[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 9th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21963 7592 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 6 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
010/09:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
6
000/00:00:00
000 0
0 0
0 216
3
016/05:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 220
8
000/00:00:00
000 0
0 0
0 216
2
018/18:04:49
685 2
7 2
9 2
9
N/A 0
7 0
0 220
9
000/00:07:35
370 -0
6 -0
0 217
7
020/01:03:00
000 0
0 0
0 0
0
N/A 0
0 0
0 221
0
000/00:00:00
000 0
0 0
0 217
7
Coasting Arc #1 (Orbit 3058)
---------------------------------------
Vector Time (GMT): 2019/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949740
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4568869
55 A = 6781836
48 meter
Y = 2166991
04 meter E =
0007440
Z = -4526732
93 I = 51
99190
XDOT = -114
172869 Wp = 120
32002
YDOT = 6953
206772 meter/sec RA = 69
76999 deg
ZDOT = 3213
607508 TA = 181
84621
MA = 181
84896
Ha = 220
667 n
mi
Hp = 216
292
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14989729
50 X = 4566286
04
Y = 7109550
66 feet Y = 2218069
18 meter
Z = -14851486
00 Z = -4504545
60
XDOT = -374
582905 XDOT = -207
526735
YDOT = 22812
358175 feet/sec YDOT = 6951
407819 meter/sec
ZDOT = 10543
331719 ZDOT = 3212
826647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2140062
43 X = -652291
03
Y = 16541317
51 feet Y = 5041793
58 meter
Z = -14751585
86 Z = -4496283
37
XDOT = -20644
675993 XDOT = -6292
497243
YDOT = 6726
879529 feet/sec YDOT = 2050
352881 meter/sec
ZDOT = 10538
919050 ZDOT = 3212
262526
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 19009
51031463
00016717 00000-0 10270-3 0 9009
2 25544 51
6401 70
5247 0002563 260
1043 99
9820 15
53762524 30590
Satellite: ISS
Catalog Number: 25544
Epoch time: 19009
51031463 = yrday
fracday
Element set: 900
Inclination: 51
6401 deg
RA of node: 70
5247 deg
Eccentricity:
0002563
Arg of perigee: 260
1043 deg
Mean anomaly: 99
9820 deg
Mean motion: 15
53762524 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3059
Checksum: 283
Coasting Arc #2 (Orbit 3072)
---------------------------------------
Vector Time (GMT): 2019/010/09:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 929656
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4652462
84 A = 6780656
48 meter
Y = 1105692
82 meter E =
0009014
Z = -4815834
59 I = 51
97861
XDOT = 1019
770050 Wp = 115
99797
YDOT = 7125
251638 meter/sec RA = 65
31303 deg
ZDOT = 2621
056288 TA = 179
74553
MA = 179
74507
Ha = 220
601 n
mi
Hp = 216
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15263985
70 X = 4663145
14
Y = 3627601
12 feet Y = 1157779
89 meter
Z = -15799982
23 Z = -4793209
05
XDOT = 3345
702263 XDOT = 927
286277
YDOT = 23376
809835 feet/sec YDOT = 7136
138168 meter/sec
ZDOT = 8599
266038 ZDOT = 2625
785622
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8082460
38 X = -2463533
92
Y = 13565978
49 feet Y = 4134910
24 meter
Z = -15697969
60 Z = -4784741
14
XDOT = -22294
348991 XDOT = -6795
317572
YDOT = -3308
211228 feet/sec YDOT = -1008
342782 meter/sec
ZDOT = 8619
702487 ZDOT = 2627
285318
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 19010
41076208
00016717 00000-0 10270-3 0 9017
2 25544 51
6417 66
0373 0002649 261
3166 98
7687 15
53779374 30736
Satellite: ISS
Catalog Number: 25544
Epoch time: 19010
41076208 = yrday
fracday
Element set: 901
Inclination: 51
6417 deg
RA of node: 66
0373 deg
Eccentricity:
0002649
Arg of perigee: 261
3166 deg
Mean anomaly: 98
7687 deg
Mean motion: 15
53779374 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3073
Checksum: 317
Coasting Arc #3 (Orbit 3088)
---------------------------------------
Vector Time (GMT): 2019/011/09:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 929656
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4942487
18 A = 6784024
35 meter
Y = -2508085
14 meter E =
0008688
Z = 3906037
57 I = 51
97487
XDOT = 21
842662 Wp = 79
13623
YDOT = -6470
074764 meter/sec RA = 60
34884 deg
ZDOT = -4117
489818 TA = 53
86928
MA = 53
78890
Ha = 220
732 n
mi
Hp = 216
213
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16215509
13 X = -4933046
80
Y = -8228625
78 feet Y = -2563302
84 meter
Z = 12815083
88 Z = 3882052
01
XDOT = 71
662276 XDOT = 114
191402
YDOT = -21227
279411 feet/sec YDOT = -6469
313989 meter/sec
ZDOT = -13508
824863 ZDOT = -4117
159677
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12524085
38 X = 3817341
22
Y = -13287433
06 feet Y = -4050009
60 meter
Z = 12707116
18 Z = 3873129
01
XDOT = 19336
587497 XDOT = 5893
791869
YDOT = 5279
568216 feet/sec YDOT = 1609
212392 meter/sec
ZDOT = -13506
494035 ZDOT = -4116
779382
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 19011
43984349
00016717 00000-0 10270-3 0 9025
2 25544 51
6417 60
9102 0002600 268
3921 91
6933 15
53765246 30898
Satellite: ISS
Catalog Number: 25544
Epoch time: 19011
43984349 = yrday
fracday
Element set: 902
Inclination: 51
6417 deg
RA of node: 60
9102 deg
Eccentricity:
0002600
Arg of perigee: 268
3921 deg
Mean anomaly: 91
6933 deg
Mean motion: 15
53765246 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3089
Checksum: 307
Coasting Arc #4 (Orbit 3103)
---------------------------------------
Vector Time (GMT): 2019/012/09:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 929656
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5056708
11 A = 6787523
68 meter
Y = 3657597
65 meter E =
0003345
Z = -2665216
07 I = 51
96812
XDOT = -1200
066801 Wp = 22
55390
YDOT = 5469
325093 meter/sec RA = 55
39287 deg
ZDOT = 5234
096003 TA = 307
53761
MA = 307
56800
Ha = 220
645 n
mi
Hp = 216
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16590249
72 X = 5028377
98
Y = 11999992
30 feet Y = 3713986
96 meter
Z = -8744147
23 Z = -2640721
49
XDOT = -3937
227037 XDOT = -1286
561147
YDOT = 17943
979964 feet/sec YDOT = 5455
421334 meter/sec
ZDOT = 17172
230980 ZDOT = 5228
056690
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16020590
03 X = -4883075
84
Y = 12825380
28 feet Y = 3909175
91 meter
Z = -8634038
87 Z = -2631655
05
XDOT = -15268
706132 XDOT = -4653
901629
YDOT = -7542
704895 feet/sec YDOT = -2299
016452 meter/sec
ZDOT = 17144
247227 ZDOT = 5225
566555
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 19012
40460649
00016717 00000-0 10270-3 0 9036
2 25544 51
6409 56
1041 0002739 272
0438 88
0401 15
53739096 31048
Satellite: ISS
Catalog Number: 25544
Epoch time: 19012
40460649 = yrday
fracday
Element set: 903
Inclination: 51
6409 deg
RA of node: 56
1041 deg
Eccentricity:
0002739
Arg of perigee: 272
0438 deg
Mean anomaly: 88
0401 deg
Mean motion: 15
53739096 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3104
Checksum: 288
Coasting Arc #5 (Orbit 3119)
---------------------------------------
Vector Time (GMT): 2019/013/09:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 929656
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4918651
52 A = 6789848
92 meter
Y = -4524731
79 meter E =
0011374
Z = 1163829
07 I = 51
95661
XDOT = 2488
257061 Wp = 128
16565
YDOT = -4229
034405 meter/sec RA = 50
44318 deg
ZDOT = -5893
452471 TA = 39
25217
MA = 39
16976
Ha = 220
641 n
mi
Hp = 216
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16137308
15 X = -4873342
32
Y = -14844920
56 feet Y = -4579482
27 meter
Z = 3818336
84 Z = 1140046
26
XDOT = 8163
573034 XDOT = 2563
989220
YDOT = -13874
784794 feet/sec YDOT = -4200
785376 meter/sec
ZDOT = -19335
473987 ZDOT = -5881
181746
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18429534
49 X = 5617322
11
Y = -11913883
03 feet Y = -3631351
55 meter
Z = 3711566
63 Z = 1131285
51
XDOT = 10478
559064 XDOT = 3193
864803
YDOT = 10169
239271 feet/sec YDOT = 3099
584130 meter/sec
ZDOT = -19279
515573 ZDOT = -5876
396347
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 19013
43368566
00016717 00000-0 10270-3 0 9046
2 25544 51
6411 50
9772 0002613 276
6157 83
4698 15
53763753 31205
Satellite: ISS
Catalog Number: 25544
Epoch time: 19013
43368566 = yrday
fracday
Element set: 904
Inclination: 51
6411 deg
RA of node: 50
9772 deg
Eccentricity:
0002613
Arg of perigee: 276
6157 deg
Mean anomaly: 83
4698 deg
Mean motion: 15
53763753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3120
Checksum: 315
Coasting Arc #6 (Orbit 3135)
---------------------------------------
Vector Time (GMT): 2019/014/09:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 929656
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4506869
78 A = 6790412
13 meter
Y = 5053122
98 meter E =
0011619
Z = 418634
18 I = 51
93647
XDOT = -3786
413666 Wp = 38
79509
YDOT = 2871
695891 meter/sec RA = 45
49519 deg
ZDOT = 6019
118696 TA = 325
70031
MA = 325
77529
Ha = 220
755 n
mi
Hp = 216
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14786318
17 X = 4447995
90
Y = 16578487
48 feet Y = 5103192
74 meter
Z = 1373471
71 Z = 440383
88
XDOT = -12422
617016 XDOT = -3847
481696
YDOT = 9421
574446 feet/sec YDOT = 2829
011929 meter/sec
ZDOT = 19747
764752 ZDOT = 6000
577617
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19582386
41 X = -5968711
38
Y = 10475410
96 feet Y = 3192905
26 meter
Z = 1470980
82 Z = 448354
96
XDOT = -5451
168339 XDOT = -1661
516110
YDOT = -12986
420799 feet/sec YDOT = -3958
261060 meter/sec
ZDOT = 19663
677444 ZDOT = 5993
488885
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 19014
46276340
00016717 00000-0 10270-3 0 9059
2 25544 51
6414 45
8498 0002610 286
0997 73
9868 15
53727650 31366
Satellite: ISS
Catalog Number: 25544
Epoch time: 19014
46276340 = yrday
fracday
Element set: 905
Inclination: 51
6414 deg
RA of node: 45
8498 deg
Eccentricity:
0002610
Arg of perigee: 286
0997 deg
Mean anomaly: 73
9868 deg
Mean motion: 15
53727650 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3136
Checksum: 329
Coasting Arc #7 (Orbit 3150)
---------------------------------------
Vector Time (GMT): 2019/015/09:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 929656
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3773935
56 A = 6788663
13 meter
Y = -5278587
54 meter E =
0004777
Z = -1987318
85 I = 51
90624
XDOT = 5019
207498 Wp = 155
56618
YDOT = -1483
527799 meter/sec RA = 40
54536 deg
ZDOT = -5600
100635 TA = 46
27854
MA = 46
23899
Ha = 220
711 n
mi
Hp = 216
096
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12381678
34 X = -3704975
18
Y = -17318200
59 feet Y = -5320404
65 meter
Z = -6520074
97 Z = -2005483
87
XDOT = 16467
216202 XDOT = 5062
625726
YDOT = -4867
217188 feet/sec YDOT = -1427
156506 meter/sec
ZDOT = -18373
033578 ZDOT = -5575
613941
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19590340
41 X = 5971135
76
Y = -8269101
09 feet Y = -2520422
01 meter
Z = -6601358
78 Z = -2012094
15
XDOT = 534
981065 XDOT = 163
062228
YDOT = 15823
145607 feet/sec YDOT = 4822
894781 meter/sec
ZDOT = -18262
294062 ZDOT = -5566
347230
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 19015
42752128
00016717 00000-0 10270-3 0 9060
2 25544 51
6406 41
0439 0002498 287
7525 72
3355 15
53766518 31516
Satellite: ISS
Catalog Number: 25544
Epoch time: 19015
42752128 = yrday
fracday
Element set: 906
Inclination: 51
6406 deg
RA of node: 41
0439 deg
Eccentricity:
0002498
Arg of perigee: 287
7525 deg
Mean anomaly: 72
3355 deg
Mean motion: 15
53766518 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3151
Checksum: 310
Coasting Arc #8 (Orbit 3163)
---------------------------------------
Vector Time (GMT): 2019/016/05:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 929656
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5936811
32 A = 6787015
80 meter
Y = -1570753
60 meter E =
0010901
Z = 2878310
91 I = 51
87931
XDOT = -970
043617 Wp = 98
34665
YDOT = -5665
009309 meter/sec RA = 36
39837 deg
ZDOT = -5077
469509 TA = 49
00691
MA = 48
91268
Ha = 220
802 n
mi
Hp = 216
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19477727
43 X = -5932786
65
Y = -5153391
08 feet Y = -1637120
83 meter
Z = 9443277
25 Z = 2849481
91
XDOT = -3182
557799 XDOT = -881
960382
YDOT = -18585
988545 feet/sec YDOT = -5675
364204 meter/sec
ZDOT = -16658
364532 ZDOT = -5081
967999
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20205479
14 X = 6158630
04
Y = -338800
06 feet Y = -103266
26 meter
Z = 9313356
96 Z = 2838711
20
XDOT = 7971
479749 XDOT = 2429
707027
YDOT = 15584
659633 feet/sec YDOT = 4750
204256 meter/sec
ZDOT = -16677
893783 ZDOT = -5083
422025
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 19016
26364531
00016717 00000-0 10270-3 0 9071
2 25544 51
6409 36
8754 0002463 283
0034 77
0843 15
53749899 31648
Satellite: ISS
Catalog Number: 25544
Epoch time: 19016
26364531 = yrday
fracday
Element set: 907
Inclination: 51
6409 deg
RA of node: 36
8754 deg
Eccentricity:
0002463
Arg of perigee: 283
0034 deg
Mean anomaly: 77
0843 deg
Mean motion: 15
53749899 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3164
Checksum: 323
Coasting Arc #9 (Orbit 3178)
---------------------------------------
Vector Time (GMT): 2019/017/05:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 929656
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6162736
42 A = 6789597
06 meter
Y = 2452193
00 meter E =
0008334
Z = -1429595
97 I = 51
86192
XDOT = -630
619576 Wp = 20
27259
YDOT = 4962
165937 meter/sec RA = 31
44126 deg
ZDOT = 5810
870849 TA = 324
18888
MA = 324
24473
Ha = 220
839 n
mi
Hp = 216
128
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20218951
51 X = 6141801
43
Y = 8045252
63 feet Y = 2520992
07 meter
Z = -4690275
49 Z = -1399710
52
XDOT = -2068
961865 XDOT = -714
286867
YDOT = 16280
071972 feet/sec YDOT = 4954
645633 meter/sec
ZDOT = 19064
536906 ZDOT = 5807
604737
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21708144
49 X = -6616642
44
Y = -1879547
08 feet Y = -572885
95 meter
Z = -4555715
07 Z = -1388581
95
XDOT = -2717
367524 XDOT = -828
253621
YDOT = -14642
044243 feet/sec YDOT = -4462
895085 meter/sec
ZDOT = 19049
105361 ZDOT = 5806
167314
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 19017
22840055
00016717 00000-0 10270-3 0 9089
2 25544 51
6422 32
0690 0002515 292
6968 67
3919 15
53754300 31795
Satellite: ISS
Catalog Number: 25544
Epoch time: 19017
22840055 = yrday
fracday
Element set: 908
Inclination: 51
6422 deg
RA of node: 32
0690 deg
Eccentricity:
0002515
Arg of perigee: 292
6968 deg
Mean anomaly: 67
3919 deg
Mean motion: 15
53754300 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3179
Checksum: 308
Coasting Arc #10 (Orbit 3194)
---------------------------------------
Vector Time (GMT): 2019/018/05:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 929656
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6009328
53 A = 6790359
29 meter
Y = -3146546
16 meter E =
0009442
Z = -173191
20 I = 51
83481
XDOT = 2330
536784 Wp = 141
34044
YDOT = -4129
403173 meter/sec RA = 26
48720 deg
ZDOT = -6025
111150 TA = 40
51990
MA = 40
44964
Ha = 220
791 n
mi
Hp = 216
068
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19715644
77 X = -5972855
08
Y = -10323314
17 feet Y = -3213542
70 meter
Z = -568212
59 Z = -202293
74
XDOT = 7646
118057 XDOT = 2405
806111
YDOT = -13547
910672 feet/sec YDOT = -4102
920045 meter/sec
ZDOT = -19767
425032 ZDOT = -6013
607960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21917229
28 X = 6680371
49
Y = 3840130
09 feet Y = 1170471
65 meter
Z = -699136
18 Z = -213096
71
XDOT = -3009
177595 XDOT = -917
197331
YDOT = 13674
721593 feet/sec YDOT = 4168
055142 meter/sec
ZDOT = -19714
923138 ZDOT = -6009
108572
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 19018
25747192
00016717 00000-0 10270-3 0 9092
2 25544 51
6412 26
9422 0002451 294
6540 65
4357 15
53767196 31956
Satellite: ISS
Catalog Number: 25544
Epoch time: 19018
25747192 = yrday
fracday
Element set: 909
Inclination: 51
6412 deg
RA of node: 26
9422 deg
Eccentricity:
0002451
Arg of perigee: 294
6540 deg
Mean anomaly: 65
4357 deg
Mean motion: 15
53767196 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3195
Checksum: 322
Coasting Arc #11 (Orbit 3202)
---------------------------------------
Vector Time (GMT): 2019/018/18:08:37
370
Vector Time (MET): N/A
Weight (LBS) : 929347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1693790
87 A = 6779955
28 meter
Y = -3842384
78 meter E =
0010587
Z = -5332147
61 I = 51
77904
XDOT = 7006
360771 Wp = 84
00450
YDOT = 3094
876972 meter/sec RA = 23
85283 deg
ZDOT = -3
503598 TA = 185
95584
MA = 185
96844
Ha = 220
929 n
mi
Hp = 217
730
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5557056
67 X = 1762531
94
Y = -12606249
26 feet Y = -3823058
72 meter
Z = -17493922
61 Z = -5323753
34
XDOT = 22986
747936 XDOT = 6971
249281
YDOT = 10153
795841 feet/sec YDOT = 3173
030656 meter/sec
ZDOT = -11
494744 ZDOT = 30
445346
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1181727
80 X = -360190
63
Y = -13774796
84 feet Y = -4198558
08 meter
Z = -17455492
52 Z = -5320434
12
XDOT = 24017
164821 XDOT = 7320
431837
YDOT = -2235
012698 feet/sec YDOT = -681
231870 meter/sec
ZDOT = 141
309502 ZDOT = 43
071136
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 19018
77200994
00016717 00000-0 10270-3 0 9105
2 25544 51
6413 24
3824 0004472 284
4244 75
6412 15
53235759 32038
Satellite: ISS
Catalog Number: 25544
Epoch time: 19018
77200994 = yrday
fracday
Element set: 910
Inclination: 51
6413 deg
RA of node: 24
3824 deg
Eccentricity:
0004472
Arg of perigee: 284
4244 deg
Mean anomaly: 75
6412 deg
Mean motion: 15
53235759 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3203
Checksum: 297
Coasting Arc #12 (Orbit 3218)
---------------------------------------
Vector Time (GMT): 2019/019/18:08:37
370
Vector Time (MET): N/A
Weight (LBS) : 929347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3003826
62 A = 6780761
12 meter
Y = 3252816
74 meter E =
0004317
Z = 5137015
27 I = 51
75093
XDOT = -6592
679813 Wp = 354
64155
YDOT = -3575
569369 meter/sec RA = 18
87205 deg
ZDOT = -1586
834264 TA = 110
66436
MA = 110
61807
Ha = 221
018 n
mi
Hp = 217
699
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9855074
21 X = -3064929
62
Y = 10671970
92 feet Y = 3218883
66 meter
Z = 16853724
64 Z = 5122275
99
XDOT = -21629
526945 XDOT = -6544
498985
YDOT = -11730
870634 feet/sec YDOT = -3649
023741 meter/sec
ZDOT = -5206
149160 ZDOT = -1618
741852
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3266097
01 X = -995506
37
Y = 14233748
22 feet Y = 4338446
46 meter
Z = 16786736
04 Z = 5116597
15
XDOT = -23527
504020 XDOT = -7171
183225
YDOT = 926
420920 feet/sec YDOT = 282
373096 meter/sec
ZDOT = -5349
668570 ZDOT = -1630
578980
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 19019
80144162
00016717 00000-0 10270-3 0 9115
2 25544 51
6411 19
2580 0004694 287
8460 72
2180 15
53260239 32194
Satellite: ISS
Catalog Number: 25544
Epoch time: 19019
80144162 = yrday
fracday
Element set: 911
Inclination: 51
6411 deg
RA of node: 19
2580 deg
Eccentricity:
0004694
Arg of perigee: 287
8460 deg
Mean anomaly: 72
2180 deg
Mean motion: 15
53260239 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3219
Checksum: 293
Coasting Arc #13 (Orbit 3222)
---------------------------------------
Vector Time (GMT): 2019/020/01:03:00
000
Vector Time (MET): N/A
Weight (LBS) : 929347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1861259
31 A = 6780083
05 meter
Y = -3801426
14 meter E =
0010428
Z = -5305654
24 I = 51
73714
XDOT = 7141
589498 Wp = 90
41858
YDOT = 2710
610427 meter/sec RA = 17
44546 deg
ZDOT = 564
087851 TA = 184
95821
MA = 184
96854
Ha = 220
966 n
mi
Hp = 217
682
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6106493
81 X = 1929401
03
Y = -12471870
52 feet Y = -3780230
68 meter
Z = -17407002
09 Z = -5296448
00
XDOT = 23430
411738 XDOT = 7108
007943
YDOT = 8893
078828 feet/sec YDOT = 2790
284828 meter/sec
ZDOT = 1850
681927 ZDOT = 598
697090
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13295316
65 X = -4052412
52
Y = 4187476
96 feet Y = 1276342
98 meter
Z = -17364911
02 Z = -5292824
88
XDOT = -9563
022131 XDOT = -2914
809145
YDOT = -22054
066733 feet/sec YDOT = -6722
079540 meter/sec
ZDOT = 2006
517542 ZDOT = 611
586547
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 19020
05880025
00016717 00000-0 10270-3 0 9120
2 25544 51
6389 17
9722 0004327 284
0956 75
9715 15
53234353 32230
Satellite: ISS
Catalog Number: 25544
Epoch time: 19020
05880025 = yrday
fracday
Element set: 912
Inclination: 51
6389 deg
RA of node: 17
9722 deg
Eccentricity:
0004327
Arg of perigee: 284
0956 deg
Mean anomaly: 75
9715 deg
Mean motion: 15
53234353 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3223
Checksum: 304
Coasting Arc #14 (Orbit 3238)
---------------------------------------
Vector Time (GMT): 2019/021/01:03:00
000
Vector Time (MET): N/A
Weight (LBS) : 929347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3194478
80 A = 6781638
04 meter
Y = 3318665
92 meter E =
0004901
Z = 4977631
07 I = 51
70940
XDOT = -6638
475849 Wp = 15
07953
YDOT = -3188
611770 meter/sec RA = 12
46084 deg
ZDOT = -2129
361526 TA = 95
67375
MA = 95
61787
Ha = 221
230 n
mi
Hp = 217
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10480573
50 X = -3255529
61
Y = 10888011
56 feet Y = 3282601
25 meter
Z = 16330810
59 Z = 4961965
88
XDOT = -21779
776408 XDOT = -6591
983515
YDOT = -10461
324706 feet/sec YDOT = -3262
587689 meter/sec
ZDOT = -6986
094244 ZDOT = -2161
495325
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15187756
70 X = 4629228
24
Y = -207116
31 feet Y = -63129
05 meter
Z = 16259635
31 Z = 4955936
84
XDOT = 7947
286409 XDOT = 2422
332898
YDOT = 21659
949039 feet/sec YDOT = 6601
952467 meter/sec
ZDOT = -7130
687759 ZDOT = -2173
433629
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 19021
08823116
00016717 00000-0 10270-3 0 9133
2 25544 51
6385 12
8459 0004240 288
2392 71
8298 15
53194640 32393
Satellite: ISS
Catalog Number: 25544
Epoch time: 19021
08823116 = yrday
fracday
Element set: 913
Inclination: 51
6385 deg
RA of node: 12
8459 deg
Eccentricity:
0004240
Arg of perigee: 288
2392 deg
Mean anomaly: 71
8298 deg
Mean motion: 15
53194640 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3239
Checksum: 310
Coasting Arc #15 (Orbit 3253)
---------------------------------------
Vector Time (GMT): 2019/022/01:03:00
000
Vector Time (MET): N/A
Weight (LBS) : 929347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4398904
72 A = 6784206
40 meter
Y = -2855355
39 meter E =
0004003
Z = -4307795
65 I = 51
68632
XDOT = 5781
475465 Wp = 108
08911
YDOT = 3576
164838 meter/sec RA = 7
48079 deg
ZDOT = 3534
834334 TA = 197
91652
MA = 197
93063
Ha = 221
209 n
mi
Hp = 217
678
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14432102
11 X = 4451431
47
Y = -9367963
88 feet Y = -2805869
82 meter
Z = -14133187
81 Z = -4286300
61
XDOT = 18968
095356 XDOT = 5723
886321
YDOT = 11732
824271 feet/sec YDOT = 3640
495113 meter/sec
ZDOT = 11597
225505 ZDOT = 3562
778127
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16955608
18 X = -5168069
37
Y = -3360932
22 feet Y = -1024412
14 meter
Z = -14035768
67 Z = -4278102
29
XDOT = -5670
369181 XDOT = -1728
328526
YDOT = -20329
394848 feet/sec YDOT = -6196
399550 meter/sec
ZDOT = 11722
851186 ZDOT = 3573
125041
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 19022
05331964
00016717 00000-0 10270-3 0 9147
2 25544 51
6392 8
0421 0004315 291
8126 68
2567 15
53226018 32546
Satellite: ISS
Catalog Number: 25544
Epoch time: 19022
05331964 = yrday
fracday
Element set: 914
Inclination: 51
6392 deg
RA of node: 8
0421 deg
Eccentricity:
0004315
Arg of perigee: 291
8126 deg
Mean anomaly: 68
2567 deg
Mean motion: 15
53226018 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3254
Checksum: 287
Coasting Arc #16 (Orbit 3269)
---------------------------------------
Vector Time (GMT): 2019/023/01:03:00
000
Vector Time (MET): N/A
Weight (LBS) : 929347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5415126
41 A = 6787425
61 meter
Y = 2388462
95 meter E =
0008801
Z = 3316730
78 I = 51
66401
XDOT = -4615
888113 Wp = 81
04236
YDOT = -3921
981327 meter/sec RA = 2
50417 deg
ZDOT = -4699
906267 TA = 60
40362
MA = 60
31596
Ha = 221
297 n
mi
Hp = 217
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17766162
75 X = -5457542
79
Y = 7836164
52 feet Y = 2327669
97 meter
Z = 10881662
67 Z = 3290323
93
XDOT = -15143
989873 XDOT = -4548
859479
YDOT = -12867
392805 feet/sec YDOT = -3973
224496 meter/sec
ZDOT = -15419
639984 ZDOT = -4722
165189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18385726
67 X = 5603969
49
Y = 6449327
83 feet Y = 1965755
12 meter
Z = 10762147
62 Z = 3280302
59
XDOT = 2677
860949 XDOT = 816
212017
YDOT = 18330
221956 feet/sec YDOT = 5587
051652 meter/sec
ZDOT = -15519
557526 ZDOT = -4730
361134
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 19023
08274763
00016717 00000-0 10270-3 0 9155
2 25544 51
6393 2
9167 0004350 294
6280 65
4419 15
53216382 32704
Satellite: ISS
Catalog Number: 25544
Epoch time: 19023
08274763 = yrday
fracday
Element set: 915
Inclination: 51
6393 deg
RA of node: 2
9167 deg
Eccentricity:
0004350
Arg of perigee: 294
6280 deg
Mean anomaly: 65
4419 deg
Mean motion: 15
53216382 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3270
Checksum: 303
Coasting Arc #17 (Orbit 3284)
---------------------------------------
Vector Time (GMT): 2019/024/01:03:00
000
Vector Time (MET): N/A
Weight (LBS) : 929347
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6154008
37 A = 6790119
39 meter
Y = -1933576
48 meter E =
0007168
Z = -2106214
15 I = 51
64171
XDOT = 3217
727730 Wp = 3
37751
YDOT = 4235
201506 meter/sec RA = 357
53280 deg
ZDOT = 5521
556528 TA = 333
30485
MA = 333
34173
Ha = 221
442 n
mi
Hp = 217
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20190316
18 X = 6185403
34
Y = -6343754
86 feet Y = -1864582
53 meter
Z = -6910151
41 Z = -2076244
83
XDOT = 10556
849507 XDOT = 3143
309423
YDOT = 13895
018064 feet/sec YDOT = 4270
768281 meter/sec
ZDOT = 18115
342940 ZDOT = 5537
005887
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19273961
58 X = -5874703
49
Y = -8846527
32 feet Y = -2696421
53 meter
Z = -6774632
48 Z = -2064907
98
XDOT = 916
768389 XDOT = 279
431005
YDOT = -15902
593477 feet/sec YDOT = -4847
110492 meter/sec
ZDOT = 18184
483208 ZDOT = 5542
630482
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 19024
04783357
00016717 00000-0 10270-3 0 9167
2 25544 51
6410 358
1124 0004387 300
1557 59
9161 15
53234844 32854
Satellite: ISS
Catalog Number: 25544
Epoch time: 19024
04783357 = yrday
fracday
Element set: 916
Inclination: 51
6410 deg
RA of node: 358
1124 deg
Eccentricity:
0004387
Arg of perigee: 300
1557 deg
Mean anomaly: 59
9161 deg
Mean motion: 15
53234844 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3285
Checksum: 305
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