[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 5th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19965 9774 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
311/22:41:23
223 1
1 1
5 1
5
N/A 0
7 -0
0 225
9
000/00:06:46
445 0
7 -0
0 223
7
312/03:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 225
9
000/00:00:00
000 0
0 0
0 223
6
317/14:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 225
3
000/00:00:00
000 0
0 0
0 223
6
Coasting Arc #1 (Orbit 3700)
---------------------------------------
Vector Time (GMT): 2019/308/10:13:11
534
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2001701
97 A = 6788586
18 meter
Y = 3696347
59 meter E =
0004482
Z = 5332331
88 I = 51
79228
XDOT = -6852
362293 Wp = 208
80294
YDOT = -3419
853901 meter/sec RA = 25
31197 deg
ZDOT = -205
579900 TA = 243
13118
MA = 243
17700
Ha = 226
686 n
mi
Hp = 222
294
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6567263
68 X = -2068788
63
Y = 12127124
65 feet Y = 3673587
96 meter
Z = 17494527
17 Z = 5322445
37
XDOT = -22481
503587 XDOT = -6812
612606
YDOT = -11219
993113 feet/sec YDOT = -3496
259596 meter/sec
ZDOT = -674
474736 ZDOT = -238
769994
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3135746
42 X = 955775
51
Y = -13488952
68 feet Y = -4111432
78 meter
Z = 17449064
02 Z = 5318474
71
XDOT = 23696
730220 XDOT = 7222
763371
YDOT = 4457
432554 feet/sec YDOT = 1358
625442 meter/sec
ZDOT = -825
531369 ZDOT = -251
621961
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 19308
47375089
00016717 00000-0 10270-3 0 9001
2 25544 51
6445 25
6961 0006404 226
6365 133
4253 15
50283801 37015
Satellite: ISS
Catalog Number: 25544
Epoch time: 19308
47375089 = yrday
fracday
Element set: 900
Inclination: 51
6445 deg
RA of node: 25
6961 deg
Eccentricity:
0006404
Arg of perigee: 226
6365 deg
Mean anomaly: 133
4253 deg
Mean motion: 15
50283801 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3701
Checksum: 300
Coasting Arc #2 (Orbit 3715)
---------------------------------------
Vector Time (GMT): 2019/309/10:13:11
534
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2187403
17 A = 6788790
09 meter
Y = -3644761
70 meter E =
0011122
Z = -5302204
37 I = 51
76184
XDOT = 6939
796265 Wp = 119
14579
YDOT = 3155
578036 meter/sec RA = 20
36392 deg
ZDOT = 689
638984 TA = 157
46522
MA = 157
41634
Ha = 226
545 n
mi
Hp = 222
498
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7176519
57 X = 2253752
84
Y = -11957879
61 feet Y = -3619929
62 meter
Z = -17395683
62 Z = -5291417
52
XDOT = 22768
360448 XDOT = 6900
643971
YDOT = 10352
946313 feet/sec YDOT = 3232
964822 meter/sec
ZDOT = 2262
595091 ZDOT = 723
255215
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3534787
59 X = -1077403
26
Y = 13554354
51 feet Y = 4131367
25 meter
Z = -17346119
94 Z = -5287097
36
XDOT = -23783
276474 XDOT = -7249
142669
YDOT = -3093
355696 feet/sec YDOT = -942
854816 meter/sec
ZDOT = 2415
611129 ZDOT = 736
278272
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 19309
44069566
00016717 00000-0 10270-3 0 9010
2 25544 51
6442 20
9054 0006294 230
0326 130
0272 15
50270945 37161
Satellite: ISS
Catalog Number: 25544
Epoch time: 19309
44069566 = yrday
fracday
Element set: 901
Inclination: 51
6442 deg
RA of node: 20
9054 deg
Eccentricity:
0006294
Arg of perigee: 230
0326 deg
Mean anomaly: 130
0272 deg
Mean motion: 15
50270945 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3716
Checksum: 285
Coasting Arc #3 (Orbit 3731)
---------------------------------------
Vector Time (GMT): 2019/310/10:13:11
534
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2361510
61 A = 6789020
83 meter
Y = 3629040
94 meter E =
0002320
Z = 5230471
46 I = 51
73127
XDOT = -7002
376518 Wp = 230
97534
YDOT = -2882
422963 meter/sec RA = 15
41262 deg
ZDOT = -1163
379893 TA = 230
16654
MA = 230
18696
Ha = 226
343 n
mi
Hp = 222
575
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7747738
22 X = -2427323
14
Y = 11906302
30 feet Y = 3602264
92 meter
Z = 17160339
44 Z = 5218840
10
XDOT = -22973
676241 XDOT = -6963
972868
YDOT = -9456
768251 feet/sec YDOT = -2960
513764 meter/sec
ZDOT = -3816
863165 ZDOT = -1197
301953
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3859348
08 X = 1176329
29
Y = -13737655
42 feet Y = -4187237
37 meter
Z = 17106928
06 Z = 5214191
67
XDOT = 23736
275255 XDOT = 7234
816698
YDOT = 1730
264044 feet/sec YDOT = 527
384481 meter/sec
ZDOT = -3971
289086 ZDOT = -1210
448913
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 19310
47209867
00016717 00000-0 10270-3 0 9026
2 25544 51
6444 15
7938 0006363 234
4892 125
5666 15
50293539 37327
Satellite: ISS
Catalog Number: 25544
Epoch time: 19310
47209867 = yrday
fracday
Element set: 902
Inclination: 51
6444 deg
RA of node: 15
7938 deg
Eccentricity:
0006363
Arg of perigee: 234
4892 deg
Mean anomaly: 125
5666 deg
Mean motion: 15
50293539 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3732
Checksum: 327
Coasting Arc #4 (Orbit 3746)
---------------------------------------
Vector Time (GMT): 2019/311/10:13:11
534
Vector Time (MET): N/A
Weight (LBS) : 932295
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2559474
03 A = 6789504
83 meter
Y = -3647882
86 meter E =
0009927
Z = -5130680
49 I = 51
70021
XDOT = 7008
156841 Wp = 128
53041
YDOT = 2608
784380 meter/sec RA = 10
46013 deg
ZDOT = 1637
348921 TA = 157
30745
MA = 157
26353
Ha = 226
161 n
mi
Hp = 222
776
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8397224
50 X = 2624997
87
Y = -11968119
61 feet Y = -3618894
73 meter
Z = -16832941
26 Z = -5118088
13
XDOT = 22992
640556 XDOT = 6970
510338
YDOT = 8559
003871 feet/sec YDOT = 2686
944073 meter/sec
ZDOT = 5371
879663 ZDOT = 1671
300966
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4215595
38 X = -1284913
47
Y = 14068415
45 feet Y = 4288053
03 meter
Z = -16775148
88 Z = -5113065
38
XDOT = -23462
808281 XDOT = -7151
463964
YDOT = -425
629841 feet/sec YDOT = -129
731976 meter/sec
ZDOT = 5526
455935 ZDOT = 1684
463769
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 19311
43903607
00016717 00000-0 10270-3 0 9037
2 25544 51
6443 11
0027 0006273 238
1880 121
8660 15
50286797 37479
Satellite: ISS
Catalog Number: 25544
Epoch time: 19311
43903607 = yrday
fracday
Element set: 903
Inclination: 51
6443 deg
RA of node: 11
0027 deg
Eccentricity:
0006273
Arg of perigee: 238
1880 deg
Mean anomaly: 121
8660 deg
Mean motion: 15
50286797 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3747
Checksum: 300
Coasting Arc #5 (Orbit 3754)
---------------------------------------
Vector Time (GMT): 2019/311/22:44:46
445
Vector Time (MET): N/A
Weight (LBS) : 932145
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5569545
23 A = 6796613
39 meter
Y = -1928605
54 meter E =
0002300
Z = -3384908
76 I = 51
70470
XDOT = 4312
965000 Wp = 222
46525
YDOT = 4297
968734 meter/sec RA = 7
86709 deg
ZDOT = 4644
236124 TA = 98
14810
MA = 98
12200
Ha = 225
868 n
mi
Hp = 223
736
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18272786
19 X = 5607139
81
Y = -6327446
01 feet Y = -1866112
82 meter
Z = -11105343
70 Z = -3357762
18
XDOT = 14150
147637 XDOT = 4242
023805
YDOT = 14100
947291 feet/sec YDOT = 4345
802793 meter/sec
ZDOT = 15236
995159 ZDOT = 4665
014859
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13439589
20 X = 4096386
79
Y = -14001686
81 feet Y = -4267714
14 meter
Z = -10981354
89 Z = -3347116
97
XDOT = 17912
508412 XDOT = 5459
732564
YDOT = 5160
128992 feet/sec YDOT = 1572
807317 meter/sec
ZDOT = 15331
320647 ZDOT = 4672
986533
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 19311
95473454
00016717 00000-0 10270-3 0 9047
2 25544 51
6451 8
4496 0006591 252
7796 107
2622 15
50006566 37558
Satellite: ISS
Catalog Number: 25544
Epoch time: 19311
95473454 = yrday
fracday
Element set: 904
Inclination: 51
6451 deg
RA of node: 8
4496 deg
Eccentricity:
0006591
Arg of perigee: 252
7796 deg
Mean anomaly: 107
2622 deg
Mean motion: 15
50006566 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3755
Checksum: 319
Coasting Arc #6 (Orbit 3757)
---------------------------------------
Vector Time (GMT): 2019/312/03:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 932145
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1860363
04 A = 6790784
78 meter
Y = -4209804
25 meter E =
0006069
Z = -4998691
93 I = 51
67523
XDOT = 7327
484998 Wp = 76
73403
YDOT = -760
940370 meter/sec RA = 7
01127 deg
ZDOT = -2086
997119 TA = 172
93958
MA = 172
93102
Ha = 225
872 n
mi
Hp = 223
610
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6103553
27 X = -1788868
21
Y = -13811693
72 feet Y = -4230208
49 meter
Z = -16399907
92 Z = -5007555
30
XDOT = 24040
305112 XDOT = 7345
587113
YDOT = -2496
523523 feet/sec YDOT = -678
898085 meter/sec
ZDOT = -6847
103410 ZDOT = -2051
358325
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13552091
98 X = -4130677
64
Y = 6560760
15 feet Y = 1999719
69 meter
Z = -16439904
35 Z = -5010882
85
XDOT = -3015
913772 XDOT = -919
250518
YDOT = -22973
375298 feet/sec YDOT = -7002
284791 meter/sec
ZDOT = -6684
507567 ZDOT = -2037
437907
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 19312
14815501
00016717 00000-0 10270-3 0 9053
2 25544 51
6409 7
4888 0006628 252
9164 107
1261 15
49996105 37583
Satellite: ISS
Catalog Number: 25544
Epoch time: 19312
14815501 = yrday
fracday
Element set: 905
Inclination: 51
6409 deg
RA of node: 7
4888 deg
Eccentricity:
0006628
Arg of perigee: 252
9164 deg
Mean anomaly: 107
1261 deg
Mean motion: 15
49996105 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3758
Checksum: 320
Coasting Arc #7 (Orbit 3773)
---------------------------------------
Vector Time (GMT): 2019/313/03:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 932145
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1806865
46 A = 6790460
87 meter
Y = 4105078
74 meter E =
0004935
Z = 5101446
08 I = 51
63994
XDOT = -7380
697139 Wp = 205
93850
YDOT = 1100
759807 meter/sec RA = 2
05725 deg
ZDOT = 1724
673655 TA = 227
35179
MA = 227
39339
Ha = 225
665 n
mi
Hp = 223
748
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5928036
30 X = 1736046
46
Y = 13468106
09 feet Y = 4124888
51 meter
Z = 16737027
82 Z = 5110051
25
XDOT = -24214
885628 XDOT = -7400
835291
YDOT = 3611
416691 feet/sec YDOT = 1018
111073 meter/sec
ZDOT = 5658
378134 ZDOT = 1688
771290
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13104691
08 X = 3994309
84
Y = -6595259
16 feet Y = -2010234
99 meter
Z = 16775852
42 Z = 5113279
82
XDOT = 4547
726500 XDOT = 1386
147037
YDOT = 23043
195596 feet/sec YDOT = 7023
566018 meter/sec
ZDOT = 5494
561346 ZDOT = 1674
742298
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 19313
17973529
00016717 00000-0 10270-3 0 9063
2 25544 51
6404 2
3784 0006567 257
0345 103
0072 15
49955304 37745
Satellite: ISS
Catalog Number: 25544
Epoch time: 19313
17973529 = yrday
fracday
Element set: 906
Inclination: 51
6404 deg
RA of node: 2
3784 deg
Eccentricity:
0006567
Arg of perigee: 257
0345 deg
Mean anomaly: 103
0072 deg
Mean motion: 15
49955304 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3774
Checksum: 312
Coasting Arc #8 (Orbit 3788)
---------------------------------------
Vector Time (GMT): 2019/314/03:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 932145
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1732597
66 A = 6789947
46 meter
Y = -4029906
72 meter E =
0007430
Z = -5189388
01 I = 51
60454
XDOT = 7396
824496 Wp = 80
53218
YDOT = -1444
492991 meter/sec RA = 357
10054 deg
ZDOT = -1348
313179 TA = 176
48518
MA = 176
47996
Ha = 225
503 n
mi
Hp = 223
578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5684375
53 X = -1662197
50
Y = -13221478
74 feet Y = -4048888
28 meter
Z = -17025551
20 Z = -5197633
49
XDOT = 24267
796902 XDOT = 7418
977006
YDOT = -4739
150233 feet/sec YDOT = -1361
652627 meter/sec
ZDOT = -4423
599670 ZDOT = -1312
327457
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12762034
38 X = -3889868
08
Y = 6556100
82 feet Y = 1998299
53 meter
Z = -17062738
34 Z = -5200722
65
XDOT = -6090
441558 XDOT = -1856
366587
YDOT = -22937
053548 feet/sec YDOT = -6991
213921 meter/sec
ZDOT = -4259
382950 ZDOT = -1298
259923
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 19314
14683738
00016717 00000-0 10270-3 0 9072
2 25544 51
6397 357
5874 0006539 259
0863 100
9552 15
50003782 37898
Satellite: ISS
Catalog Number: 25544
Epoch time: 19314
14683738 = yrday
fracday
Element set: 907
Inclination: 51
6397 deg
RA of node: 357
5874 deg
Eccentricity:
0006539
Arg of perigee: 259
0863 deg
Mean anomaly: 100
9552 deg
Mean motion: 15
50003782 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3789
Checksum: 344
Coasting Arc #9 (Orbit 3804)
---------------------------------------
Vector Time (GMT): 2019/315/03:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 932145
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1657652
41 A = 6789784
65 meter
Y = 3976974
34 meter E =
0004340
Z = 5250982
56 I = 51
57048
XDOT = -7382
344003 Wp = 234
07627
YDOT = 1795
128507 meter/sec RA = 352
14080 deg
ZDOT = 968
972953 TA = 206
61866
MA = 206
64095
Ha = 225
263 n
mi
Hp = 223
673
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5438492
17 X = 1587550
46
Y = 13047816
08 feet Y = 3995119
39 meter
Z = 17227633
08 Z = 5258864
79
XDOT = -24220
288723 XDOT = -7406
575840
YDOT = 5889
529221 feet/sec YDOT = 1712
438428 meter/sec
ZDOT = 3179
045120 ZDOT = 933
052444
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12497466
85 X = 3809227
90
Y = -6512335
36 feet Y = -1984959
82 meter
Z = 17263164
65 Z = 5261812
58
XDOT = 7643
339120 XDOT = 2329
689764
YDOT = 22677
201908 feet/sec YDOT = 6912
011142 meter/sec
ZDOT = 3015
103771 ZDOT = 919
003630
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 19315
17841180
00016717 00000-0 10270-3 0 9084
2 25544 51
6399 352
4764 0006543 263
6911 96
3494 15
49963997 38055
Satellite: ISS
Catalog Number: 25544
Epoch time: 19315
17841180 = yrday
fracday
Element set: 908
Inclination: 51
6399 deg
RA of node: 352
4764 deg
Eccentricity:
0006543
Arg of perigee: 263
6911 deg
Mean anomaly: 96
3494 deg
Mean motion: 15
49963997 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3805
Checksum: 353
Coasting Arc #10 (Orbit 3819)
---------------------------------------
Vector Time (GMT): 2019/316/03:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 932145
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1574619
37 A = 6789436
15 meter
Y = -3955922
39 meter E =
0008303
Z = -5295683
88 I = 51
53757
XDOT = 7327
649697 Wp = 85
01994
YDOT = -2140
222726 meter/sec RA = 347
17910 deg
ZDOT = -580
120796 TA = 179
42714
MA = 179
42619
Ha = 225
175 n
mi
Hp = 223
431
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5166074
04 X = -1504541
81
Y = -12978747
98 feet Y = -3973138
92 meter
Z = -17374290
95 Z = -5303162
91
XDOT = 24040
845463 XDOT = 7353
855667
YDOT = -7021
728105 feet/sec YDOT = -2058
133231 meter/sec
ZDOT = -1903
283451 ZDOT = -544
461173
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12345062
22 X = -3762774
96
Y = 6446998
87 feet Y = 1965045
26 meter
Z = -17407982
38 Z = -5305953
03
XDOT = -9157
192431 XDOT = -2791
112253
YDOT = -22233
630094 feet/sec YDOT = -6776
810453 meter/sec
ZDOT = -1740
507853 ZDOT = -530
506794
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 19316
14550690
00016717 00000-0 10270-3 0 9096
2 25544 51
6406 347
6854 0006394 266
4528 93
5891 15
50019807 38200
Satellite: ISS
Catalog Number: 25544
Epoch time: 19316
14550690 = yrday
fracday
Element set: 909
Inclination: 51
6406 deg
RA of node: 347
6854 deg
Eccentricity:
0006394
Arg of perigee: 266
4528 deg
Mean anomaly: 93
5891 deg
Mean motion: 15
50019807 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3820
Checksum: 330
Coasting Arc #11 (Orbit 3835)
---------------------------------------
Vector Time (GMT): 2019/317/03:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 932145
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1494731
93 A = 6789487
63 meter
Y = 3958388
21 meter E =
0003914
Z = 5313204
76 I = 51
50355
XDOT = -7243
567725 Wp = 265
78132
YDOT = 2481
458199 meter/sec RA = 342
21428 deg
ZDOT = 188
917963 TA = 182
41172
MA = 182
41361
Ha = 225
162 n
mi
Hp = 223
536
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4903976
13 X = 1424547
62
Y = 12986837
97 feet Y = 3974710
68 meter
Z = 17431774
14 Z = 5320295
54
XDOT = -23764
985975 XDOT = -7271
695437
YDOT = 8141
267057 feet/sec YDOT = 2400
298229 meter/sec
ZDOT = 619
809589 ZDOT = 153
662185
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12273752
59 X = 3741039
79
Y = -6399073
04 feet Y = -1950437
46 meter
Z = 17463692
44 Z = 5322933
46
XDOT = 10631
382730 XDOT = 3240
445456
YDOT = 21645
227214 feet/sec YDOT = 6597
465255 meter/sec
ZDOT = 458
849205 ZDOT = 139
857238
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 19317
17707491
00016717 00000-0 10270-3 0 9105
2 25544 51
6392 342
5741 0006334 270
4124 89
6301 15
49971892 38362
Satellite: ISS
Catalog Number: 25544
Epoch time: 19317
17707491 = yrday
fracday
Element set: 910
Inclination: 51
6392 deg
RA of node: 342
5741 deg
Eccentricity:
0006334
Arg of perigee: 270
4124 deg
Mean anomaly: 89
6301 deg
Mean motion: 15
49971892 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3836
Checksum: 321
Coasting Arc #12 (Orbit 3842)
---------------------------------------
Vector Time (GMT): 2019/317/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932145
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2127777
67 A = 6792841
53 meter
Y = -4611639
95 meter E =
0003688
Z = -4514510
00 I = 51
49964
XDOT = 6971
038462 Wp = 137
65874
YDOT = 115
058382 meter/sec RA = 339
76449 deg
ZDOT = 3166
899592 TA = 164
24771
MA = 164
23624
Ha = 225
252 n
mi
Hp = 223
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6980897
86 X = 2201117
84
Y = -15130052
33 feet Y = -4587435
30 meter
Z = -14811384
51 Z = -4503995
89
XDOT = 22870
861095 XDOT = 6953
850255
YDOT = 377
488130 feet/sec YDOT = 192
917163 meter/sec
ZDOT = 10390
090525 ZDOT = 3200
721527
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15592114
34 X = 4752476
45
Y = 5997389
37 feet Y = 1828004
28 meter
Z = -14762988
21 Z = -4499758
81
XDOT = 1666
096401 XDOT = 507
826183
YDOT = 21633
200108 feet/sec YDOT = 6593
799393 meter/sec
ZDOT = 10544
246426 ZDOT = 3213
886311
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 19317
62838243
00016717 00000-0 10270-3 0 9116
2 25544 51
6396 340
3424 0006474 275
0970 84
9442 15
49992826 38437
Satellite: ISS
Catalog Number: 25544
Epoch time: 19317
62838243 = yrday
fracday
Element set: 911
Inclination: 51
6396 deg
RA of node: 340
3424 deg
Eccentricity:
0006474
Arg of perigee: 275
0970 deg
Mean anomaly: 84
9442 deg
Mean motion: 15
49992826 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3843
Checksum: 337
Coasting Arc #13 (Orbit 3858)
---------------------------------------
Vector Time (GMT): 2019/318/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932145
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2126318
45 A = 6793482
58 meter
Y = 4797436
26 meter E =
0004859
Z = 4314477
12 I = 51
47124
XDOT = -6814
081139 Wp = 35
78375
YDOT = 129
647447 meter/sec RA = 334
79883 deg
ZDOT = -3496
505824 TA = 89
94113
MA = 89
88545
Ha = 225
389 n
mi
Hp = 223
635
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6976110
41 X = -2200764
63
Y = 15739620
29 feet Y = 4773241
68 meter
Z = 14155108
66 Z = 4303967
54
XDOT = -22355
909249 XDOT = -6798
039921
YDOT = 425
352516 feet/sec YDOT = 53
537547 meter/sec
ZDOT = -11471
475800 ZDOT = -3529
567987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16299351
99 X = -4968042
49
Y = -5665734
21 feet Y = -1726915
79 meter
Z = 14106716
30 Z = 4299727
13
XDOT = -2787
354396 XDOT = -849
585620
YDOT = -20966
573338 feet/sec YDOT = -6390
611554 meter/sec
ZDOT = -11622
188100 ZDOT = -3542
442933
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 19318
65994508
00016717 00000-0 10270-3 0 9128
2 25544 51
6397 335
2315 0006587 278
9812 81
0593 15
50026306 38597
Satellite: ISS
Catalog Number: 25544
Epoch time: 19318
65994508 = yrday
fracday
Element set: 912
Inclination: 51
6397 deg
RA of node: 335
2315 deg
Eccentricity:
0006587
Arg of perigee: 278
9812 deg
Mean anomaly: 81
0593 deg
Mean motion: 15
50026306 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3859
Checksum: 339
Coasting Arc #14 (Orbit 3873)
---------------------------------------
Vector Time (GMT): 2019/319/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932145
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2091640
47 A = 6794291
28 meter
Y = -4997159
42 meter E =
0000993
Z = -4101788
40 I = 51
44490
XDOT = 6636
231392 Wp = 144
88876
YDOT = -347
675007 meter/sec RA = 329
83147 deg
ZDOT = 3807
271989 TA = 164
58407
MA = 164
58105
Ha = 225
678 n
mi
Hp = 223
695
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6862337
48 X = 2167289
36
Y = -16394880
00 feet Y = -4973345
87 meter
Z = -13457311
03 Z = -4091444
48
XDOT = 21772
412702 XDOT = 6621
131942
YDOT = -1140
666032 feet/sec YDOT = -273
548759 meter/sec
ZDOT = 12491
049832 ZDOT = 3839
472343
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17033610
63 X = 5191844
52
Y = 5198095
09 feet Y = 1584379
38 meter
Z = -13409657
06 Z = -4087263
47
XDOT = 3783
502079 XDOT = 1153
211434
YDOT = 20206
893857 feet/sec YDOT = 6159
061248 meter/sec
ZDOT = 12637
852873 ZDOT = 3852
017556
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 19319
62703201
00016717 00000-0 10270-3 0 9135
2 25544 51
6406 330
4401 0006534 283
4487 76
5935 15
50006723 38749
Satellite: ISS
Catalog Number: 25544
Epoch time: 19319
62703201 = yrday
fracday
Element set: 913
Inclination: 51
6406 deg
RA of node: 330
4401 deg
Eccentricity:
0006534
Arg of perigee: 283
4487 deg
Mean anomaly: 76
5935 deg
Mean motion: 15
50006723 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3874
Checksum: 298
Coasting Arc #15 (Orbit 3889)
---------------------------------------
Vector Time (GMT): 2019/320/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932145
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2041286
83 A = 6795010
27 meter
Y = 5203935
32 meter E =
0006107
Z = 3861901
15 I = 51
41901
XDOT = -6443
477382 Wp = 53
62631
YDOT = 527
237687 meter/sec RA = 324
86278 deg
ZDOT = -4108
190060 TA = 79
72860
MA = 79
65974
Ha = 225
895 n
mi
Hp = 223
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6697135
28 X = -2118086
35
Y = 17073278
62 feet Y = 5180678
43 meter
Z = 12670279
35 Z = 3851799
13
XDOT = -21140
017658 XDOT = -6428
938550
YDOT = 1729
782437 feet/sec YDOT = 455
263866 meter/sec
ZDOT = -13478
313845 ZDOT = -4139
455260
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17773037
83 X = -5417221
93
Y = -4652466
19 feet Y = -1418071
70 meter
Z = 12623712
89 Z = 3847707
69
XDOT = -4618
996193 XDOT = -1407
870040
YDOT = -19385
198063 feet/sec YDOT = -5908
608370 meter/sec
ZDOT = -13620
870506 ZDOT = -4151
641330
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 19320
65858859
00016717 00000-0 10270-3 0 9141
2 25544 51
6404 325
3295 0006604 287
9831 72
0599 15
50035437 38900
Satellite: ISS
Catalog Number: 25544
Epoch time: 19320
65858859 = yrday
fracday
Element set: 914
Inclination: 51
6404 deg
RA of node: 325
3295 deg
Eccentricity:
0006604
Arg of perigee: 287
9831 deg
Mean anomaly: 72
0599 deg
Mean motion: 15
50035437 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3890
Checksum: 335
Coasting Arc #16 (Orbit 3904)
---------------------------------------
Vector Time (GMT): 2019/321/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932145
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1948710
62 A = 6795848
48 meter
Y = -5413846
01 meter E =
0001953
Z = -3613716
93 I = 51
39481
XDOT = 6243
127957 Wp = 332
31830
YDOT = -679
912017 meter/sec RA = 319
89277 deg
ZDOT = 4385
970104 TA = 344
79221
MA = 344
79808
Ha = 226
120 n
mi
Hp = 223
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6393407
56 X = 2026658
65
Y = -17761961
96 feet Y = -5391617
98 meter
Z = -11856026
68 Z = -3604061
88
XDOT = 20482
703270 XDOT = 6228
962039
YDOT = -2230
682471 feet/sec YDOT = -610
176566 meter/sec
ZDOT = 14389
665694 ZDOT = 4416
262816
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18489463
64 X = 5635588
52
Y = 3944220
63 feet Y = 1202198
45 meter
Z = -11811485
06 Z = -3600140
65
XDOT = 5326
331102 XDOT = 1623
465720
YDOT = 18529
701191 feet/sec YDOT = 5647
852923 meter/sec
ZDOT = 14527
803019 ZDOT = 4428
074360
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 19321
62567156
00016717 00000-0 10270-3 0 9157
2 25544 51
6402 320
5386 0006646 291
3782 68
6661 15
50013456 39051
Satellite: ISS
Catalog Number: 25544
Epoch time: 19321
62567156 = yrday
fracday
Element set: 915
Inclination: 51
6402 deg
RA of node: 320
5386 deg
Eccentricity:
0006646
Arg of perigee: 291
3782 deg
Mean anomaly: 68
6661 deg
Mean motion: 15
50013456 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3905
Checksum: 312
Coasting Arc #17 (Orbit 3920)
---------------------------------------
Vector Time (GMT): 2019/322/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 932145
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1842578
46 A = 6796568
62 meter
Y = 5624683
06 meter E =
0006989
Z = 3337898
20 I = 51
37381
XDOT = -6034
985607 Wp = 68
69883
YDOT = 789
047543 meter/sec RA = 314
92142 deg
ZDOT = -4650
657270 TA = 72
34152
MA = 72
26522
Ha = 226
284 n
mi
Hp = 223
451
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6045204
92 X = -1921552
17
Y = 18453684
58 feet Y = 5603636
22 meter
Z = 10951109
58 Z = 3328756
18
XDOT = -19799
821545 XDOT = -6020
769901
YDOT = 2588
738658 feet/sec YDOT = 721
639922 meter/sec
ZDOT = -15258
061909 ZDOT = -4679
938671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19182562
19 X = -5846844
96
Y = -3167814
54 feet Y = -965549
87 meter
Z = 10908897
15 Z = 3325031
85
XDOT = -5857
174536 XDOT = -1785
266799
YDOT = -17653
425386 feet/sec YDOT = -5380
764058 meter/sec
ZDOT = -15391
597594 ZDOT = -4691
358947
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 19322
65722371
00016717 00000-0 10270-3 0 9164
2 25544 51
6414 315
4281 0006683 295
4031 64
6427 15
50043425 39217
Satellite: ISS
Catalog Number: 25544
Epoch time: 19322
65722371 = yrday
fracday
Element set: 916
Inclination: 51
6414 deg
RA of node: 315
4281 deg
Eccentricity:
0006683
Arg of perigee: 295
4031 deg
Mean anomaly: 64
6427 deg
Mean motion: 15
50043425 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3921
Checksum: 295
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