[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 1st 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) : 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
337/11:31:53
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
0
337/17:35:42
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
1
337/19:30:00
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
338/16:07:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
8
000/00:00:00
000 0
0 0
0 212
9
338/18:38:53
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
0
340/11:00:00
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
344/23:07:30
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
4
348/03:56:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
3
000/00:00:00
000 0
0 0
0 213
6
Coasting Arc #1 (Orbit 2436)
---------------------------------------
Vector Time (GMT): 2018/334/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3576063
07 A = 6781445
58 meter
Y = -3766391
06 meter E =
0013991
Z = -4374471
65 I = 51
24933
XDOT = 2594
072941 Wp = 105
57330
YDOT = -6368
088591 meter/sec RA = 269
01771 deg
ZDOT = 3367
614620 TA = 198
73241
MA = 198
78395
Ha = 223
015 n
mi
Hp = 212
848
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11732490
40 X = -3512431
45
Y = -12356926
07 feet Y = -3806025
13 meter
Z = -14351941
10 Z = -4391688
62
XDOT = 8510
737994 XDOT = 2648
731699
YDOT = -20892
679105 feet/sec YDOT = -6338
774382 meter/sec
ZDOT = 11048
604397 ZDOT = 3380
348308
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15770650
70 X = 4806894
33
Y = -6278293
06 feet Y = -1913623
72 meter
Z = -14428886
96 Z = -4397924
75
XDOT = 15869
117947 XDOT = 4836
907150
YDOT = 14376
810567 feet/sec YDOT = 4382
051861 meter/sec
ZDOT = 11106
627060 ZDOT = 3385
299928
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 18334
50996722
00016717 00000-0 10270-3 0 9006
2 25544 51
6386 269
8765 0005123 96
8692 263
3044 15
54026770 24370
Satellite: ISS
Catalog Number: 25544
Epoch time: 18334
50996722 = yrday
fracday
Element set: 900
Inclination: 51
6386 deg
RA of node: 269
8765 deg
Eccentricity:
0005123
Arg of perigee: 96
8692 deg
Mean anomaly: 263
3044 deg
Mean motion: 15
54026770 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2437
Checksum: 330
Coasting Arc #2 (Orbit 2452)
---------------------------------------
Vector Time (GMT): 2018/335/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3112993
51 A = 6785170
36 meter
Y = 5101619
05 meter E =
0017862
Z = 3195366
60 I = 51
26458
XDOT = -3315
267547 Wp = 95
17813
YDOT = 5020
205435 meter/sec RA = 264
00574 deg
ZDOT = -4763
842027 TA = 47
63215
MA = 47
48107
Ha = 222
909 n
mi
Hp = 212
924
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10213233
29 X = 3040192
86
Y = 16737595
30 feet Y = 5136023
55 meter
Z = 10483486
20 Z = 3210311
92
XDOT = -10876
862031 XDOT = -3348
018044
YDOT = 16470
490271 feet/sec YDOT = 4982
948837 meter/sec
ZDOT = -15629
402977 ZDOT = -4780
025987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19235942
38 X = -5863115
24
Y = 3610434
55 feet Y = 1100460
45 meter
Z = 10550070
92 Z = 3215661
62
XDOT = -11367
002796 XDOT = -3464
662452
YDOT = -14472
469498 feet/sec YDOT = -4411
208703 meter/sec
ZDOT = -15702
763281 ZDOT = -4786
202248
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 18335
53885788
00016717 00000-0 10270-3 0 9010
2 25544 51
6395 264
7478 0005093 99
7988 260
3740 15
54050427 24535
Satellite: ISS
Catalog Number: 25544
Epoch time: 18335
53885788 = yrday
fracday
Element set: 901
Inclination: 51
6395 deg
RA of node: 264
7478 deg
Eccentricity:
0005093
Arg of perigee: 99
7988 deg
Mean anomaly: 260
3740 deg
Mean motion: 15
54050427 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2453
Checksum: 349
Coasting Arc #3 (Orbit 2467)
---------------------------------------
Vector Time (GMT): 2018/336/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2588606
58 A = 6788270
53 meter
Y = -6029727
94 meter E =
0010773
Z = -1734895
61 I = 51
27901
XDOT = 3970
432551 Wp = 63
84862
YDOT = -3321
367845 meter/sec RA = 259
00390 deg
ZDOT = 5651
444244 TA = 277
02723
MA = 277
14974
Ha = 222
971 n
mi
Hp = 212
930
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8492803
73 X = -2512560
76
Y = -19782571
99 feet Y = -6058250
28 meter
Z = -5691914
72 Z = -1747285
82
XDOT = 13026
353514 XDOT = 3979
825833
YDOT = -10896
876132 feet/sec YDOT = -3276
915374 meter/sec
ZDOT = 18541
483741 ZDOT = 5670
754184
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21472839
52 X = 6544921
49
Y = -1328867
30 feet Y = -405038
75 meter
Z = -5746915
47 Z = -1751659
84
XDOT = 5839
339242 XDOT = 1779
830601
YDOT = 14243
897323 feet/sec YDOT = 4341
539904 meter/sec
ZDOT = 18628
691690 ZDOT = 5678
025227
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 18336
50343821
00016717 00000-0 10270-3 0 9026
2 25544 51
6391 259
9401 0005134 102
7741 257
3986 15
54042974 24683
Satellite: ISS
Catalog Number: 25544
Epoch time: 18336
50343821 = yrday
fracday
Element set: 902
Inclination: 51
6391 deg
RA of node: 259
9401 deg
Eccentricity:
0005134
Arg of perigee: 102
7741 deg
Mean anomaly: 257
3986 deg
Mean motion: 15
54042974 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2468
Checksum: 313
Coasting Arc #4 (Orbit 2483)
---------------------------------------
Vector Time (GMT): 2018/337/11:31:53
000
Vector Time (MET): N/A
Weight (LBS) : 930150
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3196607
21 A = 6778878
19 meter
Y = -3320647
39 meter E =
0010994
Z = 4963742
11 I = 51
25548
XDOT = 3551
284847 Wp = 116
57472
YDOT = 6488
102139 meter/sec RA = 254
12439 deg
ZDOT = 2045
059035 TA = 313
40008
MA = 313
49156
Ha = 222
746 n
mi
Hp = 212
957
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10487556
48 X = 3209390
42
Y = -10894512
45 feet Y = -3284829
45 meter
Z = 16285243
15 Z = 4979301
27
XDOT = 11651
197005 XDOT = 3468
535159
YDOT = 21286
424342 feet/sec YDOT = 6527
352303 meter/sec
ZDOT = 6709
511269 ZDOT = 2062
109516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5324180
11 X = 1622810
10
Y = 14072538
30 feet Y = 4289309
67 meter
Z = 16355584
94 Z = 4985182
29
XDOT = -23187
302168 XDOT = -7067
489701
YDOT = 854
654954 feet/sec YDOT = 260
498830 meter/sec
ZDOT = 6785
425459 ZDOT = 2068
197680
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 18337
53231864
00016717 00000-0 10270-3 0 9034
2 25544 51
6394 254
8120 0005014 108
3861 251
7837 15
54089770 24846
Satellite: ISS
Catalog Number: 25544
Epoch time: 18337
53231864 = yrday
fracday
Element set: 903
Inclination: 51
6394 deg
RA of node: 254
8120 deg
Eccentricity:
0005014
Arg of perigee: 108
3861 deg
Mean anomaly: 251
7837 deg
Mean motion: 15
54089770 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2484
Checksum: 314
Coasting Arc #5 (Orbit 2487)
---------------------------------------
Vector Time (GMT): 2018/337/17:35:42
000
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1405040
65 A = 6783677
92 meter
Y = -5504136
37 meter E =
0016466
Z = 3696280
32 I = 51
27190
XDOT = 4858
004451 Wp = 99
77546
YDOT = 4123
171981 meter/sec RA = 252
86583 deg
ZDOT = 4274
128082 TA = 304
57987
MA = 304
73511
Ha = 222
782 n
mi
Hp = 213
057
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4609713
41 X = 1448530
14
Y = -18058190
20 feet Y = -5488181
24 meter
Z = 12126903
93 Z = 3703211
00
XDOT = 15938
334814 XDOT = 4790
775130
YDOT = 13527
467128 feet/sec YDOT = 4177
121457 meter/sec
ZDOT = 14022
729927 ZDOT = 4297
563877
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11598790
64 X = 3535311
39
Y = -14561715
35 feet Y = -4438410
84 meter
Z = 12158700
24 Z = 3705971
83
XDOT = 7759
440524 XDOT = 2365
077472
YDOT = 18028
910943 feet/sec YDOT = 5495
212055 meter/sec
ZDOT = 14127
630408 ZDOT = 4306
101748
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 18337
78953748
00016717 00000-0 10270-3 0 9044
2 25544 51
6377 253
5281 0004852 110
1173 250
0502 15
54068185 24889
Satellite: ISS
Catalog Number: 25544
Epoch time: 18337
78953748 = yrday
fracday
Element set: 904
Inclination: 51
6377 deg
RA of node: 253
5281 deg
Eccentricity:
0004852
Arg of perigee: 110
1173 deg
Mean anomaly: 250
0502 deg
Mean motion: 15
54068185 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2488
Checksum: 317
Coasting Arc #6 (Orbit 2488)
---------------------------------------
Vector Time (GMT): 2018/337/19:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4429235
88 A = 6782315
18 meter
Y = 3063526
17 meter E =
0014932
Z = 4110031
08 I = 51
26668
XDOT = -1069
311443 Wp = 88
21142
YDOT = 6605
409403 meter/sec RA = 252
41472 deg
ZDOT = -3758
853510 TA = 40
73560
MA = 40
62404
Ha = 222
872 n
mi
Hp = 212
990
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14531613
77 X = 4374684
78
Y = 10050938
88 feet Y = 3112751
75 meter
Z = 13484353
93 Z = 4131414
78
XDOT = -3508
239643 XDOT = -1124
836675
YDOT = 21671
290692 feet/sec YDOT = 6593
141342 meter/sec
ZDOT = -12332
196554 ZDOT = -3764
182480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15137959
24 X = 4614049
98
Y = 8968761
14 feet Y = 2733678
40 meter
Z = 13580150
43 Z = 4139229
85
XDOT = -1177
785499 XDOT = -358
989020
YDOT = 20759
031245 feet/sec YDOT = 6327
352724 meter/sec
ZDOT = -12356
917041 ZDOT = -3766
388314
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 18337
85384414
00016717 00000-0 10270-3 0 9051
2 25544 51
6365 253
2048 0005246 112
8209 247
3488 15
54037416 24897
Satellite: ISS
Catalog Number: 25544
Epoch time: 18337
85384414 = yrday
fracday
Element set: 905
Inclination: 51
6365 deg
RA of node: 253
2048 deg
Eccentricity:
0005246
Arg of perigee: 112
8209 deg
Mean anomaly: 247
3488 deg
Mean motion: 15
54037416 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2489
Checksum: 322
Coasting Arc #7 (Orbit 2501)
---------------------------------------
Vector Time (GMT): 2018/338/16:07:00
000
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3336085
19 A = 6778033
48 meter
Y = 2849832
86 meter E =
0018383
Z = -5182378
18 I = 51
26502
XDOT = -3707
510174 Wp = 88
39190
YDOT = -6581
929714 meter/sec RA = 248
15023 deg
ZDOT = -1236
108034 TA = 169
67949
MA = 169
64169
Ha = 222
789 n
mi
Hp = 212
924
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10945161
38 X = -3342531
17
Y = 9349845
34 feet Y = 2812490
73 meter
Z = -17002553
10 Z = -5198599
49
XDOT = -12163
747290 XDOT = -3627
629177
YDOT = -21594
257591 feet/sec YDOT = -6622
942947 meter/sec
ZDOT = -4055
472554 ZDOT = -1253
924556
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14255471
29 X = -4345067
65
Y = -1225127
40 feet Y = -373418
83 meter
Z = -17075818
53 Z = -5204709
49
XDOT = 6893
144182 XDOT = 2101
030347
YDOT = -22727
334580 feet/sec YDOT = -6927
291580 meter/sec
ZDOT = -4134
837481 ZDOT = -1260
298464
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 18338
68980424
00016717 00000-0 10270-3 0 9067
2 25544 51
6395 249
0414 0004862 111
5553 248
6118 15
54077491 25028
Satellite: ISS
Catalog Number: 25544
Epoch time: 18338
68980424 = yrday
fracday
Element set: 906
Inclination: 51
6395 deg
RA of node: 249
0414 deg
Eccentricity:
0004862
Arg of perigee: 111
5553 deg
Mean anomaly: 248
6118 deg
Mean motion: 15
54077491 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2502
Checksum: 319
Coasting Arc #8 (Orbit 2503)
---------------------------------------
Vector Time (GMT): 2018/338/18:38:53
000
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4673444
04 A = 6782199
99 meter
Y = 2643883
55 meter E =
0014602
Z = 4130879
61 I = 51
27790
XDOT = -476
344237 Wp = 88
55783
YDOT = 6689
962089 meter/sec RA = 247
58329 deg
ZDOT = -3731
051628 TA = 40
03922
MA = 39
93167
Ha = 222
778 n
mi
Hp = 213
049
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15332821
64 X = 4623466
06
Y = 8674158
62 feet Y = 2695865
53 meter
Z = 13552754
63 Z = 4153460
77
XDOT = -1562
809178 XDOT = -532
994063
YDOT = 21948
694519 feet/sec YDOT = 6684
318778 meter/sec
ZDOT = -12240
983030 ZDOT = -3733
502732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13954594
46 X = 4253360
39
Y = 10623151
70 feet Y = 3237936
64 meter
Z = 13653993
81 Z = 4161737
31
XDOT = -3609
094356 XDOT = -1100
051960
YDOT = 20538
892730 feet/sec YDOT = 6260
254504 meter/sec
ZDOT = -12252
765272 ZDOT = -3734
642855
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 18338
81841456
00016717 00000-0 10270-3 0 9074
2 25544 51
6373 248
3971 0005099 115
3972 244
7709 15
54049638 25041
Satellite: ISS
Catalog Number: 25544
Epoch time: 18338
81841456 = yrday
fracday
Element set: 907
Inclination: 51
6373 deg
RA of node: 248
3971 deg
Eccentricity:
0005099
Arg of perigee: 115
3972 deg
Mean anomaly: 244
7709 deg
Mean motion: 15
54049638 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2504
Checksum: 339
Coasting Arc #9 (Orbit 2518)
---------------------------------------
Vector Time (GMT): 2018/339/18:38:53
000
Vector Time (MET): N/A
Weight (LBS) : 945381
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4679491
34 A = 6785840
89 meter
Y = -3972980
79 meter E =
0008918
Z = -2900981
51 I = 51
30441
XDOT = 1629
501431 Wp = 94
57965
YDOT = -5564
826528 meter/sec RA = 242
57578 deg
ZDOT = 5005
337613 TA = 232
22819
MA = 232
30900
Ha = 222
916 n
mi
Hp = 212
900
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15352661
87 X = -4620624
89
Y = -13034713
88 feet Y = -4024980
72 meter
Z = -9517655
86 Z = -2923570
61
XDOT = 5346
133305 XDOT = 1667
294066
YDOT = -18257
304883 feet/sec YDOT = -5546
393437 meter/sec
ZDOT = 16421
711329 ZDOT = 5013
344608
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13676856
21 X = -4168705
77
Y = -14717886
38 feet Y = -4486011
77 meter
Z = -9618793
59 Z = -2931808
29
XDOT = 6241
752556 XDOT = 1902
486179
YDOT = -16529
693190 feet/sec YDOT = -5038
250484 meter/sec
ZDOT = 16458
344928 ZDOT = 5016
503534
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 18339
78298257
00016717 00000-0 10270-3 0 9087
2 25544 51
6377 243
5890 0005354 118
3055 241
8638 15
54074519 25192
Satellite: ISS
Catalog Number: 25544
Epoch time: 18339
78298257 = yrday
fracday
Element set: 908
Inclination: 51
6377 deg
RA of node: 243
5890 deg
Eccentricity:
0005354
Arg of perigee: 118
3055 deg
Mean anomaly: 241
8638 deg
Mean motion: 15
54074519 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2519
Checksum: 343
Coasting Arc #10 (Orbit 2529)
---------------------------------------
Vector Time (GMT): 2018/340/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965840
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3381812
68 A = 6789523
96 meter
Y = 5877613
77 meter E =
0016791
Z = -131898
60 I = 51
32973
XDOT = -4207
963079 Wp = 130
28859
YDOT = 2298
352209 meter/sec RA = 239
19316 deg
ZDOT = -5986
889431 TA = 51
13870
MA = 50
98900
Ha = 222
856 n
mi
Hp = 213
066
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11095185
94 X = 3316476
91
Y = 19283509
74 feet Y = 5915066
25 meter
Z = -432738
20 Z = -115628
77
XDOT = -13805
653147 XDOT = -4204
269542
YDOT = 7540
525619 feet/sec YDOT = 2251
317098 meter/sec
ZDOT = -19642
025693 ZDOT = -6007
321379
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22246873
43 X = -6780847
02
Y = -301700
81 feet Y = -91958
41 meter
Z = -360222
69 Z = -109795
87
XDOT = 476
315939 XDOT = 145
181098
YDOT = -13984
746192 feet/sec YDOT = -4262
550639 meter/sec
ZDOT = -19734
172373 ZDOT = -6014
975739
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 18340
49033125
00016717 00000-0 10270-3 0 9099
2 25544 51
6402 240
0678 0005071 117
5417 242
6251 15
54060306 25308
Satellite: ISS
Catalog Number: 25544
Epoch time: 18340
49033125 = yrday
fracday
Element set: 909
Inclination: 51
6402 deg
RA of node: 240
0678 deg
Eccentricity:
0005071
Arg of perigee: 117
5417 deg
Mean anomaly: 242
6251 deg
Mean motion: 15
54060306 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2530
Checksum: 271
Coasting Arc #11 (Orbit 2545)
---------------------------------------
Vector Time (GMT): 2018/341/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965840
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2589425
68 A = 6788203
08 meter
Y = -6012990
26 meter E =
0017258
Z = 1771377
53 I = 51
34289
XDOT = 5166
804385 Wp = 79
10175
YDOT = -550
291915 meter/sec RA = 234
20170 deg
ZDOT = 5641
272149 TA = 300
43788
MA = 300
60828
Ha = 222
795 n
mi
Hp = 213
151
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8495491
07 X = -2530598
81
Y = -19727658
34 feet Y = -6041618
31 meter
Z = 5811606
06 Z = 1758941
01
XDOT = 16951
457955 XDOT = 5145
171218
YDOT = -1805
419667 feet/sec YDOT = -492
634738 meter/sec
ZDOT = 18508
110724 ZDOT = 5666
318412
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21363451
86 X = 6511580
13
Y = 2365631
55 feet Y = 721044
50 meter
Z = 5756331
22 Z = 1754529
76
XDOT = -6601
200659 XDOT = -2012
045961
YDOT = 13951
611937 feet/sec YDOT = 4252
451318 meter/sec
ZDOT = 18620
827442 ZDOT = 5675
628204
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 18341
51919911
00016717 00000-0 10270-3 0 9101
2 25544 51
6399 234
9398 0004979 120
8966 239
2677 15
54068606 25468
Satellite: ISS
Catalog Number: 25544
Epoch time: 18341
51919911 = yrday
fracday
Element set: 910
Inclination: 51
6399 deg
RA of node: 234
9398 deg
Eccentricity:
0004979
Arg of perigee: 120
8966 deg
Mean anomaly: 239
2677 deg
Mean motion: 15
54068606 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2546
Checksum: 353
Coasting Arc #12 (Orbit 2560)
---------------------------------------
Vector Time (GMT): 2018/342/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965840
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1494698
82 A = 6784914
55 meter
Y = 5749094
48 meter E =
0009268
Z = -3282322
42 I = 51
35338
XDOT = -5943
351823 Wp = 111
32514
YDOT = -1131
516807 meter/sec RA = 229
20514 deg
ZDOT = -4702
413236 TA = 106
93583
MA = 106
83421
Ha = 222
711 n
mi
Hp = 213
200
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4903867
52 X = 1446243
68
Y = 18861858
53 feet Y = 5765538
73 meter
Z = -10768774
36 Z = -3275178
59
XDOT = -19499
185770 XDOT = -5907
415112
YDOT = -3712
325482 feet/sec YDOT = -1197
777966 meter/sec
ZDOT = -15427
864948 ZDOT = -4731
197106
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18931093
18 X = -5770197
20
Y = -4702020
23 feet Y = -1433175
77 meter
Z = -10737264
18 Z = -3272718
12
XDOT = 12235
834536 XDOT = 3729
482367
YDOT = -13843
430189 feet/sec YDOT = -4219
477522 meter/sec
ZDOT = -15557
226373 ZDOT = -4741
842598
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 18342
48375798
00016717 00000-0 10270-3 0 9118
2 25544 51
6409 230
1320 0004912 124
6383 235
5234 15
54084688 25618
Satellite: ISS
Catalog Number: 25544
Epoch time: 18342
48375798 = yrday
fracday
Element set: 911
Inclination: 51
6409 deg
RA of node: 230
1320 deg
Eccentricity:
0004912
Arg of perigee: 124
6383 deg
Mean anomaly: 235
5234 deg
Mean motion: 15
54084688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2561
Checksum: 310
Coasting Arc #13 (Orbit 2576)
---------------------------------------
Vector Time (GMT): 2018/343/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965840
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -224609
11 A = 6781214
62 meter
Y = -5138132
77 meter E =
0014203
Z = 4412260
90 I = 51
36248
XDOT = 6430
208097 Wp = 116
19382
YDOT = 2568
791226 meter/sec RA = 224
19995 deg
ZDOT = 3304
281197 TA = 300
27544
MA = 300
41592
Ha = 222
731 n
mi
Hp = 213
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -736906
53 X = -188568
92
Y = -16857390
98 feet Y = -5140443
55 meter
Z = 14475921
58 Z = 4411256
70
XDOT = 21096
483259 XDOT = 6384
954712
YDOT = 8427
792735 feet/sec YDOT = 2640
444830 meter/sec
ZDOT = 10840
817577 ZDOT = 3335
407501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15306781
67 X = 4665507
05
Y = 7108579
70 feet Y = 2166695
09 meter
Z = 14471955
53 Z = 4411052
04
XDOT = -16727
501115 XDOT = -5098
542340
YDOT = 13567
798988 feet/sec YDOT = 4135
465132 meter/sec
ZDOT = 10980
583667 ZDOT = 3346
881902
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 18343
51261984
00016717 00000-0 10270-3 0 9125
2 25544 51
6399 225
0036 0005007 127
0710 233
0901 15
54078260 25770
Satellite: ISS
Catalog Number: 25544
Epoch time: 18343
51261984 = yrday
fracday
Element set: 912
Inclination: 51
6399 deg
RA of node: 225
0036 deg
Eccentricity:
0005007
Arg of perigee: 127
0710 deg
Mean anomaly: 233
0901 deg
Mean motion: 15
54078260 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2577
Checksum: 289
Coasting Arc #14 (Orbit 2591)
---------------------------------------
Vector Time (GMT): 2018/344/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 965840
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1235919
49 A = 6778238
26 meter
Y = 4276422
69 meter E =
0016893
Z = -5126214
03 I = 51
37736
XDOT = -6511
370135 Wp = 91
73549
YDOT = -3721
300621 meter/sec RA = 219
18712 deg
ZDOT = -1539
437072 TA = 163
37842
MA = 163
32298
Ha = 222
558 n
mi
Hp = 213
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4054853
96 X = -1258747
30
Y = 14030258
18 feet Y = 4262474
77 meter
Z = -16818287
51 Z = -5132272
64
XDOT = -21362
762910 XDOT = -6461
795787
YDOT = -12208
991538 feet/sec YDOT = -3793
837910 meter/sec
ZDOT = -5050
646563 ZDOT = -1570
947154
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10752101
91 X = -3277240
66
Y = -9836121
64 feet Y = -2998049
88 meter
Z = -16846002
37 Z = -5134661
52
XDOT = 19786
700661 XDOT = 6030
986361
YDOT = -12764
611624 feet/sec YDOT = -3890
653623 meter/sec
ZDOT = -5192
042231 ZDOT = -1582
534472
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 18344
47717469
00016717 00000-0 10270-3 0 9136
2 25544 51
6399 220
1960 0004835 131
7950 228
3616 15
54110270 25923
Satellite: ISS
Catalog Number: 25544
Epoch time: 18344
47717469 = yrday
fracday
Element set: 913
Inclination: 51
6399 deg
RA of node: 220
1960 deg
Eccentricity:
0004835
Arg of perigee: 131
7950 deg
Mean anomaly: 228
3616 deg
Mean motion: 15
54110270 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2592
Checksum: 313
Coasting Arc #15 (Orbit 2599)
---------------------------------------
Vector Time (GMT): 2018/344/23:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 965840
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3977165
78 A = 6787580
51 meter
Y = 5070315
55 meter E =
0011547
Z = -2121455
02 I = 51
42003
XDOT = -5071
927627 Wp = 138
38595
YDOT = 1689
753227 meter/sec RA = 216
66388 deg
ZDOT = -5495
665364 TA = 65
19271
MA = 65
07264
Ha = 222
657 n
mi
Hp = 213
361
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13048444
15 X = 3930477
41
Y = 16634893
55 feet Y = 5114530
18 meter
Z = -6960154
27 Z = -2102248
12
XDOT = -16640
182502 XDOT = -5063
750918
YDOT = 5543
809801 feet/sec YDOT = 1633
081771 meter/sec
ZDOT = -18030
398177 ZDOT = -5520
282981
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20556523
20 X = 6265628
27
Y = -5059578
25 feet Y = -1542159
45 meter
Z = -6874252
51 Z = -2095272
17
XDOT = -2140
532134 XDOT = -652
434194
YDOT = 15835
278361 feet/sec YDOT = 4826
592845 meter/sec
ZDOT = -18141
357872 ZDOT = -5529
485879
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 18344
99160308
00016717 00000-0 10270-3 0 9148
2 25544 51
6384 217
6293 0005097 137
0906 223
0645 15
54088267 26002
Satellite: ISS
Catalog Number: 25544
Epoch time: 18344
99160308 = yrday
fracday
Element set: 914
Inclination: 51
6384 deg
RA of node: 217
6293 deg
Eccentricity:
0005097
Arg of perigee: 137
0906 deg
Mean anomaly: 223
0645 deg
Mean motion: 15
54088267 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2600
Checksum: 314
Coasting Arc #16 (Orbit 2615)
---------------------------------------
Vector Time (GMT): 2018/345/23:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 965840
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2824070
66 A = 6784155
16 meter
Y = -5050727
88 meter E =
0016006
Z = 3531949
00 I = 51
43640
XDOT = 6226
417749 Wp = 105
73086
YDOT = -343
100477 meter/sec RA = 211
67054 deg
ZDOT = 4466
715923 TA = 296
05065
MA = 296
21534
Ha = 222
579 n
mi
Hp = 213
407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9265323
70 X = -2784538
43
Y = -16570629
52 feet Y = -5082087
93 meter
Z = 11587759
18 Z = 3518326
15
XDOT = 20427
879754 XDOT = 6208
094726
YDOT = -1125
657733 feet/sec YDOT = -273
575267 meter/sec
ZDOT = 14654
579801 ZDOT = 4496
917111
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18917173
54 X = -5765954
49
Y = 1994423
87 feet Y = 607900
40 meter
Z = 11526966
96 Z = 3513419
53
XDOT = 7186
210964 XDOT = 2190
357102
YDOT = -17725
233313 feet/sec YDOT = -5402
651114 meter/sec
ZDOT = 14790
543711 ZDOT = 4508
157723
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 18346
02045685
00016717 00000-0 10270-3 0 9155
2 25544 51
6388 212
5003 0005027 139
9652 220
1872 15
54108250 26163
Satellite: ISS
Catalog Number: 25544
Epoch time: 18346
02045685 = yrday
fracday
Element set: 915
Inclination: 51
6388 deg
RA of node: 212
5003 deg
Eccentricity:
0005027
Arg of perigee: 139
9652 deg
Mean anomaly: 220
1872 deg
Mean motion: 15
54108250 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2616
Checksum: 292
Coasting Arc #17 (Orbit 2630)
---------------------------------------
Vector Time (GMT): 2018/346/23:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 965840
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1333886
99 A = 6780449
70 meter
Y = 4790021
55 meter E =
0012711
Z = -4620579
13 I = 51
45197
XDOT = -7010
877616 Wp = 92
79612
YDOT = -888
572854 meter/sec RA = 206
66956 deg
ZDOT = -2952
734385 TA = 147
70864
MA = 147
63076
Ha = 222
555 n
mi
Hp = 213
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4376269
66 X = 1302668
77
Y = 15715293
79 feet Y = 4804763
87 meter
Z = -15159380
33 Z = -4614174
97
XDOT = -23001
566980 XDOT = -6986
077496
YDOT = -2915
265270 feet/sec YDOT = -966
834424 meter/sec
ZDOT = -9687
448770 ZDOT = -2986
730557
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16234253
12 X = 4948200
35
Y = 1851942
17 feet Y = 564471
97 meter
Z = -15131039
06 Z = -4611940
70
XDOT = -11305
259629 XDOT = -3445
843135
YDOT = 18908
558448 feet/sec YDOT = 5763
328615 meter/sec
ZDOT = -9840
388331 ZDOT = -2999
350363
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 18346
98500767
00016717 00000-0 10270-3 0 9168
2 25544 51
6381 207
6926 0005071 142
4532 217
6975 15
54086543 26312
Satellite: ISS
Catalog Number: 25544
Epoch time: 18346
98500767 = yrday
fracday
Element set: 916
Inclination: 51
6381 deg
RA of node: 207
6926 deg
Eccentricity:
0005071
Arg of perigee: 142
4532 deg
Mean anomaly: 217
6975 deg
Mean motion: 15
54086543 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2631
Checksum: 324
Coasting Arc #18 (Orbit 2646)
---------------------------------------
Vector Time (GMT): 2018/347/23:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 965840
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 307863
09 A = 6777884
41 meter
Y = -4332068
03 meter E =
0008869
Z = 5199512
01 I = 51
47373
XDOT = 7336
897940 Wp = 136
84377
YDOT = 1921
297943 meter/sec RA = 201
66186 deg
ZDOT = 1158
830246 TA = 301
98133
MA = 302
06750
Ha = 222
431 n
mi
Hp = 213
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1010049
50 X = 331026
18
Y = -14212821
62 feet Y = -4328496
18 meter
Z = 17058766
43 Z = 5201063
42
XDOT = 24071
187466 XDOT = 7309
239183
YDOT = 6303
470940 feet/sec YDOT = 2003
189497 meter/sec
ZDOT = 3801
936503 ZDOT = 1194
403244
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12902025
03 X = -3932537
23
Y = -6025704
57 feet Y = -1836634
75 meter
Z = 17066184
25 Z = 5201772
96
XDOT = 14212
292744 XDOT = 4331
906828
YDOT = -19140
050907 feet/sec YDOT = -5833
887516 meter/sec
ZDOT = 3961
892896 ZDOT = 1207
584955
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 18348
01385775
00016717 00000-0 10270-3 0 9175
2 25544 51
6380 202
5641 0004987 146
5280 213
6189 15
54110367 26471
Satellite: ISS
Catalog Number: 25544
Epoch time: 18348
01385775 = yrday
fracday
Element set: 917
Inclination: 51
6380 deg
RA of node: 202
5641 deg
Eccentricity:
0004987
Arg of perigee: 146
5280 deg
Mean anomaly: 213
6189 deg
Mean motion: 15
54110367 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2647
Checksum: 320
Coasting Arc #19 (Orbit 2649)
---------------------------------------
Vector Time (GMT): 2018/348/03:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 965840
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4504867
82 A = 6780427
29 meter
Y = -2184416
39 meter E =
0010506
Z = 4563227
74 I = 51
48651
XDOT = 5329
203758 Wp = 93
04754
YDOT = 4601
963388 meter/sec RA = 200
62935 deg
ZDOT = -3052
560909 TA = 27
53373
MA = 27
47812
Ha = 222
281 n
mi
Hp = 213
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14779750
06 X = 4506794
06
Y = -7166720
44 feet Y = -2134029
40 meter
Z = 14971219
62 Z = 4585115
30
XDOT = 17484
264297 XDOT = 5292
174937
YDOT = 15098
305080 feet/sec YDOT = 4661
351437 meter/sec
ZDOT = -10014
963612 ZDOT = -3026
763129
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15911009
55 X = -4849675
71
Y = -3698090
19 feet Y = -1127177
89 meter
Z = 15069977
26 Z = 4593329
07
XDOT = -4366
889478 XDOT = -1331
027913
YDOT = -21625
160066 feet/sec YDOT = -6591
348788 meter/sec
ZDOT = -9899
278873 ZDOT = -3017
300201
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 18348
20676757
00016717 00000-0 10270-3 0 9180
2 25544 51
6359 201
6029 0004821 145
2178 214
9290 15
54105744 26500
Satellite: ISS
Catalog Number: 25544
Epoch time: 18348
20676757 = yrday
fracday
Element set: 918
Inclination: 51
6359 deg
RA of node: 201
6029 deg
Eccentricity:
0004821
Arg of perigee: 145
2178 deg
Mean anomaly: 214
9290 deg
Mean motion: 15
54105744 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2650
Checksum: 314
Coasting Arc #20 (Orbit 2664)
---------------------------------------
Vector Time (GMT): 2018/349/03:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 965840
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5681599
60 A = 6784187
20 meter
Y = 1287708
83 meter E =
0008887
Z = -3487684
28 I = 51
53130
XDOT = -3867
875988 Wp = 120
30870
YDOT = -4817
111653 meter/sec RA = 195
63300 deg
ZDOT = 4526
644790 TA = 198
69152
MA = 198
72418
Ha = 222
379 n
mi
Hp = 213
550
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18640418
64 X = -5678635
53
Y = 4224766
51 feet Y = 1224190
03 meter
Z = -11442533
72 Z = -3515276
23
XDOT = -12689
881852 XDOT = -3835
710273
YDOT = -15804
172091 feet/sec YDOT = -4860
185366 meter/sec
ZDOT = 14851
196819 ZDOT = 4507
933819
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17212242
66 X = 5246291
56
Y = 8135786
49 feet Y = 2479787
72 meter
Z = -11566897
50 Z = -3525590
36
XDOT = 899
827399 XDOT = 274
267391
YDOT = 19071
994243 feet/sec YDOT = 5813
143845 meter/sec
ZDOT = 14767
422949 ZDOT = 4501
110515
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 18349
17131199
00016717 00000-0 10270-3 0 9194
2 25544 51
6368 196
7948 0004769 147
0956 213
0495 15
54086837 26653
Satellite: ISS
Catalog Number: 25544
Epoch time: 18349
17131199 = yrday
fracday
Element set: 919
Inclination: 51
6368 deg
RA of node: 196
7948 deg
Eccentricity:
0004769
Arg of perigee: 147
0956 deg
Mean anomaly: 213
0495 deg
Mean motion: 15
54086837 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2665
Checksum: 361
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