[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 7th 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) : 132 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 252 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 3791)
---------------------------------------
Vector Time (GMT): 2014/339/13:00:52
258
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1391439
61 A = 6787726
77 meter
Y = 4933367
10 meter E =
0016087
Z = 4437125
53 I = 51
45488
XDOT = -6859
551861 Wp = 81
62173
YDOT = 1026
557427 meter/sec RA = 329
35524 deg
ZDOT = -3279
956046 TA = 41
57312
MA = 41
45090
Ha = 227
321 n
mi
Hp = 215
632
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4565090
57 X = -1468056
70
Y = 16185587
61 feet Y = 4917378
40 meter
Z = 14557498
46 Z = 4430180
29
XDOT = -22505
091407 XDOT = -6854
588036
YDOT = 3367
970561 feet/sec YDOT = 949
877474 meter/sec
ZDOT = -10761
010650 ZDOT = -3313
267147
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16071611
36 X = -4898627
14
Y = -5040502
31 feet Y = -1536345
10 meter
Z = 14526895
89 Z = 4427797
87
XDOT = -3200
087224 XDOT = -975
386586
YDOT = -21338
440182 feet/sec YDOT = -6503
956568 meter/sec
ZDOT = -10903
227304 ZDOT = -3323
303682
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 14339
58461381
00016717 00000-0 10270-3 0 9003
2 25544 51
6433 329
7510 0007310 97
8404 262
3577 15
51823685 37921
Satellite: ISS
Catalog Number: 25544
Epoch time: 14339
58461381 = yrday
fracday
Element set: 900
Inclination: 51
6433 deg
RA of node: 329
7510 deg
Eccentricity:
0007310
Arg of perigee: 97
8404 deg
Mean anomaly: 262
3577 deg
Mean motion: 15
51823685 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3792
Checksum: 318
Coasting Arc #2 (Orbit 3806)
---------------------------------------
Vector Time (GMT): 2014/340/13:00:52
258
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1995720
18 A = 6789746
15 meter
Y = -5222721
43 meter E =
0013640
Z = -3866360
11 I = 51
43547
XDOT = 6430
380856 Wp = 102
31902
YDOT = -577
824080 meter/sec RA = 324
37192 deg
ZDOT = 4109
202253 TA = 211
01024
MA = 211
09083
Ha = 227
309 n
mi
Hp = 215
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6547638
39 X = 2072755
29
Y = -17134912
83 feet Y = -5199972
92 meter
Z = -12684908
49 Z = -3856478
42
XDOT = 21097
050051 XDOT = 6416
402882
YDOT = -1895
748294 feet/sec YDOT = -505
993912 meter/sec
ZDOT = 13481
634689 ZDOT = 4140
406500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17092108
46 X = 5209674
66
Y = 6740192
04 feet Y = 2054410
53 meter
Z = -12641730
48 Z = -3853199
45
XDOT = 2247
753618 XDOT = 685
115303
YDOT = 19777
115815 feet/sec YDOT = 6028
064901 meter/sec
ZDOT = 13614
779499 ZDOT = 4149
784791
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 14340
55056934
00016717 00000-0 10270-3 0 9017
2 25544 51
6436 324
9522 0007401 101
0620 259
1364 15
51832581 38073
Satellite: ISS
Catalog Number: 25544
Epoch time: 14340
55056934 = yrday
fracday
Element set: 901
Inclination: 51
6436 deg
RA of node: 324
9522 deg
Eccentricity:
0007401
Arg of perigee: 101
0620 deg
Mean anomaly: 259
1364 deg
Mean motion: 15
51832581 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3807
Checksum: 284
Coasting Arc #3 (Orbit 3822)
---------------------------------------
Vector Time (GMT): 2014/341/13:00:52
258
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2551644
88 A = 6791773
83 meter
Y = 5458797
20 meter E =
0020244
Z = 3112614
18 I = 51
41819
XDOT = -5944
382387 Wp = 98
31723
YDOT =
467262 meter/sec RA = 319
38942 deg
ZDOT = -4849
680522 TA = 45
73180
MA = 45
56585
Ha = 227
184 n
mi
Hp = 215
565
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8371538
33 X = -2627616
98
Y = 17909439
64 feet Y = 5429837
97 meter
Z = 10211988
79 Z = 3100034
54
XDOT = -19502
566888 XDOT = -5920
387441
YDOT = 1
533012 feet/sec YDOT = -65
872050 meter/sec
ZDOT = -15911
025335 ZDOT = -4878
499438
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17998987
30 X = -5486091
33
Y = -8245109
63 feet Y = -2513109
42 meter
Z = 10157264
43 Z = 3095934
20
XDOT = -807
431112 XDOT = -246
105003
YDOT = -18088
081131 feet/sec YDOT = -5513
247129 meter/sec
ZDOT = -16033
886493 ZDOT = -4887
128603
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 14341
58089718
00016717 00000-0 10270-3 0 9028
2 25544 51
6439 319
8327 0007322 104
6830 255
5133 15
51895553 38236
Satellite: ISS
Catalog Number: 25544
Epoch time: 14341
58089718 = yrday
fracday
Element set: 902
Inclination: 51
6439 deg
RA of node: 319
8327 deg
Eccentricity:
0007322
Arg of perigee: 104
6830 deg
Mean anomaly: 255
5133 deg
Mean motion: 15
51895553 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3823
Checksum: 318
Coasting Arc #4 (Orbit 3837)
---------------------------------------
Vector Time (GMT): 2014/342/13:00:52
258
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2977633
00 A = 6793554
51 meter
Y = -5660113
27 meter E =
0011299
Z = -2297149
46 I = 51
40151
XDOT = 5391
008691 Wp = 79
83027
YDOT = 655
017631 meter/sec RA = 314
40893 deg
ZDOT = 5398
716727 TA = 254
54174
MA = 254
66656
Ha = 227
138 n
mi
Hp = 215
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9769137
14 X = 3051863
26
Y = -18569925
44 feet Y = -5626400
19 meter
Z = -7536579
59 Z = -2282504
71
XDOT = 17687
036387 XDOT = 5357
058127
YDOT = 2149
007977 feet/sec YDOT = 715
113048 meter/sec
ZDOT = 17712
325220 ZDOT = 5424
823191
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18836549
52 X = 5741380
29
Y = 9296055
15 feet Y = 2833437
61 meter
Z = -7473015
71 Z = -2277775
19
XDOT = -982
950070 XDOT = -299
603181
YDOT = 16254
255231 feet/sec YDOT = 4954
296995 meter/sec
ZDOT = 17823
493661 ZDOT = 5432
600868
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 14342
54680658
00016717 00000-0 10270-3 0 9036
2 25544 51
6442 315
0340 0007387 108
3116 251
8839 15
51920781 38382
Satellite: ISS
Catalog Number: 25544
Epoch time: 14342
54680658 = yrday
fracday
Element set: 903
Inclination: 51
6442 deg
RA of node: 315
0340 deg
Eccentricity:
0007387
Arg of perigee: 108
3116 deg
Mean anomaly: 251
8839 deg
Mean motion: 15
51920781 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3838
Checksum: 312
Coasting Arc #5 (Orbit 3853)
---------------------------------------
Vector Time (GMT): 2014/343/13:00:52
258
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3347856
51 A = 6794916
37 meter
Y = 5749190
45 meter E =
0021053
Z = 1334081
76 I = 51
38601
XDOT = -4809
882865 Wp = 117
25229
YDOT = -1441
339796 meter/sec RA = 309
42907 deg
ZDOT = -5797
792772 TA = 48
17401
MA = 47
99443
Ha = 227
013 n
mi
Hp = 215
537
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10983781
22 X = -3418377
03
Y = 18862173
39 feet Y = 5711358
13 meter
Z = 4376908
67 Z = 1317647
54
XDOT = -15780
455595 XDOT = -4765
244152
YDOT = -4728
805105 feet/sec YDOT = -1494
876939 meter/sec
ZDOT = -19021
629829 ZDOT = -5821
050225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19339103
96 X = -5894558
89
Y = -10150976
78 feet Y = -3094017
72 meter
Z = 4305704
67 Z = 1312378
78
XDOT = 3280
633969 XDOT = 999
937234
YDOT = -14446
820131 feet/sec YDOT = -4403
390776 meter/sec
ZDOT = -19120
498780 ZDOT = -5827
928028
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 14343
57708567
00016717 00000-0 10270-3 0 9041
2 25544 51
6451 309
9145 0007331 112
1534 248
0396 15
51960543 38547
Satellite: ISS
Catalog Number: 25544
Epoch time: 14343
57708567 = yrday
fracday
Element set: 904
Inclination: 51
6451 deg
RA of node: 309
9145 deg
Eccentricity:
0007331
Arg of perigee: 112
1534 deg
Mean anomaly: 248
0396 deg
Mean motion: 15
51960543 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3854
Checksum: 312
Coasting Arc #6 (Orbit 3868)
---------------------------------------
Vector Time (GMT): 2014/344/13:00:52
258
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3587085
97 A = 6795445
44 meter
Y = -5756107
53 meter E =
0015188
Z = -373076
32 I = 51
36891
XDOT = 4233
584247 Wp = 69
93432
YDOT = 2264
455407 meter/sec RA = 304
44986 deg
ZDOT = 5971
224379 TA = 286
03394
MA = 286
20116
Ha = 226
922 n
mi
Hp = 215
496
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11768654
77 X = 3652997
79
Y = -18884867
23 feet Y = -5715625
85 meter
Z = -1224003
69 Z = -355491
11
XDOT = 13889
712095 XDOT = 4178
941676
YDOT = 7429
315640 feet/sec YDOT = 2311
492136 meter/sec
ZDOT = 19590
631165 ZDOT = 5991
657953
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19580785
54 X = 5968223
43
Y = 10578884
38 feet Y = 3224443
96 meter
Z = -1147899
53 Z = -349879
78
XDOT = -5789
214600 XDOT = -1764
552610
YDOT = 12773
324046 feet/sec YDOT = 3893
309169 meter/sec
ZDOT = 19677
302566 ZDOT = 5997
641822
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 14344
54294860
00016717 00000-0 10270-3 0 9056
2 25544 51
6450 305
1158 0007323 115
9975 244
1932 15
52007210 38692
Satellite: ISS
Catalog Number: 25544
Epoch time: 14344
54294860 = yrday
fracday
Element set: 905
Inclination: 51
6450 deg
RA of node: 305
1158 deg
Eccentricity:
0007323
Arg of perigee: 115
9975 deg
Mean anomaly: 244
1932 deg
Mean motion: 15
52007210 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3869
Checksum: 302
Coasting Arc #7 (Orbit 3884)
---------------------------------------
Vector Time (GMT): 2014/345/13:00:52
258
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3783138
60 A = 6795212
62 meter
Y = 5595977
45 meter E =
0017546
Z = -676133
92 I = 51
35237
XDOT = -3659
637900 Wp = 131
28157
YDOT = -3178
228121 meter/sec RA = 299
46948 deg
ZDOT = -5939
721496 TA = 56
04518
MA = 55
87852
Ha = 226
789 n
mi
Hp = 215
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12411872
06 X = -3842148
52
Y = 18359506
07 feet Y = 5553342
04 meter
Z = -2218287
14 Z = -694654
85
XDOT = -12006
686024 XDOT = -3594
973016
YDOT = -10427
257615 feet/sec YDOT = -3218
790659 meter/sec
ZDOT = -19487
275250 ZDOT = -5957
342588
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19285151
97 X = -5878114
32
Y = -10901714
35 feet Y = -3322842
53 meter
Z = -2298340
00 Z = -700534
03
XDOT = 8658
263594 XDOT = 2639
038744
YDOT = -11267
110973 feet/sec YDOT = -3434
215425 meter/sec
ZDOT = -19561
782498 ZDOT = -5962
431305
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 14345
57317828
00016717 00000-0 10270-3 0 9061
2 25544 51
6459 299
9961 0007283 119
6848 240
5029 15
52035276 38856
Satellite: ISS
Catalog Number: 25544
Epoch time: 14345
57317828 = yrday
fracday
Element set: 906
Inclination: 51
6459 deg
RA of node: 299
9961 deg
Eccentricity:
0007283
Arg of perigee: 119
6848 deg
Mean anomaly: 240
5029 deg
Mean motion: 15
52035276 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3885
Checksum: 351
Coasting Arc #8 (Orbit 3900)
---------------------------------------
Vector Time (GMT): 2014/346/13:00:52
258
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3875042
52 A = 6794118
26 meter
Y = -5324675
96 meter E =
0018705
Z = 1648999
20 I = 51
33409
XDOT = 3146
385360 Wp = 83
30805
YDOT = 4066
998161 meter/sec RA = 294
48707 deg
ZDOT = 5685
138713 TA = 294
81699
MA = 295
01142
Ha = 226
702 n
mi
Hp = 215
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12713394
10 X = 3926285
99
Y = -17469409
31 feet Y = -5281056
27 meter
Z = 5410102
37 Z = 1667947
81
XDOT = 10322
786615 XDOT = 3073
056852
YDOT = 13343
169818 feet/sec YDOT = 4101
772818 meter/sec
ZDOT = 18652
029899 ZDOT = 5700
245468
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18610733
58 X = 5672551
60
Y = 10934317
83 feet Y = 3332780
07 meter
Z = 5491916
61 Z = 1673936
18
XDOT = -11500
676248 XDOT = -3505
406121
YDOT = 10087
595266 feet/sec YDOT = 3074
699037 meter/sec
ZDOT = 18715
651907 ZDOT = 5704
530701
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 14346
60338225
00016717 00000-0 10270-3 0 9071
2 25544 51
6455 294
8770 0007264 123
5111 236
6736 15
52077214 39018
Satellite: ISS
Catalog Number: 25544
Epoch time: 14346
60338225 = yrday
fracday
Element set: 907
Inclination: 51
6455 deg
RA of node: 294
8770 deg
Eccentricity:
0007264
Arg of perigee: 123
5111 deg
Mean anomaly: 236
6736 deg
Mean motion: 15
52077214 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3901
Checksum: 303
Coasting Arc #9 (Orbit 3915)
---------------------------------------
Vector Time (GMT): 2014/347/13:00:52
258
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3953763
52 A = 6792182
80 meter
Y = 4854699
60 meter E =
0012231
Z = -2630735
03 I = 51
31656
XDOT = -2655
197132 Wp = 126
10614
YDOT = -4965
120690 meter/sec RA = 289
50079 deg
ZDOT = -5196
034489 TA = 83
64546
MA = 83
50618
Ha = 226
560 n
mi
Hp = 215
498
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12971665
08 X = -3994976
78
Y = 15927492
12 feet Y = 4810255
71 meter
Z = -8631020
44 Z = -2650041
78
XDOT = -8711
276681 XDOT = -2574
237986
YDOT = -16289
766042 feet/sec YDOT = -4994
359965 meter/sec
ZDOT = -17047
357246 ZDOT = -5208
736605
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17290859
93 X = -5270254
11
Y = -11024128
26 feet Y = -3360154
29 meter
Z = -8714262
64 Z = -2656107
25
XDOT = 14404
719256 XDOT = 4390
558429
YDOT = -9137
404614 feet/sec YDOT = -2785
080926 meter/sec
ZDOT = -17100
562716 ZDOT = -5212
251516
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 14347
56917533
00016717 00000-0 10270-3 0 9083
2 25544 51
6461 290
0770 0007259 126
7994 233
3825 15
52120825 39167
Satellite: ISS
Catalog Number: 25544
Epoch time: 14347
56917533 = yrday
fracday
Element set: 908
Inclination: 51
6461 deg
RA of node: 290
0770 deg
Eccentricity:
0007259
Arg of perigee: 126
7994 deg
Mean anomaly: 233
3825 deg
Mean motion: 15
52120825 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3916
Checksum: 324
Coasting Arc #10 (Orbit 3931)
---------------------------------------
Vector Time (GMT): 2014/348/13:00:52
258
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3971855
12 A = 6789947
20 meter
Y = -4273562
14 meter E =
0018468
Z = 3462911
30 I = 51
29930
XDOT = 2247
144426 Wp = 105
67200
YDOT = 5771
770439 meter/sec RA = 284
51053 deg
ZDOT = 4520
416653 TA = 295
17298
MA = 295
36440
Ha = 226
477 n
mi
Hp = 215
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13031020
73 X = 4002526
15
Y = -14020873
15 feet Y = -4228974
89 meter
Z = 11361257
55 Z = 3482280
42
XDOT = 7372
521083 XDOT = 2160
477350
YDOT = 18936
254721 feet/sec YDOT = 5796
414738 meter/sec
ZDOT = 14830
763297 ZDOT = 4531
122664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15592912
13 X = 4752719
62
Y = 11015974
14 feet Y = 3357668
92 meter
Z = 11444647
80 Z = 3488328
65
XDOT = -17020
891962 XDOT = -5187
967870
YDOT = 8553
698005 feet/sec YDOT = 2607
167152 meter/sec
ZDOT = 14875
313851 ZDOT = 4533
995662
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 14348
59933055
00016717 00000-0 10270-3 0 9095
2 25544 51
6457 284
9574 0007283 130
8128 229
3656 15
52147931 39320
Satellite: ISS
Catalog Number: 25544
Epoch time: 14348
59933055 = yrday
fracday
Element set: 909
Inclination: 51
6457 deg
RA of node: 284
9574 deg
Eccentricity:
0007283
Arg of perigee: 130
8128 deg
Mean anomaly: 229
3656 deg
Mean motion: 15
52147931 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3932
Checksum: 339
Coasting Arc #11 (Orbit 3946)
---------------------------------------
Vector Time (GMT): 2014/349/13:00:52
258
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4013843
81 A = 6787333
08 meter
Y = 3501426
67 meter E =
0013030
Z = -4216447
75 I = 51
28482
XDOT = -1859
653440 Wp = 99
92899
YDOT = -6482
695783 meter/sec RA = 279
51460 deg
ZDOT = -3624
880524 TA = 132
77035
MA = 132
66067
Ha = 226
347 n
mi
Hp = 215
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13168778
91 X = -4032217
02
Y = 11487620
29 feet Y = 3456438
66 meter
Z = -13833489
98 Z = -4235991
04
XDOT = -6101
225198 XDOT = -1769
415624
YDOT = -21268
686952 feet/sec YDOT = -6502
986973 meter/sec
ZDOT = -11892
652637 ZDOT = -3633
695518
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13292440
06 X = -4051535
73
Y = -11241112
68 feet Y = -3426291
14 meter
Z = -13917471
97 Z = -4242045
46
XDOT = 19326
752511 XDOT = 5890
794165
YDOT = -8132
106876 feet/sec YDOT = -2478
666176 meter/sec
ZDOT = -11929
016062 ZDOT = -3635
964096
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 14349
56507769
00016717 00000-0 10270-3 0 9104
2 25544 51
6464 280
1569 0007259 134
0706 226
1044 15
52202241 39479
Satellite: ISS
Catalog Number: 25544
Epoch time: 14349
56507769 = yrday
fracday
Element set: 910
Inclination: 51
6464 deg
RA of node: 280
1569 deg
Eccentricity:
0007259
Arg of perigee: 134
0706 deg
Mean anomaly: 226
1044 deg
Mean motion: 15
52202241 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3947
Checksum: 307
Coasting Arc #12 (Orbit 3962)
---------------------------------------
Vector Time (GMT): 2014/350/13:00:52
258
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4037897
29 A = 6785139
57 meter
Y = -2649924
65 meter E =
0014506
Z = 4759549
92 I = 51
27318
XDOT = 1538
511567 Wp = 128
40905
YDOT = 7047
730321 meter/sec RA = 274
51474 deg
ZDOT = 2604
379910 TA = 295
71296
MA = 295
86265
Ha = 226
187 n
mi
Hp = 215
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13247694
52 X = 4044108
74
Y = -8693978
52 feet Y = -2604735
71 meter
Z = 15615321
27 Z = 4779180
58
XDOT = 5047
610129 XDOT = 1446
936529
YDOT = 23122
474808 feet/sec YDOT = 7064
422836 meter/sec
ZDOT = 8544
553509 ZDOT = 2611
631658
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10739319
21 X = 3273344
50
Y = 11537643
91 feet Y = 3516673
86 meter
Z = 15699513
59 Z = 4785211
74
XDOT = -21143
797697 XDOT = -6444
629538
YDOT = 7950
389978 feet/sec YDOT = 2423
278865 meter/sec
ZDOT = 8574
155467 ZDOT = 2613
402586
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 14350
59518398
00016717 00000-0 10270-3 0 9110
2 25544 51
6461 275
0367 0007275 138
7210 221
4493 15
52234022 39630
Satellite: ISS
Catalog Number: 25544
Epoch time: 14350
59518398 = yrday
fracday
Element set: 911
Inclination: 51
6461 deg
RA of node: 275
0367 deg
Eccentricity:
0007275
Arg of perigee: 138
7210 deg
Mean anomaly: 221
4493 deg
Mean motion: 15
52234022 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3963
Checksum: 304
Coasting Arc #13 (Orbit 3977)
---------------------------------------
Vector Time (GMT): 2014/351/13:00:52
258
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4114031
81 A = 6783434
25 meter
Y = 1660225
06 meter E =
0018276
Z = -5146627
61 I = 51
26714
XDOT = -1211
973225 Wp = 99
59526
YDOT = -7419
235495 meter/sec RA = 269
51017 deg
ZDOT = -1431
880818 TA = 156
56823
MA = 156
48484
Ha = 226
120 n
mi
Hp = 215
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13497479
69 X = -4107290
20
Y = 5446932
62 feet Y = 1614257
24 meter
Z = -16885261
18 Z = -5166596
71
XDOT = -3976
290108 XDOT = -1121
963849
YDOT = -24341
323803 feet/sec YDOT = -7432
285224 meter/sec
ZDOT = -4697
771711 ZDOT = -1437
550197
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7786949
95 X = -2373462
35
Y = -12178727
81 feet Y = -3712076
24 meter
Z = -16970712
34 Z = -5172673
12
XDOT = 22331
964580 XDOT = 6806
782804
YDOT = -7734
301713 feet/sec YDOT = -2357
415162 meter/sec
ZDOT = -4720
566828 ZDOT = -1438
828769
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 14351
56088663
00016717 00000-0 10270-3 0 9126
2 25544 51
6469 270
2359 0007220 141
7381 218
4285 15
52277138 39785
Satellite: ISS
Catalog Number: 25544
Epoch time: 14351
56088663 = yrday
fracday
Element set: 912
Inclination: 51
6469 deg
RA of node: 270
2359 deg
Eccentricity:
0007220
Arg of perigee: 141
7381 deg
Mean anomaly: 218
4285 deg
Mean motion: 15
52277138 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3978
Checksum: 325
Coasting Arc #14 (Orbit 3993)
---------------------------------------
Vector Time (GMT): 2014/352/13:00:52
258
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4195737
16 A = 6782604
09 meter
Y = -648620
69 meter E =
0009043
Z = 5284162
73 I = 51
26595
XDOT = 902
854945 Wp = 135
25943
YDOT = 7614
490041 meter/sec RA = 264
50418 deg
ZDOT = 211
240548 TA = 312
67937
MA = 312
75551
Ha = 225
832 n
mi
Hp = 215
755
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13765541
87 X = 4177009
37
Y = -2128020
63 feet Y = -601806
30 meter
Z = 17336491
88 Z = 5304499
67
XDOT = 2962
122523 XDOT = 816
614689
YDOT = 24981
922706 feet/sec YDOT = 7624
104139 meter/sec
ZDOT = 693
046417 ZDOT = 215
417571
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4795037
64 X = 1461527
47
Y = 12961784
25 feet Y = 3950751
84 meter
Z = 17423327
14 Z = 5310630
11
XDOT = -22952
413506 XDOT = -6995
895637
YDOT = 7508
600701 feet/sec YDOT = 2288
621494 meter/sec
ZDOT = 709
450759 ZDOT = 216
240591
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 14352
59094469
00016717 00000-0 10270-3 0 9132
2 25544 51
6467 265
1155 0007157 146
8411 213
3190 15
52328042 39947
Satellite: ISS
Catalog Number: 25544
Epoch time: 14352
59094469 = yrday
fracday
Element set: 913
Inclination: 51
6467 deg
RA of node: 265
1155 deg
Eccentricity:
0007157
Arg of perigee: 146
8411 deg
Mean anomaly: 213
3190 deg
Mean motion: 15
52328042 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3994
Checksum: 313
Coasting Arc #15 (Orbit 4008)
---------------------------------------
Vector Time (GMT): 2014/353/13:00:52
258
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4333111
39 A = 6782930
19 meter
Y = -412657
17 meter E =
0019512
Z = -5218796
91 I = 51
27163
XDOT = -547
324600 Wp = 114
79092
YDOT = -7559
598709 meter/sec RA = 259
49700 deg
ZDOT = 1047
256618 TA = 165
34221
MA = 165
28555
Ha = 225
863 n
mi
Hp = 215
677
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14216244
71 X = -4302823
48
Y = -1353862
10 feet Y = -460943
02 meter
Z = -17122037
11 Z = -5239773
19
XDOT = -1795
684383 XDOT = -467
837997
YDOT = -24801
833034 feet/sec YDOT = -7565
274904 meter/sec
ZDOT = 3435
881294 ZDOT = 1044
790177
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1714464
95 X = -522568
92
Y = -14068643
31 feet Y = -4288122
48 meter
Z = -17211408
90 Z = -5246037
43
XDOT = 22802
324072 XDOT = 6950
148377
YDOT = -6990
715954 feet/sec YDOT = -2130
770223 meter/sec
ZDOT = 3426
752625 ZDOT = 1044
474200
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 14353
55660408
00016717 00000-0 10270-3 0 9142
2 25544 51
6473 260
3147 0007118 149
9152 210
2410 15
52341903 40095
Satellite: ISS
Catalog Number: 25544
Epoch time: 14353
55660408 = yrday
fracday
Element set: 914
Inclination: 51
6473 deg
RA of node: 260
3147 deg
Eccentricity:
0007118
Arg of perigee: 149
9152 deg
Mean anomaly: 210
2410 deg
Mean motion: 15
52341903 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4009
Checksum: 281
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