[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 6th 2016
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2707 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 ET - UTC (sec) : 68 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
288/01:13:55
615 0
0 0
0 0
0
N/A 0
0 0
0 223
4
000/00:00:00
000 0
0 0
0 212
3
288/09:38:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
4
000/00:00:00
000 0
0 0
0 212
2
290/10:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
4
000/00:00:00
000 0
0 0
0 212
1
Coasting Arc #1 (Orbit 2213)
---------------------------------------
Vector Time (GMT): 2016/279/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3040680
30 A = 6777620
73 meter
Y = 2957468
22 meter E =
0019913
Z = -5302820
71 I = 51
34739
XDOT = -5279
326362 Wp = 73
54482
YDOT = -5541
821127 meter/sec RA = 226
73808 deg
ZDOT = -58
207808 TA = 195
86598
MA = 195
92846
Ha = 223
256 n
mi
Hp = 212
876
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9975985
24 X = -3047766
18
Y = 9702979
72 feet Y = 2923425
15 meter
Z = -17397705
74 Z = -5317609
35
XDOT = -17320
624548 XDOT = -5216
681179
YDOT = -18181
827844 feet/sec YDOT = -5600
507831 meter/sec
ZDOT = -190
970498 ZDOT = -83
701215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7277009
61 X = 2218032
53
Y = -11766266
75 feet Y = -3586358
11 meter
Z = -17462770
68 Z = -5322652
50
XDOT = 20283
502017 XDOT = 6182
411415
YDOT = 13017
967013 feet/sec YDOT = 3967
876346 meter/sec
ZDOT = -301
468186 ZDOT = -91
887503
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 16279
51625692
00016717 00000-0 10270-3 0 9008
2 25544 51
6414 227
7106 0006964 37
1260 323
0373 15
54040264 22143
Satellite: ISS
Catalog Number: 25544
Epoch time: 16279
51625692 = yrday
fracday
Element set: 900
Inclination: 51
6414 deg
RA of node: 227
7106 deg
Eccentricity:
0006964
Arg of perigee: 37
1260 deg
Mean anomaly: 323
0373 deg
Mean motion: 15
54040264 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2214
Checksum: 285
Coasting Arc #2 (Orbit 2229)
---------------------------------------
Vector Time (GMT): 2016/280/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4233550
91 A = 6778655
82 meter
Y = -1616213
32 meter E =
0012392
Z = 5035732
81 I = 51
37355
XDOT = 4473
688095 Wp = 47
59549
YDOT = 5956
676030 meter/sec RA = 221
72109 deg
ZDOT = -1838
143286 TA = 60
32327
MA = 60
19996
Ha = 223
208 n
mi
Hp = 212
852
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13889602
73 X = 4226847
32
Y = -5302537
14 feet Y = -1568907
96 meter
Z = 16521433
11 Z = 5056282
56
XDOT = 14677
454381 XDOT = 4415
675596
YDOT = 19542
900361 feet/sec YDOT = 6006
379286 meter/sec
ZDOT = -6030
653827 ZDOT = -1816
552270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11982448
67 X = -3652250
36
Y = 8629945
52 feet Y = 2630407
39 meter
Z = 16611462
32 Z = 5063173
71
XDOT = -18570
555351 XDOT = -5660
305271
YDOT = -14286
561278 feet/sec YDOT = -4354
543878 meter/sec
ZDOT = -5937
253883 ZDOT = -1809
674983
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 16280
54514032
00016717 00000-0 10270-3 0 9019
2 25544 51
6411 222
5832 0007047 41
0883 319
0799 15
54052873 22301
Satellite: ISS
Catalog Number: 25544
Epoch time: 16280
54514032 = yrday
fracday
Element set: 901
Inclination: 51
6411 deg
RA of node: 222
5832 deg
Eccentricity:
0007047
Arg of perigee: 41
0883 deg
Mean anomaly: 319
0799 deg
Mean motion: 15
54052873 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2230
Checksum: 284
Coasting Arc #3 (Orbit 2244)
---------------------------------------
Vector Time (GMT): 2016/281/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5248755
60 A = 6781616
98 meter
Y = 356269
15 meter E =
0013015
Z = -4289438
96 I = 51
40812
XDOT = -3278
151032 Wp = 81
53311
YDOT = -5956
266637 meter/sec RA = 216
71122 deg
ZDOT = 3527
656489 TA = 224
51812
MA = 224
62276
Ha = 223
283 n
mi
Hp = 212
674
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17220326
77 X = -5231512
82
Y = 1168862
04 feet Y = 297670
13 meter
Z = -14072962
46 Z = -4314894
64
XDOT = -10755
088689 XDOT = -3228
439007
YDOT = -19541
557207 feet/sec YDOT = -5992
646895 meter/sec
ZDOT = 11573
676145 ZDOT = 3511
853002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16172905
98 X = 4929501
74
Y = -5761822
34 feet Y = -1756203
45 meter
Z = -14184240
56 Z = -4323356
52
XDOT = 15295
911044 XDOT = 4662
193686
YDOT = 14698
999609 feet/sec YDOT = 4480
255081 meter/sec
ZDOT = 11505
547912 ZDOT = 3506
891003
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 16281
50971171
00016717 00000-0 10270-3 0 9028
2 25544 51
6409 217
7759 0006949 44
1688 316
0018 15
54059183 22457
Satellite: ISS
Catalog Number: 25544
Epoch time: 16281
50971171 = yrday
fracday
Element set: 902
Inclination: 51
6409 deg
RA of node: 217
7759 deg
Eccentricity:
0006949
Arg of perigee: 44
1688 deg
Mean anomaly: 316
0018 deg
Mean motion: 15
54059183 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2245
Checksum: 319
Coasting Arc #4 (Orbit 2260)
---------------------------------------
Vector Time (GMT): 2016/282/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5992600
30 A = 6785370
84 meter
Y = 837102
99 meter E =
0018429
Z = 3059164
86 I = 51
44817
XDOT = 1723
589720 Wp = 79
32525
YDOT = 5649
340848 meter/sec RA = 211
71206 deg
ZDOT = -4893
741293 TA = 65
43905
MA = 65
24709
Ha = 223
282 n
mi
Hp = 212
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19660762
15 X = 5967933
92
Y = 2746400
89 feet Y = 903978
57 meter
Z = 10036630
11 Z = 3088215
82
XDOT = 5654
821917 XDOT = 1684
061254
YDOT = 18534
582836 feet/sec YDOT = 5668
393819 meter/sec
ZDOT = -16055
581671 ZDOT = -4885
464829
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19558613
64 X = -5961465
44
Y = 2997863
43 feet Y = 913748
77 meter
Z = 10163448
11 Z = 3097818
98
XDOT = -10621
488851 XDOT = -3237
429802
YDOT = -14671
349609 feet/sec YDOT = -4471
827361 meter/sec
ZDOT = -16020
284009 ZDOT = -4882
982566
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 16282
53857863
00016717 00000-0 10270-3 0 9034
2 25544 51
6417 212
6474 0007000 47
4683 312
7059 15
54091560 22615
Satellite: ISS
Catalog Number: 25544
Epoch time: 16282
53857863 = yrday
fracday
Element set: 903
Inclination: 51
6417 deg
RA of node: 212
6474 deg
Eccentricity:
0007000
Arg of perigee: 47
4683 deg
Mean anomaly: 312
7059 deg
Mean motion: 15
54091560 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2261
Checksum: 303
Coasting Arc #5 (Orbit 2275)
---------------------------------------
Vector Time (GMT): 2016/283/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6349608
65 A = 6788355
51 meter
Y = -1806075
48 meter E =
0014925
Z = -1560974
13 I = 51
48532
XDOT = 47
574732 Wp = 44
43438
YDOT = -5087
913703 meter/sec RA = 206
72478 deg
ZDOT = 5736
981596 TA = 298
46245
MA = 298
61272
Ha = 223
352 n
mi
Hp = 212
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20832049
39 X = -6321358
12
Y = -5925444
48 feet Y = -1876923
22 meter
Z = -5121306
19 Z = -1591750
51
XDOT = 156
085079 XDOT = 76
597458
YDOT = -16692
630258 feet/sec YDOT = -5087
218994 meter/sec
ZDOT = 18822
118097 ZDOT = 5737
283570
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21615789
83 X = 6588492
74
Y = -670784
64 feet Y = -204455
16 meter
Z = -5255533
18 Z = -1601886
51
XDOT = 4987
741244 XDOT = 1520
263531
YDOT = 14336
684310 feet/sec YDOT = 4369
821378 meter/sec
ZDOT = 18824
215082 ZDOT = 5737
620757
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 16283
50313263
00016717 00000-0 10270-3 0 9044
2 25544 51
6410 207
8400 0007050 51
0654 309
1127 15
54087584 22760
Satellite: ISS
Catalog Number: 25544
Epoch time: 16283
50313263 = yrday
fracday
Element set: 904
Inclination: 51
6410 deg
RA of node: 207
8400 deg
Eccentricity:
0007050
Arg of perigee: 51
0654 deg
Mean anomaly: 309
1127 deg
Mean motion: 15
54087584 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2276
Checksum: 278
Coasting Arc #6 (Orbit 2291)
---------------------------------------
Vector Time (GMT): 2016/284/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6253491
44 A = 6789393
87 meter
Y = 2631611
62 meter E =
0014739
Z = -160455
77 I = 51
51899
XDOT = -1971
388186 Wp = 108
15139
YDOT = 4346
821314 meter/sec RA = 201
74529 deg
ZDOT = -5998
104929 TA = 73
57937
MA = 73
41741
Ha = 223
417 n
mi
Hp = 212
471
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20516704
19 X = 6224378
74
Y = 8633896
40 feet Y = 2701379
57 meter
Z = -526429
70 Z = -130148
54
XDOT = -6467
809009 XDOT = -1990
712464
YDOT = 14261
224784 feet/sec YDOT = 4324
667385 meter/sec
ZDOT = -19678
821947 ZDOT = -6007
728818
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22203640
52 X = -6767669
63
Y = -1612226
27 feet Y = -491406
57 meter
Z = -394360
28 Z = -120201
01
XDOT = 1325
346178 XDOT = 403
965515
YDOT = -13919
538373 feet/sec YDOT = -4242
675296 meter/sec
ZDOT = -19721
545970 ZDOT = -6011
127212
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 16284
53198188
00016717 00000-0 10270-3 0 9056
2 25544 51
6419 202
7115 0006963 55
2632 304
9175 15
54102952 22921
Satellite: ISS
Catalog Number: 25544
Epoch time: 16284
53198188 = yrday
fracday
Element set: 905
Inclination: 51
6419 deg
RA of node: 202
7115 deg
Eccentricity:
0006963
Arg of perigee: 55
2632 deg
Mean anomaly: 304
9175 deg
Mean motion: 15
54102952 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2292
Checksum: 311
Coasting Arc #7 (Orbit 2307)
---------------------------------------
Vector Time (GMT): 2016/285/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5683820
15 A = 6788034
47 meter
Y = -3216274
48 meter E =
0020894
Z = 1813085
58 I = 51
54497
XDOT = 3813
472097 Wp = 63
40987
YDOT = -3533
507664 meter/sec RA = 196
76696 deg
ZDOT = 5645
486536 TA = 316
56459
MA = 316
72901
Ha = 223
443 n
mi
Hp = 212
433
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18647703
91 X = -5656239
77
Y = -10552081
61 feet Y = -3279680
38 meter
Z = 5948443
50 Z = 1785542
09
XDOT = 12511
391393 XDOT = 3825
277691
YDOT = -11592
872912 feet/sec YDOT = -3490
796300 meter/sec
ZDOT = 18521
937453 ZDOT = 5664
040594
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21145983
91 X = 6445295
90
Y = 3652796
91 feet Y = 1113372
50 meter
Z = 5828525
24 Z = 1776534
49
XDOT = -7504
886336 XDOT = -2287
489355
YDOT = 13541
324742 feet/sec YDOT = 4127
395781 meter/sec
ZDOT = 18603
576276 ZDOT = 5670
370049
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 16285
56082124
00016717 00000-0 10270-3 0 9063
2 25544 51
6422 197
5831 0006977 58
4122 301
7711 15
54116001 23084
Satellite: ISS
Catalog Number: 25544
Epoch time: 16285
56082124 = yrday
fracday
Element set: 906
Inclination: 51
6422 deg
RA of node: 197
5831 deg
Eccentricity:
0006977
Arg of perigee: 58
4122 deg
Mean anomaly: 301
7711 deg
Mean motion: 15
54116001 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2308
Checksum: 291
Coasting Arc #8 (Orbit 2322)
---------------------------------------
Vector Time (GMT): 2016/286/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4637762
21 A = 6784647
37 meter
Y = 3671438
49 meter E =
0011189
Z = -3335540
92 I = 51
56650
XDOT = -5454
576085 Wp = 75
43587
YDOT = 2652
038846 meter/sec RA = 191
78433 deg
ZDOT = -4675
390365 TA = 143
39718
MA = 143
32068
Ha = 223
419 n
mi
Hp = 212
365
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15215755
29 X = 4612565
33
Y = 12045401
86 feet Y = 3723159
79 meter
Z = -10943375
72 Z = -3313073
26
XDOT = -17895
590831 XDOT = -5461
115229
YDOT = 8700
914849 feet/sec YDOT = 2591
005017 meter/sec
ZDOT = -15339
207234 ZDOT = -4701
903746
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18550479
19 X = -5654186
06
Y = -5883782
38 feet Y = -1793376
87 meter
Z = -10845700
25 Z = -3305769
44
XDOT = 13158
648871 XDOT = 4010
756176
YDOT = -13060
839441 feet/sec YDOT = -3980
943862 meter/sec
ZDOT = -15455
516388 ZDOT = -4710
841395
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 16286
52534769
00016717 00000-0 10270-3 0 9078
2 25544 51
6435 192
7752 0006987 61
7421 298
4436 15
54146693 23230
Satellite: ISS
Catalog Number: 25544
Epoch time: 16286
52534769 = yrday
fracday
Element set: 907
Inclination: 51
6435 deg
RA of node: 192
7752 deg
Eccentricity:
0006987
Arg of perigee: 61
7421 deg
Mean anomaly: 298
4436 deg
Mean motion: 15
54146693 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2323
Checksum: 342
Coasting Arc #9 (Orbit 2338)
---------------------------------------
Vector Time (GMT): 2016/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3213334
69 A = 6780871
50 meter
Y = -3949349
10 meter E =
0014983
Z = 4465867
64 I = 51
58518
XDOT = 6722
924759 Wp = 91
94272
YDOT = -1790
102729 meter/sec RA = 186
79391 deg
ZDOT = 3244
397461 TA = 325
36541
MA = 325
46290
Ha = 223
525 n
mi
Hp = 212
234
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10542436
63 X = -3190626
74
Y = -12957182
08 feet Y = -3985155
22 meter
Z = 14651796
71 Z = 4450313
55
XDOT = 22056
839759 XDOT = 6726
682414
YDOT = -5873
040451 feet/sec YDOT = -1714
901045 meter/sec
ZDOT = 10644
348624 ZDOT = 3277
065468
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14662782
90 X = 4469216
23
Y = 8124369
88 feet Y = 2476307
94 meter
Z = 14584378
50 Z = 4445318
57
XDOT = -17683
828399 XDOT = -5390
030896
YDOT = 12492
040138 feet/sec YDOT = 3807
573834 meter/sec
ZDOT = 10787
448579 ZDOT = 3288
014327
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 16287
55416893
00016717 00000-0 10270-3 0 9080
2 25544 51
6431 187
6470 0007018 66
0239 294
1648 15
54147526 23398
Satellite: ISS
Catalog Number: 25544
Epoch time: 16287
55416893 = yrday
fracday
Element set: 908
Inclination: 51
6431 deg
RA of node: 187
6470 deg
Eccentricity:
0007018
Arg of perigee: 66
0239 deg
Mean anomaly: 294
1648 deg
Mean motion: 15
54147526 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2339
Checksum: 332
Coasting Arc #10 (Orbit 2346)
---------------------------------------
Vector Time (GMT): 2016/288/01:13:55
615
Vector Time (MET): N/A
Weight (LBS) : 893178
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 396282
96 A = 6777490
11 meter
Y = 4235863
78 meter E =
0021151
Z = -5294235
47 I = 51
59039
XDOT = -7628
173640 Wp = 80
59357
YDOT = -51
281043 meter/sec RA = 184
02454 deg
ZDOT = -610
722101 TA = 183
55351
MA = 183
56855
Ha = 223
368 n
mi
Hp = 212
311
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1300140
95 X = 374604
46
Y = 13897190
87 feet Y = 4240173
36 meter
Z = -17369538
94 Z = -5292363
62
XDOT = -25026
816403 XDOT = -7624
066592
YDOT = -168
244893 feet/sec YDOT = -136
561519 meter/sec
ZDOT = -2003
681433 ZDOT = -647
768370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10123588
15 X = 3085669
67
Y = 9622765
68 feet Y = 2933018
98 meter
Z = -17361984
54 Z = -5291932
89
XDOT = -18386
164485 XDOT = -5604
102935
YDOT = 15428
031845 feet/sec YDOT = 4702
464106 meter/sec
ZDOT = -2165
658190 ZDOT = -660
092616
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 16288
06857481
00016717 00000-0 10270-3 0 9090
2 25544 51
6419 185
0812 0006666 69
6873 290
4996 15
54134326 23475
Satellite: ISS
Catalog Number: 25544
Epoch time: 16288
06857481 = yrday
fracday
Element set: 909
Inclination: 51
6419 deg
RA of node: 185
0812 deg
Eccentricity:
0006666
Arg of perigee: 69
6873 deg
Mean anomaly: 290
4996 deg
Mean motion: 15
54134326 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2347
Checksum: 349
Coasting Arc #11 (Orbit 2352)
---------------------------------------
Vector Time (GMT): 2016/288/09:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 878052
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2612439
73 A = 6779214
18 meter
Y = -3945793
44 meter E =
0012544
Z = 4843917
11 I = 51
60805
XDOT = 7079
839925 Wp = 95
61947
YDOT = -1664
189395 meter/sec RA = 182
29252 deg
ZDOT = 2456
026443 TA = 330
25233
MA = 330
32359
Ha = 223
359 n
mi
Hp = 212
213
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8570996
49 X = -2591652
72
Y = -12945516
55 feet Y = -3974890
62 meter
Z = 15892116
51 Z = 4831277
36
XDOT = 23227
821275 XDOT = 7085
992624
YDOT = -5459
938961 feet/sec YDOT = -1584
983142 meter/sec
ZDOT = 8057
829538 ZDOT = 2490
434212
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5574416
42 X = 1699082
13
Y = 14550233
58 feet Y = 4434911
19 meter
Z = 15837434
49 Z = 4827250
03
XDOT = -22747
901383 XDOT = -6933
560342
YDOT = -243
545780 feet/sec YDOT = -74
232754 meter/sec
ZDOT = 8208
529253 ZDOT = 2501
959716
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 16288
45437815
00016717 00000-0 10270-3 0 9100
2 25544 51
6420 183
1594 0006735 69
0120 291
1752 15
54198156 23535
Satellite: ISS
Catalog Number: 25544
Epoch time: 16288
45437815 = yrday
fracday
Element set: 910
Inclination: 51
6420 deg
RA of node: 183
1594 deg
Eccentricity:
0006735
Arg of perigee: 69
0120 deg
Mean anomaly: 291
1752 deg
Mean motion: 15
54198156 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2353
Checksum: 309
Coasting Arc #12 (Orbit 2367)
---------------------------------------
Vector Time (GMT): 2016/289/09:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 878052
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 831075
18 A = 6777329
77 meter
Y = 4162579
14 meter E =
0021514
Z = -5302072
81 I = 51
63440
XDOT = -7589
880923 Wp = 81
38165
YDOT = 801
878999 meter/sec RA = 177
29248 deg
ZDOT = -558
930846 TA = 183
26627
MA = 183
28034
Ha = 223
414 n
mi
Hp = 212
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2726624
62 X = 810222
09
Y = 13656755
71 feet Y = 4171755
50 meter
Z = -17395252
00 Z = -5298086
76
XDOT = -24901
184130 XDOT = -7595
568539
YDOT = 2630
836612 feet/sec YDOT = 716
971982 meter/sec
ZDOT = -1833
762619 ZDOT = -595
815234
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 32084
25 X = 9779
28
Y = -13947222
41 feet Y = -4251113
39 meter
Z = -17378440
89 Z = -5296948
78
XDOT = 23880
317568 XDOT = 7278
720795
YDOT = 2545
882330 feet/sec YDOT = 775
984934 meter/sec
ZDOT = -1995
177781 ZDOT = -608
130188
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 16289
41888391
00016717 00000-0 10270-3 0 9117
2 25544 51
6425 178
3508 0006965 71
7302 288
4609 15
54181908 23681
Satellite: ISS
Catalog Number: 25544
Epoch time: 16289
41888391 = yrday
fracday
Element set: 911
Inclination: 51
6425 deg
RA of node: 178
3508 deg
Eccentricity:
0006965
Arg of perigee: 71
7302 deg
Mean anomaly: 288
4609 deg
Mean motion: 15
54181908 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2368
Checksum: 342
Coasting Arc #13 (Orbit 2383)
---------------------------------------
Vector Time (GMT): 2016/290/09:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 878052
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1017645
08 A = 6777709
81 meter
Y = -4258973
91 meter E =
0011097
Z = 5165302
96 I = 51
66754
XDOT = 7546
209190 Wp = 67
53744
YDOT = 96
474842 meter/sec RA = 172
29430 deg
ZDOT = -1400
623711 TA = 35
95139
MA = 35
87678
Ha = 223
328 n
mi
Hp = 212
079
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3338730
56 X = 1040102
95
Y = -13973011
51 feet Y = -4247467
76 meter
Z = 16946532
03 Z = 5170301
57
XDOT = 24757
904166 XDOT = 7551
373320
YDOT = 316
518509 feet/sec YDOT = 180
890335 meter/sec
ZDOT = -4595
222150 ZDOT = -1363
952705
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5810753
03 X = -1771117
52
Y = 13109701
60 feet Y = 3995837
05 meter
Z = 16969030
41 Z = 5172160
47
XDOT = -23324
909773 XDOT = -7109
432499
YDOT = -4570
344908 feet/sec YDOT = -1393
041128 meter/sec
ZDOT = -4434
858981 ZDOT = -1351
745017
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 16290
44768063
00016717 00000-0 10270-3 0 9126
2 25544 51
6417 173
2232 0006888 74
7443 285
4470 15
54210492 23845
Satellite: ISS
Catalog Number: 25544
Epoch time: 16290
44768063 = yrday
fracday
Element set: 912
Inclination: 51
6417 deg
RA of node: 173
2232 deg
Eccentricity:
0006888
Arg of perigee: 74
7443 deg
Mean anomaly: 285
4470 deg
Mean motion: 15
54210492 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2384
Checksum: 315
Coasting Arc #14 (Orbit 2384)
---------------------------------------
Vector Time (GMT): 2016/290/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 892578
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6732113
32 A = 6789176
45 meter
Y = 803404
59 meter E =
0018745
Z = 167516
19 I = 51
70790
XDOT = -404
038144 Wp = 57
30219
YDOT = -4740
138634 meter/sec RA = 172
07679 deg
ZDOT = 6016
985755 TA = 304
50126
MA = 304
67814
Ha = 223
409 n
mi
Hp = 212
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22086985
97 X = -6741410
59
Y = 2635841
81 feet Y = 728069
61 meter
Z = 549593
79 Z = 134789
80
XDOT = -1325
584461 XDOT = -380
231312
YDOT = -15551
635938 feet/sec YDOT = -4744
523076 meter/sec
ZDOT = 19740
766914 ZDOT = 6015
081347
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21712423
56 X = 6617946
70
Y = -4846669
98 feet Y = -1477265
01 meter
Z = 406346
77 Z = 123854
50
XDOT = 2658
231621 XDOT = 810
228998
YDOT = 13741
235948 feet/sec YDOT = 4188
328717 meter/sec
ZDOT = 19733
147549 ZDOT = 6014
663373
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 16290
51198126
00016717 00000-0 10270-3 0 9132
2 25544 51
6427 172
9024 0006939 75
2892 284
9029 15
54180020 23850
Satellite: ISS
Catalog Number: 25544
Epoch time: 16290
51198126 = yrday
fracday
Element set: 913
Inclination: 51
6427 deg
RA of node: 172
9024 deg
Eccentricity:
0006939
Arg of perigee: 75
2892 deg
Mean anomaly: 284
9029 deg
Mean motion: 15
54180020 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2385
Checksum: 316
Coasting Arc #15 (Orbit 2399)
---------------------------------------
Vector Time (GMT): 2016/291/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 892578
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6514836
58 A = 6787724
15 meter
Y = 49936
36 meter E =
0011976
Z = -1903994
63 I = 51
73486
XDOT = -1671
405447 Wp = 112
11768
YDOT = 4931
767404 meter/sec RA = 167
11184 deg
ZDOT = -5622
357594 TA = 88
81504
MA = 88
67784
Ha = 223
411 n
mi
Hp = 212
200
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21374135
76 X = 6523043
01
Y = 163833
21 feet Y = 122835
36 meter
Z = -6246701
53 Z = -1872326
43
XDOT = -5483
613672 XDOT = -1699
117795
YDOT = 16180
339252 feet/sec YDOT = 4912
921184 meter/sec
ZDOT = -18446
055097 ZDOT = -5630
544820
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21284302
08 X = -6487455
27
Y = 2360134
39 feet Y = 719368
96 meter
Z = -6108195
45 Z = -1861777
97
XDOT = 3593
204718 XDOT = 1095
208798
YDOT = -15145
815460 feet/sec YDOT = -4616
444552 meter/sec
ZDOT = -18482
609143 ZDOT = -5633
499267
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 16291
47647182
00016717 00000-0 10270-3 0 9140
2 25544 51
6428 168
0947 0006725 80
1805 280
0107 15
54172996 24008
Satellite: ISS
Catalog Number: 25544
Epoch time: 16291
47647182 = yrday
fracday
Element set: 914
Inclination: 51
6428 deg
RA of node: 168
0947 deg
Eccentricity:
0006725
Arg of perigee: 80
1805 deg
Mean anomaly: 280
0107 deg
Mean motion: 15
54172996 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2400
Checksum: 312
Coasting Arc #16 (Orbit 2415)
---------------------------------------
Vector Time (GMT): 2016/292/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 892578
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5795277
76 A = 6784369
21 meter
Y = -934576
48 meter E =
0019375
Z = 3383512
61 I = 51
75518
XDOT = 3529
795616 Wp = 86
88497
YDOT = -4985
400721 meter/sec RA = 162
14059 deg
ZDOT = 4646
897460 TA = 312
59793
MA = 312
76120
Ha = 223
483 n
mi
Hp = 212
086
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19013378
49 X = -5800832
44
Y = -3066195
80 feet Y = -999414
01 meter
Z = 11100763
16 Z = 3355346
45
XDOT = 11580
694278 XDOT = 3562
708091
YDOT = -16356
301577 feet/sec YDOT = -4945
743858 meter/sec
ZDOT = 15245
726576 ZDOT = 4664
125019
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19323880
12 X = 5889918
66
Y = 463621
54 feet Y = 141311
85 meter
Z = 10977694
35 Z = 3346001
24
XDOT = -9137
586438 XDOT = -2785
136346
YDOT = 16344
747823 feet/sec YDOT = 4981
879136 meter/sec
ZDOT = 15321
846475 ZDOT = 4670
098806
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 16292
50525376
00016717 00000-0 10270-3 0 9156
2 25544 51
6430 162
9653 0006862 82
1028 278
0903 15
54200652 24168
Satellite: ISS
Catalog Number: 25544
Epoch time: 16292
50525376 = yrday
fracday
Element set: 915
Inclination: 51
6430 deg
RA of node: 162
9653 deg
Eccentricity:
0006862
Arg of perigee: 82
1028 deg
Mean anomaly: 278
0903 deg
Mean motion: 15
54200652 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2416
Checksum: 298
Coasting Arc #17 (Orbit 2430)
---------------------------------------
Vector Time (GMT): 2016/293/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 892578
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4654209
44 A = 6780382
39 meter
Y = 1931042
22 meter E =
0016297
Z = -4552553
11 I = 51
77202
XDOT = -5059
900453 Wp = 76
40724
YDOT = 4812
486929 meter/sec RA = 157
16161 deg
ZDOT = -3137
293504 TA = 162
17587
MA = 162
11864
Ha = 223
320 n
mi
Hp = 212
141
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15269716
02 X = 4654384
97
Y = 6335440
36 feet Y = 1983089
49 meter
Z = -14936197
86 Z = -4529943
27
XDOT = -16600
723271 XDOT = -5098
098878
YDOT = 15788
999111 feet/sec YDOT = 4755
690005 meter/sec
ZDOT = -10292
957691 ZDOT = -3161
966788
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16149851
46 X = -4922474
72
Y = -3926917
18 feet Y = -1196924
36 meter
Z = -14837575
88 Z = -4522493
13
XDOT = 13657
769220 XDOT = 4162
888058
YDOT = -16938
312941 feet/sec YDOT = -5162
797784 meter/sec
ZDOT = -10401
643639 ZDOT = -3170
420981
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 16293
46972882
00016717 00000-0 10270-3 0 9161
2 25544 51
6424 158
1571 0006768 85
1828 275
0097 15
54231802 24312
Satellite: ISS
Catalog Number: 25544
Epoch time: 16293
46972882 = yrday
fracday
Element set: 916
Inclination: 51
6424 deg
RA of node: 158
1571 deg
Eccentricity:
0006768
Arg of perigee: 85
1828 deg
Mean anomaly: 275
0097 deg
Mean motion: 15
54231802 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2431
Checksum: 327
Coasting Arc #18 (Orbit 2446)
---------------------------------------
Vector Time (GMT): 2016/294/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 892578
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3216697
99 A = 6777646
07 meter
Y = -2923310
73 meter E =
0010669
Z = 5191894
51 I = 51
79211
XDOT = 6141
679385 Wp = 103
70866
YDOT = -4412
716008 meter/sec RA = 152
17503 deg
ZDOT = 1315
822044 TA = 333
66383
MA = 333
71803
Ha = 223
436 n
mi
Hp = 212
013
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10553471
11 X = -3208990
17
Y = -9590914
46 feet Y = -2959238
71 meter
Z = 17033774
63 Z = 5176287
13
XDOT = 20149
866749 XDOT = 6184
175219
YDOT = -14477
414724 feet/sec YDOT = -4343
797971 meter/sec
ZDOT = 4317
001457 ZDOT = 1345
760725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12129643
32 X = 3697115
28
Y = 7651121
92 feet Y = 2332061
96 meter
Z = 16965935
19 Z = 5171217
05
XDOT = -16830
136919 XDOT = -5129
825733
YDOT = 16782
227670 feet/sec YDOT = 5115
222994 meter/sec
ZDOT = 4448
686534 ZDOT = 1355
959655
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 16294
49849717
00016717 00000-0 10270-3 0 9176
2 25544 51
6422 153
0281 0006798 89
7982 270
3950 15
54233098 24478
Satellite: ISS
Catalog Number: 25544
Epoch time: 16294
49849717 = yrday
fracday
Element set: 917
Inclination: 51
6422 deg
RA of node: 153
0281 deg
Eccentricity:
0006798
Arg of perigee: 89
7982 deg
Mean anomaly: 270
3950 deg
Mean motion: 15
54233098 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2447
Checksum: 348
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