[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 14th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14706 8384 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 013 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
073/19:14:08
000 0
0 0
0 0
0
N/A 0
0 0
0 224
5
000/00:00:00
000 0
0 0
0 215
4
074/01:07:11
000 0
0 0
0 0
0
N/A 0
0 0
0 224
4
000/00:00:00
000 0
0 0
0 215
5
074/14:36:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
5
000/00:00:00
000 0
0 0
0 215
6
082/14:09:43
786 0
6 2
1 2
1
N/A 2
0 0
0 224
1
000/00:05:27
573 0
3 -0
0 217
1
082/22:28:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
1
000/00:00:00
000 0
0 0
0 217
1
087/06:36:30
000 0
0 0
0 0
0
N/A 0
0 0
0 223
9
000/00:00:00
000 0
0 0
0 217
1
Coasting Arc #1 (Orbit 38)
---------------------------------------
Vector Time (GMT): 2019/072/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900065
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3032882
76 A = 6793300
80 meter
Y = 6071878
82 meter E =
0014871
Z = 92194
84 I = 52
00212
XDOT = -4181
578740 Wp = 58
24698
YDOT = -2191
108601 meter/sec RA = 115
93394 deg
ZDOT = 6040
168000 TA = 302
74060
MA = 302
88385
Ha = 224
538 n
mi
Hp = 215
447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9950402
77 X = -3101002
65
Y = 19920862
28 feet Y = 6037582
13 meter
Z = 302476
50 Z = 77296
44
XDOT = -13719
090355 XDOT = -4186
106061
YDOT = -7188
676512 feet/sec YDOT = -2237
894873 meter/sec
ZDOT = 19816
824146 ZDOT = 6019
844659
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13276568
14 X = -4046697
97
Y = 17877932
95 feet Y = 5449193
96 meter
Z = 234549
23 Z = 71490
61
XDOT = -11080
544084 XDOT = -3377
349837
YDOT = -8526
608295 feet/sec YDOT = -2598
910208 meter/sec
ZDOT = 19725
053649 ZDOT = 6012
196352
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 19072
56422397
00016717 00000-0 10270-3 0 9004
2 25544 51
6391 116
6350 0003823 99
1163 261
0421 15
52762846 398
Satellite: ISS
Catalog Number: 25544
Epoch time: 19072
56422397 = yrday
fracday
Element set: 900
Inclination: 51
6391 deg
RA of node: 116
6350 deg
Eccentricity:
0003823
Arg of perigee: 99
1163 deg
Mean anomaly: 261
0421 deg
Mean motion: 15
52762846 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 39
Checksum: 296
Coasting Arc #2 (Orbit 53)
---------------------------------------
Vector Time (GMT): 2019/073/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900065
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3359698
60 A = 6792364
47 meter
Y = -5734006
89 meter E =
0012011
Z = -1385946
57 I = 52
01357
XDOT = 3546
669112 Wp = 131
17336
YDOT = 3479
002148 meter/sec RA = 110
99452 deg
ZDOT = -5836
406387 TA = 63
83892
MA = 63
71544
Ha = 224
492 n
mi
Hp = 215
374
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11022633
19 X = 3430300
31
Y = -18812358
57 feet Y = -5696041
70 meter
Z = -4547068
79 Z = -1369454
74
XDOT = 11636
053516 XDOT = 3535
852191
YDOT = 11414
049042 feet/sec YDOT = 3518
602712 meter/sec
ZDOT = -19148
314917 ZDOT = -5819
204541
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13879302
09 X = 4230411
28
Y = -16835849
60 feet Y = -5131566
96 meter
Z = -4471940
67 Z = -1363047
52
XDOT = 8590
787816 XDOT = 2618
472126
YDOT = 12111
895913 feet/sec YDOT = 3691
705874 meter/sec
ZDOT = -19070
778542 ZDOT = -5812
773300
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 19073
52957901
00016717 00000-0 10270-3 0 9016
2 25544 51
6396 111
8322 0003881 105
0061 255
1521 15
52813382 541
Satellite: ISS
Catalog Number: 25544
Epoch time: 19073
52957901 = yrday
fracday
Element set: 901
Inclination: 51
6396 deg
RA of node: 111
8322 deg
Eccentricity:
0003881
Arg of perigee: 105
0061 deg
Mean anomaly: 255
1521 deg
Mean motion: 15
52813382 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 54
Checksum: 281
Coasting Arc #3 (Orbit 58)
---------------------------------------
Vector Time (GMT): 2019/073/19:14:08
000
Vector Time (MET): N/A
Weight (LBS) : 900065
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4233392
61 A = 6781393
48 meter
Y = -405212
31 meter E =
0006949
Z = 5277033
26 I = 51
97986
XDOT = 1854
877061 Wp = 112
88578
YDOT = -7386
901108 meter/sec RA = 109
49863 deg
ZDOT = 917
224041 TA = 328
36363
MA = 328
40538
Ha = 224
465 n
mi
Hp = 215
431
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13889083
37 X = -4254179
50
Y = -1329436
71 feet Y = -452669
04 meter
Z = 17313101
23 Z = 5256418
69
XDOT = 6085
554661 XDOT = 1932
886288
YDOT = -24235
239857 feet/sec YDOT = -7365
722357 meter/sec
ZDOT = 3009
265228 ZDOT = 926
424091
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1065947
48 X = 324900
79
Y = 14027044
99 feet Y = 4275443
31 meter
Z = 17219851
27 Z = 5248610
67
XDOT = -23889
718869 XDOT = -7281
586311
YDOT = -1945
231888 feet/sec YDOT = -592
906679 meter/sec
ZDOT = 3051
547598 ZDOT = 930
111708
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 19073
85136387
00016717 00000-0 10270-3 0 9020
2 25544 51
6387 110
2329 0003551 104
6138 255
5407 15
52837301 594
Satellite: ISS
Catalog Number: 25544
Epoch time: 19073
85136387 = yrday
fracday
Element set: 902
Inclination: 51
6387 deg
RA of node: 110
2329 deg
Eccentricity:
0003551
Arg of perigee: 104
6138 deg
Mean anomaly: 255
5407 deg
Mean motion: 15
52837301 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 59
Checksum: 298
Coasting Arc #4 (Orbit 62)
---------------------------------------
Vector Time (GMT): 2019/074/01:07:11
000
Vector Time (MET): N/A
Weight (LBS) : 915337
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2942531
67 A = 6792628
62 meter
Y = 6002897
02 meter E =
0016204
Z = 1166088
83 I = 52
01830
XDOT = -3843
793339 Wp = 67
17519
YDOT = -3041
036147 meter/sec RA = 108
28617 deg
ZDOT = 5896
543334 TA = 305
41657
MA = 305
56778
Ha = 224
360 n
mi
Hp = 215
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9653975
30 X = -3015103
24
Y = 19694544
01 feet Y = 5969585
85 meter
Z = 3825750
75 Z = 1151618
69
XDOT = -12610
870536 XDOT = -3838
143849
YDOT = -9977
152712 feet/sec YDOT = -3083
988276 meter/sec
ZDOT = 19345
614612 ZDOT = 5877
885630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6746614
05 X = 2056367
96
Y = -20882007
72 feet Y = -6364835
95 meter
Z = 3759737
28 Z = 1145967
92
XDOT = 12519
451433 XDOT = 3815
928797
YDOT = 7548
165216 feet/sec YDOT = 2300
680758 meter/sec
ZDOT = 19261
451317 ZDOT = 5870
890361
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 19074
10879143
00016717 00000-0 10270-3 0 9034
2 25544 51
6373 108
9503 0003536 106
8449 253
3091 15
52804550 639
Satellite: ISS
Catalog Number: 25544
Epoch time: 19074
10879143 = yrday
fracday
Element set: 903
Inclination: 51
6373 deg
RA of node: 108
9503 deg
Eccentricity:
0003536
Arg of perigee: 106
8449 deg
Mean anomaly: 253
3091 deg
Mean motion: 15
52804550 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 63
Checksum: 297
Coasting Arc #5 (Orbit 70)
---------------------------------------
Vector Time (GMT): 2019/074/14:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 915337
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3872464
09 A = 6781360
92 meter
Y = 1642183
95 meter E =
0018479
Z = -5335177
71 I = 51
98598
XDOT = -2403
522147 Wp = 96
62971
YDOT = 7249
065498 meter/sec RA = 105
49182 deg
ZDOT = 486
091399 TA = 177
99839
MA = 177
99098
Ha = 224
479 n
mi
Hp = 215
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12704934
67 X = 3879727
99
Y = 5387742
63 feet Y = 1685528
94 meter
Z = -17503863
86 Z = -5316349
34
XDOT = -7885
571347 XDOT = -2486
765755
YDOT = 23783
023286 feet/sec YDOT = 7221
722210 meter/sec
ZDOT = 1594
788054 ZDOT = 474
213608
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13763827
17 X = 4195214
52
Y = -1992681
61 feet Y = -607369
36 meter
Z = -17418802
12 Z = -5309250
89
XDOT = 5346
607252 XDOT = 1629
645890
YDOT = 23446
762586 feet/sec YDOT = 7146
573236 meter/sec
ZDOT = 1540
384848 ZDOT = 469
509302
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 19074
62364840
00016717 00000-0 10270-3 0 9045
2 25544 51
6372 106
3898 0003823 107
6075 252
5494 15
52781170 719
Satellite: ISS
Catalog Number: 25544
Epoch time: 19074
62364840 = yrday
fracday
Element set: 904
Inclination: 51
6372 deg
RA of node: 106
3898 deg
Eccentricity:
0003823
Arg of perigee: 107
6075 deg
Mean anomaly: 252
5494 deg
Mean motion: 15
52781170 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 71
Checksum: 308
Coasting Arc #6 (Orbit 86)
---------------------------------------
Vector Time (GMT): 2019/075/14:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 915337
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3500741
73 A = 6782377
58 meter
Y = -2829772
70 meter E =
0008368
Z = 5066768
88 I = 51
99746
XDOT = 2796
346710 Wp = 77
00774
YDOT = -6884
250343 meter/sec RA = 100
53073 deg
ZDOT = -1908
299288 TA = 31
41885
MA = 31
36889
Ha = 224
526 n
mi
Hp = 215
452
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11485373
12 X = -3493449
44
Y = -9284031
18 feet Y = -2868879
42 meter
Z = 16623257
49 Z = 5049781
68
XDOT = 9174
365848 XDOT = 2882
389850
YDOT = -22586
123173 feet/sec YDOT = -6852
498637 meter/sec
ZDOT = -6260
824436 ZDOT = -1894
506551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14753825
85 X = -4496966
12
Y = -1724321
20 feet Y = -525573
10 meter
Z = 16546632
88 Z = 5043413
70
XDOT = -4283
844849 XDOT = -1305
715910
YDOT = -22961
556266 feet/sec YDOT = -6998
682350 meter/sec
ZDOT = -6197
770841 ZDOT = -1889
080552
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 19075
65335803
00016717 00000-0 10270-3 0 9057
2 25544 51
6372 101
2666 0003720 110
1329 250
0223 15
52807253 874
Satellite: ISS
Catalog Number: 25544
Epoch time: 19075
65335803 = yrday
fracday
Element set: 905
Inclination: 51
6372 deg
RA of node: 101
2666 deg
Eccentricity:
0003720
Arg of perigee: 110
1329 deg
Mean anomaly: 250
0223 deg
Mean motion: 15
52807253 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 87
Checksum: 275
Coasting Arc #7 (Orbit 101)
---------------------------------------
Vector Time (GMT): 2019/076/14:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 915337
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3174400
17 A = 6784640
57 meter
Y = 3938171
36 meter E =
0013338
Z = -4534961
25 I = 52
00931
XDOT = -3123
520714 Wp = 110
92999
YDOT = 6208
699031 meter/sec RA = 95
57407 deg
ZDOT = 3208
204740 TA = 191
18143
MA = 191
21110
Ha = 224
427 n
mi
Hp = 215
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10414698
71 X = 3152154
45
Y = 12920509
70 feet Y = 3973545
03 meter
Z = -14878481
80 Z = -4519595
76
XDOT = -10247
771371 XDOT = -3208
299416
YDOT = 20369
747476 feet/sec YDOT = 6173
295824 meter/sec
ZDOT = 10525
606104 ZDOT = 3192
825784
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15854026
06 X = 4832307
14
Y = 5109722
12 feet Y = 1557443
30 meter
Z = -14809299
05 Z = -4513874
35
XDOT = 2812
514241 XDOT = 857
254341
YDOT = 21547
712492 feet/sec YDOT = 6567
742768 meter/sec
ZDOT = 10455
421760 ZDOT = 3186
812552
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 19076
61871035
00016717 00000-0 10270-3 0 9067
2 25544 51
6367 96
4642 0003732 112
1212 248
0336 15
52783128 1027
Satellite: ISS
Catalog Number: 25544
Epoch time: 19076
61871035 = yrday
fracday
Element set: 906
Inclination: 51
6367 deg
RA of node: 96
4642 deg
Eccentricity:
0003732
Arg of perigee: 112
1212 deg
Mean anomaly: 248
0336 deg
Mean motion: 15
52783128 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 102
Checksum: 288
Coasting Arc #8 (Orbit 117)
---------------------------------------
Vector Time (GMT): 2019/077/14:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 915337
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2843550
28 A = 6787369
57 meter
Y = -4910867
06 meter E =
0014966
Z = 3710343
15 I = 52
02059
XDOT = 3452
017981 Wp = 92
09673
YDOT = -5294
722644 meter/sec RA = 90
62197 deg
ZDOT = -4347
775770 TA = 43
93433
MA = 43
81544
Ha = 224
387 n
mi
Hp = 215
533
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9329233
20 X = -2806446
70
Y = -16111768
57 feet Y = -4942457
83 meter
Z = 12173041
84 Z = 3696621
06
XDOT = 11325
518310 XDOT = 3532
087216
YDOT = -17371
137284 feet/sec YDOT = -5255
672466 meter/sec
ZDOT = -14264
356200 ZDOT = -4330
812509
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16808327
43 X = -5123178
20
Y = -8099442
00 feet Y = -2468709
92 meter
Z = 12111391
10 Z = 3691552
01
XDOT = -830
387008 XDOT = -253
101960
YDOT = -19562
896537 feet/sec YDOT = -5962
770865 meter/sec
ZDOT = -14187
075924 ZDOT = -4324
220742
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 19077
64841816
00016717 00000-0 10270-3 0 9076
2 25544 51
6364 91
3407 0003616 116
2420 243
9104 15
52816703 1184
Satellite: ISS
Catalog Number: 25544
Epoch time: 19077
64841816 = yrday
fracday
Element set: 907
Inclination: 51
6364 deg
RA of node: 91
3407 deg
Eccentricity:
0003616
Arg of perigee: 116
2420 deg
Mean anomaly: 243
9104 deg
Mean motion: 15
52816703 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 118
Checksum: 294
Coasting Arc #9 (Orbit 132)
---------------------------------------
Vector Time (GMT): 2019/078/14:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 915337
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2548740
75 A = 6790118
86 meter
Y = 5683838
20 meter E =
0007359
Z = -2707312
79 I = 52
02967
XDOT = -3764
182220 Wp = 82
12125
YDOT = 4164
103222 meter/sec RA = 85
67583 deg
ZDOT = 5211
643275 TA = 247
50569
MA = 247
58363
Ha = 224
354 n
mi
Hp = 215
585
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8362010
34 X = 2498143
45
Y = 18647763
14 feet Y = 5712056
78 meter
Z = -8882259
82 Z = -2695055
72
XDOT = -12349
679200 XDOT = -3835
781507
YDOT = 13661
755979 feet/sec YDOT = 4121
609778 meter/sec
ZDOT = 17098
567176 ZDOT = 5193
184200
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17588074
97 X = 5360845
25
Y = 10454419
14 feet Y = 3186506
95 meter
Z = -8827319
30 Z = -2690566
92
XDOT = -1620
946518 XDOT = -494
064499
YDOT = 17057
083905 feet/sec YDOT = 5198
999174 meter/sec
ZDOT = 17014
615921 ZDOT = 5186
054933
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 19078
61376724
00016717 00000-0 10270-3 0 9086
2 25544 51
6372 86
5377 0003695 118
6256 241
5267 15
52802621 1330
Satellite: ISS
Catalog Number: 25544
Epoch time: 19078
61376724 = yrday
fracday
Element set: 908
Inclination: 51
6372 deg
RA of node: 86
5377 deg
Eccentricity:
0003695
Arg of perigee: 118
6256 deg
Mean anomaly: 241
5267 deg
Mean motion: 15
52802621 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 133
Checksum: 320
Coasting Arc #10 (Orbit 148)
---------------------------------------
Vector Time (GMT): 2019/079/14:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 915337
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2207569
61 A = 6792210
78 meter
Y = -6235397
26 meter E =
0017448
Z = 1505419
30 I = 52
03333
XDOT = 4118
087490 Wp = 118
84947
YDOT = -2868
576150 meter/sec RA = 80
73401 deg
ZDOT = -5800
280370 TA = 44
80167
MA = 44
66091
Ha = 224
290 n
mi
Hp = 215
597
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7242682
44 X = -2144991
96
Y = -20457340
11 feet Y = -6259733
75 meter
Z = 4939039
70 Z = 1494848
72
XDOT = 13510
785727 XDOT = 4178
032870
YDOT = -9411
339076 feet/sec YDOT = -2822
190432 meter/sec
ZDOT = -19029
791240 ZDOT = -5780
130498
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17900483
33 X = -5456067
32
Y = -12288057
65 feet Y = -3745399
97 meter
Z = 4891795
38 Z = 1491019
23
XDOT = 4617
248466 XDOT = 1407
337333
YDOT = -14321
306408 feet/sec YDOT = -4365
134193 meter/sec
ZDOT = -18938
306490 ZDOT = -5772
395818
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 19079
64347090
00016717 00000-0 10270-3 0 9095
2 25544 51
6374 81
4137 0003582 121
4268 238
7234 15
52815993 1495
Satellite: ISS
Catalog Number: 25544
Epoch time: 19079
64347090 = yrday
fracday
Element set: 909
Inclination: 51
6374 deg
RA of node: 81
4137 deg
Eccentricity:
0003582
Arg of perigee: 121
4268 deg
Mean anomaly: 238
7234 deg
Mean motion: 15
52815993 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 149
Checksum: 324
Coasting Arc #11 (Orbit 163)
---------------------------------------
Vector Time (GMT): 2019/080/14:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 915337
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1862009
01 A = 6793090
70 meter
Y = 6523594
69 meter E =
0012557
Z = -261818
26 I = 52
02957
XDOT = -4476
337548 Wp = 59
94443
YDOT = 1510
986754 meter/sec RA = 75
79584 deg
ZDOT = 6035
258610 TA = 297
25161
MA = 297
37947
Ha = 224
230 n
mi
Hp = 215
624
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6108953
45 X = 1790193
70
Y = 21402869
71 feet Y = 6544015
39 meter
Z = -858983
78 Z = -252948
73
XDOT = -14686
146810 XDOT = -4522
216897
YDOT = 4957
305624 feet/sec YDOT = 1460
673552 meter/sec
ZDOT = 19800
717226 ZDOT = 6013
402733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17749634
33 X = 5410088
54
Y = 13432011
40 feet Y = 4094077
08 meter
Z = -819480
40 Z = -249777
62
XDOT = -7884
459748 XDOT = -2403
183331
YDOT = 11574
325375 feet/sec YDOT = 3527
854374 meter/sec
ZDOT = 19701
641332 ZDOT = 6005
060278
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 19080
60881729
00016717 00000-0 10270-3 0 9107
2 25544 51
6370 76
6111 0003614 126
4413 233
7072 15
52825043 1641
Satellite: ISS
Catalog Number: 25544
Epoch time: 19080
60881729 = yrday
fracday
Element set: 910
Inclination: 51
6370 deg
RA of node: 76
6111 deg
Eccentricity:
0003614
Arg of perigee: 126
4413 deg
Mean anomaly: 233
7072 deg
Mean motion: 15
52825043 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 164
Checksum: 282
Coasting Arc #12 (Orbit 179)
---------------------------------------
Vector Time (GMT): 2019/081/14:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 915337
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1411944
44 A = 6792659
02 meter
Y = -6556055
27 meter E =
0013000
Z = -1045225
82 I = 52
02064
XDOT = 4860
452040 Wp = 138
26950
YDOT = -109
964566 meter/sec RA = 70
85722 deg
ZDOT = -5927
649416 TA = 52
99680
MA = 52
87790
Ha = 224
152 n
mi
Hp = 215
713
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4632363
65 X = -1333450
71
Y = -21509367
70 feet Y = -6571405
88 meter
Z = -3429218
58 Z = -1051892
98
XDOT = 15946
364961 XDOT = 4890
113657
YDOT = -360
776134 feet/sec YDOT = -55
446541 meter/sec
ZDOT = -19447
668689 ZDOT = -5903
967136
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16856311
59 X = -5137803
77
Y = -14134112
96 feet Y = -4308077
63 meter
Z = -3458734
19 Z = -1054222
18
XDOT = 11427
960287 XDOT = 3483
242296
YDOT = -8937
294920 feet/sec YDOT = -2724
087492 meter/sec
ZDOT = -19340
467252 ZDOT = -5894
974418
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 19081
63851840
00016717 00000-0 10270-3 0 9113
2 25544 51
6388 71
4873 0003466 129
8518 230
2940 15
52821383 1803
Satellite: ISS
Catalog Number: 25544
Epoch time: 19081
63851840 = yrday
fracday
Element set: 911
Inclination: 51
6388 deg
RA of node: 71
4873 deg
Eccentricity:
0003466
Arg of perigee: 129
8518 deg
Mean anomaly: 230
2940 deg
Mean motion: 15
52821383 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 180
Checksum: 310
Coasting Arc #13 (Orbit 194)
---------------------------------------
Vector Time (GMT): 2019/082/14:12:27
573
Vector Time (MET): N/A
Weight (LBS) : 915117
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4608236
40 A = 6784273
72 meter
Y = 910977
42 meter E =
0013350
Z = -4907506
42 I = 51
97685
XDOT = 1142
449180 Wp = 113
98539
YDOT = 7176
920085 meter/sec RA = 65
95880 deg
ZDOT = 2404
908622 TA = 179
51906
MA = 179
51777
Ha = 224
126 n
mi
Hp = 217
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15118885
84 X = 4621545
10
Y = 2988771
06 feet Y = 962583
79 meter
Z = -16100742
86 Z = -4885089
07
XDOT = 3748
192848 XDOT = 1050
428178
YDOT = 23546
325737 feet/sec YDOT = 7189
181508 meter/sec
ZDOT = 7890
120151 ZDOT = 2410
233889
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14396153
04 X = 4387947
45
Y = -5789486
32 feet Y = -1764635
43 meter
Z = -15999375
23 Z = -4876609
57
XDOT = 15504
379705 XDOT = 4725
734934
YDOT = 16683
068160 feet/sec YDOT = 5084
999175 meter/sec
ZDOT = 7913
480694 ZDOT = 2412
028916
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 19082
60386100
00016717 00000-0 10270-3 0 9124
2 25544 51
6388 66
6845 0002132 155
5541 204
5712 15
52416939 1953
Satellite: ISS
Catalog Number: 25544
Epoch time: 19082
60386100 = yrday
fracday
Element set: 912
Inclination: 51
6388 deg
RA of node: 66
6845 deg
Eccentricity:
0002132
Arg of perigee: 155
5541 deg
Mean anomaly: 204
5712 deg
Mean motion: 15
52416939 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 195
Checksum: 301
Coasting Arc #14 (Orbit 200)
---------------------------------------
Vector Time (GMT): 2019/082/22:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 915117
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1627890
19 A = 6785663
48 meter
Y = 4780613
10 meter E =
0010466
Z = 4527375
93 I = 51
97535
XDOT = -5076
466475 Wp = 120
93820
YDOT = -4771
787067 meter/sec RA = 64
29521 deg
ZDOT = 3202
663017 TA = 296
98893
MA = 297
09576
Ha = 224
137 n
mi
Hp = 217
057
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5340847
08 X = -1703218
92
Y = 15684426
18 feet Y = 4761988
19 meter
Z = 14853595
57 Z = 4519284
75
XDOT = -16655
073738 XDOT = -5038
286510
YDOT = -15655
469379 feet/sec YDOT = -4828
341844 meter/sec
ZDOT = 10507
424595 ZDOT = 3178
096627
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11086167
89 X = 3379063
97
Y = -12358158
38 feet Y = -3766766
68 meter
Z = 14816476
52 Z = 4516062
04
XDOT = 8462
821538 XDOT = 2579
468005
YDOT = 20098
872652 feet/sec YDOT = 6126
136384 meter/sec
ZDOT = 10396
734648 ZDOT = 3168
924721
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 19082
99009525
00016717 00000-0 10270-3 0 9130
2 25544 51
6372 64
7618 0002182 160
2996 199
8241 15
52419604 2018
Satellite: ISS
Catalog Number: 25544
Epoch time: 19082
99009525 = yrday
fracday
Element set: 913
Inclination: 51
6372 deg
RA of node: 64
7618 deg
Eccentricity:
0002182
Arg of perigee: 160
2996 deg
Mean anomaly: 199
8241 deg
Mean motion: 15
52419604 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 201
Checksum: 312
Coasting Arc #15 (Orbit 215)
---------------------------------------
Vector Time (GMT): 2019/083/22:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 915117
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2236586
99 A = 6783598
97 meter
Y = -3964339
50 meter E =
0013260
Z = -5041513
46 I = 51
95281
XDOT = 5036
680054 Wp = 85
46028
YDOT = 5401
391730 meter/sec RA = 59
33907 deg
ZDOT = -2016
422880 TA = 165
01957
MA = 164
98026
Ha = 224
135 n
mi
Hp = 217
060
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7337883
84 X = 2305240
09
Y = -13006363
19 feet Y = -3938944
98 meter
Z = -16540398
50 Z = -5030481
85
XDOT = 16524
540859 XDOT = 4985
700518
YDOT = 17721
101475 feet/sec YDOT = 5457
430195 meter/sec
ZDOT = -6615
560629 ZDOT = -1992
080775
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11743196
73 X = -3579326
36
Y = 9315067
81 feet Y = 2839232
67 meter
Z = -16490046
92 Z = -5026166
30
XDOT = -8131
012253 XDOT = -2478
332535
YDOT = -21747
099650 feet/sec YDOT = -6628
515973 meter/sec
ZDOT = -6505
968131 ZDOT = -1983
019086
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 19083
95568255
00016717 00000-0 10270-3 0 9148
2 25544 51
6369 59
9606 0002409 160
0303 200
0943 15
52432913 2167
Satellite: ISS
Catalog Number: 25544
Epoch time: 19083
95568255 = yrday
fracday
Element set: 914
Inclination: 51
6369 deg
RA of node: 59
9606 deg
Eccentricity:
0002409
Arg of perigee: 160
0303 deg
Mean anomaly: 200
0943 deg
Mean motion: 15
52432913 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 216
Checksum: 299
Coasting Arc #16 (Orbit 231)
---------------------------------------
Vector Time (GMT): 2019/084/22:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 915117
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2877616
85 A = 6782579
98 meter
Y = 3105804
07 meter E =
0004996
Z = 5296208
81 I = 51
93143
XDOT = -4910
830238 Wp = 137
05928
YDOT = -5841
156907 meter/sec RA = 54
37863 deg
ZDOT = 753
166425 TA = 305
75074
MA = 305
79719
Ha = 224
221 n
mi
Hp = 217
125
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9441000
18 X = -2937859
05
Y = 10189645
90 feet Y = 3073288
05 meter
Z = 17376013
15 Z = 5282083
88
XDOT = -16111
647762 XDOT = -4848
806254
YDOT = -19163
900613 feet/sec YDOT = -5895
726399 meter/sec
ZDOT = 2471
018455 ZDOT = 729
462435
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12552534
28 X = 3826012
45
Y = -6133881
62 feet Y = -1869607
12 meter
Z = 17311746
89 Z = 5276620
45
XDOT = 7826
239608 XDOT = 2385
437833
YDOT = 22725
818965 feet/sec YDOT = 6926
829621 meter/sec
ZDOT = 2364
377192 ZDOT = 720
662168
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 19084
98564162
00016717 00000-0 10270-3 0 9156
2 25544 51
6372 54
8388 0002343 164
4609 195
6615 15
52392167 2325
Satellite: ISS
Catalog Number: 25544
Epoch time: 19084
98564162 = yrday
fracday
Element set: 915
Inclination: 51
6372 deg
RA of node: 54
8388 deg
Eccentricity:
0002343
Arg of perigee: 164
4609 deg
Mean anomaly: 195
6615 deg
Mean motion: 15
52392167 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 232
Checksum: 325
Coasting Arc #17 (Orbit 246)
---------------------------------------
Vector Time (GMT): 2019/085/22:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 915117
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3577633
46 A = 6782387
53 meter
Y = -2237003
30 meter E =
0015648
Z = -5323531
93 I = 51
91219
XDOT = 4627
219855 Wp = 102
74903
YDOT = 6071
844474 meter/sec RA = 49
41594 deg
ZDOT = 556
249034 TA = 172
56040
MA = 172
53715
Ha = 224
051 n
mi
Hp = 217
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11737642
59 X = 3628241
11
Y = -7339249
69 feet Y = -2196713
02 meter
Z = -17465655
94 Z = -5306030
11
XDOT = 15181
167503 XDOT = 4556
276918
YDOT = 19920
749586 feet/sec YDOT = 6123
192645 meter/sec
ZDOT = 1824
964022 ZDOT = 578
553684
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13640442
66 X = -4157606
92
Y = 2888671
19 feet Y = 880466
98 meter
Z = -17386197
97 Z = -5299313
14
XDOT = -7309
274683 XDOT = -2227
866924
YDOT = -22887
929639 feet/sec YDOT = -6976
240954 meter/sec
ZDOT = 1925
232302 ZDOT = 586
810806
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 19085
95122369
00016717 00000-0 10270-3 0 9164
2 25544 51
6385 50
0375 0002449 165
6433 194
4789 15
52442457 2471
Satellite: ISS
Catalog Number: 25544
Epoch time: 19085
95122369 = yrday
fracday
Element set: 916
Inclination: 51
6385 deg
RA of node: 50
0375 deg
Eccentricity:
0002449
Arg of perigee: 165
6433 deg
Mean anomaly: 194
4789 deg
Mean motion: 15
52442457 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 247
Checksum: 329
Coasting Arc #18 (Orbit 262)
---------------------------------------
Vector Time (GMT): 2019/086/22:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 915117
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4266900
04 A = 6783528
95 meter
Y = 1396682
12 meter E =
0005139
Z = 5080999
92 I = 51
89187
XDOT = -4203
936213 Wp = 81
87336
YDOT = -6144
888576 meter/sec RA = 44
45240 deg
ZDOT = -1838
941093 TA = 25
88226
MA = 25
85656
Ha = 224
225 n
mi
Hp = 217
154
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13999015
87 X = -4306881
59
Y = 4582290
41 feet Y = 1348743
36 meter
Z = 16669947
24 Z = 5060175
82
XDOT = -13792
441644 XDOT = -4125
977361
YDOT = -20160
395589 feet/sec YDOT = -6191
464128 meter/sec
ZDOT = -6033
271301 ZDOT = -1859
172505
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14834492
78 X = 4521553
40
Y = 214598
52 feet Y = 65409
63 meter
Z = 16575546
54 Z = 5052226
58
XDOT = 6526
766380 XDOT = 1989
358393
YDOT = 22437
895962 feet/sec YDOT = 6839
070689 meter/sec
ZDOT = -6124
135933 ZDOT = -1866
636632
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 19086
98117836
00016717 00000-0 10270-3 0 9172
2 25544 51
6372 44
9157 0002494 168
8636 191
2571 15
52402962 2636
Satellite: ISS
Catalog Number: 25544
Epoch time: 19086
98117836 = yrday
fracday
Element set: 917
Inclination: 51
6372 deg
RA of node: 44
9157 deg
Eccentricity:
0002494
Arg of perigee: 168
8636 deg
Mean anomaly: 191
2571 deg
Mean motion: 15
52402962 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 263
Checksum: 332
Coasting Arc #19 (Orbit 267)
---------------------------------------
Vector Time (GMT): 2019/087/06:36:30
000
Vector Time (MET): N/A
Weight (LBS) : 915117
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3311054
03 A = 6792004
78 meter
Y = -5479973
03 meter E =
0007867
Z = -2258830
40 I = 51
91647
XDOT = 5285
135754 Wp = 144
55060
YDOT = -945
693713 meter/sec RA = 42
80979 deg
ZDOT = -5468
578986 TA = 60
45367
MA = 60
37527
Ha = 223
921 n
mi
Hp = 217
101
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10863038
16 X = -3238557
24
Y = -17978914
14 feet Y = -5516594
31 meter
Z = -7410860
88 Z = -2274737
82
XDOT = 17339
684231 XDOT = 5321
881163
YDOT = -3102
669663 feet/sec YDOT = -886
386451 meter/sec
ZDOT = -17941
532107 ZDOT = -5442
816606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14923537
63 X = 4548694
27
Y = -14746934
94 feet Y = -4494865
77 meter
Z = -7482228
63 Z = -2280583
29
XDOT = 6056
945467 XDOT = 1846
156978
YDOT = 15147
375212 feet/sec YDOT = 4616
919965 meter/sec
ZDOT = -17824
833805 ZDOT = -5433
009344
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 19087
30303696
00016717 00000-0 10270-3 0 9181
2 25544 51
6410 43
3190 0002238 169
5666 190
5533 15
52451331 2685
Satellite: ISS
Catalog Number: 25544
Epoch time: 19087
30303696 = yrday
fracday
Element set: 918
Inclination: 51
6410 deg
RA of node: 43
3190 deg
Eccentricity:
0002238
Arg of perigee: 169
5666 deg
Mean anomaly: 190
5533 deg
Mean motion: 15
52451331 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 268
Checksum: 300
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