[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 12th 2017
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 610 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
285/09:32:03
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
1
285/12:56:35
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
286/19:38:30
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
290/03:04:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
3
000/00:00:00
000 0
0 0
0 213
7
294/08:55:00
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
3
299/12:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
6
000/00:00:00
000 0
0 0
0 212
8
Coasting Arc #1 (Orbit 3983)
---------------------------------------
Vector Time (GMT): 2017/284/12:49:20
768
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -145126
61 A = 6777289
49 meter
Y = 4219552
43 meter E =
0015954
Z = -5314600
23 I = 51
63382
XDOT = -7649
846277 Wp = 74
41325
YDOT = 128
664628 meter/sec RA = 177
16258 deg
ZDOT = 316
027114 TA = 198
57486
MA = 198
63316
Ha = 221
835 n
mi
Hp = 214
185
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -476137
18 X = -166483
86
Y = 13843675
96 feet Y = 4217809
89 meter
Z = -17436352
48 Z = -5315357
28
XDOT = -25097
920857 XDOT = -7652
251613
YDOT = 422
128046 feet/sec YDOT = 43
105392 meter/sec
ZDOT = 1036
834365 ZDOT = 278
860107
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6980728
53 X = -2127726
06
Y = -11958583
32 feet Y = -3644976
19 meter
Z = -17440245
77 Z = -5315786
91
XDOT = 20248
268102 XDOT = 6171
672117
YDOT = -13067
817699 feet/sec YDOT = -3983
070835 meter/sec
ZDOT = 872
102178 ZDOT = 265
816744
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 17284
54990610
00016717 00000-0 10270-3 0 9003
2 25544 51
6408 178
2528 0004971 5
8276 354
2934 15
54159728 39849
Satellite: ISS
Catalog Number: 25544
Epoch time: 17284
54990610 = yrday
fracday
Element set: 900
Inclination: 51
6408 deg
RA of node: 178
2528 deg
Eccentricity:
0004971
Arg of perigee: 5
8276 deg
Mean anomaly: 354
2934 deg
Mean motion: 15
54159728 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3984
Checksum: 336
Coasting Arc #2 (Orbit 3997)
---------------------------------------
Vector Time (GMT): 2017/285/09:32:03
000
Vector Time (MET): N/A
Weight (LBS) : 904993
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3354725
41 A = 6779500
88 meter
Y = -3406000
26 meter E =
0007402
Z = 4800144
34 I = 51
66756
XDOT = 6625
376551 Wp = 81
07977
YDOT = -2884
142769 meter/sec RA = 172
88406 deg
ZDOT = 2581
591873 TA = 343
51033
MA = 343
53440
Ha = 221
929 n
mi
Hp = 214
125
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11006316
96 X = -3339706
30
Y = -11174541
54 feet Y = -3443430
89 meter
Z = 15748505
06 Z = 4783884
57
XDOT = 21736
799708 XDOT = 6644
595133
YDOT = -9462
410660 feet/sec YDOT = -2809
945712 meter/sec
ZDOT = 8469
789611 ZDOT = 2613
823096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7429454
84 X = 2264497
84
Y = 13894737
58 feet Y = 4235116
02 meter
Z = 15676870
59 Z = 4778310
15
XDOT = -22472
145649 XDOT = -6849
509994
YDOT = 2289
582049 feet/sec YDOT = 697
864609 meter/sec
ZDOT = 8613
017956 ZDOT = 2625
247873
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 17285
45012676
00016717 00000-0 10270-3 0 9012
2 25544 51
6390 173
7645 0004843 9
0034 351
1205 15
54171463 39987
Satellite: ISS
Catalog Number: 25544
Epoch time: 17285
45012676 = yrday
fracday
Element set: 901
Inclination: 51
6390 deg
RA of node: 173
7645 deg
Eccentricity:
0004843
Arg of perigee: 9
0034 deg
Mean anomaly: 351
1205 deg
Mean motion: 15
54171463 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3998
Checksum: 303
Coasting Arc #3 (Orbit 3999)
---------------------------------------
Vector Time (GMT): 2017/285/12:56:35
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4771094
44 A = 6784134
65 meter
Y = -3390250
71 meter E =
0014118
Z = 3424131
35 I = 51
68948
XDOT = 5393
955283 Wp = 69
03858
YDOT = 2923
871172 meter/sec RA = 172
13226 deg
ZDOT = -4600
603511 TA = 70
90525
MA = 70
75242
Ha = 221
859 n
mi
Hp = 214
037
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15653197
00 X = 4792017
59
Y = -11122869
77 feet Y = -3336779
92 meter
Z = 11234026
75 Z = 3447359
10
XDOT = 17696
703683 XDOT = 5383
206618
YDOT = 9592
753189 feet/sec YDOT = 2984
129745 meter/sec
ZDOT = -15093
843541 ZDOT = -4574
427294
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6517455
22 X = -1986520
35
Y = 17998054
27 feet Y = 5485806
94 meter
Z = 11337415
28 Z = 3455644
18
XDOT = -18783
182323 XDOT = -5725
113972
YDOT = 2674
835395 feet/sec YDOT = 815
289828 meter/sec
ZDOT = -14978
191727 ZDOT = -4565
352838
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 17285
57872925
00016717 00000-0 10270-3 0 9027
2 25544 51
6405 173
1243 0005056 9
4479 350
6768 15
54174393 40004
Satellite: ISS
Catalog Number: 25544
Epoch time: 17285
57872925 = yrday
fracday
Element set: 902
Inclination: 51
6405 deg
RA of node: 173
1243 deg
Eccentricity:
0005056
Arg of perigee: 9
4479 deg
Mean anomaly: 350
6768 deg
Mean motion: 15
54174393 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4000
Checksum: 315
Coasting Arc #4 (Orbit 4014)
---------------------------------------
Vector Time (GMT): 2017/286/12:56:35
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5801735
04 A = 6787567
93 meter
Y = 2912339
21 meter E =
0011408
Z = -1965059
57 I = 51
73324
XDOT = -3734
468112 Wp = 28
23249
YDOT = -3677
843491 meter/sec RA = 167
15873 deg
ZDOT = 5598
106811 TA = 310
11303
MA = 310
21295
Ha = 221
928 n
mi
Hp = 214
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19034563
78 X = -5824325
02
Y = 9554918
66 feet Y = 2847333
82 meter
Z = -6447045
82 Z = -1993297
88
XDOT = -12252
191968 XDOT = -3720
257027
YDOT = -12066
415652 feet/sec YDOT = -3719
525061 meter/sec
ZDOT = 18366
492163 ZDOT = 5580
000508
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9894824
34 X = 3015942
46
Y = -18816717
72 feet Y = -5735335
56 meter
Z = -6572600
27 Z = -2003328
56
XDOT = 15709
174886 XDOT = 4788
156505
YDOT = 1899
188848 feet/sec YDOT = 578
872761 meter/sec
ZDOT = 18286
694418 ZDOT = 5573
784459
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 17286
54324749
00016717 00000-0 10270-3 0 9032
2 25544 51
6409 168
3158 0005044 11
1531 348
9732 15
54147579 40158
Satellite: ISS
Catalog Number: 25544
Epoch time: 17286
54324749 = yrday
fracday
Element set: 903
Inclination: 51
6409 deg
RA of node: 168
3158 deg
Eccentricity:
0005044
Arg of perigee: 11
1531 deg
Mean anomaly: 348
9732 deg
Mean motion: 15
54147579 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4015
Checksum: 314
Coasting Arc #5 (Orbit 4019)
---------------------------------------
Vector Time (GMT): 2017/286/19:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 259380
52 A = 6777717
17 meter
Y = -4315216
20 meter E =
0007870
Z = 5217232
91 I = 51
70835
XDOT = 7521
649218 Wp = 35
26237
YDOT = -961
045984 meter/sec RA = 165
77160 deg
ZDOT = -1161
681595 TA = 65
90324
MA = 65
82094
Ha = 221
932 n
mi
Hp = 214
012
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 850985
97 X = 282272
17
Y = -14157533
47 feet Y = -4312187
29 meter
Z = 17116905
86 Z = 5218548
79
XDOT = 24677
326830 XDOT = 7537
479791
YDOT = -3153
038004 feet/sec YDOT = -876
845330 meter/sec
ZDOT = -3811
291322 ZDOT = -1125
104942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10312441
24 X = 3143232
09
Y = -9725990
61 feet Y = -2964481
94 meter
Z = 17123289
97 Z = 5219178
78
XDOT = 19330
670802 XDOT = 5891
988460
YDOT = 14030
599286 feet/sec YDOT = 4276
526662 meter/sec
ZDOT = -3649
015161 ZDOT = -1112
219821
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 17286
86475436
00016717 00000-0 10270-3 0 9048
2 25544 51
6401 166
7074 0004532 16
5738 343
5562 15
54142597 40201
Satellite: ISS
Catalog Number: 25544
Epoch time: 17286
86475436 = yrday
fracday
Element set: 904
Inclination: 51
6401 deg
RA of node: 166
7074 deg
Eccentricity:
0004532
Arg of perigee: 16
5738 deg
Mean anomaly: 343
5562 deg
Mean motion: 15
54142597 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4020
Checksum: 313
Coasting Arc #6 (Orbit 4034)
---------------------------------------
Vector Time (GMT): 2017/287/19:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1970647
54 A = 6780086
20 meter
Y = 4553128
26 meter E =
0011372
Z = -4630656
48 I = 51
74813
XDOT = -7056
220756 Wp = 86
82053
YDOT = -29
261666 meter/sec RA = 160
78249 deg
ZDOT = 2981
044121 TA = 212
85091
MA = 212
92165
Ha = 221
957 n
mi
Hp = 213
829
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6465379
07 X = -1998921
73
Y = 14938084
85 feet Y = 4530932
66 meter
Z = -15192442
51 Z = -4640298
41
XDOT = -23150
330564 XDOT = -7069
849678
YDOT = -96
002840 feet/sec YDOT = -108
245097 meter/sec
ZDOT = 9780
328482 ZDOT = 2946
733816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14808132
52 X = -4513518
79
Y = 6659446
25 feet Y = 2029799
22 meter
Z = -15235773
76 Z = -4643863
84
XDOT = -16509
074734 XDOT = -5031
965979
YDOT = -14734
092263 feet/sec YDOT = -4490
951322 meter/sec
ZDOT = 9628
207105 ZDOT = 2934
677526
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 17287
82926719
00016717 00000-0 10270-3 0 9051
2 25544 51
6402 161
9004 0004516 20
0275 340
1054 15
54167240 40357
Satellite: ISS
Catalog Number: 25544
Epoch time: 17287
82926719 = yrday
fracday
Element set: 905
Inclination: 51
6402 deg
RA of node: 161
9004 deg
Eccentricity:
0004516
Arg of perigee: 20
0275 deg
Mean anomaly: 340
1054 deg
Mean motion: 15
54167240 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4035
Checksum: 282
Coasting Arc #7 (Orbit 4050)
---------------------------------------
Vector Time (GMT): 2017/288/19:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3499569
26 A = 6783948
13 meter
Y = -4614615
08 meter E =
0014689
Z = 3525007
33 I = 51
79106
XDOT = 6092
310981 Wp = 72
32948
YDOT = 1157
404613 meter/sec RA = 155
80303 deg
ZDOT = -4513
357376 TA = 66
24272
MA = 66
08873
Ha = 222
025 n
mi
Hp = 213
802
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11481526
44 X = 3533788
09
Y = -15139813
24 feet Y = -4575288
82 meter
Z = 11564984
69 Z = 3542090
90
XDOT = 19987
896918 XDOT = 6100
839673
YDOT = 3797
259228 feet/sec YDOT = 1225
580229 meter/sec
ZDOT = -14807
602941 ZDOT = -4483
741932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18587703
69 X = 5665532
08
Y = -3710125
03 feet Y = -1130846
11 meter
Z = 11641327
63 Z = 3548276
66
XDOT = 12195
009911 XDOT = 3717
039021
YDOT = 14843
719860 feet/sec YDOT = 4524
365813 meter/sec
ZDOT = -14676
427759 ZDOT = -4473
375181
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 17288
85807970
00016717 00000-0 10270-3 0 9063
2 25544 51
6399 156
7714 0004451 24
7996 335
3370 15
54143415 40514
Satellite: ISS
Catalog Number: 25544
Epoch time: 17288
85807970 = yrday
fracday
Element set: 906
Inclination: 51
6399 deg
RA of node: 156
7714 deg
Eccentricity:
0004451
Arg of perigee: 24
7996 deg
Mean anomaly: 335
3370 deg
Mean motion: 15
54143415 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4051
Checksum: 331
Coasting Arc #8 (Orbit 4065)
---------------------------------------
Vector Time (GMT): 2017/289/19:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4655389
62 A = 6787388
02 meter
Y = 4472645
97 meter E =
0010945
Z = -2082822
08 I = 51
83318
XDOT = -4735
668410 Wp = 35
16561
YDOT = -2354
526498 meter/sec RA = 150
83645 deg
ZDOT = 5551
961982 TA = 301
84663
MA = 301
95312
Ha = 222
105 n
mi
Hp = 213
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15273588
00 X = -4694940
48
Y = 14674035
33 feet Y = 4420364
85 meter
Z = -6833405
77 Z = -2105533
37
XDOT = -15536
969850 XDOT = -4735
956564
YDOT = -7724
824470 feet/sec YDOT = -2407
484973 meter/sec
ZDOT = 18215
098365 ZDOT = 5528
956837
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21114404
03 X = -6435670
35
Y = 1182012
58 feet Y = 360277
43 meter
Z = -6934697
28 Z = -2113695
73
XDOT = -6737
765811 XDOT = -2053
671019
YDOT = -14528
891279 feet/sec YDOT = -4428
406062 meter/sec
ZDOT = 18113
379950 ZDOT = 5520
958209
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 17289
82258682
00016717 00000-0 10270-3 0 9072
2 25544 51
6411 151
9636 0004653 25
5193 334
6189 15
54142979 40661
Satellite: ISS
Catalog Number: 25544
Epoch time: 17289
82258682 = yrday
fracday
Element set: 907
Inclination: 51
6411 deg
RA of node: 151
9636 deg
Eccentricity:
0004653
Arg of perigee: 25
5193 deg
Mean anomaly: 334
6189 deg
Mean motion: 15
54142979 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4066
Checksum: 337
Coasting Arc #9 (Orbit 4070)
---------------------------------------
Vector Time (GMT): 2017/290/03:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2224043
51 A = 6777299
64 meter
Y = 3561133
58 meter E =
0017828
Z = -5335053
75 I = 51
80523
XDOT = -6550
595549 Wp = 75
22694
YDOT = 3961
550444 meter/sec RA = 149
32038 deg
ZDOT = -82
248266 TA = 193
96511
MA = 194
01448
Ha = 222
288 n
mi
Hp = 213
664
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7296730
69 X = 2209972
12
Y = 11683509
13 feet Y = 3585925
08 meter
Z = -17503457
19 Z = -5324284
47
XDOT = -21491
455213 XDOT = -6594
008280
YDOT = 12997
212742 feet/sec YDOT = 3888
054466 meter/sec
ZDOT = -269
843394 ZDOT = -114
175368
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13461488
70 X = 4103061
75
Y = -3191963
44 feet Y = -972910
46 meter
Z = -17456155
64 Z = -5320636
24
XDOT = 5037
525500 XDOT = 1535
437772
YDOT = 23573
155941 feet/sec YDOT = 7185
097931 meter/sec
ZDOT = -411
943201 ZDOT = -125
560288
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 17290
14408833
00016717 00000-0 10270-3 0 9085
2 25544 51
6382 150
3638 0004996 28
0091 332
1330 15
54151246 40712
Satellite: ISS
Catalog Number: 25544
Epoch time: 17290
14408833 = yrday
fracday
Element set: 908
Inclination: 51
6382 deg
RA of node: 150
3638 deg
Eccentricity:
0004996
Arg of perigee: 28
0091 deg
Mean anomaly: 332
1330 deg
Mean motion: 15
54151246 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4071
Checksum: 291
Coasting Arc #10 (Orbit 4086)
---------------------------------------
Vector Time (GMT): 2017/291/03:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -615426
80 A = 6778314
90 meter
Y = -4457973
79 meter E =
0010259
Z = 5064834
31 I = 51
83531
XDOT = 6781
840959 Wp = 43
59977
YDOT = -3064
424876 meter/sec RA = 144
33290 deg
ZDOT = -1863
696052 TA = 64
45058
MA = 64
34456
Ha = 222
309 n
mi
Hp = 213
513
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2019116
81 X = -590133
74
Y = -14625898
26 feet Y = -4464713
91 meter
Z = 16616910
46 Z = 5061906
64
XDOT = 22250
134381 XDOT = 6824
657220
YDOT = -10053
887387 feet/sec YDOT = -2988
346511 meter/sec
ZDOT = -6114
488359 ZDOT = -1830
647031
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14563452
35 X = -4438940
28
Y = -2512317
69 feet Y = -765754
43 meter
Z = 16604504
25 Z = 5061052
89
XDOT = -2829
102041 XDOT = -862
310302
YDOT = -23246
946593 feet/sec YDOT = -7085
669322 meter/sec
ZDOT = -5967
513296 ZDOT = -1818
898053
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 17291
17289156
00016717 00000-0 10270-3 0 9095
2 25544 51
6369 145
2345 0005053 30
0644 330
0798 15
54174294 40877
Satellite: ISS
Catalog Number: 25544
Epoch time: 17291
17289156 = yrday
fracday
Element set: 909
Inclination: 51
6369 deg
RA of node: 145
2345 deg
Eccentricity:
0005053
Arg of perigee: 30
0644 deg
Mean anomaly: 330
0798 deg
Mean motion: 15
54174294 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4087
Checksum: 316
Coasting Arc #11 (Orbit 4101)
---------------------------------------
Vector Time (GMT): 2017/292/03:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -876644
68 A = 6781449
54 meter
Y = 5187631
75 meter E =
0010797
Z = -4287209
98 I = 51
87115
XDOT = -6503
037319 Wp = 83
18251
YDOT = 1864
285688 meter/sec RA = 139
35419 deg
ZDOT = 3594
570506 TA = 223
39479
MA = 223
47985
Ha = 222
405 n
mi
Hp = 213
417
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2876130
85 X = -913763
39
Y = 17019789
19 feet Y = 5177620
50 meter
Z = -14065649
53 Z = -4291559
26
XDOT = -21335
424275 XDOT = -6540
861981
YDOT = 6116
422861 feet/sec YDOT = 1791
353182 meter/sec
ZDOT = 11793
210322 ZDOT = 3562
888006
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15450227
56 X = 4709229
36
Y = 7659867
82 feet Y = 2334727
71 meter
Z = -14085621
84 Z = -4293297
54
XDOT = 116
620735 XDOT = 35
546000
YDOT = 21138
035257 feet/sec YDOT = 6442
873146 meter/sec
ZDOT = 11652
438103 ZDOT = 3551
663134
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 17292
13739294
00016717 00000-0 10270-3 0 9107
2 25544 51
6364 140
4266 0005123 33
6420 326
5057 15
54153528 41023
Satellite: ISS
Catalog Number: 25544
Epoch time: 17292
13739294 = yrday
fracday
Element set: 910
Inclination: 51
6364 deg
RA of node: 140
4266 deg
Eccentricity:
0005123
Arg of perigee: 33
6420 deg
Mean anomaly: 326
5057 deg
Mean motion: 15
54153528 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4102
Checksum: 284
Coasting Arc #12 (Orbit 4117)
---------------------------------------
Vector Time (GMT): 2017/293/03:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2222213
22 A = 6785232
67 meter
Y = -5651160
03 meter E =
0016253
Z = 3016877
11 I = 51
90852
XDOT = 5825
950574 Wp = 80
81595
YDOT = -378
042225 meter/sec RA = 134
38577 deg
ZDOT = -4974
177333 TA = 64
75853
MA = 64
59016
Ha = 222
358 n
mi
Hp = 213
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7290725
80 X = 2270585
97
Y = -18540551
28 feet Y = -5626038
97 meter
Z = 9897890
77 Z = 3027790
23
XDOT = 19114
011068 XDOT = 5853
907659
YDOT = -1240
296014 feet/sec YDOT = -312
736625 meter/sec
ZDOT = -16319
479440 ZDOT = -4945
808031
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15809692
61 X = -4818794
31
Y = -12082414
29 feet Y = -3682719
88 meter
Z = 9947052
35 Z = 3031861
56
XDOT = 3254
824562 XDOT = 992
070526
YDOT = -17658
606567 feet/sec YDOT = -5382
343282 meter/sec
ZDOT = -16193
587629 ZDOT = -4935
805509
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 17293
16618991
00016717 00000-0 10270-3 0 9112
2 25544 51
6366 135
2966 0005129 36
1139 324
0359 15
54197845 41180
Satellite: ISS
Catalog Number: 25544
Epoch time: 17293
16618991 = yrday
fracday
Element set: 911
Inclination: 51
6366 deg
RA of node: 135
2966 deg
Eccentricity:
0005129
Arg of perigee: 36
1139 deg
Mean anomaly: 324
0359 deg
Mean motion: 15
54197845 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4118
Checksum: 326
Coasting Arc #13 (Orbit 4132)
---------------------------------------
Vector Time (GMT): 2017/294/03:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3254919
02 A = 6788180
63 meter
Y = 5767226
14 meter E =
0013498
Z = -1467286
38 I = 51
94061
XDOT = -4845
217058 Wp = 39
25872
YDOT = -1266
965014 meter/sec RA = 129
42962 deg
ZDOT = 5807
680152 TA = 304
79496
MA = 304
92191
Ha = 222
446 n
mi
Hp = 213
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10678868
19 X = -3312040
22
Y = 18921345
62 feet Y = 5730507
92 meter
Z = -4813931
70 Z = -1483237
39
XDOT = -15896
381424 XDOT = -4858
901024
YDOT = -4156
709365 feet/sec YDOT = -1321
223596 meter/sec
ZDOT = 19054
068741 ZDOT = 5784
109827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15491328
42 X = 4721756
90
Y = 15211192
25 feet Y = 4636371
40 meter
Z = -4885474
22 Z = -1489092
54
XDOT = -7078
597132 XDOT = -2157
556406
YDOT = 13254
377078 feet/sec YDOT = 4039
934133 meter/sec
ZDOT = 18949
677940 ZDOT = 5775
861836
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 17294
13068389
00016717 00000-0 10270-3 0 9121
2 25544 51
6367 130
4884 0005184 41
0789 319
0753 15
54198866 41337
Satellite: ISS
Catalog Number: 25544
Epoch time: 17294
13068389 = yrday
fracday
Element set: 912
Inclination: 51
6367 deg
RA of node: 130
4884 deg
Eccentricity:
0005184
Arg of perigee: 41
0789 deg
Mean anomaly: 319
0753 deg
Mean motion: 15
54198866 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4133
Checksum: 332
Coasting Arc #14 (Orbit 4136)
---------------------------------------
Vector Time (GMT): 2017/294/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3373448
75 A = 6777127
45 meter
Y = 2484426
70 meter E =
0018613
Z = -5342686
03 I = 51
91226
XDOT = -4663
746739 Wp = 76
84145
YDOT = 6069
367433 meter/sec RA = 128
23498 deg
ZDOT = -118
638661 TA = 192
00806
MA = 192
05249
Ha = 222
415 n
mi
Hp = 213
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11067745
25 X = 3371369
35
Y = 8151006
24 feet Y = 2522138
89 meter
Z = -17528497
48 Z = -5326303
66
XDOT = -15301
006362 XDOT = -4730
693100
YDOT = 19912
622811 feet/sec YDOT = 6016
839903 meter/sec
ZDOT = -389
234451 ZDOT = -141
457361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8288028
24 X = -2526191
01
Y = -11080307
91 feet Y = -3377277
85 meter
Z = -17456158
69 Z = -5320637
17
XDOT = 19674
024604 XDOT = 5996
642699
YDOT = -13922
519991 feet/sec YDOT = -4243
584093 meter/sec
ZDOT = -491
289680 ZDOT = -149
745094
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 17294
38788128
00016717 00000-0 10270-3 0 9139
2 25544 51
6402 129
2071 0005169 38
8895 321
2628 15
54211159 41377
Satellite: ISS
Catalog Number: 25544
Epoch time: 17294
38788128 = yrday
fracday
Element set: 913
Inclination: 51
6402 deg
RA of node: 129
2071 deg
Eccentricity:
0005169
Arg of perigee: 38
8895 deg
Mean anomaly: 321
2628 deg
Mean motion: 15
54211159 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4137
Checksum: 320
Coasting Arc #15 (Orbit 4152)
---------------------------------------
Vector Time (GMT): 2017/295/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2193024
91 A = 6778109
65 meter
Y = -3909480
90 meter E =
0010420
Z = 5079342
10 I = 51
93504
XDOT = 5211
480977 Wp = 48
96022
YDOT = -5322
939785 meter/sec RA = 123
25445 deg
ZDOT = -1837
781134 TA = 58
80247
MA = 58
70037
Ha = 222
437 n
mi
Hp = 213
152
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7194963
63 X = -2173818
69
Y = -12826380
92 feet Y = -3933897
13 meter
Z = 16664508
20 Z = 5068735
65
XDOT = 17098
034701 XDOT = 5279
543461
YDOT = -17463
713204 feet/sec YDOT = -5264
280989 meter/sec
ZDOT = -6029
465663 ZDOT = -1812
299074
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3452527
67 X = 1052330
43
Y = 14349626
33 feet Y = 4373766
11 meter
Z = 16617992
04 Z = 5065163
97
XDOT = -20269
003987 XDOT = -6177
992415
YDOT = 11762
281518 feet/sec YDOT = 3585
143407 meter/sec
ZDOT = -5915
674246 ZDOT = -1803
097510
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 17295
41666980
00016717 00000-0 10270-3 0 9146
2 25544 51
6399 124
0781 0005071 41
6639 318
4899 15
54237512 41530
Satellite: ISS
Catalog Number: 25544
Epoch time: 17295
41666980 = yrday
fracday
Element set: 914
Inclination: 51
6399 deg
RA of node: 124
0781 deg
Eccentricity:
0005071
Arg of perigee: 41
6639 deg
Mean anomaly: 318
4899 deg
Mean motion: 15
54237512 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4153
Checksum: 330
Coasting Arc #16 (Orbit 4167)
---------------------------------------
Vector Time (GMT): 2017/296/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1058996
89 A = 6781265
38 meter
Y = 5139574
21 meter E =
0011477
Z = -4304674
02 I = 51
96275
XDOT = -5387
870602 Wp = 86
79611
YDOT = 4101
823793 meter/sec RA = 118
28084 deg
ZDOT = 3580
743460 TA = 219
56885
MA = 219
65269
Ha = 222
463 n
mi
Hp = 213
155
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3474399
25 X = 1022356
63
Y = 16862120
12 feet Y = 5151211
59 meter
Z = -14122946
25 Z = -4299618
81
XDOT = -17676
740821 XDOT = -5450
731800
YDOT = 13457
427143 feet/sec YDOT = 4041
221614 meter/sec
ZDOT = 11747
845999 ZDOT = 3554
417321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 963145
82 X = 293566
85
Y = -17207194
65 feet Y = -5244752
93 meter
Z = -14101239
60 Z = -4298057
83
XDOT = 19398
804380 XDOT = 5912
755575
YDOT = -8421
506713 feet/sec YDOT = -2566
875246 meter/sec
ZDOT = 11630
458527 ZDOT = 3544
963759
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 17296
38115804
00016717 00000-0 10270-3 0 9158
2 25544 51
6402 119
2693 0005072 44
5683 315
5877 15
54211361 41689
Satellite: ISS
Catalog Number: 25544
Epoch time: 17296
38115804 = yrday
fracday
Element set: 915
Inclination: 51
6402 deg
RA of node: 119
2693 deg
Eccentricity:
0005072
Arg of perigee: 44
5683 deg
Mean anomaly: 315
5877 deg
Mean motion: 15
54211361 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4168
Checksum: 311
Coasting Arc #17 (Orbit 4183)
---------------------------------------
Vector Time (GMT): 2017/297/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 35140
38 A = 6785111
20 meter
Y = -6064704
25 meter E =
0016986
Z = 3030366
21 I = 51
99093
XDOT = 5294
696094 Wp = 83
08131
YDOT = -2466
612813 meter/sec RA = 113
31808 deg
ZDOT = -4972
053427 TA = 62
35742
MA = 62
18509
Ha = 222
499 n
mi
Hp = 212
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 115289
96 X = 88234
52
Y = -19897323
65 feet Y = -6064014
33 meter
Z = 9942146
35 Z = 3030666
06
XDOT = 17371
050177 XDOT = 5346
037286
YDOT = -8092
561723 feet/sec YDOT = -2407
116990 meter/sec
ZDOT = -16312
511243 ZDOT = -4946
208034
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4916867
43 X = -1498661
19
Y = 19279457
33 feet Y = 5876378
59 meter
Z = 9944344
82 Z = 3031036
30
XDOT = -17521
040642 XDOT = -5340
413188
YDOT = 3929
895769 feet/sec YDOT = 1197
832230 meter/sec
ZDOT = -16197
471187 ZDOT = -4936
989218
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 17297
40993964
00016717 00000-0 10270-3 0 9164
2 25544 51
6407 114
1395 0005240 47
2417 312
9171 15
54240173 41848
Satellite: ISS
Catalog Number: 25544
Epoch time: 17297
40993964 = yrday
fracday
Element set: 916
Inclination: 51
6407 deg
RA of node: 114
1395 deg
Eccentricity:
0005240
Arg of perigee: 47
2417 deg
Mean anomaly: 312
9171 deg
Mean motion: 15
54240173 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4184
Checksum: 306
Coasting Arc #18 (Orbit 4198)
---------------------------------------
Vector Time (GMT): 2017/298/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -960545
89 A = 6788193
10 meter
Y = 6550940
15 meter E =
0013429
Z = -1475801
48 I = 52
01139
XDOT = -4971
077684 Wp = 42
83087
YDOT = 571
016072 meter/sec RA = 108
36653 deg
ZDOT = 5810
663110 TA = 301
14496
MA = 301
27660
Ha = 222
582 n
mi
Hp = 213
009
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3151397
27 X = -1026559
98
Y = 21492585
80 feet Y = 6539829
53 meter
Z = -4841868
36 Z = -1480628
11
XDOT = -16309
309988 XDOT = -5005
319450
YDOT = 1873
412310 feet/sec YDOT = 515
234765 meter/sec
ZDOT = 19063
855349 ZDOT = 5786
431441
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7936965
44 X = 2419187
07
Y = -20215093
04 feet Y = -6161560
36 meter
Z = -4864240
03 Z = -1482620
36
XDOT = 14954
685726 XDOT = 4558
188209
YDOT = 1342
077681 feet/sec YDOT = 409
065277 meter/sec
ZDOT = 18956
237020 ZDOT = 5777
861044
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 17298
37442099
00016717 00000-0 10270-3 0 9170
2 25544 51
6392 109
3310 0005173 50
8310 309
3302 15
54197227 41994
Satellite: ISS
Catalog Number: 25544
Epoch time: 17298
37442099 = yrday
fracday
Element set: 917
Inclination: 51
6392 deg
RA of node: 109
3310 deg
Eccentricity:
0005173
Arg of perigee: 50
8310 deg
Mean anomaly: 309
3302 deg
Mean motion: 15
54197227 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4199
Checksum: 308
Coasting Arc #19 (Orbit 4214)
---------------------------------------
Vector Time (GMT): 2017/299/08:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1792930
86 A = 6789108
05 meter
Y = -6538162
06 meter E =
0013268
Z = -289928
04 I = 52
02445
XDOT = 4487
637835 Wp = 115
01556
YDOT = 1488
431210 meter/sec RA = 103
42196 deg
ZDOT = -6034
550685 TA = 68
09151
MA = 67
95050
Ha = 222
583 n
mi
Hp = 213
002
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5882319
11 X = 1867317
44
Y = -21450662
91 feet Y = -6517696
36 meter
Z = -951207
47 Z = -281037
55
XDOT = 14723
221245 XDOT = 4499
973732
YDOT = 4883
304494 feet/sec YDOT = 1538
683887 meter/sec
ZDOT = -19798
394637 ZDOT = -6012
720773
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10285750
13 X = -3135096
64
Y = 19723367
49 feet Y = 6011682
41 meter
Z = -910786
51 Z = -277607
73
XDOT = -12048
670447 XDOT = -3672
434752
YDOT = -7158
246965 feet/sec YDOT = -2181
833675 meter/sec
ZDOT = -19701
729737 ZDOT = -6005
087224
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 17299
40319812
00016717 00000-0 10270-3 0 9182
2 25544 51
6399 104
2021 0005005 55
7627 304
3999 15
54192270 42152
Satellite: ISS
Catalog Number: 25544
Epoch time: 17299
40319812 = yrday
fracday
Element set: 918
Inclination: 51
6399 deg
RA of node: 104
2021 deg
Eccentricity:
0005005
Arg of perigee: 55
7627 deg
Mean anomaly: 304
3999 deg
Mean motion: 15
54192270 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4215
Checksum: 308
Coasting Arc #20 (Orbit 4216)
---------------------------------------
Vector Time (GMT): 2017/299/12:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 920119
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2907881
27 A = 6787334
80 meter
Y = -5802210
61 meter E =
0009174
Z = -1988508
70 I = 52
01776
XDOT = 3642
655501 Wp = 106
55704
YDOT = 3739
740744 meter/sec RA = 102
77769 deg
ZDOT = -5609
165706 TA = 95
26146
MA = 95
15677
Ha = 222
585 n
mi
Hp = 212
844
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9540292
87 X = 2982206
40
Y = -19036124
06 feet Y = -5769277
16 meter
Z = -6523978
68 Z = -1974202
19
XDOT = 11950
969493 XDOT = 3627
813094
YDOT = 12269
490631 feet/sec YDOT = 3780
392297 meter/sec
ZDOT = -18402
774625 ZDOT = -5591
506602
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3230293
34 X = 984593
41
Y = 21066369
61 feet Y = 6421029
46 meter
Z = -6459627
04 Z = -1968894
32
XDOT = -15412
236666 XDOT = -4697
649736
YDOT = -3231
444324 feet/sec YDOT = -984
944230 meter/sec
ZDOT = -18324
952464 ZDOT = -5585
445511
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 17299
53179500
00016717 00000-0 10270-3 0 9195
2 25544 51
6376 103
5564 0005160 59
0881 301
0778 15
54247254 42176
Satellite: ISS
Catalog Number: 25544
Epoch time: 17299
53179500 = yrday
fracday
Element set: 919
Inclination: 51
6376 deg
RA of node: 103
5564 deg
Eccentricity:
0005160
Arg of perigee: 59
0881 deg
Mean anomaly: 301
0778 deg
Mean motion: 15
54247254 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4217
Checksum: 315
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list