[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 9th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 20145 3042 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 995 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
There are no maneuvers
Coasting Arc #1 (Orbit 1373)
---------------------------------------
Vector Time (GMT): 2019/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5462747
99 A = 6794781
92 meter
Y = 2956029
23 meter E =
0012038
Z = -2746194
34 I = 51
94457
XDOT = -451
403144 Wp = 33
71287
YDOT = 5628
254753 meter/sec RA = 48
66914 deg
ZDOT = 5180
971310 TA = 295
38700
MA = 295
51158
Ha = 227
792 n
mi
Hp = 217
894
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17922401
54 X = 5442626
24
Y = 9698258
62 feet Y = 3017005
44 meter
Z = -9009823
95 Z = -2719706
88
XDOT = -1480
981443 XDOT = -539
472488
YDOT = 18465
402732 feet/sec YDOT = 5622
713568 meter/sec
ZDOT = 16997
937368 ZDOT = 5178
565597
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14096366
28 X = 4296572
44
Y = -14788724
79 feet Y = -4507603
32 meter
Z = -8889977
59 Z = -2709665
17
XDOT = 16313
919444 XDOT = 4972
482646
YDOT = 5380
293720 feet/sec YDOT = 1639
913526 meter/sec
ZDOT = 16986
343964 ZDOT = 5177
437640
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 19158
50547280
00016717 00000-0 10270-3 0 9002
2 25544 51
6439 49
3558 0007757 20
2429 339
9028 15
51188225 13746
Satellite: ISS
Catalog Number: 25544
Epoch time: 19158
50547280 = yrday
fracday
Element set: 900
Inclination: 51
6439 deg
RA of node: 49
3558 deg
Eccentricity:
0007757
Arg of perigee: 20
2429 deg
Mean anomaly: 339
9028 deg
Mean motion: 15
51188225 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1374
Checksum: 322
Coasting Arc #2 (Orbit 1389)
---------------------------------------
Vector Time (GMT): 2019/159/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5645911
17 A = 6796235
32 meter
Y = -3165317
43 meter E =
0016348
Z = 2062313
52 I = 51
92649
XDOT = 868
336284 Wp = 82
63967
YDOT = -5198
076706 meter/sec RA = 43
72999 deg
ZDOT = -5561
222198 TA = 74
67703
MA = 74
49641
Ha = 227
880 n
mi
Hp = 217
769
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18523330
63 X = -5620113
58
Y = -10384899
71 feet Y = -3228310
01 meter
Z = 6766120
48 Z = 2034950
20
XDOT = 2848
872322 XDOT = 953
411267
YDOT = -17054
057433 feet/sec YDOT = -5187
889896 meter/sec
ZDOT = -18245
479653 ZDOT = -5556
798274
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14650146
18 X = -4465364
56
Y = 15427021
42 feet Y = 4702156
13 meter
Z = 6642328
86 Z = 2024581
84
XDOT = -14667
493469 XDOT = -4470
652009
YDOT = -6024
689535 feet/sec YDOT = -1836
325370 meter/sec
ZDOT = -18224
775218 ZDOT = -5554
911487
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 19159
53626603
00016717 00000-0 10270-3 0 9014
2 25544 51
6440 44
2403 0007790 24
9626 335
1900 15
51162855 13904
Satellite: ISS
Catalog Number: 25544
Epoch time: 19159
53626603 = yrday
fracday
Element set: 901
Inclination: 51
6440 deg
RA of node: 44
2403 deg
Eccentricity:
0007790
Arg of perigee: 24
9626 deg
Mean anomaly: 335
1900 deg
Mean motion: 15
51162855 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1390
Checksum: 292
Coasting Arc #3 (Orbit 1404)
---------------------------------------
Vector Time (GMT): 2019/160/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5792418
65 A = 6797088
82 meter
Y = 3258000
28 meter E =
0016514
Z = -1389450
05 I = 51
90474
XDOT = -1315
269747 Wp = 32
42966
YDOT = 4804
358291 meter/sec RA = 38
78964 deg
ZDOT = 5827
711637 TA = 312
49797
MA = 312
63738
Ha = 227
938 n
mi
Hp = 217
557
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19003998
20 X = 5762305
40
Y = 10688977
30 feet Y = 3322606
95 meter
Z = -4558563
14 Z = -1361385
56
XDOT = -4315
189460 XDOT = -1397
203323
YDOT = 15762
330352 feet/sec YDOT = 4789
191227 meter/sec
ZDOT = 19119
788834 ZDOT = 5821
124143
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14785972
89 X = 4506764
54
Y = -16059966
94 feet Y = -4895077
92 meter
Z = -4431607
92 Z = -1350754
09
XDOT = 13144
947730 XDOT = 4006
580068
YDOT = 6877
095283 feet/sec YDOT = 2096
138642 meter/sec
ZDOT = 19089
311480 ZDOT = 5818
422139
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 19160
50263052
00016717 00000-0 10270-3 0 9029
2 25544 51
6439 39
4441 0007857 27
3406 332
8157 15
51197843 14057
Satellite: ISS
Catalog Number: 25544
Epoch time: 19160
50263052 = yrday
fracday
Element set: 902
Inclination: 51
6439 deg
RA of node: 39
4441 deg
Eccentricity:
0007857
Arg of perigee: 27
3406 deg
Mean anomaly: 332
8157 deg
Mean motion: 15
51197843 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1405
Checksum: 300
Coasting Arc #4 (Orbit 1420)
---------------------------------------
Vector Time (GMT): 2019/161/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5881775
82 A = 6797839
95 meter
Y = -3343843
93 meter E =
0014390
Z = 636188
36 I = 51
87984
XDOT = 1848
862121 Wp = 95
82036
YDOT = -4412
150480 meter/sec RA = 33
84987 deg
ZDOT = -5982
325422 TA = 77
34546
MA = 77
18460
Ha = 227
997 n
mi
Hp = 217
539
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19297164
76 X = -5847037
10
Y = -10970616
58 feet Y = -3409423
90 meter
Z = 2087232
14 Z = 607701
00
XDOT = 6065
820607 XDOT = 1927
121376
YDOT = -14475
559318 feet/sec YDOT = -4391
037038 meter/sec
ZDOT = -19627
051911 ZDOT = -5973
154727
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14841910
24 X = -4523814
24
Y = 16521924
48 feet Y = 5035882
58 meter
Z = 1958378
32 Z = 596913
71
XDOT = -11614
300864 XDOT = -3540
038903
YDOT = -8064
273114 feet/sec YDOT = -2457
990445 meter/sec
ZDOT = -19584
899095 ZDOT = -5969
477244
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 19161
53342036
00016717 00000-0 10270-3 0 9034
2 25544 51
6435 34
3288 0007752 31
9685 328
1935 15
51152714 14218
Satellite: ISS
Catalog Number: 25544
Epoch time: 19161
53342036 = yrday
fracday
Element set: 903
Inclination: 51
6435 deg
RA of node: 34
3288 deg
Eccentricity:
0007752
Arg of perigee: 31
9685 deg
Mean anomaly: 328
1935 deg
Mean motion: 15
51152714 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1421
Checksum: 296
Coasting Arc #5 (Orbit 1436)
---------------------------------------
Vector Time (GMT): 2019/162/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5912432
55 A = 6797828
26 meter
Y = 3332753
09 meter E =
0019986
Z = 75682
63 I = 51
85249
XDOT = -2393
513084 Wp = 41
24693
YDOT = 4089
025722 meter/sec RA = 28
90750 deg
ZDOT = 6030
447546 TA = 319
56547
MA = 319
71384
Ha = 227
982 n
mi
Hp = 217
313
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19397744
58 X = 5874357
70
Y = 10934229
31 feet Y = 3398657
16 meter
Z = 248302
58 Z = 104310
90
XDOT = -7852
733215 XDOT = -2468
352458
YDOT = 13415
438722 feet/sec YDOT = 4061
840754 meter/sec
ZDOT = 19784
932893 ZDOT = 6018
639354
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14536699
28 X = 4430785
94
Y = -16865146
66 feet Y = -5140496
70 meter
Z = 377785
15 Z = 115148
91
XDOT = 10353
535358 XDOT = 3155
757577
YDOT = 9409
075176 feet/sec YDOT = 2867
886114 meter/sec
ZDOT = 19730
851563 ZDOT = 6013
963556
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 19162
56420460
00016717 00000-0 10270-3 0 9047
2 25544 51
6439 29
2129 0007800 34
0289 326
1361 15
51209639 14374
Satellite: ISS
Catalog Number: 25544
Epoch time: 19162
56420460 = yrday
fracday
Element set: 904
Inclination: 51
6439 deg
RA of node: 29
2129 deg
Eccentricity:
0007800
Arg of perigee: 34
0289 deg
Mean anomaly: 326
1361 deg
Mean motion: 15
51209639 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1437
Checksum: 295
Coasting Arc #6 (Orbit 1451)
---------------------------------------
Vector Time (GMT): 2019/163/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5865505
69 A = 6797617
94 meter
Y = -3331243
78 meter E =
0011209
Z = -841656
56 I = 51
82160
XDOT = 2993
100017 Wp = 97
82622
YDOT = -3785
511875 meter/sec RA = 23
96349 deg
ZDOT = -5945
321385 TA = 91
23592
MA = 91
10749
Ha = 228
069 n
mi
Hp = 217
299
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19243785
09 X = -5823730
52
Y = -10929277
50 feet Y = -3396602
31 meter
Z = -2761340
43 Z = -870048
03
XDOT = 9819
881944 XDOT = 3064
087466
YDOT = -12419
658382 feet/sec YDOT = -3751
643403 meter/sec
ZDOT = -19505
647590 ZDOT = -5930
609920
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14209017
62 X = -4330908
57
Y = 16945519
11 feet Y = 5164994
23 meter
Z = -2889735
70 Z = -880791
44
XDOT = -9193
015982 XDOT = -2802
031271
YDOT = -10986
250993 feet/sec YDOT = -3348
609303 meter/sec
ZDOT = -19438
431194 ZDOT = -5924
833828
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 19163
53056550
00016717 00000-0 10270-3 0 9051
2 25544 51
6437 24
4167 0007775 37
5740 322
5954 15
51166430 14528
Satellite: ISS
Catalog Number: 25544
Epoch time: 19163
53056550 = yrday
fracday
Element set: 905
Inclination: 51
6437 deg
RA of node: 24
4167 deg
Eccentricity:
0007775
Arg of perigee: 37
5740 deg
Mean anomaly: 322
5954 deg
Mean motion: 15
51166430 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1452
Checksum: 303
Coasting Arc #7 (Orbit 1467)
---------------------------------------
Vector Time (GMT): 2019/164/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5747745
36 A = 6796764
79 meter
Y = 3261641
53 meter E =
0021337
Z = 1537907
28 I = 51
78691
XDOT = -3580
978989 Wp = 54
48167
YDOT = 3569
662346 meter/sec RA = 19
01656 deg
ZDOT = 5768
730356 TA = 322
28456
MA = 322
43394
Ha = 228
043 n
mi
Hp = 217
074
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18857432
27 X = 5703375
20
Y = 10700923
66 feet Y = 3325668
57 meter
Z = 5045627
57 Z = 1565720
53
XDOT = -11748
618730 XDOT = -3648
651340
YDOT = 11711
490637 feet/sec YDOT = 3529
238255 meter/sec
ZDOT = 18926
280695 ZDOT = 5751
171223
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13624841
62 X = 4152851
73
Y = -16828286
76 feet Y = -5129261
81 meter
Z = 5171395
54 Z = 1576241
36
XDOT = 8394
502551 XDOT = 2558
644378
YDOT = 12631
400505 feet/sec YDOT = 3850
050874 meter/sec
ZDOT = 18846
172232 ZDOT = 5744
313296
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 19164
56134650
00016717 00000-0 10270-3 0 9064
2 25544 51
6423 19
3009 0007810 41
1633 319
0106 15
51216660 14681
Satellite: ISS
Catalog Number: 25544
Epoch time: 19164
56134650 = yrday
fracday
Element set: 906
Inclination: 51
6423 deg
RA of node: 19
3009 deg
Eccentricity:
0007810
Arg of perigee: 41
1633 deg
Mean anomaly: 319
0106 deg
Mean motion: 15
51216660 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1468
Checksum: 279
Coasting Arc #8 (Orbit 1482)
---------------------------------------
Vector Time (GMT): 2019/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5545216
46 A = 6795670
11 meter
Y = -3223253
02 meter E =
0009588
Z = -2256422
53 I = 51
75075
XDOT = 4176
607938 Wp = 81
29263
YDOT = -3382
804878 meter/sec RA = 14
06721 deg
ZDOT = -5450
262315 TA = 123
70489
MA = 123
61345
Ha = 228
127 n
mi
Hp = 217
047
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18192967
40 X = -5497800
45
Y = -10574977
11 feet Y = -3284998
08 meter
Z = -7402961
05 Z = -2283244
64
XDOT = 13702
781948 XDOT = 4240
599591
YDOT = -11098
441200 feet/sec YDOT = -3335
740548 meter/sec
ZDOT = -17881
438041 ZDOT = -5429
818792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13109654
02 X = -3995822
54
Y = 16405518
10 feet Y = 5000401
92 meter
Z = -7524226
44 Z = -2293384
22
XDOT = -7767
601937 XDOT = -2367
565070
YDOT = -14338
251780 feet/sec YDOT = -4370
299143 meter/sec
ZDOT = -17788
268606 ZDOT = -5421
864271
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 19165
52770478
00016717 00000-0 10270-3 0 9076
2 25544 51
6418 14
5053 0007746 44
1060 316
0708 15
51185928 14830
Satellite: ISS
Catalog Number: 25544
Epoch time: 19165
52770478 = yrday
fracday
Element set: 907
Inclination: 51
6418 deg
RA of node: 14
5053 deg
Eccentricity:
0007746
Arg of perigee: 44
1060 deg
Mean anomaly: 316
0708 deg
Mean motion: 15
51185928 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1483
Checksum: 310
Coasting Arc #9 (Orbit 1498)
---------------------------------------
Vector Time (GMT): 2019/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5270886
45 A = 6794204
03 meter
Y = 3149762
98 meter E =
0020073
Z = 2882345
49 I = 51
71345
XDOT = -4740
870419 Wp = 68
71853
YDOT = 3284
286573 meter/sec RA = 9
11251 deg
ZDOT = 5059
299886 TA = 324
05789
MA = 324
19274
Ha = 228
051 n
mi
Hp = 216
938
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17292934
54 X = 5221272
22
Y = 10333868
04 feet Y = 3208427
84 meter
Z = 9456514
06 Z = 2907829
69
XDOT = -15554
036809 XDOT = -4801
819350
YDOT = 10775
218416 feet/sec YDOT = 3230
929226 meter/sec
ZDOT = 16598
752908 ZDOT = 5036
122837
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12468790
29 X = 3800487
28
Y = -15753466
03 feet Y = -4801656
45 meter
Z = 9571710
85 Z = 2917457
47
XDOT = 7518
820685 XDOT = 2291
736545
YDOT = 16014
102764 feet/sec YDOT = 4881
098522 meter/sec
ZDOT = 16493
196772 ZDOT = 5027
126376
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 19166
55848260
00016717 00000-0 10270-3 0 9086
2 25544 51
6417 9
3885 0007706 47
5157 312
6644 15
51218748 14999
Satellite: ISS
Catalog Number: 25544
Epoch time: 19166
55848260 = yrday
fracday
Element set: 908
Inclination: 51
6417 deg
RA of node: 9
3885 deg
Eccentricity:
0007706
Arg of perigee: 47
5157 deg
Mean anomaly: 312
6644 deg
Mean motion: 15
51218748 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1499
Checksum: 339
Coasting Arc #10 (Orbit 1513)
---------------------------------------
Vector Time (GMT): 2019/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4919256
02 A = 6792574
01 meter
Y = -3130756
88 meter E =
0012522
Z = -3499224
29 I = 51
67328
XDOT = 5262
395059 Wp = 64
21455
YDOT = -3210
493597 meter/sec RA = 4
15425 deg
ZDOT = -4532
866865 TA = 156
77504
MA = 156
71840
Ha = 228
261 n
mi
Hp = 216
725
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16139291
42 X = -4866884
03
Y = -10271512
08 feet Y = -3185473
98 meter
Z = -11480394
65 Z = -3522993
67
XDOT = 17265
075653 XDOT = 5319
922855
YDOT = -10533
115477 feet/sec YDOT = -3151
323332 meter/sec
ZDOT = -14871
610448 ZDOT = -4507
164850
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12003642
95 X = -3658710
37
Y = 14812676
50 feet Y = 4514903
80 meter
Z = -11587809
11 Z = -3531964
22
XDOT = -7446
547778 XDOT = -2269
707763
YDOT = -17558
098334 feet/sec YDOT = -5351
708372 meter/sec
ZDOT = -14754
611579 ZDOT = -4497
205609
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 19167
52483630
00016717 00000-0 10270-3 0 9091
2 25544 51
6401 4
5919 0007924 51
6417 308
5445 15
51207261 15143
Satellite: ISS
Catalog Number: 25544
Epoch time: 19167
52483630 = yrday
fracday
Element set: 909
Inclination: 51
6401 deg
RA of node: 4
5919 deg
Eccentricity:
0007924
Arg of perigee: 51
6417 deg
Mean anomaly: 308
5445 deg
Mean motion: 15
51207261 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1514
Checksum: 298
Coasting Arc #11 (Orbit 1529)
---------------------------------------
Vector Time (GMT): 2019/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4506328
01 A = 6790951
73 meter
Y = 3106219
29 meter E =
0017022
Z = 4003735
33 I = 51
63400
XDOT = -5737
310453 Wp = 81
93325
YDOT = 3211
323514 meter/sec RA = 359
19203 deg
ZDOT = 3954
021902 TA = 326
91913
MA = 327
02548
Ha = 228
157 n
mi
Hp = 216
781
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14784540
70 X = 4451810
52
Y = 10191008
18 feet Y = 3156306
62 meter
Z = 13135614
59 Z = 4025493
59
XDOT = -18823
197025 XDOT = -5792
000438
YDOT = 10535
838301 feet/sec YDOT = 3146
858344 meter/sec
ZDOT = 12972
512803 ZDOT = 3926
019949
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11537707
19 X = 3516693
15
Y = -13664871
23 feet Y = -4165052
75 meter
Z = 13233906
04 Z = 4033694
56
XDOT = 7702
315311 XDOT = 2347
665707
YDOT = 18981
318141 feet/sec YDOT = 5785
505769 meter/sec
ZDOT = 12845
083621 ZDOT = 3915
181488
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 19168
55561178
00016717 00000-0 10270-3 0 9101
2 25544 51
6395 359
4757 0007746 55
2363 304
9516 15
51204540 15303
Satellite: ISS
Catalog Number: 25544
Epoch time: 19168
55561178 = yrday
fracday
Element set: 910
Inclination: 51
6395 deg
RA of node: 359
4757 deg
Eccentricity:
0007746
Arg of perigee: 55
2363 deg
Mean anomaly: 304
9516 deg
Mean motion: 15
51204540 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1530
Checksum: 318
Coasting Arc #12 (Orbit 1544)
---------------------------------------
Vector Time (GMT): 2019/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4039739
54 A = 6789301
49 meter
Y = -3153633
05 meter E =
0017293
Z = -4470780
70 I = 51
59506
XDOT = 6122
801524 Wp = 64
60379
YDOT = -3219
845190 meter/sec RA = 354
22485 deg
ZDOT = -3263
905083 TA = 172
41785
MA = 172
39167
Ha = 228
327 n
mi
Hp = 216
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13253738
66 X = -3982457
98
Y = -10346565
13 feet Y = -3198487
11 meter
Z = -14667915
70 Z = -4490265
67
XDOT = 20087
931510 XDOT = 6174
205878
YDOT = -10563
796554 feet/sec YDOT = -3151
087687 meter/sec
ZDOT = -10708
350010 ZDOT = -3234
038668
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11336624
17 X = -3455403
05
Y = 12312817
44 feet Y = 3752946
76 meter
Z = -14755887
93 Z = -4497594
64
XDOT = -8071
412482 XDOT = -2460
166525
YDOT = -20091
316501 feet/sec YDOT = -6123
833270 meter/sec
ZDOT = -10572
466596 ZDOT = -3222
487818
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 19169
52196270
00016717 00000-0 10270-3 0 9117
2 25544 51
6393 354
6788 0007880 59
8259 300
3672 15
51213540 15454
Satellite: ISS
Catalog Number: 25544
Epoch time: 19169
52196270 = yrday
fracday
Element set: 911
Inclination: 51
6393 deg
RA of node: 354
6788 deg
Eccentricity:
0007880
Arg of perigee: 59
8259 deg
Mean anomaly: 300
3672 deg
Mean motion: 15
51213540 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1545
Checksum: 325
Coasting Arc #13 (Orbit 1560)
---------------------------------------
Vector Time (GMT): 2019/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3528571
83 A = 6787967
94 meter
Y = 3218376
86 meter E =
0013187
Z = 4812172
90 I = 51
55769
XDOT = -6456
870627 Wp = 89
26932
YDOT = 3275
884217 meter/sec RA = 349
25376 deg
ZDOT = 2537
799184 TA = 335
71835
MA = 335
78043
Ha = 228
298 n
mi
Hp = 216
624
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11576679
23 X = 3468946
08
Y = 10558979
20 feet Y = 3257501
55 meter
Z = 15787968
82 Z = 4829169
03
XDOT = -21183
958751 XDOT = -6505
349744
YDOT = 10747
651631 feet/sec YDOT = 3203
407435 meter/sec
ZDOT = 8326
112808 ZDOT = 2506
317201
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11233517
19 X = 3423976
04
Y = -10811691
26 feet Y = -3295403
50 meter
Z = 15864643
92 Z = 4835543
47
XDOT = 8657
497220 XDOT = 2638
805153
YDOT = 21030
585639 feet/sec YDOT = 6410
122503 meter/sec
ZDOT = 8182
900288 ZDOT = 2494
148008
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 19170
55273444
00016717 00000-0 10270-3 0 9122
2 25544 51
6396 349
5622 0007872 62
9378 297
2576 15
51191673 15612
Satellite: ISS
Catalog Number: 25544
Epoch time: 19170
55273444 = yrday
fracday
Element set: 912
Inclination: 51
6396 deg
RA of node: 349
5622 deg
Eccentricity:
0007872
Arg of perigee: 62
9378 deg
Mean anomaly: 297
2576 deg
Mean motion: 15
51191673 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1561
Checksum: 338
Coasting Arc #14 (Orbit 1575)
---------------------------------------
Vector Time (GMT): 2019/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2998766
76 A = 6786811
10 meter
Y = -3362749
30 meter E =
0021311
Z = -5094766
32 I = 51
52135
XDOT = 6669
438291 Wp = 73
32219
YDOT = -3313
100407 meter/sec RA = 344
27961 deg
ZDOT = -1738
915123 TA = 179
79242
MA = 179
79153
Ha = 228
447 n
mi
Hp = 216
346
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9838473
62 X = -2936193
36
Y = -11032642
06 feet Y = -3395932
87 meter
Z = -16715112
61 Z = -5109181
66
XDOT = 21881
359221 XDOT = 6714
437242
YDOT = -10869
751992 feet/sec YDOT = -3238
266174 meter/sec
ZDOT = -5705
102110 ZDOT = -1706
409076
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11443778
87 X = -3488063
80
Y = 9240080
54 feet Y = 2816376
55 meter
Z = -16780064
96 Z = -5114563
80
XDOT = -9238
977509 XDOT = -2816
040345
YDOT = -21533
954450 feet/sec YDOT = -6563
549316 meter/sec
ZDOT = -5557
248422 ZDOT = -1693
849319
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 19171
51908081
00016717 00000-0 10270-3 0 9132
2 25544 51
6395 344
7662 0008022 68
1556 292
0447 15
51215151 15760
Satellite: ISS
Catalog Number: 25544
Epoch time: 19171
51908081 = yrday
fracday
Element set: 913
Inclination: 51
6395 deg
RA of node: 344
7662 deg
Eccentricity:
0008022
Arg of perigee: 68
1556 deg
Mean anomaly: 292
0447 deg
Mean motion: 15
51215151 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1576
Checksum: 306
Coasting Arc #15 (Orbit 1591)
---------------------------------------
Vector Time (GMT): 2019/172/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931521
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2446868
95 A = 6786199
51 meter
Y = 3534702
59 meter E =
0010511
Z = 5241627
41 I = 51
48653
XDOT = -6833
202276 Wp = 84
91855
YDOT = 3364
649726 meter/sec RA = 339
30180 deg
ZDOT = 920
201274 TA = 356
26000
MA = 356
26785
Ha = 228
445 n
mi
Hp = 216
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8027785
27 X = 2381700
41
Y = 11596793
28 feet Y = 3561700
01 meter
Z = 17196940
31 Z = 5253355
51
XDOT = -22418
642637 XDOT = -6874
788673
YDOT = 11038
877055 feet/sec YDOT = 3288
003404 meter/sec
ZDOT = 3019
033051 ZDOT = 886
908015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11799932
55 X = 3596619
44
Y = -7607604
67 feet Y = -2318797
90 meter
Z = 17249685
50 Z = 5257704
14
XDOT = 9896
691553 XDOT = 3016
511585
YDOT = 21857
610906 feet/sec YDOT = 6662
199804 meter/sec
ZDOT = 2867
613273 ZDOT = 874
048526
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 19172
54985046
00016717 00000-0 10270-3 0 9143
2 25544 51
6389 339
6500 0007988 71
6344 288
5675 15
51177284 15926
Satellite: ISS
Catalog Number: 25544
Epoch time: 19172
54985046 = yrday
fracday
Element set: 914
Inclination: 51
6389 deg
RA of node: 339
6500 deg
Eccentricity:
0007988
Arg of perigee: 71
6344 deg
Mean anomaly: 288
5675 deg
Mean motion: 15
51177284 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1592
Checksum: 353
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