[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 10th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 25144 4947 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 977 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
314/12:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
6
000/00:00:00
000 0
0 0
0 213
9
319/09:49:38
000 0
0 0
0 0
0
N/A 0
0 0
0 222
6
000/00:00:00
000 0
0 0
0 213
5
320/04:47:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 213
4
320/18:14:08
000 0
0 0
0 0
0
N/A 0
0 0
0 222
7
000/00:00:00
000 0
0 0
0 213
3
322/09:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 213
1
322/19:30:01
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 213
2
325/22:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 213
0
Coasting Arc #1 (Orbit 2110)
---------------------------------------
Vector Time (GMT): 2018/313/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2623893
94 A = 6778614
34 meter
Y = 3535443
85 meter E =
0009123
Z = 5150602
64 I = 51
71974
XDOT = -6923
880644 Wp = 40
39125
YDOT = -2943
446428 meter/sec RA = 13
98703 deg
ZDOT = -1498
564290 TA = 64
06526
MA = 63
97127
Ha = 222
514 n
mi
Hp = 214
042
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8608575
93 X = -2688252
83
Y = 11599225
23 feet Y = 3505741
63 meter
Z = 16898302
61 Z = 5137700
12
XDOT = -22716
143846 XDOT = -6883
172174
YDOT = -9656
976471 feet/sec YDOT = -3020
646408 meter/sec
ZDOT = -4916
549507 ZDOT = -1532
100219
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2718702
42 X = -828660
50
Y = -14255990
58 feet Y = -4345225
93 meter
Z = 16839763
25 Z = 5132759
84
XDOT = 21363
498902 XDOT = 6511
594465
YDOT = -10091
628916 feet/sec YDOT = -3075
928494 meter/sec
ZDOT = -5066
954141 ZDOT = -1544
407622
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 18313
54560466
00016717 00000-0 10270-3 0 9009
2 25544 51
6417 14
3624 0004607 26
3683 333
7704 15
53965391 21110
Satellite: ISS
Catalog Number: 25544
Epoch time: 18313
54560466 = yrday
fracday
Element set: 900
Inclination: 51
6417 deg
RA of node: 14
3624 deg
Eccentricity:
0004607
Arg of perigee: 26
3683 deg
Mean anomaly: 333
7704 deg
Mean motion: 15
53965391 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2111
Checksum: 293
Coasting Arc #2 (Orbit 2125)
---------------------------------------
Vector Time (GMT): 2018/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4125642
92 A = 6781332
44 meter
Y = -2952713
78 meter E =
0011423
Z = -4509081
99 I = 51
69504
XDOT = 6006
107218 Wp = 85
98378
YDOT = 3512
666228 meter/sec RA = 8
99903 deg
ZDOT = 3202
923134 TA = 216
17694
MA = 216
25426
Ha = 222
614 n
mi
Hp = 213
970
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13535573
88 X = 4180257
62
Y = -9687381
16 feet Y = -2906272
40 meter
Z = -14793576
08 Z = -4488908
05
XDOT = 19705
076174 XDOT = 5950
822732
YDOT = 11524
495499 feet/sec YDOT = 3579
521426 meter/sec
ZDOT = 10508
278000 ZDOT = 3231
965302
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1714669
15 X = -522631
16
Y = 16637482
78 feet Y = 5071104
75 meter
Z = -14702417
61 Z = -4481296
89
XDOT = -20402
063669 XDOT = -6218
549006
YDOT = 7275
707191 feet/sec YDOT = 2217
635552 meter/sec
ZDOT = 10638
380898 ZDOT = 3242
578498
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 18314
51025491
00016717 00000-0 10270-3 0 9012
2 25544 51
6405 9
5556 0004754 32
4726 327
6719 15
53955174 21268
Satellite: ISS
Catalog Number: 25544
Epoch time: 18314
51025491 = yrday
fracday
Element set: 901
Inclination: 51
6405 deg
RA of node: 9
5556 deg
Eccentricity:
0004754
Arg of perigee: 32
4726 deg
Mean anomaly: 327
6719 deg
Mean motion: 15
53955174 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2126
Checksum: 304
Coasting Arc #3 (Orbit 2126)
---------------------------------------
Vector Time (GMT): 2018/314/12:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5322744
32 A = 6784261
40 meter
Y = 2086284
93 meter E =
0015196
Z = 3644792
06 I = 51
70377
XDOT = -4668
590579 Wp = 70
96674
YDOT = -4224
706209 meter/sec RA = 8
82393 deg
ZDOT = -4379
876411 TA = 65
79982
MA = 65
64106
Ha = 222
618 n
mi
Hp = 213
914
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17463071
93 X = -5363383
04
Y = 6844766
84 feet Y = 2026534
91 meter
Z = 11957979
21 Z = 3618836
79
XDOT = -15316
898226 XDOT = -4599
726120
YDOT = -13860
584675 feet/sec YDOT = -4276
528381 meter/sec
ZDOT = -14369
673264 ZDOT = -4402
388279
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2435376
41 X = 742302
73
Y = -18672544
62 feet Y = -5691391
60 meter
Z = 11840945
92 Z = 3609120
32
XDOT = 18112
154620 XDOT = 5520
584728
YDOT = -6855
387858 feet/sec YDOT = -2089
522219 meter/sec
ZDOT = -14470
303307 ZDOT = -4410
548448
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 18314
57456382
00016717 00000-0 10270-3 0 9026
2 25544 51
6405 9
2352 0004772 31
1711 328
9724 15
53972340 21274
Satellite: ISS
Catalog Number: 25544
Epoch time: 18314
57456382 = yrday
fracday
Element set: 902
Inclination: 51
6405 deg
RA of node: 9
2352 deg
Eccentricity:
0004772
Arg of perigee: 31
1711 deg
Mean anomaly: 328
9724 deg
Mean motion: 15
53972340 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2127
Checksum: 294
Coasting Arc #4 (Orbit 2141)
---------------------------------------
Vector Time (GMT): 2018/315/12:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6227827
20 A = 6787604
16 meter
Y = -1401157
49 meter E =
0010824
Z = -2298122
81 I = 51
68289
XDOT = 3007
648533 Wp = 40
12108
YDOT = 4501
680598 meter/sec RA = 3
84909 deg
ZDOT = 5428
275244 TA = 294
30184
MA = 294
41485
Ha = 222
708 n
mi
Hp = 213
756
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20432503
93 X = 6254195
76
Y = -4596973
39 feet Y = -1331366
04 meter
Z = -7539773
01 Z = -2267805
60
XDOT = 9867
613298 XDOT = 2930
717716
YDOT = 14769
293301 feet/sec YDOT = 4534
883775 meter/sec
ZDOT = 17809
301981 ZDOT = 5442
699041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5472615
83 X = -1668053
30
Y = 20265988
24 feet Y = 6177073
22 meter
Z = -7403225
98 Z = -2256503
28
XDOT = -16133
577736 XDOT = -4917
514494
YDOT = 2145
302654 feet/sec YDOT = 653
888249 meter/sec
ZDOT = 17873
511728 ZDOT = 5447
846375
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 18315
53920784
00016717 00000-0 10270-3 0 9036
2 25544 51
6412 4
4277 0004869 36
8132 323
3354 15
53977582 21429
Satellite: ISS
Catalog Number: 25544
Epoch time: 18315
53920784 = yrday
fracday
Element set: 903
Inclination: 51
6412 deg
RA of node: 4
4277 deg
Eccentricity:
0004869
Arg of perigee: 36
8132 deg
Mean anomaly: 323
3354 deg
Mean motion: 15
53977582 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2142
Checksum: 309
Coasting Arc #5 (Orbit 2157)
---------------------------------------
Vector Time (GMT): 2018/316/12:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6718151
41 A = 6789616
76 meter
Y = 669587
26 meter E =
0014172
Z = 680309
60 I = 51
65665
XDOT = -1081
837969 Wp = 107
08267
YDOT = -4696
075822 meter/sec RA = 358
87974 deg
ZDOT = -5962
627645 TA = 65
57316
MA = 65
42536
Ha = 222
736 n
mi
Hp = 213
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22041179
18 X = -6728444
26
Y = 2196808
60 feet Y = 594402
64 meter
Z = 2231986
88 Z = 647649
63
XDOT = -3549
337167 XDOT = -1000
280941
YDOT = -15407
072906 feet/sec YDOT = -4707
717354 meter/sec
ZDOT = -19562
426656 ZDOT = -5967
685087
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7975146
60 X = 2430824
68
Y = -20680209
34 feet Y = -6303327
81 meter
Z = 2085015
95 Z = 635512
86
XDOT = 13788
506793 XDOT = 4202
736870
YDOT = 3307
959500 feet/sec YDOT = 1008
266056 meter/sec
ZDOT = -19584
484009 ZDOT = -5969
350726
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 18316
56815415
00016717 00000-0 10270-3 0 9045
2 25544 51
6414 359
2995 0004991 39
7220 320
4298 15
53970516 21587
Satellite: ISS
Catalog Number: 25544
Epoch time: 18316
56815415 = yrday
fracday
Element set: 904
Inclination: 51
6414 deg
RA of node: 359
2995 deg
Eccentricity:
0004991
Arg of perigee: 39
7220 deg
Mean anomaly: 320
4298 deg
Mean motion: 15
53970516 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2158
Checksum: 326
Coasting Arc #6 (Orbit 2173)
---------------------------------------
Vector Time (GMT): 2018/317/12:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6712016
38 A = 6789441
86 meter
Y = 45669
86 meter E =
0018618
Z = 956368
05 I = 51
62206
XDOT = -885
122267 Wp = 51
85244
YDOT = 4805
872933 meter/sec RA = 353
91073 deg
ZDOT = 5915
505904 TA = 318
51361
MA = 318
65479
Ha = 222
861 n
mi
Hp = 213
520
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22021051
11 X = 6706361
23
Y = 149835
49 feet Y = 120696
62 meter
Z = 3137690
46 Z = 988959
44
XDOT = -2903
944446 XDOT = -967
531918
YDOT = 15767
299648 feet/sec YDOT = 4795
513818 meter/sec
ZDOT = 19407
827770 ZDOT = 5911
006292
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9707161
08 X = -2958742
70
Y = 19742821
95 feet Y = 6017612
13 meter
Z = 3284242
54 Z = 1001037
13
XDOT = -11438
523316 XDOT = -3486
461907
YDOT = -8884
064200 feet/sec YDOT = -2707
862768 meter/sec
ZDOT = 19386
892626 ZDOT = 5909
124873
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 18317
59709766
00016717 00000-0 10270-3 0 9051
2 25544 51
6407 354
1719 0005158 43
3079 316
8478 15
53945960 21748
Satellite: ISS
Catalog Number: 25544
Epoch time: 18317
59709766 = yrday
fracday
Element set: 905
Inclination: 51
6407 deg
RA of node: 354
1719 deg
Eccentricity:
0005158
Arg of perigee: 43
3079 deg
Mean anomaly: 316
8478 deg
Mean motion: 15
53945960 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2174
Checksum: 343
Coasting Arc #7 (Orbit 2188)
---------------------------------------
Vector Time (GMT): 2018/318/12:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6237409
03 A = 6786928
20 meter
Y = -839002
42 meter E =
0007651
Z = -2547474
56 I = 51
58172
XDOT = 2793
729807 Wp = 87
46330
YDOT = -4805
895814 meter/sec RA = 348
93575 deg
ZDOT = -5270
925879 TA = 121
14911
MA = 121
07405
Ha = 222
792 n
mi
Hp = 213
426
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20463940
40 X = -6215189
05
Y = -2752632
60 feet Y = -908629
12 meter
Z = -8357856
17 Z = -2577720
18
XDOT = 9165
780206 XDOT = 2872
866746
YDOT = -15767
374719 feet/sec YDOT = -4774
211702 meter/sec
ZDOT = -17293
063906 ZDOT = -5257
162705
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11061267
79 X = 3371474
42
Y = -17369754
49 feet Y = -5294301
17 meter
Z = -8493738
09 Z = -2588891
37
XDOT = 9153
411495 XDOT = 2789
959824
YDOT = 14233
520078 feet/sec YDOT = 4338
376920 meter/sec
ZDOT = -17230
477638 ZDOT = -5251
849584
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 18318
56172454
00016717 00000-0 10270-3 0 9068
2 25544 51
6412 349
3645 0004979 46
6751 313
4815 15
53976248 21898
Satellite: ISS
Catalog Number: 25544
Epoch time: 18318
56172454 = yrday
fracday
Element set: 906
Inclination: 51
6412 deg
RA of node: 349
3645 deg
Eccentricity:
0004979
Arg of perigee: 46
6751 deg
Mean anomaly: 313
4815 deg
Mean motion: 15
53976248 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2189
Checksum: 340
Coasting Arc #8 (Orbit 2202)
---------------------------------------
Vector Time (GMT): 2018/319/09:49:38
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3742087
95 A = 6779732
37 meter
Y = 2940426
37 meter E =
0009714
Z = 4820312
48 I = 51
52970
XDOT = -6195
798113 Wp = 91
66825
YDOT = 3773
780354 meter/sec RA = 344
56785 deg
ZDOT = 2503
226192 TA = 333
68598
MA = 333
73529
Ha = 222
640 n
mi
Hp = 213
468
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12277191
45 X = 3685514
34
Y = 9647068
13 feet Y = 2981956
53 meter
Z = 15814673
48 Z = 4838353
14
XDOT = -20327
421631 XDOT = -6249
696596
YDOT = 12381
169142 feet/sec YDOT = 3704
193200 meter/sec
ZDOT = 8212
684358 ZDOT = 2472
997975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14817912
91 X = -4516499
86
Y = -4654676
15 feet Y = -1418745
29 meter
Z = 15895367
18 Z = 4844907
92
XDOT = 14262
947391 XDOT = 4347
346365
YDOT = -17773
930116 feet/sec YDOT = -5417
493899 meter/sec
ZDOT = 8076
219887 ZDOT = 2461
631821
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 18319
46203883
00016717 00000-0 10270-3 0 9070
2 25544 51
6414 344
8764 0004812 48
7424 311
4142 15
53997369 22033
Satellite: ISS
Catalog Number: 25544
Epoch time: 18319
46203883 = yrday
fracday
Element set: 907
Inclination: 51
6414 deg
RA of node: 344
8764 deg
Eccentricity:
0004812
Arg of perigee: 48
7424 deg
Mean anomaly: 311
4142 deg
Mean motion: 15
53997369 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2203
Checksum: 317
Coasting Arc #9 (Orbit 2214)
---------------------------------------
Vector Time (GMT): 2018/320/04:47:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5924213
99 A = 6789178
00 meter
Y = 3085442
84 meter E =
0016093
Z = 1185196
88 I = 51
53453
XDOT = -3168
288763 Wp = 106
06194
YDOT = -3812
083400 meter/sec RA = 340
59235 deg
ZDOT = -5850
891720 TA = 61
04505
MA = 60
88378
Ha = 222
808 n
mi
Hp = 213
432
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19436397
61 X = -5964033
11
Y = 10122843
97 feet Y = 3018971
50 meter
Z = 3888441
19 Z = 1156322
07
XDOT = -10394
648172 XDOT = -3097
004599
YDOT = -12506
835302 feet/sec YDOT = -3847
114726 meter/sec
ZDOT = -19195
838976 ZDOT = -5866
109294
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19643623
52 X = 5987376
45
Y = 9765741
50 feet Y = 2976598
01 meter
Z = 3758170
43 Z = 1145490
35
XDOT = -3349
578522 XDOT = -1020
951533
YDOT = 14231
592733 feet/sec YDOT = 4337
789465 meter/sec
ZDOT = -19263
712516 ZDOT = -5871
579575
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 18320
23373601
00016717 00000-0 10270-3 0 9084
2 25544 51
6401 341
0274 0004777 54
7102 305
4497 15
53989922 22159
Satellite: ISS
Catalog Number: 25544
Epoch time: 18320
23373601 = yrday
fracday
Element set: 908
Inclination: 51
6401 deg
RA of node: 341
0274 deg
Eccentricity:
0004777
Arg of perigee: 54
7102 deg
Mean anomaly: 305
4497 deg
Mean motion: 15
53989922 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2215
Checksum: 297
Coasting Arc #10 (Orbit 2223)
---------------------------------------
Vector Time (GMT): 2018/320/18:14:08
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4119762
31 A = 6779773
39 meter
Y = 2439030
27 meter E =
0010223
Z = 4791725
80 I = 51
48652
XDOT = -5656
964553 Wp = 92
15520
YDOT = 4508
357505 meter/sec RA = 337
82947 deg
ZDOT = 2563
762739 TA = 332
54477
MA = 332
59875
Ha = 222
692 n
mi
Hp = 213
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13516280
55 X = 4068906
21
Y = 8002067
81 feet Y = 2484815
91 meter
Z = 15720885
18 Z = 4811614
95
XDOT = -18559
594989 XDOT = -5719
411402
YDOT = 14791
199164 feet/sec YDOT = 4444
748207 meter/sec
ZDOT = 8411
295077 ZDOT = 2536
131172
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7234108
19 X = 2204956
17
Y = 13841316
37 feet Y = 4218833
23 meter
Z = 15809958
89 Z = 4818875
47
XDOT = -22595
426402 XDOT = -6887
085967
YDOT = 2325
381362 feet/sec YDOT = 708
776239 meter/sec
ZDOT = 8286
416870 ZDOT = 2525
699862
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 18320
81250524
00016717 00000-0 10270-3 0 9097
2 25544 51
6404 338
1480 0005007 51
9618 308
1985 15
54019810 22249
Satellite: ISS
Catalog Number: 25544
Epoch time: 18320
81250524 = yrday
fracday
Element set: 909
Inclination: 51
6404 deg
RA of node: 338
1480 deg
Eccentricity:
0005007
Arg of perigee: 51
9618 deg
Mean anomaly: 308
1985 deg
Mean motion: 15
54019810 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2224
Checksum: 290
Coasting Arc #11 (Orbit 2238)
---------------------------------------
Vector Time (GMT): 2018/321/18:14:08
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2671642
14 A = 6777870
62 meter
Y = -3348316
93 meter E =
0019254
Z = -5269405
91 I = 51
45033
XDOT = 6484
530756 Wp = 76
54264
YDOT = -3997
430096 meter/sec RA = 332
82107 deg
ZDOT = -745
567220 TA = 186
29036
MA = 186
31457
Ha = 222
898 n
mi
Hp = 213
134
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8765230
11 X = -2608405
36
Y = -10985291
77 feet Y = -3377839
51 meter
Z = -17288077
13 Z = -5282230
43
XDOT = 21274
707206 XDOT = 6532
370820
YDOT = -13114
928135 feet/sec YDOT = -3924
648076 meter/sec
ZDOT = -2446
086680 ZDOT = -713
950931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1854176
49 X = -565152
99
Y = -13859566
10 feet Y = -4224395
75 meter
Z = -17345257
63 Z = -5286834
52
XDOT = 23991
075158 XDOT = 7312
479708
YDOT = -318
387024 feet/sec YDOT = -97
044365 meter/sec
ZDOT = -2303
380299 ZDOT = -702
070315
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 18321
77711982
00016717 00000-0 10270-3 0 9105
2 25544 51
6411 333
3402 0005141 55
0242 305
1392 15
54009807 22395
Satellite: ISS
Catalog Number: 25544
Epoch time: 18321
77711982 = yrday
fracday
Element set: 910
Inclination: 51
6411 deg
RA of node: 333
3402 deg
Eccentricity:
0005141
Arg of perigee: 55
0242 deg
Mean anomaly: 305
1392 deg
Mean motion: 15
54009807 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2239
Checksum: 274
Coasting Arc #12 (Orbit 2248)
---------------------------------------
Vector Time (GMT): 2018/322/09:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 917504
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4577677
05 A = 6780159
39 meter
Y = -1683943
95 meter E =
0016067
Z = -4725163
79 I = 51
43915
XDOT = 4776
394177 Wp = 67
25257
YDOT = -5321
958071 meter/sec RA = 329
63918 deg
ZDOT = -2732
038889 TA = 175
59872
MA = 175
58457
Ha = 222
931 n
mi
Hp = 213
081
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15018625
49 X = -4535553
74
Y = -5524750
50 feet Y = -1734899
21 meter
Z = -15502505
86 Z = -4747298
62
XDOT = 15670
584571 XDOT = 4848
821842
YDOT = -17460
492359 feet/sec YDOT = -5268
140153 meter/sec
ZDOT = -8963
382181 ZDOT = -2708
660483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15905778
76 X = 4848081
37
Y = 21166
29 feet Y = 6451
49 meter
Z = -15601776
23 Z = -4755421
39
XDOT = -8711
397405 XDOT = -2655
233929
YDOT = 20666
882608 feet/sec YDOT = 6299
265819 meter/sec
ZDOT = -8857
531628 ZDOT = -2699
775640
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 18322
42019182
00016717 00000-0 10270-3 0 9112
2 25544 51
6411 330
1338 0005048 60
0773 300
0880 15
53995916 22490
Satellite: ISS
Catalog Number: 25544
Epoch time: 18322
42019182 = yrday
fracday
Element set: 911
Inclination: 51
6411 deg
RA of node: 330
1338 deg
Eccentricity:
0005048
Arg of perigee: 60
0773 deg
Mean anomaly: 300
0880 deg
Mean motion: 15
53995916 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2249
Checksum: 286
Coasting Arc #13 (Orbit 2255)
---------------------------------------
Vector Time (GMT): 2018/322/19:30:01
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5961457
56 A = 6785506
41 meter
Y = -852638
63 meter E =
0017686
Z = 3107245
09 I = 51
44639
XDOT = -1729
106037 Wp = 77
32728
YDOT = 5684
400629 meter/sec RA = 327
57952 deg
ZDOT = 4857
662934 TA = 318
57040
MA = 318
70438
Ha = 222
866 n
mi
Hp = 213
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19558587
80 X = 5955455
29
Y = -2797370
84 feet Y = -786007
02 meter
Z = 10194373
66 Z = 3136189
75
XDOT = -5672
920070 XDOT = -1816
138491
YDOT = 18649
608363 feet/sec YDOT = 5664
577952 meter/sec
ZDOT = 15937
214349 ZDOT = 4849
051968
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19672316
14 X = 5996121
96
Y = 831418
69 feet Y = 253416
42 meter
Z = 10324612
12 Z = 3146941
77
XDOT = -9046
177194 XDOT = -2757
274809
YDOT = 15837
235885 feet/sec YDOT = 4827
189498 meter/sec
ZDOT = 15897
703880 ZDOT = 4845
620143
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 18322
87034216
00016717 00000-0 10270-3 0 9127
2 25544 51
6422 327
8918 0005198 58
3062 301
8597 15
53998705 22567
Satellite: ISS
Catalog Number: 25544
Epoch time: 18322
87034216 = yrday
fracday
Element set: 912
Inclination: 51
6422 deg
RA of node: 327
8918 deg
Eccentricity:
0005198
Arg of perigee: 58
3062 deg
Mean anomaly: 301
8597 deg
Mean motion: 15
53998705 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2256
Checksum: 328
Coasting Arc #14 (Orbit 2270)
---------------------------------------
Vector Time (GMT): 2018/323/19:30:01
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5240396
24 A = 6781665
63 meter
Y = -318976
46 meter E =
0013710
Z = -4307090
91 I = 51
40575
XDOT = 3237
053744 Wp = 65
98275
YDOT = -5991
940826 meter/sec RA = 322
58112 deg
ZDOT = -3498
110193 TA = 168
26027
MA = 168
22827
Ha = 222
910 n
mi
Hp = 213
012
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17192901
04 X = -5215517
83
Y = -1046510
70 feet Y = -377439
09 meter
Z = -14130875
69 Z = -4332487
08
XDOT = 10620
255064 XDOT = 3320
809067
YDOT = -19658
598510 feet/sec YDOT = -5955
273524 meter/sec
ZDOT = -11476
739477 ZDOT = -3482
181946
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16684264
66 X = -5085363
87
Y = -3884359
82 feet Y = -1183952
87 meter
Z = -14244990
00 Z = -4341872
95
XDOT = 13541
976800 XDOT = 4127
594529
YDOT = -16383
671155 feet/sec YDOT = -4993
742968 meter/sec
ZDOT = -11404
302097 ZDOT = -3476
031279
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 18323
83494496
00016717 00000-0 10270-3 0 9135
2 25544 51
6415 323
0848 0005096 61
0989 299
0674 15
54022847 22712
Satellite: ISS
Catalog Number: 25544
Epoch time: 18323
83494496 = yrday
fracday
Element set: 913
Inclination: 51
6415 deg
RA of node: 323
0848 deg
Eccentricity:
0005096
Arg of perigee: 61
0989 deg
Mean anomaly: 299
0674 deg
Mean motion: 15
54022847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2271
Checksum: 331
Coasting Arc #15 (Orbit 2286)
---------------------------------------
Vector Time (GMT): 2018/324/19:30:01
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4233233
96 A = 6778711
11 meter
Y = 1589893
83 meter E =
0009115
Z = 5042418
49 I = 51
37023
XDOT = -4420
944812 Wp = 95
68561
YDOT = 6005
334780 meter/sec RA = 317
57054 deg
ZDOT = 1814
269697 TA = 336
67933
MA = 336
72065
Ha = 222
819 n
mi
Hp = 213
097
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13888562
86 X = 4190646
67
Y = 5216187
11 feet Y = 1636994
57 meter
Z = 16543367
76 Z = 5062879
19
XDOT = -14504
412113 XDOT = -4496
582556
YDOT = 19702
541930 feet/sec YDOT = 5955
473750 meter/sec
ZDOT = 5952
328401 ZDOT = 1792
610139
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12841161
84 X = 3913986
13
Y = 7222279
11 feet Y = 2201350
67 meter
Z = 16635114
97 Z = 5070383
04
XDOT = -16804
175993 XDOT = -5121
912843
YDOT = 16365
909728 feet/sec YDOT = 4988
329285 meter/sec
ZDOT = 5854
136817 ZDOT = 1784
340902
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 18324
86385178
00016717 00000-0 10270-3 0 9146
2 25544 51
6416 317
9563 0005099 65
8926 294
2759 15
54020615 22874
Satellite: ISS
Catalog Number: 25544
Epoch time: 18324
86385178 = yrday
fracday
Element set: 914
Inclination: 51
6416 deg
RA of node: 317
9563 deg
Eccentricity:
0005099
Arg of perigee: 65
8926 deg
Mean anomaly: 294
2759 deg
Mean motion: 15
54020615 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2287
Checksum: 344
Coasting Arc #16 (Orbit 2301)
---------------------------------------
Vector Time (GMT): 2018/325/19:30:01
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3076113
99 A = 6777597
72 meter
Y = -2921423
75 meter E =
0019611
Z = -5302639
45 I = 51
34290
XDOT = 5213
723051 Wp = 84
58731
YDOT = -5603
166784 meter/sec RA = 312
55191 deg
ZDOT = 64
482499 TA = 186
01904
MA = 186
04264
Ha = 222
902 n
mi
Hp = 212
922
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10092237
49 X = -3017459
06
Y = -9584723
59 feet Y = -2955494
81 meter
Z = -17397111
05 Z = -5317440
21
XDOT = 17105
390586 XDOT = 5275
678499
YDOT = -18383
093124 feet/sec YDOT = -5544
516899 meter/sec
ZDOT = 211
556756 ZDOT = 89
959893
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8615267
64 X = -2625933
58
Y = -10825541
40 feet Y = -3299625
02 meter
Z = -17463232
05 Z = -5322793
13
XDOT = 18603
224175 XDOT = 5670
262729
YDOT = -15321
565143 feet/sec YDOT = -4670
013055 meter/sec
ZDOT = 326
844240 ZDOT = 99
622124
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 18325
82844590
00016717 00000-0 10270-3 0 9152
2 25544 51
6416 313
1480 0005051 67
5322 292
6365 15
54048263 23029
Satellite: ISS
Catalog Number: 25544
Epoch time: 18325
82844590 = yrday
fracday
Element set: 915
Inclination: 51
6416 deg
RA of node: 313
1480 deg
Eccentricity:
0005051
Arg of perigee: 67
5322 deg
Mean anomaly: 292
6365 deg
Mean motion: 15
54048263 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2302
Checksum: 295
Coasting Arc #17 (Orbit 2303)
---------------------------------------
Vector Time (GMT): 2018/325/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5518849
23 A = 6786242
62 meter
Y = 2814304
48 meter E =
0008811
Z = -2777468
54 I = 51
36561
XDOT = -349
921780 Wp = 92
62054
YDOT = -5705
416290 meter/sec RA = 311
98229 deg
ZDOT = -5100
228106 TA = 118
96185
MA = 118
87349
Ha = 222
909 n
mi
Hp = 212
990
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18106460
72 X = -5536417
55
Y = 9233282
41 feet Y = 2752490
77 meter
Z = -9112429
59 Z = -2804320
47
XDOT = -1148
037336 XDOT = -261
321317
YDOT = -18718
557381 feet/sec YDOT = -5708
833728 meter/sec
ZDOT = -16733
031844 ZDOT = -5101
713012
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9491473
48 X = -2893001
12
Y = 17910556
63 feet Y = 5459137
66 meter
Z = -9233509
05 Z = -2814373
56
XDOT = -10276
021772 XDOT = -3132
131436
YDOT = -14051
031506 feet/sec YDOT = -4282
754403 meter/sec
ZDOT = -16738
917724 ZDOT = -5102
022122
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 18325
95705774
00016717 00000-0 10270-3 0 9167
2 25544 51
6381 312
5043 0005054 68
6004 291
5688 15
54034614 23043
Satellite: ISS
Catalog Number: 25544
Epoch time: 18325
95705774 = yrday
fracday
Element set: 916
Inclination: 51
6381 deg
RA of node: 312
5043 deg
Eccentricity:
0005054
Arg of perigee: 68
6004 deg
Mean anomaly: 291
5688 deg
Mean motion: 15
54034614 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2304
Checksum: 304
Coasting Arc #18 (Orbit 2319)
---------------------------------------
Vector Time (GMT): 2018/326/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5215946
66 A = 6782561
98 meter
Y = -1564284
13 meter E =
0015143
Z = 4030968
61 I = 51
33128
XDOT = -1043
489588 Wp = 92
99621
YDOT = 6541
465019 meter/sec RA = 306
97946 deg
ZDOT = 3875
371779 TA = 316
64704
MA = 316
76607
Ha = 222
776 n
mi
Hp = 213
038
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17112685
90 X = 5213470
41
Y = -5132165
77 feet Y = -1505969
92 meter
Z = 13224962
63 Z = 4056300
44
XDOT = -3423
522271 XDOT = -1135
385546
YDOT = 21461
499405 feet/sec YDOT = 6529
281897 meter/sec
ZDOT = 12714
474339 ZDOT = 3870
079986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10764498
43 X = 3281019
12
Y = -14151979
63 feet Y = -4313523
39 meter
Z = 13339033
95 Z = 4065737
55
XDOT = 8734
698527 XDOT = 2662
336111
YDOT = 18645
828775 feet/sec YDOT = 5683
248611 meter/sec
ZDOT = 12689
791110 ZDOT = 3867
848330
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 18326
98595345
00016717 00000-0 10270-3 0 9173
2 25544 51
6374 307
3753 0004936 73
2496 286
9198 15
54041354 23201
Satellite: ISS
Catalog Number: 25544
Epoch time: 18326
98595345 = yrday
fracday
Element set: 917
Inclination: 51
6374 deg
RA of node: 307
3753 deg
Eccentricity:
0004936
Arg of perigee: 73
2496 deg
Mean anomaly: 286
9198 deg
Mean motion: 15
54041354 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2320
Checksum: 338
Coasting Arc #19 (Orbit 2334)
---------------------------------------
Vector Time (GMT): 2018/327/22:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4684112
12 A = 6779229
61 meter
Y = 66361
67 meter E =
0017420
Z = -4916478
35 I = 51
30081
XDOT = 2241
827882 Wp = 74
90316
YDOT = -6970
365739 meter/sec RA = 301
96519 deg
ZDOT = -2232
152365 TA = 173
16825
MA = 173
14448
Ha = 222
979 n
mi
Hp = 212
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15367821
92 X = -4660623
81
Y = 217722
02 feet Y = 14112
46 meter
Z = -16130178
31 Z = -4939175
65
XDOT = 7355
078352 XDOT = 2330
448726
YDOT = -22868
654000 feet/sec YDOT = -6944
800347 meter/sec
ZDOT = -7323
334532 ZDOT = -2221
047467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12064306
41 X = -3677200
59
Y = 9347089
91 feet Y = 2848993
00 meter
Z = -16232203
39 Z = -4947575
59
XDOT = -7150
594297 XDOT = -2179
501142
YDOT = -21846
269096 feet/sec YDOT = -6658
742820 meter/sec
ZDOT = -7272
471018 ZDOT = -2216
649166
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 18327
95053992
00016717 00000-0 10270-3 0 9189
2 25544 51
6372 302
5668 0005117 78
5641 281
6086 15
54045330 23355
Satellite: ISS
Catalog Number: 25544
Epoch time: 18327
95053992 = yrday
fracday
Element set: 918
Inclination: 51
6372 deg
RA of node: 302
5668 deg
Eccentricity:
0005117
Arg of perigee: 78
5641 deg
Mean anomaly: 281
6086 deg
Mean motion: 15
54045330 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2335
Checksum: 318
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