[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 2nd 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19998 2692 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
276/07:36:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
9
000/00:00:00
000 0
0 0
0 218
4
278/06:48:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
9
000/00:00:00
000 0
0 0
0 218
5
281/10:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
6
000/00:00:00
000 0
0 0
0 218
7
284/20:40:00
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
2
Coasting Arc #1 (Orbit 3189)
---------------------------------------
Vector Time (GMT): 2019/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 964293
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6712880
93 A = 6801004
64 meter
Y = 1038555
54 meter E =
0018659
Z = -132667
04 I = 51
60448
XDOT = -831
937369 Wp = 124
62962
YDOT = 4688
525767 meter/sec RA = 187
90773 deg
ZDOT = -6004
570270 TA = 56
79806
MA = 56
61929
Ha = 229
977 n
mi
Hp = 218
348
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22023887
55 X = 6701413
01
Y = 3407334
43 feet Y = 1113559
58 meter
Z = -435259
31 Z = -100085
73
XDOT = -2729
453310 XDOT = -855
136621
YDOT = 15382
302385 feet/sec YDOT = 4679
092411 meter/sec
ZDOT = -19700
033694 ZDOT = -6008
668184
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22283143
53 X = -6791902
15
Y = 479762
18 feet Y = 146231
51 meter
Z = -286956
87 Z = -87464
45
XDOT = -86
142282 XDOT = -26
256168
YDOT = -13973
375721 feet/sec YDOT = -4259
084920 meter/sec
ZDOT = -19718
904707 ZDOT = -6010
322155
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 19275
53213308
00016717 00000-0 10270-3 0 9006
2 25544 51
6421 188
9438 0007328 106
1989 253
9968 15
50119890 31900
Satellite: ISS
Catalog Number: 25544
Epoch time: 19275
53213308 = yrday
fracday
Element set: 900
Inclination: 51
6421 deg
RA of node: 188
9438 deg
Eccentricity:
0007328
Arg of perigee: 106
1989 deg
Mean anomaly: 253
9968 deg
Mean motion: 15
50119890 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3190
Checksum: 330
Coasting Arc #2 (Orbit 3202)
---------------------------------------
Vector Time (GMT): 2019/276/07:36:30
000
Vector Time (MET): N/A
Weight (LBS) : 949220
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2766426
26 A = 6791403
78 meter
Y = -3967806
10 meter E =
0014910
Z = 4758094
54 I = 51
59645
XDOT = 6993
764956 Wp = 114
24275
YDOT = -1652
142933 meter/sec RA = 183
87652 deg
ZDOT = 2675
931080 TA = 309
24876
MA = 309
38098
Ha = 229
921 n
mi
Hp = 218
396
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9076201
62 X = -2744964
03
Y = -13017736
55 feet Y = -3998622
03 meter
Z = 15610546
40 Z = 4744708
37
XDOT = 22945
423083 XDOT = 6998
721515
YDOT = -5420
416446 feet/sec YDOT = -1573
905896 meter/sec
ZDOT = 8779
301443 ZDOT = 2709
916799
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5407784
96 X = -1648292
86
Y = 14982942
73 feet Y = 4566800
94 meter
Z = 15549770
05 Z = 4739569
91
XDOT = -16462
154241 XDOT = -5017
664613
YDOT = -15256
925703 feet/sec YDOT = -4650
310954 meter/sec
ZDOT = 8934
139417 ZDOT = 2723
125694
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 19276
37021323
00016717 00000-0 10270-3 0 9014
2 25544 51
6387 184
7911 0007218 109
9986 250
1942 15
50155246 32038
Satellite: ISS
Catalog Number: 25544
Epoch time: 19276
37021323 = yrday
fracday
Element set: 901
Inclination: 51
6387 deg
RA of node: 184
7911 deg
Eccentricity:
0007218
Arg of perigee: 109
9986 deg
Mean anomaly: 250
1942 deg
Mean motion: 15
50155246 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3203
Checksum: 306
Coasting Arc #3 (Orbit 3217)
---------------------------------------
Vector Time (GMT): 2019/277/07:36:30
000
Vector Time (MET): N/A
Weight (LBS) : 949220
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2633373
28 A = 6790784
22 meter
Y = 3863196
02 meter E =
0018303
Z = -4941044
99 I = 51
62811
XDOT = -7049
127868 Wp = 88
49520
YDOT = 1923
100233 meter/sec RA = 178
91702 deg
ZDOT = -2260
095986 TA = 159
39886
MA = 159
32497
Ha = 229
898 n
mi
Hp = 218
496
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8639676
10 X = 2613979
33
Y = 12674527
64 feet Y = 3892535
67 meter
Z = -16210777
52 Z = -4928300
12
XDOT = -23127
059936 XDOT = -7059
130197
YDOT = 6309
383967 feet/sec YDOT = 1844
215915 meter/sec
ZDOT = -7415
013077 ZDOT = -2294
362786
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5125210
86 X = 1562164
27
Y = -14522145
45 feet Y = -4426349
93 meter
Z = -16152908
92 Z = -4923406
64
XDOT = 17594
169952 XDOT = 5362
703001
YDOT = 14605
895552 feet/sec YDOT = 4451
876964 meter/sec
ZDOT = -7571
168202 ZDOT = -2307
692068
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 19277
33722830
00016717 00000-0 10270-3 0 9023
2 25544 51
6393 179
9984 0007303 112
9748 247
2174 15
50130792 32185
Satellite: ISS
Catalog Number: 25544
Epoch time: 19277
33722830 = yrday
fracday
Element set: 902
Inclination: 51
6393 deg
RA of node: 179
9984 deg
Eccentricity:
0007303
Arg of perigee: 112
9748 deg
Mean anomaly: 247
2174 deg
Mean motion: 15
50130792 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3218
Checksum: 322
Coasting Arc #4 (Orbit 3232)
---------------------------------------
Vector Time (GMT): 2019/278/06:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 949220
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3349168
06 A = 6791371
77 meter
Y = 3469417
65 meter E =
0017144
Z = -4797095
33 I = 51
66245
XDOT = -6626
626749 Wp = 89
22600
YDOT = 2771
679869 meter/sec RA = 174
13242 deg
ZDOT = -2629
837809 TA = 154
81912
MA = 154
73543
Ha = 229
882 n
mi
Hp = 218
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10988084
20 X = 3333424
95
Y = 11382603
84 feet Y = 3506782
24 meter
Z = -15738501
74 Z = -4780864
52
XDOT = -21740
901409 XDOT = -6644
353562
YDOT = 9093
437890 feet/sec YDOT = 2697
477058 meter/sec
ZDOT = -8628
076801 ZDOT = -2662
070911
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5686342
86 X = 1733197
30
Y = -14841964
34 feet Y = -4523830
73 meter
Z = -15664727
93 Z = -4774609
07
XDOT = 16258
459581 XDOT = 4955
578480
YDOT = 15462
946999 feet/sec YDOT = 4713
106245 meter/sec
ZDOT = -8775
031436 ZDOT = -2674
629582
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 19278
30423838
00016717 00000-0 10270-3 0 9038
2 25544 51
6394 175
2067 0007325 115
9053 244
2853 15
50135981 32336
Satellite: ISS
Catalog Number: 25544
Epoch time: 19278
30423838 = yrday
fracday
Element set: 903
Inclination: 51
6394 deg
RA of node: 175
2067 deg
Eccentricity:
0007325
Arg of perigee: 115
9053 deg
Mean anomaly: 244
2853 deg
Mean motion: 15
50135981 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3233
Checksum: 308
Coasting Arc #5 (Orbit 3248)
---------------------------------------
Vector Time (GMT): 2019/279/06:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 949220
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3222583
92 A = 6790634
44 meter
Y = -3355895
93 meter E =
0013763
Z = 4938550
58 I = 51
69305
XDOT = 6656
562421 Wp = 121
12492
YDOT = -3075
509991 meter/sec RA = 169
17970 deg
ZDOT = 2242
166400 TA = 306
93355
MA = 307
05953
Ha = 229
818 n
mi
Hp = 218
539
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10572781
88 X = -3208806
69
Y = -11010157
26 feet Y = -3391855
93 meter
Z = 16202593
78 Z = 4922929
96
XDOT = 21839
115555 XDOT = 6679
567669
YDOT = -10090
255877 feet/sec YDOT = -3000
942906 meter/sec
ZDOT = 7356
188975 ZDOT = 2274
557666
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5273828
03 X = -1607462
78
Y = 14404515
61 feet Y = 4390496
36 meter
Z = 16131583
70 Z = 4916906
71
XDOT = -17505
168381 XDOT = -5335
575323
YDOT = -14855
384520 feet/sec YDOT = -4527
921202 meter/sec
ZDOT = 7503
901252 ZDOT = 2287
189102
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 19279
33571266
00016717 00000-0 10270-3 0 9042
2 25544 51
6390 170
0966 0007144 119
9819 240
2042 15
50170534 32492
Satellite: ISS
Catalog Number: 25544
Epoch time: 19279
33571266 = yrday
fracday
Element set: 904
Inclination: 51
6390 deg
RA of node: 170
0966 deg
Eccentricity:
0007144
Arg of perigee: 119
9819 deg
Mean anomaly: 240
2042 deg
Mean motion: 15
50170534 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3249
Checksum: 308
Coasting Arc #6 (Orbit 3263)
---------------------------------------
Vector Time (GMT): 2019/280/06:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 949220
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3061772
20 A = 6790126
16 meter
Y = 3310661
80 meter E =
0018700
Z = -5092400
20 I = 51
72390
XDOT = -6629
584410 Wp = 92
95452
YDOT = 3356
975231 meter/sec RA = 164
22664 deg
ZDOT = -1810
254686 TA = 159
53553
MA = 159
46051
Ha = 229
750 n
mi
Hp = 218
705
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10045184
38 X = 3049260
02
Y = 10861751
30 feet Y = 3344830
51 meter
Z = -16707349
73 Z = -5077557
73
XDOT = -21750
605019 XDOT = -6657
837106
YDOT = 11013
698266 feet/sec YDOT = 3282
680490 meter/sec
ZDOT = -5939
155793 ZDOT = -1842
527623
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5128573
38 X = 1563189
17
Y = -13958196
85 feet Y = -4254458
40 meter
Z = -16639873
24 Z = -5071833
36
XDOT = 18586
342675 XDOT = 5665
117247
YDOT = 14058
476119 feet/sec YDOT = 4285
023521 meter/sec
ZDOT = -6086
363760 ZDOT = -1855
123674
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 19280
30271969
00016717 00000-0 10270-3 0 9059
2 25544 51
6392 165
3042 0007183 123
3082 236
8758 15
50142719 32646
Satellite: ISS
Catalog Number: 25544
Epoch time: 19280
30271969 = yrday
fracday
Element set: 905
Inclination: 51
6392 deg
RA of node: 165
3042 deg
Eccentricity:
0007183
Arg of perigee: 123
3082 deg
Mean anomaly: 236
8758 deg
Mean motion: 15
50142719 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3264
Checksum: 309
Coasting Arc #7 (Orbit 3279)
---------------------------------------
Vector Time (GMT): 2019/281/06:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 949220
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2920648
26 A = 6789545
08 meter
Y = -3262259
20 meter E =
0011584
Z = 5182381
63 I = 51
75550
XDOT = 6587
662823 Wp = 126
81937
YDOT = -3667
702972 meter/sec RA = 159
27758 deg
ZDOT = 1394
906942 TA = 309
73651
MA = 309
83853
Ha = 229
681 n
mi
Hp = 218
695
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9582179
34 X = -2909124
89
Y = -10702950
15 feet Y = -3294855
23 meter
Z = 17002564
40 Z = 5168222
34
XDOT = 21613
067003 XDOT = 6621
410824
YDOT = -12033
146234 feet/sec YDOT = -3593
846301 meter/sec
ZDOT = 4576
466345 ZDOT = 1426
989626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4961619
65 X = -1512301
67
Y = 13562394
03 feet Y = 4133817
70 meter
Z = 16938190
50 Z = 5162760
46
XDOT = -19703
308956 XDOT = -6005
568570
YDOT = -13143
341521 feet/sec YDOT = -4006
090496 meter/sec
ZDOT = 4722
841884 ZDOT = 1439
522206
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 19281
33418866
00016717 00000-0 10270-3 0 9063
2 25544 51
6405 160
1940 0007021 127
4671 232
7119 15
50183600 32809
Satellite: ISS
Catalog Number: 25544
Epoch time: 19281
33418866 = yrday
fracday
Element set: 906
Inclination: 51
6405 deg
RA of node: 160
1940 deg
Eccentricity:
0007021
Arg of perigee: 127
4671 deg
Mean anomaly: 232
7119 deg
Mean motion: 15
50183600 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3280
Checksum: 286
Coasting Arc #8 (Orbit 3281)
---------------------------------------
Vector Time (GMT): 2019/281/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 949220
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 904047
29 A = 6788996
37 meter
Y = 4147239
81 meter E =
0020946
Z = -5316405
50 I = 51
76155
XDOT = -7250
193670 Wp = 105
29625
YDOT = 2354
717386 meter/sec RA = 158
44778 deg
ZDOT = 600
587955 TA = 170
46276
MA = 170
42293
Ha = 229
594 n
mi
Hp = 218
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2966034
41 X = 883428
70
Y = 13606429
81 feet Y = 4157233
90 meter
Z = -17442275
25 Z = -5312064
28
XDOT = -23786
724638 XDOT = -7278
903286
YDOT = 7725
450743 feet/sec YDOT = 2273
480115 meter/sec
ZDOT = 1970
432924 ZDOT = 565
299239
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2400742
13 X = -731746
20
Y = -13742334
59 feet Y = -4188663
58 meter
Z = -17422684
50 Z = -5310434
24
XDOT = 23153
274267 XDOT = 7057
117997
YDOT = -6353
083344 feet/sec YDOT = -1936
419803 meter/sec
ZDOT = 1809
504726 ZDOT = 551
537040
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 19281
46312283
00016717 00000-0 10270-3 0 9074
2 25544 51
6433 159
5559 0007046 127
3162 232
8632 15
50176207 32827
Satellite: ISS
Catalog Number: 25544
Epoch time: 19281
46312283 = yrday
fracday
Element set: 907
Inclination: 51
6433 deg
RA of node: 159
5559 deg
Eccentricity:
0007046
Arg of perigee: 127
3162 deg
Mean anomaly: 232
8632 deg
Mean motion: 15
50176207 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3282
Checksum: 305
Coasting Arc #9 (Orbit 3297)
---------------------------------------
Vector Time (GMT): 2019/282/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 949220
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -793189
04 A = 6789106
14 meter
Y = -4221826
02 meter E =
0008708
Z = 5249722
02 I = 51
79292
XDOT = 7126
048540 Wp = 108
17280
YDOT = -2635
025155 meter/sec RA = 153
49990 deg
ZDOT = -1043
631425 TA = 351
79310
MA = 351
80734
Ha = 229
520 n
mi
Hp = 218
753
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2602326
24 X = -771420
76
Y = -13851135
22 feet Y = -4230573
91 meter
Z = 17223497
44 Z = 5245922
17
XDOT = 23379
424345 XDOT = 7160
053938
YDOT = -8645
095653 feet/sec YDOT = -2555
146592 meter/sec
ZDOT = -3423
987615 ZDOT = -1008
932808
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2263788
77 X = 690002
82
Y = 13931646
53 feet Y = 4246365
86 meter
Z = 17206376
68 Z = 5244503
61
XDOT = -22656
422373 XDOT = -6905
677539
YDOT = 7709
853630 feet/sec YDOT = 2349
963386 meter/sec
ZDOT = -3265
716227 ZDOT = -995
390306
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 19282
49458759
00016717 00000-0 10270-3 0 9088
2 25544 51
6432 154
4450 0006949 131
1526 229
0225 15
50208138 32980
Satellite: ISS
Catalog Number: 25544
Epoch time: 19282
49458759 = yrday
fracday
Element set: 908
Inclination: 51
6432 deg
RA of node: 154
4450 deg
Eccentricity:
0006949
Arg of perigee: 131
1526 deg
Mean anomaly: 229
0225 deg
Mean motion: 15
50208138 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3298
Checksum: 322
Coasting Arc #10 (Orbit 3312)
---------------------------------------
Vector Time (GMT): 2019/283/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 949220
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 694386
53 A = 6789564
22 meter
Y = 4351857
18 meter E =
0019957
Z = -5182631
39 I = 51
82294
XDOT = -6930
303699 Wp = 112
41803
YDOT = 2872
942008 meter/sec RA = 148
55410 deg
ZDOT = 1481
022973 TA = 171
86112
MA = 171
82870
Ha = 229
471 n
mi
Hp = 218
889
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2278171
03 X = 670845
72
Y = 14277746
65 feet Y = 4359490
22 meter
Z = -17003383
83 Z = -5179315
85
XDOT = -22737
216860 XDOT = -6969
108733
YDOT = 9425
662757 feet/sec YDOT = 2795
225616 meter/sec
ZDOT = 4858
999255 ZDOT = 1447
263423
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2170882
35 X = -661684
94
Y = -14312165
28 feet Y = -4362347
98 meter
Z = -16988477
54 Z = -5178087
95
XDOT = 21869
393487 XDOT = 6665
791135
YDOT = -8913
035819 feet/sec YDOT = -2716
693318 meter/sec
ZDOT = 4704
979268 ZDOT = 1434
077681
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 19283
46158668
00016717 00000-0 10270-3 0 9093
2 25544 51
6427 149
6537 0006967 134
3391 225
8331 15
50180865 33137
Satellite: ISS
Catalog Number: 25544
Epoch time: 19283
46158668 = yrday
fracday
Element set: 909
Inclination: 51
6427 deg
RA of node: 149
6537 deg
Eccentricity:
0006967
Arg of perigee: 134
3391 deg
Mean anomaly: 225
8331 deg
Mean motion: 15
50180865 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3313
Checksum: 334
Coasting Arc #11 (Orbit 3328)
---------------------------------------
Vector Time (GMT): 2019/284/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 949220
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -621543
83 A = 6789912
42 meter
Y = -4477217
21 meter E =
0009313
Z = 5058231
03 I = 51
85259
XDOT = 6746
600798 Wp = 102
89492
YDOT = -3102
484812 meter/sec RA = 143
61070 deg
ZDOT = -1916
171320 TA = 5
63513
MA = 5
62465
Ha = 229
357 n
mi
Hp = 218
967
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2039185
78 X = -596002
43
Y = -14689032
84 feet Y = -4484024
45 meter
Z = 16595246
15 Z = 5055274
23
XDOT = 22134
517054 XDOT = 6790
100055
YDOT = -10178
755945 feet/sec YDOT = -3026
796523 meter/sec
ZDOT = -6286
651313 ZDOT = -1883
292574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2175708
21 X = 663155
86
Y = 14684422
39 feet Y = 4475811
94 meter
Z = 16581983
96 Z = 5054188
71
XDOT = -21088
499001 XDOT = -6427
774496
YDOT = 10057
658109 feet/sec YDOT = 3065
574192 meter/sec
ZDOT = -6136
618990 ZDOT = -1870
441468
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
49304776
00016717 00000-0 10270-3 0 9102
2 25544 51
6428 144
5430 0006834 139
1292 221
0372 15
50216561 33293
Satellite: ISS
Catalog Number: 25544
Epoch time: 19284
49304776 = yrday
fracday
Element set: 910
Inclination: 51
6428 deg
RA of node: 144
5430 deg
Eccentricity:
0006834
Arg of perigee: 139
1292 deg
Mean anomaly: 221
0372 deg
Mean motion: 15
50216561 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3329
Checksum: 299
Coasting Arc #12 (Orbit 3334)
---------------------------------------
Vector Time (GMT): 2019/284/20:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 949220
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3818838
42 A = 6789679
87 meter
Y = 2173557
96 meter E =
0018006
Z = -5190699
84 I = 51
86153
XDOT = -5105
048825 Wp = 100
23406
YDOT = 5507
234506 meter/sec RA = 141
59324 deg
ZDOT = -1457
132375 TA = 155
79244
MA = 155
70773
Ha = 229
482 n
mi
Hp = 219
183
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12528997
44 X = 3819463
08
Y = 7131095
67 feet Y = 2216265
89 meter
Z = -17029855
11 Z = -5172147
82
XDOT = -16748
847850 XDOT = -5159
174873
YDOT = 18068
354678 feet/sec YDOT = 5449
843465 meter/sec
ZDOT = -4780
618029 ZDOT = -1482
063088
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7221142
15 X = 2201004
13
Y = 12591792
63 feet Y = 3837978
39 meter
Z = -16945386
74 Z = -5164953
88
XDOT = -22685
486456 XDOT = -6914
536272
YDOT = 6455
741408 feet/sec YDOT = 1967
709981 meter/sec
ZDOT = -4894
541097 ZDOT = -1491
856127
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
87984634
00016717 00000-0 10270-3 0 9112
2 25544 51
6423 142
6226 0007203 143
2429 216
9216 15
50156979 33352
Satellite: ISS
Catalog Number: 25544
Epoch time: 19284
87984634 = yrday
fracday
Element set: 911
Inclination: 51
6423 deg
RA of node: 142
6226 deg
Eccentricity:
0007203
Arg of perigee: 143
2429 deg
Mean anomaly: 216
9216 deg
Mean motion: 15
50156979 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3335
Checksum: 318
Coasting Arc #13 (Orbit 3350)
---------------------------------------
Vector Time (GMT): 2019/285/20:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 949220
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3677858
31 A = 6789165
98 meter
Y = -2202349
19 meter E =
0010702
Z = 5259633
93 I = 51
88615
XDOT = 4939
833617 Wp = 138
33924
YDOT = -5772
204035 meter/sec RA = 136
65177 deg
ZDOT = 1028
266464 TA = 301
79363
MA = 301
89783
Ha = 229
457 n
mi
Hp = 219
087
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12066464
27 X = -3678506
45
Y = -7225555
08 feet Y = -2243480
71 meter
Z = 17256016
85 Z = 5241766
63
XDOT = 16206
803204 XDOT = 4999
018107
YDOT = -18937
677281 feet/sec YDOT = -5716
632306 meter/sec
ZDOT = 3373
577638 ZDOT = 1052
407028
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6989594
90 X = -2130428
52
Y = -12318873
91 feet Y = -3754792
77 meter
Z = 17174668
33 Z = 5234838
91
XDOT = 22551
047186 XDOT = 6873
559182
YDOT = -7896
687559 feet/sec YDOT = -2406
910368 meter/sec
ZDOT = 3483
928532 ZDOT = 1061
901416
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
91130299
00016717 00000-0 10270-3 0 9129
2 25544 51
6426 137
5114 0007158 146
0319 214
1291 15
50206052 33511
Satellite: ISS
Catalog Number: 25544
Epoch time: 19285
91130299 = yrday
fracday
Element set: 912
Inclination: 51
6426 deg
RA of node: 137
5114 deg
Eccentricity:
0007158
Arg of perigee: 146
0319 deg
Mean anomaly: 214
1291 deg
Mean motion: 15
50206052 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3351
Checksum: 284
Coasting Arc #14 (Orbit 3365)
---------------------------------------
Vector Time (GMT): 2019/286/20:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 949220
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3542887
35 A = 6789053
62 meter
Y = 2303227
70 meter E =
0018885
Z = -5328902
11 I = 51
90726
XDOT = -4733
840814 Wp = 105
40715
YDOT = 5981
023395 meter/sec RA = 131
71157 deg
ZDOT = -568
735938 TA = 159
21005
MA = 159
13313
Ha = 229
328 n
mi
Hp = 219
388
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11623646
15 X = 3542754
05
Y = 7556521
32 feet Y = 2342845
54 meter
Z = -17483274
63 Z = -5311692
27
XDOT = -15530
973798 XDOT = -4797
607861
YDOT = 19622
780168 feet/sec YDOT = 5927
729649 meter/sec
ZDOT = -1865
931555 ZDOT = -591
887054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6654365
92 X = 2028250
73
Y = 12274484
60 feet Y = 3741262
90 meter
Z = -17404927
41 Z = -5305021
87
XDOT = -22152
602334 XDOT = -6752
113191
YDOT = 9244
256033 feet/sec YDOT = 2817
649239 meter/sec
ZDOT = -1971
800837 ZDOT = -601
004895
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
87829365
00016717 00000-0 10270-3 0 9135
2 25544 51
6411 132
7200 0007096 149
3050 210
8516 15
50161466 33665
Satellite: ISS
Catalog Number: 25544
Epoch time: 19286
87829365 = yrday
fracday
Element set: 913
Inclination: 51
6411 deg
RA of node: 132
7200 deg
Eccentricity:
0007096
Arg of perigee: 149
3050 deg
Mean anomaly: 210
8516 deg
Mean motion: 15
50161466 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3366
Checksum: 304
Coasting Arc #15 (Orbit 3381)
---------------------------------------
Vector Time (GMT): 2019/287/20:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 949220
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3437711
02 A = 6788788
68 meter
Y = -2387690
45 meter E =
0008733
Z = 5340259
74 I = 51
92834
XDOT = 4510
097666 Wp = 140
07489
YDOT = -6198
555148 meter/sec RA = 126
77299 deg
ZDOT = 125
227322 TA = 308
69721
MA = 308
77528
Ha = 229
306 n
mi
Hp = 219
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11278579
47 X = -3436696
31
Y = -7833630
10 feet Y = -2426127
28 meter
Z = 17520537
19 Z = 5323562
88
XDOT = 14796
908352 XDOT = 4578
468206
YDOT = -20336
467022 feet/sec YDOT = -6147
737759 meter/sec
ZDOT = 410
850793 ZDOT = 147
302750
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6430287
00 X = -1959951
48
Y = -12242589
85 feet Y = -3731541
38 meter
Z = 17444533
29 Z = 5317093
75
XDOT = 21676
234844 XDOT = 6606
916380
YDOT = -10624
715988 feet/sec YDOT = -3238
413433 meter/sec
ZDOT = 511
848085 ZDOT = 156
011296
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
90974648
00016717 00000-0 10270-3 0 9146
2 25544 51
6411 127
6089 0007115 153
3445 206
8073 15
50208875 33825
Satellite: ISS
Catalog Number: 25544
Epoch time: 19287
90974648 = yrday
fracday
Element set: 914
Inclination: 51
6411 deg
RA of node: 127
6089 deg
Eccentricity:
0007115
Arg of perigee: 153
3445 deg
Mean anomaly: 206
8073 deg
Mean motion: 15
50208875 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3382
Checksum: 325
Coasting Arc #16 (Orbit 3396)
---------------------------------------
Vector Time (GMT): 2019/288/20:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 949220
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3352749
17 A = 6788947
08 meter
Y = 2534771
96 meter E =
0018954
Z = -5346895
89 I = 51
94700
XDOT = -4252
427161 Wp = 112
06193
YDOT = 6348
703852 meter/sec RA = 121
83463 deg
ZDOT = 337
267897 TA = 161
18326
MA = 161
11311
Ha = 229
148 n
mi
Hp = 219
627
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10999833
22 X = 3350128
36
Y = 8316180
97 feet Y = 2572249
80 meter
Z = -17542309
36 Z = -5330615
59
XDOT = -13951
532682 XDOT = -4324
742461
YDOT = 20829
080879 feet/sec YDOT = 6300
745889 meter/sec
ZDOT = 1106
521973 ZDOT = 316
434641
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6173666
59 X = 1881733
58
Y = 12435238
55 feet Y = 3790260
71 meter
Z = -17468213
93 Z = -5324311
60
XDOT = -20944
813007 XDOT = -6383
979004
YDOT = 11846
361031 feet/sec YDOT = 3610
770842 meter/sec
ZDOT = 1011
157217 ZDOT = 308
200720
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
87673237
00016717 00000-0 10270-3 0 9154
2 25544 51
6406 122
8166 0007010 156
3108 203
8366 15
50168899 33974
Satellite: ISS
Catalog Number: 25544
Epoch time: 19288
87673237 = yrday
fracday
Element set: 915
Inclination: 51
6406 deg
RA of node: 122
8166 deg
Eccentricity:
0007010
Arg of perigee: 156
3108 deg
Mean anomaly: 203
8366 deg
Mean motion: 15
50168899 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3397
Checksum: 332
Coasting Arc #17 (Orbit 3412)
---------------------------------------
Vector Time (GMT): 2019/289/20:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 949220
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3297687
77 A = 6788945
55 meter
Y = -2661695
50 meter E =
0007252
Z = 5298752
44 I = 51
96477
XDOT = 3988
311518 Wp = 134
11529
YDOT = -6500
378547 meter/sec RA = 116
89843 deg
ZDOT = -787
416903 TA = 323
35234
MA = 323
40192
Ha = 229
113 n
mi
Hp = 219
557
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10819185
60 X = -3293417
92
Y = -8732596
78 feet Y = -2698548
49 meter
Z = 17384358
39 Z = 5282743
55
XDOT = 13085
011542 XDOT = 4064
529151
YDOT = -21326
701269 feet/sec YDOT = -6455
352303 meter/sec
ZDOT = -2583
388788 ZDOT = -767
857287
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6041727
48 X = -1841518
54
Y = -12622919
91 feet Y = -3847465
99 meter
Z = 17311509
53 Z = 5276548
10
XDOT = 20162
102462 XDOT = 6145
408830
YDOT = -13051
108768 feet/sec YDOT = -3977
977953 meter/sec
ZDOT = -2493
798377 ZDOT = -760
109745
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
90817862
00016717 00000-0 10270-3 0 9164
2 25544 51
6412 117
7054 0006954 159
6032 200
5398 15
50216949 34136
Satellite: ISS
Catalog Number: 25544
Epoch time: 19289
90817862 = yrday
fracday
Element set: 916
Inclination: 51
6412 deg
RA of node: 117
7054 deg
Eccentricity:
0006954
Arg of perigee: 159
6032 deg
Mean anomaly: 200
5398 deg
Mean motion: 15
50216949 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3413
Checksum: 324
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