[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 3rd 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15282 6 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 540 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
002/14:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
4
000/00:00:00
000 0
0 0
0 215
3
005/18:56:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
0
000/00:00:00
000 0
0 0
0 214
8
012/22:27:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
4
000/00:00:00
000 0
0 0
0 214
1
013/10:05:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
2
000/00:00:00
000 0
0 0
0 214
2
Coasting Arc #1 (Orbit 1258)
---------------------------------------
Vector Time (GMT): 2018/001/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4086515
83 A = 6788946
42 meter
Y = -5410434
07 meter E =
0009689
Z = 237236
59 I = 51
95093
XDOT = 3903
778188 Wp = 130
59900
YDOT = 2677
254561 meter/sec RA = 128
63308 deg
ZDOT = -6031
908633 TA = 46
85598
MA = 46
77501
Ha = 220
316 n
mi
Hp = 215
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13407204
17 X = 4145560
68
Y = -17750767
94 feet Y = -5364405
75 meter
Z = 778335
26 Z = 257230
13
XDOT = 12807
671220 XDOT = 3902
850037
YDOT = 8783
643572 feet/sec YDOT = 2720
904878 meter/sec
ZDOT = -19789
726485 ZDOT = -6012
947373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19847036
65 X = 6049376
77
Y = 10039433
29 feet Y = 3060019
27 meter
Z = 868105
60 Z = 264598
59
XDOT = -5614
848304 XDOT = -1711
405763
YDOT = 12843
389586 feet/sec YDOT = 3914
665146 meter/sec
ZDOT = -19705
725221 ZDOT = -6006
305047
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 18001
53268823
00016717 00000-0 10270-3 0 9004
2 25544 51
6396 129
5325 0002916 317
6567 42
4360 15
54249652 12591
Satellite: ISS
Catalog Number: 25544
Epoch time: 18001
53268823 = yrday
fracday
Element set: 900
Inclination: 51
6396 deg
RA of node: 129
5325 deg
Eccentricity:
0002916
Arg of perigee: 317
6567 deg
Mean anomaly: 42
4360 deg
Mean motion: 15
54249652 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1259
Checksum: 309
Coasting Arc #2 (Orbit 1274)
---------------------------------------
Vector Time (GMT): 2018/002/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4583334
92 A = 6788059
37 meter
Y = 4767494
35 meter E =
0013738
Z = 1495403
61 I = 51
96836
XDOT = -2580
320656 Wp = 49
76734
YDOT = -4308
116229 meter/sec RA = 123
68450 deg
ZDOT = 5799
800419 TA = 326
49318
MA = 326
58001
Ha = 220
451 n
mi
Hp = 215
100
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15037188
06 X = -4643569
50
Y = 15641385
67 feet Y = 4715903
39 meter
Z = 4906179
84 Z = 1472993
85
XDOT = -8465
618950 XDOT = -2560
126491
YDOT = -14134
239597 feet/sec YDOT = -4336
858945 meter/sec
ZDOT = 19028
216599 ZDOT = 5787
314738
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18272145
01 X = -5569349
80
Y = -11741987
25 feet Y = -3578957
71 meter
Z = 4805728
17 Z = 1464785
95
XDOT = 11337
381548 XDOT = 3455
633896
YDOT = -9841
074035 feet/sec YDOT = -2999
559366 meter/sec
ZDOT = 18973
269952 ZDOT = 5783
052681
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 18002
56144496
00016717 00000-0 10270-3 0 9018
2 25544 51
6404 124
4039 0002858 323
0016 37
0940 15
54253853 12752
Satellite: ISS
Catalog Number: 25544
Epoch time: 18002
56144496 = yrday
fracday
Element set: 901
Inclination: 51
6404 deg
RA of node: 124
4039 deg
Eccentricity:
0002858
Arg of perigee: 323
0016 deg
Mean anomaly: 37
0940 deg
Mean motion: 15
54253853 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1275
Checksum: 284
Coasting Arc #3 (Orbit 1275)
---------------------------------------
Vector Time (GMT): 2018/002/14:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4147354
22 A = 6777522
69 meter
Y = 1160558
70 meter E =
0012888
Z = -5244435
53 I = 51
93495
XDOT = -3356
900415 Wp = 69
16093
YDOT = 6787
536286 meter/sec RA = 123
14868 deg
ZDOT = -1150
452170 TA = 189
82795
MA = 189
85319
Ha = 220
408 n
mi
Hp = 215
331
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13606805
18 X = 4159542
76
Y = 3807607
30 feet Y = 1207006
05 meter
Z = -17206153
30 Z = -5224259
56
XDOT = -11013
452805 XDOT = -3426
962744
YDOT = 22268
819836 feet/sec YDOT = 6749
605528 meter/sec
ZDOT = -3774
449377 ZDOT = -1166
928016
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8076211
62 X = 2461629
30
Y = 11725806
61 feet Y = 3574025
85 meter
Z = -17116512
42 Z = -5217112
98
XDOT = -21865
523494 XDOT = -6664
611561
YDOT = 9431
298760 feet/sec YDOT = 2874
659862 meter/sec
ZDOT = -3848
785130 ZDOT = -1173
109708
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 18002
62574153
00016717 00000-0 10270-3 0 9023
2 25544 51
6404 124
0859 0003119 321
0926 39
0001 15
54228328 12767
Satellite: ISS
Catalog Number: 25544
Epoch time: 18002
62574153 = yrday
fracday
Element set: 902
Inclination: 51
6404 deg
RA of node: 124
0859 deg
Eccentricity:
0003119
Arg of perigee: 321
0926 deg
Mean anomaly: 39
0001 deg
Mean motion: 15
54228328 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1276
Checksum: 274
Coasting Arc #4 (Orbit 1291)
---------------------------------------
Vector Time (GMT): 2018/003/14:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3199019
54 A = 6777108
31 meter
Y = -2786888
95 meter E =
0004289
Z = 5284400
71 I = 51
95218
XDOT = 4165
547476 Wp = 13
58408
YDOT = -6384
460888 meter/sec RA = 118
16852 deg
ZDOT = -841
141187 TA = 84
44594
MA = 84
39702
Ha = 220
479 n
mi
Hp = 215
056
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10495470
93 X = -3193286
51
Y = -9143336
45 feet Y = -2822631
05 meter
Z = 17337272
66 Z = 5268874
84
XDOT = 13666
494344 XDOT = 4240
716408
YDOT = -20946
393989 feet/sec YDOT = -6337
458507 meter/sec
ZDOT = -2759
649564 ZDOT = -820
724757
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2503445
02 X = -763050
04
Y = -13779187
95 feet Y = -4199896
49 meter
Z = 17268563
26 Z = 5263458
08
XDOT = 22805
660546 XDOT = 6951
165334
YDOT = -7504
133504 feet/sec YDOT = -2287
259892 meter/sec
ZDOT = -2667
813827 ZDOT = -813
149654
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 18003
65449246
00016717 00000-0 10270-3 0 9032
2 25544 51
6413 118
9568 0003176 324
5859 35
5083 15
54286083 12923
Satellite: ISS
Catalog Number: 25544
Epoch time: 18003
65449246 = yrday
fracday
Element set: 903
Inclination: 51
6413 deg
RA of node: 118
9568 deg
Eccentricity:
0003176
Arg of perigee: 324
5859 deg
Mean anomaly: 35
5083 deg
Mean motion: 15
54286083 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1292
Checksum: 319
Coasting Arc #5 (Orbit 1306)
---------------------------------------
Vector Time (GMT): 2018/004/14:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2214345
02 A = 6779337
67 meter
Y = 4293119
38 meter E =
0009078
Z = -4764714
74 I = 51
97371
XDOT = -4656
185037 Wp = 94
74551
YDOT = 5434
224547 meter/sec RA = 113
19260 deg
ZDOT = 2736
200985 TA = 202
19550
MA = 202
23483
Ha = 220
610 n
mi
Hp = 214
969
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7264911
49 X = 2189317
73
Y = 14085037
33 feet Y = 4317742
11 meter
Z = -15632266
21 Z = -4754018
87
XDOT = -15276
197627 XDOT = -4729
896750
YDOT = 17828
820692 feet/sec YDOT = 5381
743554 meter/sec
ZDOT = 8977
037353 ZDOT = 2713
404578
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2855797
88 X = -870447
19
Y = 15635805
34 feet Y = 4765793
47 meter
Z = -15585280
62 Z = -4750393
53
XDOT = -21918
223113 XDOT = -6680
674405
YDOT = 4830
521892 feet/sec YDOT = 1472
343073 meter/sec
ZDOT = 8874
730901 ZDOT = 2705
017979
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 18004
61894351
00016717 00000-0 10270-3 0 9041
2 25544 51
6408 114
1487 0003201 333
3025 26
7963 15
54277776 13072
Satellite: ISS
Catalog Number: 25544
Epoch time: 18004
61894351 = yrday
fracday
Element set: 904
Inclination: 51
6408 deg
RA of node: 114
1487 deg
Eccentricity:
0003201
Arg of perigee: 333
3025 deg
Mean anomaly: 26
7963 deg
Mean motion: 15
54277776 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1307
Checksum: 297
Coasting Arc #6 (Orbit 1322)
---------------------------------------
Vector Time (GMT): 2018/005/14:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1219236
60 A = 6783025
42 meter
Y = -5547382
11 meter E =
0011148
Z = 3702771
65 I = 51
99833
XDOT = 4893
992122 Wp = 68
37636
YDOT = -3990
252326 meter/sec RA = 108
22596 deg
ZDOT = -4352
116014 TA = 67
75155
MA = 67
63335
Ha = 220
631 n
mi
Hp = 214
832
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4000120
08 X = -1175099
50
Y = -18200072
53 feet Y = -5560769
83 meter
Z = 12148200
96 Z = 3696956
06
XDOT = 16056
404599 XDOT = 4959
388427
YDOT = -13091
379022 feet/sec YDOT = -3935
158500 meter/sec
ZDOT = -14278
595845 ZDOT = -4328
184413
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7688290
32 X = 2343390
89
Y = -16992416
20 feet Y = -5179288
46 meter
Z = 12123133
72 Z = 3695131
16
XDOT = 19537
990242 XDOT = 5955
179426
YDOT = -1304
448682 feet/sec YDOT = -397
595958 meter/sec
ZDOT = -14171
437064 ZDOT = -4319
454017
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 18005
64768460
00016717 00000-0 10270-3 0 9057
2 25544 51
6408 109
0196 0003362 336
3354 23
7644 15
54305159 13236
Satellite: ISS
Catalog Number: 25544
Epoch time: 18005
64768460 = yrday
fracday
Element set: 905
Inclination: 51
6408 deg
RA of node: 109
0196 deg
Eccentricity:
0003362
Arg of perigee: 336
3354 deg
Mean anomaly: 23
7644 deg
Mean motion: 15
54305159 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1323
Checksum: 297
Coasting Arc #7 (Orbit 1325)
---------------------------------------
Vector Time (GMT): 2018/005/18:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4426163
18 A = 6778283
35 meter
Y = 943332
36 meter E =
0003802
Z = 5042968
98 I = 51
98061
XDOT = 685
533802 Wp = 91
01916
YDOT = -7379
321966 meter/sec RA = 107
36854 deg
ZDOT = 1980
704117 TA = 339
84128
MA = 339
85629
Ha = 220
962 n
mi
Hp = 214
785
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14521532
73 X = -4460878
53
Y = 3094922
43 feet Y = 893641
65 meter
Z = 16545173
82 Z = 5021384
26
XDOT = 2249
126647 XDOT = 758
379346
YDOT = -24210
373903 feet/sec YDOT = -7371
248638 meter/sec
ZDOT = 6498
373087 ZDOT = 1984
210764
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11388638
42 X = -3471256
99
Y = 9691656
75 feet Y = 2954016
98 meter
Z = 16448919
08 Z = 5013630
54
XDOT = -8885
971601 XDOT = -2708
444144
YDOT = -21507
015008 feet/sec YDOT = -6555
338174 meter/sec
ZDOT = 6515
091104 ZDOT = 1985
799768
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 18005
84057478
00016717 00000-0 10270-3 0 9060
2 25544 51
6376 108
0585 0003379 341
6359 18
4672 15
54255109 13267
Satellite: ISS
Catalog Number: 25544
Epoch time: 18005
84057478 = yrday
fracday
Element set: 906
Inclination: 51
6376 deg
RA of node: 108
0585 deg
Eccentricity:
0003379
Arg of perigee: 341
6359 deg
Mean anomaly: 18
4672 deg
Mean motion: 15
54255109 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1326
Checksum: 321
Coasting Arc #8 (Orbit 1340)
---------------------------------------
Vector Time (GMT): 2018/006/18:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4085049
03 A = 6776976
43 meter
Y = 883822
79 meter E =
0014416
Z = -5346751
08 I = 51
98534
XDOT = -1635
875133 Wp = 76
88062
YDOT = 7481
691403 meter/sec RA = 102
39189 deg
ZDOT = -9
960059 TA = 193
00619
MA = 193
04341
Ha = 220
895 n
mi
Hp = 214
827
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13402391
85 X = 4100833
66
Y = 2899681
08 feet Y = 929593
01 meter
Z = -17541834
25 Z = -5326869
21
XDOT = -5367
044400 XDOT = -1719
367460
YDOT = 24546
231636 feet/sec YDOT = 7462
931093 meter/sec
ZDOT = -32
677358 ZDOT = -18
109058
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13197081
72 X = 4022470
51
Y = -4118612
23 feet Y = -1255353
01 meter
Z = -17453431
57 Z = -5319805
94
XDOT = 7087
988644 XDOT = 2160
418939
YDOT = 23052
888293 feet/sec YDOT = 7026
520352 meter/sec
ZDOT = -70
093628 ZDOT = -21
364538
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 18006
80501503
00016717 00000-0 10270-3 0 9071
2 25544 51
6379 103
2501 0003360 345
5512 14
5544 15
54259553 13418
Satellite: ISS
Catalog Number: 25544
Epoch time: 18006
80501503 = yrday
fracday
Element set: 907
Inclination: 51
6379 deg
RA of node: 103
2501 deg
Eccentricity:
0003360
Arg of perigee: 345
5512 deg
Mean anomaly: 14
5544 deg
Mean motion: 15
54259553 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1341
Checksum: 273
Coasting Arc #9 (Orbit 1356)
---------------------------------------
Vector Time (GMT): 2018/007/18:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3623950
04 A = 6778152
49 meter
Y = -2707581
83 meter E =
0007826
Z = 5046128
35 I = 51
99580
XDOT = 2464
369114 Wp = 31
85083
YDOT = -6990
090977 meter/sec RA = 97
41478 deg
ZDOT = -1972
963112 TA = 77
24663
MA = 77
15918
Ha = 221
014 n
mi
Hp = 214
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11889599
86 X = -3617914
99
Y = -8883142
49 feet Y = -2748073
69 meter
Z = 16555539
19 Z = 5028539
21
XDOT = 8085
200506 XDOT = 2551
934564
YDOT = -22933
369348 feet/sec YDOT = -6962
043063 meter/sec
ZDOT = -6472
976089 ZDOT = -1960
779644
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14843762
01 X = -4524378
66
Y = -1584099
50 feet Y = -482833
53 meter
Z = 16477622
44 Z = 5022379
32
XDOT = -4718
602092 XDOT = -1438
229918
YDOT = -22809
721042 feet/sec YDOT = -6952
402974 meter/sec
ZDOT = -6417
654909 ZDOT = -1956
101216
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 18007
83374423
00016717 00000-0 10270-3 0 9085
2 25544 51
6380 98
1202 0003488 348
6800 11
4274 15
54289293 13572
Satellite: ISS
Catalog Number: 25544
Epoch time: 18007
83374423 = yrday
fracday
Element set: 908
Inclination: 51
6380 deg
RA of node: 98
1202 deg
Eccentricity:
0003488
Arg of perigee: 348
6800 deg
Mean anomaly: 11
4274 deg
Mean motion: 15
54289293 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1357
Checksum: 311
Coasting Arc #10 (Orbit 1371)
---------------------------------------
Vector Time (GMT): 2018/008/18:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3105984
72 A = 6781471
35 meter
Y = 4320685
97 meter E =
0007047
Z = -4209300
80 I = 52
00975
XDOT = -3165
326855 Wp = 82
46159
YDOT = 5900
125691 meter/sec RA = 92
44547 deg
ZDOT = 3726
825868 TA = 225
61428
MA = 225
67201
Ha = 221
110 n
mi
Hp = 214
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10190238
58 X = 3077885
24
Y = 14175478
90 feet Y = 4355262
21 meter
Z = -13810041
99 Z = -4194281
23
XDOT = -10384
930628 XDOT = -3249
171239
YDOT = 19357
367751 feet/sec YDOT = 5864
259942 meter/sec
ZDOT = 12227
118989 ZDOT = 3711
246409
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16160847
57 X = 4925826
34
Y = 6740685
37 feet Y = 2054560
90 meter
Z = -13743820
09 Z = -4189116
36
XDOT = 1646
648150 XDOT = 501
898356
YDOT = 20797
295882 feet/sec YDOT = 6339
015785 meter/sec
ZDOT = 12156
827290 ZDOT = 3705
400958
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 18008
79817291
00016717 00000-0 10270-3 0 9097
2 25544 51
6378 93
3117 0003602 353
5000 6
6106 15
54273031 13726
Satellite: ISS
Catalog Number: 25544
Epoch time: 18008
79817291 = yrday
fracday
Element set: 909
Inclination: 51
6378 deg
RA of node: 93
3117 deg
Eccentricity:
0003602
Arg of perigee: 353
5000 deg
Mean anomaly: 6
6106 deg
Mean motion: 15
54273031 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1372
Checksum: 287
Coasting Arc #11 (Orbit 1387)
---------------------------------------
Vector Time (GMT): 2018/009/18:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2495208
56 A = 6785321
97 meter
Y = -5610609
55 meter E =
0012979
Z = 2878094
01 I = 52
02342
XDOT = 3788
358654 Wp = 83
24449
YDOT = -4306
801014 meter/sec RA = 87
48614 deg
ZDOT = -5090
281033 TA = 64
18032
MA = 64
04649
Ha = 221
077 n
mi
Hp = 214
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8186379
80 X = -2446263
97
Y = -18407511
64 feet Y = -5638239
11 meter
Z = 9442565
64 Z = 2866091
88
XDOT = 12428
998208 XDOT = 3860
962703
YDOT = -14129
924588 feet/sec YDOT = -4264
030866 meter/sec
ZDOT = -16700
397089 ZDOT = -5071
702381
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16825288
70 X = -5128347
99
Y = -11124435
82 feet Y = -3390728
04 meter
Z = 9389991
10 Z = 2862069
29
XDOT = 2206
792290 XDOT = 672
630290
YDOT = -17422
627057 feet/sec YDOT = -5310
416727 meter/sec
ZDOT = -16616
983076 ZDOT = -5064
856441
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 18009
82689159
00016717 00000-0 10270-3 0 9104
2 25544 51
6378 88
1817 0003649 355
8067 4
3055 15
54312879 13883
Satellite: ISS
Catalog Number: 25544
Epoch time: 18009
82689159 = yrday
fracday
Element set: 910
Inclination: 51
6378 deg
RA of node: 88
1817 deg
Eccentricity:
0003649
Arg of perigee: 355
8067 deg
Mean anomaly: 4
3055 deg
Mean motion: 15
54312879 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1388
Checksum: 341
Coasting Arc #12 (Orbit 1402)
---------------------------------------
Vector Time (GMT): 2018/010/18:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1828701
06 A = 6788100
78 meter
Y = 6408628
03 meter E =
0012105
Z = -1256838
65 I = 52
03136
XDOT = -4315
144773 Wp = 27
56477
YDOT = 2377
687675 meter/sec RA = 82
53720 deg
ZDOT = 5878
250216 TA = 318
83908
MA = 318
93032
Ha = 221
161 n
mi
Hp = 214
244
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5999675
38 X = 1763007
18
Y = 21025682
51 feet Y = 6428710
56 meter
Z = -4123486
39 Z = -1248114
75
XDOT = -14157
299125 XDOT = -4369
965351
YDOT = 7800
812582 feet/sec YDOT = 2329
125981 meter/sec
ZDOT = 19285
597820 ZDOT = 5857
155768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16599448
79 X = 5059511
99
Y = 14242343
04 feet Y = 4341066
16 meter
Z = -4085649
77 Z = -1245306
05
XDOT = -6597
362652 XDOT = -2010
876136
YDOT = 13163
263532 feet/sec YDOT = 4012
162724 meter/sec
ZDOT = 19191
273378 ZDOT = 5849
500125
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 18010
79130962
00016717 00000-0 10270-3 0 9116
2 25544 51
6388 83
3732 0003581 1
0095 359
1065 15
54324142 14039
Satellite: ISS
Catalog Number: 25544
Epoch time: 18010
79130962 = yrday
fracday
Element set: 911
Inclination: 51
6388 deg
RA of node: 83
3732 deg
Eccentricity:
0003581
Arg of perigee: 1
0095 deg
Mean anomaly: 359
1065 deg
Mean motion: 15
54324142 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1403
Checksum: 279
Coasting Arc #13 (Orbit 1418)
---------------------------------------
Vector Time (GMT): 2018/011/18:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1036697
82 A = 6788618
58 meter
Y = -6684477
27 meter E =
0008636
Z = -542935
22 I = 52
02862
XDOT = 4748
594174 Wp = 120
74121
YDOT = -254
233379 meter/sec RA = 77
59260 deg
ZDOT = -6012
075182 TA = 65
08376
MA = 64
99404
Ha = 221
215 n
mi
Hp = 214
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3401239
57 X = -959235
86
Y = -21930699
72 feet Y = -6695637
19 meter
Z = -1781283
53 Z = -547783
37
XDOT = 15579
377211 XDOT = 4780
287532
YDOT = -834
099014 feet/sec YDOT = -200
953789 meter/sec
ZDOT = -19724
656109 ZDOT = -5988
931284
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15176015
44 X = -4625649
51
Y = -16190709
13 feet Y = -4934928
14 meter
Z = -1801800
43 Z = -549188
77
XDOT = 11315
274564 XDOT = 3448
895687
YDOT = -8449
603496 feet/sec YDOT = -2575
439145 meter/sec
ZDOT = -19621
537540 ZDOT = -5980
644642
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 18011
82001601
00016717 00000-0 10270-3 0 9129
2 25544 51
6395 78
2432 0003795 3
5453 356
5726 15
54327553 14190
Satellite: ISS
Catalog Number: 25544
Epoch time: 18011
82001601 = yrday
fracday
Element set: 912
Inclination: 51
6395 deg
RA of node: 78
2432 deg
Eccentricity:
0003795
Arg of perigee: 3
5453 deg
Mean anomaly: 356
5726 deg
Mean motion: 15
54327553 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1419
Checksum: 293
Coasting Arc #14 (Orbit 1434)
---------------------------------------
Vector Time (GMT): 2018/012/18:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 157423
94 A = 6786540
92 meter
Y = 6391793
78 meter E =
0015753
Z = 2248968
58 I = 52
01370
XDOT = -5052
803810 Wp = 59
48037
YDOT = -1812
288703 meter/sec RA = 72
64629 deg
ZDOT = 5483
741691 TA = 325
41758
MA = 325
51994
Ha = 221
236 n
mi
Hp = 214
058
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 516482
75 X = 75013
24
Y = 20970452
03 feet Y = 6393093
26 meter
Z = 7378505
82 Z = 2249533
57
XDOT = -16577
440320 XDOT = -5058
799751
YDOT = -5945
829079 feet/sec YDOT = -1868
826520 meter/sec
ZDOT = 17991
278514 ZDOT = 5459
182368
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12514004
08 X = 3814268
45
Y = 16834623
96 feet Y = 5131193
38 meter
Z = 7379979
60 Z = 2249417
78
XDOT = -15829
318346 XDOT = -4824
776232
YDOT = 3897
801910 feet/sec YDOT = 1188
050022 meter/sec
ZDOT = 17882
189399 ZDOT = 5450
491329
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 18012
84871686
00016717 00000-0 10270-3 0 9131
2 25544 51
6393 73
1144 0003654 6
8991 353
2212 15
54350662 14358
Satellite: ISS
Catalog Number: 25544
Epoch time: 18012
84871686 = yrday
fracday
Element set: 913
Inclination: 51
6393 deg
RA of node: 73
1144 deg
Eccentricity:
0003654
Arg of perigee: 6
8991 deg
Mean anomaly: 353
2212 deg
Mean motion: 15
54350662 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1435
Checksum: 303
Coasting Arc #15 (Orbit 1436)
---------------------------------------
Vector Time (GMT): 2018/012/22:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 926807
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4430690
88 A = 6781205
07 meter
Y = -2889714
15 meter E =
0012149
Z = 4238469
10 I = 51
99642
XDOT = 831
916622 Wp = 57
65883
YDOT = -6682
246937 meter/sec RA = 71
87508 deg
ZDOT = -3672
211414 TA = 69
82273
MA = 69
69210
Ha = 221
366 n
mi
Hp = 214
070
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14536387
41 X = -4418636
15
Y = -9480689
46 feet Y = -2939194
06 meter
Z = 13905738
51 Z = 4216975
54
XDOT = 2729
385243 XDOT = 924
415038
YDOT = -21923
382339 feet/sec YDOT = -6672
426426 meter/sec
ZDOT = -12047
937711 ZDOT = -3667
946086
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9892541
32 X = -3015246
59
Y = 14351580
17 feet Y = 4374361
64 meter
Z = 13810480
36 Z = 4209434
41
XDOT = -20788
914620 XDOT = -6336
461176
YDOT = -2710
985756 feet/sec YDOT = -826
308458 meter/sec
ZDOT = -12027
848131 ZDOT = -3666
088110
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 18012
97730549
00016717 00000-0 10270-3 0 9148
2 25544 51
6415 72
4748 0003793 7
7056 352
4154 15
54336800 14377
Satellite: ISS
Catalog Number: 25544
Epoch time: 18012
97730549 = yrday
fracday
Element set: 914
Inclination: 51
6415 deg
RA of node: 72
4748 deg
Eccentricity:
0003793
Arg of perigee: 7
7056 deg
Mean anomaly: 352
4154 deg
Mean motion: 15
54336800 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1437
Checksum: 309
Coasting Arc #16 (Orbit 1443)
---------------------------------------
Vector Time (GMT): 2018/013/10:05:30
000
Vector Time (MET): N/A
Weight (LBS) : 904658
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4300411
42 A = 6784082
77 meter
Y = 4049515
55 meter E =
0006261
Z = -3336731
06 I = 52
00109
XDOT = -1777
776865 Wp = 53
51489
YDOT = 5770
449130 meter/sec RA = 69
46684 deg
ZDOT = 4721
652957 TA = 267
86607
MA = 267
93777
Ha = 221
213 n
mi
Hp = 214
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14108961
37 X = 4271017
00
Y = 13285812
17 feet Y = 4097441
59 meter
Z = -10947280
39 Z = -3315912
39
XDOT = -5832
601264 XDOT = -1865
106591
YDOT = 18931
919719 feet/sec YDOT = 5750
080170 meter/sec
ZDOT = 15490
987393 ZDOT = 4712
805517
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14838870
99 X = -4522887
88
Y = 12545542
65 feet Y = 3823881
40 meter
Z = -10855220
45 Z = -3308671
19
XDOT = -17203
014609 XDOT = -5243
478853
YDOT = -7006
751119 feet/sec YDOT = -2135
657741 meter/sec
ZDOT = 15450
632190 ZDOT = 4709
352691
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 18013
42735879
00016717 00000-0 10270-3 0 9151
2 25544 51
6416 70
2279 0003334 6
4516 353
6679 15
54335305 14443
Satellite: ISS
Catalog Number: 25544
Epoch time: 18013
42735879 = yrday
fracday
Element set: 915
Inclination: 51
6416 deg
RA of node: 70
2279 deg
Eccentricity:
0003334
Arg of perigee: 6
4516 deg
Mean anomaly: 353
6679 deg
Mean motion: 15
54335305 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1444
Checksum: 308
Coasting Arc #17 (Orbit 1459)
---------------------------------------
Vector Time (GMT): 2018/014/10:05:30
000
Vector Time (MET): N/A
Weight (LBS) : 904658
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3991489
67 A = 6787431
05 meter
Y = -5197656
15 meter E =
0013591
Z = 1749075
14 I = 52
00009
XDOT = 2941
986653 Wp = 100
69587
YDOT = -4191
817028 meter/sec RA = 64
51351 deg
ZDOT = -5707
820812 TA = 60
20288
MA = 60
06779
Ha = 221
283 n
mi
Hp = 213
994
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13095438
54 X = -3941567
42
Y = -17052677
65 feet Y = -5242012
72 meter
Z = 5738435
50 Z = 1729806
90
XDOT = 9652
187181 XDOT = 3016
367331
YDOT = -13752
680539 feet/sec YDOT = -4158
501382 meter/sec
ZDOT = -18726
446234 ZDOT = -5693
349477
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18266232
84 X = 5567547
77
Y = -11384063
39 feet Y = -3469862
52 meter
Z = 5653477
37 Z = 1723179
90
XDOT = 11891
087155 XDOT = 3624
403365
YDOT = 9754
361757 feet/sec YDOT = 2973
129463 meter/sec
ZDOT = -18661
292361 ZDOT = -5687
961912
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 18014
45605177
00016717 00000-0 10270-3 0 9163
2 25544 51
6417 65
0985 0003486 12
4553 347
6685 15
54349075 14603
Satellite: ISS
Catalog Number: 25544
Epoch time: 18014
45605177 = yrday
fracday
Element set: 916
Inclination: 51
6417 deg
RA of node: 65
0985 deg
Eccentricity:
0003486
Arg of perigee: 12
4553 deg
Mean anomaly: 347
6685 deg
Mean motion: 15
54349075 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1460
Checksum: 320
Coasting Arc #18 (Orbit 1475)
---------------------------------------
Vector Time (GMT): 2018/015/10:05:30
000
Vector Time (MET): N/A
Weight (LBS) : 904658
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3434789
61 A = 6788792
96 meter
Y = 5846249
09 meter E =
0015449
Z = -149
29 I = 51
98884
XDOT = -4077
076430 Wp = 38
60283
YDOT = 2386
952653 meter/sec RA = 59
56589 deg
ZDOT = 6044
540157 TA = 321
39557
MA = 321
50593
Ha = 221
454 n
mi
Hp = 213
911
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11268994
80 X = 3369160
73
Y = 19180607
26 feet Y = 5884292
31 meter
Z = -489
80 Z = 16376
56
XDOT = -13376
235006 XDOT = -4132
825761
YDOT = 7831
209490 feet/sec YDOT = 2341
047810 meter/sec
ZDOT = 19831
168493 ZDOT = 6024
600175
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20036778
64 X = -6107210
13
Y = 9664793
68 feet Y = 2945829
11 meter
Z = 72138
00 Z = 21987
66
XDOT = -5998
970863 XDOT = -1828
486319
YDOT = -12640
029639 feet/sec YDOT = -3852
681034 meter/sec
ZDOT = 19741
951230 ZDOT = 6017
346735
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 18015
48474117
00016717 00000-0 10270-3 0 9176
2 25544 51
6413 59
9690 0003686 15
6486 344
4780 15
54314423 14763
Satellite: ISS
Catalog Number: 25544
Epoch time: 18015
48474117 = yrday
fracday
Element set: 917
Inclination: 51
6413 deg
RA of node: 59
9690 deg
Eccentricity:
0003686
Arg of perigee: 15
6486 deg
Mean anomaly: 344
4780 deg
Mean motion: 15
54314423 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1476
Checksum: 323
Coasting Arc #19 (Orbit 1490)
---------------------------------------
Vector Time (GMT): 2018/016/10:05:30
000
Vector Time (MET): N/A
Weight (LBS) : 904658
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2562940
76 A = 6787274
63 meter
Y = -6024729
27 meter E =
0006309
Z = -1788354
35 I = 51
96582
XDOT = 5110
575103 Wp = 112
32575
YDOT = -490
592753 meter/sec RA = 54
61750 deg
ZDOT = -5689
694770 TA = 87
21854
MA = 87
14633
Ha = 221
393 n
mi
Hp = 213
768
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8408598
30 X = -2486693
39
Y = -19766172
16 feet Y = -6052963
38 meter
Z = -5867304
29 Z = -1800619
26
XDOT = 16766
978685 XDOT = 5143
318302
YDOT = -1609
556277 feet/sec YDOT = -433
259322 meter/sec
ZDOT = -18666
977593 ZDOT = -5664
790280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20265401
00 X = 6176894
22
Y = -7077260
77 feet Y = -2157149
08 meter
Z = -5920916
25 Z = -1804695
27
XDOT = 2
201689 XDOT =
671075
YDOT = 15480
581130 feet/sec YDOT = 4718
481128 meter/sec
ZDOT = -18555
963754 ZDOT = -5655
857752
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 18016
44913168
00016717 00000-0 10270-3 0 9188
2 25544 51
6403 55
1604 0003548 20
6661 339
4635 15
54358533 14913
Satellite: ISS
Catalog Number: 25544
Epoch time: 18016
44913168 = yrday
fracday
Element set: 918
Inclination: 51
6403 deg
RA of node: 55
1604 deg
Eccentricity:
0003548
Arg of perigee: 20
6661 deg
Mean anomaly: 339
4635 deg
Mean motion: 15
54358533 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1491
Checksum: 305
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