[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 19th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 30138 95 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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 3306)
---------------------------------------
Vector Time (GMT): 2014/050/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5864672
49 A = 6799083
45 meter
Y = 3149804
15 meter E =
0012180
Z = -1355723
53 I = 51
45189
XDOT = -1272
268896 Wp = 145
76532
YDOT = -4848
376600 meter/sec RA = 322
42175 deg
ZDOT = -5796
037564 TA = 49
01780
MA = 48
91250
Ha = 227
513 n
mi
Hp = 219
708
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19241051
48 X = -5892872
82
Y = 10334003
11 feet Y = 3084063
80 meter
Z = -4447911
84 Z = -1384281
84
XDOT = -4174
110551 XDOT = -1189
803675
YDOT = -15906
747376 feet/sec YDOT = -4862
143453 meter/sec
ZDOT = -19015
871272 ZDOT = -5802
017193
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21781746
38 X = -6639076
30
Y = -1214085
73 feet Y = -370053
33 meter
Z = -4568930
14 Z = -1392609
91
XDOT = 4756
029481 XDOT = 1449
637786
YDOT = -14097
588254 feet/sec YDOT = -4296
944900 meter/sec
ZDOT = -19040
292287 ZDOT = -5803
481089
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 14050
52955885
00016717 00000-0 10270-3 0 9004
2 25544 51
6500 322
8568 0003647 155
3472 204
7854 15
50497588 33075
Satellite: ISS
Catalog Number: 25544
Epoch time: 14050
52955885 = yrday
fracday
Element set: 900
Inclination: 51
6500 deg
RA of node: 322
8568 deg
Eccentricity:
0003647
Arg of perigee: 155
3472 deg
Mean anomaly: 204
7854 deg
Mean motion: 15
50497588 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3307
Checksum: 323
Coasting Arc #2 (Orbit 3322)
---------------------------------------
Vector Time (GMT): 2014/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5685683
81 A = 6798308
33 meter
Y = -3235555
73 meter E =
0014299
Z = 1831825
60 I = 51
42534
XDOT = 1077
586153 Wp = 80
48246
YDOT = 5095
597276 meter/sec RA = 317
45229 deg
ZDOT = 5620
437871 TA = 299
69347
MA = 299
83573
Ha = 227
414 n
mi
Hp = 219
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18653818
28 X = 5712543
59
Y = -10615340
32 feet Y = -3171824
42 meter
Z = 6009926
51 Z = 1859511
19
XDOT = 3535
387640 XDOT = 993
223869
YDOT = 16717
838833 feet/sec YDOT = 5107
176369 meter/sec
ZDOT = 18439
756795 ZDOT = 5625
467204
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21427544
95 X = 6531115
70
Y = 294080
82 feet Y = 89635
83 meter
Z = 6127269
95 Z = 1867591
88
XDOT = -5511
306003 XDOT = -1679
846070
YDOT = 14581
270496 feet/sec YDOT = 4444
371247 meter/sec
ZDOT = 18460
129719 ZDOT = 5626
647538
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 14051
56077843
00016717 00000-0 10270-3 0 9019
2 25544 51
6496 317
7441 0003534 157
8668 202
2636 15
50541187 33235
Satellite: ISS
Catalog Number: 25544
Epoch time: 14051
56077843 = yrday
fracday
Element set: 901
Inclination: 51
6496 deg
RA of node: 317
7441 deg
Eccentricity:
0003534
Arg of perigee: 157
8668 deg
Mean anomaly: 202
2636 deg
Mean motion: 15
50541187 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3323
Checksum: 308
Coasting Arc #3 (Orbit 3337)
---------------------------------------
Vector Time (GMT): 2014/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5497024
43 A = 6797306
42 meter
Y = 3233738
96 meter E =
0008904
Z = -2342844
42 I = 51
40064
XDOT = -885
322397 Wp = 145
31764
YDOT = -5386
697611 meter/sec RA = 312
48049 deg
ZDOT = -5375
090929 TA = 60
86383
MA = 60
77474
Ha = 227
229 n
mi
Hp = 219
770
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18034857
05 X = -5521395
56
Y = 10609379
80 feet Y = 3172131
26 meter
Z = -7686497
44 Z = -2369607
46
XDOT = -2904
601040 XDOT = -798
911052
YDOT = -17672
892423 feet/sec YDOT = -5396
115130 meter/sec
ZDOT = -17634
812759 ZDOT = -5379
181353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20878563
36 X = -6363786
11
Y = 379112
77 feet Y = 115553
57 meter
Z = -7799943
37 Z = -2377422
74
XDOT = 6296
696561 XDOT = 1919
233112
YDOT = -15237
264081 feet/sec YDOT = -4644
318092 meter/sec
ZDOT = -17651
179345 ZDOT = -5380
079464
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 14052
52752340
00016717 00000-0 10270-3 0 9029
2 25544 51
6501 312
9508 0003579 164
6144 195
5116 15
50568957 33384
Satellite: ISS
Catalog Number: 25544
Epoch time: 14052
52752340 = yrday
fracday
Element set: 902
Inclination: 51
6501 deg
RA of node: 312
9508 deg
Eccentricity:
0003579
Arg of perigee: 164
6144 deg
Mean anomaly: 195
5116 deg
Mean motion: 15
50568957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3338
Checksum: 307
Coasting Arc #4 (Orbit 3353)
---------------------------------------
Vector Time (GMT): 2014/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5287239
87 A = 6796182
91 meter
Y = -3214127
07 meter E =
0014028
Z = 2800449
96 I = 51
37689
XDOT = 753
250085 Wp = 94
30370
YDOT = 5686
677645 meter/sec RA = 307
50589 deg
ZDOT = 5081
468343 TA = 297
55122
MA = 297
69368
Ha = 227
124 n
mi
Hp = 219
762
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17346587
50 X = 5309184
43
Y = -10545036
33 feet Y = -3154878
89 meter
Z = 9187827
95 Z = 2826187
92
XDOT = 2471
292929 XDOT = 664
920461
YDOT = 18657
078889 feet/sec YDOT = 5694
607427 meter/sec
ZDOT = 16671
484064 ZDOT = 5084
912574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20225125
55 X = 6164618
27
Y = -1014506
36 feet Y = -309221
54 meter
Z = 9296942
77 Z = 2833708
16
XDOT = -6898
973011 XDOT = -2102
806974
YDOT = 16051
136923 feet/sec YDOT = 4892
386534 meter/sec
ZDOT = 16685
079294 ZDOT = 5085
612169
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 14053
55869503
00016717 00000-0 10270-3 0 9034
2 25544 51
6499 307
8376 0003452 166
4054 193
7191 15
50612447 33541
Satellite: ISS
Catalog Number: 25544
Epoch time: 14053
55869503 = yrday
fracday
Element set: 903
Inclination: 51
6499 deg
RA of node: 307
8376 deg
Eccentricity:
0003452
Arg of perigee: 166
4054 deg
Mean anomaly: 193
7191 deg
Mean motion: 15
50612447 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3354
Checksum: 319
Coasting Arc #5 (Orbit 3368)
---------------------------------------
Vector Time (GMT): 2014/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5082921
36 A = 6794856
81 meter
Y = 3099696
69 meter E =
0006330
Z = -3275124
19 I = 51
35501
XDOT = -635
124392 Wp = 127
51337
YDOT = -6006
694376 meter/sec RA = 302
52911 deg
ZDOT = -4709
312874 TA = 90
59350
MA = 90
52097
Ha = 226
917 n
mi
Hp = 219
845
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16676251
18 X = -5101295
77
Y = 10169608
57 feet Y = 3042753
29 meter
Z = -10745158
10 Z = -3299860
83
XDOT = -2083
741445 XDOT = -545
032915
YDOT = -19707
002545 feet/sec YDOT = -6013
293276 meter/sec
ZDOT = -15450
501554 ZDOT = -4712
179025
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19428041
10 X = -5921666
93
Y = 1343440
97 feet Y = 409480
81 meter
Z = -10850027
64 Z = -3307088
42
XDOT = 7442
506828 XDOT = 2268
476081
YDOT = -16979
539914 feet/sec YDOT = -5175
363766 meter/sec
ZDOT = -15461
611676 ZDOT = -4712
699239
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 14054
52539479
00016717 00000-0 10270-3 0 9049
2 25544 51
6502 303
0441 0003475 174
3908 185
7283 15
50644570 33699
Satellite: ISS
Catalog Number: 25544
Epoch time: 14054
52539479 = yrday
fracday
Element set: 904
Inclination: 51
6502 deg
RA of node: 303
0441 deg
Eccentricity:
0003475
Arg of perigee: 174
3908 deg
Mean anomaly: 185
7283 deg
Mean motion: 15
50644570 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3369
Checksum: 312
Coasting Arc #6 (Orbit 3384)
---------------------------------------
Vector Time (GMT): 2014/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4872430
70 A = 6793533
50 meter
Y = -2960986
27 meter E =
0012710
Z = 3687371
98 I = 51
33495
XDOT = 578
574953 Wp = 110
31655
YDOT = 6320
898499 meter/sec RA = 297
54953 deg
ZDOT = 4294
798230 TA = 293
75062
MA = 293
88388
Ha = 226
811 n
mi
Hp = 219
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15985665
03 X = 4887267
19
Y = -9714521
88 feet Y = -2906416
48 meter
Z = 12097677
09 Z = 3711077
39
XDOT = 1898
211788 XDOT = 486
987816
YDOT = 20737
855969 feet/sec YDOT = 6326
856629 meter/sec
ZDOT = 14090
545375 ZDOT = 4297
386033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18573302
53 X = 5661142
61
Y = -1582483
16 feet Y = -482340
87 meter
Z = 12198171
71 Z = 3718002
74
XDOT = -7761
282825 XDOT = -2365
639005
YDOT = 18008
552047 feet/sec YDOT = 5489
006664 meter/sec
ZDOT = 14100
438860 ZDOT = 4297
813764
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 14055
55651901
00016717 00000-0 10270-3 0 9059
2 25544 51
6501 297
9306 0003347 175
6533 184
4648 15
50681097 33859
Satellite: ISS
Catalog Number: 25544
Epoch time: 14055
55651901 = yrday
fracday
Element set: 905
Inclination: 51
6501 deg
RA of node: 297
9306 deg
Eccentricity:
0003347
Arg of perigee: 175
6533 deg
Mean anomaly: 184
4648 deg
Mean motion: 15
50681097 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3385
Checksum: 322
Coasting Arc #7 (Orbit 3399)
---------------------------------------
Vector Time (GMT): 2014/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4685521
56 A = 6792060
54 meter
Y = 2727960
57 meter E =
0006900
Z = -4096310
55 I = 51
31662
XDOT = -541
111216 Wp = 97
36714
YDOT = -6625
655164 meter/sec RA = 292
56770 deg
ZDOT = -3799
840147 TA = 133
18817
MA = 133
13050
Ha = 226
594 n
mi
Hp = 219
914
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15372446
08 X = -4695779
82
Y = 8950001
87 feet Y = 2675506
47 meter
Z = -13439339
06 Z = -4119096
79
XDOT = -1775
299265 XDOT = -448
523391
YDOT = -21737
713792 feet/sec YDOT = -6631
188755 meter/sec
ZDOT = -12466
667149 ZDOT = -3802
243456
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17652736
55 X = -5380554
10
Y = 1479977
63 feet Y = 451097
18 meter
Z = -13535916
10 Z = -4125747
23
XDOT = 7952
526139 XDOT = 2423
929967
YDOT = -19057
659063 feet/sec YDOT = -5808
774482 meter/sec
ZDOT = -12475
745017 ZDOT = -3802
607081
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 14056
52317375
00016717 00000-0 10270-3 0 9062
2 25544 51
6497 293
1369 0003365 184
2257 175
8866 15
50724561 34007
Satellite: ISS
Catalog Number: 25544
Epoch time: 14056
52317375 = yrday
fracday
Element set: 906
Inclination: 51
6497 deg
RA of node: 293
1369 deg
Eccentricity:
0003365
Arg of perigee: 184
2257 deg
Mean anomaly: 175
8866 deg
Mean motion: 15
50724561 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3400
Checksum: 323
Coasting Arc #8 (Orbit 3415)
---------------------------------------
Vector Time (GMT): 2014/057/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4508580
20 A = 6790764
49 meter
Y = -2469546
22 meter E =
0010494
Z = 4433679
66 I = 51
30121
XDOT = 557
965560 Wp = 128
17403
YDOT = 6909
197390 meter/sec RA = 287
58345 deg
ZDOT = 3269
345983 TA = 288
63546
MA = 288
74938
Ha = 226
486 n
mi
Hp = 219
992
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14791929
78 X = 4514323
22
Y = -8102185
77 feet Y = -2419095
94 meter
Z = 14546193
11 Z = 4455595
35
XDOT = 1830
595669 XDOT = 464
782820
YDOT = 22667
970439 feet/sec YDOT = 6914
916153 meter/sec
ZDOT = 10726
200732 ZDOT = 3271
829583
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16737914
56 X = 5101716
36
Y = -1256451
78 feet Y = -382966
50 meter
Z = 14639053
25 Z = 4461983
43
XDOT = -7911
586824 XDOT = -2411
451664
YDOT = 20129
736923 feet/sec YDOT = 6135
543814 meter/sec
ZDOT = 10735
587027 ZDOT = 3272
206926
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 14057
55425063
00016717 00000-0 10270-3 0 9071
2 25544 51
6495 288
0233 0003258 185
4887 174
6229 15
50747552 34163
Satellite: ISS
Catalog Number: 25544
Epoch time: 14057
55425063 = yrday
fracday
Element set: 907
Inclination: 51
6495 deg
RA of node: 288
0233 deg
Eccentricity:
0003258
Arg of perigee: 185
4887 deg
Mean anomaly: 174
6229 deg
Mean motion: 15
50747552 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3416
Checksum: 328
Coasting Arc #9 (Orbit 3430)
---------------------------------------
Vector Time (GMT): 2014/058/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4373409
12 A = 6789399
05 meter
Y = 2126696
95 meter E =
0009817
Z = -4746472
64 I = 51
28748
XDOT = -590
437145 Wp = 87
67101
YDOT = -7152
170180 meter/sec RA = 282
59649 deg
ZDOT = -2664
965002 TA = 155
85587
MA = 155
80982
Ha = 226
282 n
mi
Hp = 219
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14348455
13 X = -4373808
99
Y = 6977352
19 feet Y = 2077787
98 meter
Z = -15572416
80 Z = -4767718
72
XDOT = -1937
129741 XDOT = -497
470852
YDOT = -23465
125261 feet/sec YDOT = -7158
253285 meter/sec
ZDOT = -8743
323499 ZDOT = -2667
606683
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15851521
19 X = -4831543
66
Y = 693146
06 feet Y = 211270
92 meter
Z = -15662394
38 Z = -4773897
81
XDOT = 7711
907779 XDOT = 2350
589491
YDOT = -21103
751215 feet/sec YDOT = -6432
423370 meter/sec
ZDOT = -8753
355450 ZDOT = -2668
022741
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 14058
52086023
00016717 00000-0 10270-3 0 9089
2 25544 51
6482 283
2288 0003284 193
6145 166
4918 15
50805045 34316
Satellite: ISS
Catalog Number: 25544
Epoch time: 14058
52086023 = yrday
fracday
Element set: 908
Inclination: 51
6482 deg
RA of node: 283
2288 deg
Eccentricity:
0003284
Arg of perigee: 193
6145 deg
Mean anomaly: 166
4918 deg
Mean motion: 15
50805045 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3431
Checksum: 309
Coasting Arc #10 (Orbit 3446)
---------------------------------------
Vector Time (GMT): 2014/059/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4262704
27 A = 6788388
51 meter
Y = -1763324
84 meter E =
0007632
Z = 4978581
23 I = 51
27808
XDOT = 661
267424 Wp = 146
98892
YDOT = 7359
944219 meter/sec RA = 277
60802 deg
ZDOT = 2032
812502 TA = 283
09370
MA = 283
17888
Ha = 226
156 n
mi
Hp = 220
112
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13985250
24 X = 4257921
54
Y = -5785186
49 feet Y = -1715682
69 meter
Z = 16333927
92 Z = 4999276
98
XDOT = 2169
512546 XDOT = 569
043197
YDOT = 24146
798620 feet/sec YDOT = 7366
823528 meter/sec
ZDOT = 6669
332355 ZDOT = 2035
799874
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15039492
43 X = 4584037
29
Y = -6350
68 feet Y = -1935
69 meter
Z = 16421523
55 Z = 5005280
38
XDOT = -7313
105883 XDOT = -2229
034673
YDOT = 22014
917323 feet/sec YDOT = 6710
146800 meter/sec
ZDOT = 6680
808064 ZDOT = 2036
310298
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 14059
55188913
00016717 00000-0 10270-3 0 9095
2 25544 51
6479 278
1147 0003221 195
5721 164
5332 15
50815304 34476
Satellite: ISS
Catalog Number: 25544
Epoch time: 14059
55188913 = yrday
fracday
Element set: 909
Inclination: 51
6479 deg
RA of node: 278
1147 deg
Eccentricity:
0003221
Arg of perigee: 195
5721 deg
Mean anomaly: 164
5332 deg
Mean motion: 15
50815304 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3447
Checksum: 315
Coasting Arc #11 (Orbit 3461)
---------------------------------------
Vector Time (GMT): 2014/060/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4208393
55 A = 6787419
72 meter
Y = 1335021
43 meter E =
0012475
Z = -5165955
07 I = 51
27064
XDOT = -735
114129 Wp = 92
40558
YDOT = -7499
496723 meter/sec RA = 272
61660 deg
ZDOT = -1342
553302 TA = 164
61969
MA = 164
58174
Ha = 225
995 n
mi
Hp = 220
005
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13807065
44 X = -4197915
19
Y = 4379991
57 feet Y = 1288018
34 meter
Z = -16948671
50 Z = -5186373
21
XDOT = -2411
791763 XDOT = -644
676865
YDOT = -24604
648040 feet/sec YDOT = -7507
211764 meter/sec
ZDOT = -4404
702433 ZDOT = -1345
903605
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14350443
16 X = -4374015
08
Y = -974410
98 feet Y = -297000
47 meter
Z = -17035027
22 Z = -5192276
30
XDOT = 6773
076450 XDOT = 2064
433702
YDOT = -22707
466707 feet/sec YDOT = -6921
235852 meter/sec
ZDOT = -4417
704354 ZDOT = -1346
516287
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 14060
51845336
00016717 00000-0 10270-3 0 9104
2 25544 51
6462 273
3189 0003249 202
2291 157
8719 15
50882783 34625
Satellite: ISS
Catalog Number: 25544
Epoch time: 14060
51845336 = yrday
fracday
Element set: 910
Inclination: 51
6462 deg
RA of node: 273
3189 deg
Eccentricity:
0003249
Arg of perigee: 202
2291 deg
Mean anomaly: 157
8719 deg
Mean motion: 15
50882783 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3462
Checksum: 313
Coasting Arc #12 (Orbit 3477)
---------------------------------------
Vector Time (GMT): 2014/061/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4188331
92 A = 6786933
02 meter
Y = -896703
77 meter E =
0004388
Z = 5263888
91 I = 51
26872
XDOT = 823
733907 Wp = 162
88732
YDOT = 7593
427304 meter/sec RA = 267
62523 deg
ZDOT = 633
862694 TA = 281
00214
MA = 281
05149
Ha = 225
821 n
mi
Hp = 220
214
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13741246
46 X = 4172477
85
Y = -2941941
51 feet Y = -849955
02 meter
Z = 17269976
75 Z = 5284196
58
XDOT = 2702
539065 XDOT = 735
682216
YDOT = 24912
819240 feet/sec YDOT = 7602
146594 meter/sec
ZDOT = 2079
602013 ZDOT = 637
649225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13795106
10 X = 4204748
34
Y = 2049459
46 feet Y = 624675
24 meter
Z = 17355798
30 Z = 5290047
32
XDOT = -6107
824824 XDOT = -1861
665007
YDOT = 23257
945172 feet/sec YDOT = 7089
021688 meter/sec
ZDOT = 2094
444274 ZDOT = 638
386615
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 14061
54943325
00016717 00000-0 10270-3 0 9116
2 25544 51
6463 268
2043 0003241 205
4783 154
6209 15
50888059 34789
Satellite: ISS
Catalog Number: 25544
Epoch time: 14061
54943325 = yrday
fracday
Element set: 911
Inclination: 51
6463 deg
RA of node: 268
2043 deg
Eccentricity:
0003241
Arg of perigee: 205
4783 deg
Mean anomaly: 154
6209 deg
Mean motion: 15
50888059 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3478
Checksum: 309
Coasting Arc #13 (Orbit 3492)
---------------------------------------
Vector Time (GMT): 2014/062/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4231993
73 A = 6786607
99 meter
Y = 421039
59 meter E =
0013560
Z = -5300312
73 I = 51
26912
XDOT = -895
258039 Wp = 102
92188
YDOT = -7600
297769 meter/sec RA = 262
63144 deg
ZDOT = 108
329231 TA = 168
13375
MA = 168
10176
Ha = 225
725 n
mi
Hp = 220
037
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13884493
87 X = -4210640
38
Y = 1381363
49 feet Y = 373833
34 meter
Z = -17389477
46 Z = -5320819
16
XDOT = -2937
198291 XDOT = -810
729488
YDOT = -24935
360135 feet/sec YDOT = -7609
836476 meter/sec
ZDOT = 355
410863 ZDOT = 104
186661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13438090
29 X = -4095929
92
Y = -3329578
35 feet Y = -1014855
48 meter
Z = -17476066
47 Z = -5326705
06
XDOT = 5368
340507 XDOT = 1636
270187
YDOT = -23493
039901 feet/sec YDOT = -7160
678562 meter/sec
ZDOT = 339
056055 ZDOT = 103
344286
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 14062
51595177
00016717 00000-0 10270-3 0 9123
2 25544 51
6450 263
4077 0003246 210
0958 150
0007 15
50957486 34934
Satellite: ISS
Catalog Number: 25544
Epoch time: 14062
51595177 = yrday
fracday
Element set: 912
Inclination: 51
6450 deg
RA of node: 263
4077 deg
Eccentricity:
0003246
Arg of perigee: 210
0958 deg
Mean anomaly: 150
0007 deg
Mean motion: 15
50957486 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3493
Checksum: 301
Coasting Arc #14 (Orbit 3508)
---------------------------------------
Vector Time (GMT): 2014/063/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4312093
67 A = 6786806
63 meter
Y = 50038
85 meter E =
0001460
Z = 5239600
61 I = 51
27526
XDOT = 952
524343 Wp = 135
69642
YDOT = 7556
694040 meter/sec RA = 257
63946 deg
ZDOT = -856
958419 TA = 322
53817
MA = 322
54834
Ha = 225
486 n
mi
Hp = 220
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14147288
95 X = 4285761
50
Y = 164169
46 feet Y = 98112
93 meter
Z = 17190290
71 Z = 5260484
05
XDOT = 3125
079866 XDOT = 872
115702
YDOT = 24792
303282 feet/sec YDOT = 7566
896071 meter/sec
ZDOT = -2811
543371 ZDOT = -852
527552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13249285
58 X = 4038382
25
Y = 4646726
48 feet Y = 1416322
23 meter
Z = 17278402
57 Z = 5266457
10
XDOT = -4612
118682 XDOT = -1405
773774
YDOT = 23528
968235 feet/sec YDOT = 7171
629518 meter/sec
ZDOT = -2793
956379 ZDOT = -851
597904
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 14063
54688147
00016717 00000-0 10270-3 0 9138
2 25544 51
6454 258
2930 0003275 214
7439 145
3499 15
50966669 35098
Satellite: ISS
Catalog Number: 25544
Epoch time: 14063
54688147 = yrday
fracday
Element set: 913
Inclination: 51
6454 deg
RA of node: 258
2930 deg
Eccentricity:
0003275
Arg of perigee: 214
7439 deg
Mean anomaly: 145
3499 deg
Mean motion: 15
50966669 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3509
Checksum: 340
Coasting Arc #15 (Orbit 3523)
---------------------------------------
Vector Time (GMT): 2014/064/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4452915
40 A = 6787240
20 meter
Y = -526233
14 meter E =
0012481
Z = -5106319
66 I = 51
28407
XDOT = -968
893244 Wp = 115
80302
YDOT = -7420
339675 meter/sec RA = 252
64623 deg
ZDOT = 1607
369787 TA = 169
82314
MA = 169
79784
Ha = 225
463 n
mi
Hp = 220
063
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14609302
49 X = -4421895
25
Y = -1726486
67 feet Y = -575855
66 meter
Z = -16753017
26 Z = -5127875
78
XDOT = -3178
783609 XDOT = -893
653377
YDOT = -24344
946439 feet/sec YDOT = -7430
753577 meter/sec
ZDOT = 5273
522924 ZDOT = 1602
846703
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13295993
66 X = -4052618
87
Y = -6047776
24 feet Y = -1843362
20 meter
Z = -16843901
51 Z = -5134021
18
XDOT = 3886
218138 XDOT = 1184
519289
YDOT = -23201
616644 feet/sec YDOT = -7071
852753 meter/sec
ZDOT = 5255
518615 ZDOT = 1601
882074
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 14064
51335342
00016717 00000-0 10270-3 0 9143
2 25544 51
6446 253
4962 0003235 217
4541 142
6385 15
51031235 35245
Satellite: ISS
Catalog Number: 25544
Epoch time: 14064
51335342 = yrday
fracday
Element set: 914
Inclination: 51
6446 deg
RA of node: 253
4962 deg
Eccentricity:
0003235
Arg of perigee: 217
4541 deg
Mean anomaly: 142
6385 deg
Mean motion: 15
51031235 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3524
Checksum: 282
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