[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 24th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15204 0235 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 584 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
297/21:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
2
000/00:00:00
000 0
0 0
0 220
7
301/10:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
8
000/00:00:00
000 0
0 0
0 221
1
304/19:44:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
3
000/00:00:00
000 0
0 0
0 221
8
305/15:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
2
000/00:00:00
000 0
0 0
0 221
9
306/13:59:43
634 0
0 0
0 0
0
N/A 0
0 0
0 227
1
000/00:00:00
000 0
0 0
0 222
1
308/07:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 226
7
000/00:00:00
000 0
0 0
0 222
3
308/09:10:00
000 0
0 0
0 0
0
N/A 0
0 0
0 226
7
000/00:00:00
000 0
0 0
0 222
2
Coasting Arc #1 (Orbit 3515)
---------------------------------------
Vector Time (GMT): 2019/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4181269
78 A = 6788889
83 meter
Y = 146877
47 meter E =
0006852
Z = 5344110
73 I = 52
00493
XDOT = -582
670275 Wp = 159
15471
YDOT = -7638
217872 meter/sec RA = 84
16474 deg
ZDOT = -252
085311 TA = 293
20114
MA = 293
27330
Ha = 228
659 n
mi
Hp = 220
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13718076
71 X = -4208560
43
Y = 481881
47 feet Y = 99967
16 meter
Z = 17533171
67 Z = 5323733
20
XDOT = -1911
647884 XDOT = -495
989698
YDOT = -25059
769921 feet/sec YDOT = -7644
249049 meter/sec
ZDOT = -827
051546 ZDOT = -254
704934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11647176
61 X = 3550059
43
Y = -7484193
08 feet Y = -2281182
05 meter
Z = 17440185
73 Z = 5315768
61
XDOT = 13896
166569 XDOT = 4235
551570
YDOT = 19719
057607 feet/sec YDOT = 6010
368759 meter/sec
ZDOT = -838
432295 ZDOT = -255
554163
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 19296
54792676
00016717 00000-0 10270-3 0 9000
2 25544 51
6398 84
7954 0006912 180
3487 179
7660 15
50179317 35160
Satellite: ISS
Catalog Number: 25544
Epoch time: 19296
54792676 = yrday
fracday
Element set: 900
Inclination: 51
6398 deg
RA of node: 84
7954 deg
Eccentricity:
0006912
Arg of perigee: 180
3487 deg
Mean anomaly: 179
7660 deg
Mean motion: 15
50179317 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3516
Checksum: 354
Coasting Arc #2 (Orbit 3530)
---------------------------------------
Vector Time (GMT): 2019/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4235189
19 A = 6788923
17 meter
Y = 28641
17 meter E =
0016311
Z = -5318798
97 I = 52
00162
XDOT = 864
515683 Wp = 120
56528
YDOT = 7567
596399 meter/sec RA = 79
23167 deg
ZDOT = 722
729773 TA = 156
35691
MA = 156
28187
Ha = 228
367 n
mi
Hp = 220
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13894977
65 X = 4260390
22
Y = 93967
09 feet Y = 76142
66 meter
Z = -17450127
85 Z = -5298164
56
XDOT = 2836
337542 XDOT = 776
317709
YDOT = 24828
072174 feet/sec YDOT = 7576
770917 meter/sec
ZDOT = 2371
160671 ZDOT = 726
714678
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11969415
31 X = -3648277
79
Y = 7286231
33 feet Y = 2220843
31 meter
Z = -17355982
42 Z = -5290103
44
XDOT = -14918
297565 XDOT = -4547
097098
YDOT = -18766
511849 feet/sec YDOT = -5720
032812 meter/sec
ZDOT = 2388
763708 ZDOT = 728
095178
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 19297
51489290
00016717 00000-0 10270-3 0 9014
2 25544 51
6405 80
0041 0006898 183
8788 176
2310 15
50226081 35312
Satellite: ISS
Catalog Number: 25544
Epoch time: 19297
51489290 = yrday
fracday
Element set: 901
Inclination: 51
6405 deg
RA of node: 80
0041 deg
Eccentricity:
0006898
Arg of perigee: 183
8788 deg
Mean anomaly: 176
2310 deg
Mean motion: 15
50226081 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3531
Checksum: 310
Coasting Arc #3 (Orbit 3537)
---------------------------------------
Vector Time (GMT): 2019/297/21:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3016698
75 A = 6791046
03 meter
Y = 3714631
71 meter E =
0011549
Z = 4817759
36 I = 52
00426
XDOT = -3523
687080 Wp = 149
66544
YDOT = -6278
180466 meter/sec RA = 77
22393 deg
ZDOT = 2621
827485 TA = 274
53319
MA = 274
66510
Ha = 228
239 n
mi
Hp = 220
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9897305
60 X = -3081414
94
Y = 12187111
91 feet Y = 3680535
30 meter
Z = 15806297
13 Z = 4802947
77
XDOT = -11560
653148 XDOT = -3465
956304
YDOT = -20597
704942 feet/sec YDOT = -6317
261868 meter/sec
ZDOT = 8601
796209 ZDOT = 2604
851118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9818017
31 X = -2992531
68
Y = 12338141
07 feet Y = 3760665
40 meter
Z = 15738430
50 Z = 4797073
62
XDOT = -11029
294040 XDOT = -3361
728823
YDOT = -19702
953415 feet/sec YDOT = -6005
460201 meter/sec
ZDOT = 8524
823852 ZDOT = 2598
366310
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 19297
96614327
00016717 00000-0 10270-3 0 9025
2 25544 51
6389 77
7712 0006454 186
3353 173
7717 15
50204940 35385
Satellite: ISS
Catalog Number: 25544
Epoch time: 19297
96614327 = yrday
fracday
Element set: 902
Inclination: 51
6389 deg
RA of node: 77
7712 deg
Eccentricity:
0006454
Arg of perigee: 186
3353 deg
Mean anomaly: 173
7717 deg
Mean motion: 15
50204940 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3538
Checksum: 334
Coasting Arc #4 (Orbit 3552)
---------------------------------------
Vector Time (GMT): 2019/298/21:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2971196
89 A = 6790324
48 meter
Y = -3524897
75 meter E =
0011322
Z = -4993970
95 I = 51
99341
XDOT = 3794
887931 Wp = 105
12211
YDOT = 6279
642454 meter/sec RA = 72
29036 deg
ZDOT = -2181
556835 TA = 143
71182
MA = 143
63498
Ha = 228
135 n
mi
Hp = 220
899
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9748021
29 X = 3034650
86
Y = -11564625
18 feet Y = -3491317
29 meter
Z = -16384419
12 Z = -4979383
36
XDOT = 12450
419721 XDOT = 3734
982081
YDOT = 20602
501489 feet/sec YDOT = 6321
744462 meter/sec
ZDOT = -7157
338696 ZDOT = -2163
268312
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9479159
51 X = 2889247
82
Y = -11878369
39 feet Y = -3620526
99 meter
Z = -16317583
77 Z = -4973599
53
XDOT = 12291
986437 XDOT = 3746
597466
YDOT = 19495
868777 feet/sec YDOT = 5942
340803 meter/sec
ZDOT = -7074
393998 ZDOT = -2156
275290
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 19298
93310957
00016717 00000-0 10270-3 0 9036
2 25544 51
6389 72
9788 0006454 189
3698 170
7333 15
50208963 35537
Satellite: ISS
Catalog Number: 25544
Epoch time: 19298
93310957 = yrday
fracday
Element set: 903
Inclination: 51
6389 deg
RA of node: 72
9788 deg
Eccentricity:
0006454
Arg of perigee: 189
3698 deg
Mean anomaly: 170
7333 deg
Mean motion: 15
50208963 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3553
Checksum: 357
Coasting Arc #5 (Orbit 3568)
---------------------------------------
Vector Time (GMT): 2019/299/21:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2931999
61 A = 6789765
35 meter
Y = 3363761
07 meter E =
0009597
Z = 5117582
37 I = 51
98100
XDOT = -4086
330929 Wp = 163
29783
YDOT = -6240
371965 meter/sec RA = 67
35659 deg
ZDOT = 1750
840773 TA = 269
78569
MA = 269
89566
Ha = 227
979 n
mi
Hp = 221
037
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9619421
29 X = -2994255
20
Y = 11035961
51 feet Y = 3330625
62 meter
Z = 16789968
41 Z = 5103188
06
XDOT = -13406
597537 XDOT = -4024
750380
YDOT = -20473
661301 feet/sec YDOT = -6285
723769 meter/sec
ZDOT = 5744
228259 ZDOT = 1731
140438
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9173910
23 X = -2796207
84
Y = 11505442
81 feet Y = 3506858
97 meter
Z = 16724021
90 Z = 5097481
88
XDOT = -13603
561570 XDOT = -4146
365566
YDOT = -19113
320905 feet/sec YDOT = -5825
740212 meter/sec
ZDOT = 5654
856905 ZDOT = 1723
600385
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 19299
96453869
00016717 00000-0 10270-3 0 9041
2 25544 51
6396 67
8675 0006414 194
4189 165
6780 15
50212878 35697
Satellite: ISS
Catalog Number: 25544
Epoch time: 19299
96453869 = yrday
fracday
Element set: 904
Inclination: 51
6396 deg
RA of node: 67
8675 deg
Eccentricity:
0006414
Arg of perigee: 194
4189 deg
Mean anomaly: 165
6780 deg
Mean motion: 15
50212878 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3569
Checksum: 372
Coasting Arc #6 (Orbit 3583)
---------------------------------------
Vector Time (GMT): 2019/300/21:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2957399
10 A = 6789289
68 meter
Y = -3175943
42 meter E =
0012500
Z = -5230891
90 I = 51
96656
XDOT = 4353
691111 Wp = 106
93083
YDOT = 6162
281697 meter/sec RA = 62
42062 deg
ZDOT = -1286
057553 TA = 150
78684
MA = 150
71687
Ha = 227
833 n
mi
Hp = 221
242
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9702752
96 X = 3018103
09
Y = -10419761
89 feet Y = -3142532
54 meter
Z = -17161718
83 Z = -5216377
97
XDOT = 14283
763487 XDOT = 4290
706234
YDOT = 20217
459636 feet/sec YDOT = 6210
615512 meter/sec
ZDOT = -4219
348928 ZDOT = -1265
061661
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9101391
84 X = 2774104
23
Y = -11052467
22 feet Y = -3368792
01 meter
Z = -17095235
62 Z = -5210627
82
XDOT = 14822
582008 XDOT = 4517
922996
YDOT = 18553
890164 feet/sec YDOT = 5655
225722 meter/sec
ZDOT = -4124
080560 ZDOT = -1257
019755
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 19300
93150062
00016717 00000-0 10270-3 0 9051
2 25544 51
6406 63
0751 0006314 197
4463 162
6471 15
50216405 35840
Satellite: ISS
Catalog Number: 25544
Epoch time: 19300
93150062 = yrday
fracday
Element set: 905
Inclination: 51
6406 deg
RA of node: 63
0751 deg
Eccentricity:
0006314
Arg of perigee: 197
4463 deg
Mean anomaly: 162
6471 deg
Mean motion: 15
50216405 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3584
Checksum: 285
Coasting Arc #7 (Orbit 3592)
---------------------------------------
Vector Time (GMT): 2019/301/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3182875
90 A = 6800608
60 meter
Y = 5998011
64 meter E =
0007738
Z = 344905
99 I = 51
99751
XDOT = -4316
149960 Wp = 75
43108
YDOT = 1937
760641 meter/sec RA = 59
77252 deg
ZDOT = 6021
372104 TA = 288
26009
MA = 288
34429
Ha = 227
842 n
mi
Hp = 221
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10442506
24 X = 3113892
42
Y = 19678515
87 feet Y = 6033219
11 meter
Z = 1131581
34 Z = 360199
89
XDOT = -14160
596982 XDOT = -4366
747100
YDOT = 6357
482419 feet/sec YDOT = 1889
211715 meter/sec
ZDOT = 19755
157822 ZDOT = 6000
282298
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15691242
87 X = -4782690
83
Y = -15808645
79 feet Y = -4818475
24 meter
Z = 1200839
37 Z = 366015
84
XDOT = 10683
681414 XDOT = 3256
386095
YDOT = -9084
995187 feet/sec YDOT = -2769
106533 meter/sec
ZDOT = 19658
776825 ZDOT = 5991
995176
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 19301
51167735
00016717 00000-0 10270-3 0 9062
2 25544 51
6422 60
1963 0006756 198
4559 161
6348 15
50235763 35938
Satellite: ISS
Catalog Number: 25544
Epoch time: 19301
51167735 = yrday
fracday
Element set: 906
Inclination: 51
6422 deg
RA of node: 60
1963 deg
Eccentricity:
0006756
Arg of perigee: 198
4559 deg
Mean anomaly: 161
6348 deg
Mean motion: 15
50235763 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3593
Checksum: 324
Coasting Arc #8 (Orbit 3607)
---------------------------------------
Vector Time (GMT): 2019/302/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3374760
85 A = 6800386
92 meter
Y = -5842452
71 meter E =
0014635
Z = -773769
09 I = 51
97842
XDOT = 4456
230096 Wp = 163
97340
YDOT = -1787
911313 meter/sec RA = 54
84354 deg
ZDOT = -5976
316420 TA = 24
34235
MA = 24
27329
Ha = 227
674 n
mi
Hp = 221
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11072050
05 X = -3305419
38
Y = -19168151
95 feet Y = -5879803
97 meter
Z = -2538612
50 Z = -789994
42
XDOT = 14620
177479 XDOT = 4504
922320
YDOT = -5865
850764 feet/sec YDOT = -1737
806398 meter/sec
ZDOT = -19607
337335 ZDOT = -5954
550805
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16394776
48 X = 4997127
87
Y = 14860721
96 feet Y = 4529548
05 meter
Z = -2612114
43 Z = -796172
48
XDOT = -11162
225557 XDOT = -3402
246350
YDOT = 8908
247112 feet/sec YDOT = 2715
233720 meter/sec
ZDOT = -19507
883147 ZDOT = -5946
002783
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 19302
47863796
00016717 00000-0 10270-3 0 9079
2 25544 51
6416 55
4049 0006704 202
8328 157
2525 15
50241487 36085
Satellite: ISS
Catalog Number: 25544
Epoch time: 19302
47863796 = yrday
fracday
Element set: 907
Inclination: 51
6416 deg
RA of node: 55
4049 deg
Eccentricity:
0006704
Arg of perigee: 202
8328 deg
Mean anomaly: 157
2525 deg
Mean motion: 15
50241487 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3608
Checksum: 318
Coasting Arc #9 (Orbit 3623)
---------------------------------------
Vector Time (GMT): 2019/303/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3570357
20 A = 6800043
06 meter
Y = 5665046
79 meter E =
0008709
Z = 1171278
93 I = 51
95872
XDOT = -4605
415084 Wp = 81
96795
YDOT = 1678
406311 meter/sec RA = 49
91282 deg
ZDOT = 5884
437174 TA = 290
66907
MA = 290
76242
Ha = 227
557 n
mi
Hp = 221
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11713770
35 X = 3501054
07
Y = 18586111
52 feet Y = 5704585
53 meter
Z = 3842778
65 Z = 1188454
63
XDOT = -15109
629542 XDOT = -4652
425335
YDOT = 5506
582386 feet/sec YDOT = 1626
642361 meter/sec
ZDOT = 19305
896240 ZDOT = 5861
951026
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17059267
23 X = -5199664
65
Y = -13821471
82 feet Y = -4212784
61 meter
Z = 3920615
19 Z = 1195003
51
XDOT = 11639
664786 XDOT = 3547
769827
YDOT = -8886
134325 feet/sec YDOT = -2708
493742 meter/sec
ZDOT = 19203
161455 ZDOT = 5853
123612
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 19303
51006043
00016717 00000-0 10270-3 0 9080
2 25544 51
6431 50
2938 0006752 206
4382 153
6425 15
50243317 36246
Satellite: ISS
Catalog Number: 25544
Epoch time: 19303
51006043 = yrday
fracday
Element set: 908
Inclination: 51
6431 deg
RA of node: 50
2938 deg
Eccentricity:
0006752
Arg of perigee: 206
4382 deg
Mean anomaly: 153
6425 deg
Mean motion: 15
50243317 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3624
Checksum: 280
Coasting Arc #10 (Orbit 3638)
---------------------------------------
Vector Time (GMT): 2019/304/10:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3707559
34 A = 6799541
70 meter
Y = -5464503
94 meter E =
0012083
Z = -1589233
80 I = 51
93506
XDOT = 4798
754616 Wp = 172
38115
YDOT = -1584
686964 meter/sec RA = 44
98055 deg
ZDOT = -5762
904823 TA = 24
90789
MA = 24
84962
Ha = 227
368 n
mi
Hp = 221
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12163908
61 X = -3638458
32
Y = -17928162
53 feet Y = -5505578
06 meter
Z = -5214021
64 Z = -1607076
50
XDOT = 15743
945590 XDOT = 4844
112043
YDOT = -5199
104213 feet/sec YDOT = -1530
770102 meter/sec
ZDOT = -18907
168056 ZDOT = -5739
483605
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17486343
28 X = 5329837
43
Y = 12757643
98 feet Y = 3888529
89 meter
Z = -5294905
55 Z = -1613887
21
XDOT = -12239
567620 XDOT = -3730
620211
YDOT = 8995
782686 feet/sec YDOT = 2741
914563 meter/sec
ZDOT = -18800
173218 ZDOT = -5730
292797
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 19304
47701704
00016717 00000-0 10270-3 0 9093
2 25544 51
6435 45
5023 0006631 210
3173 149
7595 15
50245162 36390
Satellite: ISS
Catalog Number: 25544
Epoch time: 19304
47701704 = yrday
fracday
Element set: 909
Inclination: 51
6435 deg
RA of node: 45
5023 deg
Eccentricity:
0006631
Arg of perigee: 210
3173 deg
Mean anomaly: 149
7595 deg
Mean motion: 15
50245162 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3639
Checksum: 297
Coasting Arc #11 (Orbit 3644)
---------------------------------------
Vector Time (GMT): 2019/304/19:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5289541
39 A = 6793185
18 meter
Y = -400644
42 meter E =
0006868
Z = 4236377
10 I = 51
90210
XDOT = -2470
673848 Wp = 110
86383
YDOT = -6256
981568 meter/sec RA = 43
09755 deg
ZDOT = -3674
202931 TA = 16
67243
MA = 16
64986
Ha = 227
310 n
mi
Hp = 221
792
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17354138
40 X = -5305246
55
Y = -1314450
19 feet Y = -459883
77 meter
Z = 13898875
00 Z = 4210643
76
XDOT = -8105
885328 XDOT = -2382
675206
YDOT = -20528
154752 feet/sec YDOT = -6284
118220 meter/sec
ZDOT = -12054
471560 ZDOT = -3685
991299
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15246807
62 X = -4647226
96
Y = -8583542
15 feet Y = -2616263
65 meter
Z = 13781519
76 Z = 4200607
22
XDOT = 805
341882 XDOT = 245
468206
YDOT = -20883
115078 feet/sec YDOT = -6365
173476 meter/sec
ZDOT = -12107
656440 ZDOT = -3690
413683
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 19304
86379812
00016717 00000-0 10270-3 0 9109
2 25544 51
6408 43
5895 0006188 213
8040 146
2716 15
50245219 36450
Satellite: ISS
Catalog Number: 25544
Epoch time: 19304
86379812 = yrday
fracday
Element set: 910
Inclination: 51
6408 deg
RA of node: 43
5895 deg
Eccentricity:
0006188
Arg of perigee: 213
8040 deg
Mean anomaly: 146
2716 deg
Mean motion: 15
50245219 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3645
Checksum: 313
Coasting Arc #12 (Orbit 3657)
---------------------------------------
Vector Time (GMT): 2019/305/15:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 919680
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5819653
68 A = 6796531
09 meter
Y = -1535420
73 meter E =
0011148
Z = 3141727
46 I = 51
89432
XDOT = -1103
653239 Wp = 123
58002
YDOT = -5810
437018 meter/sec RA = 38
94522 deg
ZDOT = -4877
616102 TA = 20
39970
MA = 20
35521
Ha = 227
185 n
mi
Hp = 221
881
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19093351
97 X = -5817312
68
Y = -5037469
58 feet Y = -1600487
24 meter
Z = 10307504
79 Z = 3113462
86
XDOT = -3620
909577 XDOT = -1014
904031
YDOT = -19063
113575 feet/sec YDOT = -5822
282425 meter/sec
ZDOT = -16002
677501 ZDOT = -4882
762007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2147008
81 X = 654408
28
Y = -19696725
47 feet Y = -6003561
92 meter
Z = 10178713
23 Z = 3102471
79
XDOT = 16898
469952 XDOT = 5150
653641
YDOT = -6450
627311 feet/sec YDOT = -1966
151205 meter/sec
ZDOT = -16025
593278 ZDOT = -4884
600831
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 19305
70182482
00016717 00000-0 10270-3 0 9119
2 25544 51
6428 39
4366 0006220 216
1932 143
8799 15
50260673 36581
Satellite: ISS
Catalog Number: 25544
Epoch time: 19305
70182482 = yrday
fracday
Element set: 911
Inclination: 51
6428 deg
RA of node: 39
4366 deg
Eccentricity:
0006220
Arg of perigee: 216
1932 deg
Mean anomaly: 143
8799 deg
Mean motion: 15
50260673 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3658
Checksum: 314
Coasting Arc #13 (Orbit 3671)
---------------------------------------
Vector Time (GMT): 2019/306/13:59:43
634
Vector Time (MET): N/A
Weight (LBS) : 919680
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -587480
59 A = 6791383
56 meter
Y = -4875437
52 meter E =
0006197
Z = -4695795
41 I = 51
85222
XDOT = 6825
943651 Wp = 103
26698
YDOT = 1942
840720 meter/sec RA = 34
44563 deg
ZDOT = -2875
720239 TA = 138
23232
MA = 138
18500
Ha = 227
057 n
mi
Hp = 222
064
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1927429
75 X = -510108
46
Y = -15995529
91 feet Y = -4881574
36 meter
Z = -15406152
92 Z = -4698461
46
XDOT = 22394
828251 XDOT = 6817
679784
YDOT = 6374
149343 feet/sec YDOT = 2019
127136 meter/sec
ZDOT = -9434
777686 ZDOT = -2842
581863
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15693560
14 X = 4783397
13
Y = 3594982
97 feet Y = 1095750
81 meter
Z = -15417839
60 Z = -4699357
51
XDOT = -13210
999433 XDOT = -4026
712627
YDOT = 17920
194941 feet/sec YDOT = 5462
075418 meter/sec
ZDOT = -9283
796917 ZDOT = -2829
701300
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 19306
60431507
00016717 00000-0 10270-3 0 9125
2 25544 51
6424 34
9636 0006462 219
2083 140
8600 15
50226057 36728
Satellite: ISS
Catalog Number: 25544
Epoch time: 19306
60431507 = yrday
fracday
Element set: 912
Inclination: 51
6424 deg
RA of node: 34
9636 deg
Eccentricity:
0006462
Arg of perigee: 219
2083 deg
Mean anomaly: 140
8600 deg
Mean motion: 15
50226057 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3672
Checksum: 287
Coasting Arc #14 (Orbit 3687)
---------------------------------------
Vector Time (GMT): 2019/307/13:59:43
634
Vector Time (MET): N/A
Weight (LBS) : 919680
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 526541
39 A = 6790582
63 meter
Y = 4700978
45 meter E =
0008278
Z = 4873663
10 I = 51
82200
XDOT = -7038
349180 Wp = 168
82982
YDOT = -1765
048974 meter/sec RA = 29
50158 deg
ZDOT = 2454
304833 TA = 257
07070
MA = 257
16317
Ha = 226
786 n
mi
Hp = 222
231
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1727498
01 X = 450260
71
Y = 15423157
64 feet Y = 4706439
97 meter
Z = 15989708
33 Z = 4876035
72
XDOT = -23091
696786 XDOT = -7030
010582
YDOT = -5790
843091 feet/sec YDOT = -1843
710203 meter/sec
ZDOT = 8052
181211 ZDOT = 2420
134952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15145642
91 X = -4616391
96
Y = -3337083
26 feet Y = -1017142
98 meter
Z = 16000068
42 Z = 4876820
85
XDOT = 12563
774850 XDOT = 3829
438574
YDOT = -19025
668832 feet/sec YDOT = -5799
023860 meter/sec
ZDOT = 7896
484314 ZDOT = 2406
848419
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 19307
63572786
00016717 00000-0 10270-3 0 9135
2 25544 51
6429 29
8520 0006390 223
9880 136
0762 15
50253586 36885
Satellite: ISS
Catalog Number: 25544
Epoch time: 19307
63572786 = yrday
fracday
Element set: 913
Inclination: 51
6429 deg
RA of node: 29
8520 deg
Eccentricity:
0006390
Arg of perigee: 223
9880 deg
Mean anomaly: 136
0762 deg
Mean motion: 15
50253586 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3688
Checksum: 334
Coasting Arc #15 (Orbit 3698)
---------------------------------------
Vector Time (GMT): 2019/308/07:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 919680
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1165988
19 A = 6791063
65 meter
Y = 4720512
49 meter E =
0008398
Z = 4742431
89 I = 51
80116
XDOT = -7071
037600 Wp = 163
80387
YDOT = -1033
585924 meter/sec RA = 25
99746 deg
ZDOT = 2758
272767 TA = 258
87777
MA = 258
97221
Ha = 226
709 n
mi
Hp = 222
269
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3825420
56 X = 1090079
02
Y = 15487245
70 feet Y = 4733126
87 meter
Z = 15559159
76 Z = 4747911
60
XDOT = -23198
942258 XDOT = -7072
352517
YDOT = -3391
029935 feet/sec YDOT = -1112
666659 meter/sec
ZDOT = 9049
451336 ZDOT = 2723
920711
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5224368
94 X = 1592387
65
Y = -15047614
63 feet Y = -4586512
94 meter
Z = 15583688
18 Z = 4749908
16
XDOT = 16656
744663 XDOT = 5076
975773
YDOT = 15023
381339 feet/sec YDOT = 4579
126632 meter/sec
ZDOT = 8892
856834 ZDOT = 2710
542763
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19308
34482369
00016717 00000-0 10270-3 0 9142
2 25544 51
6412 26
3343 0006410 225
3627 134
7001 15
50265675 36995
Satellite: ISS
Catalog Number: 25544
Epoch time: 19308
34482369 = yrday
fracday
Element set: 914
Inclination: 51
6412 deg
RA of node: 26
3343 deg
Eccentricity:
0006410
Arg of perigee: 225
3627 deg
Mean anomaly: 134
7001 deg
Mean motion: 15
50265675 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3699
Checksum: 301
Coasting Arc #16 (Orbit 3699)
---------------------------------------
Vector Time (GMT): 2019/308/09:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 934394
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4640205
17 A = 6798070
12 meter
Y = -4329502
34 meter E =
0008221
Z = -2422450
87 I = 51
82402
XDOT = 4955
130123 Wp = 182
97432
YDOT = -2310
412914 meter/sec RA = 25
55157 deg
ZDOT = -5369
469635 TA = 24
00298
MA = 23
96469
Ha = 226
723 n
mi
Hp = 222
244
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15223770
26 X = -4579679
50
Y = -14204404
02 feet Y = -4381053
93 meter
Z = -7947673
46 Z = -2444844
57
XDOT = 16256
988592 XDOT = 5006
679753
YDOT = -7580
094863 feet/sec YDOT = -2254
712830 meter/sec
ZDOT = -17616
370193 ZDOT = -5345
274028
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15153851
38 X = 4618893
90
Y = 14221879
24 feet Y = 4334828
79 meter
Z = -8049392
96 Z = -2453454
97
XDOT = -15346
937806 XDOT = -4677
746643
YDOT = 6457
767707 feet/sec YDOT = 1968
327597 meter/sec
ZDOT = -17505
773576 ZDOT = -5335
759786
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19308
40928731
00016717 00000-0 10270-3 0 9158
2 25544 51
6435 26
0154 0006441 224
8551 135
2079 15
50254952 37001
Satellite: ISS
Catalog Number: 25544
Epoch time: 19308
40928731 = yrday
fracday
Element set: 915
Inclination: 51
6435 deg
RA of node: 26
0154 deg
Eccentricity:
0006441
Arg of perigee: 224
8551 deg
Mean anomaly: 135
2079 deg
Mean motion: 15
50254952 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3700
Checksum: 293
Coasting Arc #17 (Orbit 3715)
---------------------------------------
Vector Time (GMT): 2019/309/09:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 934394
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4656589
85 A = 6797209
37 meter
Y = 4092053
29 meter E =
0008615
Z = 2783515
13 I = 51
79092
XDOT = -5165
039574 Wp = 102
88037
YDOT = 2375
131541 meter/sec RA = 20
60888 deg
ZDOT = 5133
725441 TA = 288
53954
MA = 288
63312
Ha = 226
590 n
mi
Hp = 222
339
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15277525
74 X = 4596964
30
Y = 13425371
70 feet Y = 4143793
17 meter
Z = 9132267
47 Z = 2805990
55
XDOT = -16945
667893 XDOT = -5216
152179
YDOT = 7792
426315 feet/sec YDOT = 2317
086612 meter/sec
ZDOT = 16842
931236 ZDOT = 5108
511193
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15429467
96 X = -4702901
84
Y = -13179512
08 feet Y = -4017115
28 meter
Z = 9234375
29 Z = 2814637
59
XDOT = 15970
378961 XDOT = 4867
771507
YDOT = -6941
622941 feet/sec YDOT = -2115
806672 meter/sec
ZDOT = 16727
687313 ZDOT = 5098
599093
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19309
44069556
00016717 00000-0 10270-3 0 9165
2 25544 51
6437 20
9043 0006430 228
3021 131
7580 15
50276704 37166
Satellite: ISS
Catalog Number: 25544
Epoch time: 19309
44069556 = yrday
fracday
Element set: 916
Inclination: 51
6437 deg
RA of node: 20
9043 deg
Eccentricity:
0006430
Arg of perigee: 228
3021 deg
Mean anomaly: 131
7580 deg
Mean motion: 15
50276704 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3716
Checksum: 295
Coasting Arc #18 (Orbit 3730)
---------------------------------------
Vector Time (GMT): 2019/310/09:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 934394
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4614273
28 A = 6796359
36 meter
Y = -3868566
55 meter E =
0004921
Z = -3145385
60 I = 51
75626
XDOT = 5381
997935 Wp = 187
04586
YDOT = -2470
106889 meter/sec RA = 15
66396 deg
ZDOT = -4861
304722 TA = 29
07743
MA = 29
05004
Ha = 226
405 n
mi
Hp = 222
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15138691
88 X = -4555392
17
Y = -12692147
49 feet Y = -3919837
42 meter
Z = -10319506
55 Z = -3167657
25
XDOT = 17657
473540 XDOT = 5432
833208
YDOT = -8104
025227 feet/sec YDOT = -2409
637387 meter/sec
ZDOT = -15949
162475 ZDOT = -4835
037167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15482726
97 X = 4719135
18
Y = 12184294
07 feet Y = 3713772
83 meter
Z = -10420698
56 Z = -3176228
92
XDOT = -16596
688149 XDOT = -5058
670548
YDOT = 7562
645649 feet/sec YDOT = 2305
094394 meter/sec
ZDOT = -15829
112651 ZDOT = -4824
713536
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19310
40764160
00016717 00000-0 10270-3 0 9177
2 25544 51
6437 16
1131 0006451 232
2442 127
8124 15
50252735 37310
Satellite: ISS
Catalog Number: 25544
Epoch time: 19310
40764160 = yrday
fracday
Element set: 917
Inclination: 51
6437 deg
RA of node: 16
1131 deg
Eccentricity:
0006451
Arg of perigee: 232
2442 deg
Mean anomaly: 127
8124 deg
Mean motion: 15
50252735 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3731
Checksum: 271
Coasting Arc #19 (Orbit 3746)
---------------------------------------
Vector Time (GMT): 2019/311/09:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 934394
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4558728
31 A = 6795349
98 meter
Y = 3650818
86 meter E =
0007907
Z = 3471554
07 I = 51
72161
XDOT = -5572
688563 Wp = 119
10951
YDOT = 2609
456263 meter/sec RA = 10
71549 deg
ZDOT = 4562
049791 TA = 281
49901
MA = 281
58778
Ha = 226
223 n
mi
Hp = 222
641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14956457
72 X = 4500701
84
Y = 11977752
18 feet Y = 3701473
40 meter
Z = 11389613
10 Z = 3493558
01
XDOT = -18283
098960 XDOT = -5623
614333
YDOT = 8561
208212 feet/sec YDOT = 2546
853857 meter/sec
ZDOT = 14967
354957 ZDOT = 4534
855606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15464759
91 X = -4713658
82
Y = -11212307
32 feet Y = -3417511
27 meter
Z = 11489596
47 Z = 3502029
00
XDOT = 17110
599562 XDOT = 5215
310746
YDOT = -8351
215173 feet/sec YDOT = -2545
450385 meter/sec
ZDOT = 14843
074722 ZDOT = 4524
169175
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19311
43904575
00016717 00000-0 10270-3 0 9188
2 25544 51
6446 11
0017 0006425 236
3089 123
7449 15
50286178 37470
Satellite: ISS
Catalog Number: 25544
Epoch time: 19311
43904575 = yrday
fracday
Element set: 918
Inclination: 51
6446 deg
RA of node: 11
0017 deg
Eccentricity:
0006425
Arg of perigee: 236
3089 deg
Mean anomaly: 123
7449 deg
Mean motion: 15
50286178 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3747
Checksum: 312
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