[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 12th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14601 2445 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 584 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
284/20:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
5
000/00:00:00
000 0
0 0
0 219
1
289/20:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
0
000/00:00:00
000 0
0 0
0 219
5
292/20:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
8
000/00:00:00
000 0
0 0
0 220
1
297/21:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
1
000/00:00:00
000 0
0 0
0 220
7
Coasting Arc #1 (Orbit 3329)
---------------------------------------
Vector Time (GMT): 2019/284/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5790397
73 A = 6796028
18 meter
Y = 962085
99 meter E =
0017740
Z = 3415633
74 I = 51
87276
XDOT = 1774
266191 Wp = 106
40927
YDOT = -5844
390170 meter/sec RA = 143
39098 deg
ZDOT = 4629
241722 TA = 293
33486
MA = 293
52142
Ha = 229
454 n
mi
Hp = 219
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18997367
87 X = -5817317
13
Y = 3156450
11 feet Y = 897183
49 meter
Z = 11206147
44 Z = 3387440
39
XDOT = 5821
083303 XDOT = 1817
001462
YDOT = -19174
508433 feet/sec YDOT = -5824
309680 meter/sec
ZDOT = 15187
800924 ZDOT = 4637
964891
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17021992
01 X = 5188303
17
Y = -9164058
94 feet Y = -2793205
17 meter
Z = 11077577
14 Z = 3376445
51
XDOT = 131
324060 XDOT = 40
027574
YDOT = 18750
968803 feet/sec YDOT = 5715
295291 meter/sec
ZDOT = 15227
849945 ZDOT = 4641
448663
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 19284
55742076
00016717 00000-0 10270-3 0 9007
2 25544 51
6418 144
2219 0006811 137
9790 222
1884 15
50178645 33300
Satellite: ISS
Catalog Number: 25544
Epoch time: 19284
55742076 = yrday
fracday
Element set: 900
Inclination: 51
6418 deg
RA of node: 144
2219 deg
Eccentricity:
0006811
Arg of perigee: 137
9790 deg
Mean anomaly: 222
1884 deg
Mean motion: 15
50178645 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3330
Checksum: 311
Coasting Arc #2 (Orbit 3334)
---------------------------------------
Vector Time (GMT): 2019/284/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5077227
01 A = 6792457
85 meter
Y = 480745
15 meter E =
0013341
Z = -4496267
65 I = 51
87084
XDOT = -3449
693187 Wp = 101
36842
YDOT = 6001
085794 meter/sec RA = 141
61937 deg
ZDOT = -3264
548915 TA = 135
84641
MA = 135
73984
Ha = 229
518 n
mi
Hp = 219
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16657568
94 X = 5093314
47
Y = 1577247
87 feet Y = 537611
80 meter
Z = -14751534
29 Z = -4471565
06
XDOT = -11317
891034 XDOT = -3500
685121
YDOT = 19688
601686 feet/sec YDOT = 5962
223456 meter/sec
ZDOT = -10710
462318 ZDOT = -3281
430869
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13375110
51 X = 4076733
68
Y = 10216546
14 feet Y = 3114003
26 meter
Z = -14638944
00 Z = -4461950
13
XDOT = -19224
673222 XDOT = -5859
680398
YDOT = 9761
846249 feet/sec YDOT = 2975
410737 meter/sec
ZDOT = -10787
716874 ZDOT = -3288
096103
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 19284
87974840
00016717 00000-0 10270-3 0 9019
2 25544 51
6422 142
6214 0007279 142
8119 217
3537 15
50175576 33357
Satellite: ISS
Catalog Number: 25544
Epoch time: 19284
87974840 = yrday
fracday
Element set: 901
Inclination: 51
6422 deg
RA of node: 142
6214 deg
Eccentricity:
0007279
Arg of perigee: 142
8119 deg
Mean anomaly: 217
3537 deg
Mean motion: 15
50175576 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3335
Checksum: 320
Coasting Arc #3 (Orbit 3350)
---------------------------------------
Vector Time (GMT): 2019/285/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4891886
86 A = 6791560
82 meter
Y = -437563
47 meter E =
0014894
Z = 4685357
67 I = 51
89410
XDOT = 3341
486097 Wp = 129
72591
YDOT = -6264
749340 meter/sec RA = 136
67931 deg
ZDOT = 2888
344592 TA = 291
58282
MA = 291
74146
Ha = 229
445 n
mi
Hp = 219
054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16049497
56 X = -4909389
56
Y = -1435575
68 feet Y = -492365
40 meter
Z = 15371908
36 Z = 4661551
86
XDOT = 10962
880895 XDOT = 3397
261790
YDOT = -20553
639568 feet/sec YDOT = -6227
070339 meter/sec
ZDOT = 9476
196168 ZDOT = 2904
712625
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13104343
98 X = -3994204
04
Y = -9552366
81 feet Y = -2911561
40 meter
Z = 15263396
52 Z = 4652283
26
XDOT = 19234
093689 XDOT = 5862
551756
YDOT = -11043
566873 feet/sec YDOT = -3366
079183 meter/sec
ZDOT = 9551
135749 ZDOT = 2911
186176
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 19285
91119338
00016717 00000-0 10270-3 0 9029
2 25544 51
6425 137
5100 0007207 145
6108 214
5510 15
50223728 33518
Satellite: ISS
Catalog Number: 25544
Epoch time: 19285
91119338 = yrday
fracday
Element set: 902
Inclination: 51
6425 deg
RA of node: 137
5100 deg
Eccentricity:
0007207
Arg of perigee: 145
6108 deg
Mean anomaly: 214
5510 deg
Mean motion: 15
50223728 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3351
Checksum: 281
Coasting Arc #4 (Orbit 3365)
---------------------------------------
Vector Time (GMT): 2019/286/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4703651
82 A = 6790917
15 meter
Y = 480314
11 meter E =
0015028
Z = -4886302
62 I = 51
91353
XDOT = -3210
413206 Wp = 100
27970
YDOT = 6495
196078 meter/sec RA = 131
74047 deg
ZDOT = -2460
981829 TA = 145
65057
MA = 145
55332
Ha = 229
364 n
mi
Hp = 219
344
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15431928
55 X = 4721666
65
Y = 1575833
71 feet Y = 533013
95 meter
Z = -16031176
59 Z = -4863409
87
XDOT = -10532
851727 XDOT = -3270
851439
YDOT = 21309
698417 feet/sec YDOT = 6458
956815 meter/sec
ZDOT = -8074
087365 ZDOT = -2476
724516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12665735
70 X = 3860516
24
Y = 9140117
07 feet Y = 2785907
68 meter
Z = -15926823
05 Z = -4854495
66
XDOT = -19069
092771 XDOT = -5812
259476
YDOT = 12281
721302 feet/sec YDOT = 3743
468653 meter/sec
ZDOT = -8146
204949 ZDOT = -2482
963268
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 19286
87817358
00016717 00000-0 10270-3 0 9033
2 25544 51
6410 132
7186 0007173 148
9925 211
1650 15
50177859 33665
Satellite: ISS
Catalog Number: 25544
Epoch time: 19286
87817358 = yrday
fracday
Element set: 903
Inclination: 51
6410 deg
RA of node: 132
7186 deg
Eccentricity:
0007173
Arg of perigee: 148
9925 deg
Mean anomaly: 211
1650 deg
Mean motion: 15
50177859 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3366
Checksum: 332
Coasting Arc #5 (Orbit 3381)
---------------------------------------
Vector Time (GMT): 2019/287/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4536044
71 A = 6790173
53 meter
Y = -504383
49 meter E =
0012806
Z = 5023392
51 I = 51
93292
XDOT = 3033
108168 Wp = 139
36264
YDOT = -6734
433729 meter/sec RA = 126
80264 deg
ZDOT = 2050
264702 TA = 290
70758
MA = 290
84481
Ha = 229
308 n
mi
Hp = 219
286
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14882036
47 X = -4554468
86
Y = -1654801
46 feet Y = -555211
37 meter
Z = 16480946
56 Z = 5001312
87
XDOT = 9951
142282 XDOT = 3098
229845
YDOT = -22094
598850 feet/sec YDOT = -6700
151095 meter/sec
ZDOT = 6726
590231 ZDOT = 2065
157450
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12304680
18 X = -3750466
52
Y = -8724433
34 feet Y = -2659207
28 meter
Z = 16380295
64 Z = 4992714
11
XDOT = 18749
814003 XDOT = 5714
943308
YDOT = -13609
829637 feet/sec YDOT = -4148
276073 meter/sec
ZDOT = 6794
865131 ZDOT = 2071
074892
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 19287
90961469
00016717 00000-0 10270-3 0 9042
2 25544 51
6411 127
6073 0007154 152
7708 207
3819 15
50222436 33829
Satellite: ISS
Catalog Number: 25544
Epoch time: 19287
90961469 = yrday
fracday
Element set: 904
Inclination: 51
6411 deg
RA of node: 127
6073 deg
Eccentricity:
0007154
Arg of perigee: 152
7708 deg
Mean anomaly: 207
3819 deg
Mean motion: 15
50222436 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3382
Checksum: 315
Coasting Arc #6 (Orbit 3396)
---------------------------------------
Vector Time (GMT): 2019/288/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4381051
74 A = 6789727
19 meter
Y = 608631
88 meter E =
0016470
Z = -5164311
94 I = 51
94967
XDOT = -2833
959872 Wp = 102
96713
YDOT = 6925
198479 meter/sec RA = 121
86495 deg
ZDOT = -1595
853408 TA = 151
71795
MA = 151
62842
Ha = 229
180 n
mi
Hp = 219
595
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14373529
34 X = 4399006
25
Y = 1996823
76 feet Y = 657723
98 meter
Z = -16943280
65 Z = -5142986
31
XDOT = -9297
768610 XDOT = -2903
436851
YDOT = 22720
467452 feet/sec YDOT = 6893
118574 meter/sec
ZDOT = -5235
739528 ZDOT = -1609
789244
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11846091
56 X = 3610688
71
Y = 8575576
97 feet Y = 2613835
86 meter
Z = -16846067
93 Z = -5134681
50
XDOT = -18234
983169 XDOT = -5558
022870
YDOT = 14829
563980 feet/sec YDOT = 4520
051101 meter/sec
ZDOT = -5299
683992 ZDOT = -1615
343681
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 19288
87658968
00016717 00000-0 10270-3 0 9057
2 25544 51
6406 122
8151 0007083 156
0829 204
0652 15
50183654 33972
Satellite: ISS
Catalog Number: 25544
Epoch time: 19288
87658968 = yrday
fracday
Element set: 905
Inclination: 51
6406 deg
RA of node: 122
8151 deg
Eccentricity:
0007083
Arg of perigee: 156
0829 deg
Mean anomaly: 204
0652 deg
Mean motion: 15
50183654 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3397
Checksum: 333
Coasting Arc #7 (Orbit 3411)
---------------------------------------
Vector Time (GMT): 2019/289/20:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1426561
49 A = 6792264
64 meter
Y = 4915481
39 meter E =
0015020
Z = -4480545
97 I = 51
97547
XDOT = -5207
366040 Wp = 130
87588
YDOT = 4525
096178 meter/sec RA = 117
01564 deg
ZDOT = 3304
068516 TA = 172
38850
MA = 172
36568
Ha = 229
014 n
mi
Hp = 219
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4680319
85 X = 1393253
71
Y = 16126907
46 feet Y = 4931247
80 meter
Z = -14699953
96 Z = -4473697
17
XDOT = -17084
534252 XDOT = -5273
629714
YDOT = 14846
116069 feet/sec YDOT = 4466
493362 meter/sec
ZDOT = 10840
119803 ZDOT = 3278
611282
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5569401
70 X = -1697553
64
Y = 15870506
40 feet Y = 4837330
35 meter
Z = -14669014
14 Z = -4471115
51
XDOT = -21444
663221 XDOT = -6536
333350
YDOT = 2393
403281 feet/sec YDOT = 729
509320 meter/sec
ZDOT = 10723
752208 ZDOT = 3268
599673
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 19289
84356011
00016717 00000-0 10270-3 0 9060
2 25544 51
6410 118
0231 0007049 157
7710 202
3747 15
50234637 34124
Satellite: ISS
Catalog Number: 25544
Epoch time: 19289
84356011 = yrday
fracday
Element set: 906
Inclination: 51
6410 deg
RA of node: 118
0231 deg
Eccentricity:
0007049
Arg of perigee: 157
7710 deg
Mean anomaly: 202
3747 deg
Mean motion: 15
50234637 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3412
Checksum: 288
Coasting Arc #8 (Orbit 3427)
---------------------------------------
Vector Time (GMT): 2019/290/20:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1503071
47 A = 6793102
99 meter
Y = -5087940
70 meter E =
0012432
Z = 4229863
39 I = 51
99281
XDOT = 4956
599981 Wp = 108
24674
YDOT = -4539
194998 meter/sec RA = 112
08261 deg
ZDOT = -3693
619881 TA = 19
45687
MA = 19
40946
Ha = 228
927 n
mi
Hp = 219
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4931336
85 X = -1466611
79
Y = -16692718
85 feet Y = -5104545
17 meter
Z = 13877504
56 Z = 4222650
50
XDOT = 16261
810960 XDOT = 5024
932208
YDOT = -14892
372040 feet/sec YDOT = -4483
384798 meter/sec
ZDOT = -12118
175461 ZDOT = -3669
375897
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5417597
72 X = 1651283
78
Y = -16568576
67 feet Y = -5050102
17 meter
Z = 13844926
17 Z = 4219933
50
XDOT = 20714
722910 XDOT = 6313
847543
YDOT = -3274
154015 feet/sec YDOT = -997
962144 meter/sec
ZDOT = -12007
317975 ZDOT = -3659
830519
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 19290
87499285
00016717 00000-0 10270-3 0 9077
2 25544 51
6413 112
9117 0006898 162
5370 197
6019 15
50247042 34289
Satellite: ISS
Catalog Number: 25544
Epoch time: 19290
87499285 = yrday
fracday
Element set: 907
Inclination: 51
6413 deg
RA of node: 112
9117 deg
Eccentricity:
0006898
Arg of perigee: 162
5370 deg
Mean anomaly: 197
6019 deg
Mean motion: 15
50247042 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3428
Checksum: 330
Coasting Arc #9 (Orbit 3442)
---------------------------------------
Vector Time (GMT): 2019/291/20:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1624419
99 A = 6794023
08 meter
Y = 5273185
03 meter E =
0012057
Z = -3978008
67 I = 52
00668
XDOT = -4690
374829 Wp = 136
60367
YDOT = 4494
314810 meter/sec RA = 107
15121 deg
ZDOT = 4041
035301 TA = 175
48821
MA = 175
47733
Ha = 228
851 n
mi
Hp = 219
745
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5329461
90 X = 1584656
38
Y = 17300475
81 feet Y = 5291128
10 meter
Z = -13051209
56 Z = -3970214
26
XDOT = -15388
368861 XDOT = -4759
912522
YDOT = 14745
127328 feet/sec YDOT = 4441
474926 meter/sec
ZDOT = 13257
989833 ZDOT = 4018
081783
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5144656
64 X = -1568091
34
Y = 17382747
24 feet Y = 5298261
36 meter
Z = -13016001
87 Z = -3967277
37
XDOT = -19801
773888 XDOT = -6035
580681
YDOT = 3991
275075 feet/sec YDOT = 1216
540643 meter/sec
ZDOT = 13152
999332 ZDOT = 4009
034197
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 19291
84196125
00016717 00000-0 10270-3 0 9083
2 25544 51
6406 108
1201 0007045 164
6041 195
5325 15
50243105 34435
Satellite: ISS
Catalog Number: 25544
Epoch time: 19291
84196125 = yrday
fracday
Element set: 908
Inclination: 51
6406 deg
RA of node: 108
1201 deg
Eccentricity:
0007045
Arg of perigee: 164
6041 deg
Mean anomaly: 195
5325 deg
Mean motion: 15
50243105 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3443
Checksum: 282
Coasting Arc #10 (Orbit 3458)
---------------------------------------
Vector Time (GMT): 2019/292/20:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1761419
08 A = 6794933
26 meter
Y = -5425375
24 meter E =
0014242
Z = 3675942
41 I = 52
01967
XDOT = 4465
285436 Wp = 113
88569
YDOT = -4428
733690 meter/sec RA = 102
22062 deg
ZDOT = -4389
006361 TA = 22
70258
MA = 22
63966
Ha = 228
717 n
mi
Hp = 219
895
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5778933
98 X = -1718476
08
Y = -17799787
54 feet Y = -5444832
59 meter
Z = 12060178
52 Z = 3667490
19
XDOT = 14649
886600 XDOT = 4535
796718
YDOT = -14529
966174 feet/sec YDOT = -4378
405429 meter/sec
ZDOT = -14399
627169 ZDOT = -4367
144031
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4744240
74 X = 1446044
58
Y = -18128440
04 feet Y = -5525548
52 meter
Z = 12021990
76 Z = 3664302
78
XDOT = 18951
644788 XDOT = 5776
461332
YDOT = -4540
157986 feet/sec YDOT = -1383
840154 meter/sec
ZDOT = -14299
598238 ZDOT = -4358
517543
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 19292
87338817
00016717 00000-0 10270-3 0 9094
2 25544 51
6417 103
0085 0006793 169
5066 190
6228 15
50255955 34592
Satellite: ISS
Catalog Number: 25544
Epoch time: 19292
87338817 = yrday
fracday
Element set: 909
Inclination: 51
6417 deg
RA of node: 103
0085 deg
Eccentricity:
0006793
Arg of perigee: 169
5066 deg
Mean anomaly: 190
6228 deg
Mean motion: 15
50255955 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3459
Checksum: 340
Coasting Arc #11 (Orbit 3458)
---------------------------------------
Vector Time (GMT): 2019/292/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4031136
23 A = 6788838
96 meter
Y = 1151462
77 meter E =
0017707
Z = -5353895
12 I = 51
99906
XDOT = -1791
386008 Wp = 114
00899
YDOT = 7433
226866 meter/sec RA = 102
12391 deg
ZDOT = 243
507534 TA = 158
34361
MA = 158
26864
Ha = 228
790 n
mi
Hp = 220
071
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13225512
56 X = 4043967
38
Y = 3777765
01 feet Y = 1196613
57 meter
Z = -17565272
71 Z = -5334281
82
XDOT = -5877
250681 XDOT = -1875
556213
YDOT = 24387
227250 feet/sec YDOT = 7412
723696 meter/sec
ZDOT = 798
909232 ZDOT = 234
601107
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10636092
33 X = 3241880
94
Y = 8898965
66 feet Y = 2712404
73 meter
Z = -17475881
84 Z = -5326648
79
XDOT = -14684
143771 XDOT = -4475
727021
YDOT = 19079
882453 feet/sec YDOT = 5815
548172 meter/sec
ZDOT = 757
776191 ZDOT = 230
970183
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 19292
87338976
00016717 00000-0 10270-3 0 9102
2 25544 51
6418 103
0085 0006847 168
3972 191
7337 15
50200544 34593
Satellite: ISS
Catalog Number: 25544
Epoch time: 19292
87338976 = yrday
fracday
Element set: 910
Inclination: 51
6418 deg
RA of node: 103
0085 deg
Eccentricity:
0006847
Arg of perigee: 168
3972 deg
Mean anomaly: 191
7337 deg
Mean motion: 15
50200544 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3459
Checksum: 329
Coasting Arc #12 (Orbit 3474)
---------------------------------------
Vector Time (GMT): 2019/293/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4017505
24 A = 6788840
47 meter
Y = -1302606
26 meter E =
0006534
Z = 5311403
87 I = 52
00510
XDOT = 1499
974212 Wp = 144
81094
YDOT = -7484
475124 meter/sec RA = 97
19104 deg
ZDOT = -705
739973 TA = 311
86987
MA = 311
92561
Ha = 228
763 n
mi
Hp = 219
984
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13180791
46 X = -4028440
76
Y = -4273642
58 feet Y = -1347594
02 meter
Z = 17425865
70 Z = 5291861
47
XDOT = 4921
175236 XDOT = 1586
984447
YDOT = -24555
364580 feet/sec YDOT = -7467
214843 meter/sec
ZDOT = -2315
419858 ZDOT = -698
242275
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10550819
21 X = -3215889
69
Y = -9152787
08 feet Y = -2789769
50 meter
Z = 17336804
28 Z = 5284257
94
XDOT = 13518
111254 XDOT = 4120
320310
YDOT = -19873
148289 feet/sec YDOT = -6057
335598 meter/sec
ZDOT = -2280
689951 ZDOT = -695
154297
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 19293
90481383
00016717 00000-0 10270-3 0 9119
2 25544 51
6415 97
8978 0006779 171
2728 188
8542 15
50242537 34758
Satellite: ISS
Catalog Number: 25544
Epoch time: 19293
90481383 = yrday
fracday
Element set: 911
Inclination: 51
6415 deg
RA of node: 97
8978 deg
Eccentricity:
0006779
Arg of perigee: 171
2728 deg
Mean anomaly: 188
8542 deg
Mean motion: 15
50242537 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3475
Checksum: 351
Coasting Arc #13 (Orbit 3489)
---------------------------------------
Vector Time (GMT): 2019/294/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4049390
64 A = 6789247
94 meter
Y = 1489701
26 meter E =
0017042
Z = -5255904
69 I = 52
00973
XDOT = -1212
417069 Wp = 121
58144
YDOT = 7461
434579 meter/sec RA = 92
25741 deg
ZDOT = 1174
857019 TA = 159
68927
MA = 159
62140
Ha = 228
567 n
mi
Hp = 220
344
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13285402
38 X = 4057961
98
Y = 4887471
32 feet Y = 1535032
31 meter
Z = -17243781
78 Z = -5236213
22
XDOT = -3977
746290 XDOT = -1301
469755
YDOT = 24479
772240 feet/sec YDOT = 7447
378553 meter/sec
ZDOT = 3854
517779 ZDOT = 1168
751169
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10571081
13 X = 3222065
53
Y = 9577479
00 feet Y = 2919215
60 meter
Z = -17154050
30 Z = -5228554
53
XDOT = -12237
303031 XDOT = -3729
929964
YDOT = 20394
384313 feet/sec YDOT = 6216
208339 meter/sec
ZDOT = 3826
122812 ZDOT = 1166
202233
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 19294
87177351
00016717 00000-0 10270-3 0 9124
2 25544 51
6421 93
1058 0006742 175
2502 184
8713 15
50209560 34909
Satellite: ISS
Catalog Number: 25544
Epoch time: 19294
87177351 = yrday
fracday
Element set: 912
Inclination: 51
6421 deg
RA of node: 93
1058 deg
Eccentricity:
0006742
Arg of perigee: 175
2502 deg
Mean anomaly: 184
8713 deg
Mean motion: 15
50209560 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3490
Checksum: 307
Coasting Arc #14 (Orbit 3505)
---------------------------------------
Vector Time (GMT): 2019/295/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4103026
02 A = 6789524
81 meter
Y = -1641658
03 meter E =
0005798
Z = 5149732
46 I = 52
01025
XDOT = 928
699404 Wp = 131
65309
YDOT = -7432
591039 meter/sec RA = 87
32470 deg
ZDOT = -1632
028164 TA = 334
00385
MA = 334
03296
Ha = 228
559 n
mi
Hp = 220
243
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13461371
45 X = -4109378
36
Y = -5386017
15 feet Y = -1687576
37 meter
Z = 16895447
69 Z = 5129785
90
XDOT = 3046
914055 XDOT = 1019
671336
YDOT = -24385
141203 feet/sec YDOT = -7421
697044 meter/sec
ZDOT = -5354
423109 ZDOT = -1627
295735
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10716221
66 X = -3266304
36
Y = -9921852
05 feet Y = -3024180
50 meter
Z = 16804561
88 Z = 5122030
46
XDOT = 10953
459156 XDOT = 3338
614351
YDOT = -20847
331665 feet/sec YDOT = -6354
266691 meter/sec
ZDOT = -5332
282592 ZDOT = -1625
279734
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 19295
90319303
00016717 00000-0 10270-3 0 9135
2 25544 51
6410 87
9945 0006719 178
0625 182
0553 15
50252488 35061
Satellite: ISS
Catalog Number: 25544
Epoch time: 19295
90319303 = yrday
fracday
Element set: 913
Inclination: 51
6410 deg
RA of node: 87
9945 deg
Eccentricity:
0006719
Arg of perigee: 178
0625 deg
Mean anomaly: 182
0553 deg
Mean motion: 15
50252488 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3506
Checksum: 320
Coasting Arc #15 (Orbit 3520)
---------------------------------------
Vector Time (GMT): 2019/296/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4203840
39 A = 6790192
96 meter
Y = 1813124
33 meter E =
0015429
Z = -5028030
15 I = 52
01108
XDOT = -662
812678 Wp = 129
90692
YDOT = 7331
370235 meter/sec RA = 82
39142 deg
ZDOT = 2084
173599 TA = 160
34446
MA = 160
28493
Ha = 228
294 n
mi
Hp = 220
653
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13792127
28 X = 4207676
70
Y = 5948570
64 feet Y = 1860155
88 meter
Z = -16496161
91 Z = -5007600
02
XDOT = -2174
582276 XDOT = -754
868788
YDOT = 24053
051952 feet/sec YDOT = 7323
443566 meter/sec
ZDOT = 6837
839891 ZDOT = 2080
729970
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10999232
86 X = 3352566
17
Y = 10377252
23 feet Y = 3162986
48 meter
Z = -16403083
18 Z = -4999659
75
XDOT = -9622
582576 XDOT = -2932
963169
YDOT = 21010
083627 feet/sec YDOT = 6403
873489 meter/sec
ZDOT = 6821
574961 ZDOT = 2079
216048
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 19296
87014573
00016717 00000-0 10270-3 0 9144
2 25544 51
6427 83
2023 0006585 182
7710 177
3406 15
50222372 35213
Satellite: ISS
Catalog Number: 25544
Epoch time: 19296
87014573 = yrday
fracday
Element set: 914
Inclination: 51
6427 deg
RA of node: 83
2023 deg
Eccentricity:
0006585
Arg of perigee: 182
7710 deg
Mean anomaly: 177
3406 deg
Mean motion: 15
50222372 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3521
Checksum: 301
Coasting Arc #16 (Orbit 3536)
---------------------------------------
Vector Time (GMT): 2019/297/20:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4320492
75 A = 6790720
44 meter
Y = -1945240
11 meter E =
0006389
Z = 4858438
55 I = 52
00607
XDOT = 413
635703 Wp = 117
32137
YDOT = -7226
470017 meter/sec RA = 77
45851 deg
ZDOT = -2525
836639 TA = 357
38976
MA = 357
39309
Ha = 228
282 n
mi
Hp = 220
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14174844
97 X = -4322019
30
Y = -6382021
37 feet Y = -1993563
15 meter
Z = 15939759
01 Z = 4837447
35
XDOT = 1357
072515 XDOT = 506
682717
YDOT = -23708
891133 feet/sec YDOT = -7221
324346 meter/sec
ZDOT = -8286
865613 ZDOT = -2523
600888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11391547
08 X = -3472143
55
Y = -10720467
49 feet Y = -3267598
49 meter
Z = 15844133
80 Z = 4829291
98
XDOT = 8344
894369 XDOT = 2543
523804
YDOT = -21097
282225 feet/sec YDOT = -6430
451622 meter/sec
ZDOT = -8276
107499 ZDOT = -2522
557566
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 19297
90155827
00016717 00000-0 10270-3 0 9158
2 25544 51
6410 78
0906 0006522 185
3858 174
7224 15
50265196 35377
Satellite: ISS
Catalog Number: 25544
Epoch time: 19297
90155827 = yrday
fracday
Element set: 915
Inclination: 51
6410 deg
RA of node: 78
0906 deg
Eccentricity:
0006522
Arg of perigee: 185
3858 deg
Mean anomaly: 174
7224 deg
Mean motion: 15
50265196 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3537
Checksum: 329
Coasting Arc #17 (Orbit 3537)
---------------------------------------
Vector Time (GMT): 2019/297/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1854725
33 A = 6794500
07 meter
Y = 5304772
55 meter E =
0013206
Z = 3816512
09 I = 52
01650
XDOT = -4427
938169 Wp = 126
64434
YDOT = -4603
781428 meter/sec RA = 77
24670 deg
ZDOT = 4229
386513 TA = 278
81889
MA = 278
96841
Ha = 228
112 n
mi
Hp = 220
662
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6085056
85 X = -1932445
73
Y = 17404109
43 feet Y = 5283597
38 meter
Z = 12521365
12 Z = 3807313
31
XDOT = -14527
356196 XDOT = -4396
672535
YDOT = -15104
269777 feet/sec YDOT = -4653
122681 meter/sec
ZDOT = 13875
940002 ZDOT = 4207
953193
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6286442
32 X = -1916107
62
Y = 17362923
21 feet Y = 5292218
99 meter
Z = 12478985
02 Z = 3803594
63
XDOT = -13252
512106 XDOT = -4039
365690
YDOT = -14743
125065 feet/sec YDOT = -4493
704520 meter/sec
ZDOT = 13778
502868 ZDOT = 4199
687674
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 19297
96602155
00016717 00000-0 10270-3 0 9166
2 25544 51
6392 77
7715 0006535 187
1869 172
9189 15
50259192 35386
Satellite: ISS
Catalog Number: 25544
Epoch time: 19297
96602155 = yrday
fracday
Element set: 916
Inclination: 51
6392 deg
RA of node: 77
7715 deg
Eccentricity:
0006535
Arg of perigee: 187
1869 deg
Mean anomaly: 172
9189 deg
Mean motion: 15
50259192 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3538
Checksum: 356
Coasting Arc #18 (Orbit 3552)
---------------------------------------
Vector Time (GMT): 2019/298/21:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1742420
74 A = 6793572
01 meter
Y = -5118283
16 meter E =
0007130
Z = -4115596
12 I = 52
00451
XDOT = 4662
984939 Wp = 123
98724
YDOT = 4687
669423 meter/sec RA = 72
31490 deg
ZDOT = -3864
219625 TA = 106
23934
MA = 106
16089
Ha = 228
088 n
mi
Hp = 220
828
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5716603
48 X = 1819517
00
Y = -16792267
59 feet Y = -5098367
40 meter
Z = -13502611
93 Z = -4106944
32
XDOT = 15298
507017 XDOT = 4628
990061
YDOT = 15379
492859 feet/sec YDOT = 4739
623864 meter/sec
ZDOT = -12677
885910 ZDOT = -3841
651093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5631448
35 X = 1716465
46
Y = -16852950
90 feet Y = -5136779
44 meter
Z = -13462732
65 Z = -4103440
91
XDOT = 14314
929210 XDOT = 4363
190423
YDOT = 14806
190669 feet/sec YDOT = 4512
926916 meter/sec
ZDOT = -12575
287401 ZDOT = -3832
947600
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 19298
93297035
00016717 00000-0 10270-3 0 9172
2 25544 51
6390 72
9786 0006475 189
7422 170
3598 15
50233015 35534
Satellite: ISS
Catalog Number: 25544
Epoch time: 19298
93297035 = yrday
fracday
Element set: 917
Inclination: 51
6390 deg
RA of node: 72
9786 deg
Eccentricity:
0006475
Arg of perigee: 189
7422 deg
Mean anomaly: 170
3598 deg
Mean motion: 15
50233015 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3553
Checksum: 340
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