[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 31st 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16550 5887 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
306/13:59:45
869 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
311/22:40:57
510 1
0 1
3 1
3
N/A 0
6 -0
0 225
9
000/00:05:51
019 0
6 0
0 223
7
312/03:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 225
9
000/00:00:00
000 0
0 0
0 223
5
317/14:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 225
2
000/00:00:00
000 0
0 0
0 223
6
Coasting Arc #1 (Orbit 3623)
---------------------------------------
Vector Time (GMT): 2019/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5096648
19 A = 6792409
81 meter
Y = 602062
95 meter E =
0010660
Z = -4459526
12 I = 51
93310
XDOT = 2144
989204 Wp = 149
01957
YDOT = 6548
248950 meter/sec RA = 49
62244 deg
ZDOT = 3330
143930 TA = 154
55905
MA = 154
50653
Ha = 227
538 n
mi
Hp = 221
681
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16721286
71 X = 5111199
44
Y = 1975272
16 feet Y = 659138
71 meter
Z = -14630991
19 Z = -4434732
48
XDOT = 7037
366156 XDOT = 2055
428932
YDOT = 21483
756396 feet/sec YDOT = 6571
734911 meter/sec
ZDOT = 10925
669063 ZDOT = 3340
346352
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14527033
17 X = -4427839
71
Y = 8704240
06 feet Y = 2653052
37 meter
Z = -14517938
72 Z = -4425067
72
XDOT = -17996
353581 XDOT = -5485
288571
YDOT = -11705
986932 feet/sec YDOT = -3567
984817 meter/sec
ZDOT = 10971
611937 ZDOT = 3344
147318
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
51006657
00016717 00000-0 10270-3 0 9003
2 25544 51
6442 50
2951 0006725 207
0625 153
0176 15
50240737 36240
Satellite: ISS
Catalog Number: 25544
Epoch time: 19303
51006657 = yrday
fracday
Element set: 900
Inclination: 51
6442 deg
RA of node: 50
2951 deg
Eccentricity:
0006725
Arg of perigee: 207
0625 deg
Mean anomaly: 153
0176 deg
Mean motion: 15
50240737 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3624
Checksum: 277
Coasting Arc #2 (Orbit 3639)
---------------------------------------
Vector Time (GMT): 2019/304/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5293200
16 A = 6793367
23 meter
Y = -596584
80 meter E =
0007382
Z = 4208288
40 I = 51
91386
XDOT = -2244
672874 Wp = 114
66768
YDOT = -6317
136362 meter/sec RA = 44
68520 deg
ZDOT = -3716
792461 TA = 13
36960
MA = 13
35005
Ha = 227
582 n
mi
Hp = 221
687
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17366142
26 X = -5306577
58
Y = -1957299
22 feet Y = -655852
04 meter
Z = 13806720
47 Z = 4182542
90
XDOT = -7364
412317 XDOT = -2155
811455
YDOT = -20725
512999 feet/sec YDOT = -6341
740897 meter/sec
ZDOT = -12194
200989 ZDOT = -3727
480879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14863519
43 X = 4530400
72
Y = -9365764
68 feet Y = -2854685
07 meter
Z = 13689327
57 Z = 4172507
04
XDOT = 17940
694581 XDOT = 5468
323708
YDOT = 10567
909893 feet/sec YDOT = 3221
098935 meter/sec
ZDOT = -12242
366654 ZDOT = -3731
473356
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
54148842
00016717 00000-0 10270-3 0 9011
2 25544 51
6445 45
1838 0006579 209
9298 150
1478 15
50216720 36400
Satellite: ISS
Catalog Number: 25544
Epoch time: 19304
54148842 = yrday
fracday
Element set: 901
Inclination: 51
6445 deg
RA of node: 45
1838 deg
Eccentricity:
0006579
Arg of perigee: 209
9298 deg
Mean anomaly: 150
1478 deg
Mean motion: 15
50216720 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3640
Checksum: 315
Coasting Arc #3 (Orbit 3654)
---------------------------------------
Vector Time (GMT): 2019/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949211
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5511792
34 A = 6794240
08 meter
Y = 564442
71 meter E =
0007515
Z = -3940111
47 I = 51
89228
XDOT = 2293
721796 Wp = 160
63152
YDOT = 6061
710485 meter/sec RA = 39
74765 deg
ZDOT = 4072
370373 TA = 151
93234
MA = 151
89180
Ha = 227
201 n
mi
Hp = 222
029
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18083308
19 X = 5524210
16
Y = 1851846
16 feet Y = 626149
05 meter
Z = -12926874
90 Z = -3913306
55
XDOT = 7525
333976 XDOT = 2205
985821
YDOT = 19887
501591 feet/sec YDOT = 6086
869776 meter/sec
ZDOT = 13360
795186 ZDOT = 4083
299770
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15181077
61 X = -4627192
46
Y = 10154571
75 feet Y = 3095113
47 meter
Z = -12804648
34 Z = -3902856
81
XDOT = -17664
701488 XDOT = -5384
201013
YDOT = -9479
449338 feet/sec YDOT = -2889
336158 meter/sec
ZDOT = 13410
072050 ZDOT = 4087
389961
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
50844297
00016717 00000-0 10270-3 0 9026
2 25544 51
6443 40
3928 0006551 215
0847 144
9873 15
50239705 36557
Satellite: ISS
Catalog Number: 25544
Epoch time: 19305
50844297 = yrday
fracday
Element set: 902
Inclination: 51
6443 deg
RA of node: 40
3928 deg
Eccentricity:
0006551
Arg of perigee: 215
0847 deg
Mean anomaly: 144
9873 deg
Mean motion: 15
50239705 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3655
Checksum: 317
Coasting Arc #4 (Orbit 3670)
---------------------------------------
Vector Time (GMT): 2019/306/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916487
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5711398
96 A = 6795212
58 meter
Y = -493099
10 meter E =
0009126
Z = 3637544
95 I = 51
86859
XDOT = -2310
573261 Wp = 118
70354
YDOT = -5826
029802 meter/sec RA = 34
80872 deg
ZDOT = -4413
544201 TA = 18
36450
MA = 18
33158
Ha = 227
234 n
mi
Hp = 222
025
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18738185
55 X = -5723129
94
Y = -1617779
21 feet Y = -557033
72 meter
Z = 11934202
60 Z = 3609772
18
XDOT = -7580
620934 XDOT = -2223
814301
YDOT = -19114
271005 feet/sec YDOT = -5851
383003 meter/sec
ZDOT = -14480
131893 ZDOT = -4424
557760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15344208
42 X = 4676914
73
Y = -11013576
39 feet Y = -3356938
08 meter
Z = 11807556
99 Z = 3598943
37
XDOT = 17314
728220 XDOT = 5277
529161
YDOT = 8531
140022 feet/sec YDOT = 2600
291479 meter/sec
ZDOT = -14529
805962 ZDOT = -4428
684857
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
53986195
00016717 00000-0 10270-3 0 9035
2 25544 51
6439 35
2820 0006496 218
0103 142
0590 15
50230480 36716
Satellite: ISS
Catalog Number: 25544
Epoch time: 19306
53986195 = yrday
fracday
Element set: 903
Inclination: 51
6439 deg
RA of node: 35
2820 deg
Eccentricity:
0006496
Arg of perigee: 218
0103 deg
Mean anomaly: 142
0590 deg
Mean motion: 15
50230480 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3671
Checksum: 295
Coasting Arc #5 (Orbit 3671)
---------------------------------------
Vector Time (GMT): 2019/306/13:59:45
869
Vector Time (MET): N/A
Weight (LBS) : 916487
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -578277
40 A = 6791376
59 meter
Y = -4872795
32 meter E =
0006225
Z = -4699713
41 I = 51
85241
XDOT = 6826
934177 Wp = 103
01034
YDOT = 1951
184245 meter/sec RA = 34
44518 deg
ZDOT = -2867
625983 TA = 138
57648
MA = 138
52928
Ha = 227
056 n
mi
Hp = 222
068
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1897235
56 X = -500916
47
Y = -15986861
28 feet Y = -4878829
30 meter
Z = -15419007
27 Z = -4702334
79
XDOT = 22398
078007 XDOT = 6818
537618
YDOT = 6401
523113 feet/sec YDOT = 2027
480996 meter/sec
ZDOT = -9408
221729 ZDOT = -2834
483118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15675914
00 X = 4778018
59
Y = 3618108
39 feet Y = 1102799
44 meter
Z = -15430490
38 Z = -4703213
47
XDOT = -13233
047211 XDOT = -4033
432790
YDOT = 17917
482256 feet/sec YDOT = 5461
248592 meter/sec
ZDOT = -9257
221293 ZDOT = -2821
601050
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
60432527
00016717 00000-0 10270-3 0 9049
2 25544 51
6426 34
9635 0006442 219
2472 140
8212 15
50223243 36722
Satellite: ISS
Catalog Number: 25544
Epoch time: 19306
60432527 = yrday
fracday
Element set: 904
Inclination: 51
6426 deg
RA of node: 34
9635 deg
Eccentricity:
0006442
Arg of perigee: 219
2472 deg
Mean anomaly: 140
8212 deg
Mean motion: 15
50223243 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3672
Checksum: 285
Coasting Arc #6 (Orbit 3687)
---------------------------------------
Vector Time (GMT): 2019/307/13:59:45
869
Vector Time (MET): N/A
Weight (LBS) : 916487
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 518194
24 A = 6790580
17 meter
Y = 4698850
80 meter E =
0008257
Z = 4876595
99 I = 51
82220
XDOT = -7039
148619 Wp = 168
87102
YDOT = -1772
121664 meter/sec RA = 29
50118 deg
ZDOT = 2446
932116 TA = 257
10652
MA = 257
19877
Ha = 226
786 n
mi
Hp = 222
235
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1700112
35 X = 441923
73
Y = 15416177
17 feet Y = 4704219
03 meter
Z = 15999330
68 Z = 4878928
09
XDOT = -23094
319617 XDOT = -7030
695060
YDOT = -5814
047454 feet/sec YDOT = -1850
791190 meter/sec
ZDOT = 8027
992506 ZDOT = 2412
758630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15130894
65 X = -4611896
69
Y = -3358455
48 feet Y = -1023657
23 meter
Z = 16009506
13 Z = 4879697
47
XDOT = 12581
730321 XDOT = 3834
911402
YDOT = -19023
836049 feet/sec YDOT = -5798
465228 meter/sec
ZDOT = 7872
279864 ZDOT = 2399
470903
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
63574008
00016717 00000-0 10270-3 0 9055
2 25544 51
6431 29
8519 0006371 224
0273 136
0371 15
50250362 36888
Satellite: ISS
Catalog Number: 25544
Epoch time: 19307
63574008 = yrday
fracday
Element set: 905
Inclination: 51
6431 deg
RA of node: 29
8519 deg
Eccentricity:
0006371
Arg of perigee: 224
0273 deg
Mean anomaly: 136
0371 deg
Mean motion: 15
50250362 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3688
Checksum: 297
Coasting Arc #7 (Orbit 3698)
---------------------------------------
Vector Time (GMT): 2019/308/07:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916487
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1174344
44 A = 6791086
35 meter
Y = 4721701
10 meter E =
0008391
Z = 4739194
42 I = 51
80144
XDOT = -7069
292945 Wp = 163
56741
YDOT = -1026
502399 meter/sec RA = 25
99731 deg
ZDOT = 2765
397247 TA = 259
03807
MA = 259
13248
Ha = 226
709 n
mi
Hp = 222
272
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3852836
08 X = 1098437
08
Y = 15491145
36 feet Y = 4734408
95 meter
Z = 15548538
13 Z = 4744714
73
XDOT = -23193
218323 XDOT = -7070
721809
YDOT = -3367
790022 feet/sec YDOT = -1105
564261 meter/sec
ZDOT = 9072
825612 ZDOT = 2731
053389
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5203330
28 X = 1585975
07
Y = -15065727
87 feet Y = -4592033
86 meter
Z = 15573251
62 Z = 4746727
09
XDOT = 16663
277413 XDOT = 5078
966955
YDOT = 15002
344253 feet/sec YDOT = 4572
714528 meter/sec
ZDOT = 8916
267806 ZDOT = 2717
678427
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
34483745
00016717 00000-0 10270-3 0 9062
2 25544 51
6414 26
3342 0006391 225
3968 134
6662 15
50262263 36994
Satellite: ISS
Catalog Number: 25544
Epoch time: 19308
34483745 = yrday
fracday
Element set: 906
Inclination: 51
6414 deg
RA of node: 26
3342 deg
Eccentricity:
0006391
Arg of perigee: 225
3968 deg
Mean anomaly: 134
6662 deg
Mean motion: 15
50262263 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3699
Checksum: 320
Coasting Arc #8 (Orbit 3699)
---------------------------------------
Vector Time (GMT): 2019/308/09:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 931200
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4646170
71 A = 6798093
40 meter
Y = -4326718
30 meter E =
0008226
Z = -2416039
39 I = 51
82431
XDOT = 4948
025869 Wp = 182
88450
YDOT = -2316
999073 meter/sec RA = 25
55134 deg
ZDOT = -5373
167633 TA = 24
01544
MA = 23
97710
Ha = 226
723 n
mi
Hp = 222
248
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15243342
22 X = -4585706
86
Y = -14195270
02 feet Y = -4378336
95 meter
Z = -7926638
42 Z = -2438462
22
XDOT = 16233
680672 XDOT = 4999
667638
YDOT = -7601
702997 feet/sec YDOT = -2261
377919 meter/sec
ZDOT = -17628
502732 ZDOT = -5349
006312
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15173575
10 X = 4624905
69
Y = 14212766
07 feet Y = 4332051
10 meter
Z = -8028491
06 Z = -2447084
08
XDOT = -15324
401081 XDOT = -4670
877449
YDOT = 6477
964317 feet/sec YDOT = 1974
483524 meter/sec
ZDOT = -17518
061859 ZDOT = -5339
505255
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
40930122
00016717 00000-0 10270-3 0 9076
2 25544 51
6437 26
0152 0006422 224
8887 135
1745 15
50251487 37001
Satellite: ISS
Catalog Number: 25544
Epoch time: 19308
40930122 = yrday
fracday
Element set: 907
Inclination: 51
6437 deg
RA of node: 26
0152 deg
Eccentricity:
0006422
Arg of perigee: 224
8887 deg
Mean anomaly: 135
1745 deg
Mean motion: 15
50251487 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3700
Checksum: 291
Coasting Arc #9 (Orbit 3715)
---------------------------------------
Vector Time (GMT): 2019/309/09:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 931200
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4663868
39 A = 6797238
13 meter
Y = 4088677
59 meter E =
0008621
Z = 2776298
65 I = 51
79123
XDOT = -5156
700090 Wp = 102
58237
YDOT = 2382
442776 meter/sec RA = 20
60871 deg
ZDOT = 5138
730434 TA = 288
74666
MA = 288
84018
Ha = 226
591 n
mi
Hp = 222
343
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15301405
49 X = 4604315
11
Y = 13414296
57 feet Y = 4140499
27 meter
Z = 9108591
37 Z = 2798809
60
XDOT = -16918
307382 XDOT = -5207
919384
YDOT = 7816
413306 feet/sec YDOT = 2324
490509 meter/sec
ZDOT = 16859
351819 ZDOT = 5113
556438
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15453325
75 X = -4710173
69
Y = -13168050
39 feet Y = -4013621
76 meter
Z = 9210861
59 Z = 2807470
61
XDOT = 15943
583488 XDOT = 4859
604247
YDOT = -6963
429903 feet/sec YDOT = -2122
453434 meter/sec
ZDOT = 16744
290762 ZDOT = 5103
659824
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
44071199
00016717 00000-0 10270-3 0 9082
2 25544 51
6439 20
9042 0006411 228
3326 131
7276 15
50272663 37166
Satellite: ISS
Catalog Number: 25544
Epoch time: 19309
44071199 = yrday
fracday
Element set: 908
Inclination: 51
6439 deg
RA of node: 20
9042 deg
Eccentricity:
0006411
Arg of perigee: 228
3326 deg
Mean anomaly: 131
7276 deg
Mean motion: 15
50272663 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3716
Checksum: 302
Coasting Arc #10 (Orbit 3730)
---------------------------------------
Vector Time (GMT): 2019/310/09:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 931200
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4623113
06 A = 6796393
02 meter
Y = -3864501
74 meter E =
0004937
Z = -3137439
83 I = 51
75657
XDOT = 5372
352324 Wp = 187
00798
YDOT = -2478
147566 meter/sec RA = 15
66385 deg
ZDOT = -4867
867736 TA = 29
00943
MA = 28
98200
Ha = 226
407 n
mi
Hp = 222
531
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15167693
76 X = -4564315
34
Y = -12678811
47 feet Y = -3915871
92 meter
Z = -10293437
75 Z = -3159754
62
XDOT = 17625
827835 XDOT = 5423
310108
YDOT = -8130
405400 feet/sec YDOT = -2417
785243 meter/sec
ZDOT = -15970
694671 ZDOT = -4841
646738
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15511444
17 X = 4727888
18
Y = 12169992
92 feet Y = 3709413
84 meter
Z = -10394826
94 Z = -3168343
25
XDOT = -16565
370903 XDOT = -5049
125051
YDOT = 7585
870194 feet/sec YDOT = 2312
173235 meter/sec
ZDOT = -15850
856388 ZDOT = -4831
341027
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
40766063
00016717 00000-0 10270-3 0 9092
2 25544 51
6439 16
1131 0006432 232
2757 127
7811 15
50248438 37317
Satellite: ISS
Catalog Number: 25544
Epoch time: 19310
40766063 = yrday
fracday
Element set: 909
Inclination: 51
6439 deg
RA of node: 16
1131 deg
Eccentricity:
0006432
Arg of perigee: 232
2757 deg
Mean anomaly: 127
7811 deg
Mean motion: 15
50248438 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3731
Checksum: 293
Coasting Arc #11 (Orbit 3746)
---------------------------------------
Vector Time (GMT): 2019/311/09:10:00
000
Vector Time (MET): N/A
Weight (LBS) : 931200
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4569275
92 A = 6795389
42 meter
Y = 3645848
78 meter E =
0007913
Z = 3462925
17 I = 51
72194
XDOT = -5561
712358 Wp = 118
70907
YDOT = 2618
221281 meter/sec RA = 10
71546 deg
ZDOT = 4570
427457 TA = 281
77713
MA = 281
86589
Ha = 226
226 n
mi
Hp = 222
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14991062
73 X = 4511346
15
Y = 11961446
12 feet Y = 3696621
80 meter
Z = 11361303
07 Z = 3484980
58
XDOT = -18247
087790 XDOT = -5612
777652
YDOT = 8589
964832 feet/sec YDOT = 2555
740839 meter/sec
ZDOT = 14994
840738 ZDOT = 4543
286252
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15498687
93 X = -4724000
08
Y = -11194264
41 feet Y = -3412011
79 meter
Z = 11461521
67 Z = 3493471
80
XDOT = 17074
684836 XDOT = 5204
363938
YDOT = -8375
654865 feet/sec YDOT = -2552
899603 meter/sec
ZDOT = 14870
801240 ZDOT = 4532
620218
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
43906783
00016717 00000-0 10270-3 0 9103
2 25544 51
6448 11
0017 0006407 236
3392 123
7148 15
50281309 37476
Satellite: ISS
Catalog Number: 25544
Epoch time: 19311
43906783 = yrday
fracday
Element set: 910
Inclination: 51
6448 deg
RA of node: 11
0017 deg
Eccentricity:
0006407
Arg of perigee: 236
3392 deg
Mean anomaly: 123
7148 deg
Mean motion: 15
50281309 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3747
Checksum: 293
Coasting Arc #12 (Orbit 3754)
---------------------------------------
Vector Time (GMT): 2019/311/22:43:53
019
Vector Time (MET): N/A
Weight (LBS) : 931071
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5314107
14 A = 6795807
63 meter
Y = -2167962
26 meter E =
0002974
Z = -3640971
26 I = 51
70231
XDOT = 4704
224721 Wp = 197
58608
YDOT = 4150
640510 meter/sec RA = 7
87052 deg
ZDOT = 4390
815192 TA = 119
36840
MA = 119
33870
Ha = 225
937 n
mi
Hp = 223
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17434734
71 X = 5355641
09
Y = -7112737
08 feet Y = -2108304
01 meter
Z = -11945443
78 Z = -3615055
96
XDOT = 15433
808140 XDOT = 4636
132913
YDOT = 13617
586975 feet/sec YDOT = 4202
865838 meter/sec
ZDOT = 14405
561654 ZDOT = 4413
501477
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12396305
95 X = 3778394
05
Y = -14272603
64 feet Y = -4350289
59 meter
Z = -11827045
89 Z = -3604883
59
XDOT = 18799
355919 XDOT = 5730
043684
YDOT = 4295
184914 feet/sec YDOT = 1309
172362 meter/sec
ZDOT = 14508
600849 ZDOT = 4422
221539
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
95477238
00016717 00000-0 10270-3 0 9119
2 25544 51
6452 8
4501 0006580 251
1502 108
8940 15
50024087 37550
Satellite: ISS
Catalog Number: 25544
Epoch time: 19311
95477238 = yrday
fracday
Element set: 911
Inclination: 51
6452 deg
RA of node: 8
4501 deg
Eccentricity:
0006580
Arg of perigee: 251
1502 deg
Mean anomaly: 108
8940 deg
Mean motion: 15
50024087 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3755
Checksum: 293
Coasting Arc #13 (Orbit 3757)
---------------------------------------
Vector Time (GMT): 2019/312/03:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 931071
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1882345
92 A = 6790755
13 meter
Y = -4207464
41 meter E =
0006055
Z = -4992350
66 I = 51
67545
XDOT = 7320
341807 Wp = 78
34823
YDOT = -777
008311 meter/sec RA = 7
01218 deg
ZDOT = -2106
230383 TA = 171
13088
MA = 171
12018
Ha = 225
937 n
mi
Hp = 223
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6175675
61 X = -1810906
43
Y = -13804017
10 feet Y = -4228114
80 meter
Z = -16379103
23 Z = -5001320
95
XDOT = 24016
869444 XDOT = 7338
717555
YDOT = -2549
239864 feet/sec YDOT = -695
044376 meter/sec
ZDOT = -6910
204669 ZDOT = -2070
625624
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13541421
95 X = -4127425
41
Y = 6632640
41 feet Y = 2021628
80 meter
Z = -16419587
47 Z = -5004690
26
XDOT = -3062
392052 XDOT = -933
417098
YDOT = -22948
976175 feet/sec YDOT = -6994
847938 meter/sec
ZDOT = -6747
762416 ZDOT = -2056
717984
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19312
14819015
00016717 00000-0 10270-3 0 9125
2 25544 51
6411 7
4892 0006621 251
2063 108
8369 15
50015087 37584
Satellite: ISS
Catalog Number: 25544
Epoch time: 19312
14819015 = yrday
fracday
Element set: 912
Inclination: 51
6411 deg
RA of node: 7
4892 deg
Eccentricity:
0006621
Arg of perigee: 251
2063 deg
Mean anomaly: 108
8369 deg
Mean motion: 15
50015087 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3758
Checksum: 293
Coasting Arc #14 (Orbit 3773)
---------------------------------------
Vector Time (GMT): 2019/313/03:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 931071
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1822244
10 A = 6790427
66 meter
Y = 4102743
13 meter E =
0005087
Z = 5097799
61 I = 51
64012
XDOT = -7375
958626 Wp = 204
08840
YDOT = 1111
483925 meter/sec RA = 2
05802 deg
ZDOT = 1738
134887 TA = 229
06665
MA = 229
11070
Ha = 225
742 n
mi
Hp = 223
712
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5978491
14 X = 1751467
79
Y = 13460443
33 feet Y = 4122725
11 meter
Z = 16725064
32 Z = 5106479
59
XDOT = -24199
339323 XDOT = -7396
282438
YDOT = 3646
600804 feet/sec YDOT = 1028
887143 meter/sec
ZDOT = 5702
542280 ZDOT = 1702
255089
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13094075
47 X = 3991074
20
Y = -6645256
84 feet Y = -2025474
29 meter
Z = 16764230
27 Z = 5109737
39
XDOT = 4578
312025 XDOT = 1395
469505
YDOT = 23026
683409 feet/sec YDOT = 7018
533103 meter/sec
ZDOT = 5538
827312 ZDOT = 1688
234565
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19313
17975865
00016717 00000-0 10270-3 0 9136
2 25544 51
6406 2
3788 0006562 255
3117 104
7307 15
49971846 37742
Satellite: ISS
Catalog Number: 25544
Epoch time: 19313
17975865 = yrday
fracday
Element set: 913
Inclination: 51
6406 deg
RA of node: 2
3788 deg
Eccentricity:
0006562
Arg of perigee: 255
3117 deg
Mean anomaly: 104
7307 deg
Mean motion: 15
49971846 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3774
Checksum: 332
Coasting Arc #15 (Orbit 3788)
---------------------------------------
Vector Time (GMT): 2019/314/03:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 931071
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1741233
61 A = 6789913
37 meter
Y = -4028184
16 meter E =
0007429
Z = -5187776
00 I = 51
60469
XDOT = 7394
240478 Wp = 81
95561
YDOT = -1450
514540 meter/sec RA = 357
10116 deg
ZDOT = -1356
176633 TA = 174
98588
MA = 174
97843
Ha = 225
581 n
mi
Hp = 223
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5712708
70 X = -1670859
91
Y = -13215827
29 feet Y = -4047262
44 meter
Z = -17020262
48 Z = -5196063
50
XDOT = 24259
319154 XDOT = 7416
498713
YDOT = -4758
905971 feet/sec YDOT = -1367
702481 meter/sec
ZDOT = -4449
398401 ZDOT = -1320
203206
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12754247
38 X = -3887494
60
Y = 6583958
70 feet Y = 2006790
61 meter
Z = -17057641
35 Z = -5199169
08
XDOT = -6107
480772 XDOT = -1861
560139
YDOT = -22927
843460 feet/sec YDOT = -6988
406687 meter/sec
ZDOT = -4285
237131 ZDOT = -1306
140277
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19314
14685130
00016717 00000-0 10270-3 0 9148
2 25544 51
6399 357
5878 0006542 257
3478 102
6941 15
50017695 37890
Satellite: ISS
Catalog Number: 25544
Epoch time: 19314
14685130 = yrday
fracday
Element set: 914
Inclination: 51
6399 deg
RA of node: 357
5878 deg
Eccentricity:
0006542
Arg of perigee: 257
3478 deg
Mean anomaly: 102
6941 deg
Mean motion: 15
50017695 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3789
Checksum: 342
Coasting Arc #16 (Orbit 3804)
---------------------------------------
Vector Time (GMT): 2019/315/03:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 931071
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1661587
18 A = 6789753
39 meter
Y = 3975992
09 meter E =
0004440
Z = 5250447
99 I = 51
57061
XDOT = -7381
274057 Wp = 231
74373
YDOT = 1797
697487 meter/sec RA = 352
14132 deg
ZDOT = 972
455259 TA = 208
91637
MA = 208
94098
Ha = 225
335 n
mi
Hp = 223
678
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5451401
51 X = 1591498
51
Y = 13044593
48 feet Y = 3994181
22 meter
Z = 17225879
22 Z = 5258349
36
XDOT = -24216
778403 XDOT = -7405
551617
YDOT = 5897
957634 feet/sec YDOT = 1715
019117 meter/sec
ZDOT = 3190
470011 ZDOT = 936
539838
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12493056
68 X = 3807883
68
Y = -6524900
60 feet Y = -1988789
70 meter
Z = 17261498
17 Z = 5261304
64
XDOT = 7650
496215 XDOT = 2331
871246
YDOT = 22673
321499 feet/sec YDOT = 6910
828393 meter/sec
ZDOT = 3026
551589 ZDOT = 922
492924
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19315
17841732
00016717 00000-0 10270-3 0 9155
2 25544 51
6401 352
4767 0006546 261
9576 98
0832 15
49975430 38053
Satellite: ISS
Catalog Number: 25544
Epoch time: 19315
17841732 = yrday
fracday
Element set: 915
Inclination: 51
6401 deg
RA of node: 352
4767 deg
Eccentricity:
0006546
Arg of perigee: 261
9576 deg
Mean anomaly: 98
0832 deg
Mean motion: 15
49975430 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3805
Checksum: 332
Coasting Arc #17 (Orbit 3819)
---------------------------------------
Vector Time (GMT): 2019/316/03:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 931071
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1573860
72 A = 6789409
78 meter
Y = -3956112
57 meter E =
0008297
Z = -5295724
33 I = 51
53771
XDOT = 7327
848453 Wp = 86
39501
YDOT = -2139
770132 meter/sec RA = 347
17952 deg
ZDOT = -579
581685 TA = 178
05840
MA = 178
05518
Ha = 225
215 n
mi
Hp = 223
435
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5163585
04 X = -1503780
90
Y = -12979371
94 feet Y = -3973320
61 meter
Z = -17374423
67 Z = -5303199
67
XDOT = 24041
497548 XDOT = 7354
046728
YDOT = -7020
243214 feet/sec YDOT = -2057
678456 meter/sec
ZDOT = -1901
514715 ZDOT = -543
921115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12345956
51 X = -3763047
54
Y = 6444592
86 feet Y = 1964311
90 meter
Z = -17408098
26 Z = -5305988
35
XDOT = -9155
962386 XDOT = -2790
737335
YDOT = -22234
364612 feet/sec YDOT = -6777
034334 meter/sec
ZDOT = -1738
734845 ZDOT = -529
966381
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19316
14550609
00016717 00000-0 10270-3 0 9164
2 25544 51
6408 347
6857 0006403 264
6807 95
3613 15
50028721 38203
Satellite: ISS
Catalog Number: 25544
Epoch time: 19316
14550609 = yrday
fracday
Element set: 916
Inclination: 51
6408 deg
RA of node: 347
6857 deg
Eccentricity:
0006403
Arg of perigee: 264
6807 deg
Mean anomaly: 95
3613 deg
Mean motion: 15
50028721 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3820
Checksum: 311
Coasting Arc #18 (Orbit 3835)
---------------------------------------
Vector Time (GMT): 2019/317/03:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 931071
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1491399
79 A = 6789468
60 meter
Y = 3959510
86 meter E =
0003941
Z = 5313292
42 I = 51
50368
XDOT = -7244
480978 Wp = 263
01958
YDOT = 2479
032198 meter/sec RA = 342
21464 deg
ZDOT = 185
723360 TA = 185
20291
MA = 185
20701
Ha = 225
150 n
mi
Hp = 223
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4893043
93 X = 1421202
76
Y = 12990521
20 feet Y = 3975795
99 meter
Z = 17432061
75 Z = 5320366
99
XDOT = -23767
982212 XDOT = -7272
565976
YDOT = 8133
307736 feet/sec YDOT = 2397
862254 meter/sec
ZDOT = 609
328609 ZDOT = 150
463249
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12278796
47 X = 3742577
16
Y = -6388696
35 feet Y = -1947274
65 meter
Z = 17463906
01 Z = 5322998
55
XDOT = 10624
616126 XDOT = 3238
382995
YDOT = 21648
773385 feet/sec YDOT = 6598
546128 meter/sec
ZDOT = 448
348721 ZDOT = 136
656690
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19317
17706903
00016717 00000-0 10270-3 0 9179
2 25544 51
6394 342
5743 0006346 268
6313 91
4110 15
49978292 38368
Satellite: ISS
Catalog Number: 25544
Epoch time: 19317
17706903 = yrday
fracday
Element set: 917
Inclination: 51
6394 deg
RA of node: 342
5743 deg
Eccentricity:
0006346
Arg of perigee: 268
6313 deg
Mean anomaly: 91
4110 deg
Mean motion: 15
49978292 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3836
Checksum: 331
Coasting Arc #19 (Orbit 3842)
---------------------------------------
Vector Time (GMT): 2019/317/14:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 931071
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2132566
78 A = 6792834
63 meter
Y = -4611567
25 meter E =
0003816
Z = -4512395
06 I = 51
49981
XDOT = 6969
184986 Wp = 139
91426
YDOT = 118
984438 meter/sec RA = 339
76484 deg
ZDOT = 3170
693578 TA = 162
03612
MA = 162
02263
Ha = 225
182 n
mi
Hp = 223
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6996610
17 X = 2205895
51
Y = -15129813
80 feet Y = -4587309
11 meter
Z = -14804445
72 Z = -4501857
71
XDOT = 22864
780139 XDOT = 6951
934585
YDOT = 390
368891 feet/sec YDOT = 196
822144 meter/sec
ZDOT = 10402
537984 ZDOT = 3204
506358
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15592979
36 X = 4752740
11
Y = 6013032
40 feet Y = 1832772
27 meter
Z = -14755943
51 Z = -4497611
58
XDOT = 1653
953354 XDOT = 504
124982
YDOT = 21627
894806 feet/sec YDOT = 6592
182337 meter/sec
ZDOT = 10556
651757 ZDOT = 3217
667455
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19317
62837486
00016717 00000-0 10270-3 0 9181
2 25544 51
6397 340
3427 0006476 273
3536 86
6873 15
49998035 38437
Satellite: ISS
Catalog Number: 25544
Epoch time: 19317
62837486 = yrday
fracday
Element set: 918
Inclination: 51
6397 deg
RA of node: 340
3427 deg
Eccentricity:
0006476
Arg of perigee: 273
3536 deg
Mean anomaly: 86
6873 deg
Mean motion: 15
49998035 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3843
Checksum: 362
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