[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 4th 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 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 031 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
124/06:48:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 217
3
128/05:34:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
0
000/00:00:00
000 0
0 0
0 217
2
131/09:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
1
000/00:00:00
000 0
0 0
0 217
3
134/18:04:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
2
000/00:00:00
000 0
0 0
0 217
1
Coasting Arc #1 (Orbit 831)
---------------------------------------
Vector Time (GMT): 2019/123/13:11:49
422
Vector Time (MET): N/A
Weight (LBS) : 944482
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1667613
40 A = 6787973
34 meter
Y = -5450814
55 meter E =
0010557
Z = 3677446
38 I = 51
38239
XDOT = 6261
991120 Wp = 95
39522
YDOT = 1000
592426 meter/sec RA = 221
96923 deg
ZDOT = 4311
062379 TA = 308
53953
MA = 308
63410
Ha = 222
893 n
mi
Hp = 217
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5471172
57 X = -1624400
21
Y = -17883249
84 feet Y = -5469221
34 meter
Z = 12065112
81 Z = 3669450
57
XDOT = 20544
590290 XDOT = 6229
395689
YDOT = 3282
783550 feet/sec YDOT = 1070
436151 meter/sec
ZDOT = 14143
905443 ZDOT = 4341
402150
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18125327
20 X = -5524599
73
Y = -4698728
24 feet Y = -1432172
37 meter
Z = 12029371
05 Z = 3666552
30
XDOT = 13218
902679 XDOT = 4029
121536
YDOT = -14332
128929 feet/sec YDOT = -4368
432898 meter/sec
ZDOT = 14281
057094 ZDOT = 4352
866202
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 19123
60645597
00016717 00000-0 10270-3 0 9005
2 25544 51
6417 222
7752 0001270 271
2755 88
8251 15
52638134 8325
Satellite: ISS
Catalog Number: 25544
Epoch time: 19123
60645597 = yrday
fracday
Element set: 900
Inclination: 51
6417 deg
RA of node: 222
7752 deg
Eccentricity:
0001270
Arg of perigee: 271
2755 deg
Mean anomaly: 88
8251 deg
Mean motion: 15
52638134 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 832
Checksum: 304
Coasting Arc #2 (Orbit 842)
---------------------------------------
Vector Time (GMT): 2019/124/06:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 944482
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5001036
51 A = 6793434
23 meter
Y = 4552217
82 meter E =
0009743
Z = -594684
31 I = 51
41624
XDOT = -3613
714709 Wp = 141
82867
YDOT = 3199
930712 meter/sec RA = 218
28710 deg
ZDOT = -5954
612864 TA = 44
60555
MA = 44
52719
Ha = 222
921 n
mi
Hp = 217
340
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16407600
11 X = 4952649
33
Y = 14935097
84 feet Y = 4607872
37 meter
Z = -1951064
01 Z = -570508
15
XDOT = -11856
019386 XDOT = -3620
303898
YDOT = 10498
460342 feet/sec YDOT = 3159
482850 meter/sec
ZDOT = -19536
131445 ZDOT = -5972
183246
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4120401
65 X = 1255898
42
Y = 21810599
62 feet Y = 6647870
76 meter
Z = -1842057
10 Z = -561459
00
XDOT = -14091
068624 XDOT = -4294
957717
YDOT = 1022
910213 feet/sec YDOT = 311
783033 meter/sec
ZDOT = -19615
856433 ZDOT = -5978
913041
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 19124
31446565
00016717 00000-0 10270-3 0 9019
2 25544 51
6384 219
2524 0001223 298
0719 62
0310 15
52670987 8435
Satellite: ISS
Catalog Number: 25544
Epoch time: 19124
31446565 = yrday
fracday
Element set: 901
Inclination: 51
6384 deg
RA of node: 219
2524 deg
Eccentricity:
0001223
Arg of perigee: 298
0719 deg
Mean anomaly: 62
0310 deg
Mean motion: 15
52670987 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 843
Checksum: 298
Coasting Arc #3 (Orbit 858)
---------------------------------------
Vector Time (GMT): 2019/125/06:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 944482
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4574747
22 A = 6792430
18 meter
Y = -4690507
66 meter E =
0013188
Z = 1765964
49 I = 51
43816
XDOT = 4612
597035 Wp = 62
25000
YDOT = -2360
784609 meter/sec RA = 213
30800 deg
ZDOT = 5652
208802 TA = 317
18989
MA = 317
29251
Ha = 223
018 n
mi
Hp = 217
409
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15009013
20 X = -4530534
88
Y = -15388804
64 feet Y = -4741418
53 meter
Z = 5793846
75 Z = 1743848
85
XDOT = 15133
192373 XDOT = 4611
197315
YDOT = -7745
356329 feet/sec YDOT = -2309
211331 meter/sec
ZDOT = 18543
992132 ZDOT = 5674
612064
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3118033
98 X = -950376
76
Y = -21295747
82 feet Y = -6490943
93 meter
Z = 5694157
94 Z = 1735579
34
XDOT = 15139
872282 XDOT = 4614
633072
YDOT = 2792
359242 feet/sec YDOT = 851
111097 meter/sec
ZDOT = 18645
523276 ZDOT = 5683
155495
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 19125
34429743
00016717 00000-0 10270-3 0 9023
2 25544 51
6373 214
1301 0001021 286
6165 73
4875 15
52625653 8593
Satellite: ISS
Catalog Number: 25544
Epoch time: 19125
34429743 = yrday
fracday
Element set: 902
Inclination: 51
6373 deg
RA of node: 214
1301 deg
Eccentricity:
0001021
Arg of perigee: 286
6165 deg
Mean anomaly: 73
4875 deg
Mean motion: 15
52625653 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 859
Checksum: 300
Coasting Arc #4 (Orbit 873)
---------------------------------------
Vector Time (GMT): 2019/126/06:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 944482
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3938742
06 A = 6790202
97 meter
Y = 4725286
96 meter E =
0003608
Z = -2875276
32 I = 51
45999
XDOT = -5553
870852 Wp = 118
64718
YDOT = 1566
740516 meter/sec RA = 208
32829 deg
ZDOT = -5039
754399 TA = 94
12880
MA = 94
08756
Ha = 223
010 n
mi
Hp = 217
375
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12922382
07 X = 3899576
60
Y = 15502909
96 feet Y = 4769113
90 meter
Z = -9433321
25 Z = -2856237
85
XDOT = -18221
361063 XDOT = -5546
496979
YDOT = 5140
224789 feet/sec YDOT = 1504
674751 meter/sec
ZDOT = -16534
627293 ZDOT = -5066
715587
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1730150
57 X = 527349
89
Y = 20148095
03 feet Y = 6141139
36 meter
Z = -9347543
59 Z = -2849131
29
XDOT = -16308
770311 XDOT = -4970
913191
YDOT = -6317
291981 feet/sec YDOT = -1925
510596 meter/sec
ZDOT = -16656
732276 ZDOT = -5076
971998
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 19126
30976143
00016717 00000-0 10270-3 0 9032
2 25544 51
6379 209
3287 0001048 296
6321 63
4723 15
52646855 8747
Satellite: ISS
Catalog Number: 25544
Epoch time: 19126
30976143 = yrday
fracday
Element set: 903
Inclination: 51
6379 deg
RA of node: 209
3287 deg
Eccentricity:
0001048
Arg of perigee: 296
6321 deg
Mean anomaly: 63
4723 deg
Mean motion: 15
52646855 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 874
Checksum: 323
Coasting Arc #5 (Orbit 889)
---------------------------------------
Vector Time (GMT): 2019/127/06:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3137687
92 A = 6787549
75 meter
Y = -4654897
71 meter E =
0010474
Z = 3807302
23 I = 51
48117
XDOT = 6372
220457 Wp = 95
80176
YDOT = -870
446749 meter/sec RA = 203
34448 deg
ZDOT = 4176
321133 TA = 310
03917
MA = 310
13102
Ha = 223
010 n
mi
Hp = 217
362
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10294251
70 X = -3103896
43
Y = -15271974
13 feet Y = -4689796
89 meter
Z = 12491149
04 Z = 3792141
95
XDOT = 20906
235095 XDOT = 6361
193817
YDOT = -2855
796421 feet/sec YDOT = -799
250091 meter/sec
ZDOT = 13701
840988 ZDOT = 4207
248722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -45597
43 X = -13898
10
Y = -18463560
08 feet Y = -5627693
11 meter
Z = 12422901
69 Z = 3786500
44
XDOT = 17496
289360 XDOT = 5332
868997
YDOT = 9294
357438 feet/sec YDOT = 2832
920147 meter/sec
ZDOT = 13841
858995 ZDOT = 4218
998622
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 19127
33958697
00016717 00000-0 10270-3 0 9041
2 25544 51
6381 204
2058 0001074 292
1165 67
9873 15
52653182 8900
Satellite: ISS
Catalog Number: 25544
Epoch time: 19127
33958697 = yrday
fracday
Element set: 904
Inclination: 51
6381 deg
RA of node: 204
2058 deg
Eccentricity:
0001074
Arg of perigee: 292
1165 deg
Mean anomaly: 67
9873 deg
Mean motion: 15
52653182 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 890
Checksum: 325
Coasting Arc #6 (Orbit 903)
---------------------------------------
Vector Time (GMT): 2019/128/05:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5282735
19 A = 6786876
16 meter
Y = 1557693
65 meter E =
0006023
Z = -3972090
71 I = 51
50759
XDOT = -4416
226474 Wp = 104
80686
YDOT = -4825
859001 meter/sec RA = 198
56665 deg
ZDOT = 3984
474019 TA = 206
83153
MA = 206
86270
Ha = 223
040 n
mi
Hp = 217
178
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17331808
37 X = -5280466
64
Y = 5110543
49 feet Y = 1498631
46 meter
Z = -13031793
66 Z = -3997746
99
XDOT = -14488
932000 XDOT = -4381
288771
YDOT = -15832
870738 feet/sec YDOT = -4875
049351 meter/sec
ZDOT = 13072
421321 ZDOT = 3963
105739
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14711495
19 X = -4484063
74
Y = -10345924
13 feet Y = -3153437
67 meter
Z = -13148028
19 Z = -4007518
99
XDOT = 2607
248103 XDOT = 794
689222
YDOT = -20183
222393 feet/sec YDOT = -6151
846185 meter/sec
ZDOT = 12976
078698 ZDOT = 3955
108787
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 19128
24068320
00016717 00000-0 10270-3 0 9058
2 25544 51
6372 199
7244 0000991 307
9838 52
1224 15
52637409 9040
Satellite: ISS
Catalog Number: 25544
Epoch time: 19128
24068320 = yrday
fracday
Element set: 905
Inclination: 51
6372 deg
RA of node: 199
7244 deg
Eccentricity:
0000991
Arg of perigee: 307
9838 deg
Mean anomaly: 52
1224 deg
Mean motion: 15
52637409 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 904
Checksum: 312
Coasting Arc #7 (Orbit 919)
---------------------------------------
Vector Time (GMT): 2019/129/05:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5969998
32 A = 6789662
94 meter
Y = -1047504
68 meter E =
0012077
Z = 3048324
21 I = 51
54724
XDOT = 3365
073089 Wp = 93
30858
YDOT = 4828
539777 meter/sec RA = 193
58674 deg
ZDOT = -4914
932732 TA = 51
68048
MA = 51
57196
Ha = 222
979 n
mi
Hp = 217
309
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19586608
67 X = 5966460
90
Y = -3436695
13 feet Y = -980764
06 meter
Z = 10001063
67 Z = 3077315
83
XDOT = 11040
266039 XDOT = 3334
703139
YDOT = 15841
665936 feet/sec YDOT = 4866
001057 meter/sec
ZDOT = -16125
107389 ZDOT = -4898
659584
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15036248
34 X = 4583048
49
Y = 12911760
95 feet Y = 3935504
74 meter
Z = 10132376
45 Z = 3088348
34
XDOT = -4234
890018 XDOT = -1290
794478
YDOT = 17569
254097 feet/sec YDOT = 5355
108649 meter/sec
ZDOT = -16051
810069 ZDOT = -4892
591709
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 19129
27050561
00016717 00000-0 10270-3 0 9061
2 25544 51
6357 194
6024 0001094 306
7009 53
4042 15
52626461 9201
Satellite: ISS
Catalog Number: 25544
Epoch time: 19129
27050561 = yrday
fracday
Element set: 906
Inclination: 51
6357 deg
RA of node: 194
6024 deg
Eccentricity:
0001094
Arg of perigee: 306
7009 deg
Mean anomaly: 53
4042 deg
Mean motion: 15
52626461 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 920
Checksum: 286
Coasting Arc #8 (Orbit 934)
---------------------------------------
Vector Time (GMT): 2019/130/05:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6461642
98 A = 6791893
43 meter
Y = 617001
31 meter E =
0006755
Z = -1989942
43 I = 51
58969
XDOT = -2169
021709 Wp = 32
28957
YDOT = -4795
706733 meter/sec RA = 188
61350 deg
ZDOT = 5570
513015 TA = 305
74443
MA = 305
80724
Ha = 223
027 n
mi
Hp = 217
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21199616
08 X = -6458396
14
Y = 2024282
51 feet Y = 544761
04 meter
Z = -6528682
50 Z = -2021322
90
XDOT = -7116
212956 XDOT = -2142
292154
YDOT = -15733
945973 feet/sec YDOT = -4819
813325 meter/sec
ZDOT = 18275
961334 ZDOT = 5560
041126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15239255
15 X = -4644924
97
Y = -14812517
25 feet Y = -4514855
26 meter
Z = -6670799
97 Z = -2033259
83
XDOT = 6223
433412 XDOT = 1896
902504
YDOT = -14591
374551 feet/sec YDOT = -4447
450963 meter/sec
ZDOT = 18228
910483 ZDOT = 5556
171915
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 19130
23596319
00016717 00000-0 10270-3 0 9076
2 25544 51
6379 189
8000 0001018 312
6501 47
4565 15
52644294 9357
Satellite: ISS
Catalog Number: 25544
Epoch time: 19130
23596319 = yrday
fracday
Element set: 907
Inclination: 51
6379 deg
RA of node: 189
8000 deg
Eccentricity:
0001018
Arg of perigee: 312
6501 deg
Mean anomaly: 47
4565 deg
Mean motion: 15
52644294 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 935
Checksum: 307
Coasting Arc #9 (Orbit 950)
---------------------------------------
Vector Time (GMT): 2019/131/05:34:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6738125
13 A = 6793309
06 meter
Y = -199702
05 meter E =
0012273
Z = 792852
89 I = 51
62707
XDOT = 847
433208 Wp = 125
07522
YDOT = 4768
974813 meter/sec RA = 183
64609 deg
ZDOT = -5942
540821 TA = 46
35610
MA = 46
25440
Ha = 223
076 n
mi
Hp = 217
199
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22106709
73 X = 6736006
21
Y = -655190
46 feet Y = -124363
53 meter
Z = 2601223
39 Z = 825579
10
XDOT = 2780
292677 XDOT = 822
907823
YDOT = 15646
242824 feet/sec YDOT = 4778
314746 meter/sec
ZDOT = -19496
525003 ZDOT = -5938
483486
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15080462
14 X = 4596524
86
Y = 16153097
85 feet Y = 4923464
23 meter
Z = 2749426
17 Z = 838025
10
XDOT = -8646
781212 XDOT = -2635
538914
YDOT = 11418
813396 feet/sec YDOT = 3480
454323 meter/sec
ZDOT = -19478
506756 ZDOT = -5937
048859
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 19131
26578133
00016717 00000-0 10270-3 0 9085
2 25544 51
6374 184
6771 0001144 321
3568 38
7502 15
52658738 9510
Satellite: ISS
Catalog Number: 25544
Epoch time: 19131
26578133 = yrday
fracday
Element set: 908
Inclination: 51
6374 deg
RA of node: 184
6771 deg
Eccentricity:
0001144
Arg of perigee: 321
3568 deg
Mean anomaly: 38
7502 deg
Mean motion: 15
52658738 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 951
Checksum: 319
Coasting Arc #10 (Orbit 952)
---------------------------------------
Vector Time (GMT): 2019/131/09:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -320922
40 A = 6781678
25 meter
Y = 4207271
46 meter E =
0014041
Z = -5321278
24 I = 51
59619
XDOT = -7641
099895 Wp = 87
15781
YDOT = -465
194820 meter/sec RA = 182
92669 deg
ZDOT = 93
917278 TA = 183
73390
MA = 183
74439
Ha = 223
053 n
mi
Hp = 217
271
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1052895
02 X = -342097
59
Y = 13803384
06 feet Y = 4203564
69 meter
Z = -17458261
94 Z = -5322888
27
XDOT = -25069
225378 XDOT = -7635
786252
YDOT = -1526
229724 feet/sec YDOT = -550
613244 meter/sec
ZDOT = 308
127553 ZDOT = 56
812465
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 84545
69 X = 25769
53
Y = 13833630
91 feet Y = 4216490
70 meter
Z = -17465864
35 Z = -5323595
45
XDOT = -24106
250911 XDOT = -7347
585278
YDOT = 320
563853 feet/sec YDOT = 97
707862 meter/sec
ZDOT = 140
143440 ZDOT = 42
715721
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 19131
39450806
00016717 00000-0 10270-3 0 9096
2 25544 51
6407 184
0393 0001235 316
8885 43
2170 15
52645868 9537
Satellite: ISS
Catalog Number: 25544
Epoch time: 19131
39450806 = yrday
fracday
Element set: 909
Inclination: 51
6407 deg
RA of node: 184
0393 deg
Eccentricity:
0001235
Arg of perigee: 316
8885 deg
Mean anomaly: 43
2170 deg
Mean motion: 15
52645868 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 953
Checksum: 317
Coasting Arc #11 (Orbit 968)
---------------------------------------
Vector Time (GMT): 2019/132/09:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1511517
23 A = 6782236
17 meter
Y = -4138019
44 meter E =
0004590
Z = 5154881
99 I = 51
63188
XDOT = 7472
408273 Wp = 39
41773
YDOT = 894
776375 meter/sec RA = 177
94099 deg
ZDOT = -1468
606120 TA = 64
74574
MA = 64
69818
Ha = 222
964 n
mi
Hp = 217
234
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4959046
04 X = 1532637
81
Y = -13576179
28 feet Y = -4120998
79 meter
Z = 16912342
48 Z = 5162275
46
XDOT = 24515
775173 XDOT = 7468
980949
YDOT = 2935
618029 feet/sec YDOT = 978
318993 meter/sec
ZDOT = -4818
261549 ZDOT = -1432
316176
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3591693
35 X = 1094748
13
Y = -13959244
63 feet Y = -4254777
76 meter
Z = 16946130
47 Z = 5165180
57
XDOT = 23694
789840 XDOT = 7222
171943
YDOT = 430
200160 feet/sec YDOT = 131
125009 meter/sec
ZDOT = -4653
974435 ZDOT = -1418
531408
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 19132
42432483
00016717 00000-0 10270-3 0 9104
2 25544 51
6407 178
9169 0001278 320
4570 39
6489 15
52679835 9699
Satellite: ISS
Catalog Number: 25544
Epoch time: 19132
42432483 = yrday
fracday
Element set: 910
Inclination: 51
6407 deg
RA of node: 178
9169 deg
Eccentricity:
0001278
Arg of perigee: 320
4570 deg
Mean anomaly: 39
6489 deg
Mean motion: 15
52679835 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 969
Checksum: 337
Coasting Arc #12 (Orbit 983)
---------------------------------------
Vector Time (GMT): 2019/133/09:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2633687
53 A = 6784030
19 meter
Y = 4095646
32 meter E =
0010146
Z = -4733264
29 I = 51
67062
XDOT = -7019
137773 Wp = 105
19490
YDOT = -1329
777703 meter/sec RA = 172
96132 deg
ZDOT = 2757
294099 TA = 192
11591
MA = 192
14033
Ha = 223
080 n
mi
Hp = 217
107
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8640707
11 X = -2656298
82
Y = 13437159
84 feet Y = 4066068
32 meter
Z = -15529082
32 Z = -4746112
58
XDOT = -23028
667234 XDOT = -7017
139592
YDOT = -4362
787738 feet/sec YDOT = -1408
259542 meter/sec
ZDOT = 9046
240482 ZDOT = 2723
202447
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7035308
96 X = -2144362
17
Y = 14279472
86 feet Y = 4352383
33 meter
Z = -15587577
25 Z = -4751093
55
XDOT = -22383
604242 XDOT = -6822
522573
YDOT = -1329
978856 feet/sec YDOT = -405
377555 meter/sec
ZDOT = 8891
920339 ZDOT = 2710
257319
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 19133
38977886
00016717 00000-0 10270-3 0 9112
2 25544 51
6402 174
1160 0001188 327
1266 32
9811 15
52671807 9842
Satellite: ISS
Catalog Number: 25544
Epoch time: 19133
38977886 = yrday
fracday
Element set: 911
Inclination: 51
6402 deg
RA of node: 174
1160 deg
Eccentricity:
0001188
Arg of perigee: 327
1266 deg
Mean anomaly: 32
9811 deg
Mean motion: 15
52671807 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 984
Checksum: 318
Coasting Arc #13 (Orbit 999)
---------------------------------------
Vector Time (GMT): 2019/134/09:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3659979
94 A = 6786567
94 meter
Y = -4038037
63 meter E =
0010388
Z = 4038358
50 I = 51
71284
XDOT = 6336
796293 Wp = 70
70798
YDOT = 1813
631734 meter/sec RA = 167
98690 deg
ZDOT = -3917
999935 TA = 59
95949
MA = 59
85649
Ha = 223
038 n
mi
Hp = 217
161
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12007808
21 X = 3685246
17
Y = -13248154
96 feet Y = -3996968
00 meter
Z = 13249207
67 Z = 4056198
70
XDOT = 20790
014086 XDOT = 6335
076384
YDOT = 5950
235348 feet/sec YDOT = 1884
484708 meter/sec
ZDOT = -12854
330496 ZDOT = -3887
222070
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10168009
80 X = 3099209
39
Y = -14634095
59 feet Y = -4460472
34 meter
Z = 13330318
62 Z = 4063081
12
XDOT = 20388
834814 XDOT = 6214
516851
YDOT = 2549
879700 feet/sec YDOT = 777
203332 meter/sec
ZDOT = -12715
039017 ZDOT = -3875
543892
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 19134
41959295
00016717 00000-0 10270-3 0 9122
2 25544 51
6410 168
9935 0001389 332
4422 27
6656 15
52674468 10002
Satellite: ISS
Catalog Number: 25544
Epoch time: 19134
41959295 = yrday
fracday
Element set: 912
Inclination: 51
6410 deg
RA of node: 168
9935 deg
Eccentricity:
0001389
Arg of perigee: 332
4422 deg
Mean anomaly: 27
6656 deg
Mean motion: 15
52674468 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1000
Checksum: 318
Coasting Arc #14 (Orbit 1005)
---------------------------------------
Vector Time (GMT): 2019/134/18:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3776514
06 A = 6783910
92 meter
Y = -2963610
78 meter E =
0006451
Z = 4789002
16 I = 51
71409
XDOT = 6206
724022 Wp = 109
31751
YDOT = -3660
671528 meter/sec RA = 166
17434 deg
ZDOT = 2624
176299 TA = 314
81054
MA = 314
86297
Ha = 223
250 n
mi
Hp = 217
138
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12390137
98 X = -3766355
95
Y = -9723132
47 feet Y = -3005785
71 meter
Z = 15711949
33 Z = 4770681
71
XDOT = 20363
267789 XDOT = 6234
450497
YDOT = -12010
077193 feet/sec YDOT = -3591
108625 meter/sec
ZDOT = 8609
502293 ZDOT = 2654
393757
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3942467
92 X = 1201664
22
Y = 15333171
09 feet Y = 4673550
55 meter
Z = 15629171
02 Z = 4763771
33
XDOT = -22292
113806 XDOT = -6794
636288
YDOT = -3200
458386 feet/sec YDOT = -975
499716 meter/sec
ZDOT = 8746
660779 ZDOT = 2665
982205
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 19134
80577315
00016717 00000-0 10270-3 0 9135
2 25544 51
6391 167
0745 0001599 338
9463 21
1623 15
52684500 10065
Satellite: ISS
Catalog Number: 25544
Epoch time: 19134
80577315 = yrday
fracday
Element set: 913
Inclination: 51
6391 deg
RA of node: 167
0745 deg
Eccentricity:
0001599
Arg of perigee: 338
9463 deg
Mean anomaly: 21
1623 deg
Mean motion: 15
52684500 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1006
Checksum: 304
Coasting Arc #15 (Orbit 1020)
---------------------------------------
Vector Time (GMT): 2019/135/18:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2725474
16 A = 6782259
44 meter
Y = 3407795
73 meter E =
0014001
Z = -5204451
20 I = 51
73982
XDOT = -6739
446296 Wp = 73
22952
YDOT = 3386
550716 meter/sec RA = 161
19830 deg
ZDOT = -1310
842163 TA = 184
16909
MA = 184
18076
Ha = 223
302 n
mi
Hp = 217
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8941844
37 X = 2712445
32
Y = 11180432
20 feet Y = 3438201
19 meter
Z = -17074971
14 Z = -5191243
25
XDOT = -22111
044277 XDOT = -6770
447354
YDOT = 11110
730695 feet/sec YDOT = 3311
012205 meter/sec
ZDOT = -4300
663264 ZDOT = -1343
655497
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -577555
51 X = -176038
92
Y = -14375551
79 feet Y = -4381668
18 meter
Z = -17015382
01 Z = -5186288
44
XDOT = 23295
447131 XDOT = 7100
452285
YDOT = 4334
716337 feet/sec YDOT = 1321
221540 meter/sec
ZDOT = -4449
580298 ZDOT = -1356
232075
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 19135
77122435
00016717 00000-0 10270-3 0 9142
2 25544 51
6385 162
2722 0001678 349
5769 10
5347 15
52655895 10212
Satellite: ISS
Catalog Number: 25544
Epoch time: 19135
77122435 = yrday
fracday
Element set: 914
Inclination: 51
6385 deg
RA of node: 162
2722 deg
Eccentricity:
0001678
Arg of perigee: 349
5769 deg
Mean anomaly: 10
5347 deg
Mean motion: 15
52655895 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1021
Checksum: 318
Coasting Arc #16 (Orbit 1036)
---------------------------------------
Vector Time (GMT): 2019/136/18:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1620362
64 A = 6781555
28 meter
Y = -3870800
89 meter E =
0002604
Z = 5325675
68 I = 51
76909
XDOT = 7038
453113 Wp = 49
35531
YDOT = -3042
322251 meter/sec RA = 156
22330 deg
ZDOT = -68
055625 TA = 41
30190
MA = 41
28220
Ha = 223
260 n
mi
Hp = 217
079
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5316150
41 X = -1602827
42
Y = -12699477
98 feet Y = -3888823
10 meter
Z = 17472689
23 Z = 5317846
86
XDOT = 23092
037773 XDOT = 7072
280696
YDOT = -9981
372215 feet/sec YDOT = -2963
424194 meter/sec
ZDOT = -223
279608 ZDOT = -33
782854
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3003422
22 X = -915443
09
Y = 13481316
06 feet Y = 4109105
13 meter
Z = 17437506
63 Z = 5314952
02
XDOT = -23592
676898 XDOT = -7191
047919
YDOT = -5161
300687 feet/sec YDOT = -1573
164449 meter/sec
ZDOT = -67
754455 ZDOT = -20
651558
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 19136
80103545
00016717 00000-0 10270-3 0 9159
2 25544 51
6386 157
1509 0001728 345
1936 14
9165 15
52684175 10379
Satellite: ISS
Catalog Number: 25544
Epoch time: 19136
80103545 = yrday
fracday
Element set: 915
Inclination: 51
6386 deg
RA of node: 157
1509 deg
Eccentricity:
0001728
Arg of perigee: 345
1936 deg
Mean anomaly: 14
9165 deg
Mean motion: 15
52684175 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1037
Checksum: 312
Coasting Arc #17 (Orbit 1051)
---------------------------------------
Vector Time (GMT): 2019/137/18:04:00
000
Vector Time (MET): N/A
Weight (LBS) : 964623
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 536087
98 A = 6782293
90 meter
Y = 4356781
56 meter E =
0013445
Z = -5181934
95 I = 51
80183
XDOT = -7062
303845 Wp = 93
81026
YDOT = 2580
872863 meter/sec RA = 151
24834 deg
ZDOT = 1441
640253 TA = 190
03955
MA = 190
06644
Ha = 223
358 n
mi
Hp = 217
041
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1758818
83 X = 512500
79
Y = 14293902
77 feet Y = 4362644
93 meter
Z = -17001098
93 Z = -5179387
80
XDOT = -23170
288205 XDOT = -7097
641832
YDOT = 8467
430653 feet/sec YDOT = 2501
699556 meter/sec
ZDOT = 4729
790855 ZDOT = 1407
247920
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6605459
32 X = 2013344
00
Y = -12812414
39 feet Y = -3905223
91 meter
Z = -16989891
40 Z = -5178518
90
XDOT = 22956
985897 XDOT = 6997
289301
YDOT = 5780
762060 feet/sec YDOT = 1761
976276 meter/sec
ZDOT = 4573
735451 ZDOT = 1394
074566
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 19137
76648324
00016717 00000-0 10270-3 0 9165
2 25544 51
6391 152
3476 0001770 353
7406 6
3723 15
52654756 10523
Satellite: ISS
Catalog Number: 25544
Epoch time: 19137
76648324 = yrday
fracday
Element set: 916
Inclination: 51
6391 deg
RA of node: 152
3476 deg
Eccentricity:
0001770
Arg of perigee: 353
7406 deg
Mean anomaly: 6
3723 deg
Mean motion: 15
52654756 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1052
Checksum: 312
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