[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 14th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 24007 8258 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 049 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
319/09:49:38
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
5
320/05:28:00
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
5
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
0 223
0
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
325/21:45:00
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
Coasting Arc #1 (Orbit 2156)
---------------------------------------
Vector Time (GMT): 2018/316/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6261652
13 A = 6788193
18 meter
Y = -1683840
07 meter E =
0011825
Z = -1995691
52 I = 51
65232
XDOT = 2941
989032 Wp = 38
81451
YDOT = 4362
938606 meter/sec RA = 359
04097 deg
ZDOT = 5576
467184 TA = 299
15593
MA = 299
27421
Ha = 222
781 n
mi
Hp = 213
709
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20543478
13 X = 6289710
10
Y = -5524409
67 feet Y = -1613660
94 meter
Z = -6547544
35 Z = -1965206
00
XDOT = 9652
194988 XDOT = 2865
894780
YDOT = 14314
103039 feet/sec YDOT = 4395
412204 meter/sec
ZDOT = 18295
496012 ZDOT = 5590
574002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8767666
41 X = -2672384
72
Y = 19428361
93 feet Y = 5921764
72 meter
Z = -6410203
68 Z = -1953830
08
XDOT = -15697
027908 XDOT = -4784
454106
YDOT = -1056
381499 feet/sec YDOT = -321
985081 meter/sec
ZDOT = 18358
297501 ZDOT = 5595
609078
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
50385145
00016717 00000-0 10270-3 0 9007
2 25544 51
6409 359
6196 0004941 38
8013 321
3494 15
53960916 21573
Satellite: ISS
Catalog Number: 25544
Epoch time: 18316
50385145 = yrday
fracday
Element set: 900
Inclination: 51
6409 deg
RA of node: 359
6196 deg
Eccentricity:
0004941
Arg of perigee: 38
8013 deg
Mean anomaly: 321
3494 deg
Mean motion: 15
53960916 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2157
Checksum: 314
Coasting Arc #2 (Orbit 2172)
---------------------------------------
Vector Time (GMT): 2018/317/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6706136
32 A = 6789729
91 meter
Y = 976708
17 meter E =
0013692
Z = 351939
50 I = 51
62465
XDOT = -1004
533178 Wp = 109
64653
YDOT = -4669
641272 meter/sec RA = 354
07042 deg
ZDOT = -5996
326951 TA = 66
56033
MA = 66
41644
Ha = 222
762 n
mi
Hp = 213
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22001759
59 X = -6718269
29
Y = 3204423
12 feet Y = 901647
64 meter
Z = 1154657
16 Z = 319333
52
XDOT = -3295
712525 XDOT = -923
113870
YDOT = -15320
345380 feet/sec YDOT = -4680
419129 meter/sec
ZDOT = -19672
988686 ZDOT = -6001
009164
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11134552
59 X = 3393811
63
Y = -19253178
49 feet Y = -5868368
80 meter
Z = 1007890
12 Z = 307204
91
XDOT = 12578
444449 XDOT = 3833
909868
YDOT = 6206
952129 feet/sec YDOT = 1891
879009 meter/sec
ZDOT = -19693
362702 ZDOT = -6002
536952
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
53279802
00016717 00000-0 10270-3 0 9014
2 25544 51
6410 354
4915 0004999 42
6889 317
4652 15
53976336 21737
Satellite: ISS
Catalog Number: 25544
Epoch time: 18317
53279802 = yrday
fracday
Element set: 901
Inclination: 51
6410 deg
RA of node: 354
4915 deg
Eccentricity:
0004999
Arg of perigee: 42
6889 deg
Mean anomaly: 317
4652 deg
Mean motion: 15
53976336 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2173
Checksum: 335
Coasting Arc #3 (Orbit 2188)
---------------------------------------
Vector Time (GMT): 2018/318/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6653314
33 A = 6789159
67 meter
Y = -249461
47 meter E =
0018915
Z = 1277971
70 I = 51
58926
XDOT = -946
943576 Wp = 55
41713
YDOT = 4893
262217 meter/sec RA = 349
09872 deg
ZDOT = 5834
157853 TA = 318
50300
MA = 318
64647
Ha = 222
925 n
mi
Hp = 213
458
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21828459
09 X = 6649401
60
Y = -818443
15 feet Y = -175081
42 meter
Z = 4192820
54 Z = 1310282
10
XDOT = -3106
770262 XDOT = -1029
930648
YDOT = 16054
009897 feet/sec YDOT = 4882
208600 meter/sec
ZDOT = 19140
937837 ZDOT = 5829
356496
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12572297
57 X = -3832036
30
Y = 17828321
52 feet Y = 5434072
40 meter
Z = 4338145
37 Z = 1322266
71
XDOT = -9503
104551 XDOT = -2896
546267
YDOT = -11392
887906 feet/sec YDOT = -3472
552234 meter/sec
ZDOT = 19118
636793 ZDOT = 5827
360495
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
56174252
00016717 00000-0 10270-3 0 9022
2 25544 51
6407 349
3636 0005225 46
2312 313
9272 15
53934233 21896
Satellite: ISS
Catalog Number: 25544
Epoch time: 18318
56174252 = yrday
fracday
Element set: 902
Inclination: 51
6407 deg
RA of node: 349
3636 deg
Eccentricity:
0005225
Arg of perigee: 46
2312 deg
Mean anomaly: 313
9272 deg
Mean motion: 15
53934233 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2189
Checksum: 302
Coasting Arc #4 (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 = 3753682
94 A = 6779783
95 meter
Y = 2933367
89 meter E =
0009742
Z = 4815641
95 I = 51
52963
XDOT = -6186
794373 Wp = 91
52448
YDOT = 3780
857045 meter/sec RA = 344
56749 deg
ZDOT = 2514
764714 TA = 333
70856
MA = 333
75798
Ha = 222
660 n
mi
Hp = 213
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12315232
76 X = 3697210
09
Y = 9623910
39 feet Y = 2975028
28 meter
Z = 15799350
22 Z = 4833739
18
XDOT = -20297
881801 XDOT = -6240
828707
YDOT = 12404
386631 feet/sec YDOT = 3711
369817 meter/sec
ZDOT = 8250
540401 ZDOT = 2484
579905
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14845244
47 X = -4524830
51
Y = -4619403
36 feet Y = -1407994
14 meter
Z = 15880299
30 Z = 4840315
23
XDOT = 14229
863199 XDOT = 4337
262303
YDOT = -17783
141621 feet/sec YDOT = -5420
301566 meter/sec
ZDOT = 8114
270089 ZDOT = 2473
229523
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
46206084
00016717 00000-0 10270-3 0 9032
2 25544 51
6413 344
8760 0004828 48
4835 311
6731 15
53986178 22030
Satellite: ISS
Catalog Number: 25544
Epoch time: 18319
46206084 = yrday
fracday
Element set: 903
Inclination: 51
6413 deg
RA of node: 344
8760 deg
Eccentricity:
0004828
Arg of perigee: 48
4835 deg
Mean anomaly: 311
6731 deg
Mean motion: 15
53986178 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2203
Checksum: 316
Coasting Arc #5 (Orbit 2214)
---------------------------------------
Vector Time (GMT): 2018/320/05:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 902349
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4516014
50 A = 6786175
23 meter
Y = -4106524
58 meter E =
0009335
Z = -2966242
97 I = 51
52417
XDOT = 5351
463439 Wp = 59
01769
YDOT = 2299
258645 meter/sec RA = 340
43801 deg
ZDOT = 4980
647800 TA = 267
04369
MA = 267
15052
Ha = 222
895 n
mi
Hp = 213
506
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14816320
54 X = 4576007
79
Y = -13472849
69 feet Y = -4055687
88 meter
Z = -9731768
28 Z = -2944159
82
XDOT = 17557
294749 XDOT = 5301
161085
YDOT = 7543
499491 feet/sec YDOT = 2358
821081 meter/sec
ZDOT = 16340
708006 ZDOT = 5006
521550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20067555
57 X = -6116590
94
Y = -517974
43 feet Y = -157878
61 meter
Z = -9631887
81 Z = -2935799
40
XDOT = -7458
814282 XDOT = -2273
446593
YDOT = -16037
693447 feet/sec YDOT = -4888
288963 meter/sec
ZDOT = 16456
711298 ZDOT = 5016
005604
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
23376399
00016717 00000-0 10270-3 0 9047
2 25544 51
6410 341
0279 0004828 53
0675 307
0920 15
53955283 22150
Satellite: ISS
Catalog Number: 25544
Epoch time: 18320
23376399 = yrday
fracday
Element set: 904
Inclination: 51
6410 deg
RA of node: 341
0279 deg
Eccentricity:
0004828
Arg of perigee: 53
0675 deg
Mean anomaly: 307
0920 deg
Mean motion: 15
53955283 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2215
Checksum: 301
Coasting Arc #6 (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 = 4135638
12 A = 6779843
05 meter
Y = 2426372
63 meter E =
0010270
Z = 4784532
06 I = 51
48648
XDOT = -5642
098994 Wp = 92
00490
YDOT = 4517
133296 meter/sec RA = 337
82925 deg
ZDOT = 2580
986461 TA = 332
51300
MA = 332
56728
Ha = 222
717 n
mi
Hp = 213
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13568366
53 X = 4084957
33
Y = 7960540
13 feet Y = 2472336
79 meter
Z = 15697283
65 Z = 4804498
75
XDOT = -18510
823472 XDOT = -5704
728746
YDOT = 14819
991128 feet/sec YDOT = 4453
689212 meter/sec
ZDOT = 8467
803351 ZDOT = 2553
426662
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7300362
07 X = 2225150
36
Y = 13833295
11 feet Y = 4216388
35 meter
Z = 15786707
81 Z = 4811788
54
XDOT = -22569
863744 XDOT = -6879
294469
YDOT = 2370
425028 feet/sec YDOT = 722
505548 meter/sec
ZDOT = 8343
246565 ZDOT = 2543
021553
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
81253819
00016717 00000-0 10270-3 0 9053
2 25544 51
6403 338
1476 0005024 51
7031 308
4573 15
54005893 22241
Satellite: ISS
Catalog Number: 25544
Epoch time: 18320
81253819 = yrday
fracday
Element set: 905
Inclination: 51
6403 deg
RA of node: 338
1476 deg
Eccentricity:
0005024
Arg of perigee: 51
7031 deg
Mean anomaly: 308
4573 deg
Mean motion: 15
54005893 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2224
Checksum: 288
Coasting Arc #7 (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 = -2695167
69 A = 6777926
96 meter
Y = -3333816
68 meter E =
0019248
Z = -5266685
99 I = 51
45023
XDOT = 6472
144369 Wp = 76
30853
YDOT = -4012
821286 meter/sec RA = 332
82105 deg
ZDOT = -769
843006 TA = 186
29020
MA = 186
31440
Ha = 222
926 n
mi
Hp = 213
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8842413
68 X = -2632104
53
Y = -10937718
77 feet Y = -3363603
31 meter
Z = -17279153
50 Z = -5279625
21
XDOT = 21234
069452 XDOT = 6520
275382
YDOT = -13165
424168 feet/sec YDOT = -3940
176153 meter/sec
ZDOT = -2525
731646 ZDOT = -738
286180
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1944878
08 X = -592798
84
Y = -13857926
93 feet Y = -4223896
13 meter
Z = -17336851
72 Z = -5284272
40
XDOT = 23982
374224 XDOT = 7309
827663
YDOT = -375
656998 feet/sec YDOT = -114
500253 meter/sec
ZDOT = -2383
290412 ZDOT = -726
426917
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
77716187
00016717 00000-0 10270-3 0 9062
2 25544 51
6410 333
3398 0005157 54
7475 305
4160 15
53994446 22396
Satellite: ISS
Catalog Number: 25544
Epoch time: 18321
77716187 = yrday
fracday
Element set: 906
Inclination: 51
6410 deg
RA of node: 333
3398 deg
Eccentricity:
0005157
Arg of perigee: 54
7475 deg
Mean anomaly: 305
4160 deg
Mean motion: 15
53994446 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2239
Checksum: 322
Coasting Arc #8 (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 = -4597715
84 A = 6780253
07 meter
Y = -1661593
96 meter E =
0016008
Z = -4713682
14 I = 51
43917
XDOT = 4751
904446 Wp = 67
05682
YDOT = -5330
877696 meter/sec RA = 329
63916 deg
ZDOT = -2757
219916 TA = 175
52333
MA = 175
50900
Ha = 222
960 n
mi
Hp = 213
106
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15084369
55 X = -4555896
74
Y = -5451423
75 feet Y = -1712775
00 meter
Z = -15464836
42 Z = -4735915
06
XDOT = 15590
237685 XDOT = 4824
555992
YDOT = -17489
756221 feet/sec YDOT = -5277
332387 meter/sec
ZDOT = -9045
997099 ZDOT = -2733
959930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15942307
88 X = 4859215
44
Y = -70474
19 feet Y = -21480
53 meter
Z = -15564550
88 Z = -4744075
11
XDOT = -8633
086213 XDOT = -2631
364678
YDOT = 20664
056885 feet/sec YDOT = 6298
404539 meter/sec
ZDOT = -8940
677653 ZDOT = -2725
118549
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
42024052
00016717 00000-0 10270-3 0 9079
2 25544 51
6409 330
1335 0005063 59
7757 300
3896 15
53979389 22494
Satellite: ISS
Catalog Number: 25544
Epoch time: 18322
42024052 = yrday
fracday
Element set: 907
Inclination: 51
6409 deg
RA of node: 330
1335 deg
Eccentricity:
0005063
Arg of perigee: 59
7757 deg
Mean anomaly: 300
3896 deg
Mean motion: 15
53979389 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2249
Checksum: 317
Coasting Arc #9 (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 = 5969318
43 A = 6785616
27 meter
Y = -878678
23 meter E =
0017739
Z = 3084983
14 I = 51
44646
XDOT = -1694
082044 Wp = 76
97534
YDOT = 5679
338601 meter/sec RA = 327
57932 deg
ZDOT = 4875
854143 TA = 318
62529
MA = 318
75951
Ha = 222
897 n
mi
Hp = 213
193
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19584378
05 X = 5963714
90
Y = -2882802
60 feet Y = -811956
49 meter
Z = 10121335
76 Z = 3113966
96
XDOT = -5558
011957 XDOT = -1781
148862
YDOT = 18633
000661 feet/sec YDOT = 5659
907395 meter/sec
ZDOT = 15996
896794 ZDOT = 4867
413231
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19713840
19 X = 6008778
49
Y = 752262
56 feet Y = 229289
63 meter
Z = 10251753
90 Z = 3124734
59
XDOT = -8936
339925 XDOT = -2723
796409
YDOT = 15838
922786 feet/sec YDOT = 4827
703665 meter/sec
ZDOT = 15958
151503 ZDOT = 4864
044578
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
87039581
00016717 00000-0 10270-3 0 9082
2 25544 51
6420 327
8915 0005213 58
0031 302
1628 15
53981322 22569
Satellite: ISS
Catalog Number: 25544
Epoch time: 18322
87039581 = yrday
fracday
Element set: 908
Inclination: 51
6420 deg
RA of node: 327
8915 deg
Eccentricity:
0005213
Arg of perigee: 58
0031 deg
Mean anomaly: 302
1628 deg
Mean motion: 15
53981322 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2256
Checksum: 295
Coasting Arc #10 (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 = -5258470
21 A = 6781793
73 meter
Y = -285415
36 meter E =
0013614
Z = -4287461
52 I = 51
40586
XDOT = 3199
669691 Wp = 65
86662
YDOT = -5994
078459 meter/sec RA = 322
58123 deg
ZDOT = -3528
727635 TA = 168
01457
MA = 167
98214
Ha = 222
943 n
mi
Hp = 213
042
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17252198
86 X = -5234061
10
Y = -936402
11 feet Y = -344082
74 meter
Z = -14066474
80 Z = -4312946
63
XDOT = 10497
603974 XDOT = 3283
600424
YDOT = -19665
611743 feet/sec YDOT = -5957
828231 meter/sec
ZDOT = -11577
190402 ZDOT = -3512
980565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16761517
07 X = -5108910
40
Y = -3785748
80 feet Y = -1153896
23 meter
Z = -14180993
59 Z = -4322366
85
XDOT = 13430
067273 XDOT = 4093
484505
YDOT = -16405
302468 feet/sec YDOT = -5000
336192 meter/sec
ZDOT = -11505
567135 ZDOT = -3506
896863
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
83500996
00016717 00000-0 10270-3 0 9093
2 25544 51
6414 323
0846 0005111 60
7787 299
3876 15
54003360 22715
Satellite: ISS
Catalog Number: 25544
Epoch time: 18323
83500996 = yrday
fracday
Element set: 909
Inclination: 51
6414 deg
RA of node: 323
0846 deg
Eccentricity:
0005111
Arg of perigee: 60
7787 deg
Mean anomaly: 299
3876 deg
Mean motion: 15
54003360 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2271
Checksum: 312
Coasting Arc #11 (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 = 4262762
51 A = 6778825
85 meter
Y = 1549639
98 meter E =
0009215
Z = 5030154
89 I = 51
37027
XDOT = -4384
488774 Wp = 95
68949
YDOT = 6018
793261 meter/sec RA = 317
57100 deg
ZDOT = 1857
554819 TA = 336
24029
MA = 336
28280
Ha = 222
857 n
mi
Hp = 213
129
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13985441
31 X = 4220682
73
Y = 5084120
67 feet Y = 1597073
77 meter
Z = 16503132
86 Z = 5050760
27
XDOT = -14384
805690 XDOT = -4460
489986
YDOT = 19746
697051 feet/sec YDOT = 5969
337875 meter/sec
ZDOT = 6094
339958 ZDOT = 1836
071474
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12956991
95 X = 3949291
15
Y = 7106250
18 feet Y = 2165985
05 meter
Z = 16595535
96 Z = 5058319
36
XDOT = -16701
932860 XDOT = -5090
749136
YDOT = 16418
903640 feet/sec YDOT = 5004
481830 meter/sec
ZDOT = 5996
938555 ZDOT = 1827
866872
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
86393006
00016717 00000-0 10270-3 0 9101
2 25544 51
6415 317
9562 0005117 65
5407 294
6279 15
53999140 22872
Satellite: ISS
Catalog Number: 25544
Epoch time: 18324
86393006 = yrday
fracday
Element set: 910
Inclination: 51
6415 deg
RA of node: 317
9562 deg
Eccentricity:
0005117
Arg of perigee: 65
5407 deg
Mean anomaly: 294
6279 deg
Mean motion: 15
53999140 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2287
Checksum: 327
Coasting Arc #12 (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 = -3117306
42 A = 6777660
48 meter
Y = -2876986
30 meter E =
0019632
Z = -5302980
77 I = 51
34276
XDOT = 5182
587172 Wp = 84
16856
YDOT = -5632
263066 meter/sec RA = 312
55266 deg
ZDOT = 11
085685 TA = 185
92608
MA = 185
94934
Ha = 222
941 n
mi
Hp = 212
954
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10227383
27 X = -3059143
68
Y = -9438931
42 feet Y = -2911520
75 meter
Z = -17398230
87 Z = -5317982
83
XDOT = 17003
238753 XDOT = 5245
129678
YDOT = -18478
553367 feet/sec YDOT = -5573
958080 meter/sec
ZDOT = 36
370359 ZDOT = 36
413252
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8768561
28 X = -2672657
48
Y = -10698979
45 feet Y = -3261048
93 meter
Z = -17465262
78 Z = -5323412
10
XDOT = 18525
038653 XDOT = 5646
431782
YDOT = -15418
420866 feet/sec YDOT = -4699
534680 meter/sec
ZDOT = 150
988442 ZDOT = 46
021277
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
82853767
00016717 00000-0 10270-3 0 9114
2 25544 51
6415 313
1479 0005068 67
1628 293
0059 15
54025864 23026
Satellite: ISS
Catalog Number: 25544
Epoch time: 18325
82853767 = yrday
fracday
Element set: 911
Inclination: 51
6415 deg
RA of node: 313
1479 deg
Eccentricity:
0005068
Arg of perigee: 67
1628 deg
Mean anomaly: 293
0059 deg
Mean motion: 15
54025864 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2302
Checksum: 314
Coasting Arc #13 (Orbit 2303)
---------------------------------------
Vector Time (GMT): 2018/325/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4216289
33 A = 6778559
82 meter
Y = 1425434
00 meter E =
0008679
Z = 5105408
86 I = 51
34112
XDOT = -4038
664689 Wp = 95
30296
YDOT = 6335
958417 meter/sec RA = 312
09491 deg
ZDOT = 1563
233345 TA = 339
55933
MA = 339
59404
Ha = 222
894 n
mi
Hp = 213
141
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13832970
24 X = 4175236
30
Y = 4676620
74 feet Y = 1472353
71 meter
Z = 16750029
06 Z = 5125791
04
XDOT = -13250
212235 XDOT = -4116
808553
YDOT = 20787
265149 feet/sec YDOT = 6290
358263 meter/sec
ZDOT = 5128
718325 ZDOT = 1543
424858
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14376372
08 X = 4381918
21
Y = -1863069
73 feet Y = -567863
65 meter
Z = 16841443
46 Z = 5133271
97
XDOT = -2873
181081 XDOT = -875
745593
YDOT = 23468
993453 feet/sec YDOT = 7153
349204 meter/sec
ZDOT = 5038
810162 ZDOT = 1535
829337
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
95715235
00016717 00000-0 10270-3 0 9126
2 25544 51
6393 312
5051 0005094 68
2831 291
8864 15
53978826 23043
Satellite: ISS
Catalog Number: 25544
Epoch time: 18325
95715235 = yrday
fracday
Element set: 912
Inclination: 51
6393 deg
RA of node: 312
5051 deg
Eccentricity:
0005094
Arg of perigee: 68
2831 deg
Mean anomaly: 291
8864 deg
Mean motion: 15
53978826 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2304
Checksum: 323
Coasting Arc #14 (Orbit 2318)
---------------------------------------
Vector Time (GMT): 2018/326/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3164536
99 A = 6777727
39 meter
Y = -2842801
73 meter E =
0019673
Z = -5293561
30 I = 51
31532
XDOT = 4810
810665 Wp = 87
32381
YDOT = -5944
356628 meter/sec RA = 307
07368 deg
ZDOT = 318
282527 TA = 185
71871
MA = 185
74121
Ha = 222
995 n
mi
Hp = 212
905
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10382339
21 X = -3106798
76
Y = -9326777
34 feet Y = -2877866
58 meter
Z = -17367327
09 Z = -5308793
90
XDOT = 15783
499557 XDOT = 4875
378479
YDOT = -19502
482374 feet/sec YDOT = -5890
197802 meter/sec
ZDOT = 1044
234013 ZDOT = 341
808827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13394667
29 X = -4082694
59
Y = -3604923
66 feet Y = -1098780
73 meter
Z = -17435400
97 Z = -5314310
22
XDOT = 4856
323408 XDOT = 1480
207375
YDOT = -23579
824701 feet/sec YDOT = -7187
130569 meter/sec
ZDOT = 1150
792054 ZDOT = 350
761418
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
92175607
00016717 00000-0 10270-3 0 9138
2 25544 51
6375 307
6961 0005096 72
7229 287
4481 15
54017006 23198
Satellite: ISS
Catalog Number: 25544
Epoch time: 18326
92175607 = yrday
fracday
Element set: 913
Inclination: 51
6375 deg
RA of node: 307
6961 deg
Eccentricity:
0005096
Arg of perigee: 72
7229 deg
Mean anomaly: 287
4481 deg
Mean motion: 15
54017006 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2319
Checksum: 320
Coasting Arc #15 (Orbit 2334)
---------------------------------------
Vector Time (GMT): 2018/327/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2034803
27 A = 6779320
14 meter
Y = 4183261
41 meter E =
0011210
Z = 4924140
22 I = 51
30200
XDOT = -5271
512274 Wp = 65
58855
YDOT = 5134
890733 meter/sec RA = 302
05331 deg
ZDOT = -2175
483519 TA = 45
75673
MA = 45
66476
Ha = 222
901 n
mi
Hp = 213
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6675863
76 X = 1963954
18
Y = 13724610
92 feet Y = 4205619
40 meter
Z = 16155315
68 Z = 4933853
14
XDOT = -17294
987777 XDOT = -5317
972652
YDOT = 16846
754372 feet/sec YDOT = 5075
681445 meter/sec
ZDOT = -7137
413119 ZDOT = -2201
203710
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12271612
05 X = 3740387
35
Y = 8996981
52 feet Y = 2742279
97 meter
Z = 16198400
78 Z = 4937272
56
XDOT = -6590
872962 XDOT = -2008
898079
YDOT = 22099
439465 feet/sec YDOT = 6735
909149 meter/sec
ZDOT = -7253
716535 ZDOT = -2210
932800
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
95066457
00016717 00000-0 10270-3 0 9145
2 25544 51
6381 302
5678 0004928 76
6055 283
5647 15
54007565 23355
Satellite: ISS
Catalog Number: 25544
Epoch time: 18327
95066457 = yrday
fracday
Element set: 914
Inclination: 51
6381 deg
RA of node: 302
5678 deg
Eccentricity:
0004928
Arg of perigee: 76
6055 deg
Mean anomaly: 283
5647 deg
Mean motion: 15
54007565 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2335
Checksum: 334
Coasting Arc #16 (Orbit 2349)
---------------------------------------
Vector Time (GMT): 2018/328/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -963411
41 A = 6782508
71 meter
Y = -5329543
02 meter E =
0012101
Z = -4094466
24 I = 51
29595
XDOT = 5397
992044 Wp = 97
38772
YDOT = -3885
878675 meter/sec RA = 297
03713 deg
ZDOT = 3796
063847 TA = 212
00870
MA = 212
08225
Ha = 222
990 n
mi
Hp = 212
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3160798
59 X = -883854
21
Y = -17485377
35 feet Y = -5339871
28 meter
Z = -13433288
19 Z = -4098953
59
XDOT = 17709
947650 XDOT = 5422
604183
YDOT = -12748
945783 feet/sec YDOT = -3825
377372 meter/sec
ZDOT = 12454
277714 ZDOT = 3822
345320
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11203764
28 X = -3414907
35
Y = -13772502
66 feet Y = -4197858
81 meter
Z = -13452737
16 Z = -4100394
29
XDOT = 8174
686874 XDOT = 2491
644559
YDOT = -18904
934467 feet/sec YDOT = -5762
224026 meter/sec
ZDOT = 12572
931803 ZDOT = 3832
229614
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 18328
91526267
00016717 00000-0 10270-3 0 9153
2 25544 51
6379 297
7587 0005060 81
0848 279
0877 15
54026885 23502
Satellite: ISS
Catalog Number: 25544
Epoch time: 18328
91526267 = yrday
fracday
Element set: 915
Inclination: 51
6379 deg
RA of node: 297
7587 deg
Eccentricity:
0005060
Arg of perigee: 81
0848 deg
Mean anomaly: 279
0877 deg
Mean motion: 15
54026885 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2350
Checksum: 349
Coasting Arc #17 (Orbit 2365)
---------------------------------------
Vector Time (GMT): 2018/329/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -65188
74 A = 6786214
02 meter
Y = 6167701
33 meter E =
0018176
Z = 2811779
29 I = 51
29438
XDOT = -5296
984006 Wp = 95
28651
YDOT = 2266
118575 meter/sec RA = 292
03086 deg
ZDOT = -5066
907683 TA = 52
60407
MA = 52
43873
Ha = 222
911 n
mi
Hp = 212
990
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -213873
80 X = -147811
19
Y = 20235240
58 feet Y = 6166510
05 meter
Z = 9224997
68 Z = 2811262
65
XDOT = -17378
556449 XDOT = -5297
317966
YDOT = 7434
772229 feet/sec YDOT = 2206
882729 meter/sec
ZDOT = -16623
712870 ZDOT = -5092
639532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9926329
54 X = 3025545
24
Y = 17636232
98 feet Y = 5375523
81 meter
Z = 9221851
97 Z = 2810820
48
XDOT = -9911
205969 XDOT = -3020
935579
YDOT = 14377
233797 feet/sec YDOT = 4382
180861 meter/sec
ZDOT = -16739
678632 ZDOT = -5102
254047
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 18329
94416140
00016717 00000-0 10270-3 0 9166
2 25544 51
6379 292
6302 0004933 83
4783 276
6931 15
54048553 23660
Satellite: ISS
Catalog Number: 25544
Epoch time: 18329
94416140 = yrday
fracday
Element set: 916
Inclination: 51
6379 deg
RA of node: 292
6302 deg
Eccentricity:
0004933
Arg of perigee: 83
4783 deg
Mean anomaly: 276
6931 deg
Mean motion: 15
54048553 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2366
Checksum: 330
Coasting Arc #18 (Orbit 2380)
---------------------------------------
Vector Time (GMT): 2018/330/21:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 932630
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 936344
82 A = 6788904
92 meter
Y = -6595411
43 meter E =
0012776
Z = -1293529
42 I = 51
29110
XDOT = 4992
012114 Wp = 56
16345
YDOT = -419
805447 meter/sec RA = 287
03275 deg
ZDOT = 5802
402600 TA = 289
69738
MA = 289
83517
Ha = 223
038 n
mi
Hp = 212
917
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3071997
44 X = 1016310
30
Y = -21638488
94 feet Y = -6584493
32 meter
Z = -4243862
92 Z = -1288787
42
XDOT = 16377
992499 XDOT = 4968
150204
YDOT = -1377
314460 feet/sec YDOT = -364
115348 meter/sec
ZDOT = 19036
753937 ZDOT = 5826
594293
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8535752
92 X = -2601697
49
Y = -20124365
30 feet Y = -6133906
54 meter
Z = -4221680
65 Z = -1286768
26
XDOT = 11730
563550 XDOT = 3575
475770
YDOT = -8958
413742 feet/sec YDOT = -2730
524509 meter/sec
ZDOT = 19145
554754 ZDOT = 5835
565089
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 18330
90875396
00016717 00000-0 10270-3 0 9177
2 25544 51
6371 287
8225 0005163 89
6763 270
4981 15
54031044 23815
Satellite: ISS
Catalog Number: 25544
Epoch time: 18330
90875396 = yrday
fracday
Element set: 917
Inclination: 51
6371 deg
RA of node: 287
8225 deg
Eccentricity:
0005163
Arg of perigee: 89
6763 deg
Mean anomaly: 270
4981 deg
Mean motion: 15
54031044 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2381
Checksum: 326
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