[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 19th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15403 1558 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
050/05:58:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
9
000/00:00:00
000 0
0 0
0 214
5
054/08:04:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
2
000/00:00:00
000 0
0 0
0 214
1
057/02:24:38
197 -2
8 2
8 2
8
N/A -0
0 -0
3 224
4
000/00:07:16
395 -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
6
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
5
062/10:55:42
000 0
0 0
0 0
0
N/A 0
0 0
0 224
4
000/00:00:00
000 0
0 0
0 215
5
Coasting Arc #1 (Orbit 3680)
---------------------------------------
Vector Time (GMT): 2019/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1900558
39 A = 6788364
37 meter
Y = 5865565
19 meter E =
0008014
Z = -2849572
46 I = 51
34539
XDOT = -5730
497433 Wp = 74
17926
YDOT = -589
862092 meter/sec RA = 230
35213 deg
ZDOT = -5045
935751 TA = 138
31475
MA = 138
25365
Ha = 224
051 n
mi
Hp = 214
515
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6235427
78 X = 1848667
95
Y = 19243980
30 feet Y = 5886528
34 meter
Z = -9348991
03 Z = -2840466
75
XDOT = -18800
844595 XDOT = -5698
965922
YDOT = -1935
243085 feet/sec YDOT = -653
768363 meter/sec
ZDOT = -16554
907320 ZDOT = -5073
694913
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5103671
76 X = -1555599
15
Y = 19593906
34 feet Y = 5972222
65 meter
Z = -9308401
55 Z = -2837200
79
XDOT = -13248
271307 XDOT = -4038
073094
YDOT = -11359
744957 feet/sec YDOT = -3462
450263 meter/sec
ZDOT = -16680
150836 ZDOT = -5084
109975
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 19049
52645881
00016717 00000-0 10270-3 0 9009
2 25544 51
6347 231
2748 0005718 39
0062 321
1502 15
53287921 36811
Satellite: ISS
Catalog Number: 25544
Epoch time: 19049
52645881 = yrday
fracday
Element set: 900
Inclination: 51
6347 deg
RA of node: 231
2748 deg
Eccentricity:
0005718
Arg of perigee: 39
0062 deg
Mean anomaly: 321
1502 deg
Mean motion: 15
53287921 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3681
Checksum: 304
Coasting Arc #2 (Orbit 3692)
---------------------------------------
Vector Time (GMT): 2019/050/05:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2506581
09 A = 6779922
77 meter
Y = -3467036
99 meter E =
0007015
Z = 5253805
86 I = 51
33749
XDOT = 5645
718657 Wp = 66
01658
YDOT = 5147
652613 meter/sec RA = 226
59465 deg
ZDOT = 705
478539 TA = 17
23284
MA = 17
20904
Ha = 223
911 n
mi
Hp = 214
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8223691
24 X = 2519644
90
Y = -11374793
26 feet Y = -3438933
32 meter
Z = 17236895
88 Z = 5266013
43
XDOT = 18522
699007 XDOT = 5584
309839
YDOT = 16888
624057 feet/sec YDOT = 5210
443661 meter/sec
ZDOT = 2314
562136 ZDOT = 732
753047
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5267885
36 X = 1605651
46
Y = 12936441
52 feet Y = 3943027
38 meter
Z = 17292294
92 Z = 5270691
49
XDOT = -23227
979145 XDOT = -7079
888043
YDOT = 6209
824184 feet/sec YDOT = 1892
754411 meter/sec
ZDOT = 2437
242771 ZDOT = 742
871597
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 19050
29850955
00016717 00000-0 10270-3 0 9016
2 25544 51
6385 227
4343 0005661 40
0533 320
1036 15
53305162 36935
Satellite: ISS
Catalog Number: 25544
Epoch time: 19050
29850955 = yrday
fracday
Element set: 901
Inclination: 51
6385 deg
RA of node: 227
4343 deg
Eccentricity:
0005661
Arg of perigee: 40
0533 deg
Mean anomaly: 320
1036 deg
Mean motion: 15
53305162 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3693
Checksum: 285
Coasting Arc #3 (Orbit 3707)
---------------------------------------
Vector Time (GMT): 2019/051/05:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3550031
96 A = 6780051
45 meter
Y = 2454612
36 meter E =
0018525
Z = -5244515
48 I = 51
36283
XDOT = -5177
973961 Wp = 82
51417
YDOT = -5563
136145 meter/sec RA = 221
58331 deg
ZDOT = 906
376870 TA = 196
17616
MA = 196
23537
Ha = 224
119 n
mi
Hp = 214
232
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11647086
50 X = -3551742
08
Y = 8053190
17 feet Y = 2414903
42 meter
Z = -17206415
61 Z = -5261764
06
XDOT = -16988
103548 XDOT = -5119
783116
YDOT = -18251
759006 feet/sec YDOT = -5620
714424 meter/sec
ZDOT = 2973
677396 ZDOT = 881
366748
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -871361
47 X = -265590
98
Y = -14037683
58 feet Y = -4278685
96 meter
Z = -17284484
45 Z = -5268310
86
XDOT = 23413
727966 XDOT = 7136
504284
YDOT = -4955
757439 feet/sec YDOT = -1510
514867 meter/sec
ZDOT = 2861
227271 ZDOT = 872
102072
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 19051
26357124
00016717 00000-0 10270-3 0 9025
2 25544 51
6398 222
6292 0005800 43
3373 316
8234 15
53290395 37082
Satellite: ISS
Catalog Number: 25544
Epoch time: 19051
26357124 = yrday
fracday
Element set: 902
Inclination: 51
6398 deg
RA of node: 222
6292 deg
Eccentricity:
0005800
Arg of perigee: 43
3373 deg
Mean anomaly: 316
8234 deg
Mean motion: 15
53290395 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3708
Checksum: 301
Coasting Arc #4 (Orbit 3723)
---------------------------------------
Vector Time (GMT): 2019/052/05:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4543809
91 A = 6781681
46 meter
Y = -1423631
63 meter E =
0012773
Z = 4822916
97 I = 51
39422
XDOT = 4437
072370 Wp = 53
78969
YDOT = 5749
393736 meter/sec RA = 216
57610 deg
ZDOT = -2471
193808 TA = 60
61837
MA = 60
49089
Ha = 224
008 n
mi
Hp = 214
247
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14907512
83 X = 4535965
18
Y = -4670707
43 feet Y = -1372862
92 meter
Z = 15823218
41 Z = 4844969
65
XDOT = 14557
324047 XDOT = 4384
454649
YDOT = 18862
840342 feet/sec YDOT = 5798
717715 meter/sec
ZDOT = -8107
591233 ZDOT = -2449
769107
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3458933
19 X = -1054282
84
Y = 15130131
13 feet Y = 4611663
97 meter
Z = 15922895
48 Z = 4853298
54
XDOT = -22558
762728 XDOT = -6875
910880
YDOT = 3315
018886 feet/sec YDOT = 1010
417756 meter/sec
ZDOT = -8011
320813 ZDOT = -2441
850584
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 19052
29296672
00016717 00000-0 10270-3 0 9030
2 25544 51
6398 217
5041 0005851 45
9800 314
1834 15
53320976 37240
Satellite: ISS
Catalog Number: 25544
Epoch time: 19052
29296672 = yrday
fracday
Element set: 903
Inclination: 51
6398 deg
RA of node: 217
5041 deg
Eccentricity:
0005851
Arg of perigee: 45
9800 deg
Mean anomaly: 314
1834 deg
Mean motion: 15
53320976 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3724
Checksum: 314
Coasting Arc #5 (Orbit 3738)
---------------------------------------
Vector Time (GMT): 2019/053/05:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5401936
78 A = 6784611
57 meter
Y = 501472
02 meter E =
0011522
Z = -4083170
19 I = 51
43141
XDOT = -3415
365952 Wp = 83
77603
YDOT = -5684
780701 meter/sec RA = 211
57666 deg
ZDOT = 3830
830219 TA = 225
94894
MA = 226
04390
Ha = 224
159 n
mi
Hp = 214
155
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17722889
69 X = -5387309
51
Y = 1645249
41 feet Y = 441145
12 meter
Z = -13396227
66 Z = -4109374
79
XDOT = -11205
268870 XDOT = -3370
150981
YDOT = -18650
855319 feet/sec YDOT = -5722
720470 meter/sec
ZDOT = 12568
340613 ZDOT = 3814
350425
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7223880
57 X = 2201838
80
Y = -16169048
01 feet Y = -4928325
83 meter
Z = -13514585
30 Z = -4119245
60
XDOT = 20610
950139 XDOT = 6282
217602
YDOT = -1206
089905 feet/sec YDOT = -367
616203 meter/sec
ZDOT = 12494
374092 ZDOT = 3808
285223
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 19053
25802585
00016717 00000-0 10270-3 0 9044
2 25544 51
6401 212
6996 0005776 49
2181 310
9472 15
53282192 37390
Satellite: ISS
Catalog Number: 25544
Epoch time: 19053
25802585 = yrday
fracday
Element set: 904
Inclination: 51
6401 deg
RA of node: 212
6996 deg
Eccentricity:
0005776
Arg of perigee: 49
2181 deg
Mean anomaly: 310
9472 deg
Mean motion: 15
53282192 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3739
Checksum: 318
Coasting Arc #6 (Orbit 3754)
---------------------------------------
Vector Time (GMT): 2019/054/05:58:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6070888
97 A = 6787855
07 meter
Y = 365986
43 meter E =
0017833
Z = 3001251
09 I = 51
47184
XDOT = 2127
329672 Wp = 83
74409
YDOT = 5465
282170 meter/sec RA = 206
58632 deg
ZDOT = -4942
377941 TA = 61
80715
MA = 61
62716
Ha = 224
211 n
mi
Hp = 214
114
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19917614
73 X = 6051767
01
Y = 1200742
89 feet Y = 433768
75 meter
Z = 9846624
31 Z = 3030694
27
XDOT = 6979
428059 XDOT = 2090
064209
YDOT = 17930
715780 feet/sec YDOT = 5488
862579 meter/sec
ZDOT = -16215
150724 ZDOT = -4932
135402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10503242
46 X = -3201388
30
Y = 16887855
38 feet Y = 5147418
32 meter
Z = 9979549
52 Z = 3041766
70
XDOT = -17910
747575 XDOT = -5459
195861
YDOT = -1532
412823 feet/sec YDOT = -467
079429 meter/sec
ZDOT = -16169
318742 ZDOT = -4928
408353
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 19054
28741967
00016717 00000-0 10270-3 0 9055
2 25544 51
6408 207
5747 0005871 53
5163 306
6529 15
53288711 37554
Satellite: ISS
Catalog Number: 25544
Epoch time: 19054
28741967 = yrday
fracday
Element set: 905
Inclination: 51
6408 deg
RA of node: 207
5747 deg
Eccentricity:
0005871
Arg of perigee: 53
5163 deg
Mean anomaly: 306
6529 deg
Mean motion: 15
53288711 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3755
Checksum: 333
Coasting Arc #7 (Orbit 3755)
---------------------------------------
Vector Time (GMT): 2019/054/08:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2186036
34 A = 6779801
54 meter
Y = 3636457
46 meter E =
0019581
Z = -5304702
70 I = 51
44543
XDOT = -6746
984757 Wp = 81
82737
YDOT = -3597
802561 meter/sec RA = 206
17047 deg
ZDOT = 317
774178 TA = 191
19453
MA = 191
23815
Ha = 224
196 n
mi
Hp = 214
102
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7172035
25 X = -2200770
84
Y = 11930634
72 feet Y = 3611928
75 meter
Z = -17403880
26 Z = -5315357
65
XDOT = -22135
776762 XDOT = -6707
795214
YDOT = -11803
814176 feet/sec YDOT = -3673
032904 meter/sec
ZDOT = 1042
566200 ZDOT = 285
095888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12287409
14 X = -3745202
31
Y = -6411781
07 feet Y = -1954310
87 meter
Z = -17452272
71 Z = -5319452
72
XDOT = 10143
287184 XDOT = 3091
673934
YDOT = -21842
020027 feet/sec YDOT = -6657
447704 meter/sec
ZDOT = 895
278939 ZDOT = 272
881021
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 19054
35175494
00016717 00000-0 10270-3 0 9060
2 25544 51
6387 207
2522 0005720 52
6294 307
5379 15
53299271 37563
Satellite: ISS
Catalog Number: 25544
Epoch time: 19054
35175494 = yrday
fracday
Element set: 906
Inclination: 51
6387 deg
RA of node: 207
2522 deg
Eccentricity:
0005720
Arg of perigee: 52
6294 deg
Mean anomaly: 307
5379 deg
Mean motion: 15
53299271 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3756
Checksum: 327
Coasting Arc #8 (Orbit 3771)
---------------------------------------
Vector Time (GMT): 2019/055/08:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3471536
46 A = 6780945
73 meter
Y = -2941796
14 meter E =
0011344
Z = 5021117
44 I = 51
47968
XDOT = 6225
746782 Wp = 56
44229
YDOT = 4051
128003 meter/sec RA = 201
16799 deg
ZDOT = -1921
623527 TA = 52
27963
MA = 52
17686
Ha = 224
138 n
mi
Hp = 214
141
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11389555
33 X = 3479784
94
Y = -9651562
15 feet Y = -2902928
44 meter
Z = 16473482
41 Z = 5038000
94
XDOT = 20425
678420 XDOT = 6189
317286
YDOT = 13291
102371 feet/sec YDOT = 4120
544797 meter/sec
ZDOT = -6304
539129 ZDOT = -1891
470376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10419393
30 X = 3175831
08
Y = 10572867
68 feet Y = 3222610
07 meter
Z = 16549953
39 Z = 5044425
79
XDOT = -11048
142544 XDOT = -3367
473847
YDOT = 20591
192877 feet/sec YDOT = 6276
195589 meter/sec
ZDOT = -6168
672090 ZDOT = -1880
211253
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 19055
38114524
00016717 00000-0 10270-3 0 9072
2 25544 51
6387 202
1269 0005731 56
3831 303
7867 15
53296011 37722
Satellite: ISS
Catalog Number: 25544
Epoch time: 19055
38114524 = yrday
fracday
Element set: 907
Inclination: 51
6387 deg
RA of node: 202
1269 deg
Eccentricity:
0005731
Arg of perigee: 56
3831 deg
Mean anomaly: 303
7867 deg
Mean motion: 15
53296011 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3772
Checksum: 308
Coasting Arc #9 (Orbit 3786)
---------------------------------------
Vector Time (GMT): 2019/056/08:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4630985
20 A = 6783443
62 meter
Y = 2300851
65 meter E =
0013579
Z = -4402425
46 I = 51
51768
XDOT = -5342
124802 Wp = 92
26189
YDOT = -4332
997673 meter/sec RA = 196
17190 deg
ZDOT = 3363
373425 TA = 211
83258
MA = 211
91473
Ha = 224
254 n
mi
Hp = 213
960
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15193521
00 X = -4634985
49
Y = 7548725
89 feet Y = 2249042
07 meter
Z = -14443653
10 Z = -4424930
67
XDOT = -17526
656174 XDOT = -5309
612179
YDOT = -14215
871632 feet/sec YDOT = -4392
555025 meter/sec
ZDOT = 11034
689713 ZDOT = 3337
502942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8838868
84 X = -2694087
22
Y = -14378769
62 feet Y = -4382648
98 meter
Z = -14545474
89 Z = -4433460
75
XDOT = 11573
220507 XDOT = 3527
517611
YDOT = -18131
092610 feet/sec YDOT = -5526
357028 meter/sec
ZDOT = 10918
169169 ZDOT = 3327
857963
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
34619830
00016717 00000-0 10270-3 0 9080
2 25544 51
6368 197
3218 0005724 60
8763 299
2962 15
53295329 37878
Satellite: ISS
Catalog Number: 25544
Epoch time: 19056
34619830 = yrday
fracday
Element set: 908
Inclination: 51
6368 deg
RA of node: 197
3218 deg
Eccentricity:
0005724
Arg of perigee: 60
8763 deg
Mean anomaly: 299
2962 deg
Mean motion: 15
53295329 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3787
Checksum: 352
Coasting Arc #10 (Orbit 3798)
---------------------------------------
Vector Time (GMT): 2019/057/02:28:16
395
Vector Time (MET): N/A
Weight (LBS) : 900452
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1496900
10 A = 6781411
57 meter
Y = 3980623
32 meter E =
0017772
Z = -5297466
64 I = 51
53262
XDOT = -7353
510186 Wp = 86
36807
YDOT = -2051
202599 meter/sec RA = 192
36900 deg
ZDOT = 539
226238 TA = 188
77927
MA = 188
81040
Ha = 224
363 n
mi
Hp = 215
585
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4911089
57 X = -1515569
46
Y = 13059787
79 feet Y = 3963779
25 meter
Z = -17380139
89 Z = -5304783
50
XDOT = -24125
689586 XDOT = -7332
645765
YDOT = -6729
667320 feet/sec YDOT = -2133
317995 meter/sec
ZDOT = 1769
114955 ZDOT = 503
556862
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2013237
45 X = 613634
78
Y = -13764568
11 feet Y = -4195440
36 meter
Z = -17413490
74 Z = -5307631
98
XDOT = 24000
506705 XDOT = 7315
354444
YDOT = 1486
957930 feet/sec YDOT = 453
224777 meter/sec
ZDOT = 1608
147134 ZDOT = 490
163246
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
11824273
00016717 00000-0 10270-3 0 9096
2 25544 51
6392 193
4790 0003766 53
3997 306
7501 15
52765296 37997
Satellite: ISS
Catalog Number: 25544
Epoch time: 19057
11824273 = yrday
fracday
Element set: 909
Inclination: 51
6392 deg
RA of node: 193
4790 deg
Eccentricity:
0003766
Arg of perigee: 53
3997 deg
Mean anomaly: 306
7501 deg
Mean motion: 15
52765296 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3799
Checksum: 347
Coasting Arc #11 (Orbit 3806)
---------------------------------------
Vector Time (GMT): 2019/057/14:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 900452
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2331713
02 A = 6781960
38 meter
Y = 3754178
94 meter E =
0016572
Z = -5158886
37 I = 51
55214
XDOT = -7115
502873 Wp = 93
35836
YDOT = -2408
776561 meter/sec RA = 189
78711 deg
ZDOT = 1466
300702 TA = 190
78283
MA = 190
81841
Ha = 224
280 n
mi
Hp = 215
578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7649977
09 X = -2348461
33
Y = 12316860
04 feet Y = 3728010
19 meter
Z = -16925480
21 Z = -5170253
68
XDOT = -23344
825698 XDOT = -7095
160801
YDOT = -7902
810241 feet/sec YDOT = -2488
233270 meter/sec
ZDOT = 4810
697842 ZDOT = 1431
786230
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3292996
86 X = -1003705
44
Y = 14058195
38 feet Y = 4284937
95 meter
Z = -16977113
58 Z = -5174624
22
XDOT = -23650
358923 XDOT = -7208
629400
YDOT = 69
245417 feet/sec YDOT = 21
106003 meter/sec
ZDOT = 4654
962094 ZDOT = 1418
832446
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
63311040
00016717 00000-0 10270-3 0 9108
2 25544 51
6399 190
9153 0003457 59
5158 300
6335 15
52777616 38070
Satellite: ISS
Catalog Number: 25544
Epoch time: 19057
63311040 = yrday
fracday
Element set: 910
Inclination: 51
6399 deg
RA of node: 190
9153 deg
Eccentricity:
0003457
Arg of perigee: 59
5158 deg
Mean anomaly: 300
6335 deg
Mean motion: 15
52777616 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3807
Checksum: 312
Coasting Arc #12 (Orbit 3822)
---------------------------------------
Vector Time (GMT): 2019/058/14:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 900452
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3477277
32 A = 6783769
54 meter
Y = -3441728
43 meter E =
0011361
Z = 4692830
86 I = 51
59180
XDOT = 6568
945356 Wp = 62
86623
YDOT = 2788
692499 meter/sec RA = 184
79921 deg
ZDOT = -2811
887790 TA = 55
08041
MA = 54
97371
Ha = 224
194 n
mi
Hp = 215
597
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11408390
16 X = 3492710
45
Y = -11291759
95 feet Y = -3402756
59 meter
Z = 15396426
70 Z = 4709759
54
XDOT = 21551
657993 XDOT = 6550
931575
YDOT = 9149
253605 feet/sec YDOT = 2862
050189 meter/sec
ZDOT = -9225
353642 ZDOT = -2780
022680
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6946390
82 X = 2117259
92
Y = -14388669
99 feet Y = -4385666
61 meter
Z = 15473170
15 Z = 4716222
26
XDOT = 22371
917659 XDOT = 6818
960502
YDOT = 998
145492 feet/sec YDOT = 304
234746 meter/sec
ZDOT = -9081
592832 ZDOT = -2768
069495
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
66284614
00016717 00000-0 10270-3 0 9119
2 25544 51
6403 185
7920 0003518 61
1827 298
9678 15
52797260 38234
Satellite: ISS
Catalog Number: 25544
Epoch time: 19058
66284614 = yrday
fracday
Element set: 911
Inclination: 51
6403 deg
RA of node: 185
7920 deg
Eccentricity:
0003518
Arg of perigee: 61
1827 deg
Mean anomaly: 298
9678 deg
Mean motion: 15
52797260 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3823
Checksum: 337
Coasting Arc #13 (Orbit 3837)
---------------------------------------
Vector Time (GMT): 2019/059/14:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 900452
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4485446
59 A = 6786374
30 meter
Y = 3174217
14 meter E =
0009977
Z = -3991700
32 I = 51
63248
XDOT = -5747
143349 Wp = 94
74459
YDOT = -3130
160470 meter/sec RA = 179
81988 deg
ZDOT = 3976
684245 TA = 216
69934
MA = 216
76771
Ha = 224
315 n
mi
Hp = 215
452
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14716032
12 X = -4501219
11
Y = 10414098
22 feet Y = 3123969
38 meter
Z = -13096129
66 Z = -4013526
99
XDOT = -18855
457182 XDOT = -5731
030046
YDOT = -10269
555348 feet/sec YDOT = -3194
338773 meter/sec
ZDOT = 13046
864320 ZDOT = 3948
806559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10119129
80 X = -3084310
76
Y = 14833035
10 feet Y = 4521109
10 meter
Z = -13194996
67 Z = -4021834
98
XDOT = -20244
173809 XDOT = -6170
424177
YDOT = -2338
920971 feet/sec YDOT = -712
903112 meter/sec
ZDOT = 12921
124667 ZDOT = 3938
358798
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
62822340
00016717 00000-0 10270-3 0 9121
2 25544 51
6390 180
9905 0003568 66
8494 293
3034 15
52793528 38380
Satellite: ISS
Catalog Number: 25544
Epoch time: 19059
62822340 = yrday
fracday
Element set: 912
Inclination: 51
6390 deg
RA of node: 180
9905 deg
Eccentricity:
0003568
Arg of perigee: 66
8494 deg
Mean anomaly: 293
3034 deg
Mean motion: 15
52793528 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3838
Checksum: 335
Coasting Arc #14 (Orbit 3853)
---------------------------------------
Vector Time (GMT): 2019/060/14:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 900452
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5342313
96 A = 6789241
75 meter
Y = -2883081
82 meter E =
0016270
Z = 3025702
13 I = 51
67577
XDOT = 4702
680716 Wp = 90
48513
YDOT = 3500
467786 meter/sec RA = 174
84728 deg
ZDOT = -4944
938409 TA = 54
86177
MA = 54
70940
Ha = 224
282 n
mi
Hp = 215
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17527276
76 X = 5359459
47
Y = -9458929
84 feet Y = -2823244
31 meter
Z = 9926844
27 Z = 3051694
33
XDOT = 15428
742508 XDOT = 4687
207251
YDOT = 11484
474363 feet/sec YDOT = 3552
969684 meter/sec
ZDOT = -16223
551211 ZDOT = -4922
132782
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12848426
31 X = 3916200
34
Y = -15140818
74 feet Y = -4614921
55 meter
Z = 10044529
40 Z = 3061572
56
XDOT = 17537
419553 XDOT = 5345
405480
YDOT = 4138
391740 feet/sec YDOT = 1261
381802 meter/sec
ZDOT = -16120
742036 ZDOT = -4913
602173
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
65795605
00016717 00000-0 10270-3 0 9130
2 25544 51
6395 175
8675 0003563 67
8809 292
2721 15
52794988 38548
Satellite: ISS
Catalog Number: 25544
Epoch time: 19060
65795605 = yrday
fracday
Element set: 913
Inclination: 51
6395 deg
RA of node: 175
8675 deg
Eccentricity:
0003563
Arg of perigee: 67
8809 deg
Mean anomaly: 292
2721 deg
Mean motion: 15
52794988 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3854
Checksum: 362
Coasting Arc #15 (Orbit 3855)
---------------------------------------
Vector Time (GMT): 2019/060/17:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 900452
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6096829
50 A = 6790587
04 meter
Y = -1454657
05 meter E =
0017641
Z = 2590520
46 I = 51
68217
XDOT = 3316
488588 Wp = 74
72513
YDOT = -4499
566329 meter/sec RA = 174
35631 deg
ZDOT = 5253
483229 TA = 314
40734
MA = 314
55162
Ha = 224
643 n
mi
Hp = 215
481
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20002721
45 X = -6092693
03
Y = -4772496
89 feet Y = -1522812
80 meter
Z = 8499082
88 Z = 2560915
10
XDOT = 10880
868070 XDOT = 3341
039558
YDOT = -14762
356722 feet/sec YDOT = -4462
341498 meter/sec
ZDOT = 17235
837367 ZDOT = 5269
653003
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14104673
14 X = -4299104
37
Y = 15039896
08 feet Y = 4584160
33 meter
Z = 8365388
42 Z = 2549770
39
XDOT = -6368
107771 XDOT = -1940
999249
YDOT = -15646
620799 feet/sec YDOT = -4769
090020 meter/sec
ZDOT = 17309
251380 ZDOT = 5275
859821
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
78667435
00016717 00000-0 10270-3 0 9144
2 25544 51
6386 175
2277 0004020 68
1329 292
0250 15
52751267 38560
Satellite: ISS
Catalog Number: 25544
Epoch time: 19060
78667435 = yrday
fracday
Element set: 914
Inclination: 51
6386 deg
RA of node: 175
2277 deg
Eccentricity:
0004020
Arg of perigee: 68
1329 deg
Mean anomaly: 292
0250 deg
Mean motion: 15
52751267 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3856
Checksum: 318
Coasting Arc #16 (Orbit 3864)
---------------------------------------
Vector Time (GMT): 2019/061/07:48:58
000
Vector Time (MET): N/A
Weight (LBS) : 900452
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4360202
40 A = 6787348
17 meter
Y = -3631924
83 meter E =
0015109
Z = 3712829
83 I = 51
68964
XDOT = 5810
091522 Wp = 81
15357
YDOT = 2555
529681 meter/sec RA = 171
33183 deg
ZDOT = -4306
063344 TA = 54
59940
MA = 54
45836
Ha = 224
322 n
mi
Hp = 215
539
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14305126
00 X = 4382457
09
Y = -11915763
89 feet Y = -3583041
36 meter
Z = 12181200
24 Z = 3734063
85
XDOT = 19061
980059 XDOT = 5801
999052
YDOT = 8384
283731 feet/sec YDOT = 2620
456690 meter/sec
ZDOT = -14127
504410 ZDOT = -4277
860529
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13375913
28 X = 4076978
37
Y = 12858964
69 feet Y = 3919412
44 meter
Z = 12277445
55 Z = 3742165
40
XDOT = -5336
201110 XDOT = -1626
474098
YDOT = 18971
388042 feet/sec YDOT = 5782
479075 meter/sec
ZDOT = -14000
218845 ZDOT = -4267
266704
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
36589592
00016717 00000-0 10270-3 0 9157
2 25544 51
6366 172
3430 0003566 70
0388 290
1148 15
52770346 38652
Satellite: ISS
Catalog Number: 25544
Epoch time: 19061
36589592 = yrday
fracday
Element set: 915
Inclination: 51
6366 deg
RA of node: 172
3430 deg
Eccentricity:
0003566
Arg of perigee: 70
0388 deg
Mean anomaly: 290
1148 deg
Mean motion: 15
52770346 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3865
Checksum: 323
Coasting Arc #17 (Orbit 3879)
---------------------------------------
Vector Time (GMT): 2019/062/07:48:58
000
Vector Time (MET): N/A
Weight (LBS) : 900452
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5162233
80 A = 6790007
52 meter
Y = 3467094
47 meter E =
0008507
Z = -2728551
04 I = 51
73199
XDOT = -4766
244574 Wp = 66
73079
YDOT = -3040
463428 meter/sec RA = 166
36450 deg
ZDOT = 5170
060662 TA = 262
48727
MA = 262
58392
Ha = 224
457 n
mi
Hp = 215
362
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16936462
59 X = -5187366
69
Y = 11374981
85 feet Y = 3409226
04 meter
Z = -8951939
09 Z = -2753687
93
XDOT = -15637
285349 XDOT = -4757
003715
YDOT = -9975
273715 feet/sec YDOT = -3093
710869 meter/sec
ZDOT = 16962
141281 ZDOT = 5146
931238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13389500
21 X = -4081119
67
Y = -15326553
66 feet Y = -4671533
56 meter
Z = -9065827
46 Z = -2763264
21
XDOT = 6815
175933 XDOT = 2077
265624
YDOT = -15894
601245 feet/sec YDOT = -4844
674460 meter/sec
ZDOT = 16857
807495 ZDOT = 5138
259724
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
33126677
00016717 00000-0 10270-3 0 9167
2 25544 51
6372 167
5402 0003827 76
0266 284
1311 15
52783012 38801
Satellite: ISS
Catalog Number: 25544
Epoch time: 19062
33126677 = yrday
fracday
Element set: 916
Inclination: 51
6372 deg
RA of node: 167
5402 deg
Eccentricity:
0003827
Arg of perigee: 76
0266 deg
Mean anomaly: 284
1311 deg
Mean motion: 15
52783012 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3880
Checksum: 302
Coasting Arc #18 (Orbit 3881)
---------------------------------------
Vector Time (GMT): 2019/062/10:55:42
000
Vector Time (MET): N/A
Weight (LBS) : 935669
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5498450
13 A = 6791008
58 meter
Y = 3261371
63 meter E =
0009152
Z = -2288611
95 I = 51
74211
XDOT = -4238
357357 Wp = 57
45091
YDOT = -3345
106167 meter/sec RA = 165
72334 deg
ZDOT = 5436
485864 TA = 277
13040
MA = 277
23446
Ha = 224
438 n
mi
Hp = 215
455
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18039534
56 X = -5523394
52
Y = 10700038
15 feet Y = 3199744
48 meter
Z = -7508569
40 Z = -2315381
55
XDOT = -13905
371906 XDOT = -4227
043243
YDOT = -10974
757765 feet/sec YDOT = -3392
438782 meter/sec
ZDOT = 17836
239712 ZDOT = 5415
925723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20841418
90 X = -6352464
48
Y = -1927501
56 feet Y = -587502
48 meter
Z = -7629825
27 Z = -2325570
74
XDOT = -5028
229307 XDOT = -1532
604293
YDOT = -15603
698165 feet/sec YDOT = -4756
007201 meter/sec
ZDOT = 17743
541232 ZDOT = 5408
231367
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
45998253
00016717 00000-0 10270-3 0 9178
2 25544 51
6400 166
9003 0003694 75
8649 284
2913 15
52762522 38821
Satellite: ISS
Catalog Number: 25544
Epoch time: 19062
45998253 = yrday
fracday
Element set: 917
Inclination: 51
6400 deg
RA of node: 166
9003 deg
Eccentricity:
0003694
Arg of perigee: 75
8649 deg
Mean anomaly: 284
2913 deg
Mean motion: 15
52762522 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3882
Checksum: 333
Coasting Arc #19 (Orbit 3897)
---------------------------------------
Vector Time (GMT): 2019/063/10:55:42
000
Vector Time (MET): N/A
Weight (LBS) : 935669
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6005468
66 A = 6792763
40 meter
Y = -2977528
17 meter E =
0016572
Z = 1057711
54 I = 51
77960
XDOT = 2977
119473 Wp = 115
27441
YDOT = 3884
574199 meter/sec RA = 160
76587 deg
ZDOT = -5902
849927 TA = 53
28248
MA = 53
13037
Ha = 224
454 n
mi
Hp = 215
438
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19702981
17 X = 6033180
23
Y = -9768793
21 feet Y = -2910215
78 meter
Z = 3470182
21 Z = 1086950
74
XDOT = 9767
452338 XDOT = 2962
131900
YDOT = 12744
666007 feet/sec YDOT = 3917
782104 meter/sec
ZDOT = -19366
305534 ZDOT = -5888
425283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21720960
14 X = 6620548
65
Y = 3301535
50 feet Y = 1006308
02 meter
Z = 3602597
16 Z = 1098071
62
XDOT = 1026
680426 XDOT = 312
932194
YDOT = 14531
997159 feet/sec YDOT = 4429
352734 meter/sec
ZDOT = -19301
374048 ZDOT = -5883
058810
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
48970845
00016717 00000-0 10270-3 0 9180
2 25544 51
6397 161
7777 0003650 82
6567 277
5000 15
52773634 38989
Satellite: ISS
Catalog Number: 25544
Epoch time: 19063
48970845 = yrday
fracday
Element set: 918
Inclination: 51
6397 deg
RA of node: 161
7777 deg
Eccentricity:
0003650
Arg of perigee: 82
6567 deg
Mean anomaly: 277
5000 deg
Mean motion: 15
52773634 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3898
Checksum: 353
Coasting Arc #20 (Orbit 3912)
---------------------------------------
Vector Time (GMT): 2019/064/10:55:42
000
Vector Time (MET): N/A
Weight (LBS) : 935669
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6247236
78 A = 6793228
89 meter
Y = 2645780
76 meter E =
0015518
Z = 185770
13 I = 51
81381
XDOT = -1688
530471 Wp = 55
48120
YDOT = -4434
337834 meter/sec RA = 155
81269 deg
ZDOT = 6022
484571 TA = 306
51446
MA = 306
65727
Ha = 224
454 n
mi
Hp = 215
449
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20496183
67 X = -6277260
70
Y = 8680383
07 feet Y = 2575751
94 meter
Z = 609482
07 Z = 155350
87
XDOT = -5539
798133 XDOT = -1668
072202
YDOT = -14548
352475 feet/sec YDOT = -4453
105146 meter/sec
ZDOT = 19758
807649 ZDOT = 6014
332655
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21844933
99 X = -6658335
88
Y = -4288401
03 feet Y = -1307104
63 meter
Z = 471740
92 Z = 143786
63
XDOT = 3134
625473 XDOT = 955
433844
YDOT = -13635
378213 feet/sec YDOT = -4156
063279 meter/sec
ZDOT = 19722
272425 ZDOT = 6011
348635
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
51943109
00016717 00000-0 10270-3 0 9199
2 25544 51
6412 156
6554 0003710 83
3814 276
7761 15
52785667 39135
Satellite: ISS
Catalog Number: 25544
Epoch time: 19064
51943109 = yrday
fracday
Element set: 919
Inclination: 51
6412 deg
RA of node: 156
6554 deg
Eccentricity:
0003710
Arg of perigee: 83
3814 deg
Mean anomaly: 276
7761 deg
Mean motion: 15
52785667 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3913
Checksum: 328
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