[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
February 4th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17659 2714 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 5 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
037/01:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 222
9
000/00:00:00
000 0
0 0
0 216
1
039/16:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
2
000/00:00:00
000 0
0 0
0 215
6
040/11:22:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
2
000/00:00:00
000 0
0 0
0 215
5
044/15:48:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
7
000/00:00:00
000 0
0 0
0 215
1
Coasting Arc #1 (Orbit 3462)
---------------------------------------
Vector Time (GMT): 2019/035/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3167300
52 A = 6791913
49 meter
Y = -5986717
40 meter E =
0015206
Z = -368643
93 I = 51
33256
XDOT = 4392
050434 Wp = 25
88808
YDOT = 1962
280560 meter/sec RA = 300
37760 deg
ZDOT = 5975
107059 TA = 330
12047
MA = 330
20719
Ha = 222
984 n
mi
Hp = 216
193
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10391405
91 X = 3235800
90
Y = -19641461
29 feet Y = -5950915
43 meter
Z = -1209461
71 Z = -353092
45
XDOT = 14409
614284 XDOT = 4340
758321
YDOT = 6437
928348 feet/sec YDOT = 2011
108730 meter/sec
ZDOT = 19603
369617 ZDOT = 5996
316808
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21407932
70 X = 6525137
89
Y = -5969519
86 feet Y = -1819509
65 meter
Z = -1138580
89 Z = -347039
46
XDOT = 4717
111713 XDOT = 1437
775650
YDOT = 13230
313694 feet/sec YDOT = 4032
599614 meter/sec
ZDOT = 19698
806039 ZDOT = 6004
196081
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 19035
50067092
00016717 00000-0 10270-3 0 9004
2 25544 51
6415 301
1063 0005380 349
1232 10
9803 15
53223109 34636
Satellite: ISS
Catalog Number: 25544
Epoch time: 19035
50067092 = yrday
fracday
Element set: 900
Inclination: 51
6415 deg
RA of node: 301
1063 deg
Eccentricity:
0005380
Arg of perigee: 349
1232 deg
Mean anomaly: 10
9803 deg
Mean motion: 15
53223109 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3463
Checksum: 264
Coasting Arc #2 (Orbit 3478)
---------------------------------------
Vector Time (GMT): 2019/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3620337
72 A = 6791499
78 meter
Y = 5646293
53 meter E =
0005605
Z = -1061025
63 I = 51
31533
XDOT = -3583
458193 Wp = 114
04674
YDOT = -3393
910273 meter/sec RA = 295
39061 deg
ZDOT = -5860
510584 TA = 77
49980
MA = 77
43710
Ha = 223
044 n
mi
Hp = 216
137
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11877748
43 X = -3678053
37
Y = 18524585
09 feet Y = 5605485
67 meter
Z = -3481055
22 Z = -1078751
63
XDOT = -11756
752601 XDOT = -3516
773921
YDOT = -11134
876224 feet/sec YDOT = -3433
610242 meter/sec
ZDOT = -19227
396929 ZDOT = -5877
755163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21523929
99 X = -6560493
86
Y = 4515942
14 feet Y = 1376459
16 meter
Z = -3561686
41 Z = -1085602
02
XDOT = 131
754337 XDOT = 40
158722
YDOT = -14529
700980 feet/sec YDOT = -4428
652859 meter/sec
ZDOT = -19304
781564 ZDOT = -5884
097421
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 19036
53010002
00016717 00000-0 10270-3 0 9018
2 25544 51
6415 295
9825 0005210 351
4829 8
6234 15
53208675 34792
Satellite: ISS
Catalog Number: 25544
Epoch time: 19036
53010002 = yrday
fracday
Element set: 901
Inclination: 51
6415 deg
RA of node: 295
9825 deg
Eccentricity:
0005210
Arg of perigee: 351
4829 deg
Mean anomaly: 8
6234 deg
Mean motion: 15
53208675 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3479
Checksum: 294
Coasting Arc #3 (Orbit 3487)
---------------------------------------
Vector Time (GMT): 2019/037/01:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4324587
68 A = 6780302
57 meter
Y = 460951
43 meter E =
0003937
Z = 5199035
89 I = 51
26896
XDOT = -2088
017577 Wp = 40
15416
YDOT = 7298
705814 meter/sec RA = 292
59101 deg
ZDOT = 1092
209428 TA = 39
34176
MA = 39
31317
Ha = 222
862 n
mi
Hp = 216
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14188279
79 X = 4293858
47
Y = 1512307
85 feet Y = 509140
31 meter
Z = 17057204
36 Z = 5219967
87
XDOT = -6850
451368 XDOT = -2174
783776
YDOT = 23945
885218 feet/sec YDOT = 7274
871033 meter/sec
ZDOT = 3583
364265 ZDOT = 1081
855987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12274510
23 X = -3741270
72
Y = -7050005
28 feet Y = -2148841
61 meter
Z = 17151571
45 Z = 5227798
98
XDOT = 15416
664953 XDOT = 4698
999478
YDOT = -18259
133920 feet/sec YDOT = -5565
384019 meter/sec
ZDOT = 3535
805886 ZDOT = 1077
713634
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 19037
10915057
00016717 00000-0 10270-3 0 9027
2 25544 51
6400 293
0977 0005088 353
3260 6
7823 15
53244720 34880
Satellite: ISS
Catalog Number: 25544
Epoch time: 19037
10915057 = yrday
fracday
Element set: 902
Inclination: 51
6400 deg
RA of node: 293
0977 deg
Eccentricity:
0005088
Arg of perigee: 353
3260 deg
Mean anomaly: 6
7823 deg
Mean motion: 15
53244720 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3488
Checksum: 301
Coasting Arc #4 (Orbit 3502)
---------------------------------------
Vector Time (GMT): 2019/038/01:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3865393
55 A = 6780105
44 meter
Y = -1819454
74 meter E =
0015104
Z = -5277098
26 I = 51
25638
XDOT = 2687
922434 Wp = 73
69042
YDOT = -7151
719758 meter/sec RA = 287
57443 deg
ZDOT = 502
295725 TA = 201
10327
MA = 201
16565
Ha = 223
175 n
mi
Hp = 215
766
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12681737
36 X = -3819128
08
Y = -5969339
70 feet Y = -1862421
80 meter
Z = -17313314
51 Z = -5295761
95
XDOT = 8818
643155 XDOT = 2765
255402
YDOT = -23463
647500 feet/sec YDOT = -7121
229117 meter/sec
ZDOT = 1647
951853 ZDOT = 515
540417
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9279626
91 X = 2828430
28
Y = 10364989
06 feet Y = 3159248
67 meter
Z = -17397294
74 Z = -5302695
44
XDOT = -16439
290090 XDOT = -5010
695619
YDOT = 17556
143734 feet/sec YDOT = 5351
112610 meter/sec
ZDOT = 1708
512848 ZDOT = 520
754716
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 19038
07423716
00016717 00000-0 10270-3 0 9031
2 25544 51
6402 288
2933 0005239 358
0324 2
0806 15
53215453 35030
Satellite: ISS
Catalog Number: 25544
Epoch time: 19038
07423716 = yrday
fracday
Element set: 903
Inclination: 51
6402 deg
RA of node: 288
2933 deg
Eccentricity:
0005239
Arg of perigee: 358
0324 deg
Mean anomaly: 2
0806 deg
Mean motion: 15
53215453 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3503
Checksum: 285
Coasting Arc #5 (Orbit 3518)
---------------------------------------
Vector Time (GMT): 2019/039/01:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3370013
39 A = 6781344
22 meter
Y = 3168427
58 meter E =
0010124
Z = 4957041
19 I = 51
25085
XDOT = -3189
956528 Wp = 31
74105
YDOT = 6657
103943 meter/sec RA = 282
55875 deg
ZDOT = -2075
989660 TA = 78
62765
MA = 78
51393
Ha = 223
159 n
mi
Hp = 215
701
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11056474
38 X = 3310254
69
Y = 10395103
61 feet Y = 3205779
56 meter
Z = 16263258
51 Z = 4973265
76
XDOT = -10465
736641 XDOT = -3254
077294
YDOT = 21840
892200 feet/sec YDOT = 6621
072989 meter/sec
ZDOT = -6810
989699 ZDOT = -2091
640997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6312821
78 X = -1924148
08
Y = -13714146
42 feet Y = -4180071
83 meter
Z = 16336090
45 Z = 4979240
37
XDOT = 16774
728923 XDOT = 5112
937376
YDOT = -15960
274365 feet/sec YDOT = -4864
691627 meter/sec
ZDOT = -6882
329868 ZDOT = -2097
734144
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 19039
10365996
00016717 00000-0 10270-3 0 9042
2 25544 51
6391 283
1691 0005250 2
1504 357
9669 15
53259652 35197
Satellite: ISS
Catalog Number: 25544
Epoch time: 19039
10365996 = yrday
fracday
Element set: 904
Inclination: 51
6391 deg
RA of node: 283
1691 deg
Eccentricity:
0005250
Arg of perigee: 2
1504 deg
Mean anomaly: 357
9669 deg
Mean motion: 15
53259652 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3519
Checksum: 323
Coasting Arc #6 (Orbit 3527)
---------------------------------------
Vector Time (GMT): 2019/039/16:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2552402
99 A = 6784690
17 meter
Y = -4757932
05 meter E =
0007976
Z = -4113127
81 I = 51
25490
XDOT = 3959
111464 Wp = 70
65105
YDOT = -5371
273651 meter/sec RA = 279
47146 deg
ZDOT = 3765
075185 TA = 238
36555
MA = 238
44339
Ha = 223
242 n
mi
Hp = 215
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8374025
56 X = -2479029
90
Y = -15610013
28 feet Y = -4786064
79 meter
Z = -13494513
81 Z = -4125347
67
XDOT = 12989
210841 XDOT = 4000
592066
YDOT = -17622
288881 feet/sec YDOT = -5326
767950 meter/sec
ZDOT = 12352
608876 ZDOT = 3784
407709
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13142628
74 X = -4005873
24
Y = -11814888
31 feet Y = -3601177
96 meter
Z = -13549112
35 Z = -4129769
45
XDOT = 5205
290955 XDOT = 1586
572683
YDOT = -20024
508090 feet/sec YDOT = -6103
470066 meter/sec
ZDOT = 12440
401034 ZDOT = 3791
834235
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 19039
68271119
00016717 00000-0 10270-3 0 9059
2 25544 51
6362 280
2831 0005125 4
5569 355
5629 15
53240765 35282
Satellite: ISS
Catalog Number: 25544
Epoch time: 19039
68271119 = yrday
fracday
Element set: 905
Inclination: 51
6362 deg
RA of node: 280
2831 deg
Eccentricity:
0005125
Arg of perigee: 4
5569 deg
Mean anomaly: 355
5629 deg
Mean motion: 15
53240765 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3528
Checksum: 315
Coasting Arc #7 (Orbit 3540)
---------------------------------------
Vector Time (GMT): 2019/040/11:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3834608
29 A = 6780881
13 meter
Y = 2415043
86 meter E =
0009863
Z = 5042260
72 I = 51
24372
XDOT = -2130
771893 Wp = 29
72276
YDOT = 7145
371259 meter/sec RA = 275
48100 deg
ZDOT = -1791
975287 TA = 77
76940
MA = 77
65896
Ha = 223
221 n
mi
Hp = 215
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12580735
85 X = 3782825
55
Y = 7923372
26 feet Y = 2457635
91 meter
Z = 16542850
13 Z = 5060761
54
XDOT = -6990
721433 XDOT = -2201
810831
YDOT = 23442
819092 feet/sec YDOT = 7121
146167 meter/sec
ZDOT = -5879
184014 ZDOT = -1802
498560
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1690914
75 X = 515390
82
Y = 14677744
25 feet Y = 4473776
45 meter
Z = 16626041
74 Z = 5067617
52
XDOT = -21521
214446 XDOT = -6559
666163
YDOT = 9230
258165 feet/sec YDOT = 2813
382689 meter/sec
ZDOT = -5927
419684 ZDOT = -1806
677520
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 19040
51911462
00016717 00000-0 10270-3 0 9066
2 25544 51
6410 276
1237 0005494 4
5406 355
5795 15
53288655 35418
Satellite: ISS
Catalog Number: 25544
Epoch time: 19040
51911462 = yrday
fracday
Element set: 906
Inclination: 51
6410 deg
RA of node: 276
1237 deg
Eccentricity:
0005494
Arg of perigee: 4
5406 deg
Mean anomaly: 355
5795 deg
Mean motion: 15
53288655 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3541
Checksum: 308
Coasting Arc #8 (Orbit 3555)
---------------------------------------
Vector Time (GMT): 2019/041/11:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3544241
93 A = 6783388
92 meter
Y = -3699195
13 meter E =
0009906
Z = -4453357
74 I = 51
24945
XDOT = 2647
723596 Wp = 77
09969
YDOT = -6419
744144 meter/sec RA = 270
46690 deg
ZDOT = 3233
641036 TA = 225
63035
MA = 225
71154
Ha = 223
433 n
mi
Hp = 215
359
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11628090
31 X = -3480981
46
Y = -12136466
95 feet Y = -3738475
86 meter
Z = -14610753
74 Z = -4470420
21
XDOT = 8686
757205 XDOT = 2703
607212
YDOT = -21062
152704 feet/sec YDOT = -6389
822796 meter/sec
ZDOT = 10609
058518 ZDOT = 3246
638592
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1888447
46 X = 575598
79
Y = -16634199
41 feet Y = -5070103
98 meter
Z = -14687328
39 Z = -4476697
69
XDOT = 20459
860321 XDOT = 6236
165426
YDOT = -7073
123156 feet/sec YDOT = -2155
887938 meter/sec
ZDOT = 10668
361637 ZDOT = 3251
716627
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 19041
48419605
00016717 00000-0 10270-3 0 9076
2 25544 51
6408 271
3187 0005571 8
6557 351
4690 15
53255092 35568
Satellite: ISS
Catalog Number: 25544
Epoch time: 19041
48419605 = yrday
fracday
Element set: 907
Inclination: 51
6408 deg
RA of node: 271
3187 deg
Eccentricity:
0005571
Arg of perigee: 8
6557 deg
Mean anomaly: 351
4690 deg
Mean motion: 15
53255092 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3556
Checksum: 318
Coasting Arc #9 (Orbit 3571)
---------------------------------------
Vector Time (GMT): 2019/042/11:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3210574
11 A = 6786509
40 meter
Y = 4834533
37 meter E =
0014688
Z = 3512194
27 I = 51
26035
XDOT = -3169
289664 Wp = 65
84202
YDOT = 5365
172248 meter/sec RA = 265
45964 deg
ZDOT = -4467
296149 TA = 72
56840
MA = 72
40787
Ha = 223
547 n
mi
Hp = 215
226
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10533379
62 X = 3139214
30
Y = 15861329
96 feet Y = 4870037
43 meter
Z = 11522947
08 Z = 3527616
28
XDOT = -10397
931967 XDOT = -3207
349617
YDOT = 17602
271155 feet/sec YDOT = 5329
518012 meter/sec
ZDOT = -14656
483429 ZDOT = -4482
783879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5118309
76 X = -1560060
82
Y = 18295909
11 feet Y = 5576593
10 meter
Z = 11592014
44 Z = 3533246
00
XDOT = -18708
294681 XDOT = -5702
288219
YDOT = 4139
927982 feet/sec YDOT = 1261
850049 meter/sec
ZDOT = -14726
897665 ZDOT = -4488
758408
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
51361357
00016717 00000-0 10270-3 0 9082
2 25544 51
6402 266
1936 0005702 12
8847 347
2450 15
53280812 35724
Satellite: ISS
Catalog Number: 25544
Epoch time: 19042
51361357 = yrday
fracday
Element set: 908
Inclination: 51
6402 deg
RA of node: 266
1936 deg
Eccentricity:
0005702
Arg of perigee: 12
8847 deg
Mean anomaly: 347
2450 deg
Mean motion: 15
53280812 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3572
Checksum: 300
Coasting Arc #10 (Orbit 3586)
---------------------------------------
Vector Time (GMT): 2019/043/11:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2868865
04 A = 6789528
92 meter
Y = -5680812
95 meter E =
0010861
Z = -2353929
42 I = 51
27347
XDOT = 3674
513425 Wp = 30
52894
YDOT = -4068
180602 meter/sec RA = 260
45972 deg
ZDOT = 5359
638343 TA = 303
06878
MA = 303
17303
Ha = 223
611 n
mi
Hp = 215
244
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9412286
88 X = -2793693
42
Y = -18637837
77 feet Y = -5712474
37 meter
Z = -7722865
55 Z = -2367682
36
XDOT = 12055
490238 XDOT = 3693
698020
YDOT = -13347
049218 feet/sec YDOT = -4026
982172 meter/sec
ZDOT = 17584
115297 ZDOT = 5377
534287
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7599781
32 X = 2316413
35
Y = -19422932
75 feet Y = -5920109
90 meter
Z = -7784330
46 Z = -2372663
92
XDOT = 16489
417093 XDOT = 5025
974330
YDOT = -601
703977 feet/sec YDOT = -183
399372 meter/sec
ZDOT = 17665
253734 ZDOT = 5384
369338
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
47869224
00016717 00000-0 10270-3 0 9095
2 25544 51
6399 261
3891 0005631 14
7718 345
3597 15
53238269 35871
Satellite: ISS
Catalog Number: 25544
Epoch time: 19043
47869224 = yrday
fracday
Element set: 909
Inclination: 51
6399 deg
RA of node: 261
3891 deg
Eccentricity:
0005631
Arg of perigee: 14
7718 deg
Mean anomaly: 345
3597 deg
Mean motion: 15
53238269 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3587
Checksum: 350
Coasting Arc #11 (Orbit 3602)
---------------------------------------
Vector Time (GMT): 2019/044/11:22:30
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2436160
92 A = 6791490
70 meter
Y = 6259441
12 meter E =
0013285
Z = 982306
76 I = 51
28721
XDOT = -4199
578045 Wp = 100
25448
YDOT = 2566
836586 meter/sec RA = 255
46574 deg
ZDOT = -5875
544772 TA = 69
05801
MA = 68
91588
Ha = 223
754 n
mi
Hp = 215
104
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7992653
93 X = 2361213
58
Y = 20536224
16 feet Y = 6286264
94 meter
Z = 3222791
20 Z = 993958
43
XDOT = -13778
143192 XDOT = -4199
429215
YDOT = 8421
379876 feet/sec YDOT = 2519
874698 meter/sec
ZDOT = -19276
721694 ZDOT = -5895
944196
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9600608
49 X = -2926265
47
Y = 19826997
69 feet Y = 6043268
90 meter
Z = 3274733
87 Z = 998138
88
XDOT = -14017
055702 XDOT = -4272
398578
YDOT = -3553
204205 feet/sec YDOT = -1083
016642 meter/sec
ZDOT = -19369
002038 ZDOT = -5903
671821
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
50810728
00016717 00000-0 10270-3 0 9107
2 25544 51
6405 256
2636 0005596 19
7238 340
4129 15
53240048 36035
Satellite: ISS
Catalog Number: 25544
Epoch time: 19044
50810728 = yrday
fracday
Element set: 910
Inclination: 51
6405 deg
RA of node: 256
2636 deg
Eccentricity:
0005596
Arg of perigee: 19
7238 deg
Mean anomaly: 340
4129 deg
Mean motion: 15
53240048 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3603
Checksum: 296
Coasting Arc #12 (Orbit 3605)
---------------------------------------
Vector Time (GMT): 2019/044/15:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4437334
31 A = 6783126
22 meter
Y = 2390544
90 meter E =
0012997
Z = 4534821
89 I = 51
25756
XDOT = -618
592124 Wp = 51
22312
YDOT = 7000
242400 meter/sec RA = 254
52448 deg
ZDOT = -3070
930321 TA = 69
73630
MA = 69
59663
Ha = 223
655 n
mi
Hp = 215
069
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14558183
43 X = 4388245
39
Y = 7842995
07 feet Y = 2439891
86 meter
Z = 14878024
59 Z = 4556257
28
XDOT = -2029
501718 XDOT = -681
908138
YDOT = 22966
674542 feet/sec YDOT = 6992
970803 meter/sec
ZDOT = -10075
230711 ZDOT = -3074
089061
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16247753
50 X = 4952315
27
Y = 2565944
10 feet Y = 782099
76 meter
Z = 14974489
28 Z = 4564224
33
XDOT = 6006
323713 XDOT = 1830
727468
YDOT = 21118
165531 feet/sec YDOT = 6436
816854 meter/sec
ZDOT = -10090
172010 ZDOT = -3075
484429
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
70112389
00016717 00000-0 10270-3 0 9118
2 25544 51
6374 255
2972 0005210 24
9586 335
1817 15
53224674 36064
Satellite: ISS
Catalog Number: 25544
Epoch time: 19044
70112389 = yrday
fracday
Element set: 911
Inclination: 51
6374 deg
RA of node: 255
2972 deg
Eccentricity:
0005210
Arg of perigee: 24
9586 deg
Mean anomaly: 335
1817 deg
Mean motion: 15
53224674 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3606
Checksum: 306
Coasting Arc #13 (Orbit 3620)
---------------------------------------
Vector Time (GMT): 2019/045/15:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4467759
35 A = 6786095
79 meter
Y = -3560322
29 meter E =
0008803
Z = -3666307
06 I = 51
27822
XDOT = 1388
241384 Wp = 66
04526
YDOT = -6175
603226 meter/sec RA = 249
51848 deg
ZDOT = 4317
119474 TA = 250
14443
MA = 250
23933
Ha = 223
718 n
mi
Hp = 214
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14658003
13 X = -4409806
14
Y = -11680847
42 feet Y = -3609959
86 meter
Z = -12028566
46 Z = -3687868
70
XDOT = 4554
597716 XDOT = 1436
225674
YDOT = -20261
165438 feet/sec YDOT = -6159
810646 meter/sec
ZDOT = 14163
777803 ZDOT = 4323
979477
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17744316
12 X = -5408467
55
Y = -5839276
55 feet Y = -1779811
49 meter
Z = -12125500
32 Z = -3695852
50
XDOT = -3340
912667 XDOT = -1018
310181
YDOT = -19245
457260 feet/sec YDOT = -5866
015373 meter/sec
ZDOT = 14195
325658 ZDOT = 4326
735261
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
66619744
00016717 00000-0 10270-3 0 9122
2 25544 51
6379 250
4936 0005260 27
9732 332
1702 15
53251022 36211
Satellite: ISS
Catalog Number: 25544
Epoch time: 19045
66619744 = yrday
fracday
Element set: 912
Inclination: 51
6379 deg
RA of node: 250
4936 deg
Eccentricity:
0005260
Arg of perigee: 27
9732 deg
Mean anomaly: 332
1702 deg
Mean motion: 15
53251022 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3621
Checksum: 297
Coasting Arc #14 (Orbit 3636)
---------------------------------------
Vector Time (GMT): 2019/046/15:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4377529
90 A = 6789201
78 meter
Y = 4545329
22 meter E =
0015952
Z = 2491822
83 I = 51
30059
XDOT = -2258
985201 Wp = 86
48581
YDOT = 5084
472843 meter/sec RA = 244
51919 deg
ZDOT = -5275
817021 TA = 65
44111
MA = 65
27493
Ha = 223
775 n
mi
Hp = 214
865
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14361974
74 X = 4314273
73
Y = 14912497
45 feet Y = 4593928
10 meter
Z = 8175271
75 Z = 2512933
25
XDOT = -7411
368769 XDOT = -2290
046794
YDOT = 16681
341348 feet/sec YDOT = 5059
037668 meter/sec
ZDOT = -17309
110962 ZDOT = -5286
865520
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18773782
24 X = 5722248
83
Y = 8639132
44 feet Y = 2633207
57 meter
Z = 8270094
18 Z = 2520724
71
XDOT = -51
602109 XDOT = -15
728323
YDOT = 16824
014713 feet/sec YDOT = 5127
959685 meter/sec
ZDOT = -17359
444531 ZDOT = -5291
158693
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
69560899
00016717 00000-0 10270-3 0 9133
2 25544 51
6373 245
3681 0005165 31
1858 328
9600 15
53248252 36373
Satellite: ISS
Catalog Number: 25544
Epoch time: 19046
69560899 = yrday
fracday
Element set: 913
Inclination: 51
6373 deg
RA of node: 245
3681 deg
Eccentricity:
0005165
Arg of perigee: 31
1858 deg
Mean anomaly: 328
9600 deg
Mean motion: 15
53248252 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3637
Checksum: 330
Coasting Arc #15 (Orbit 3651)
---------------------------------------
Vector Time (GMT): 2019/047/15:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4168488
74 A = 6791237
74 meter
Y = -5221653
52 meter E =
0014445
Z = -1180138
68 I = 51
32417
XDOT = 3165
074823 Wp = 36
84611
YDOT = -3835
084751 meter/sec RA = 239
52729 deg
ZDOT = 5837
608568 TA = 310
28051
MA = 310
40671
Ha = 223
829 n
mi
Hp = 214
761
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13676144
17 X = -4104056
61
Y = -17131409
20 feet Y = -5267908
20 meter
Z = -3871846
05 Z = -1200230
72
XDOT = 10384
103749 XDOT = 3179
369381
YDOT = -12582
299053 feet/sec YDOT = -3799
610796 meter/sec
ZDOT = 19152
259081 ZDOT = 5853
017650
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19160140
62 X = -5840010
86
Y = -10616242
29 feet Y = -3235830
65 meter
Z = -3962032
76 Z = -1207627
59
XDOT = 3896
364525 XDOT = 1187
611907
YDOT = -14147
858159 feet/sec YDOT = -4312
267167 meter/sec
ZDOT = 19222
148651 ZDOT = 5858
910909
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
66067990
00016717 00000-0 10270-3 0 9146
2 25544 51
6387 240
5636 0005298 34
2830 325
8664 15
53259027 36521
Satellite: ISS
Catalog Number: 25544
Epoch time: 19047
66067990 = yrday
fracday
Element set: 914
Inclination: 51
6387 deg
RA of node: 240
5636 deg
Eccentricity:
0005298
Arg of perigee: 34
2830 deg
Mean anomaly: 325
8664 deg
Mean motion: 15
53259027 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3652
Checksum: 331
Coasting Arc #16 (Orbit 3667)
---------------------------------------
Vector Time (GMT): 2019/048/15:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3759549
78 A = 6791781
66 meter
Y = 5646996
15 meter E =
0012033
Z = -267296
10 I = 51
34308
XDOT = -4113
562523 Wp = 110
70044
YDOT = 2466
270596 meter/sec RA = 234
53976 deg
ZDOT = -5977
303401 TA = 72
18945
MA = 72
05820
Ha = 223
933 n
mi
Hp = 214
638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12334480
90 X = 3697422
40
Y = 18526890
26 feet Y = 5688690
68 meter
Z = -876955
71 Z = -249185
06
XDOT = -13495
940037 XDOT = -4111
801717
YDOT = 8091
438964 feet/sec YDOT = 2420
279669 meter/sec
ZDOT = -19610
575464 ZDOT = -5997
280734
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18693398
13 X = 5697747
75
Y = 12086265
98 feet Y = 3683893
87 meter
Z = -795722
35 Z = -242536
17
XDOT = -8160
115314 XDOT = -2487
203148
YDOT = 11376
978257 feet/sec YDOT = 3467
702973 meter/sec
ZDOT = -19700
957834 ZDOT = -6004
851948
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
69008663
00016717 00000-0 10270-3 0 9153
2 25544 51
6378 235
4383 0005348 37
9934 322
1595 15
53275232 36680
Satellite: ISS
Catalog Number: 25544
Epoch time: 19048
69008663 = yrday
fracday
Element set: 915
Inclination: 51
6378 deg
RA of node: 235
4383 deg
Eccentricity:
0005348
Arg of perigee: 37
9934 deg
Mean anomaly: 322
1595 deg
Mean motion: 15
53275232 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3668
Checksum: 337
Coasting Arc #17 (Orbit 3683)
---------------------------------------
Vector Time (GMT): 2019/049/15:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3178119
28 A = 6790692
67 meter
Y = -5758723
51 meter E =
0018993
Z = 1647893
27 I = 51
36000
XDOT = 5018
092978 Wp = 57
92863
YDOT = -1129
248608 meter/sec RA = 229
55291 deg
ZDOT = 5693
272581 TA = 320
19913
MA = 320
33830
Ha = 223
974 n
mi
Hp = 214
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10426900
52 X = -3121491
71
Y = -18893449
83 feet Y = -5793946
78 meter
Z = 5406473
99 Z = 1632593
37
XDOT = 16463
559640 XDOT = 5002
693696
YDOT = -3704
883886 feet/sec YDOT = -1073
218693 meter/sec
ZDOT = 18678
715817 ZDOT = 5717
610485
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17340927
66 X = -5285514
75
Y = -12872900
83 feet Y = -3923660
17 meter
Z = 5337912
92 Z = 1626995
86
XDOT = 12404
188425 XDOT = 3780
796632
YDOT = -8865
755488 feet/sec YDOT = -2702
282273 meter/sec
ZDOT = 18788
667960 ZDOT = 5726
785994
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
71949236
00016717 00000-0 10270-3 0 9168
2 25544 51
6383 230
3135 0005333 42
5697 317
5868 15
53276391 36843
Satellite: ISS
Catalog Number: 25544
Epoch time: 19049
71949236 = yrday
fracday
Element set: 916
Inclination: 51
6383 deg
RA of node: 230
3135 deg
Eccentricity:
0005333
Arg of perigee: 42
5697 deg
Mean anomaly: 317
5868 deg
Mean motion: 15
53276391 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3684
Checksum: 335
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