[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 22nd 2018
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13813 3262 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 468 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
142/00:19:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
4
000/00:00:00
000 0
0 0
0 213
5
144/09:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
4
000/00:00:00
000 0
0 0
0 213
6
146/20:57:30
000 0
0 0
0 0
0
N/A 0
0 0
0 222
2
000/00:00:00
000 0
0 0
0 213
6
148/06:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
2
000/00:00:00
000 0
0 0
0 213
8
153/12:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
0
000/00:00:00
000 0
0 0
0 213
9
154/09:16:30
000 0
0 0
0 0
0
N/A 0
0 0
0 221
9
000/00:00:00
000 0
0 0
0 214
0
Coasting Arc #1 (Orbit 3435)
---------------------------------------
Vector Time (GMT): 2018/141/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1151755
45 A = 6777809
30 meter
Y = 4116354
13 meter E =
0018273
Z = -5275967
06 I = 51
80007
XDOT = -6942
107181 Wp = 98
97842
YDOT = 3096
944507 meter/sec RA = 150
60795 deg
ZDOT = 900
669254 TA = 179
63317
MA = 179
63183
Ha = 222
476 n
mi
Hp = 213
452
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3778725
24 X = 1131267
54
Y = 13505098
86 feet Y = 4129119
71 meter
Z = -17309603
23 Z = -5270421
67
XDOT = -22775
942196 XDOT = -6980
597091
YDOT = 10160
579090 feet/sec YDOT = 3019
097803 meter/sec
ZDOT = 2954
951621 ZDOT = 866
853626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13528659
49 X = 4123535
41
Y = 3805576
86 feet Y = 1159939
83 meter
Z = -17285305
34 Z = -5268561
07
XDOT = -3096
080786 XDOT = -943
685424
YDOT = 23741
445348 feet/sec YDOT = 7236
392542 meter/sec
ZDOT = 2803
393633 ZDOT = 854
474379
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 18141
51464103
00016717 00000-0 10270-3 0 9006
2 25544 51
6380 151
6812 0003822 106
0423 254
1151 15
54057724 34365
Satellite: ISS
Catalog Number: 25544
Epoch time: 18141
51464103 = yrday
fracday
Element set: 900
Inclination: 51
6380 deg
RA of node: 151
6812 deg
Eccentricity:
0003822
Arg of perigee: 106
0423 deg
Mean anomaly: 254
1151 deg
Mean motion: 15
54057724 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3436
Checksum: 265
Coasting Arc #2 (Orbit 3443)
---------------------------------------
Vector Time (GMT): 2018/142/00:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2051070
62 A = 6777504
98 meter
Y = 3666075
57 meter E =
0018511
Z = -5334557
27 I = 51
81170
XDOT = -6566
140961 Wp = 94
98388
YDOT = 3930
683448 meter/sec RA = 148
05955 deg
ZDOT = 175
648528 TA = 176
69520
MA = 176
68295
Ha = 222
417 n
mi
Hp = 213
472
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6729234
32 X = 2035835
62
Y = 12027806
98 feet Y = 3688927
23 meter
Z = -17501828
31 Z = -5324630
62
XDOT = -21542
457222 XDOT = -6610
460139
YDOT = 12895
943071 feet/sec YDOT = 3857
008522 meter/sec
ZDOT = 576
274699 ZDOT = 143
645072
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13817516
40 X = -4211579
00
Y = 750450
68 feet Y = 228737
37 meter
Z = -17457886
29 Z = -5321163
74
XDOT = -1856
140140 XDOT = -565
751515
YDOT = -24029
907994 feet/sec YDOT = -7324
315956 meter/sec
ZDOT = 432
708470 ZDOT = 131
889542
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 18142
02907435
00016717 00000-0 10270-3 0 9014
2 25544 51
6358 149
1139 0003790 108
6556 251
5008 15
54081431 34446
Satellite: ISS
Catalog Number: 25544
Epoch time: 18142
02907435 = yrday
fracday
Element set: 901
Inclination: 51
6358 deg
RA of node: 149
1139 deg
Eccentricity:
0003790
Arg of perigee: 108
6556 deg
Mean anomaly: 251
5008 deg
Mean motion: 15
54081431 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3444
Checksum: 294
Coasting Arc #3 (Orbit 3459)
---------------------------------------
Vector Time (GMT): 2018/143/00:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -501002
74 A = 6778918
51 meter
Y = -4539953
46 meter E =
0008658
Z = 5002427
32 I = 51
84416
XDOT = 6739
321934 Wp = 77
81478
YDOT = -3030
148322 meter/sec RA = 143
07389 deg
ZDOT = -2070
254236 TA = 32
27704
MA = 32
22409
Ha = 222
466 n
mi
Hp = 213
493
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1643709
78 X = -474497
74
Y = -14894860
43 feet Y = -4545408
07 meter
Z = 16412163
12 Z = 5000057
76
XDOT = 22110
636268 XDOT = 6782
761239
YDOT = -9941
431502 feet/sec YDOT = -2954
541592 meter/sec
ZDOT = -6792
172691 ZDOT = -2037
411484
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14192665
02 X = 4325924
30
Y = 4843196
62 feet Y = 1476206
33 meter
Z = 16402117
35 Z = 4999365
37
XDOT = -233
469124 XDOT = -71
161389
YDOT = 23241
513847 feet/sec YDOT = 7084
013421 meter/sec
ZDOT = -6644
944086 ZDOT = -2025
378957
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 18143
05793873
00016717 00000-0 10270-3 0 9028
2 25544 51
6362 143
9847 0003752 112
2132 247
9419 15
54055122 34609
Satellite: ISS
Catalog Number: 25544
Epoch time: 18143
05793873 = yrday
fracday
Element set: 902
Inclination: 51
6362 deg
RA of node: 143
9847 deg
Eccentricity:
0003752
Arg of perigee: 112
2132 deg
Mean anomaly: 247
9419 deg
Mean motion: 15
54055122 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3460
Checksum: 301
Coasting Arc #4 (Orbit 3474)
---------------------------------------
Vector Time (GMT): 2018/144/00:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 907607
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -943240
98 A = 6782013
10 meter
Y = 5260901
26 meter E =
0011806
Z = -4187271
19 I = 51
88039
XDOT = -6427
618823 Wp = 112
15050
YDOT = 1822
746238 meter/sec RA = 138
09636 deg
ZDOT = 3742
116783 TA = 196
23085
MA = 196
26870
Ha = 222
431 n
mi
Hp = 213
395
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3094622
63 X = -981660
02
Y = 17260174
72 feet Y = 5250138
65 meter
Z = -13737766
36 Z = -4191946
24
XDOT = -21087
988264 XDOT = -6465
700908
YDOT = 5980
138575 feet/sec YDOT = 1750
655083 meter/sec
ZDOT = 12277
286034 ZDOT = 3710
801010
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14447998
17 X = -4403749
84
Y = -9907224
45 feet Y = -3019722
01 meter
Z = -13759316
77 Z = -4193839
75
XDOT = 2638
767295 XDOT = 804
296272
YDOT = -20685
619570 feet/sec YDOT = -6304
976845 meter/sec
ZDOT = 12137
016577 ZDOT = 3699
362653
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 18144
02249693
00016717 00000-0 10270-3 0 9033
2 25544 51
6360 139
1761 0003958 115
9065 244
2496 15
54085438 34756
Satellite: ISS
Catalog Number: 25544
Epoch time: 18144
02249693 = yrday
fracday
Element set: 903
Inclination: 51
6360 deg
RA of node: 139
1761 deg
Eccentricity:
0003958
Arg of perigee: 115
9065 deg
Mean anomaly: 244
2496 deg
Mean motion: 15
54085438 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3475
Checksum: 323
Coasting Arc #5 (Orbit 3480)
---------------------------------------
Vector Time (GMT): 2018/144/09:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4285485
98 A = 6778721
84 meter
Y = 1409747
96 meter E =
0016119
Z = -5073720
84 I = 51
88150
XDOT = -4232
422612 Wp = 84
93036
YDOT = 6095
115070 meter/sec RA = 136
27347 deg
ZDOT = -1885
105532 TA = 166
85278
MA = 166
81072
Ha = 222
424 n
mi
Hp = 213
581
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14059993
36 X = 4294048
94
Y = 4625157
35 feet Y = 1457719
31 meter
Z = -16646065
75 Z = -5052882
40
XDOT = -13885
900958 XDOT = -4291
108370
YDOT = 19997
096687 feet/sec YDOT = 6047
457153 meter/sec
ZDOT = -6184
729437 ZDOT = -1905
807620
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14884982
25 X = 4536942
59
Y = -775249
92 feet Y = -236296
18 meter
Z = -16553044
73 Z = -5045368
03
XDOT = -5793
342012 XDOT = -1765
810645
YDOT = 22549
881414 feet/sec YDOT = 6873
203855 meter/sec
ZDOT = -6278
062120 ZDOT = -1913
553334
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 18144
40831964
00016717 00000-0 10270-3 0 9044
2 25544 51
6393 137
2562 0003857 115
7772 244
3779 15
54076022 34812
Satellite: ISS
Catalog Number: 25544
Epoch time: 18144
40831964 = yrday
fracday
Element set: 904
Inclination: 51
6393 deg
RA of node: 137
2562 deg
Eccentricity:
0003857
Arg of perigee: 115
7772 deg
Mean anomaly: 244
3779 deg
Mean motion: 15
54076022 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3481
Checksum: 320
Coasting Arc #6 (Orbit 3496)
---------------------------------------
Vector Time (GMT): 2018/145/09:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3132117
71 A = 6777443
70 meter
Y = -2767374
54 meter E =
0006183
Z = 5330209
05 I = 51
89933
XDOT = 5070
876162 Wp = 107
82569
YDOT = -5759
185227 meter/sec RA = 131
29202 deg
ZDOT = -12
197843 TA = 342
27928
MA = 342
30083
Ha = 222
527 n
mi
Hp = 213
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10275976
73 X = -3126831
03
Y = -9079312
80 feet Y = -2802370
74 meter
Z = 17487562
51 Z = 5315006
84
XDOT = 16636
732816 XDOT = 5134
959320
YDOT = -18894
964656 feet/sec YDOT = -5702
120885 meter/sec
ZDOT = -40
019169 ZDOT = 12
590376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13038546
32 X = -3974148
92
Y = -4515238
51 feet Y = -1376244
70 meter
Z = 17419913
68 Z = 5309589
69
XDOT = 8001
465976 XDOT = 2438
846830
YDOT = -22806
236580 feet/sec YDOT = -6951
340910 meter/sec
ZDOT = 71
565493 ZDOT = 21
813162
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 18145
43717947
00016717 00000-0 10270-3 0 9053
2 25544 51
6380 132
1274 0003934 117
6321 242
5232 15
54094048 34978
Satellite: ISS
Catalog Number: 25544
Epoch time: 18145
43717947 = yrday
fracday
Element set: 905
Inclination: 51
6380 deg
RA of node: 132
1274 deg
Eccentricity:
0003934
Arg of perigee: 117
6321 deg
Mean anomaly: 242
5232 deg
Mean motion: 15
54094048 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3497
Checksum: 305
Coasting Arc #7 (Orbit 3511)
---------------------------------------
Vector Time (GMT): 2018/146/09:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1921919
98 A = 6778688
43 meter
Y = 4089321
02 meter E =
0016621
Z = -5068250
41 I = 51
92595
XDOT = -5507
170937 Wp = 108
02690
YDOT = 4961
065848 meter/sec RA = 126
31192 deg
ZDOT = 1914
624880 TA = 180
49612
MA = 180
49777
Ha = 222
330 n
mi
Hp = 213
621
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6305511
75 X = 1900668
48
Y = 13416407
55 feet Y = 4110694
74 meter
Z = -16628118
13 Z = -5058965
61
XDOT = -18068
146118 XDOT = -5571
538000
YDOT = 16276
462756 feet/sec YDOT = 4899
120852 meter/sec
ZDOT = 6281
577691 ZDOT = 1887
716531
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11151381
68 X = 3398941
14
Y = 9837093
40 feet Y = 2998346
07 meter
Z = -16587105
31 Z = -5055749
70
XDOT = -9582
849185 XDOT = -2920
852432
YDOT = 21250
208987 feet/sec YDOT = 6477
063699 meter/sec
ZDOT = 6160
589545 ZDOT = 1877
747693
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 18146
40173279
00016717 00000-0 10270-3 0 9066
2 25544 51
6396 127
3193 0003708 120
9224 239
2293 15
54073344 35123
Satellite: ISS
Catalog Number: 25544
Epoch time: 18146
40173279 = yrday
fracday
Element set: 906
Inclination: 51
6396 deg
RA of node: 127
3193 deg
Eccentricity:
0003708
Arg of perigee: 120
9224 deg
Mean anomaly: 239
2293 deg
Mean motion: 15
54073344 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3512
Checksum: 303
Coasting Arc #8 (Orbit 3519)
---------------------------------------
Vector Time (GMT): 2018/146/20:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1084034
37 A = 6780382
97 meter
Y = -4850176
31 meter E =
0010704
Z = 4604111
61 I = 51
93983
XDOT = 5676
155913 Wp = 81
24520
YDOT = -4168
801813 meter/sec RA = 123
89993 deg
ZDOT = -3047
541147 TA = 39
08467
MA = 39
00738
Ha = 222
194 n
mi
Hp = 213
615
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3556543
22 X = -1052082
50
Y = -15912651
92 feet Y = -4862120
40 meter
Z = 15105353
06 Z = 4598922
93
XDOT = 18622
558771 XDOT = 5737
154306
YDOT = -13677
171304 feet/sec YDOT = -4104
985850 meter/sec
ZDOT = -9998
494578 ZDOT = -3019
820060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8364375
63 X = 2549461
69
Y = 14020722
73 feet Y = 4273516
29 meter
Z = 15082762
89 Z = 4597226
13
XDOT = -12564
675124 XDOT = -3829
712978
YDOT = 18144
544322 feet/sec YDOT = 5530
457109 meter/sec
ZDOT = -9873
961618 ZDOT = -3009
583501
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 18146
91615922
00016717 00000-0 10270-3 0 9079
2 25544 51
6380 124
7541 0003379 122
3683 237
7797 15
54116660 35203
Satellite: ISS
Catalog Number: 25544
Epoch time: 18146
91615922 = yrday
fracday
Element set: 907
Inclination: 51
6380 deg
RA of node: 124
7541 deg
Eccentricity:
0003379
Arg of perigee: 122
3683 deg
Mean anomaly: 237
7797 deg
Mean motion: 15
54116660 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3520
Checksum: 316
Coasting Arc #9 (Orbit 3534)
---------------------------------------
Vector Time (GMT): 2018/147/20:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -44635
69 A = 6784121
57 meter
Y = 5795954
95 meter E =
0008362
Z = -3534928
55 I = 51
96805
XDOT = -5548
587438 Wp = 108
37126
YDOT = 2715
528459 meter/sec RA = 118
93328 deg
ZDOT = 4528
710335 TA = 210
24916
MA = 210
29746
Ha = 222
179 n
mi
Hp = 213
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -146442
54 X = -92273
23
Y = 19015600
22 feet Y = 5795189
76 meter
Z = -11597534
60 Z = -3535260
55
XDOT = -18204
027026 XDOT = -5600
539278
YDOT = 8909
214105 feet/sec YDOT = 2653
189440 meter/sec
ZDOT = 14857
973541 ZDOT = 4501
630845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6081606
30 X = -1853673
60
Y = -18016009
48 feet Y = -5491279
69 meter
Z = -11599774
71 Z = -3535611
33
XDOT = 13124
490279 XDOT = 4000
344637
YDOT = -13905
512970 feet/sec YDOT = -4238
400353 meter/sec
ZDOT = 14736
478899 ZDOT = 4491
678768
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 18147
88071160
00016717 00000-0 10270-3 0 9087
2 25544 51
6364 119
9455 0003531 127
4148 232
7326 15
54098484 35359
Satellite: ISS
Catalog Number: 25544
Epoch time: 18147
88071160 = yrday
fracday
Element set: 908
Inclination: 51
6364 deg
RA of node: 119
9455 deg
Eccentricity:
0003531
Arg of perigee: 127
4148 deg
Mean anomaly: 232
7326 deg
Mean motion: 15
54098484 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3535
Checksum: 320
Coasting Arc #10 (Orbit 3540)
---------------------------------------
Vector Time (GMT): 2018/148/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3838682
64 A = 6777547
13 meter
Y = 1677305
58 meter E =
0017702
Z = -5342962
29 I = 51
95348
XDOT = -3325
102446 Wp = 96
43079
YDOT = 6891
889918 meter/sec RA = 117
09162 deg
ZDOT = -227
956371 TA = 171
41743
MA = 171
38711
Ha = 222
241 n
mi
Hp = 213
823
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12594103
15 X = 3845594
96
Y = 5502971
06 feet Y = 1720271
55 meter
Z = -17529403
84 Z = -5324298
04
XDOT = -10909
128761 XDOT = -3400
815006
YDOT = 22611
187396 feet/sec YDOT = 6854
283020 meter/sec
ZDOT = -747
888355 ZDOT = -244
292042
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9168483
98 X = 2794553
92
Y = 10380063
05 feet Y = 3163843
22 meter
Z = -17446126
10 Z = -5317579
24
XDOT = -18720
219388 XDOT = -5705
922869
YDOT = 15168
075665 feet/sec YDOT = 4623
229463 meter/sec
ZDOT = -821
873219 ZDOT = -250
506957
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 18148
26653274
00016717 00000-0 10270-3 0 9093
2 25544 51
6382 118
0227 0003672 131
2037 228
9433 15
54071429 35415
Satellite: ISS
Catalog Number: 25544
Epoch time: 18148
26653274 = yrday
fracday
Element set: 909
Inclination: 51
6382 deg
RA of node: 118
0227 deg
Eccentricity:
0003672
Arg of perigee: 131
2037 deg
Mean anomaly: 228
9433 deg
Mean motion: 15
54071429 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3541
Checksum: 302
Coasting Arc #11 (Orbit 3556)
---------------------------------------
Vector Time (GMT): 2018/149/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2997063
60 A = 6778271
87 meter
Y = -3265922
45 meter E =
0006753
Z = 5122290
03 I = 51
97153
XDOT = 3999
005228 Wp = 86
73998
YDOT = -6326
662471 meter/sec RA = 112
11472 deg
ZDOT = -1691
702416 TA = 19
52610
MA = 19
50024
Ha = 222
221 n
mi
Hp = 213
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9832885
83 X = -2985202
17
Y = -10714968
66 feet Y = -3299371
96 meter
Z = 16805413
47 Z = 5107759
53
XDOT = 13120
095892 XDOT = 4077
672005
YDOT = -20756
766636 feet/sec YDOT = -6281
502787 meter/sec
ZDOT = -5550
204776 ZDOT = -1672
086019
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4689106
93 X = -1429239
79
Y = -13844662
34 feet Y = -4219853
08 meter
Z = 16740839
88 Z = 5102608
00
XDOT = 19489
007775 XDOT = 5940
249570
YDOT = -13214
038474 feet/sec YDOT = -4027
638927 meter/sec
ZDOT = -5461
592556 ZDOT = -1664
693411
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 18149
29538315
00016717 00000-0 10270-3 0 9107
2 25544 51
6391 112
8941 0003597 134
4453 225
6995 15
54124897 35575
Satellite: ISS
Catalog Number: 25544
Epoch time: 18149
29538315 = yrday
fracday
Element set: 910
Inclination: 51
6391 deg
RA of node: 112
8941 deg
Eccentricity:
0003597
Arg of perigee: 134
4453 deg
Mean anomaly: 225
6995 deg
Mean motion: 15
54124897 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3557
Checksum: 336
Coasting Arc #12 (Orbit 3571)
---------------------------------------
Vector Time (GMT): 2018/150/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2147900
97 A = 6781239
69 meter
Y = 4703268
58 meter E =
0012395
Z = -4400466
46 I = 51
99321
XDOT = -4419
312690 Wp = 117
22887
YDOT = 5227
490966 meter/sec RA = 107
14394 deg
ZDOT = 3431
997855 TA = 187
42988
MA = 187
44826
Ha = 222
164 n
mi
Hp = 213
720
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7046919
19 X = 2116523
51
Y = 15430671
20 feet Y = 4727113
04 meter
Z = -14437225
93 Z = -4390108
15
XDOT = -14499
057383 XDOT = -4494
110518
YDOT = 17150
560912 feet/sec YDOT = 5177
652489 meter/sec
ZDOT = 11259
835483 ZDOT = 3410
349115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 495472
50 X = 151020
02
Y = 16995201
10 feet Y = 5180137
29 meter
Z = -14391519
13 Z = -4386535
03
XDOT = -18906
818441 XDOT = -5762
798261
YDOT = 9998
105196 feet/sec YDOT = 3047
422464 meter/sec
ZDOT = 11162
255095 ZDOT = 3402
255353
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 18150
25993060
00016717 00000-0 10270-3 0 9118
2 25544 51
6396 108
0860 0003694 133
0473 227
0989 15
54111596 35720
Satellite: ISS
Catalog Number: 25544
Epoch time: 18150
25993060 = yrday
fracday
Element set: 911
Inclination: 51
6396 deg
RA of node: 108
0860 deg
Eccentricity:
0003694
Arg of perigee: 133
0473 deg
Mean anomaly: 227
0989 deg
Mean motion: 15
54111596 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3572
Checksum: 312
Coasting Arc #13 (Orbit 3587)
---------------------------------------
Vector Time (GMT): 2018/151/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1293879
29 A = 6785005
96 meter
Y = -5833962
11 meter E =
0015622
Z = 3196397
36 I = 52
01441
XDOT = 4666
430762 Wp = 103
17969
YDOT = -3696
845848 meter/sec RA = 102
18402 deg
ZDOT = -4842
086500 TA = 40
06281
MA = 39
94769
Ha = 222
097 n
mi
Hp = 213
730
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4245010
80 X = -1244072
73
Y = -19140295
65 feet Y = -5848153
13 meter
Z = 10486867
97 Z = 3190232
22
XDOT = 15309
812210 XDOT = 4730
943611
YDOT = -12128
759345 feet/sec YDOT = -3644
301204 meter/sec
ZDOT = -15886
110564 ZDOT = -4819
262208
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3231708
77 X = 985024
83
Y = -19351693
06 feet Y = -5898396
05 meter
Z = 10460089
29 Z = 3188235
22
XDOT = 17442
486770 XDOT = 5316
469968
YDOT = -5647
544553 feet/sec YDOT = -1721
371580 meter/sec
ZDOT = -15783
460726 ZDOT = -4810
798829
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 18151
28877801
00016717 00000-0 10270-3 0 9127
2 25544 51
6393 102
9579 0003605 138
2634 221
8794 15
54132134 35889
Satellite: ISS
Catalog Number: 25544
Epoch time: 18151
28877801 = yrday
fracday
Element set: 912
Inclination: 51
6393 deg
RA of node: 102
9579 deg
Eccentricity:
0003605
Arg of perigee: 138
2634 deg
Mean anomaly: 221
8794 deg
Mean motion: 15
54132134 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3588
Checksum: 320
Coasting Arc #14 (Orbit 3602)
---------------------------------------
Vector Time (GMT): 2018/152/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 503367
40 A = 6788110
12 meter
Y = 6552677
71 meter E =
0007751
Z = -1697155
27 I = 52
03164
XDOT = -4742
274983 Wp = 65
81625
YDOT = 1842
535641 meter/sec RA = 97
23371 deg
ZDOT = 5731
090973 TA = 275
69212
MA = 275
78049
Ha = 222
058 n
mi
Hp = 213
773
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1651467
86 X = 438300
09
Y = 21498286
45 feet Y = 6557943
14 meter
Z = -5568094
73 Z = -1694867
17
XDOT = -15558
644958 XDOT = -4790
365056
YDOT = 6045
064438 feet/sec YDOT = 1789
234543 meter/sec
ZDOT = 18802
791907 ZDOT = 5707
937957
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6199484
61 X = -1889602
91
Y = 20653661
04 feet Y = 6295235
88 meter
Z = -5558778
78 Z = -1694315
77
XDOT = -15301
905255 XDOT = -4664
020722
YDOT = 418
686416 feet/sec YDOT = 127
615620 meter/sec
ZDOT = 18698
915570 ZDOT = 5699
429466
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 18152
25332202
00016717 00000-0 10270-3 0 9137
2 25544 51
6402 98
1499 0003697 141
0088 219
1332 15
54127071 36033
Satellite: ISS
Catalog Number: 25544
Epoch time: 18152
25332202 = yrday
fracday
Element set: 913
Inclination: 51
6402 deg
RA of node: 98
1499 deg
Eccentricity:
0003697
Arg of perigee: 141
0088 deg
Mean anomaly: 219
1332 deg
Mean motion: 15
54127071 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3603
Checksum: 284
Coasting Arc #15 (Orbit 3618)
---------------------------------------
Vector Time (GMT): 2018/153/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 286542
62 A = 6789367
68 meter
Y = -6775557
63 meter E =
0015684
Z = -19951
70 I = 52
03955
XDOT = 4713
928932 Wp = 136
65302
YDOT = 208
875330 meter/sec RA = 92
29012 deg
ZDOT = -6048
018252 TA = 43
56078
MA = 43
43703
Ha = 222
045 n
mi
Hp = 213
828
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 940100
46 X = 362384
38
Y = -22229519
80 feet Y = -6771929
26 meter
Z = -65458
34 Z = -18376
51
XDOT = 15465
646101 XDOT = 4740
621061
YDOT = 685
286517 feet/sec YDOT = 261
739821 meter/sec
ZDOT = -19842
579566 ZDOT = -6025
054678
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8563006
63 X = 2610004
42
Y = -20535609
13 feet Y = -6259253
66 meter
Z = -57439
43 Z = -17507
54
XDOT = 12902
455812 XDOT = 3932
668532
YDOT = 5405
884259 feet/sec YDOT = 1647
713522 meter/sec
ZDOT = -19739
833090 ZDOT = -6016
701126
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 18153
28216477
00016717 00000-0 10270-3 0 9147
2 25544 51
6409 93
0213 0003640 143
5340 216
6061 15
54116066 36194
Satellite: ISS
Catalog Number: 25544
Epoch time: 18153
28216477 = yrday
fracday
Element set: 914
Inclination: 51
6409 deg
RA of node: 93
0213 deg
Eccentricity:
0003640
Arg of perigee: 143
5340 deg
Mean anomaly: 216
6061 deg
Mean motion: 15
54116066 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3619
Checksum: 285
Coasting Arc #16 (Orbit 3622)
---------------------------------------
Vector Time (GMT): 2018/153/12:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 922320
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3566205
02 A = 6780907
42 meter
Y = -3637442
55 meter E =
0010833
Z = -4485349
48 I = 52
01084
XDOT = 2460
100398 Wp = 86
78419
YDOT = 6463
869817 meter/sec RA = 90
98772 deg
ZDOT = -3292
218451 TA = 150
19810
MA = 150
13636
Ha = 221
971 n
mi
Hp = 213
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11700147
72 X = 3628402
37
Y = -11933866
64 feet Y = -3597214
40 meter
Z = -14715713
51 Z = -4467875
48
XDOT = 8071
195532 XDOT = 2403
628700
YDOT = 21206
921971 feet/sec YDOT = 6491
065055 meter/sec
ZDOT = -10801
241636 ZDOT = -3280
404370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8801656
56 X = -2682744
92
Y = -14288191
60 feet Y = -4355040
80 meter
Z = -14636983
17 Z = -4461352
47
XDOT = 21489
225095 XDOT = 6549
915809
YDOT = -2246
970017 feet/sec YDOT = -684
876461 meter/sec
ZDOT = -10749
292947 ZDOT = -3276
384490
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 18153
53937618
00016717 00000-0 10270-3 0 9153
2 25544 51
6400 91
7395 0003376 142
1846 217
9544 15
54127162 36237
Satellite: ISS
Catalog Number: 25544
Epoch time: 18153
53937618 = yrday
fracday
Element set: 915
Inclination: 51
6400 deg
RA of node: 91
7395 deg
Eccentricity:
0003376
Arg of perigee: 142
1846 deg
Mean anomaly: 217
9544 deg
Mean motion: 15
54127162 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3623
Checksum: 314
Coasting Arc #17 (Orbit 3636)
---------------------------------------
Vector Time (GMT): 2018/154/09:16:30
000
Vector Time (MET): N/A
Weight (LBS) : 907088
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3510231
08 A = 6779876
24 meter
Y = 3344647
17 meter E =
0010891
Z = 4734393
75 I = 52
00503
XDOT = -2571
727591 Wp = 126
51367
YDOT = -6666
274234 meter/sec RA = 86
67619 deg
ZDOT = 2791
927398 TA = 295
92534
MA = 296
03754
Ha = 221
941 n
mi
Hp = 213
960
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11516506
16 X = -3570368
16
Y = 10973251
87 feet Y = 3305056
48 meter
Z = 15532787
90 Z = 4717196
62
XDOT = -8437
426479 XDOT = -2510
554074
YDOT = -21870
978458 feet/sec YDOT = -6694
691384 meter/sec
ZDOT = 9159
866791 ZDOT = 2779
582537
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4566481
16 X = -1391863
46
Y = 15316321
41 feet Y = 4668414
77 meter
Z = 15455329
79 Z = 4710784
52
XDOT = -17185
938326 XDOT = -5238
274002
YDOT = -14347
884129 feet/sec YDOT = -4373
235083 meter/sec
ZDOT = 9105
579126 ZDOT = 2775
380518
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 18154
43961075
00016717 00000-0 10270-3 0 9168
2 25544 51
6377 87
2526 0003395 149
4589 210
6762 15
54139152 36370
Satellite: ISS
Catalog Number: 25544
Epoch time: 18154
43961075 = yrday
fracday
Element set: 916
Inclination: 51
6377 deg
RA of node: 87
2526 deg
Eccentricity:
0003395
Arg of perigee: 149
4589 deg
Mean anomaly: 210
6762 deg
Mean motion: 15
54139152 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3637
Checksum: 332
Coasting Arc #18 (Orbit 3651)
---------------------------------------
Vector Time (GMT): 2018/155/09:16:30
000
Vector Time (MET): N/A
Weight (LBS) : 907088
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3934125
84 A = 6777694
12 meter
Y = -1637253
07 meter E =
0016005
Z = -5284173
89 I = 51
99488
XDOT = 1816
434483 Wp = 94
21604
YDOT = 7378
971517 meter/sec RA = 81
70310 deg
ZDOT = -937
534606 TA = 166
86518
MA = 166
82345
Ha = 221
879 n
mi
Hp = 214
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12907237
01 X = 3977809
38
Y = -5371565
19 feet Y = -1593014
09 meter
Z = -17336528
51 Z = -5264957
37
XDOT = 5959
430717 XDOT = 1738
339849
YDOT = 24209
224137 feet/sec YDOT = 7398
847595 meter/sec
ZDOT = -3075
900939 ZDOT = -928
899805
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8390942
62 X = 2557559
31
Y = -11314851
21 feet Y = -3448766
65 meter
Z = -17250273
18 Z = -5257883
27
XDOT = 16774
603333 XDOT = 5112
899096
YDOT = 17053
959051 feet/sec YDOT = 5198
046719 meter/sec
ZDOT = -3038
333250 ZDOT = -926
083975
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 18155
40414828
00016717 00000-0 10270-3 0 9176
2 25544 51
6381 82
4437 0003408 151
2567 208
8774 15
54110420 36521
Satellite: ISS
Catalog Number: 25544
Epoch time: 18155
40414828 = yrday
fracday
Element set: 917
Inclination: 51
6381 deg
RA of node: 82
4437 deg
Eccentricity:
0003408
Arg of perigee: 151
2567 deg
Mean anomaly: 208
8774 deg
Mean motion: 15
54110420 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3652
Checksum: 301
Coasting Arc #19 (Orbit 3667)
---------------------------------------
Vector Time (GMT): 2018/156/09:16:30
000
Vector Time (MET): N/A
Weight (LBS) : 907088
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4261976
63 A = 6777710
37 meter
Y = -148306
19 meter E =
0004611
Z = 5263900
52 I = 51
98997
XDOT = -974
765881 Wp = 103
07744
YDOT = -7543
897302 meter/sec RA = 76
72784 deg
ZDOT = -1002
054274 TA = 356
46257
MA = 356
46583
Ha = 221
939 n
mi
Hp = 214
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13982862
96 X = -4285570
72
Y = -486568
86 feet Y = -196099
02 meter
Z = 17270014
82 Z = 5243139
99
XDOT = -3198
050792 XDOT = -885
468059
YDOT = -24750
319232 feet/sec YDOT = -7554
298406 meter/sec
ZDOT = -3287
579639 ZDOT = -1006
573252
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12211490
38 X = -3722062
27
Y = 7059537
28 feet Y = 2151746
96 meter
Z = 17177108
42 Z = 5235582
65
XDOT = -15295
854403 XDOT = -4662
176422
YDOT = -18415
050655 feet/sec YDOT = -5612
907440 meter/sec
ZDOT = -3306
688730 ZDOT = -1007
878725
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 18156
43298401
00016717 00000-0 10270-3 0 9188
2 25544 51
6389 77
3153 0003308 154
6361 205
4955 15
54118028 36688
Satellite: ISS
Catalog Number: 25544
Epoch time: 18156
43298401 = yrday
fracday
Element set: 918
Inclination: 51
6389 deg
RA of node: 77
3153 deg
Eccentricity:
0003308
Arg of perigee: 154
6361 deg
Mean anomaly: 205
4955 deg
Mean motion: 15
54118028 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3668
Checksum: 320
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