[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 26th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14929 5437 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 118 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
271/01:02:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
3
000/00:00:00
000 0
0 0
0 216
1
274/09:07:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
8
000/00:00:00
000 0
0 0
0 216
3
277/07:57:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
5
000/00:00:00
000 0
0 0
0 216
4
280/14:44:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
1
000/00:00:00
000 0
0 0
0 216
6
283/18:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
2
000/00:00:00
000 0
0 0
0 216
5
Coasting Arc #1 (Orbit 1426)
---------------------------------------
Vector Time (GMT): 2018/269/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 909660
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 401337
08 A = 6782413
71 meter
Y = -5203220
29 meter E =
0009499
Z = 4329884
20 I = 51
32533
XDOT = 5987
373762 Wp = 132
59286
YDOT = 3333
555009 meter/sec RA = 232
79691 deg
ZDOT = 3439
818749 TA = 282
28077
MA = 282
38711
Ha = 221
297 n
mi
Hp = 215
947
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1316722
72 X = 438458
57
Y = -17070932
71 feet Y = -5198524
17 meter
Z = 14205656
82 Z = 4331924
58
XDOT = 19643
614706 XDOT = 5932
943008
YDOT = 10936
860266 feet/sec YDOT = 3400
206059 meter/sec
ZDOT = 11285
494582 ZDOT = 3468
771051
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 80424
80 X = 24513
48
Y = 17113425
41 feet Y = 5216172
07 meter
Z = 14215322
39 Z = 4332830
26
XDOT = -19095
895204 XDOT = -5820
428858
YDOT = -9422
559455 feet/sec YDOT = -2871
996122 meter/sec
ZDOT = 11415
056136 ZDOT = 3479
309110
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 18269
55456592
00016717 00000-0 10270-3 0 9004
2 25544 51
6383 233
5618 0004016 212
9128 147
1775 15
53770035 14274
Satellite: ISS
Catalog Number: 25544
Epoch time: 18269
55456592 = yrday
fracday
Element set: 900
Inclination: 51
6383 deg
RA of node: 233
5618 deg
Eccentricity:
0004016
Arg of perigee: 212
9128 deg
Mean anomaly: 147
1775 deg
Mean motion: 15
53770035 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1427
Checksum: 312
Coasting Arc #2 (Orbit 1441)
---------------------------------------
Vector Time (GMT): 2018/270/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1595763
71 A = 6779675
44 meter
Y = 4248935
87 meter E =
0010414
Z = -5045325
99 I = 51
33640
XDOT = -5984
659182 Wp = 89
91139
YDOT = -4417
108544 meter/sec RA = 227
78451 deg
ZDOT = -1830
287202 TA = 162
28807
MA = 162
25174
Ha = 221
231 n
mi
Hp = 215
997
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5235445
25 X = -1618649
99
Y = 13940078
30 feet Y = 4230962
40 meter
Z = -16552906
80 Z = -5053133
84
XDOT = -19634
708602 XDOT = -5925
930347
YDOT = -14491
825933 feet/sec YDOT = -4483
704986 meter/sec
ZDOT = -6004
879271 ZDOT = -1859
215904
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3803195
80 X = 1159214
08
Y = -14356069
81 feet Y = -4375730
08 meter
Z = -16588349
97 Z = -5056129
07
XDOT = 19813
474438 XDOT = 6039
147009
YDOT = 12324
684031 feet/sec YDOT = 3756
563693 meter/sec
ZDOT = -6134
242543 ZDOT = -1869
717127
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 18270
51934240
00016717 00000-0 10270-3 0 9014
2 25544 51
6380 228
7546 0003815 216
3551 143
7343 15
53728343 14426
Satellite: ISS
Catalog Number: 25544
Epoch time: 18270
51934240 = yrday
fracday
Element set: 901
Inclination: 51
6380 deg
RA of node: 228
7546 deg
Eccentricity:
0003815
Arg of perigee: 216
3551 deg
Mean anomaly: 143
7343 deg
Mean motion: 15
53728343 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1442
Checksum: 294
Coasting Arc #3 (Orbit 1450)
---------------------------------------
Vector Time (GMT): 2018/271/01:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -429424
17 A = 6782690
38 meter
Y = -5256317
98 meter E =
0009532
Z = 4263186
48 I = 51
36116
XDOT = 6370
176060 Wp = 132
57295
YDOT = 2368
044425 meter/sec RA = 225
07318 deg
ZDOT = 3549
941288 TA = 281
02135
MA = 281
12855
Ha = 221
289 n
mi
Hp = 216
069
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1408871
95 X = -391323
31
Y = -17245137
73 feet Y = -5260906
63 meter
Z = 13986832
28 Z = 4261193
53
XDOT = 20899
527756 XDOT = 6325
978451
YDOT = 7769
174623 feet/sec YDOT = 2439
033392 meter/sec
ZDOT = 11646
789004 ZDOT = 3580
778315
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7720298
11 X = -2353146
86
Y = -15492339
22 feet Y = -4722065
00 meter
Z = 13978397
44 Z = 4260615
54
XDOT = 21090
739967 XDOT = 6428
457542
YDOT = 156
920046 feet/sec YDOT = 47
829230 meter/sec
ZDOT = 11784
920177 ZDOT = 3592
043670
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 18271
09820555
00016717 00000-0 10270-3 0 9022
2 25544 51
6400 225
8675 0004351 215
1523 144
9343 15
53765733 14519
Satellite: ISS
Catalog Number: 25544
Epoch time: 18271
09820555 = yrday
fracday
Element set: 902
Inclination: 51
6400 deg
RA of node: 225
8675 deg
Eccentricity:
0004351
Arg of perigee: 215
1523 deg
Mean anomaly: 144
9343 deg
Mean motion: 15
53765733 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1451
Checksum: 295
Coasting Arc #4 (Orbit 1465)
---------------------------------------
Vector Time (GMT): 2018/272/01:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -881023
84 A = 6779809
71 meter
Y = 4490358
67 meter E =
0009661
Z = -5010982
10 I = 51
37633
XDOT = -6546
785478 Wp = 90
64573
YDOT = -3463
819411 meter/sec RA = 220
06525 deg
ZDOT = -1956
276809 TA = 160
29437
MA = 160
25701
Ha = 221
165 n
mi
Hp = 216
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2890498
17 X = -906829
65
Y = 14732147
87 feet Y = 4480361
75 meter
Z = -16440229
99 Z = -5015324
94
XDOT = -21478
954979 XDOT = -6498
062780
YDOT = -11364
236913 feet/sec YDOT = -3536
757845 meter/sec
ZDOT = -6418
231000 ZDOT = -1987
960767
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3066995
64 X = 934820
27
Y = 14674107
54 feet Y = 4472667
98 meter
Z = -16460146
67 Z = -5017052
71
XDOT = -23083
002248 XDOT = -7035
699085
YDOT = -2521
573057 feet/sec YDOT = -768
575468 meter/sec
ZDOT = -6560
072565 ZDOT = -1999
510118
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 18272
06297764
00016717 00000-0 10270-3 0 9031
2 25544 51
6409 221
0618 0004288 219
3082 140
7760 15
53738707 14662
Satellite: ISS
Catalog Number: 25544
Epoch time: 18272
06297764 = yrday
fracday
Element set: 903
Inclination: 51
6409 deg
RA of node: 221
0618 deg
Eccentricity:
0004288
Arg of perigee: 219
3082 deg
Mean anomaly: 140
7760 deg
Mean motion: 15
53738707 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1466
Checksum: 317
Coasting Arc #5 (Orbit 1481)
---------------------------------------
Vector Time (GMT): 2018/273/01:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2241368
12 A = 6778367
25 meter
Y = -3590944
74 meter E =
0003551
Z = 5294616
18 I = 51
39814
XDOT = 6365
008872 Wp = 187
46657
YDOT = 4271
423302 meter/sec RA = 215
05262 deg
ZDOT = 199
052109 TA = 260
60983
MA = 260
64998
Ha = 220
934 n
mi
Hp = 216
225
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7353569
93 X = 2255637
57
Y = -11781314
76 feet Y = -3565800
09 meter
Z = 17370788
00 Z = 5305539
04
XDOT = 20882
575041 XDOT = 6315
804661
YDOT = 14013
855979 feet/sec YDOT = 4342
326142 meter/sec
ZDOT = 653
058100 ZDOT = 229
851877
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1944563
21 X = 592702
87
Y = -13688527
11 feet Y = -4172263
06 meter
Z = 17420147
63 Z = 5309661
00
XDOT = 23734
616447 XDOT = 7234
311093
YDOT = 4392
483774 feet/sec YDOT = 1338
829054 meter/sec
ZDOT = 790
873483 ZDOT = 241
058238
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 18273
09206204
00016717 00000-0 10270-3 0 9045
2 25544 51
6410 215
9344 0004187 223
6983 136
3838 15
53785089 14828
Satellite: ISS
Catalog Number: 25544
Epoch time: 18273
09206204 = yrday
fracday
Element set: 904
Inclination: 51
6410 deg
RA of node: 215
9344 deg
Eccentricity:
0004187
Arg of perigee: 223
6983 deg
Mean anomaly: 136
3838 deg
Mean motion: 15
53785089 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1482
Checksum: 317
Coasting Arc #6 (Orbit 1496)
---------------------------------------
Vector Time (GMT): 2018/274/01:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3600147
22 A = 6779177
37 meter
Y = 2631390
19 meter E =
0011804
Z = -5116399
11 I = 51
42805
XDOT = -5760
359035 Wp = 118
83945
YDOT = -4792
352954 meter/sec RA = 210
04275 deg
ZDOT = 1585
740749 TA = 166
53219
MA = 166
50066
Ha = 220
919 n
mi
Hp = 216
141
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11811506
63 X = -3604451
45
Y = 8633169
91 feet Y = 2591106
55 meter
Z = -16786086
32 Z = -5133898
21
XDOT = -18898
815733 XDOT = -5714
044296
YDOT = -15722
942764 feet/sec YDOT = -4856
510253 meter/sec
ZDOT = 5202
561514 ZDOT = 1557
871216
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7073735
75 X = -2156074
66
Y = 12702528
85 feet Y = 3871730
79 meter
Z = -16864875
60 Z = -5140414
08
XDOT = -22818
422230 XDOT = -6955
055096
YDOT = -5953
058447 feet/sec YDOT = -1814
492215 meter/sec
ZDOT = 5077
925872 ZDOT = 1547
751806
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 18274
05682858
00016717 00000-0 10270-3 0 9056
2 25544 51
6405 211
1293 0004106 226
1476 133
9338 15
53776021 14979
Satellite: ISS
Catalog Number: 25544
Epoch time: 18274
05682858 = yrday
fracday
Element set: 905
Inclination: 51
6405 deg
RA of node: 211
1293 deg
Eccentricity:
0004106
Arg of perigee: 226
1476 deg
Mean anomaly: 133
9338 deg
Mean motion: 15
53776021 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1497
Checksum: 309
Coasting Arc #7 (Orbit 1502)
---------------------------------------
Vector Time (GMT): 2018/274/09:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5505669
65 A = 6789917
50 meter
Y = -3847358
24 meter E =
0009576
Z = 963796
10 I = 51
46996
XDOT = 3461
758601 Wp = 58
10708
YDOT = -3467
010388 meter/sec RA = 208
38480 deg
ZDOT = 5897
177637 TA = 312
35399
MA = 312
43504
Ha = 220
831 n
mi
Hp = 216
268
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18063220
63 X = -5466919
90
Y = -12622566
40 feet Y = -3908709
75 meter
Z = 3162060
70 Z = 937145
38
XDOT = 11357
475726 XDOT = 3471
624621
YDOT = -11374
705999 feet/sec YDOT = -3428
243200 meter/sec
ZDOT = 19347
695661 ZDOT = 5914
017990
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7951740
74 X = 2423690
58
Y = 20569855
09 feet Y = 6269691
83 meter
Z = 3042799
81 Z = 927445
38
XDOT = -14166
060893 XDOT = -4317
815360
YDOT = 2583
716204 feet/sec YDOT = 787
516699 meter/sec
ZDOT = 19423
609541 ZDOT = 5920
316188
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 18274
44273239
00016717 00000-0 10270-3 0 9069
2 25544 51
6367 209
2091 0003937 228
7032 131
3781 15
53801115 15032
Satellite: ISS
Catalog Number: 25544
Epoch time: 18274
44273239 = yrday
fracday
Element set: 906
Inclination: 51
6367 deg
RA of node: 209
2091 deg
Eccentricity:
0003937
Arg of perigee: 228
7032 deg
Mean anomaly: 131
3781 deg
Mean motion: 15
53801115 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1503
Checksum: 295
Coasting Arc #8 (Orbit 1517)
---------------------------------------
Vector Time (GMT): 2018/275/09:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4721821
94 A = 6787857
16 meter
Y = 4193561
14 meter E =
0005828
Z = -2480015
24 I = 51
49313
XDOT = -4961
057512 Wp = 170
98216
YDOT = 2452
650698 meter/sec RA = 203
40210 deg
ZDOT = -5305
640542 TA = 36
86485
MA = 36
82480
Ha = 220
766 n
mi
Hp = 216
408
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15491541
81 X = 4686624
16
Y = 13758402
69 feet Y = 4246166
94 meter
Z = -8136532
93 Z = -2457163
69
XDOT = -16276
435408 XDOT = -4962
342772
YDOT = 8046
754258 feet/sec YDOT = 2397
165336 meter/sec
ZDOT = -17406
957159 ZDOT = -5329
743072
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5556702
72 X = -1693682
99
Y = -20001428
47 feet Y = -6096435
40 meter
Z = -8034338
45 Z = -2448866
36
XDOT = 16477
814982 XDOT = 5022
438007
YDOT = 2448
151807 feet/sec YDOT = 746
196671 meter/sec
ZDOT = -17515
385898 ZDOT = -5338
689622
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 18275
40749582
00016717 00000-0 10270-3 0 9076
2 25544 51
6376 204
4017 0003732 235
8541 124
2258 15
53759838 15184
Satellite: ISS
Catalog Number: 25544
Epoch time: 18275
40749582 = yrday
fracday
Element set: 907
Inclination: 51
6376 deg
RA of node: 204
4017 deg
Eccentricity:
0003732
Arg of perigee: 235
8541 deg
Mean anomaly: 124
2258 deg
Mean motion: 15
53759838 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1518
Checksum: 324
Coasting Arc #9 (Orbit 1533)
---------------------------------------
Vector Time (GMT): 2018/276/09:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 943739
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3607660
41 A = 6784409
06 meter
Y = -4346479
17 meter E =
0008834
Z = 3753424
81 I = 51
51296
XDOT = 6213
167911 Wp = 111
16356
YDOT = -1485
105074 meter/sec RA = 198
41544 deg
ZDOT = 4240
930361 TA = 293
83164
MA = 293
92421
Ha = 220
603 n
mi
Hp = 216
439
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11836156
20 X = -3577021
00
Y = -14260102
27 feet Y = -4386651
06 meter
Z = 12314385
86 Z = 3735974
56
XDOT = 20384
409158 XDOT = 6208
712679
YDOT = -4872
391975 feet/sec YDOT = -1415
649849 meter/sec
ZDOT = 13913
813520 ZDOT = 4271
101178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2557372
35 X = 779487
09
Y = 18407027
88 feet Y = 5610462
10 meter
Z = 12236436
61 Z = 3729665
88
XDOT = -18449
712611 XDOT = -5623
472404
YDOT = -6800
888053 feet/sec YDOT = -2072
910679 meter/sec
ZDOT = 14049
412574 ZDOT = 4282
260953
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 18276
43656888
00016717 00000-0 10270-3 0 9087
2 25544 51
6378 199
2751 0003867 240
0551 120
0217 15
53793237 15348
Satellite: ISS
Catalog Number: 25544
Epoch time: 18276
43656888 = yrday
fracday
Element set: 908
Inclination: 51
6378 deg
RA of node: 199
2751 deg
Eccentricity:
0003867
Arg of perigee: 240
0551 deg
Mean anomaly: 120
0217 deg
Mean motion: 15
53793237 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1534
Checksum: 329
Coasting Arc #10 (Orbit 1547)
---------------------------------------
Vector Time (GMT): 2018/277/07:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6219185
83 A = 6787344
22 meter
Y = 648782
19 meter E =
0001400
Z = -2638785
35 I = 51
55185
XDOT = -2722
664625 Wp = 34
20496
YDOT = -4916
416702 meter/sec RA = 193
62047 deg
ZDOT = 5210
585778 TA = 296
02973
MA = 296
04414
Ha = 220
547 n
mi
Hp = 216
375
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20404152
99 X = -6213160
61
Y = 2128550
49 feet Y = 579268
47 meter
Z = -8657432
26 Z = -2668981
49
XDOT = -8932
626724 XDOT = -2692
795882
YDOT = -16129
976058 feet/sec YDOT = -4946
696112 meter/sec
ZDOT = 17095
097697 ZDOT = 5197
432820
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15065499
26 X = 4591964
17
Y = 13839208
41 feet Y = 4218190
72 meter
Z = -8793086
07 Z = -2680132
63
XDOT = -5088
988491 XDOT = -1551
123692
YDOT = 16359
386641 feet/sec YDOT = 4986
341048 meter/sec
ZDOT = 17036
481189 ZDOT = 5192
719467
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 18277
33700709
00016717 00000-0 10270-3 0 9090
2 25544 51
6367 194
7889 0003656 243
3020 116
7758 15
53763560 15484
Satellite: ISS
Catalog Number: 25544
Epoch time: 18277
33700709 = yrday
fracday
Element set: 909
Inclination: 51
6367 deg
RA of node: 194
7889 deg
Eccentricity:
0003656
Arg of perigee: 243
3020 deg
Mean anomaly: 116
7758 deg
Mean motion: 15
53763560 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1548
Checksum: 338
Coasting Arc #11 (Orbit 1563)
---------------------------------------
Vector Time (GMT): 2018/278/07:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6685760
74 A = 6789733
17 meter
Y = 103238
68 meter E =
0011820
Z = 1138666
16 I = 51
59323
XDOT = 929
517751 Wp = 137
10538
YDOT = 4848
322501 meter/sec RA = 188
64354 deg
ZDOT = -5869
910806 TA = 30
52425
MA = 30
45551
Ha = 220
357 n
mi
Hp = 216
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21934910
58 X = 6678578
35
Y = 338709
58 feet Y = 177963
43 meter
Z = 3735781
38 Z = 1171125
88
XDOT = 3049
598920 XDOT = 903
746366
YDOT = 15906
569885 feet/sec YDOT = 4858
572439 meter/sec
ZDOT = -19258
237553 ZDOT = -5865
458512
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14536044
64 X = -4430586
41
Y = -16396586
76 feet Y = -4997679
64 meter
Z = 3881550
93 Z = 1183096
72
XDOT = 8396
825848 XDOT = 2559
352519
YDOT = -12018
864817 feet/sec YDOT = -3663
349996 meter/sec
ZDOT = -19238
676439 ZDOT = -5863
948579
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 18278
36607507
00016717 00000-0 10270-3 0 9108
2 25544 51
6375 189
6611 0003736 249
4186 110
6566 15
53786332 15648
Satellite: ISS
Catalog Number: 25544
Epoch time: 18278
36607507 = yrday
fracday
Element set: 910
Inclination: 51
6375 deg
RA of node: 189
6611 deg
Eccentricity:
0003736
Arg of perigee: 249
4186 deg
Mean anomaly: 110
6566 deg
Mean motion: 15
53786332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1564
Checksum: 330
Coasting Arc #12 (Orbit 1579)
---------------------------------------
Vector Time (GMT): 2018/279/07:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6724255
29 A = 6790184
27 meter
Y = -787586
41 meter E =
0009399
Z = 448532
73 I = 51
62848
XDOT = 953
319331 Wp = 41
50572
YDOT = -4691
067027 meter/sec RA = 183
67350 deg
ZDOT = 5989
671227 TA = 323
33112
MA = 323
39540
Ha = 220
302 n
mi
Hp = 216
504
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22061205
03 X = -6717127
26
Y = -2583944
91 feet Y = -862741
80 meter
Z = 1471564
09 Z = 415885
92
XDOT = 3127
688093 XDOT = 976
610526
YDOT = -15390
639851 feet/sec YDOT = -4680
275504 meter/sec
ZDOT = 19651
152321 ZDOT = 5994
359190
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13296313
80 X = 4052716
45
Y = 17804253
99 feet Y = 5426736
62 meter
Z = 1324997
51 Z = 403859
24
XDOT = -11937
877356 XDOT = -3638
665018
YDOT = 7433
589324 feet/sec YDOT = 2265
758026 meter/sec
ZDOT = 19672
624381 ZDOT = 5996
215911
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 18279
39513731
00016717 00000-0 10270-3 0 9118
2 25544 51
6382 184
5342 0003769 250
9917 109
0828 15
53810979 15802
Satellite: ISS
Catalog Number: 25544
Epoch time: 18279
39513731 = yrday
fracday
Element set: 911
Inclination: 51
6382 deg
RA of node: 184
5342 deg
Eccentricity:
0003769
Arg of perigee: 250
9917 deg
Mean anomaly: 109
0828 deg
Mean motion: 15
53810979 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1580
Checksum: 334
Coasting Arc #13 (Orbit 1594)
---------------------------------------
Vector Time (GMT): 2018/280/07:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6312660
05 A = 6788652
94 meter
Y = 1453998
42 meter E =
0006015
Z = -2018260
17 I = 51
65657
XDOT = -2805
318009 Wp = 173
64160
YDOT = 4465
977052 meter/sec RA = 178
70393 deg
ZDOT = -5564
439427 TA = 28
64626
MA = 28
61323
Ha = 220
287 n
mi
Hp = 216
578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20710826
92 X = 6305735
58
Y = 4770336
02 feet Y = 1524552
01 meter
Z = -6621588
48 Z = -1987612
23
XDOT = -9203
799241 XDOT = -2828
020003
YDOT = 14652
155683 feet/sec YDOT = 4434
478448 meter/sec
ZDOT = -18256
034866 ZDOT = -5578
122449
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11118085
94 X = -3388792
59
Y = -18162742
95 feet Y = -5536004
05 meter
Z = -6484043
89 Z = -1976336
58
XDOT = 15496
625991 XDOT = 4723
371602
YDOT = -2955
509624 feet/sec YDOT = -900
839333 meter/sec
ZDOT = -18317
892824 ZDOT = -5583
293733
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 18280
35988194
00016717 00000-0 10270-3 0 9126
2 25544 51
6386 179
7274 0003724 258
6093 101
4641 15
53791030 15958
Satellite: ISS
Catalog Number: 25544
Epoch time: 18280
35988194 = yrday
fracday
Element set: 912
Inclination: 51
6386 deg
RA of node: 179
7274 deg
Eccentricity:
0003724
Arg of perigee: 258
6093 deg
Mean anomaly: 101
4641 deg
Mean motion: 15
53791030 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1595
Checksum: 328
Coasting Arc #14 (Orbit 1598)
---------------------------------------
Vector Time (GMT): 2018/280/14:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6395649
87 A = 6789182
58 meter
Y = 1587351
35 meter E =
0005630
Z = -1619537
57 I = 51
66899
XDOT = -2543
951519 Wp = 9
68298
YDOT = -4413
217747 meter/sec RA = 177
26583 deg
ZDOT = 5729
021970 TA = 332
60397
MA = 332
63365
Ha = 220
131 n
mi
Hp = 216
626
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20983103
25 X = -6405057
81
Y = 5207845
64 feet Y = 1515777
95 meter
Z = -5313443
47 Z = -1650628
71
XDOT = -8346
297635 XDOT = -2522
241421
YDOT = -14479
060849 feet/sec YDOT = -4441
543900 meter/sec
ZDOT = 18796
003840 ZDOT = 5716
717497
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7283468
86 X = 2220001
31
Y = -20318909
94 feet Y = -6193203
75 meter
Z = -5453250
39 Z = -1662150
72
XDOT = 15263
593542 XDOT = 4652
343312
YDOT = 448
690095 feet/sec YDOT = 136
760741 meter/sec
ZDOT = 18741
117697 ZDOT = 5712
292674
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 18280
61714518
00016717 00000-0 10270-3 0 9133
2 25544 51
6398 178
4466 0003931 261
4721 98
5986 15
53775130 15995
Satellite: ISS
Catalog Number: 25544
Epoch time: 18280
61714518 = yrday
fracday
Element set: 913
Inclination: 51
6398 deg
RA of node: 178
4466 deg
Eccentricity:
0003931
Arg of perigee: 261
4721 deg
Mean anomaly: 98
5986 deg
Mean motion: 15
53775130 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1599
Checksum: 342
Coasting Arc #15 (Orbit 1614)
---------------------------------------
Vector Time (GMT): 2018/281/14:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6720451
53 A = 6790365
93 meter
Y = -927687
63 meter E =
0010221
Z = 24027
00 I = 51
70627
XDOT = 674
552808 Wp = 152
02247
YDOT = 4704
149069 meter/sec RA = 172
30081 deg
ZDOT = -6018
572195 TA = 27
71898
MA = 27
66454
Ha = 220
151 n
mi
Hp = 216
663
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22048725
50 X = 6730209
00
Y = -3043594
59 feet Y = -852480
31 meter
Z = 78828
75 Z = 56696
87
XDOT = 2213
099763 XDOT = 651
135010
YDOT = 15433
559939 feet/sec YDOT = 4711
560708 meter/sec
ZDOT = -19745
971767 ZDOT = -6015
352867
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9348309
92 X = -2849364
86
Y = 20198369
90 feet Y = 6156463
15 meter
Z = 225683
55 Z = 68788
34
XDOT = -12780
442848 XDOT = -3895
478980
YDOT = -5681
467943 feet/sec YDOT = -1731
711429 meter/sec
ZDOT = -19731
922350 ZDOT = -6014
289932
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 18281
64620176
00016717 00000-0 10270-3 0 9144
2 25544 51
6403 173
3200 0003993 262
7254 97
3444 15
53771473 16156
Satellite: ISS
Catalog Number: 25544
Epoch time: 18281
64620176 = yrday
fracday
Element set: 914
Inclination: 51
6403 deg
RA of node: 173
3200 deg
Eccentricity:
0003993
Arg of perigee: 262
7254 deg
Mean anomaly: 97
3444 deg
Mean motion: 15
53771473 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1615
Checksum: 304
Coasting Arc #16 (Orbit 1630)
---------------------------------------
Vector Time (GMT): 2018/282/14:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6598442
90 A = 6789239
66 meter
Y = 223173
26 meter E =
0010355
Z = 1557943
36 I = 51
73472
XDOT = 1197
475527 Wp = 52
90283
YDOT = -4922
990278 meter/sec RA = 167
33597 deg
ZDOT = 5756
690756 TA = 324
10548
MA = 324
17501
Ha = 220
018 n
mi
Hp = 216
665
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21648434
72 X = -6608015
88
Y = 732195
74 feet Y = 149331
55 meter
Z = 5111362
74 Z = 1525866
57
XDOT = 3928
725482 XDOT = 1224
473304
YDOT = -16151
542908 feet/sec YDOT = -4909
447655 meter/sec
ZDOT = 18886
780696 ZDOT = 5762
573924
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10773270
38 X = 3283692
81
Y = -18830300
89 feet Y = -5739475
71 meter
Z = 4967220
45 Z = 1514008
79
XDOT = 10367
202591 XDOT = 3159
923350
YDOT = 10938
572291 feet/sec YDOT = 3334
076834 meter/sec
ZDOT = 18913
650205 ZDOT = 5764
880582
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 18282
67525186
00016717 00000-0 10270-3 0 9154
2 25544 51
6394 168
1913 0004056 267
2401 92
8287 15
53826011 16315
Satellite: ISS
Catalog Number: 25544
Epoch time: 18282
67525186 = yrday
fracday
Element set: 915
Inclination: 51
6394 deg
RA of node: 168
1913 deg
Eccentricity:
0004056
Arg of perigee: 267
2401 deg
Mean anomaly: 92
8287 deg
Mean motion: 15
53826011 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1631
Checksum: 313
Coasting Arc #17 (Orbit 1645)
---------------------------------------
Vector Time (GMT): 2018/283/14:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6050724
70 A = 6786518
27 meter
Y = 572865
14 meter E =
0001549
Z = -3017788
91 I = 51
75549
XDOT = -2951
162622 Wp = 170
92047
YDOT = 5041
539086 meter/sec RA = 162
36970 deg
ZDOT = -4961
944640 TA = 43
56909
MA = 43
55685
Ha = 220
094 n
mi
Hp = 216
709
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19851458
99 X = 6058528
20
Y = 1879478
82 feet Y = 640571
88 meter
Z = -9900882
26 Z = -2988377
07
XDOT = -9682
292068 XDOT = -2983
216155
YDOT = 16540
482564 feet/sec YDOT = 5008
357420 meter/sec
ZDOT = -16279
345932 ZDOT = -4976
359022
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11790763
90 X = -3593824
84
Y = 16161352
89 feet Y = 4925980
36 meter
Z = -9768771
35 Z = -2977521
51
XDOT = -8147
920468 XDOT = -2483
486159
YDOT = -15820
260793 feet/sec YDOT = -4822
015490 meter/sec
ZDOT = -16344
569369 ZDOT = -4981
824744
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 18283
63998630
00016717 00000-0 10270-3 0 9160
2 25544 51
6375 163
3846 0003963 272
2646 87
8052 15
53802710 16469
Satellite: ISS
Catalog Number: 25544
Epoch time: 18283
63998630 = yrday
fracday
Element set: 916
Inclination: 51
6375 deg
RA of node: 163
3846 deg
Eccentricity:
0003963
Arg of perigee: 272
2646 deg
Mean anomaly: 87
8052 deg
Mean motion: 15
53802710 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1646
Checksum: 333
Coasting Arc #18 (Orbit 1647)
---------------------------------------
Vector Time (GMT): 2018/283/18:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 928631
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 671262
50 A = 6778372
33 meter
Y = 4182932
49 meter E =
0011093
Z = -5301012
80 I = 51
73327
XDOT = -7383
283097 Wp = 97
88885
YDOT = 1948
994631 meter/sec RA = 161
64404 deg
ZDOT = 602
571678 TA = 177
86383
MA = 177
85908
Ha = 220
152 n
mi
Hp = 216
521
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2202304
81 X = 650187
98
Y = 13723531
79 feet Y = 4190320
67 meter
Z = -17391774
27 Z = -5297803
56
XDOT = -24223
369740 XDOT = -7407
455592
YDOT = 6394
339342 feet/sec YDOT = 1866
294535 meter/sec
ZDOT = 1976
941200 ZDOT = 566
646583
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12142133
64 X = -3700922
33
Y = 6800175
92 feet Y = 2072693
62 meter
Z = -17377729
47 Z = -5296731
94
XDOT = -13680
887964 XDOT = -4169
934651
YDOT = -19785
610196 feet/sec YDOT = -6030
653988 meter/sec
ZDOT = 1815
333775 ZDOT = 553
313735
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 18283
76861904
00016717 00000-0 10270-3 0 9178
2 25544 51
6378 162
7410 0003688 264
8620 95
2104 15
53814239 16487
Satellite: ISS
Catalog Number: 25544
Epoch time: 18283
76861904 = yrday
fracday
Element set: 917
Inclination: 51
6378 deg
RA of node: 162
7410 deg
Eccentricity:
0003688
Arg of perigee: 264
8620 deg
Mean anomaly: 95
2104 deg
Mean motion: 15
53814239 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1648
Checksum: 329
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