[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 25th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21527 82 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 2903)
---------------------------------------
Vector Time (GMT): 2014/024/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4179831
03 A = 6789624
03 meter
Y = 193858
41 meter E =
0005632
Z = 5342194
26 I = 51
98597
XDOT = -53
625939 Wp = 79
62414
YDOT = -7662
495110 meter/sec RA = 90
98365 deg
ZDOT = 236
875343 TA = 8
13284
MA = 8
12371
Ha = 228
955 n
mi
Hp = 220
131
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13713356
41 X = -4207638
68
Y = 636018
42 feet Y = 146961
39 meter
Z = 17526884
06 Z = 5321821
79
XDOT = -175
938120 XDOT = 30
911119
YDOT = -25139
419653 feet/sec YDOT = -7662
622116 meter/sec
ZDOT = 777
150076 ZDOT = 236
820170
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8045291
43 X = -2452204
83
Y = -11257971
69 feet Y = -3431429
77 meter
Z = 17440862
58 Z = 5315974
91
XDOT = 20185
891096 XDOT = 6152
659606
YDOT = -13223
929511 feet/sec YDOT = -4030
653715 meter/sec
ZDOT = 778
134681 ZDOT = 237
175451
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 14024
54879061
00016717 00000-0 10270-3 0 9008
2 25544 51
6481 91
5693 0003435 64
4574 295
6931 15
49925789 29044
Satellite: ISS
Catalog Number: 25544
Epoch time: 14024
54879061 = yrday
fracday
Element set: 900
Inclination: 51
6481 deg
RA of node: 91
5693 deg
Eccentricity:
0003435
Arg of perigee: 64
4574 deg
Mean anomaly: 295
6931 deg
Mean motion: 15
49925789 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2904
Checksum: 336
Coasting Arc #2 (Orbit 2918)
---------------------------------------
Vector Time (GMT): 2014/025/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4187175
30 A = 6789698
26 meter
Y = -162023
78 meter E =
0018162
Z = -5358014
98 I = 51
98504
XDOT = 438
304236 Wp = 86
23978
YDOT = 7634
766676 meter/sec RA = 86
05166 deg
ZDOT = 113
140515 TA = 184
82733
MA = 184
84487
Ha = 228
908 n
mi
Hp = 220
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13737451
77 X = 4214703
25
Y = -531574
07 feet Y = -115046
11 meter
Z = -17578789
30 Z = -5337607
53
XDOT = 1438
006024 XDOT = 352
348398
YDOT = 25048
447100 feet/sec YDOT = 7639
187466 meter/sec
ZDOT = 371
195916 ZDOT = 115
061062
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8164685
06 X = 2488596
01
Y = 11196433
22 feet Y = 3412672
84 meter
Z = -17492620
91 Z = -5331750
85
XDOT = -19174
454147 XDOT = -5844
373624
YDOT = 14565
455806 feet/sec YDOT = 4439
550930 meter/sec
ZDOT = 378
074584 ZDOT = 115
237133
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 14025
51594781
00016717 00000-0 10270-3 0 9010
2 25544 51
6476 86
7787 0003581 66
8120 293
3407 15
49901665 29199
Satellite: ISS
Catalog Number: 25544
Epoch time: 14025
51594781 = yrday
fracday
Element set: 901
Inclination: 51
6476 deg
RA of node: 86
7787 deg
Eccentricity:
0003581
Arg of perigee: 66
8120 deg
Mean anomaly: 293
3407 deg
Mean motion: 15
49901665 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2919
Checksum: 333
Coasting Arc #3 (Orbit 2934)
---------------------------------------
Vector Time (GMT): 2014/026/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4199069
05 A = 6789557
39 meter
Y = 113039
86 meter E =
0006358
Z = 5329156
49 I = 51
98271
XDOT = -812
179120 Wp = 69
78690
YDOT = -7608
518830 meter/sec RA = 81
11964 deg
ZDOT = -475
965153 TA = 24
74814
MA = 24
71765
Ha = 228
985 n
mi
Hp = 219
955
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13776473
26 X = -4225908
12
Y = 370865
69 feet Y = 65932
96 meter
Z = 17484109
22 Z = 5308692
99
XDOT = -2664
629659 XDOT = -724
726534
YDOT = -24962
332121 feet/sec YDOT = -7617
112146 meter/sec
ZDOT = -1561
565464 ZDOT = -479
698392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8246211
20 X = -2513445
18
Y = -11177773
41 feet Y = -3406985
34 meter
Z = 17397707
16 Z = 5302821
14
XDOT = 18144
292257 XDOT = 5530
380280
YDOT = -15852
074836 feet/sec YDOT = -4831
712410 meter/sec
ZDOT = -1576
086363 ZDOT = -480
391123
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 14026
54756483
00016717 00000-0 10270-3 0 9024
2 25544 51
6481 81
6690 0003625 70
2870 289
8671 15
49968515 29350
Satellite: ISS
Catalog Number: 25544
Epoch time: 14026
54756483 = yrday
fracday
Element set: 902
Inclination: 51
6481 deg
RA of node: 81
6690 deg
Eccentricity:
0003625
Arg of perigee: 70
2870 deg
Mean anomaly: 289
8671 deg
Mean motion: 15
49968515 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2935
Checksum: 338
Coasting Arc #4 (Orbit 2949)
---------------------------------------
Vector Time (GMT): 2014/027/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4254635
06 A = 6789793
52 meter
Y = -73776
51 meter E =
0017978
Z = -5306487
09 I = 51
97776
XDOT = 1172
415459 Wp = 91
57094
YDOT = 7511
351736 meter/sec RA = 76
18668 deg
ZDOT = 837
559015 TA = 186
40818
MA = 186
43121
Ha = 228
929 n
mi
Hp = 220
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13958776
46 X = 4280920
72
Y = -242048
91 feet Y = -26051
27 meter
Z = -17409734
56 Z = -5285755
09
XDOT = 3846
507410 XDOT = 1084
266168
YDOT = 24643
542441 feet/sec YDOT = 7523
969529 meter/sec
ZDOT = 2747
897031 ZDOT = 843
040574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8439411
64 X = 2572332
67
Y = 11257113
49 feet Y = 3431168
19 meter
Z = -17322199
98 Z = -5279806
55
XDOT = -16906
306557 XDOT = -5153
042239
YDOT = 16926
701424 feet/sec YDOT = 5159
258594 meter/sec
ZDOT = 2769
803031 ZDOT = 844
235964
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
51469416
00016717 00000-0 10270-3 0 9030
2 25544 51
6483 76
8780 0003761 72
7796 287
3766 15
49947932 29508
Satellite: ISS
Catalog Number: 25544
Epoch time: 14027
51469416 = yrday
fracday
Element set: 903
Inclination: 51
6483 deg
RA of node: 76
8780 deg
Eccentricity:
0003761
Arg of perigee: 72
7796 deg
Mean anomaly: 287
3766 deg
Mean motion: 15
49947932 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2950
Checksum: 352
Coasting Arc #5 (Orbit 2965)
---------------------------------------
Vector Time (GMT): 2014/028/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4317149
09 A = 6789850
93 meter
Y = 19805
41 meter E =
0007804
Z = 5235046
19 I = 51
96993
XDOT = -1513
357053 Wp = 65
61872
YDOT = -7417
014971 meter/sec RA = 71
25368 deg
ZDOT = -1215
392037 TA = 36
01798
MA = 35
96543
Ha = 229
020 n
mi
Hp = 219
772
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14163874
98 X = -4342479
42
Y = 64978
37 feet Y = -28613
55 meter
Z = 17175348
39 Z = 5214012
93
XDOT = -4965
082195 XDOT = -1424
401981
YDOT = -24334
038618 feet/sec YDOT = -7433
440871 meter/sec
ZDOT = -3987
506682 ZDOT = -1222
527820
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8612229
73 X = -2625007
62
Y = -11379439
01 feet Y = -3468453
01 meter
Z = 17086545
47 Z = 5207979
06
XDOT = 15679
221656 XDOT = 4779
026761
YDOT = -17919
717393 feet/sec YDOT = -5461
929861 meter/sec
ZDOT = -4016
404099 ZDOT = -1224
199969
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
54628162
00016717 00000-0 10270-3 0 9040
2 25544 51
6478 71
7681 0003851 76
4283 283
7296 15
50012242 29662
Satellite: ISS
Catalog Number: 25544
Epoch time: 14028
54628162 = yrday
fracday
Element set: 904
Inclination: 51
6478 deg
RA of node: 71
7681 deg
Eccentricity:
0003851
Arg of perigee: 76
4283 deg
Mean anomaly: 283
7296 deg
Mean motion: 15
50012242 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2966
Checksum: 316
Coasting Arc #6 (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 = 4420800
76 A = 6790258
51 meter
Y = 10579
12 meter E =
0017183
Z = -5169222
96 I = 51
96098
XDOT = 1830
173894 Wp = 96
73997
YDOT = 7255
929031 meter/sec RA = 66
31930 deg
ZDOT = 1582
596637 TA = 188
47659
MA = 188
50565
Ha = 228
929 n
mi
Hp = 219
894
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14503939
50 X = 4445463
75
Y = 34708
40 feet Y = 60153
38 meter
Z = -16959392
93 Z = -5147687
92
XDOT = 6004
507525 XDOT = 1741
212883
YDOT = 23805
541441 feet/sec YDOT = 7275
897752 meter/sec
ZDOT = 5192
246185 ZDOT = 1591
271284
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8935734
10 X = 2723611
75
Y = 11558277
88 feet Y = 3522963
10 meter
Z = -16868471
85 Z = -5141510
22
XDOT = -14294
403169 XDOT = -4356
934086
YDOT = 18668
143789 feet/sec YDOT = 5690
050227 meter/sec
ZDOT = 5227
662907 ZDOT = 1593
391654
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
51338264
00016717 00000-0 10270-3 0 9050
2 25544 51
6486 66
9768 0003904 78
9050 281
2539 15
49995223 29818
Satellite: ISS
Catalog Number: 25544
Epoch time: 14029
51338264 = yrday
fracday
Element set: 905
Inclination: 51
6486 deg
RA of node: 66
9768 deg
Eccentricity:
0003904
Arg of perigee: 78
9050 deg
Mean anomaly: 281
2539 deg
Mean motion: 15
49995223 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2981
Checksum: 342
Coasting Arc #7 (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 = -4531856
81 A = 6790526
32 meter
Y = -52628
24 meter E =
0009633
Z = 5050257
97 I = 51
94794
XDOT = -2118
685354 Wp = 66
69173
YDOT = -7100
654223 meter/sec RA = 61
38418 deg
ZDOT = -1968
517103 TA = 42
37487
MA = 42
30051
Ha = 229
027 n
mi
Hp = 219
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14868296
62 X = -4555463
38
Y = -172664
84 feet Y = -103438
37 meter
Z = 16569087
82 Z = 5028186
09
XDOT = -6951
067435 XDOT = -2029
564617
YDOT = -23296
109657 feet/sec YDOT = -7123
848407 meter/sec
ZDOT = -6458
389446 ZDOT = -1978
592672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9252619
84 X = -2820198
53
Y = -11771335
44 feet Y = -3587903
04 meter
Z = 16475904
12 Z = 5021855
58
XDOT = 12959
042348 XDOT = 3949
916108
YDOT = -19314
511293 feet/sec YDOT = -5887
063042 meter/sec
ZDOT = -6499
744639 ZDOT = -1981
122166
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
54494028
00016717 00000-0 10270-3 0 9067
2 25544 51
6473 61
8662 0004029 82
5940 277
5668 15
50056906 29975
Satellite: ISS
Catalog Number: 25544
Epoch time: 14030
54494028 = yrday
fracday
Element set: 906
Inclination: 51
6473 deg
RA of node: 61
8662 deg
Eccentricity:
0004029
Arg of perigee: 82
5940 deg
Mean anomaly: 277
5668 deg
Mean motion: 15
50056906 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2997
Checksum: 326
Coasting Arc #8 (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 = 4677969
69 A = 6791107
03 meter
Y = 58366
12 meter E =
0015751
Z = -4937084
57 I = 51
93505
XDOT = 2373
996023 Wp = 101
29381
YDOT = 6886
913392 meter/sec RA = 56
44811 deg
ZDOT = 2334
129700 TA = 191
49153
MA = 191
52753
Ha = 228
902 n
mi
Hp = 219
770
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15347669
59 X = 4700951
48
Y = 191489
88 feet Y = 110806
55 meter
Z = -16197784
02 Z = -4914304
45
XDOT = 7788
700862 XDOT = 2285
470432
YDOT = 22594
860211 feet/sec YDOT = 6912
966014 meter/sec
ZDOT = 7657
905839 ZDOT = 2345
446747
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9744669
92 X = 2970175
39
Y = 11988969
75 feet Y = 3654237
98 meter
Z = -16101610
16 Z = -4907770
78
XDOT = -11527
203097 XDOT = -3513
491504
YDOT = 19702
128519 feet/sec YDOT = 6005
208773 meter/sec
ZDOT = 7704
536546 ZDOT = 2348
342739
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
51201256
00016717 00000-0 10270-3 0 9075
2 25544 51
6482 57
0748 0003989 85
0382 275
1224 15
50041453 30121
Satellite: ISS
Catalog Number: 25544
Epoch time: 14031
51201256 = yrday
fracday
Element set: 907
Inclination: 51
6482 deg
RA of node: 57
0748 deg
Eccentricity:
0003989
Arg of perigee: 85
0382 deg
Mean anomaly: 275
1224 deg
Mean motion: 15
50041453 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3012
Checksum: 280
Coasting Arc #9 (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 = -4829698
85 A = 6791574
61 meter
Y = -72805
00 meter E =
0011576
Z = 4766491
67 I = 51
91794
XDOT = -2591
997927 Wp = 71
22926
YDOT = -6683
703779 meter/sec RA = 51
51044 deg
ZDOT = -2719
437586 TA = 45
60072
MA = 45
50600
Ha = 228
982 n
mi
Hp = 219
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15845468
66 X = -4851679
29
Y = -238861
56 feet Y = -126936
46 meter
Z = 15638096
04 Z = 4742976
87
XDOT = -8503
930208 XDOT = -2503
856788
YDOT = -21928
162005 feet/sec YDOT = -6712
196461 meter/sec
ZDOT = -8922
039323 ZDOT = -2731
814433
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10236505
02 X = -3120086
73
Y = -12224765
22 feet Y = -3726108
44 meter
Z = 15538824
28 Z = 4736233
64
XDOT = 10190
271669 XDOT = 3105
994805
YDOT = -19976
515201 feet/sec YDOT = -6088
841833 meter/sec
ZDOT = -8973
175312 ZDOT = -2735
023835
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
54353997
00016717 00000-0 10270-3 0 9080
2 25544 51
6468 51
9632 0004096 88
6196 271
5423 15
50102112 30280
Satellite: ISS
Catalog Number: 25544
Epoch time: 14032
54353997 = yrday
fracday
Element set: 908
Inclination: 51
6468 deg
RA of node: 51
9632 deg
Eccentricity:
0004096
Arg of perigee: 88
6196 deg
Mean anomaly: 271
5423 deg
Mean motion: 15
50102112 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3028
Checksum: 304
Coasting Arc #10 (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 = 5007182
27 A = 6792312
71 meter
Y = 40271
21 meter E =
0013777
Z = -4602619
11 I = 51
90114
XDOT = 2770
631463 Wp = 104
40446
YDOT = 6434
134366 meter/sec RA = 46
57267 deg
ZDOT = 3074
835409 TA = 196
28576
MA = 196
33007
Ha = 228
855 n
mi
Hp = 219
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16427763
34 X = 5028717
38
Y = 132123
39 feet Y = 96384
85 meter
Z = -15100456
39 Z = -4578243
13
XDOT = 9089
998237 XDOT = 2683
541364
YDOT = 21109
364718 feet/sec YDOT = 6464
630582 meter/sec
ZDOT = 10088
042679 ZDOT = 3088
082532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10910560
47 X = 3325538
83
Y = 12407494
15 feet Y = 3781804
22 meter
Z = -14997546
72 Z = -4571252
24
XDOT = -8822
713512 XDOT = -2689
163079
YDOT = 20001
019831 feet/sec YDOT = 6096
310845 meter/sec
ZDOT = 10142
889225 ZDOT = 3091
552636
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
51058344
00016717 00000-0 10270-3 0 9097
2 25544 51
6477 47
1720 0004033 91
1466 269
0147 15
50086281 30435
Satellite: ISS
Catalog Number: 25544
Epoch time: 14033
51058344 = yrday
fracday
Element set: 909
Inclination: 51
6477 deg
RA of node: 47
1720 deg
Eccentricity:
0004033
Arg of perigee: 91
1466 deg
Mean anomaly: 269
0147 deg
Mean motion: 15
50086281 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3043
Checksum: 286
Coasting Arc #11 (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 = -5186297
91 A = 6792947
18 meter
Y = -14561
86 meter E =
0013462
Z = 4377360
04 I = 51
88090
XDOT = -2903
525374 Wp = 78
04037
YDOT = -6201
639210 meter/sec RA = 41
63266 deg
ZDOT = -3449
056534 TA = 46
89090
MA = 46
77836
Ha = 228
885 n
mi
Hp = 219
464
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17015413
09 X = -5207013
07
Y = -47775
12 feet Y = -72673
89 meter
Z = 14361417
46 Z = 4352115
85
XDOT = -9526
001882 XDOT = -2817
207335
YDOT = -20346
585336 feet/sec YDOT = -6233
625883 meter/sec
ZDOT = -11315
802277 ZDOT = -3462
951147
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11580126
91 X = -3529622
68
Y = -12588764
87 feet Y = -3837055
53 meter
Z = 14254842
57 Z = 4344876
01
XDOT = 7599
585363 XDOT = 2316
353619
YDOT = -19913
021348 feet/sec YDOT = -6069
488907 meter/sec
ZDOT = -11373
413806 ZDOT = -3466
616528
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
54208018
00016717 00000-0 10270-3 0 9108
2 25544 51
6467 42
0602 0004061 94
5614 265
6001 15
50147532 30595
Satellite: ISS
Catalog Number: 25544
Epoch time: 14034
54208018 = yrday
fracday
Element set: 910
Inclination: 51
6467 deg
RA of node: 42
0602 deg
Eccentricity:
0004061
Arg of perigee: 94
5614 deg
Mean anomaly: 265
6001 deg
Mean motion: 15
50147532 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3059
Checksum: 267
Coasting Arc #12 (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 = 5379322
03 A = 6793800
67 meter
Y = -65763
25 meter E =
0011484
Z = -4160632
90 I = 51
86027
XDOT = 2995
027124 Wp = 104
52838
YDOT = 5937
750656 meter/sec RA = 36
69288 deg
ZDOT = 3784
388647 TA = 204
40840
MA = 204
46283
Ha = 228
792 n
mi
Hp = 219
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17648694
31 X = 5399868
35
Y = -215758
69 feet Y = -5493
60 meter
Z = -13650370
42 Z = -4134451
37
XDOT = 9826
204475 XDOT = 2910
024179
YDOT = 19480
809238 feet/sec YDOT = 5970
767912 meter/sec
ZDOT = 12415
973251 ZDOT = 3798
731048
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12420134
30 X = 3785656
93
Y = 12659733
64 feet Y = 3858686
81 meter
Z = -13539829
52 Z = -4126940
04
XDOT = -6407
931524 XDOT = -1953
137529
YDOT = 19608
434036 feet/sec YDOT = 5976
650694 meter/sec
ZDOT = 12475
510893 ZDOT = 3802
535720
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
50909466
00016717 00000-0 10270-3 0 9111
2 25544 51
6471 37
2692 0004060 97
2543 262
9070 15
50131746 30748
Satellite: ISS
Catalog Number: 25544
Epoch time: 14035
50909466 = yrday
fracday
Element set: 911
Inclination: 51
6471 deg
RA of node: 37
2692 deg
Eccentricity:
0004060
Arg of perigee: 97
2543 deg
Mean anomaly: 262
9070 deg
Mean motion: 15
50131746 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3074
Checksum: 293
Coasting Arc #13 (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 = -5568159
11 A = 6794551
06 meter
Y = 139097
23 meter E =
0015172
Z = 3878984
98 I = 51
83735
XDOT = -3033
658317 Wp = 86
40865
YDOT = -5699
224524 meter/sec RA = 31
75053 deg
ZDOT = -4135
486632 TA = 46
96883
MA = 46
84185
Ha = 228
758 n
mi
Hp = 219
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18268238
54 X = -5588143
32
Y = 456355
73 feet Y = 76718
96 meter
Z = 12726328
67 Z = 3851887
42
XDOT = -9952
947233 XDOT = -2949
614218
YDOT = -18698
243188 feet/sec YDOT = -5732
679112 meter/sec
ZDOT = -13567
869528 ZDOT = -4150
019132
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13238914
92 X = -4035221
27
Y = -12710902
10 feet Y = -3874282
96 meter
Z = 12611912
64 Z = 3844110
97
XDOT = 5410
286335 XDOT = 1649
055275
YDOT = -19205
962239 feet/sec YDOT = -5853
977290 meter/sec
ZDOT = -13628
241280 ZDOT = -4153
887942
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
54056001
00016717 00000-0 10270-3 0 9125
2 25544 51
6465 32
1573 0003983 100
5096 259
6504 15
50192914 30904
Satellite: ISS
Catalog Number: 25544
Epoch time: 14036
54056001 = yrday
fracday
Element set: 912
Inclination: 51
6465 deg
RA of node: 32
1573 deg
Eccentricity:
0003983
Arg of perigee: 100
5096 deg
Mean anomaly: 259
6504 deg
Mean motion: 15
50192914 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3090
Checksum: 283
Coasting Arc #14 (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 = 5757529
31 A = 6795448
48 meter
Y = -270853
16 meter E =
0009304
Z = -3608712
13 I = 51
81343
XDOT = 3033
769784 Wp = 98
97704
YDOT = 5445
683950 meter/sec RA = 26
80807 deg
ZDOT = 4439
878147 TA = 218
55782
MA = 218
62431
Ha = 228
708 n
mi
Hp = 219
519
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18889531
87 X = 5777659
90
Y = -888625
85 feet Y = -206356
35 meter
Z = -11839606
73 Z = -3580694
28
XDOT = 9953
312938 XDOT = 2951
082199
YDOT = 17866
417159 feet/sec YDOT = 5479
147326 meter/sec
ZDOT = 14566
529355 ZDOT = 4454
414572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14198186
28 X = 4327607
18
Y = 12601718
16 feet Y = 3841003
70 meter
Z = -11721286
75 Z = -3572648
20
XDOT = -4493
883235 XDOT = -1369
735610
YDOT = 18642
425008 feet/sec YDOT = 5682
211142 meter/sec
ZDOT = 14626
953107 ZDOT = 4458
295307
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
50754478
00016717 00000-0 10270-3 0 9136
2 25544 51
6464 27
3662 0004073 103
4104 256
7501 15
50180977 31059
Satellite: ISS
Catalog Number: 25544
Epoch time: 14037
50754478 = yrday
fracday
Element set: 913
Inclination: 51
6464 deg
RA of node: 27
3662 deg
Eccentricity:
0004073
Arg of perigee: 103
4104 deg
Mean anomaly: 256
7501 deg
Mean motion: 15
50180977 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3105
Checksum: 289
Coasting Arc #15 (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 = -5935603
09 A = 6796249
43 meter
Y = 392771
74 meter E =
0016582
Z = 3270710
61 I = 51
78829
XDOT = -2976
204241 Wp = 95
82756
YDOT = -5227
141038 meter/sec RA = 21
86305 deg
ZDOT = -4754
353302 TA = 46
35170
MA = 46
21432
Ha = 228
622 n
mi
Hp = 219
431
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19473763
42 X = -5955441
86
Y = 1288621
18 feet Y = 326285
18 meter
Z = 10730677
85 Z = 3241828
46
XDOT = -9764
449608 XDOT = -2894
437154
YDOT = -17149
412854 feet/sec YDOT = -5259
965784 meter/sec
ZDOT = -15598
271987 ZDOT = -4768
612370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15107269
05 X = -4604695
61
Y = -12460399
20 feet Y = -3797929
68 meter
Z = 10608691
10 Z = 3233529
05
XDOT = 3815
470101 XDOT = 1162
955287
YDOT = -18010
575749 feet/sec YDOT = -5489
623488 meter/sec
ZDOT = -15657
556201 ZDOT = -4772
423130
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
53897790
00016717 00000-0 10270-3 0 9146
2 25544 51
6461 22
2542 0003922 106
6206 253
5376 15
50237658 31219
Satellite: ISS
Catalog Number: 25544
Epoch time: 14038
53897790 = yrday
fracday
Element set: 914
Inclination: 51
6461 deg
RA of node: 22
2542 deg
Eccentricity:
0003922
Arg of perigee: 106
6206 deg
Mean anomaly: 253
5376 deg
Mean motion: 15
50237658 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3121
Checksum: 299
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