[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 9th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15282 6 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
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 3525)
---------------------------------------
Vector Time (GMT): 2019/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916020
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4179173
40 A = 6783390
16 meter
Y = -2919224
59 meter E =
0008924
Z = 4466444
86 I = 51
25561
XDOT = 1355
391014 Wp = 76
09470
YDOT = 6840
235079 meter/sec RA = 280
39300 deg
ZDOT = 3199
213260 TA = 341
56931
MA = 341
60163
Ha = 223
260 n
mi
Hp = 215
690
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13711198
81 X = 4189811
36
Y = -9577508
49 feet Y = -2872430
42 meter
Z = 14653690
50 Z = 4486771
27
XDOT = 4446
820912 XDOT = 1263
261185
YDOT = 22441
716137 feet/sec YDOT = 6854
877061 meter/sec
ZDOT = 10496
106496 ZDOT = 3205
572939
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16503370
34 X = 5030227
28
Y = 2158570
89 feet Y = 657932
41 meter
Z = 14745698
56 Z = 4494488
92
XDOT = -11804
147628 XDOT = -3597
904197
YDOT = 18283
446288 feet/sec YDOT = 5572
794429 meter/sec
ZDOT = 10524
039876 ZDOT = 3207
727354
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
55403633
00016717 00000-0 10270-3 0 9008
2 25544 51
6404 280
9282 0005479 3
8234 356
2959 15
53222475 35269
Satellite: ISS
Catalog Number: 25544
Epoch time: 19039
55403633 = yrday
fracday
Element set: 900
Inclination: 51
6404 deg
RA of node: 280
9282 deg
Eccentricity:
0005479
Arg of perigee: 3
8234 deg
Mean anomaly: 356
2959 deg
Mean motion: 15
53222475 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3526
Checksum: 311
Coasting Arc #2 (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 = -2553247
34 A = 6784690
92 meter
Y = -4756832
84 meter E =
0007971
Z = -4113899
33 I = 51
25476
XDOT = 3958
420827 Wp = 70
83315
YDOT = -5372
528629 meter/sec RA = 279
47124 deg
ZDOT = 3763
977711 TA = 238
17020
MA = 238
24783
Ha = 223
238 n
mi
Hp = 215
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8376795
74 X = -2479882
73
Y = -15606406
94 feet Y = -4784975
06 meter
Z = -13497045
06 Z = -4126123
32
XDOT = 12986
944969 XDOT = 3999
920844
YDOT = -17626
406263 feet/sec YDOT = -5328
030542 meter/sec
ZDOT = 12349
008239 ZDOT = 3783
306927
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13143975
44 X = -4006283
71
Y = -11810555
78 feet Y = -3599857
40 meter
Z = -13551662
32 Z = -4130546
67
XDOT = 5202
086957 XDOT = 1585
596105
YDOT = -20027
506730 feet/sec YDOT = -6104
384051 meter/sec
ZDOT = 12436
785615 ZDOT = 3790
732256
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
68271360
00016717 00000-0 10270-3 0 9013
2 25544 51
6362 280
2830 0005101 4
5817 355
5381 15
53239583 35282
Satellite: ISS
Catalog Number: 25544
Epoch time: 19039
68271360 = yrday
fracday
Element set: 901
Inclination: 51
6362 deg
RA of node: 280
2830 deg
Eccentricity:
0005101
Arg of perigee: 4
5817 deg
Mean anomaly: 355
5381 deg
Mean motion: 15
53239583 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3528
Checksum: 299
Coasting Arc #3 (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 = 3835215
81 A = 6780883
95 meter
Y = 2413064
51 meter E =
0009839
Z = 5042744
13 I = 51
24358
XDOT = -2129
411353 Wp = 29
77425
YDOT = 7146
222685 meter/sec RA = 275
48079 deg
ZDOT = -1790
211034 TA = 77
70007
MA = 77
58993
Ha = 223
217 n
mi
Hp = 215
550
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12582729
03 X = 3783452
81
Y = 7916878
31 feet Y = 2455663
46 meter
Z = 16544436
12 Z = 5061247
95
XDOT = -6986
257720 XDOT = -2200
468482
YDOT = 23445
612485 feet/sec YDOT = 7122
012706 meter/sec
ZDOT = -5873
395781 ZDOT = -1800
727742
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1697208
72 X = 517309
22
Y = 14675197
45 feet Y = 4473000
18 meter
Z = 16627641
47 Z = 5068105
12
XDOT = -21520
785990 XDOT = -6559
535570
YDOT = 9234
996120 feet/sec YDOT = 2814
826817 meter/sec
ZDOT = -5921
601931 ZDOT = -1804
904268
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
51911781
00016717 00000-0 10270-3 0 9026
2 25544 51
6410 276
1236 0005471 4
5559 355
5642 15
53286957 35415
Satellite: ISS
Catalog Number: 25544
Epoch time: 19040
51911781 = yrday
fracday
Element set: 902
Inclination: 51
6410 deg
RA of node: 276
1236 deg
Eccentricity:
0005471
Arg of perigee: 4
5559 deg
Mean anomaly: 355
5642 deg
Mean motion: 15
53286957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3541
Checksum: 305
Coasting Arc #4 (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 = -3545275
63 A = 6783391
02 meter
Y = -3696761
75 meter E =
0009906
Z = -4454580
49 I = 51
24930
XDOT = 2645
987308 Wp = 77
24783
YDOT = -6421
531017 meter/sec RA = 270
46668 deg
ZDOT = 3231
472318 TA = 225
45775
MA = 225
53870
Ha = 223
430 n
mi
Hp = 215
365
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11631481
72 X = -3482036
36
Y = -12128483
45 feet Y = -3736054
17 meter
Z = -14614765
40 Z = -4471648
04
XDOT = 8681
060723 XDOT = 2701
901568
YDOT = -21068
015148 feet/sec YDOT = -6391
628914 meter/sec
ZDOT = 10601
943299 ZDOT = 3244
461514
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1880168
98 X = 573075
50
Y = -16631646
27 feet Y = -5069325
78 meter
Z = -14691363
19 Z = -4477927
50
XDOT = 20460
907791 XDOT = 6236
484695
YDOT = -7080
615219 feet/sec YDOT = -2158
171519 meter/sec
ZDOT = 10661
208898 ZDOT = 3249
536472
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
48420048
00016717 00000-0 10270-3 0 9035
2 25544 51
6407 271
3186 0005548 8
6783 351
4465 15
53252787 35569
Satellite: ISS
Catalog Number: 25544
Epoch time: 19041
48420048 = yrday
fracday
Element set: 903
Inclination: 51
6407 deg
RA of node: 271
3186 deg
Eccentricity:
0005548
Arg of perigee: 8
6783 deg
Mean anomaly: 351
4465 deg
Mean motion: 15
53252787 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3556
Checksum: 318
Coasting Arc #5 (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 = 3212282
34 A = 6786510
79 meter
Y = 4831671
20 meter E =
0014675
Z = 3514555
43 I = 51
26019
XDOT = -3167
111939 Wp = 65
87812
YDOT = 5368
453918 meter/sec RA = 265
45942 deg
ZDOT = -4464
913604 TA = 72
49794
MA = 72
33762
Ha = 223
545 n
mi
Hp = 215
234
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10538984
05 X = 3140942
94
Y = 15851939
65 feet Y = 4867194
48 meter
Z = 11530693
67 Z = 3529985
79
XDOT = -10390
787201 XDOT = -3205
220324
YDOT = 17613
037788 feet/sec YDOT = 5332
823764 meter/sec
ZDOT = -14648
666681 ZDOT = -4480
390873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5107579
70 X = -1556790
29
Y = 18293943
41 feet Y = 5575993
95 meter
Z = 11599798
97 Z = 3535618
73
XDOT = -18711
915750 XDOT = -5703
391921
YDOT = 4151
560802 feet/sec YDOT = 1265
395733 meter/sec
ZDOT = -14719
034069 ZDOT = -4486
361584
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
51361975
00016717 00000-0 10270-3 0 9044
2 25544 51
6402 266
1935 0005679 12
9127 347
2170 15
53277885 35723
Satellite: ISS
Catalog Number: 25544
Epoch time: 19042
51361975 = yrday
fracday
Element set: 904
Inclination: 51
6402 deg
RA of node: 266
1935 deg
Eccentricity:
0005679
Arg of perigee: 12
9127 deg
Mean anomaly: 347
2170 deg
Mean motion: 15
53277885 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3572
Checksum: 321
Coasting Arc #6 (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 = -2871501
30 A = 6789531
63 meter
Y = -5677941
61 meter E =
0010827
Z = -2357721
06 I = 51
27331
XDOT = 3671
904050 Wp = 30
60493
YDOT = -4073
320818 meter/sec RA = 260
45949 deg
ZDOT = 5357
478722 TA = 302
94702
MA = 303
05109
Ha = 223
611 n
mi
Hp = 215
253
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9420936
04 X = -2796343
17
Y = -18628417
36 feet Y = -5709632
59 meter
Z = -7735305
33 Z = -2371486
84
XDOT = 12046
929298 XDOT = 3691
156809
YDOT = -13363
913444 feet/sec YDOT = -4032
151187 meter/sec
ZDOT = 17577
029927 ZDOT = 5375
362156
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7587049
64 X = 2312532
73
Y = -19423003
41 feet Y = -5920131
44 meter
Z = -7796828
45 Z = -2376473
31
XDOT = 16496
259302 XDOT = 5028
059835
YDOT = -618
382670 feet/sec YDOT = -188
483038 meter/sec
ZDOT = 17658
112454 ZDOT = 5382
192676
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
47870046
00016717 00000-0 10270-3 0 9055
2 25544 51
6398 261
3890 0005608 14
8005 345
3311 15
53234703 35876
Satellite: ISS
Catalog Number: 25544
Epoch time: 19043
47870046 = yrday
fracday
Element set: 905
Inclination: 51
6398 deg
RA of node: 261
3890 deg
Eccentricity:
0005608
Arg of perigee: 14
8005 deg
Mean anomaly: 345
3311 deg
Mean motion: 15
53234703 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3587
Checksum: 305
Coasting Arc #7 (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 = 2440085
77 A = 6791498
02 meter
Y = 6257042
17 meter E =
0013296
Z = 987757
78 I = 51
28707
XDOT = -4196
699692 Wp = 100
30075
YDOT = 2574
267143 meter/sec RA = 255
46550 deg
ZDOT = -5874
371949 TA = 68
95169
MA = 68
80954
Ha = 223
754 n
mi
Hp = 215
114
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8005530
75 X = 2365138
49
Y = 20528353
57 feet Y = 6283909
87 meter
Z = 3240675
14 Z = 999428
52
XDOT = -13768
699778 XDOT = -4196
639863
YDOT = 8445
758343 feet/sec YDOT = 2527
336945 meter/sec
ZDOT = -19272
873849 ZDOT = -5894
757608
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9586156
48 X = -2921860
49
Y = 19830973
31 feet Y = 6044480
66 meter
Z = 3292704
05 Z = 1003616
20
XDOT = -14028
193150 XDOT = -4275
793272
YDOT = -3530
754290 feet/sec YDOT = -1076
173908 meter/sec
ZDOT = -19365
092831 ZDOT = -5902
480295
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
50811810
00016717 00000-0 10270-3 0 9065
2 25544 51
6404 256
2635 0005574 19
7641 340
3726 15
53235945 36039
Satellite: ISS
Catalog Number: 25544
Epoch time: 19044
50811810 = yrday
fracday
Element set: 906
Inclination: 51
6404 deg
RA of node: 256
2635 deg
Eccentricity:
0005574
Arg of perigee: 19
7641 deg
Mean anomaly: 340
3726 deg
Mean motion: 15
53235945 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3603
Checksum: 298
Coasting Arc #8 (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 = 4437959
36 A = 6783127
41 meter
Y = 2383701
67 meter E =
0012969
Z = 4537808
71 I = 51
25739
XDOT = -613
058201 Wp = 51
22774
YDOT = 7003
210397 meter/sec RA = 254
52432 deg
ZDOT = -3065
274811 TA = 69
66847
MA = 69
52916
Ha = 223
655 n
mi
Hp = 215
079
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14560234
11 X = 4388932
40
Y = 7820543
52 feet Y = 2433055
97 meter
Z = 14887823
86 Z = 4559247
29
XDOT = -2011
345805 XDOT = -676
435287
YDOT = 22976
412064 feet/sec YDOT = 6996
000342 meter/sec
ZDOT = -10056
675889 ZDOT = -3068
406818
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16242127
99 X = 4950600
61
Y = 2544118
98 feet Y = 775447
46 meter
Z = 14984303
61 Z = 4567215
74
XDOT = 6024
980633 XDOT = 1836
414097
YDOT = 21121
734623 feet/sec YDOT = 6437
904713 meter/sec
ZDOT = -10071
496881 ZDOT = -3069
792249
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
70113525
00016717 00000-0 10270-3 0 9076
2 25544 51
6373 255
2972 0005188 25
0253 335
1149 15
53220270 36066
Satellite: ISS
Catalog Number: 25544
Epoch time: 19044
70113525 = yrday
fracday
Element set: 907
Inclination: 51
6373 deg
RA of node: 255
2972 deg
Eccentricity:
0005188
Arg of perigee: 25
0253 deg
Mean anomaly: 335
1149 deg
Mean motion: 15
53220270 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3606
Checksum: 286
Coasting Arc #9 (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 = -4469496
88 A = 6786093
86 meter
Y = -3552729
73 meter E =
0008796
Z = -3671608
15 I = 51
27803
XDOT = 1381
227436 Wp = 66
31930
YDOT = -6181
164494 meter/sec RA = 249
51831 deg
ZDOT = 4311
342309 TA = 249
79097
MA = 249
88558
Ha = 223
720 n
mi
Hp = 214
881
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14663703
67 X = -4411602
69
Y = -11655937
44 feet Y = -3602387
06 meter
Z = -12045958
51 Z = -3693178
37
XDOT = 4531
586075 XDOT = 1429
302497
YDOT = -20279
411070 feet/sec YDOT = -6165
449842 meter/sec
ZDOT = 14144
823847 ZDOT = 4318
168461
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17740826
83 X = -5407404
02
Y = -5813989
12 feet Y = -1772103
88 meter
Z = -12142931
83 Z = -3701165
62
XDOT = -3366
892828 XDOT = -1026
228934
YDOT = -19254
792638 feet/sec YDOT = -5868
860796 meter/sec
ZDOT = 14176
219520 ZDOT = 4320
911710
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
66621171
00016717 00000-0 10270-3 0 9084
2 25544 51
6378 250
4935 0005238 28
0405 332
1028 15
53245992 36213
Satellite: ISS
Catalog Number: 25544
Epoch time: 19045
66621171 = yrday
fracday
Element set: 908
Inclination: 51
6378 deg
RA of node: 250
4935 deg
Eccentricity:
0005238
Arg of perigee: 28
0405 deg
Mean anomaly: 332
1028 deg
Mean motion: 15
53245992 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3621
Checksum: 301
Coasting Arc #10 (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 = 4381004
03 A = 6789201
15 meter
Y = 4537530
97 meter E =
0015948
Z = 2499883
58 I = 51
30040
XDOT = -2250
434176 Wp = 86
46117
YDOT = 5093
348607 meter/sec RA = 244
51900 deg
ZDOT = -5270
927325 TA = 65
36671
MA = 65
20067
Ha = 223
778 n
mi
Hp = 214
878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14373372
81 X = 4317795
65
Y = 14886912
63 feet Y = 4586168
97 meter
Z = 8201717
79 Z = 2521011
00
XDOT = -7383
314226 XDOT = -2281
619407
YDOT = 16710
461309 feet/sec YDOT = 5068
008365 meter/sec
ZDOT = -17293
068651 ZDOT = -5281
934587
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18774857
05 X = 5722576
43
Y = 8611217
51 feet Y = 2624699
10 meter
Z = 8296617
62 Z = 2528809
05
XDOT = -16
969274 XDOT = -5
172235
YDOT = 16840
802842 feet/sec YDOT = 5133
076706 meter/sec
ZDOT = -17343
216996 ZDOT = -5286
212540
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
69562680
00016717 00000-0 10270-3 0 9098
2 25544 51
6372 245
3680 0005143 31
2656 328
8802 15
53242525 36374
Satellite: ISS
Catalog Number: 25544
Epoch time: 19046
69562680 = yrday
fracday
Element set: 909
Inclination: 51
6372 deg
RA of node: 245
3680 deg
Eccentricity:
0005143
Arg of perigee: 31
2656 deg
Mean anomaly: 328
8802 deg
Mean motion: 15
53242525 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3637
Checksum: 316
Coasting Arc #11 (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 = -4174396
05 A = 6791244
79 meter
Y = -5214531
55 meter E =
0014392
Z = -1190974
21 I = 51
32400
XDOT = 3155
163071 Wp = 36
85856
YDOT = -3847
471762 meter/sec RA = 239
52708 deg
ZDOT = 5834
756719 TA = 310
14787
MA = 310
27384
Ha = 223
832 n
mi
Hp = 214
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13695525
08 X = -4109990
48
Y = -17108043
15 feet Y = -5260852
44 meter
Z = -3907395
70 Z = -1211095
01
XDOT = 10351
584878 XDOT = 3169
610734
YDOT = -12622
938851 feet/sec YDOT = -3812
107791 meter/sec
ZDOT = 19142
902623 ZDOT = 5850
118027
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19168903
80 X = -5842681
88
Y = -10587337
14 feet Y = -3227020
36 meter
Z = -3997712
85 Z = -1218502
88
XDOT = 3852
950908 XDOT = 1174
379437
YDOT = -14172
374894 feet/sec YDOT = -4319
739868 meter/sec
ZDOT = 19212
577745 ZDOT = 5855
993697
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
66070141
00016717 00000-0 10270-3 0 9104
2 25544 51
6386 240
5636 0005276 34
3616 325
7877 15
53252744 36523
Satellite: ISS
Catalog Number: 25544
Epoch time: 19047
66070141 = yrday
fracday
Element set: 910
Inclination: 51
6386 deg
RA of node: 240
5636 deg
Eccentricity:
0005276
Arg of perigee: 34
3616 deg
Mean anomaly: 325
7877 deg
Mean motion: 15
53252744 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3652
Checksum: 311
Coasting Arc #12 (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 = 3768722
81 A = 6791804
90 meter
Y = 5641475
66 meter E =
0012070
Z = -253981
09 I = 51
34296
XDOT = -4102
876418 Wp = 110
78033
YDOT = 2482
326879 meter/sec RA = 234
53955 deg
ZDOT = -5978
039744 TA = 71
96550
MA = 71
83402
Ha = 223
938 n
mi
Hp = 214
653
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12364576
14 X = 3706591
80
Y = 18508778
42 feet Y = 5683272
75 meter
Z = -833271
29 Z = -235825
50
XDOT = -13460
880637 XDOT = -4101
292375
YDOT = 8144
117058 feet/sec YDOT = 2436
454463 meter/sec
ZDOT = -19612
991287 ZDOT = -5997
965599
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18713533
20 X = 5703884
92
Y = 12057793
33 feet Y = 3675215
41 meter
Z = -751836
38 Z = -229159
73
XDOT = -8109
051175 XDOT = -2471
638798
YDOT = 11409
880084 feet/sec YDOT = 3477
731450 meter/sec
ZDOT = -19703
142763 ZDOT = -6005
517914
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
69011254
00016717 00000-0 10270-3 0 9119
2 25544 51
6378 235
4383 0005325 38
0811 322
0717 15
53268187 36687
Satellite: ISS
Catalog Number: 25544
Epoch time: 19048
69011254 = yrday
fracday
Element set: 911
Inclination: 51
6378 deg
RA of node: 235
4383 deg
Eccentricity:
0005325
Arg of perigee: 38
0811 deg
Mean anomaly: 322
0717 deg
Mean motion: 15
53268187 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3668
Checksum: 310
Coasting Arc #13 (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 = -3191344
76 A = 6790736
21 meter
Y = -5755750
98 meter E =
0018976
Z = 1632910
18 I = 51
35994
XDOT = 5007
353029 Wp = 57
83016
YDOT = -1148
659009 meter/sec RA = 229
55275 deg
ZDOT = 5698
779949 TA = 320
12698
MA = 320
26623
Ha = 223
980 n
mi
Hp = 214
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10470291
20 X = -3134676
67
Y = -18883697
45 feet Y = -5791121
92 meter
Z = 5357316
86 Z = 1617546
13
XDOT = 16428
323587 XDOT = 4992
144847
YDOT = -3768
566301 feet/sec YDOT = -1092
748126 meter/sec
ZDOT = 18696
784611 ZDOT = 5723
066150
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17376099
06 X = -5296234
99
Y = -12846212
66 feet Y = -3915525
62 meter
Z = 5288466
00 Z = 1611924
44
XDOT = 12347
603121 XDOT = 3763
549431
YDOT = -8906
543024 feet/sec YDOT = -2714
714314 meter/sec
ZDOT = 18806
505056 ZDOT = 5732
222741
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
71952313
00016717 00000-0 10270-3 0 9124
2 25544 51
6382 230
3135 0005311 42
6646 317
4917 15
53268545 36849
Satellite: ISS
Catalog Number: 25544
Epoch time: 19049
71952313 = yrday
fracday
Element set: 912
Inclination: 51
6382 deg
RA of node: 230
3135 deg
Eccentricity:
0005311
Arg of perigee: 42
6646 deg
Mean anomaly: 317
4917 deg
Mean motion: 15
53268545 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3684
Checksum: 307
Coasting Arc #14 (Orbit 3698)
---------------------------------------
Vector Time (GMT): 2019/050/15:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2380414
27 A = 6788216
12 meter
Y = 5641345
37 meter E =
0008162
Z = -2939905
58 I = 51
37470
XDOT = -5814
089683 Wp = 77
39976
YDOT = -138
165621 meter/sec RA = 224
56300 deg
ZDOT = -4982
731662 TA = 136
24429
MA = 136
17958
Ha = 224
033 n
mi
Hp = 214
538
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7809758
11 X = 2331434
23
Y = 18508350
95 feet Y = 5667690
76 meter
Z = -9645359
51 Z = -2928462
11
XDOT = -19075
097384 XDOT = -5787
909961
YDOT = -453
299280 feet/sec YDOT = -203
036787 meter/sec
ZDOT = -16347
544822 ZDOT = -5010
909871
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15056264
65 X = 4589149
47
Y = 13335856
51 feet Y = 4064769
06 meter
Z = -9594173
37 Z = -2924304
04
XDOT = -16351
772476 XDOT = -4984
020251
YDOT = 6632
598413 feet/sec YDOT = 2021
615996 meter/sec
ZDOT = -16474
734766 ZDOT = -5021
499157
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
68459463
00016717 00000-0 10270-3 0 9131
2 25544 51
6390 225
5086 0005306 45
6080 314
5506 15
53265985 36991
Satellite: ISS
Catalog Number: 25544
Epoch time: 19050
68459463 = yrday
fracday
Element set: 913
Inclination: 51
6390 deg
RA of node: 225
5086 deg
Eccentricity:
0005306
Arg of perigee: 45
6080 deg
Mean anomaly: 314
5506 deg
Mean motion: 15
53265985 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3699
Checksum: 326
Coasting Arc #15 (Orbit 3714)
---------------------------------------
Vector Time (GMT): 2019/051/15:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1397415
33 A = 6784996
74 meter
Y = -5292989
93 meter E =
0014815
Z = 3994615
64 I = 51
38966
XDOT = 6466
243698 Wp = 84
70884
YDOT = 1269
272217 meter/sec RA = 219
56823 deg
ZDOT = 3932
624994 TA = 324
25940
MA = 324
35847
Ha = 224
037 n
mi
Hp = 214
395
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4584695
98 X = -1357526
86
Y = -17365452
51 feet Y = -5308393
39 meter
Z = 13105694
36 Z = 3987925
09
XDOT = 21214
710294 XDOT = 6432
467771
YDOT = 4164
278926 feet/sec YDOT = 1341
393791 meter/sec
ZDOT = 12902
312974 ZDOT = 3963
952565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11907266
66 X = -3629334
88
Y = -13474975
77 feet Y = -4107172
62 meter
Z = 13075918
00 Z = 3985539
81
XDOT = 19793
329712 XDOT = 6033
006896
YDOT = -4797
267138 feet/sec YDOT = -1462
207024 meter/sec
ZDOT = 13043
641136 ZDOT = 3975
701818
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
71400033
00016717 00000-0 10270-3 0 9146
2 25544 51
6399 220
3834 0005348 49
0512 311
1102 15
53300226 37150
Satellite: ISS
Catalog Number: 25544
Epoch time: 19051
71400033 = yrday
fracday
Element set: 914
Inclination: 51
6399 deg
RA of node: 220
3834 deg
Eccentricity:
0005348
Arg of perigee: 49
0512 deg
Mean anomaly: 311
1102 deg
Mean motion: 15
53300226 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3715
Checksum: 260
Coasting Arc #16 (Orbit 3729)
---------------------------------------
Vector Time (GMT): 2019/052/15:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 232466
70 A = 6782181
87 meter
Y = 4807131
26 meter E =
0016436
Z = -4794449
27 I = 51
40623
XDOT = -6854
903487 Wp = 65
64379
YDOT = -2231
927945 meter/sec RA = 214
56888 deg
ZDOT = -2570
542906 TA = 178
90880
MA = 178
90521
Ha = 224
135 n
mi
Hp = 214
394
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 762686
03 X = 201982
98
Y = 15771428
02 feet Y = 4809559
89 meter
Z = -15729820
43 Z = -4793394
62
XDOT = -22489
840838 XDOT = -6816
949981
YDOT = -7322
598245 feet/sec YDOT = -2308
372336 meter/sec
ZDOT = -8433
539719 ZDOT = -2603
748283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8026011
88 X = 2446328
42
Y = 13602963
57 feet Y = 4146183
29 meter
Z = -15725437
92 Z = -4793113
48
XDOT = -22295
049076 XDOT = -6795
530958
YDOT = 3233
263584 feet/sec YDOT = 985
498741 meter/sec
ZDOT = -8583
284576 ZDOT = -2616
185139
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
67907019
00016717 00000-0 10270-3 0 9159
2 25544 51
6400 215
5796 0005345 51
8617 308
3016 15
53251840 37306
Satellite: ISS
Catalog Number: 25544
Epoch time: 19052
67907019 = yrday
fracday
Element set: 915
Inclination: 51
6400 deg
RA of node: 215
5796 deg
Eccentricity:
0005345
Arg of perigee: 51
8617 deg
Mean anomaly: 308
3016 deg
Mean motion: 15
53251840 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3730
Checksum: 299
Coasting Arc #17 (Orbit 3745)
---------------------------------------
Vector Time (GMT): 2019/053/15:48:00
000
Vector Time (MET): N/A
Weight (LBS) : 900744
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1031736
33 A = 6780147
52 meter
Y = -4197725
54 meter E =
0007637
Z = 5216792
55 I = 51
42867
XDOT = 6982
192037 Wp = 82
92822
YDOT = 3008
031767 meter/sec RA = 209
56492 deg
ZDOT = 1039
163391 TA = 357
09467
MA = 357
09910
Ha = 224
051 n
mi
Hp = 214
280
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3384961
72 X = 1053259
96
Y = -13772065
41 feet Y = -4186067
02 meter
Z = 17115461
11 Z = 5221856
98
XDOT = 22907
454188 XDOT = 6942
988857
YDOT = 9868
870627 feet/sec YDOT = 3085
892433 meter/sec
ZDOT = 3409
328712 ZDOT = 1072
984125
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3667502
59 X = -1117854
79
Y = -13670506
29 feet Y = -4166770
32 meter
Z = 17138653
48 Z = 5223861
58
XDOT = 23827
997270 XDOT = 7262
773568
YDOT = -1925
532298 feet/sec YDOT = -586
902244 meter/sec
ZDOT = 3561
808228 ZDOT = 1085
639148
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
70847448
00016717 00000-0 10270-3 0 9164
2 25544 51
6407 210
4544 0005364 55
3856 304
7801 15
53299068 37466
Satellite: ISS
Catalog Number: 25544
Epoch time: 19053
70847448 = yrday
fracday
Element set: 916
Inclination: 51
6407 deg
RA of node: 210
4544 deg
Eccentricity:
0005364
Arg of perigee: 55
3856 deg
Mean anomaly: 304
7801 deg
Mean motion: 15
53299068 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3746
Checksum: 324
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