[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 25th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15282 6 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 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
057/02:24:45
635 -2
9 2
9 2
9
N/A -0
0 -0
3 224
4
000/00:07:31
270 -0
3 -0
2 215
6
057/14:52:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
3
000/00:00:00
000 0
0 0
0 215
6
060/17:27:30
000 0
0 0
0 0
0
N/A 0
0 0
0 224
7
000/00:00:00
000 0
0 0
0 215
5
061/07:48:58
000 0
0 0
0 0
0
N/A 0
0 0
0 224
3
000/00:00:00
000 0
0 0
0 215
6
062/10:55:42
000 0
0 0
0 0
0
N/A 0
0 0
0 224
5
000/00:00:00
000 0
0 0
0 215
5
066/23:27:30
000 0
0 0
0 0
0
N/A 0
0 0
0 224
6
000/00:00:00
000 0
0 0
0 215
4
067/07:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
5
000/00:00:00
000 0
0 0
0 215
4
Coasting Arc #1 (Orbit 3790)
---------------------------------------
Vector Time (GMT): 2019/056/13:50:53
514
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4966117
14 A = 6788437
48 meter
Y = 3663737
46 meter E =
0009207
Z = -2835769
48 I = 51
54447
XDOT = -4983
875685 Wp = 90
95418
YDOT = 2837
378710 meter/sec RA = 195
01487 deg
ZDOT = -5076
596165 TA = 121
26703
MA = 121
17682
Ha = 224
305 n
mi
Hp = 214
121
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16293035
22 X = 4938553
54
Y = 12020136
04 feet Y = 3719117
75 meter
Z = -9303705
66 Z = -2811713
41
XDOT = -16351
298179 XDOT = -4990
574640
YDOT = 9308
985269 feet/sec YDOT = 2781
607747 meter/sec
ZDOT = -16655
499229 ZDOT = -5100
822141
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16759771
50 X = 5108378
35
Y = 11448215
80 feet Y = 3489416
18 meter
Z = -9195326
01 Z = -2802735
37
XDOT = -15073
975635 XDOT = -4594
547774
YDOT = 8640
328407 feet/sec YDOT = 2633
572099 meter/sec
ZDOT = -16765
136699 ZDOT = -5110
013666
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 19056
60355319
00016717 00000-0 10270-3 0 9000
2 25544 51
6395 196
0383 0005600 66
1327 294
0412 15
53290581 37918
Satellite: ISS
Catalog Number: 25544
Epoch time: 19056
60355319 = yrday
fracday
Element set: 900
Inclination: 51
6395 deg
RA of node: 196
0383 deg
Eccentricity:
0005600
Arg of perigee: 66
1327 deg
Mean anomaly: 294
0412 deg
Mean motion: 15
53290581 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3791
Checksum: 302
Coasting Arc #2 (Orbit 3798)
---------------------------------------
Vector Time (GMT): 2019/057/02:28:31
270
Vector Time (MET): N/A
Weight (LBS) : 900442
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1601275
07 A = 6781509
48 meter
Y = 3950946
41 meter E =
0017609
Z = -5289118
82 I = 51
53279
XDOT = -7325
616691 Wp = 86
76794
YDOT = -2122
681361 meter/sec RA = 192
36682 deg
ZDOT = 634
991565 TA = 189
29867
MA = 189
33132
Ha = 224
372 n
mi
Hp = 215
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5253527
15 X = -1619645
37
Y = 12962422
60 feet Y = 3932936
82 meter
Z = -17352752
02 Z = -5296941
96
XDOT = -24034
175496 XDOT = -7304
420217
YDOT = -6964
177692 feet/sec YDOT = -2204
482970 meter/sec
ZDOT = 2083
305661 ZDOT = 599
458494
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2353633
72 X = 717387
56
Y = -13742137
24 feet Y = -4188603
43 meter
Z = -17388387
57 Z = -5299980
53
XDOT = 23964
774984 XDOT = 7304
463415
YDOT = 1682
900886 feet/sec YDOT = 512
948190 meter/sec
ZDOT = 1922
958919 ZDOT = 586
117879
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 19057
11825022
00016717 00000-0 10270-3 0 9011
2 25544 51
6392 193
4788 0003728 51
9655 308
1833 15
52743342 37999
Satellite: ISS
Catalog Number: 25544
Epoch time: 19057
11825022 = yrday
fracday
Element set: 901
Inclination: 51
6392 deg
RA of node: 193
4788 deg
Eccentricity:
0003728
Arg of perigee: 51
9655 deg
Mean anomaly: 308
1833 deg
Mean motion: 15
52743342 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3799
Checksum: 324
Coasting Arc #3 (Orbit 3806)
---------------------------------------
Vector Time (GMT): 2019/057/14:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 900442
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2322721
01 A = 6782014
87 meter
Y = 3757223
05 meter E =
0016500
Z = -5160728
88 I = 51
55215
XDOT = -7119
264103 Wp = 93
14346
YDOT = -2402
743935 meter/sec RA = 189
78674 deg
ZDOT = 1458
067806 TA = 190
91640
MA = 190
95225
Ha = 224
288 n
mi
Hp = 215
641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7620475
76 X = -2339495
08
Y = 12326847
28 feet Y = 3731154
71 meter
Z = -16931525
19 Z = -5172052
57
XDOT = -23357
165692 XDOT = -7098
949220
YDOT = -7883
018161 feet/sec YDOT = -2482
242857 meter/sec
ZDOT = 4783
687026 ZDOT = 1423
534997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3261814
05 X = -994200
92
Y = 14058411
68 feet Y = 4285003
88 meter
Z = -16982961
76 Z = -5176406
74
XDOT = -23655
680672 XDOT = -7210
251469
YDOT = 89
576981 feet/sec YDOT = 27
303064 meter/sec
ZDOT = 4627
867988 ZDOT = 1410
574163
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 19057
63312495
00016717 00000-0 10270-3 0 9024
2 25544 51
6399 190
9152 0003414 58
0355 302
1129 15
52756245 38078
Satellite: ISS
Catalog Number: 25544
Epoch time: 19057
63312495 = yrday
fracday
Element set: 902
Inclination: 51
6399 deg
RA of node: 190
9152 deg
Eccentricity:
0003414
Arg of perigee: 58
0355 deg
Mean anomaly: 302
1129 deg
Mean motion: 15
52756245 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3807
Checksum: 306
Coasting Arc #4 (Orbit 3822)
---------------------------------------
Vector Time (GMT): 2019/058/14:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 900442
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3461294
49 A = 6783804
55 meter
Y = -3448598
41 meter E =
0011280
Z = 4699757
90 I = 51
59175
XDOT = 6579
672383 Wp = 62
30389
YDOT = 2777
878048 meter/sec RA = 184
79903 deg
ZDOT = -2797
185997 TA = 55
48461
MA = 55
37815
Ha = 224
204 n
mi
Hp = 215
658
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11355953
05 X = 3476771
98
Y = -11314299
25 feet Y = -3409805
05 meter
Z = 15419153
21 Z = 4716609
06
XDOT = 21586
851649 XDOT = 6561
707323
YDOT = 9113
773123 feet/sec YDOT = 2851
355968 meter/sec
ZDOT = -9177
119413 ZDOT = -2765
268661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6889311
45 X = 2099862
13
Y = -14392593
14 feet Y = -4386862
39 meter
Z = 15495546
89 Z = 4723042
69
XDOT = 22392
842440 XDOT = 6825
338376
YDOT = 957
311561 feet/sec YDOT = 291
788564 meter/sec
ZDOT = -9033
121830 ZDOT = -2753
295534
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 19058
66287484
00016717 00000-0 10270-3 0 9038
2 25544 51
6403 185
7920 0003477 59
7072 300
4424 15
52775995 38232
Satellite: ISS
Catalog Number: 25544
Epoch time: 19058
66287484 = yrday
fracday
Element set: 903
Inclination: 51
6403 deg
RA of node: 185
7920 deg
Eccentricity:
0003477
Arg of perigee: 59
7072 deg
Mean anomaly: 300
4424 deg
Mean motion: 15
52775995 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3823
Checksum: 334
Coasting Arc #5 (Orbit 3837)
---------------------------------------
Vector Time (GMT): 2019/059/14:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 900442
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4464516
29 A = 6786387
77 meter
Y = 3185578
11 meter E =
0009958
Z = -4006109
24 I = 51
63235
XDOT = -5767
845485 Wp = 94
63908
YDOT = -3115
465474 meter/sec RA = 179
81980 deg
ZDOT = 3958
195956 TA = 216
57008
MA = 216
63811
Ha = 224
326 n
mi
Hp = 215
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14647363
16 X = -4480347
42
Y = 10451371
74 feet Y = 3135564
07 meter
Z = -13143403
01 Z = -4027834
38
XDOT = -18923
377574 XDOT = -5751
805163
YDOT = -10221
343419 feet/sec YDOT = -3179
875691 meter/sec
ZDOT = 12986
207206 ZDOT = 3930
217531
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10041509
53 X = -3060652
11
Y = 14844122
08 feet Y = 4524488
41 meter
Z = -13241812
09 Z = -4036104
32
XDOT = -20290
017066 XDOT = -6184
397202
YDOT = -2275
983611 feet/sec YDOT = -693
719805 meter/sec
ZDOT = 12860
011237 ZDOT = 3919
731425
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 19059
62826543
00016717 00000-0 10270-3 0 9041
2 25544 51
6390 180
9906 0003527 65
4234 294
7286 15
52772269 38386
Satellite: ISS
Catalog Number: 25544
Epoch time: 19059
62826543 = yrday
fracday
Element set: 904
Inclination: 51
6390 deg
RA of node: 180
9906 deg
Eccentricity:
0003527
Arg of perigee: 65
4234 deg
Mean anomaly: 294
7286 deg
Mean motion: 15
52772269 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3838
Checksum: 341
Coasting Arc #6 (Orbit 3853)
---------------------------------------
Vector Time (GMT): 2019/060/14:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 900442
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5319599
04 A = 6789241
76 meter
Y = -2900026
88 meter E =
0016171
Z = 3049612
01 I = 51
67561
XDOT = 4735
518546 Wp = 89
91756
YDOT = 3482
555231 meter/sec RA = 174
84725 deg
ZDOT = -4926
073696 TA = 55
11616
MA = 54
96426
Ha = 224
293 n
mi
Hp = 215
564
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17452752
76 X = 5336819
59
Y = -9514523
90 feet Y = -2840442
97 meter
Z = 10005288
76 Z = 3075494
06
XDOT = 15536
478169 XDOT = 4720
151311
YDOT = 11425
706137 feet/sec YDOT = 3535
424939 meter/sec
ZDOT = -16161
659106 ZDOT = -4903
108299
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12758339
43 X = 3888741
86
Y = -15165446
76 feet Y = -4622428
17 meter
Z = 10122477
31 Z = 3085331
08
XDOT = 17614
367200 XDOT = 5368
859123
YDOT = 4051
312376 feet/sec YDOT = 1234
840012 meter/sec
ZDOT = -16058
126528 ZDOT = -4894
516966
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 19060
65801235
00016717 00000-0 10270-3 0 9058
2 25544 51
6395 175
8677 0003523 66
4043 293
7479 15
52773750 38541
Satellite: ISS
Catalog Number: 25544
Epoch time: 19060
65801235 = yrday
fracday
Element set: 905
Inclination: 51
6395 deg
RA of node: 175
8677 deg
Eccentricity:
0003523
Arg of perigee: 66
4043 deg
Mean anomaly: 293
7479 deg
Mean motion: 15
52773750 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3854
Checksum: 333
Coasting Arc #7 (Orbit 3855)
---------------------------------------
Vector Time (GMT): 2019/060/17:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 900442
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6113169
80 A = 6790706
28 meter
Y = -1432383
43 meter E =
0017616
Z = 2564535
17 I = 51
68240
XDOT = 3277
835104 Wp = 74
14758
YDOT = -4508
699643 meter/sec RA = 174
35624 deg
ZDOT = 5269
832272 TA = 314
66453
MA = 314
80797
Ha = 224
655 n
mi
Hp = 215
539
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20056331
36 X = -6109154
97
Y = -4699420
69 feet Y = -1500722
58 meter
Z = 8413829
31 Z = 2534850
14
XDOT = 10754
052177 XDOT = 3302
411665
YDOT = -14792
321662 feet/sec YDOT = -4471
906918 meter/sec
ZDOT = 17289
475957 ZDOT = 5285
814348
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14067595
85 X = -4287803
21
Y = 15122222
39 feet Y = 4609253
39 meter
Z = 8279773
12 Z = 2523674
85
XDOT = -6451
272556 XDOT = -1966
347875
YDOT = -15553
828819 feet/sec YDOT = -4740
807024 meter/sec
ZDOT = 17362
042342 ZDOT = 5291
950506
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 19060
78673245
00016717 00000-0 10270-3 0 9061
2 25544 51
6385 175
2278 0003982 66
8265 293
3306 15
52729623 38567
Satellite: ISS
Catalog Number: 25544
Epoch time: 19060
78673245 = yrday
fracday
Element set: 906
Inclination: 51
6385 deg
RA of node: 175
2278 deg
Eccentricity:
0003982
Arg of perigee: 66
8265 deg
Mean anomaly: 293
3306 deg
Mean motion: 15
52729623 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3856
Checksum: 342
Coasting Arc #8 (Orbit 3864)
---------------------------------------
Vector Time (GMT): 2019/061/07:48:58
000
Vector Time (MET): N/A
Weight (LBS) : 900442
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4327199
29 A = 6787336
01 meter
Y = -3646437
22 meter E =
0014997
Z = 3737274
21 I = 51
68942
XDOT = 5841
513226 Wp = 80
48470
YDOT = 2529
086549 meter/sec RA = 171
33201 deg
ZDOT = -4278
913652 TA = 54
90013
MA = 54
75962
Ha = 224
337 n
mi
Hp = 215
597
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14196848
06 X = 4349499
98
Y = -11963376
70 feet Y = -3597922
55 meter
Z = 12261398
32 Z = 3758348
02
XDOT = 19165
069639 XDOT = 5833
582240
YDOT = 8297
528049 feet/sec YDOT = 2594
365842 meter/sec
ZDOT = -14038
430616 ZDOT = -4250
557811
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13411538
52 X = 4087836
94
Y = 12745662
52 feet Y = 3884877
94 meter
Z = 12356920
60 Z = 3766389
40
XDOT = -5247
191170 XDOT = -1599
343868
YDOT = 19061
354279 feet/sec YDOT = 5809
900784 meter/sec
ZDOT = -13910
451431 ZDOT = -4239
905596
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 19061
36596211
00016717 00000-0 10270-3 0 9074
2 25544 51
6365 172
3432 0003529 68
6224 291
5305 15
52748085 38659
Satellite: ISS
Catalog Number: 25544
Epoch time: 19061
36596211 = yrday
fracday
Element set: 907
Inclination: 51
6365 deg
RA of node: 172
3432 deg
Eccentricity:
0003529
Arg of perigee: 68
6224 deg
Mean anomaly: 291
5305 deg
Mean motion: 15
52748085 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3865
Checksum: 317
Coasting Arc #9 (Orbit 3879)
---------------------------------------
Vector Time (GMT): 2019/062/07:48:58
000
Vector Time (MET): N/A
Weight (LBS) : 900442
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5129273
48 A = 6789987
67 meter
Y = 3487914
95 meter E =
0008442
Z = -2764048
47 I = 51
73175
XDOT = -4811
364126 Wp = 66
96599
YDOT = -3009
996482 meter/sec RA = 166
36466 deg
ZDOT = 5145
953124 TA = 261
80711
MA = 261
90287
Ha = 224
471 n
mi
Hp = 215
417
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16828325
08 X = -5154469
22
Y = 11443290
52 feet Y = 3430414
76 meter
Z = -9068400
49 Z = -2789025
41
XDOT = -15785
315373 XDOT = -4802
343505
YDOT = -9875
316542 feet/sec YDOT = -3063
749715 meter/sec
ZDOT = 16883
048307 ZDOT = 5122
603994
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13443690
49 X = -4097636
86
Y = -15209974
29 feet Y = -4636000
16 meter
Z = -9181567
32 Z = -2798541
72
XDOT = 6706
117286 XDOT = 2044
024549
YDOT = -16024
536052 feet/sec YDOT = -4884
278589 meter/sec
ZDOT = 16777
719083 ZDOT = 5113
848777
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 19062
33134642
00016717 00000-0 10270-3 0 9089
2 25544 51
6371 167
5404 0003786 74
6961 285
4609 15
52761382 38802
Satellite: ISS
Catalog Number: 25544
Epoch time: 19062
33134642 = yrday
fracday
Element set: 908
Inclination: 51
6371 deg
RA of node: 167
5404 deg
Eccentricity:
0003786
Arg of perigee: 74
6961 deg
Mean anomaly: 285
4609 deg
Mean motion: 15
52761382 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3880
Checksum: 325
Coasting Arc #10 (Orbit 3881)
---------------------------------------
Vector Time (GMT): 2019/062/10:55:42
000
Vector Time (MET): N/A
Weight (LBS) : 935659
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5468448
24 A = 6790997
74 meter
Y = 3284809
45 meter E =
0009054
Z = -2326797
31 I = 51
74189
XDOT = -4287
552082 Wp = 57
46197
YDOT = -3315
766071 meter/sec RA = 165
72346 deg
ZDOT = 5415
761152 TA = 276
66427
MA = 276
76731
Ha = 224
452 n
mi
Hp = 215
511
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17941103
16 X = -5493471
47
Y = 10776933
91 feet Y = 3223517
36 meter
Z = -7633849
45 Z = -2353421
37
XDOT = -14066
771923 XDOT = -4276
461734
YDOT = -10878
497608 feet/sec YDOT = -3363
650069 meter/sec
ZDOT = 17768
245249 ZDOT = 5394
961501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20806360
91 X = -6341778
80
Y = -1806933
64 feet Y = -550753
37 meter
Z = -7754449
11 Z = -2363556
09
XDOT = -5206
211247 XDOT = -1586
853188
YDOT = -15623
070868 feet/sec YDOT = -4761
912001 meter/sec
ZDOT = 17674
461873 ZDOT = 5387
175979
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 19062
46006399
00016717 00000-0 10270-3 0 9091
2 25544 51
6399 166
9006 0003651 74
4508 285
7047 15
52740394 38820
Satellite: ISS
Catalog Number: 25544
Epoch time: 19062
46006399 = yrday
fracday
Element set: 909
Inclination: 51
6399 deg
RA of node: 166
9006 deg
Eccentricity:
0003651
Arg of perigee: 74
4508 deg
Mean anomaly: 285
7047 deg
Mean motion: 15
52740394 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3882
Checksum: 335
Coasting Arc #11 (Orbit 3897)
---------------------------------------
Vector Time (GMT): 2019/063/10:55:42
000
Vector Time (MET): N/A
Weight (LBS) : 935659
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5980726
35 A = 6792781
51 meter
Y = -3009536
97 meter E =
0016547
Z = 1106449
83 I = 51
77948
XDOT = 3040
278460 Wp = 114
66275
YDOT = 3852
950566 meter/sec RA = 160
76597 deg
ZDOT = -5891
326501 TA = 53
35927
MA = 53
20724
Ha = 224
469 n
mi
Hp = 215
492
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19621805
60 X = 6008560
95
Y = -9873808
94 feet Y = -2942500
57 meter
Z = 3630084
73 Z = 1135569
14
XDOT = 9974
666863 XDOT = 3025
583844
YDOT = 12640
913929 feet/sec YDOT = 3886
866397 meter/sec
ZDOT = -19328
499019 ZDOT = -5876
594347
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21713915
76 X = 6618401
52
Y = 3168342
21 feet Y = 965710
71 meter
Z = 3761960
01 Z = 1146645
41
XDOT = 1245
980540 XDOT = 379
774868
YDOT = 14566
397204 feet/sec YDOT = 4439
837868 meter/sec
ZDOT = -19262
174897 ZDOT = -5871
110909
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 19063
48980439
00016717 00000-0 10270-3 0 9102
2 25544 51
6396 161
7781 0003606 81
2981 278
8579 15
52751578 38987
Satellite: ISS
Catalog Number: 25544
Epoch time: 19063
48980439 = yrday
fracday
Element set: 910
Inclination: 51
6396 deg
RA of node: 161
7781 deg
Eccentricity:
0003606
Arg of perigee: 81
2981 deg
Mean anomaly: 278
8579 deg
Mean motion: 15
52751578 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3898
Checksum: 363
Coasting Arc #12 (Orbit 3913)
---------------------------------------
Vector Time (GMT): 2019/064/10:55:42
000
Vector Time (MET): N/A
Weight (LBS) : 935659
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6230914
54 A = 6793298
94 meter
Y = 2687582
54 meter E =
0015405
Z = 128762
06 I = 51
81387
XDOT = -1763
955763 Wp = 54
75211
YDOT = -4402
113136 meter/sec RA = 155
81285 deg
ZDOT = 6024
413827 TA = 306
63096
MA = 306
77252
Ha = 224
470 n
mi
Hp = 215
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20442633
00 X = -6261130
20
Y = 8817528
01 feet Y = 2617735
16 meter
Z = 422447
72 Z = 98421
62
XDOT = -5787
256439 XDOT = -1743
861605
YDOT = -14442
628400 feet/sec YDOT = -4421
725942 meter/sec
ZDOT = 19765
137228 ZDOT = 6015
894643
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21876327
07 X = -6667904
49
Y = -4144099
54 feet Y = -1263121
54 meter
Z = 285059
88 Z = 86886
25
XDOT = 2880
894969 XDOT = 878
096787
YDOT = -13684
096451 feet/sec YDOT = -4170
912598 meter/sec
ZDOT = 19726
938963 ZDOT = 6012
770996
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 19064
51954157
00016717 00000-0 10270-3 0 9116
2 25544 51
6412 156
6559 0003669 81
9850 278
1718 15
52763463 39146
Satellite: ISS
Catalog Number: 25544
Epoch time: 19064
51954157 = yrday
fracday
Element set: 911
Inclination: 51
6412 deg
RA of node: 156
6559 deg
Eccentricity:
0003669
Arg of perigee: 81
9850 deg
Mean anomaly: 278
1718 deg
Mean motion: 15
52763463 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3914
Checksum: 336
Coasting Arc #13 (Orbit 3928)
---------------------------------------
Vector Time (GMT): 2019/065/10:55:42
000
Vector Time (MET): N/A
Weight (LBS) : 935659
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6259348
07 A = 6792491
37 meter
Y = -2221071
43 meter E =
0011147
Z = -1409837
00 I = 51
84063
XDOT = 463
360967 Wp = 126
76060
YDOT = 4971
733070 meter/sec RA = 150
86166 deg
ZDOT = -5813
577930 TA = 68
55156
MA = 68
43271
Ha = 224
523 n
mi
Hp = 215
485
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20535918
86 X = 6290567
59
Y = -7286979
76 feet Y = -2150900
63 meter
Z = -4625449
49 Z = -1379355
95
XDOT = 1520
213146 XDOT = 435
969792
YDOT = 16311
460205 feet/sec YDOT = 4976
760865 meter/sec
ZDOT = -19073
418406 ZDOT = -5811
394247
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21211088
86 X = 6465139
88
Y = 5115795
03 feet Y = 1559294
33 meter
Z = -4487445
96 Z = -1367773
53
XDOT = -7146
111745 XDOT = -2178
134860
YDOT = 13020
336948 feet/sec YDOT = 3968
598702 meter/sec
ZDOT = -19063
909340 ZDOT = -5810
679567
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 19065
48491714
00016717 00000-0 10270-3 0 9129
2 25544 51
6407 151
8536 0003683 85
9588 274
1984 15
52767741 39290
Satellite: ISS
Catalog Number: 25544
Epoch time: 19065
48491714 = yrday
fracday
Element set: 912
Inclination: 51
6407 deg
RA of node: 151
8536 deg
Eccentricity:
0003683
Arg of perigee: 85
9588 deg
Mean anomaly: 274
1984 deg
Mean motion: 15
52767741 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3929
Checksum: 353
Coasting Arc #14 (Orbit 3944)
---------------------------------------
Vector Time (GMT): 2019/066/10:55:42
000
Vector Time (MET): N/A
Weight (LBS) : 935659
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6054566
38 A = 6790559
03 meter
Y = 1667618
59 meter E =
0017331
Z = 2563243
38 I = 51
86280
XDOT = 732
553530 Wp = 78
76025
YDOT = -5508
264024 meter/sec RA = 145
90972 deg
ZDOT = 5287
026349 TA = 309
95475
MA = 310
10687
Ha = 224
549 n
mi
Hp = 215
460
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19864062
94 X = -6085214
80
Y = 5471189
59 feet Y = 1599741
15 meter
Z = 8409591
14 Z = 2533758
39
XDOT = 2403
390846 XDOT = 768
413019
YDOT = -18071
732362 feet/sec YDOT = -5499
870934 meter/sec
ZDOT = 17345
886973 ZDOT = 5290
672546
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19783805
97 X = -6030104
06
Y = -5944997
20 feet Y = -1812035
15 meter
Z = 8276120
15 Z = 2522561
42
XDOT = 11103
072928 XDOT = 3384
216628
YDOT = -12652
886965 feet/sec YDOT = -3856
599947 meter/sec
ZDOT = 17362
785565 ZDOT = 5292
177040
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 19066
51464892
00016717 00000-0 10270-3 0 9132
2 25544 51
6408 146
7316 0003725 88
3848 271
7731 15
52781088 39454
Satellite: ISS
Catalog Number: 25544
Epoch time: 19066
51464892 = yrday
fracday
Element set: 913
Inclination: 51
6408 deg
RA of node: 146
7316 deg
Eccentricity:
0003725
Arg of perigee: 88
3848 deg
Mean anomaly: 271
7731 deg
Mean motion: 15
52781088 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3945
Checksum: 340
Coasting Arc #15 (Orbit 3952)
---------------------------------------
Vector Time (GMT): 2019/066/23:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 935659
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4271789
40 A = 6782822
20 meter
Y = -1696823
43 meter E =
0009587
Z = 4981079
06 I = 51
85070
XDOT = 4745
030962 Wp = 108
59037
YDOT = -5634
035497 meter/sec RA = 143
31925 deg
ZDOT = 2143
745653 TA = 320
56057
MA = 320
63032
Ha = 224
629 n
mi
Hp = 215
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14015057
10 X = -4276692
54
Y = -5567005
99 feet Y = -1744620
34 meter
Z = 16342122
90 Z = 4960316
91
XDOT = 15567
686883 XDOT = 4797
266700
YDOT = -18484
368428 feet/sec YDOT = -5580
680902 meter/sec
ZDOT = 7033
286264 ZDOT = 2166
922499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10710642
64 X = 3264603
88
Y = 10758795
99 feet Y = 3279281
02 meter
Z = 16248347
77 Z = 4952496
40
XDOT = -20841
493558 XDOT = -6352
487237
YDOT = 9935
672887 feet/sec YDOT = 3028
393096 meter/sec
ZDOT = 7138
529484 ZDOT = 2175
823787
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 19067
02951515
00016717 00000-0 10270-3 0 9143
2 25544 51
6402 144
1735 0003784 83
9294 276
2289 15
52787597 39534
Satellite: ISS
Catalog Number: 25544
Epoch time: 19067
02951515 = yrday
fracday
Element set: 914
Inclination: 51
6402 deg
RA of node: 144
1735 deg
Eccentricity:
0003784
Arg of perigee: 83
9294 deg
Mean anomaly: 276
2289 deg
Mean motion: 15
52787597 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3953
Checksum: 341
Coasting Arc #16 (Orbit 3957)
---------------------------------------
Vector Time (GMT): 2019/067/07:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 910211
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5924046
28 A = 6790832
41 meter
Y = 2264583
37 meter E =
0017376
Z = 2406632
20 I = 51
88370
XDOT = 110
015073 Wp = 77
85323
YDOT = -5463
054745 meter/sec RA = 141
75926 deg
ZDOT = 5382
229805 TA = 308
95088
MA = 309
10560
Ha = 224
524 n
mi
Hp = 215
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19435847
38 X = -5960619
15
Y = 7429735
48 feet Y = 2198132
36 meter
Z = 7895774
95 Z = 2377766
66
XDOT = 360
941840 XDOT = 144
952762
YDOT = -17923
407957 feet/sec YDOT = -5461
628443 meter/sec
ZDOT = 17658
234269 ZDOT = 5382
849765
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7367039
05 X = -2245473
50
Y = -19512229
95 feet Y = -5947327
69 meter
Z = 7765050
73 Z = 2366787
46
XDOT = 16498
496488 XDOT = 5028
741730
YDOT = 838
085427 feet/sec YDOT = 255
448438 meter/sec
ZDOT = 17661
447615 ZDOT = 5383
209233
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 19067
35130506
00016717 00000-0 10270-3 0 9159
2 25544 51
6380 142
5676 0003752 92
7274 267
4307 15
52798109 39585
Satellite: ISS
Catalog Number: 25544
Epoch time: 19067
35130506 = yrday
fracday
Element set: 915
Inclination: 51
6380 deg
RA of node: 142
5676 deg
Eccentricity:
0003752
Arg of perigee: 92
7274 deg
Mean anomaly: 267
4307 deg
Mean motion: 15
52798109 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3958
Checksum: 328
Coasting Arc #17 (Orbit 3972)
---------------------------------------
Vector Time (GMT): 2019/068/07:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 910211
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5624075
45 A = 6788207
01 meter
Y = -1529869
68 meter E =
0008741
Z = -3487166
49 I = 51
90066
XDOT = -1187
191204 Wp = 91
14474
YDOT = 6029
828850 meter/sec RA = 136
80550 deg
ZDOT = -4570
120151 TA = 129
58025
MA = 129
50301
Ha = 224
540 n
mi
Hp = 215
488
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18451691
11 X = 5657703
47
Y = -5019257
48 feet Y = -1466789
75 meter
Z = -11440834
94 Z = -3459765
21
XDOT = -3894
984265 XDOT = -1232
331303
YDOT = 19782
903052 feet/sec YDOT = 6016
299881 meter/sec
ZDOT = -14993
832518 ZDOT = -4575
997423
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5278170
91 X = 1608786
49
Y = 18455948
07 feet Y = 5625372
97 meter
Z = -11316777
26 Z = -3449353
71
XDOT = -18487
119157 XDOT = -5634
873919
YDOT = -3902
931641 feet/sec YDOT = -1189
613564 meter/sec
ZDOT = -15020
876217 ZDOT = -4578
363071
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 19068
31667550
00016717 00000-0 10270-3 0 9161
2 25544 51
6384 137
7645 0003809 93
8284 266
3303 15
52783989 39738
Satellite: ISS
Catalog Number: 25544
Epoch time: 19068
31667550 = yrday
fracday
Element set: 916
Inclination: 51
6384 deg
RA of node: 137
7645 deg
Eccentricity:
0003809
Arg of perigee: 93
8284 deg
Mean anomaly: 266
3303 deg
Mean motion: 15
52783989 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3973
Checksum: 353
Coasting Arc #18 (Orbit 3988)
---------------------------------------
Vector Time (GMT): 2019/069/07:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 910211
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5171677
27 A = 6785352
20 meter
Y = 689288
01 meter E =
0013567
Z = 4329047
05 I = 51
91485
XDOT = 2097
263021 Wp = 105
04038
YDOT = -6482
360040 meter/sec RA = 131
84821 deg
ZDOT = 3525
009914 TA = 309
17987
MA = 309
30030
Ha = 224
588 n
mi
Hp = 215
388
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16967445
12 X = -5200028
72
Y = 2261443
61 feet Y = 631296
68 meter
Z = 14202910
25 Z = 4303856
16
XDOT = 6880
784188 XDOT = 2152
472275
YDOT = -21267
585434 feet/sec YDOT = -6458
597875 meter/sec
ZDOT = 11564
993155 ZDOT = 3535
332426
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2792898
04 X = -851275
32
Y = -16983328
58 feet Y = -5176518
55 meter
Z = 14088905
27 Z = 4294298
33
XDOT = 20230
016104 XDOT = 6166
108909
YDOT = 6340
978423 feet/sec YDOT = 1932
730223 meter/sec
ZDOT = 11612
192431 ZDOT = 3539
396253
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 19069
34640005
00016717 00000-0 10270-3 0 9172
2 25544 51
6384 132
6416 0003783 98
1363 262
0218 15
52808001 39893
Satellite: ISS
Catalog Number: 25544
Epoch time: 19069
34640005 = yrday
fracday
Element set: 917
Inclination: 51
6384 deg
RA of node: 132
6416 deg
Eccentricity:
0003783
Arg of perigee: 98
1363 deg
Mean anomaly: 262
0218 deg
Mean motion: 15
52808001 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3989
Checksum: 309
Coasting Arc #19 (Orbit 4003)
---------------------------------------
Vector Time (GMT): 2019/070/07:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 910211
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4630945
18 A = 6782982
07 meter
Y = 303479
38 meter E =
0015652
Z = -4961048
93 I = 51
92782
XDOT = -2850
415873 Wp = 80
19333
YDOT = 6737
099968 meter/sec RA = 126
88734 deg
ZDOT = -2252
077208 TA = 167
87825
MA = 167
84054
Ha = 224
499 n
mi
Hp = 215
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15193389
71 X = 4651305
38
Y = 995667
27 feet Y = 355379
19 meter
Z = -16276407
26 Z = -4938504
17
XDOT = -9351
758114 XDOT = -2914
600869
YDOT = 22103
346353 feet/sec YDOT = 6704
865515 meter/sec
ZDOT = -7388
704752 ZDOT = -2266
080004
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -253637
19 X = -77308
62
Y = 15332154
39 feet Y = 4673240
66 meter
Z = -16174442
41 Z = -4929970
05
XDOT = -21408
684994 XDOT = -6525
367186
YDOT = -8204
149612 feet/sec YDOT = -2500
624802 meter/sec
ZDOT = -7452
590159 ZDOT = -2271
549480
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 19070
31176721
00016717 00000-0 10270-3 0 9181
2 25544 51
6381 127
8395 0003801 101
0139 259
1441 15
52784501 40040
Satellite: ISS
Catalog Number: 25544
Epoch time: 19070
31176721 = yrday
fracday
Element set: 918
Inclination: 51
6381 deg
RA of node: 127
8395 deg
Eccentricity:
0003801
Arg of perigee: 101
0139 deg
Mean anomaly: 259
1441 deg
Mean motion: 15
52784501 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4004
Checksum: 285
Coasting Arc #20 (Orbit 4019)
---------------------------------------
Vector Time (GMT): 2019/071/07:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 910211
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4026666
60 A = 6781419
72 meter
Y = -1354638
98 meter E =
0007011
Z = 5280447
43 I = 51
94314
XDOT = 3435
396418 Wp = 112
39759
YDOT = -6803
605104 meter/sec RA = 121
92262 deg
ZDOT = 870
790809 TA = 329
29321
MA = 329
33422
Ha = 224
530 n
mi
Hp = 215
410
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13210848
43 X = -4036868
82
Y = -4444353
61 feet Y = -1399724
58 meter
Z = 17324302
61 Z = 5260862
76
XDOT = 11270
985624 XDOT = 3506
991120
YDOT = -22321
539055 feet/sec YDOT = -6764
787715 meter/sec
ZDOT = 2856
925228 ZDOT = 887
653112
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3560503
39 X = 1085241
43
Y = -13588964
88 feet Y = -4141916
49 meter
Z = 17235808
81 Z = 5253474
52
XDOT = 22019
663961 XDOT = 6711
593575
YDOT = 9505
306748 feet/sec YDOT = 2897
217497 meter/sec
ZDOT = 2933
773465 ZDOT = 894
214152
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 19071
34148800
00016717 00000-0 10270-3 0 9193
2 25544 51
6392 122
7157 0003679 104
4506 255
7054 15
52820757 40204
Satellite: ISS
Catalog Number: 25544
Epoch time: 19071
34148800 = yrday
fracday
Element set: 919
Inclination: 51
6392 deg
RA of node: 122
7157 deg
Eccentricity:
0003679
Arg of perigee: 104
4506 deg
Mean anomaly: 255
7054 deg
Mean motion: 15
52820757 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4020
Checksum: 301
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