[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 11th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15846 6289 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 922 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
057/02:24:42
809 -2
9 3
0 3
0
N/A -0
3 -0
0 224
3
000/00:07:25
618 -0
4 -0
0 215
7
Coasting Arc #1 (Orbit 3571)
---------------------------------------
Vector Time (GMT): 2019/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4245111
37 A = 6780566
11 meter
Y = -1292954
78 meter E =
0015023
Z = -5138971
91 I = 51
23907
XDOT = 548
817165 Wp = 79
32624
YDOT = -7500
045645 meter/sec RA = 265
34135 deg
ZDOT = 1439
972764 TA = 204
59429
MA = 204
66601
Ha = 223
524 n
mi
Hp = 215
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13927530
75 X = -4205375
73
Y = -4241977
62 feet Y = -1340204
65 meter
Z = -16860144
07 Z = -5159496
24
XDOT = 1800
581249 XDOT = 625
649502
YDOT = -24606
448966 feet/sec YDOT = -7493
478721 meter/sec
ZDOT = 4724
320091 ZDOT = 1442
825655
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7935197
35 X = -2418648
15
Y = -12077964
25 feet Y = -3681363
50 meter
Z = -16952591
76 Z = -5167149
97
XDOT = 16173
237952 XDOT = 4929
602928
YDOT = -17246
961962 feet/sec YDOT = -5256
874006 meter/sec
ZDOT = 4737
960925 ZDOT = 1444
130490
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 19042
51361131
00016717 00000-0 10270-3 0 9004
2 25544 51
6390 266
1925 0005552 12
7990 347
3303 15
53262599 35729
Satellite: ISS
Catalog Number: 25544
Epoch time: 19042
51361131 = yrday
fracday
Element set: 900
Inclination: 51
6390 deg
RA of node: 266
1925 deg
Eccentricity:
0005552
Arg of perigee: 12
7990 deg
Mean anomaly: 347
3303 deg
Mean motion: 15
53262599 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3572
Checksum: 297
Coasting Arc #2 (Orbit 3587)
---------------------------------------
Vector Time (GMT): 2019/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4200736
81 A = 6782692
30 meter
Y = 2679161
43 meter E =
0012620
Z = 4598856
23 I = 51
25101
XDOT = -1209
212236 Wp = 45
17081
YDOT = 6976
182815 meter/sec RA = 260
32684 deg
ZDOT = -2945
853531 TA = 74
40777
MA = 74
26852
Ha = 223
474 n
mi
Hp = 215
191
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13781944
92 X = 4148127
03
Y = 8789899
72 feet Y = 2725843
00 meter
Z = 15088110
98 Z = 4619133
73
XDOT = -3967
231747 XDOT = -1272
822852
YDOT = 22887
738893 feet/sec YDOT = 6962
304788 meter/sec
ZDOT = -9664
873791 ZDOT = -2951
882103
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5197857
10 X = 1584306
84
Y = 15408641
26 feet Y = 4696553
86 meter
Z = 15179311
31 Z = 4626654
09
XDOT = -16214
519659 XDOT = -4942
185592
YDOT = 15062
356097 feet/sec YDOT = 4591
006138 meter/sec
ZDOT = -9692
772655 ZDOT = -2954
357105
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 19043
54302527
00016717 00000-0 10270-3 0 9013
2 25544 51
6398 261
0680 0005579 14
4841 345
6470 15
53290483 35888
Satellite: ISS
Catalog Number: 25544
Epoch time: 19043
54302527 = yrday
fracday
Element set: 901
Inclination: 51
6398 deg
RA of node: 261
0680 deg
Eccentricity:
0005579
Arg of perigee: 14
4841 deg
Mean anomaly: 345
6470 deg
Mean motion: 15
53290483 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3588
Checksum: 315
Coasting Arc #3 (Orbit 3602)
---------------------------------------
Vector Time (GMT): 2019/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4126904
09 A = 6785778
89 meter
Y = -3864237
90 meter E =
0008539
Z = -3756026
70 I = 51
26713
XDOT = 1894
796584 Wp = 63
09967
YDOT = -6110
839291 meter/sec RA = 255
31730 deg
ZDOT = 4216
229464 TA = 251
71590
MA = 251
80882
Ha = 223
610 n
mi
Hp = 215
049
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13539711
58 X = -4065141
89
Y = -12677945
86 feet Y = -3910042
55 meter
Z = -12322922
23 Z = -3775923
34
XDOT = 6216
524226 XDOT = 1942
509026
YDOT = -20048
685338 feet/sec YDOT = -6089
383501 meter/sec
ZDOT = 13832
773833 ZDOT = 4225
549561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2910171
16 X = -887020
17
Y = -18258540
15 feet Y = -5565203
04 meter
Z = -12412297
47 Z = -3783268
27
XDOT = 15762
967918 XDOT = 4804
552621
YDOT = -11920
166168 feet/sec YDOT = -3633
266648 meter/sec
ZDOT = 13875
424136 ZDOT = 4229
229277
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 19044
50810013
00016717 00000-0 10270-3 0 9025
2 25544 51
6391 256
2621 0005531 18
7007 341
4348 15
53264645 36038
Satellite: ISS
Catalog Number: 25544
Epoch time: 19044
50810013 = yrday
fracday
Element set: 902
Inclination: 51
6391 deg
RA of node: 256
2621 deg
Eccentricity:
0005531
Arg of perigee: 18
7007 deg
Mean anomaly: 341
4348 deg
Mean motion: 15
53264645 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3603
Checksum: 277
Coasting Arc #4 (Orbit 3618)
---------------------------------------
Vector Time (GMT): 2019/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3954037
18 A = 6788812
69 meter
Y = 4861155
07 meter E =
0015547
Z = 2602120
52 I = 51
28654
XDOT = -2656
202373 Wp = 81
63505
YDOT = 4962
541570 meter/sec RA = 250
31705 deg
ZDOT = -5205
577495 TA = 68
92563
MA = 68
75946
Ha = 223
712 n
mi
Hp = 214
901
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12972562
94 X = 3886745
02
Y = 15948671
49 feet Y = 4904995
62 meter
Z = 8537140
83 Z = 2621164
04
XDOT = -8714
574715 XDOT = -2686
212042
YDOT = 16281
304364 feet/sec YDOT = 4932
670257 meter/sec
ZDOT = -17078
666323 ZDOT = -5218
553050
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 836328
37 X = 254912
89
Y = 20505654
52 feet Y = 6250123
50 meter
Z = 8622585
02 Z = 2628163
91
XDOT = -15124
529676 XDOT = -4609
956645
YDOT = 7862
810555 feet/sec YDOT = 2396
584657 meter/sec
ZDOT = -17137
688638 ZDOT = -5223
567497
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 19045
53750918
00016717 00000-0 10270-3 0 9037
2 25544 51
6386 251
1372 0005711 21
9538 338
1858 15
53301417 36199
Satellite: ISS
Catalog Number: 25544
Epoch time: 19045
53750918 = yrday
fracday
Element set: 903
Inclination: 51
6386 deg
RA of node: 251
1372 deg
Eccentricity:
0005711
Arg of perigee: 21
9538 deg
Mean anomaly: 338
1858 deg
Mean motion: 15
53301417 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3619
Checksum: 310
Coasting Arc #5 (Orbit 3633)
---------------------------------------
Vector Time (GMT): 2019/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3693150
36 A = 6791112
17 meter
Y = -5540493
45 meter E =
0014210
Z = -1301739
64 I = 51
30449
XDOT = 3440
053862 Wp = 33
47985
YDOT = -3646
612820 meter/sec RA = 245
32313 deg
ZDOT = 5803
031706 TA = 312
28917
MA = 312
40954
Ha = 223
751 n
mi
Hp = 214
925
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12116635
05 X = -3624597
50
Y = -18177471
96 feet Y = -5581409
52 meter
Z = -4270799
35 Z = -1319512
82
XDOT = 11286
265952 XDOT = 3452
388230
YDOT = -11963
952821 feet/sec YDOT = -3608
074822 meter/sec
ZDOT = 19038
817934 ZDOT = 5819
771835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 782894
43 X = 238626
22
Y = -21815902
00 feet Y = -6649486
93 meter
Z = -4350466
06 Z = -1326022
06
XDOT = 14450
421918 XDOT = 4404
488601
YDOT = -3266
267162 feet/sec YDOT = -995
558231 meter/sec
ZDOT = 19114
696636 ZDOT = 5826
159535
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 19046
50258106
00016717 00000-0 10270-3 0 9048
2 25544 51
6370 246
3323 0005472 26
1410 334
0017 15
53258508 36345
Satellite: ISS
Catalog Number: 25544
Epoch time: 19046
50258106 = yrday
fracday
Element set: 904
Inclination: 51
6370 deg
RA of node: 246
3323 deg
Eccentricity:
0005472
Arg of perigee: 26
1410 deg
Mean anomaly: 334
0017 deg
Mean motion: 15
53258508 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3634
Checksum: 277
Coasting Arc #6 (Orbit 3649)
---------------------------------------
Vector Time (GMT): 2019/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3260910
90 A = 6791764
78 meter
Y = 5953487
14 meter E =
0011642
Z = -141387
18 I = 51
32197
XDOT = -4257
022784 Wp = 107
98101
YDOT = 2199
427439 meter/sec RA = 240
33371 deg
ZDOT = -5980
631645 TA = 73
54754
MA = 73
41962
Ha = 223
877 n
mi
Hp = 214
749
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10698526
57 X = 3194781
73
Y = 19532438
13 feet Y = 5989583
17 meter
Z = -463868
69 Z = -125707
80
XDOT = -13966
610184 XDOT = -4252
251072
YDOT = 7215
969289 feet/sec YDOT = 2151
849174 meter/sec
ZDOT = -19621
494897 ZDOT = -6001
298598
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2318474
17 X = -706670
93
Y = 22150834
94 feet Y = 6751574
49 meter
Z = -393666
15 Z = -119989
44
XDOT = -13866
536473 XDOT = -4226
520317
YDOT = -1773
531259 feet/sec YDOT = -540
572328 meter/sec
ZDOT = -19714
959637 ZDOT = -6009
119697
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 19047
53198704
00016717 00000-0 10270-3 0 9050
2 25544 51
6372 241
2066 0005636 29
5091 330
6379 15
53287463 36502
Satellite: ISS
Catalog Number: 25544
Epoch time: 19047
53198704 = yrday
fracday
Element set: 905
Inclination: 51
6372 deg
RA of node: 241
2066 deg
Eccentricity:
0005636
Arg of perigee: 29
5091 deg
Mean anomaly: 330
6379 deg
Mean motion: 15
53287463 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3650
Checksum: 316
Coasting Arc #7 (Orbit 3665)
---------------------------------------
Vector Time (GMT): 2019/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2684627
37 A = 6790881
65 meter
Y = -6035792
00 meter E =
0018981
Z = 1529569
10 I = 51
33465
XDOT = 5039
186880 Wp = 54
52194
YDOT = -778
374258 meter/sec RA = 235
34417 deg
ZDOT = 5733
571043 TA = 322
27034
MA = 322
40329
Ha = 223
948 n
mi
Hp = 214
702
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8807832
57 X = -2624363
51
Y = -19802467
19 feet Y = -6065476
41 meter
Z = 5018271
31 Z = 1516674
93
XDOT = 16532
765354 XDOT = 5019
666611
YDOT = -2553
721319 feet/sec YDOT = -722
131674 meter/sec
ZDOT = 18810
928618 ZDOT = 5758
001455
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3634251
21 X = 1107719
77
Y = -21379502
37 feet Y = -6516472
32 meter
Z = 4960621
42 Z = 1511997
41
XDOT = 13505
845844 XDOT = 4116
581813
YDOT = 6716
448496 feet/sec YDOT = 2047
173501 meter/sec
ZDOT = 18921
255830 ZDOT = 5767
198777
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 19048
56139123
00016717 00000-0 10270-3 0 9065
2 25544 51
6357 236
0804 0005545 34
8574 325
2940 15
53264098 36661
Satellite: ISS
Catalog Number: 25544
Epoch time: 19048
56139123 = yrday
fracday
Element set: 906
Inclination: 51
6357 deg
RA of node: 236
0804 deg
Eccentricity:
0005545
Arg of perigee: 34
8574 deg
Mean anomaly: 325
2940 deg
Mean motion: 15
53264098 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3666
Checksum: 320
Coasting Arc #8 (Orbit 3680)
---------------------------------------
Vector Time (GMT): 2019/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1898849
53 A = 6788359
08 meter
Y = 5865378
95 meter E =
0007970
Z = -2851002
16 I = 51
34568
XDOT = -5731
190321 Wp = 74
37707
YDOT = -592
086360 meter/sec RA = 230
35290 deg
ZDOT = -5044
950153 TA = 138
13531
MA = 138
07433
Ha = 224
031 n
mi
Hp = 214
531
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6229821
29 X = 1846968
25
Y = 19243369
25 feet Y = 5886323
04 meter
Z = -9353681
63 Z = -2841904
73
XDOT = -18803
117851 XDOT = -5699
638674
YDOT = -1942
540551 feet/sec YDOT = -656
000266 meter/sec
ZDOT = -16551
673730 ZDOT = -5072
712631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5108031
57 X = -1556928
02
Y = 19590378
40 feet Y = 5971147
34 meter
Z = -9313129
51 Z = -2838641
88
XDOT = -13246
514670 XDOT = -4037
537671
YDOT = -11366
806753 feet/sec YDOT = -3464
602698 meter/sec
ZDOT = -16676
932021 ZDOT = -5083
128880
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 19049
52645541
00016717 00000-0 10270-3 0 9079
2 25544 51
6350 231
2753 0005661 39
0078 321
1482 15
53288542 36812
Satellite: ISS
Catalog Number: 25544
Epoch time: 19049
52645541 = yrday
fracday
Element set: 907
Inclination: 51
6350 deg
RA of node: 231
2753 deg
Eccentricity:
0005661
Arg of perigee: 39
0078 deg
Mean anomaly: 321
1482 deg
Mean motion: 15
53288542 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3681
Checksum: 305
Coasting Arc #9 (Orbit 3696)
---------------------------------------
Vector Time (GMT): 2019/050/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -960027
95 A = 6785227
39 meter
Y = -5439460
53 meter E =
0014726
Z = 3926530
33 I = 51
35748
XDOT = 6287
505945 Wp = 81
97655
YDOT = 1797
040684 meter/sec RA = 225
35573 deg
ZDOT = 4015
820370 TA = 325
90917
MA = 326
00367
Ha = 223
959 n
mi
Hp = 214
522
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3149697
98 X = -918203
33
Y = -17845999
12 feet Y = -5449962
13 meter
Z = 12882317
35 Z = 3921968
94
XDOT = 20628
300345 XDOT = 6247
437609
YDOT = 5895
802768 feet/sec YDOT = 1867
128180 meter/sec
ZDOT = 13175
263680 ZDOT = 4046
264346
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6634605
55 X = 2022227
77
Y = -16878999
16 feet Y = -5144718
94 meter
Z = 12862184
06 Z = 3920393
70
XDOT = 13136
141647 XDOT = 4003
895974
YDOT = 15335
206558 feet/sec YDOT = 4674
170959 meter/sec
ZDOT = 13312
540117 ZDOT = 4057
662228
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 19050
55585457
00016717 00000-0 10270-3 0 9084
2 25544 51
6352 226
1492 0005379 42
3678 317
7888 15
53296201 36975
Satellite: ISS
Catalog Number: 25544
Epoch time: 19050
55585457 = yrday
fracday
Element set: 908
Inclination: 51
6352 deg
RA of node: 226
1492 deg
Eccentricity:
0005379
Arg of perigee: 42
3678 deg
Mean anomaly: 317
7888 deg
Mean motion: 15
53296201 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3697
Checksum: 343
Coasting Arc #10 (Orbit 3711)
---------------------------------------
Vector Time (GMT): 2019/051/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -149198
59 A = 6782229
95 meter
Y = 4854116
88 meter E =
0016429
Z = -4750284
03 I = 51
37311
XDOT = -6600
089411 Wp = 63
62864
YDOT = -2812
123865 meter/sec RA = 220
35352 deg
ZDOT = -2666
329017 TA = 179
88868
MA = 179
88831
Ha = 224
149 n
mi
Hp = 214
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -489496
67 X = -180394
01
Y = 15925580
30 feet Y = 4852273
58 meter
Z = -15584921
36 Z = -4751084
97
XDOT = -21653
836651 XDOT = -6555
201737
YDOT = -9226
128165 feet/sec YDOT = -2885
679935 meter/sec
ZDOT = -8747
798611 ZDOT = -2698
279597
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8473221
11 X = -2582637
79
Y = 13488632
37 feet Y = 4111335
14 meter
Z = -15588932
29 Z = -4751506
56
XDOT = -12857
507605 XDOT = -3918
968318
YDOT = -18352
977179 feet/sec YDOT = -5593
987444 meter/sec
ZDOT = -8891
811447 ZDOT = -2710
224129
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 19051
52091546
00016717 00000-0 10270-3 0 9094
2 25544 51
6367 221
3441 0005692 47
9525 312
2111 15
53292838 37121
Satellite: ISS
Catalog Number: 25544
Epoch time: 19051
52091546 = yrday
fracday
Element set: 909
Inclination: 51
6367 deg
RA of node: 221
3441 deg
Eccentricity:
0005692
Arg of perigee: 47
9525 deg
Mean anomaly: 312
2111 deg
Mean motion: 15
53292838 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3712
Checksum: 299
Coasting Arc #11 (Orbit 3727)
---------------------------------------
Vector Time (GMT): 2019/052/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1351980
55 A = 6780346
60 meter
Y = -4129764
16 meter E =
0007846
Z = 5197904
50 I = 51
39172
XDOT = 6670
940430 Wp = 80
67963
YDOT = 3616
986698 meter/sec RA = 215
34660 deg
ZDOT = 1138
375005 TA = 358
37504
MA = 358
37759
Ha = 224
174 n
mi
Hp = 214
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4435631
72 X = 1372812
31
Y = -13549095
01 feet Y = -4114528
33 meter
Z = 17053492
45 Z = 5204522
80
XDOT = 21886
287499 XDOT = 6624
469003
YDOT = 11866
754260 feet/sec YDOT = 3691
326101 meter/sec
ZDOT = 3734
826132 ZDOT = 1170
665916
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10477046
81 X = 3193403
87
Y = -9615252
39 feet Y = -2930728
93 meter
Z = 17083700
44 Z = 5207111
89
XDOT = 12384
385782 XDOT = 3774
760786
YDOT = 20389
961532 feet/sec YDOT = 6214
860275 meter/sec
ZDOT = 3880
330050 ZDOT = 1182
724599
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 19052
55031127
00016717 00000-0 10270-3 0 9109
2 25544 51
6357 216
2180 0005672 51
4562 308
7098 15
53256238 37287
Satellite: ISS
Catalog Number: 25544
Epoch time: 19052
55031127 = yrday
fracday
Element set: 910
Inclination: 51
6357 deg
RA of node: 216
2180 deg
Eccentricity:
0005672
Arg of perigee: 51
4562 deg
Mean anomaly: 308
7098 deg
Mean motion: 15
53256238 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3728
Checksum: 300
Coasting Arc #12 (Orbit 3742)
---------------------------------------
Vector Time (GMT): 2019/053/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2598931
92 A = 6779859
30 meter
Y = 3371633
92 meter E =
0019508
Z = -5293430
60 I = 51
41996
XDOT = -6391
191884 Wp = 83
67869
YDOT = -4182
295893 meter/sec RA = 210
34079 deg
ZDOT = 477
625908 TA = 190
87932
MA = 190
92158
Ha = 224
197 n
mi
Hp = 214
084
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8526679
54 X = -2610729
25
Y = 11061791
06 feet Y = 3342504
29 meter
Z = -17366898
31 Z = -5306084
04
XDOT = -20968
477311 XDOT = -6346
269267
YDOT = -13721
443220 feet/sec YDOT = -4253
515436 meter/sec
ZDOT = 1567
014135 ZDOT = 446
690029
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12696441
22 X = -3869875
29
Y = 5645441
97 feet Y = 1720730
71 meter
Z = -17424293
60 Z = -5310924
69
XDOT = -11369
731426 XDOT = -3465
494139
YDOT = -21200
410265 feet/sec YDOT = -6461
885049 meter/sec
ZDOT = 1427
654297 ZDOT = 435
149030
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 19053
51536651
00016717 00000-0 10270-3 0 9119
2 25544 51
6375 211
4144 0005605 55
7779 304
3903 15
53292538 37434
Satellite: ISS
Catalog Number: 25544
Epoch time: 19053
51536651 = yrday
fracday
Element set: 911
Inclination: 51
6375 deg
RA of node: 211
4144 deg
Eccentricity:
0005605
Arg of perigee: 55
7779 deg
Mean anomaly: 304
3903 deg
Mean motion: 15
53292538 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3743
Checksum: 307
Coasting Arc #13 (Orbit 3758)
---------------------------------------
Vector Time (GMT): 2019/054/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3816246
36 A = 6781255
16 meter
Y = -2576057
11 meter E =
0011640
Z = 4971865
06 I = 51
45398
XDOT = 5800
644735 Wp = 58
40451
YDOT = 4573
789588 meter/sec RA = 205
33546 deg
ZDOT = -2073
021450 TA = 51
85840
MA = 51
75355
Ha = 224
189 n
mi
Hp = 214
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12520493
31 X = 3820618
71
Y = -8451630
94 feet Y = -2533356
23 meter
Z = 16311893
23 Z = 4990413
57
XDOT = 19030
986663 XDOT = 5759
137661
YDOT = 15005
871353 feet/sec YDOT = 4638
424162 meter/sec
ZDOT = -6801
251476 ZDOT = -2044
945761
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14919640
48 X = 4547506
42
Y = -1688525
02 feet Y = -514662
43 meter
Z = 16395849
79 Z = 4997455
02
XDOT = 9755
428258 XDOT = 2973
454533
YDOT = 21081
222421 feet/sec YDOT = 6425
556594 meter/sec
ZDOT = -6674
819889 ZDOT = -2034
485102
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 19054
54475764
00016717 00000-0 10270-3 0 9121
2 25544 51
6377 206
2878 0005652 59
5984 300
5726 15
53258735 37593
Satellite: ISS
Catalog Number: 25544
Epoch time: 19054
54475764 = yrday
fracday
Element set: 912
Inclination: 51
6377 deg
RA of node: 206
2878 deg
Eccentricity:
0005652
Arg of perigee: 59
5984 deg
Mean anomaly: 300
5726 deg
Mean motion: 15
53258735 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3759
Checksum: 348
Coasting Arc #14 (Orbit 3773)
---------------------------------------
Vector Time (GMT): 2019/055/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4905424
88 A = 6783769
20 meter
Y = 1845939
04 meter E =
0013161
Z = -4318556
98 I = 51
49393
XDOT = -4864
467856 Wp = 92
21494
YDOT = -4769
336654 meter/sec RA = 200
33951 deg
ZDOT = 3495
640844 TA = 213
43312
MA = 213
51628
Ha = 224
251 n
mi
Hp = 213
972
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16093913
64 X = -4904725
20
Y = 6056230
44 feet Y = 1791086
70 meter
Z = -14168494
02 Z = -4342383
86
XDOT = -15959
540209 XDOT = -4827
753934
YDOT = -15647
429967 feet/sec YDOT = -4823
528961 meter/sec
ZDOT = 11468
637939 ZDOT = 3472
100929
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17010221
08 X = -5184715
39
Y = -1810949
38 feet Y = -551977
37 meter
Z = -14276240
65 Z = -4351398
15
XDOT = -7387
878236 XDOT = -2251
825286
YDOT = -19956
788143 feet/sec YDOT = -6082
829026 meter/sec
ZDOT = 11362
689044 ZDOT = 3463
347621
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 19055
50980729
00016717 00000-0 10270-3 0 9131
2 25544 51
6384 201
4840 0005660 62
2390 297
9336 15
53287820 37748
Satellite: ISS
Catalog Number: 25544
Epoch time: 19055
50980729 = yrday
fracday
Element set: 913
Inclination: 51
6384 deg
RA of node: 201
4840 deg
Eccentricity:
0005660
Arg of perigee: 62
2390 deg
Mean anomaly: 297
9336 deg
Mean motion: 15
53287820 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3774
Checksum: 323
Coasting Arc #15 (Orbit 3789)
---------------------------------------
Vector Time (GMT): 2019/056/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5811529
45 A = 6787062
68 meter
Y = -1128042
97 meter E =
0017788
Z = 3305951
06 I = 51
53571
XDOT = 3627
609658 Wp = 84
12669
YDOT = 4862
950574 meter/sec RA = 195
35120 deg
ZDOT = -4694
113212 TA = 57
36037
MA = 57
18885
Ha = 224
225 n
mi
Hp = 214
043
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19066697
66 X = 5807653
33
Y = -3700928
39 feet Y = -1063075
85 meter
Z = 10846296
13 Z = 3334171
63
XDOT = 11901
606491 XDOT = 3595
762299
YDOT = 15954
562251 feet/sec YDOT = 4903
338661 meter/sec
ZDOT = -15400
633898 ZDOT = -4676
569515
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18708927
44 X = 5702481
08
Y = 4942540
18 feet Y = 1506486
25 meter
Z = 10973846
22 Z = 3344828
33
XDOT = 4217
129105 XDOT = 1285
380951
YDOT = 18225
139848 feet/sec YDOT = 5555
022626 meter/sec
ZDOT = -15321
760536 ZDOT = -4670
072611
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 19056
53919339
00016717 00000-0 10270-3 0 9145
2 25544 51
6377 196
3584 0005593 66
7844 293
3897 15
53278312 37901
Satellite: ISS
Catalog Number: 25544
Epoch time: 19056
53919339 = yrday
fracday
Element set: 914
Inclination: 51
6377 deg
RA of node: 196
3584 deg
Eccentricity:
0005593
Arg of perigee: 66
7844 deg
Mean anomaly: 293
3897 deg
Mean motion: 15
53278312 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3790
Checksum: 360
Coasting Arc #16 (Orbit 3798)
---------------------------------------
Vector Time (GMT): 2019/057/02:28:25
618
Vector Time (MET): N/A
Weight (LBS) : 900439
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1577005
32 A = 6781499
59 meter
Y = 3957857
25 meter E =
0017536
Z = -5291173
05 I = 51
53311
XDOT = -7332
314259 Wp = 86
66579
YDOT = -2106
279122 meter/sec RA = 192
36943 deg
ZDOT = 612
591191 TA = 189
18566
MA = 189
21778
Ha = 224
337 n
mi
Hp = 215
681
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5173901
95 X = -1595444
71
Y = 12985095
98 feet Y = 3940118
68 meter
Z = -17359491
64 Z = -5298878
47
XDOT = -24056
149144 XDOT = -7311
191894
YDOT = -6910
364574 feet/sec YDOT = -2188
156044 meter/sec
ZDOT = 2009
813620 ZDOT = 577
025405
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2276667
86 X = 693928
36
Y = -13746954
02 feet Y = -4190071
58 meter
Z = -17394595
93 Z = -5301872
84
XDOT = 23973
602613 XDOT = 7307
154076
YDOT = 1641
725590 feet/sec YDOT = 500
397960 meter/sec
ZDOT = 1849
317876 ZDOT = 563
672088
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 19057
11822316
00016717 00000-0 10270-3 0 9159
2 25544 51
6397 193
4804 0003645 51
2819 308
8658 15
52743755 37996
Satellite: ISS
Catalog Number: 25544
Epoch time: 19057
11822316 = yrday
fracday
Element set: 915
Inclination: 51
6397 deg
RA of node: 193
4804 deg
Eccentricity:
0003645
Arg of perigee: 51
2819 deg
Mean anomaly: 308
8658 deg
Mean motion: 15
52743755 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3799
Checksum: 339
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