25544 51
6484 66
9816 0003704 80
2402 279
9167 15
49887016 29816
Satellite: ISS
Catalog Number: 25544
Epoch time: 14029
51352827 = yrday
fracday
Element set: 900
Inclination: 51
6484 deg
RA of node: 66
9816 deg
Eccentricity:
0003704
Arg of perigee: 80
2402 deg
Mean anomaly: 279
9167 deg
Mean motion: 15
49887016 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2981
Checksum: 326
Coasting Arc #2 (Orbit 2996)
---------------------------------------
Vector Time (GMT): 2014/030/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4491736
69 A = 6790693
87 meter
Y = 79101
35 meter E =
0009122
Z = 5086065
28 I = 51
94728
XDOT = -2224
711622 Wp = 66
86778
YDOT = -7100
268114 meter/sec RA = 61
39112 deg
ZDOT = -1848
200750 TA = 40
99317
MA = 40
92464
Ha = 229
131 n
mi
Hp = 219
856
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14736668
94 X = -4516993
21
Y = 259518
86 feet Y = 28730
64 meter
Z = 16686565
87 Z = 5064184
28
XDOT = -7298
922643 XDOT = -2136
171764
YDOT = -23294
842893 feet/sec YDOT = -7124
651199 meter/sec
ZDOT = -6063
650753 ZDOT = -1858
792776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9507272
09 X = -2897816
53
Y = -11398406
47 feet Y = -3474234
29 meter
Z = 16594166
13 Z = 5057901
84
XDOT = 12765
602300 XDOT = 3890
955581
YDOT = -19568
048596 feet/sec YDOT = -5964
341212 meter/sec
ZDOT = -6107
186630 ZDOT = -1861
470485
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
54515810
00016717 00000-0 10270-3 0 9015
2 25544 51
6471 61
8714 0003833 83
8821 276
2766 15
49947400 29976
Satellite: ISS
Catalog Number: 25544
Epoch time: 14030
54515810 = yrday
fracday
Element set: 901
Inclination: 51
6471 deg
RA of node: 61
8714 deg
Eccentricity:
0003833
Arg of perigee: 83
8821 deg
Mean anomaly: 276
2766 deg
Mean motion: 15
49947400 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2997
Checksum: 315
Coasting Arc #3 (Orbit 3011)
---------------------------------------
Vector Time (GMT): 2014/031/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4617921
17 A = 6791195
24 meter
Y = -110727
62 meter E =
0015955
Z = -4992787
00 I = 51
93413
XDOT = 2517
996531 Wp = 101
20574
YDOT = 6886
272953 meter/sec RA = 56
45598 deg
ZDOT = 2179
110600 TA = 189
99200
MA = 190
02376
Ha = 228
999 n
mi
Hp = 220
016
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15150660
00 X = 4643068
84
Y = -363279
58 feet Y = -58946
58 meter
Z = -16380534
78 Z = -4970293
31
XDOT = 8261
143475 XDOT = 2430
220412
YDOT = 22592
759031 feet/sec YDOT = 6913
940067 meter/sec
ZDOT = 7149
312993 ZDOT = 2191
128983
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10045443
30 X = 3061851
12
Y = 11483317
48 feet Y = 3500115
17 meter
Z = -16285542
01 Z = -4963833
20
XDOT = -11257
925942 XDOT = -3431
415827
YDOT = 20044
176749 feet/sec YDOT = 6109
465073 meter/sec
ZDOT = 7198
905048 ZDOT = 2194
226259
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
51229825
00016717 00000-0 10270-3 0 9022
2 25544 51
6481 57
0804 0003784 86
3017 273
8566 15
49932253 30124
Satellite: ISS
Catalog Number: 25544
Epoch time: 14031
51229825 = yrday
fracday
Element set: 902
Inclination: 51
6481 deg
RA of node: 57
0804 deg
Eccentricity:
0003784
Arg of perigee: 86
3017 deg
Mean anomaly: 273
8566 deg
Mean motion: 15
49932253 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3012
Checksum: 300
Coasting Arc #4 (Orbit 3027)
---------------------------------------
Vector Time (GMT): 2014/032/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4747389
83 A = 6791569
80 meter
Y = 132326
99 meter E =
0010848
Z = 4847539
74 I = 51
91669
XDOT = -2778
617397 Wp = 70
46269
YDOT = -6682
568909 meter/sec RA = 51
51919 deg
ZDOT = -2530
655543 TA = 44
37414
MA = 44
28726
Ha = 229
086 n
mi
Hp = 219
760
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15575425
95 X = -4772063
92
Y = 434143
65 feet Y = 79100
91 meter
Z = 15904001
78 Z = 4824418
23
XDOT = -9116
198809 XDOT = -2691
392098
YDOT = -21924
438679 feet/sec YDOT = -6713
153602 meter/sec
ZDOT = -8302
675665 ZDOT = -2543
941163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10570675
35 X = -3221941
85
Y = -11581864
10 feet Y = -3530152
18 meter
Z = 15806356
11 Z = 4817777
34
XDOT = 9831
745771 XDOT = 2996
716111
YDOT = -20416
119558 feet/sec YDOT = -6222
833241 meter/sec
ZDOT = -8357
648880 ZDOT = -2547
411379
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
54389841
00016717 00000-0 10270-3 0 9032
2 25544 51
6466 51
9693 0003898 89
8418 270
3179 15
49991228 30281
Satellite: ISS
Catalog Number: 25544
Epoch time: 14032
54389841 = yrday
fracday
Element set: 903
Inclination: 51
6466 deg
RA of node: 51
9693 deg
Eccentricity:
0003898
Arg of perigee: 89
8418 deg
Mean anomaly: 270
3179 deg
Mean motion: 15
49991228 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3028
Checksum: 347
Coasting Arc #5 (Orbit 3042)
---------------------------------------
Vector Time (GMT): 2014/033/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4901104
76 A = 6792209
47 meter
Y = -196055
94 meter E =
0014257
Z = -4711980
50 I = 51
89956
XDOT = 3000
656245 Wp = 104
67553
YDOT = 6430
772826 meter/sec RA = 46
58218 deg
ZDOT = 2857
239682 TA = 193
63998
MA = 193
67855
Ha = 228
949 n
mi
Hp = 219
928
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16079740
02 X = 4925821
65
Y = -643228
15 feet Y = -141110
75 meter
Z = -15459253
62 Z = -4688112
08
XDOT = 9844
672720 XDOT = 2914
643628
YDOT = 21098
336044 feet/sec YDOT = 6463
847337 meter/sec
ZDOT = 9374
145937 ZDOT = 2871
606826
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11258378
57 X = 3431553
79
Y = 11633027
10 feet Y = 3545746
66 meter
Z = -15358447
07 Z = -4681254
67
XDOT = -8365
133158 XDOT = -2549
692587
YDOT = 20534
344701 feet/sec YDOT = 6258
868265 meter/sec
ZDOT = 9433
721853 ZDOT = 2875
398421
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
51101025
00016717 00000-0 10270-3 0 9047
2 25544 51
6475 47
1785 0003824 92
3358 267
8231 15
49975904 30431
Satellite: ISS
Catalog Number: 25544
Epoch time: 14033
51101025 = yrday
fracday
Element set: 904
Inclination: 51
6475 deg
RA of node: 47
1785 deg
Eccentricity:
0003824
Arg of perigee: 92
3358 deg
Mean anomaly: 267
8231 deg
Mean motion: 15
49975904 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3043
Checksum: 302
Coasting Arc #6 (Orbit 3058)
---------------------------------------
Vector Time (GMT): 2014/034/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5055714
93 A = 6792736
81 meter
Y = 251507
24 meter E =
0012563
Z = 4520747
13 I = 51
87896
XDOT = -3183
035934 Wp = 76
16934
YDOT = -6195
287518 meter/sec RA = 41
64286 deg
ZDOT = -3204
647167 TA = 45
97575
MA = 45
87230
Ha = 228
991 n
mi
Hp = 219
714
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16586991
25 X = -5080111
56
Y = 825154
97 feet Y = 194834
89 meter
Z = 14831847
53 Z = 4496128
32
XDOT = -10443
031281 XDOT = -3097
955390
YDOT = -20325
746451 feet/sec YDOT = -6230
406760 meter/sec
ZDOT = -10513
934274 ZDOT = -3219
902586
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11932096
86 X = -3636903
12
Y = -11683656
65 feet Y = -3561178
55 meter
Z = 14727867
88 Z = 4489054
13
XDOT = 7024
178467 XDOT = 2140
969597
YDOT = -20550
042865 feet/sec YDOT = -6263
653065 meter/sec
ZDOT = -10577
292030 ZDOT = -3223
958611
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
54258030
00016717 00000-0 10270-3 0 9051
2 25544 51
6465 42
0672 0003861 95
7531 264
4060 15
50035222 30592
Satellite: ISS
Catalog Number: 25544
Epoch time: 14034
54258030 = yrday
fracday
Element set: 905
Inclination: 51
6465 deg
RA of node: 42
0672 deg
Eccentricity:
0003861
Arg of perigee: 95
7531 deg
Mean anomaly: 264
4060 deg
Mean motion: 15
50035222 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3059
Checksum: 277
Coasting Arc #7 (Orbit 3073)
---------------------------------------
Vector Time (GMT): 2014/035/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5224321
64 A = 6793489
64 meter
Y = -356493
30 meter E =
0012199
Z = -4340162
90 I = 51
85798
XDOT = 3323
920528 Wp = 106
18872
YDOT = 5924
974800 meter/sec RA = 36
70362 deg
ZDOT = 3519
295273 TA = 199
58011
MA = 199
62700
Ha = 228
885 n
mi
Hp = 219
854
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17140162
85 X = 5249002
57
Y = -1169597
45 feet Y = -297933
86 meter
Z = -14239379
60 Z = -4314724
26
XDOT = 10905
251077 XDOT = 3240
323722
YDOT = 19438
893702 feet/sec YDOT = 5961
677799 meter/sec
ZDOT = 11546
244334 ZDOT = 3535
238786
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12760048
36 X = 3889262
74
Y = 11635416
66 feet Y = 3546475
00 meter
Z = -14131925
46 Z = -4307410
88
XDOT = -5702
352666 XDOT = -1738
077093
YDOT = 20337
959973 feet/sec YDOT = 6199
010200 meter/sec
ZDOT = 11612
543536 ZDOT = 3539
503270
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
50966367
00016717 00000-0 10270-3 0 9068
2 25544 51
6469 37
2766 0003846 98
3483 261
8103 15
50019908 30743
Satellite: ISS
Catalog Number: 25544
Epoch time: 14035
50966367 = yrday
fracday
Element set: 906
Inclination: 51
6469 deg
RA of node: 37
2766 deg
Eccentricity:
0003846
Arg of perigee: 98
3483 deg
Mean anomaly: 261
8103 deg
Mean motion: 15
50019908 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3074
Checksum: 325
Coasting Arc #8 (Orbit 3089)
---------------------------------------
Vector Time (GMT): 2014/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5389895
77 A = 6794138
35 meter
Y = 453399
27 meter E =
0014189
Z = 4100402
65 I = 51
83471
XDOT = -3418
996479 Wp = 83
43792
YDOT = -5678
571317 meter/sec RA = 31
76175 deg
ZDOT = -3853
278372 TA = 46
35476
MA = 46
23719
Ha = 228
867 n
mi
Hp = 219
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17683385
07 X = -5414483
40
Y = 1487530
43 feet Y = 392988
73 meter
Z = 13452764
60 Z = 4074159
87
XDOT = -11217
180049 XDOT = -3336
525551
YDOT = -18630
483324 feet/sec YDOT = -5716
343786 meter/sec
ZDOT = -12641
989409 ZDOT = -3869
686590
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13562987
20 X = -4133998
50
Y = -11572844
50 feet Y = -3527403
00 meter
Z = 13341903
09 Z = 4066612
06
XDOT = 4551
190573 XDOT = 1387
202887
YDOT = -20036
707491 feet/sec YDOT = -6107
188443 meter/sec
ZDOT = -12710
283062 ZDOT = -3874
094277
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
54120289
00016717 00000-0 10270-3 0 9079
2 25544 51
6463 32
1652 0003780 101
6846 258
4729 15
50079306 30905
Satellite: ISS
Catalog Number: 25544
Epoch time: 14036
54120289 = yrday
fracday
Element set: 907
Inclination: 51
6463 deg
RA of node: 32
1652 deg
Eccentricity:
0003780
Arg of perigee: 101
6846 deg
Mean anomaly: 258
4729 deg
Mean motion: 15
50079306 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3090
Checksum: 298
Coasting Arc #9 (Orbit 3104)
---------------------------------------
Vector Time (GMT): 2014/037/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5557584
47 A = 6794955
17 meter
Y = -604101
16 meter E =
0010028
Z = -3873009
22 I = 51
81053
XDOT = 3473
918534 Wp = 103
89390
YDOT = 5412
008256 meter/sec RA = 26
81959 deg
ZDOT = 4147
434848 TA = 209
67340
MA = 209
73032
Ha = 228
801 n
mi
Hp = 219
789
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18233544
85 X = 5582740
23
Y = -1981959
19 feet Y = -541812
18 meter
Z = -12706723
16 Z = -3845950
45
XDOT = 11397
370519 XDOT = 3392
995385
YDOT = 17755
932600 feet/sec YDOT = 5450
403513 meter/sec
ZDOT = 13607
069710 ZDOT = 4164
113715
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14495737
74 X = 4418300
86
Y = 11364696
54 feet Y = 3463959
50 meter
Z = -12592394
27 Z = -3838161
77
XDOT = -3468
719934 XDOT = -1057
265836
YDOT = 19553
865263 feet/sec YDOT = 5960
018132 meter/sec
ZDOT = 13676
543307 ZDOT = 4168
610400
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
50825708
00016717 00000-0 10270-3 0 9085
2 25544 51
6462 27
3744 0003853 104
3729 255
7849 15
50067217 31051
Satellite: ISS
Catalog Number: 25544
Epoch time: 14037
50825708 = yrday
fracday
Element set: 908
Inclination: 51
6462 deg
RA of node: 27
3744 deg
Eccentricity:
0003853
Arg of perigee: 104
3729 deg
Mean anomaly: 255
7849 deg
Mean motion: 15
50067217 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3105
Checksum: 310
Coasting Arc #10 (Orbit 3120)
---------------------------------------
Vector Time (GMT): 2014/038/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5717151
49 A = 6795682
49 meter
Y = 744828
24 meter E =
0015643
Z = 3583316
34 I = 51
78511
XDOT = -3478
544794 Wp = 91
85828
YDOT = -5178
316431 meter/sec RA = 21
87486 deg
ZDOT = -4457
316578 TA = 45
93189
MA = 45
80320
Ha = 228
734 n
mi
Hp = 219
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18757058
70 X = -5742461
80
Y = 2443662
21 feet Y = 680753
97 meter
Z = 11756287
19 Z = 3555482
08
XDOT = -11412
548536 XDOT = -3398
729231
YDOT = -16989
227135 feet/sec YDOT = -5216
769575 meter/sec
ZDOT = -14623
742053 ZDOT = -4474
020656
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15382347
21 X = -4688539
43
Y = -11132562
50 feet Y = -3393205
05 meter
Z = 11638662
77 Z = 3547464
41
XDOT = 2598
378642 XDOT = 791
985810
YDOT = -19008
128101 feet/sec YDOT = -5793
677445 meter/sec
ZDOT = -14693
355747 ZDOT = -4478
534832
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
53976464
00016717 00000-0 10270-3 0 9096
2 25544 51
6459 22
2630 0003715 107
7376 252
4181 15
50123457 31217
Satellite: ISS
Catalog Number: 25544
Epoch time: 14038
53976464 = yrday
fracday
Element set: 909
Inclination: 51
6459 deg
RA of node: 22
2630 deg
Eccentricity:
0003715
Arg of perigee: 107
7376 deg
Mean anomaly: 252
4181 deg
Mean motion: 15
50123457 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3121
Checksum: 297
Coasting Arc #11 (Orbit 3135)
---------------------------------------
Vector Time (GMT): 2014/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5866365
41 A = 6796493
73 meter
Y = -939944
73 meter E =
0008213
Z = -3308567
74 I = 51
75873
XDOT = 3448
892491 Wp = 95
04100
YDOT = 4939
198324 meter/sec RA = 16
92929 deg
ZDOT = 4721
380605 TA = 226
68227
MA = 226
75077
Ha = 228
687 n
mi
Hp = 219
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19246605
68 X = 5892511
80
Y = -3083808
18 feet Y = -874197
15 meter
Z = -10854881
02 Z = -3280006
66
XDOT = 11315
264079 XDOT = 3370
470334
YDOT = 16204
718910 feet/sec YDOT = 4977
327644 meter/sec
ZDOT = 15490
093847 ZDOT = 4737
944023
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16360270
77 X = 4986610
53
Y = 10718655
20 feet Y = 3267046
11 meter
Z = -10734156
52 Z = -3271770
91
XDOT = -1829
758719 XDOT = -557
710457
YDOT = 18343
230296 feet/sec YDOT = 5591
016594 meter/sec
ZDOT = 15559
150543 ZDOT = 4742
429086
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
50678856
00016717 00000-0 10270-3 0 9100
2 25544 51
6459 17
4718 0003828 110
6434 249
5128 15
50119509 31360
Satellite: ISS
Catalog Number: 25544
Epoch time: 14039
50678856 = yrday
fracday
Element set: 910
Inclination: 51
6459 deg
RA of node: 17
4718 deg
Eccentricity:
0003828
Arg of perigee: 110
6434 deg
Mean anomaly: 249
5128 deg
Mean motion: 15
50119509 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3136
Checksum: 314
Coasting Arc #12 (Orbit 3151)
---------------------------------------
Vector Time (GMT): 2014/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6001716
49 A = 6797242
64 meter
Y = 1120749
90 meter E =
0016787
Z = 2969208
22 I = 51
73189
XDOT = -3367
117704 Wp = 101
08409
YDOT = -4742
660422 meter/sec RA = 11
98142 deg
ZDOT = -4995
057813 TA = 45
06451
MA = 44
92846
Ha = 228
598 n
mi
Hp = 219
680
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19690670
91 X = -6028226
12
Y = 3677000
99 feet Y = 1053486
69 meter
Z = 9741496
77 Z = 2939988
83
XDOT = -11046
974093 XDOT = -3289
570006
YDOT = -15559
909522 feet/sec YDOT = -4779
880175 meter/sec
ZDOT = -16387
984951 ZDOT = -5011
226073
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17262107
09 X = -5261490
24
Y = -10278815
53 feet Y = -3132982
97 meter
Z = 9617963
75 Z = 2931555
35
XDOT = 1305
410010 XDOT = 397
888971
YDOT = -17654
431282 feet/sec YDOT = -5381
070655 meter/sec
ZDOT = -16455
405001 ZDOT = -5015
607444
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
53826371
00016717 00000-0 10270-3 0 9113
2 25544 51
6460 12
3601 0003684 114
1766 245
9770 15
50167313 31521
Satellite: ISS
Catalog Number: 25544
Epoch time: 14040
53826371 = yrday
fracday
Element set: 911
Inclination: 51
6460 deg
RA of node: 12
3601 deg
Eccentricity:
0003684
Arg of perigee: 114
1766 deg
Mean anomaly: 245
9770 deg
Mean motion: 15
50167313 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3152
Checksum: 278
Coasting Arc #13 (Orbit 3166)
---------------------------------------
Vector Time (GMT): 2014/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6114908
07 A = 6797967
26 meter
Y = -1352654
64 meter E =
0007491
Z = -2648218
65 I = 51
70412
XDOT = 3261
291630 Wp = 79
23208
YDOT = 4554
108970 meter/sec RA = 7
03237 deg
ZDOT = 5218
316471 TA = 251
01586
MA = 251
09704
Ha = 228
538 n
mi
Hp = 219
704
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20062034
35 X = 6142443
22
Y = -4437843
29 feet Y = -1284119
92 meter
Z = -8688381
41 Z = -2618446
99
XDOT = 10699
775689 XDOT = 3184
775792
YDOT = 14941
302394 feet/sec YDOT = 4590
151107 meter/sec
ZDOT = 17120
460862 ZDOT = 5233
973096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18206821
92 X = 5549439
32
Y = 9636557
25 feet Y = 2937222
65 meter
Z = -8562479
02 Z = -2609843
60
XDOT = -894
405343 XDOT = -272
614749
YDOT = 16918
899416 feet/sec YDOT = 5156
880542 meter/sec
ZDOT = 17185
752955 ZDOT = 5238
217501
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
50525635
00016717 00000-0 10270-3 0 9121
2 25544 51
6461 7
5686 0003759 117
4831 242
6702 15
50175517 31673
Satellite: ISS
Catalog Number: 25544
Epoch time: 14041
50525635 = yrday
fracday
Element set: 912
Inclination: 51
6461 deg
RA of node: 7
5686 deg
Eccentricity:
0003759
Arg of perigee: 117
4831 deg
Mean anomaly: 242
6702 deg
Mean motion: 15
50175517 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3167
Checksum: 298
Coasting Arc #14 (Orbit 3182)
---------------------------------------
Vector Time (GMT): 2014/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6208625
11 A = 6798660
03 meter
Y = 1563225
16 meter E =
0017439
Z = 2261684
09 I = 51
67658
XDOT = -3105
018101 Wp = 110
79340
YDOT = -4417
524207 meter/sec RA = 2
08126 deg
ZDOT = -5442
506808 TA = 44
08323
MA = 43
94434
Ha = 228
449 n
mi
Hp = 219
684
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20369504
95 X = -6236630
29
Y = 5128691
48 feet Y = 1493639
83 meter
Z = 7420223
38 Z = 2231456
08
XDOT = -10187
067262 XDOT = -3028
952237
YDOT = -14493
189656 feet/sec YDOT = -4451
821368 meter/sec
ZDOT = -17855
993465 ZDOT = -5457
405312
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19039483
67 X = -5803234
62
Y = -8977719
67 feet Y = -2736408
96 meter
Z = 7292361
37 Z = 2222711
75
XDOT = 744
292112 XDOT = 226
860236
YDOT = -16208
483954 feet/sec YDOT = -4940
345909 meter/sec
ZDOT = -17918
109466 ZDOT = -5461
439765
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 14042
53669858
00016717 00000-0 10270-3 0 9132
2 25544 51
6467 2
4569 0003666 121
2510 238
9005 15
50210886 31838
Satellite: ISS
Catalog Number: 25544
Epoch time: 14042
53669858 = yrday
fracday
Element set: 913
Inclination: 51
6467 deg
RA of node: 2
4569 deg
Eccentricity:
0003666
Arg of perigee: 121
2510 deg
Mean anomaly: 238
9005 deg
Mean motion: 15
50210886 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3183
Checksum: 304
Coasting Arc #15 (Orbit 3197)
---------------------------------------
Vector Time (GMT): 2014/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6270325
74 A = 6799217
75 meter
Y = -1817930
34 meter E =
0008283
Z = -1897754
28 I = 51
64787
XDOT = 2938
637032 Wp = 64
67637
YDOT = 4299
646214 meter/sec RA = 357
12880 deg
ZDOT = 5613
340714 TA = 274
47261
MA = 274
56724
Ha = 228
362 n
mi
Hp = 219
699
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20571934
84 X = 6299406
68
Y = -5964338
40 feet Y = -1747649
04 meter
Z = -6226227
95 Z = -1867223
94
XDOT = 9641
197612 XDOT = 2863
071876
YDOT = 14106
450832 feet/sec YDOT = 4332
085677 meter/sec
ZDOT = 18416
472160 ZDOT = 5627
432120
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19862543
80 X = 6054103
35
Y = 8114744
65 feet Y = 2473374
17 meter
Z = -6097050
37 Z = -1858380
95
XDOT = -695
079142 XDOT = -211
860122
YDOT = 15525
759351 feet/sec YDOT = 4732
251450 meter/sec
ZDOT = 18475
203052 ZDOT = 5631
241890
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 14043
50365929
00016717 00000-0 10270-3 0 9143
2 25544 51
6469 357
6653 0003660 124
9383 235
2112 15
50231512 31985
Satellite: ISS
Catalog Number: 25544
Epoch time: 14043
50365929 = yrday
fracday
Element set: 914
Inclination: 51
6469 deg
RA of node: 357
6653 deg
Eccentricity:
0003660
Arg of perigee: 124
9383 deg
Mean anomaly: 235
2112 deg
Mean motion: 15
50231512 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3198
Checksum: 302
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