[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 6th 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 482 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
069/22:27:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
1
000/00:00:00
000 0
0 0
0 214
5
072/21:25:56
618 -0
5 0
7 0
7
N/A 0
4 -0
1 220
9
000/00:01:53
236 0
2 0
0 215
1
073/06:47:30
000 0
0 0
0 0
0
N/A 0
0 0
0 220
9
000/00:00:00
000 0
0 0
0 215
1
077/07:56:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 215
3
Coasting Arc #1 (Orbit 2238)
---------------------------------------
Vector Time (GMT): 2018/064/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 462443
88 A = 6777280
06 meter
Y = -4233062
00 meter E =
0003899
Z = 5269140
32 I = 51
65274
XDOT = 7631
818594 Wp = 109
46067
YDOT = -127
910913 meter/sec RA = 174
44239 deg
ZDOT = -773
367544 TA = 347
91952
MA = 347
92887
Ha = 221
429 n
mi
Hp = 214
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1517204
34 X = 484150
26
Y = -13887998
67 feet Y = -4227768
56 meter
Z = 17287205
79 Z = 5271439
98
XDOT = 25038
774915 XDOT = 7636
438301
YDOT = -419
655227 feet/sec YDOT = -42
540943 meter/sec
ZDOT = -2537
295091 ZDOT = -736
283882
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5555469
69 X = 1693307
16
Y = -12804074
40 feet Y = -3902681
88 meter
Z = 17297928
65 Z = 5272408
65
XDOT = 23064
665305 XDOT = 7030
109985
YDOT = 6806
482429 feet/sec YDOT = 2074
615844 meter/sec
ZDOT = -2371
958833 ZDOT = -722
973052
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 18064
54701166
00016717 00000-0 10270-3 0 9006
2 25544 51
6410 175
3858 0002848 160
8601 199
2659 15
54209707 22397
Satellite: ISS
Catalog Number: 25544
Epoch time: 18064
54701166 = yrday
fracday
Element set: 900
Inclination: 51
6410 deg
RA of node: 175
3858 deg
Eccentricity:
0002848
Arg of perigee: 160
8601 deg
Mean anomaly: 199
2659 deg
Mean motion: 15
54209707 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2239
Checksum: 317
Coasting Arc #2 (Orbit 2253)
---------------------------------------
Vector Time (GMT): 2018/065/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2251023
88 A = 6779363
21 meter
Y = 4261101
57 meter E =
0013235
Z = -4780922
81 I = 51
69203
XDOT = -7140
351201 Wp = 119
34232
YDOT = -798
753766 meter/sec RA = 169
44815 deg
ZDOT = 2649
218816 TA = 176
82185
MA = 176
81343
Ha = 221
402 n
mi
Hp = 214
114
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7385248
96 X = -2275282
31
Y = 13979992
01 feet Y = 4235792
88 meter
Z = -15685442
29 Z = -4791916
85
XDOT = -23426
349086 XDOT = -7143
757068
YDOT = -2620
583221 feet/sec YDOT = -878
620817 meter/sec
ZDOT = 8691
662781 ZDOT = 2614
525503
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10991414
27 X = -3350183
07
Y = 11296715
22 feet Y = 3443238
80 meter
Z = -15734936
17 Z = -4796008
54
XDOT = -20916
092118 XDOT = -6375
224878
YDOT = -8456
092824 feet/sec YDOT = -2577
417093 meter/sec
ZDOT = 8537
069791 ZDOT = 2602
098872
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 18065
51150713
00016717 00000-0 10270-3 0 9011
2 25544 51
6406 170
5790 0002929 163
8903 196
2344 15
54210246 22547
Satellite: ISS
Catalog Number: 25544
Epoch time: 18065
51150713 = yrday
fracday
Element set: 901
Inclination: 51
6406 deg
RA of node: 170
5790 deg
Eccentricity:
0002929
Arg of perigee: 163
8903 deg
Mean anomaly: 196
2344 deg
Mean motion: 15
54210246 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2254
Checksum: 292
Coasting Arc #3 (Orbit 2269)
---------------------------------------
Vector Time (GMT): 2018/066/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3824416
48 A = 6783088
44 meter
Y = -4141758
52 meter E =
0012186
Z = 3760490
31 I = 51
73642
XDOT = 6128
609033 Wp = 97
28162
YDOT = 1782
700943 meter/sec RA = 164
46274 deg
ZDOT = -4259
041661 TA = 37
74646
MA = 37
66104
Ha = 221
341 n
mi
Hp = 214
261
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12547298
15 X = 3852180
13
Y = -13588446
59 feet Y = -4098835
66 meter
Z = 12337566
63 Z = 3779135
73
XDOT = 20106
985017 XDOT = 6128
906962
YDOT = 5848
756375 feet/sec YDOT = 1851
236505 meter/sec
ZDOT = -13973
233795 ZDOT = -4229
270630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15679759
72 X = 4779190
76
Y = -9703385
31 feet Y = -2957591
84 meter
Z = 12421174
29 Z = 3785973
92
XDOT = 17152
416538 XDOT = 5228
056561
YDOT = 9956
433904 feet/sec YDOT = 3034
721054 meter/sec
ZDOT = -13840
683024 ZDOT = -4218
640186
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 18066
54029898
00016717 00000-0 10270-3 0 9025
2 25544 51
6407 165
4498 0002916 166
7306 193
3924 15
54181761 22700
Satellite: ISS
Catalog Number: 25544
Epoch time: 18066
54029898 = yrday
fracday
Element set: 902
Inclination: 51
6407 deg
RA of node: 165
4498 deg
Eccentricity:
0002916
Arg of perigee: 166
7306 deg
Mean anomaly: 193
3924 deg
Mean motion: 15
54181761 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2270
Checksum: 329
Coasting Arc #4 (Orbit 2284)
---------------------------------------
Vector Time (GMT): 2018/067/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5047828
39 A = 6786757
92 meter
Y = 3874110
43 meter E =
0004590
Z = -2361921
20 I = 51
78029
XDOT = -4665
737393 Wp = 74
49092
YDOT = -2793
851667 meter/sec RA = 159
49040 deg
ZDOT = 5398
827636 TA = 259
21779
MA = 259
26946
Ha = 221
254 n
mi
Hp = 214
381
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16561116
76 X = -5079301
68
Y = 12710336
06 feet Y = 3817485
96 meter
Z = -7749085
31 Z = -2386518
41
XDOT = -15307
537380 XDOT = -4660
373509
YDOT = -9166
180010 feet/sec YDOT = -2845
996692 meter/sec
ZDOT = 17712
689093 ZDOT = 5376
176521
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19198489
56 X = -5851699
62
Y = 8094579
80 feet Y = 2467227
92 meter
Z = -7859219
46 Z = -2395490
09
XDOT = -11996
894535 XDOT = -3656
653454
YDOT = -11385
175261 feet/sec YDOT = -3470
201420 meter/sec
ZDOT = 17611
990441 ZDOT = 5368
134686
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 18067
50478587
00016717 00000-0 10270-3 0 9036
2 25544 51
6409 160
6416 0002604 172
2324 187
8869 15
54174787 22857
Satellite: ISS
Catalog Number: 25544
Epoch time: 18067
50478587 = yrday
fracday
Element set: 903
Inclination: 51
6409 deg
RA of node: 160
6416 deg
Eccentricity:
0002604
Arg of perigee: 172
2324 deg
Mean anomaly: 187
8869 deg
Mean motion: 15
54174787 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2285
Checksum: 337
Coasting Arc #5 (Orbit 2300)
---------------------------------------
Vector Time (GMT): 2018/068/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5842938
07 A = 6788929
93 meter
Y = -3373260
08 meter E =
0015301
Z = 677259
98 I = 51
81701
XDOT = 2909
218074 Wp = 135
31621
YDOT = 3824
074552 meter/sec RA = 154
52914 deg
ZDOT = -5980
741286 TA = 37
38357
MA = 37
27721
Ha = 221
262 n
mi
Hp = 214
374
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19169744
34 X = 5876934
78
Y = -11067126
25 feet Y = -3307730
19 meter
Z = 2221981
56 Z = 705725
55
XDOT = 9544
678722 XDOT = 2895
291069
YDOT = 12546
176352 feet/sec YDOT = 3856
529086 meter/sec
ZDOT = -19621
854614 ZDOT = -5966
643559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21235455
88 X = 6472566
95
Y = -6199487
60 feet Y = -1889603
82 meter
Z = 2349329
82 Z = 716075
73
XDOT = 5964
689608 XDOT = 1818
037392
YDOT = 12935
239313 feet/sec YDOT = 3942
660943 meter/sec
ZDOT = -19559
413390 ZDOT = -5961
709201
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 18068
53357098
00016717 00000-0 10270-3 0 9044
2 25544 51
6399 155
5131 0002782 173
7238 186
3950 15
54192430 23018
Satellite: ISS
Catalog Number: 25544
Epoch time: 18068
53357098 = yrday
fracday
Element set: 904
Inclination: 51
6399 deg
RA of node: 155
5131 deg
Eccentricity:
0002782
Arg of perigee: 173
7238 deg
Mean anomaly: 186
3950 deg
Mean motion: 15
54192430 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2301
Checksum: 316
Coasting Arc #6 (Orbit 2316)
---------------------------------------
Vector Time (GMT): 2018/069/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6152492
24 A = 6788702
20 meter
Y = 2659060
68 meter E =
0012370
Z = 1047792
12 I = 51
84598
XDOT = -1046
673427 Wp = 66
70927
YDOT = -4770
913445 meter/sec RA = 149
57177 deg
ZDOT = 5911
078914 TA = 304
61818
MA = 304
73477
Ha = 221
163 n
mi
Hp = 214
516
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20185341
98 X = -6186858
88
Y = 8723952
37 feet Y = 2590067
21 meter
Z = 3437638
18 Z = 1017822
08
XDOT = -3433
967937 XDOT = -1021
958601
YDOT = -15652
603165 feet/sec YDOT = -4782
479425 meter/sec
ZDOT = 19393
303523 ZDOT = 5906
054982
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21635272
84 X = -6594431
16
Y = 4046437
07 feet Y = 1233354
02 meter
Z = 3303641
68 Z = 1006949
98
XDOT = 277
296478 XDOT = 84
519967
YDOT = -14473
599350 feet/sec YDOT = -4411
553082 meter/sec
ZDOT = 19371
443192 ZDOT = 5904
415885
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 18069
56235228
00016717 00000-0 10270-3 0 9059
2 25544 51
6404 150
3839 0002628 178
1178 181
9985 15
54196990 23175
Satellite: ISS
Catalog Number: 25544
Epoch time: 18069
56235228 = yrday
fracday
Element set: 905
Inclination: 51
6404 deg
RA of node: 150
3839 deg
Eccentricity:
0002628
Arg of perigee: 178
1178 deg
Mean anomaly: 181
9985 deg
Mean motion: 15
54196990 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2317
Checksum: 338
Coasting Arc #7 (Orbit 2322)
---------------------------------------
Vector Time (GMT): 2018/069/22:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 41067
95 A = 6778616
77 meter
Y = 4617572
78 meter E =
0013384
Z = -4974814
06 I = 51
82445
XDOT = -6936
277761 Wp = 115
09963
YDOT = 2407
621885 meter/sec RA = 147
38002 deg
ZDOT = 2176
518079 TA = 176
10030
MA = 176
08986
Ha = 221
068 n
mi
Hp = 214
462
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 134737
37 X = 13594
70
Y = 15149516
99 feet Y = 4617878
03 meter
Z = -16321568
43 Z = -4974681
65
XDOT = -22756
816802 XDOT = -6973
257188
YDOT = 7899
021931 feet/sec YDOT = 2329
849062 meter/sec
ZDOT = 7140
807345 ZDOT = 2142
734424
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8589028
20 X = 2617935
80
Y = -12480242
17 feet Y = -3803977
81 meter
Z = -16321512
34 Z = -4974796
96
XDOT = 22247
437453 XDOT = 6781
018936
YDOT = 6165
622031 feet/sec YDOT = 1879
281595 meter/sec
ZDOT = 6989
818813 ZDOT = 2130
496774
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 18069
94814526
00016717 00000-0 10270-3 0 9066
2 25544 51
6400 148
4623 0002213 177
1132 183
0033 15
54212630 23233
Satellite: ISS
Catalog Number: 25544
Epoch time: 18069
94814526 = yrday
fracday
Element set: 906
Inclination: 51
6400 deg
RA of node: 148
4623 deg
Eccentricity:
0002213
Arg of perigee: 177
1132 deg
Mean anomaly: 183
0033 deg
Mean motion: 15
54212630 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2323
Checksum: 273
Coasting Arc #8 (Orbit 2338)
---------------------------------------
Vector Time (GMT): 2018/070/22:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1507230
87 A = 6782015
64 meter
Y = -5199781
79 meter E =
0010375
Z = 4076016
13 I = 51
86302
XDOT = 6512
518306 Wp = 89
40452
YDOT = -1164
707833 meter/sec RA = 142
40199 deg
ZDOT = -3885
396348 TA = 40
71377
MA = 40
63627
Ha = 221
049 n
mi
Hp = 214
488
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4944983
19 X = 1545465
35
Y = -17059651
54 feet Y = -5182712
78 meter
Z = 13372756
33 Z = 4083430
92
XDOT = 21366
529874 XDOT = 6543
931326
YDOT = -3821
219923 feet/sec YDOT = -1091
705051 meter/sec
ZDOT = -12747
363346 ZDOT = -3853
684819
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13658143
87 X = -4163002
25
Y = 11315367
19 feet Y = 3448923
92 meter
Z = 13406444
44 Z = 4086284
26
XDOT = -19022
566675 XDOT = -5798
078323
YDOT = -7992
344890 feet/sec YDOT = -2436
066722 meter/sec
ZDOT = -12605
744095 ZDOT = -3842
230800
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 18070
97692217
00016717 00000-0 10270-3 0 9073
2 25544 51
6401 143
3340 0002192 178
6696 181
4463 15
54205275 23394
Satellite: ISS
Catalog Number: 25544
Epoch time: 18070
97692217 = yrday
fracday
Element set: 907
Inclination: 51
6401 deg
RA of node: 143
3340 deg
Eccentricity:
0002192
Arg of perigee: 178
6696 deg
Mean anomaly: 181
4463 deg
Mean motion: 15
54205275 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2339
Checksum: 311
Coasting Arc #9 (Orbit 2353)
---------------------------------------
Vector Time (GMT): 2018/071/22:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 904792
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2814250
23 A = 6785761
76 meter
Y = 5524316
30 meter E =
0003947
Z = -2761409
73 I = 51
90163
XDOT = -5654
383967 Wp = 86
58491
YDOT = -303
062207 meter/sec RA = 137
43511 deg
ZDOT = 5162
875487 TA = 242
28279
MA = 242
32283
Ha = 220
947 n
mi
Hp = 214
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9233104
44 X = -2862402
20
Y = 18124397
31 feet Y = 5492575
93 meter
Z = -9059743
20 Z = -2775197
63
XDOT = -18551
128502 XDOT = -5675
652963
YDOT = -994
298580 feet/sec YDOT = -366
411871 meter/sec
ZDOT = 16938
567872 ZDOT = 5135
357225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17649278
02 X = 5379499
94
Y = -10055674
98 feet Y = -3064969
74 meter
Z = -9121914
72 Z = -2780359
61
XDOT = 14284
600317 XDOT = 4353
946177
YDOT = 9836
841994 feet/sec YDOT = 2998
269440 meter/sec
ZDOT = 16815
814642 ZDOT = 5125
460303
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 18071
94139804
00016717 00000-0 10270-3 0 9080
2 25544 51
6405 138
5254 0002177 183
7524 176
3613 15
54227463 23548
Satellite: ISS
Catalog Number: 25544
Epoch time: 18071
94139804 = yrday
fracday
Element set: 908
Inclination: 51
6405 deg
RA of node: 138
5254 deg
Eccentricity:
0002177
Arg of perigee: 183
7524 deg
Mean anomaly: 176
3613 deg
Mean motion: 15
54227463 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2354
Checksum: 312
Coasting Arc #10 (Orbit 2368)
---------------------------------------
Vector Time (GMT): 2018/072/21:26:53
236
Vector Time (MET): N/A
Weight (LBS) : 904716
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1118863
81 A = 6779129
19 meter
Y = 4509420
81 meter E =
0012140
Z = -4947847
64 I = 51
90049
XDOT = -6118
018887 Wp = 116
42654
YDOT = 4009
322652 meter/sec RA = 132
68125 deg
ZDOT = 2269
624519 TA = 175
70062
MA = 175
69018
Ha = 220
878 n
mi
Hp = 215
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3670813
04 X = 1092388
76
Y = 14794687
69 feet Y = 4521784
17 meter
Z = -16233095
92 Z = -4942477
44
XDOT = -20072
240443 XDOT = -6173
421992
YDOT = 13153
945710 feet/sec YDOT = 3940
597215 meter/sec
ZDOT = 7446
274667 ZDOT = 2239
770788
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8397100
06 X = 2559436
10
Y = -12751727
14 feet Y = -3886726
43 meter
Z = -16209664
43 Z = -4940705
72
XDOT = 22342
223717 XDOT = 6809
909789
YDOT = 5412
950409 feet/sec YDOT = 1649
867285 meter/sec
ZDOT = 7312
578012 ZDOT = 2228
873778
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 18072
90587236
00016717 00000-0 10270-3 0 9094
2 25544 51
6404 133
7165 0002095 205
3156 154
7894 15
54085050 23697
Satellite: ISS
Catalog Number: 25544
Epoch time: 18072
90587236 = yrday
fracday
Element set: 909
Inclination: 51
6404 deg
RA of node: 133
7165 deg
Eccentricity:
0002095
Arg of perigee: 205
3156 deg
Mean anomaly: 154
7894 deg
Mean motion: 15
54085050 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2369
Checksum: 315
Coasting Arc #11 (Orbit 2374)
---------------------------------------
Vector Time (GMT): 2018/073/06:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 904716
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -572474
60 A = 6782718
35 meter
Y = 5458897
25 meter E =
0007151
Z = -3992957
52 I = 51
92044
XDOT = -6114
668339 Wp = 128
67888
YDOT = 2289
154437 meter/sec RA = 130
73625 deg
ZDOT = 4006
722489 TA = 182
96028
MA = 182
96451
Ha = 220
941 n
mi
Hp = 215
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1878197
52 X = -614079
54
Y = 17909767
90 feet Y = 5452262
39 meter
Z = -13100254
33 Z = -3995840
00
XDOT = -20061
247832 XDOT = -6159
274083
YDOT = 7510
349202 feet/sec YDOT = 2220
527042 meter/sec
ZDOT = 13145
414989 ZDOT = 3976
911423
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17975614
24 X = -5478967
22
Y = -900297
30 feet Y = -274410
62 meter
Z = -13113765
01 Z = -3997075
58
XDOT = -8568
076697 XDOT = -2611
549777
YDOT = -18439
002066 feet/sec YDOT = -5620
207830 meter/sec
ZDOT = 13012
106572 ZDOT = 3966
090083
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 18073
29169538
00016717 00000-0 10270-3 0 9100
2 25544 51
6398 131
7890 0002556 202
5449 157
5591 15
54075644 23758
Satellite: ISS
Catalog Number: 25544
Epoch time: 18073
29169538 = yrday
fracday
Element set: 910
Inclination: 51
6398 deg
RA of node: 131
7890 deg
Eccentricity:
0002556
Arg of perigee: 202
5449 deg
Mean anomaly: 157
5591 deg
Mean motion: 15
54075644 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2375
Checksum: 332
Coasting Arc #12 (Orbit 2390)
---------------------------------------
Vector Time (GMT): 2018/074/06:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 904716
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1748470
80 A = 6786466
71 meter
Y = -5985944
63 meter E =
0013273
Z = 2658877
34 I = 51
95348
XDOT = 5561
822627 Wp = 113
26451
YDOT = -708
431894 meter/sec RA = 125
77484 deg
ZDOT = -5236
776961 TA = 36
86541
MA = 36
77424
Ha = 220
932 n
mi
Hp = 215
089
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5736452
75 X = 1802362
07
Y = -19638925
94 feet Y = -5966090
37 meter
Z = 8723350
86 Z = 2667502
32
XDOT = 18247
449563 XDOT = 5594
768279
YDOT = -2324
251621 feet/sec YDOT = -646
052208 meter/sec
ZDOT = -17181
026774 ZDOT = -5209
679843
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19973818
51 X = 6088019
88
Y = 4353766
26 feet Y = 1327027
96 meter
Z = 8762559
32 Z = 2670828
08
XDOT = 3864
758546 XDOT = 1177
978405
YDOT = 16707
522951 feet/sec YDOT = 5092
452996 meter/sec
ZDOT = -17060
006918 ZDOT = -5199
890109
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 18074
32055633
00016717 00000-0 10270-3 0 9116
2 25544 51
6397 126
6603 0002563 203
7818 156
3217 15
54073021 23910
Satellite: ISS
Catalog Number: 25544
Epoch time: 18074
32055633 = yrday
fracday
Element set: 911
Inclination: 51
6397 deg
RA of node: 126
6603 deg
Eccentricity:
0002563
Arg of perigee: 203
7818 deg
Mean anomaly: 156
3217 deg
Mean motion: 15
54073021 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2391
Checksum: 290
Coasting Arc #13 (Orbit 2405)
---------------------------------------
Vector Time (GMT): 2018/075/06:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 904716
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2683102
36 A = 6788944
00 meter
Y = 6139452
65 meter E =
0007070
Z = -1076636
49 I = 51
98029
XDOT = -4760
836987 Wp = 41
98118
YDOT = -1047
985274 meter/sec RA = 120
82389 deg
ZDOT = 5915
968838 TA = 306
40067
MA = 306
46586
Ha = 220
827 n
mi
Hp = 215
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8802829
26 X = -2746326
30
Y = 20142561
17 feet Y = 6109094
69 meter
Z = -3532271
95 Z = -1089824
31
XDOT = -15619
543920 XDOT = -4777
500610
YDOT = -3438
271897 feet/sec YDOT = -1101
316592 meter/sec
ZDOT = 19409
346583 ZDOT = 5892
802299
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20808384
93 X = -6342395
73
Y = -7056846
52 feet Y = -2150926
82 meter
Z = -3591873
12 Z = -1094802
93
XDOT = 1587
647281 XDOT = 483
914891
YDOT = -14462
951304 feet/sec YDOT = -4408
307558 meter/sec
ZDOT = 19306
073436 ZDOT = 5884
491183
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 18075
28511135
00016717 00000-0 10270-3 0 9127
2 25544 51
6397 121
8528 0002460 208
2961 151
8059 15
54084620 24066
Satellite: ISS
Catalog Number: 25544
Epoch time: 18075
28511135 = yrday
fracday
Element set: 912
Inclination: 51
6397 deg
RA of node: 121
8528 deg
Eccentricity:
0002460
Arg of perigee: 208
2961 deg
Mean anomaly: 151
8059 deg
Mean motion: 15
54084620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2406
Checksum: 297
Coasting Arc #14 (Orbit 2421)
---------------------------------------
Vector Time (GMT): 2018/076/06:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 904716
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3393056
12 A = 6789242
46 meter
Y = -5837419
07 meter E =
0011693
Z = -646389
07 I = 51
99735
XDOT = 3815
224541 Wp = 151
39335
YDOT = 2875
933612 meter/sec RA = 115
87781 deg
ZDOT = -5999
629766 TA = 35
55300
MA = 35
47514
Ha = 220
771 n
mi
Hp = 215
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11132073
90 X = 3461219
34
Y = -19151637
36 feet Y = -5799094
55 meter
Z = -2120699
05 Z = -629740
53
XDOT = 12517
140881 XDOT = 3811
924305
YDOT = 9435
477730 feet/sec YDOT = 2918
578761 meter/sec
ZDOT = -19683
824691 ZDOT = -5981
105322
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20180545
85 X = 6151030
38
Y = 9152399
86 feet Y = 2789651
48 meter
Z = -2045676
72 Z = -623522
26
XDOT = -7439
573220 XDOT = -2267
581918
YDOT = 12064
233903 feet/sec YDOT = 3677
178494 meter/sec
ZDOT = -19601
490918 ZDOT = -5974
534432
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 18076
31396810
00016717 00000-0 10270-3 0 9134
2 25544 51
6397 116
7241 0002507 212
9448 147
1549 15
54101742 24220
Satellite: ISS
Catalog Number: 25544
Epoch time: 18076
31396810 = yrday
fracday
Element set: 913
Inclination: 51
6397 deg
RA of node: 116
7241 deg
Eccentricity:
0002507
Arg of perigee: 212
9448 deg
Mean anomaly: 147
1549 deg
Mean motion: 15
54101742 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2422
Checksum: 298
Coasting Arc #15 (Orbit 2437)
---------------------------------------
Vector Time (GMT): 2018/077/06:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 904716
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3852362
77 A = 6787232
87 meter
Y = 5097393
63 meter E =
0012041
Z = 2275160
57 I = 52
00486
XDOT = -2819
664257 Wp = 78
69027
YDOT = -4580
621943 meter/sec RA = 110
93007 deg
ZDOT = 5466
232662 TA = 306
50261
MA = 306
61346
Ha = 220
716 n
mi
Hp = 215
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12638985
48 X = -3920128
38
Y = 16723732
39 feet Y = 5053935
29 meter
Z = 7464437
57 Z = 2256281
89
XDOT = -9250
866984 XDOT = -2794
784895
YDOT = -15028
287214 feet/sec YDOT = -4612
013466 meter/sec
ZDOT = 17933
834194 ZDOT = 5452
596867
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18106805
26 X = -5518954
24
Y = -10622193
96 feet Y = -3237644
72 meter
Z = 7379539
69 Z = 2249283
70
XDOT = 13039
533589 XDOT = 3974
449838
YDOT = -9759
221659 feet/sec YDOT = -2974
610762 meter/sec
ZDOT = 17873
534285 ZDOT = 5447
853250
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 18077
34282168
00016717 00000-0 10270-3 0 9149
2 25544 51
6405 111
5953 0002375 215
2685 144
8311 15
54112822 24384
Satellite: ISS
Catalog Number: 25544
Epoch time: 18077
34282168 = yrday
fracday
Element set: 914
Inclination: 51
6405 deg
RA of node: 111
5953 deg
Eccentricity:
0002375
Arg of perigee: 215
2685 deg
Mean anomaly: 144
8311 deg
Mean motion: 15
54112822 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2438
Checksum: 297
Coasting Arc #16 (Orbit 2437)
---------------------------------------
Vector Time (GMT): 2018/077/07:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904716
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2755512
09 A = 6778963
99 meter
Y = 3709064
84 meter E =
0011705
Z = -4971070
04 I = 51
97809
XDOT = -4137
118898 Wp = 116
84893
YDOT = 6051
122916 meter/sec RA = 110
65869 deg
ZDOT = 2220
558786 TA = 174
75116
MA = 174
73888
Ha = 220
626 n
mi
Hp = 215
271
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9040394
01 X = 2737978
27
Y = 12168847
92 feet Y = 3739780
12 meter
Z = -16309284
92 Z = -4957727
90
XDOT = -13573
224732 XDOT = -4215
262980
YDOT = 19852
765473 feet/sec YDOT = 6004
422198 meter/sec
ZDOT = 7285
297855 ZDOT = 2200
271512
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7404106
69 X = -2256771
72
Y = 13300862
21 feet Y = 4054102
80 meter
Z = -16250188
51 Z = -4953057
46
XDOT = -22704
130864 XDOT = -6920
219087
YDOT = -3844
868301 feet/sec YDOT = -1171
915858 meter/sec
ZDOT = 7193
993956 ZDOT = 2192
729358
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 18077
34282150
00016717 00000-0 10270-3 0 9151
2 25544 51
6406 111
5969 0002324 218
0409 142
0579 15
54123482 24381
Satellite: ISS
Catalog Number: 25544
Epoch time: 18077
34282150 = yrday
fracday
Element set: 915
Inclination: 51
6406 deg
RA of node: 111
5969 deg
Eccentricity:
0002324
Arg of perigee: 218
0409 deg
Mean anomaly: 142
0579 deg
Mean motion: 15
54123482 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2438
Checksum: 296
Coasting Arc #17 (Orbit 2453)
---------------------------------------
Vector Time (GMT): 2018/078/07:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904716
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1893714
46 A = 6782347
02 meter
Y = -5065026
20 meter E =
0008867
Z = 4086699
71 I = 51
99945
XDOT = 4513
566042 Wp = 85
85536
YDOT = -4831
866514 meter/sec RA = 105
69056 deg
ZDOT = -3889
199579 TA = 44
22533
MA = 44
15450
Ha = 220
673 n
mi
Hp = 215
254
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6212973
93 X = -1856786
25
Y = -16617540
03 feet Y = -5085995
97 meter
Z = 13407807
44 Z = 4077591
10
XDOT = 14808
287541 XDOT = 4586
153513
YDOT = -15852
580425 feet/sec YDOT = -4780
987393 meter/sec
ZDOT = -12759
841138 ZDOT = -3867
097269
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12408630
02 X = 3782150
43
Y = -12721682
52 feet Y = -3877568
83 meter
Z = 13367785
05 Z = 4074500
88
XDOT = 19727
809452 XDOT = 6013
036321
YDOT = 5911
589870 feet/sec YDOT = 1801
852592 meter/sec
ZDOT = -12660
573608 ZDOT = -3858
942836
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 18078
37167413
00016717 00000-0 10270-3 0 9160
2 25544 51
6401 106
4681 0002262 222
5964 137
5014 15
54106373 24548
Satellite: ISS
Catalog Number: 25544
Epoch time: 18078
37167413 = yrday
fracday
Element set: 916
Inclination: 51
6401 deg
RA of node: 106
4681 deg
Eccentricity:
0002262
Arg of perigee: 222
5964 deg
Mean anomaly: 137
5014 deg
Mean motion: 15
54106373 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2454
Checksum: 292
Coasting Arc #18 (Orbit 2468)
---------------------------------------
Vector Time (GMT): 2018/079/07:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 904716
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1071847
48 A = 6786135
20 meter
Y = 6087807
58 meter E =
0002423
Z = -2801024
48 I = 52
01947
XDOT = -4695
272825 Wp = 69
71601
YDOT = 3192
823810 meter/sec RA = 100
73324 deg
ZDOT = 5147
059859 TA = 258
70777
MA = 258
73501
Ha = 220
511 n
mi
Hp = 215
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3516559
99 X = 1017298
25
Y = 19973121
99 feet Y = 6099488
36 meter
Z = -9189712
87 Z = -2795951
07
XDOT = -15404
438403 XDOT = -4755
628680
YDOT = 10475
143734 feet/sec YDOT = 3139
981224 meter/sec
ZDOT = 16886
679327 ZDOT = 5124
104775
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16397272
20 X = -4997888
57
Y = 11950845
08 feet Y = 3642617
58 meter
Z = -9167845
18 Z = -2794359
21
XDOT = -15335
082278 XDOT = -4674
133078
YDOT = -8176
432025 feet/sec YDOT = -2492
176481 meter/sec
ZDOT = 16783
800898 ZDOT = 5115
702514
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 18079
33622127
00016717 00000-0 10270-3 0 9176
2 25544 51
6398 101
6602 0002377 229
8078 130
2867 15
54087804 24695
Satellite: ISS
Catalog Number: 25544
Epoch time: 18079
33622127 = yrday
fracday
Element set: 917
Inclination: 51
6398 deg
RA of node: 101
6602 deg
Eccentricity:
0002377
Arg of perigee: 229
8078 deg
Mean anomaly: 130
2867 deg
Mean motion: 15
54087804 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2469
Checksum: 325
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