[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 6th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19998 2692 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 748 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
218/16:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 225
4
000/00:00:00
000 0
0 0
0 221
2
220/06:28:00
000 0
0 0
0 0
0
N/A 0
0 0
0 225
2
000/00:00:00
000 0
0 0
0 221
4
227/05:42:47
315 0
3 1
8 1
8
N/A 1
7 0
0 223
7
000/00:09:34
629 0
4 -0
0 222
9
227/08:44:47
258 0
6 1
8 1
8
N/A 1
7 -0
0 224
0
000/00:09:34
515 0
1 -0
0 223
7
Coasting Arc #1 (Orbit 2289)
---------------------------------------
Vector Time (GMT): 2019/217/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952577
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4749332
44 A = 6789620
13 meter
Y = -1642432
28 meter E =
0004984
Z = -4569353
45 I = 51
98043
XDOT = -612
365741 Wp = 101
30020
YDOT = 6958
463390 meter/sec RA = 115
61534 deg
ZDOT = -3141
518741 TA = 137
34406
MA = 137
30535
Ha = 225
591 n
mi
Hp = 221
085
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15581799
34 X = 4789540
65
Y = -5388557
36 feet Y = -1589097
06 meter
Z = -14991317
10 Z = -4546185
68
XDOT = -2009
073955 XDOT = -674
872249
YDOT = 22829
604297 feet/sec YDOT = 6951
266014 meter/sec
ZDOT = -10306
820017 ZDOT = -3144
645099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14618084
92 X = -4455592
28
Y = -7829084
03 feet Y = -2386304
81 meter
Z = -14885753
12 Z = -4537177
55
XDOT = 17482
135862 XDOT = 5328
555011
YDOT = -13041
147438 feet/sec YDOT = -3974
941739 meter/sec
ZDOT = -10321
566793 ZDOT = -3146
013558
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 19217
52178050
00016717 00000-0 10270-3 0 9005
2 25544 51
6434 116
5103 0006074 224
4396 135
6268 15
51043523 22902
Satellite: ISS
Catalog Number: 25544
Epoch time: 19217
52178050 = yrday
fracday
Element set: 900
Inclination: 51
6434 deg
RA of node: 116
5103 deg
Eccentricity:
0006074
Arg of perigee: 224
4396 deg
Mean anomaly: 135
6268 deg
Mean motion: 15
51043523 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2290
Checksum: 281
Coasting Arc #2 (Orbit 2305)
---------------------------------------
Vector Time (GMT): 2019/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 952577
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4549820
14 A = 6788422
24 meter
Y = 1249459
43 meter E =
0007799
Z = 4882104
41 I = 51
98972
XDOT = 668
128864 Wp = 167
37341
YDOT = -7223
935929 meter/sec RA = 110
67359 deg
ZDOT = 2463
306352 TA = 258
49942
MA = 258
58701
Ha = 225
458 n
mi
Hp = 221
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14927231
44 X = -4587168
09
Y = 4099276
34 feet Y = 1198371
24 meter
Z = 16017402
91 Z = 4859912
64
XDOT = 2192
023831 XDOT = 736
894098
YDOT = -23700
577194 feet/sec YDOT = -7216
079988 meter/sec
ZDOT = 8081
713752 ZDOT = 2466
718744
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13372174
71 X = 4075838
85
Y = 8002484
98 feet Y = 2439157
42 meter
Z = 15916302
30 Z = 4851288
94
XDOT = -17989
507479 XDOT = -5483
201880
YDOT = 13901
162702 feet/sec YDOT = 4237
074392 meter/sec
ZDOT = 8097
797572 ZDOT = 2468
208700
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 19218
55267197
00016717 00000-0 10270-3 0 9011
2 25544 51
6434 111
3948 0005992 227
5041 132
5605 15
51026395 23068
Satellite: ISS
Catalog Number: 25544
Epoch time: 19218
55267197 = yrday
fracday
Element set: 901
Inclination: 51
6434 deg
RA of node: 111
3948 deg
Eccentricity:
0005992
Arg of perigee: 227
5041 deg
Mean anomaly: 132
5605 deg
Mean motion: 15
51026395 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2306
Checksum: 303
Coasting Arc #3 (Orbit 2307)
---------------------------------------
Vector Time (GMT): 2019/218/16:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 937301
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -447286
53 A = 6796245
45 meter
Y = 6403101
56 meter E =
0000511
Z = -2232793
09 I = 52
01389
XDOT = -5111
605668 Wp = 299
15205
YDOT = 1556
419694 meter/sec RA = 109
75777 deg
ZDOT = 5486
712190 TA = 36
21189
MA = 36
20842
Ha = 225
380 n
mi
Hp = 221
172
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1467475
50 X = -508009
06
Y = 21007551
07 feet Y = 6397760
21 meter
Z = -7325436
64 Z = -2235113
19
XDOT = -16770
359804 XDOT = -5155
281213
YDOT = 5106
363825 feet/sec YDOT = 1499
013827 meter/sec
ZDOT = 18001
024246 ZDOT = 5461
776139
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5061387
11 X = -1542710
79
Y = -20437490
04 feet Y = -6229346
97 meter
Z = -7336488
89 Z = -2236161
81
XDOT = 13035
860720 XDOT = 3973
330348
YDOT = -9650
266923 feet/sec YDOT = -2941
401358 meter/sec
ZDOT = 17887
407764 ZDOT = 5452
081886
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 19218
68153190
00016717 00000-0 10270-3 0 9023
2 25544 51
6392 110
7522 0006181 227
9428 132
1198 15
51027003 23088
Satellite: ISS
Catalog Number: 25544
Epoch time: 19218
68153190 = yrday
fracday
Element set: 902
Inclination: 51
6392 deg
RA of node: 110
7522 deg
Eccentricity:
0006181
Arg of perigee: 227
9428 deg
Mean anomaly: 132
1198 deg
Mean motion: 15
51027003 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2308
Checksum: 285
Coasting Arc #4 (Orbit 2323)
---------------------------------------
Vector Time (GMT): 2019/219/16:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 937301
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 463554
55 A = 6797148
82 meter
Y = -6585337
08 meter E =
0012377
Z = 1584818
07 I = 52
02765
XDOT = 4936
804751 Wp = 143
69893
YDOT = -1044
766738 meter/sec RA = 104
82600 deg
ZDOT = -5772
011807 TA = 19
07646
MA = 19
03015
Ha = 225
089 n
mi
Hp = 221
297
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1520848
27 X = 529461
13
Y = -21605436
62 feet Y = -6579784
83 meter
Z = 5199534
36 Z = 1587229
69
XDOT = 16196
865980 XDOT = 4976
157707
YDOT = -3427
712394 feet/sec YDOT = -989
339698 meter/sec
ZDOT = -18937
046610 ZDOT = -5747
935317
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5540403
30 X = 1688714
93
Y = 20935426
64 feet Y = 6381118
04 meter
Z = 5211033
58 Z = 1588323
04
XDOT = -12827
766407 XDOT = -3909
903201
YDOT = 8091
903238 feet/sec YDOT = 2466
412107 meter/sec
ZDOT = -18827
373069 ZDOT = -5738
583311
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 19219
71242002
00016717 00000-0 10270-3 0 9030
2 25544 51
6393 105
6372 0006189 234
1955 125
8621 15
51077688 23240
Satellite: ISS
Catalog Number: 25544
Epoch time: 19219
71242002 = yrday
fracday
Element set: 903
Inclination: 51
6393 deg
RA of node: 105
6372 deg
Eccentricity:
0006189
Arg of perigee: 234
1955 deg
Mean anomaly: 125
8621 deg
Mean motion: 15
51077688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2324
Checksum: 304
Coasting Arc #5 (Orbit 2332)
---------------------------------------
Vector Time (GMT): 2019/220/06:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 937301
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4100953
47 A = 6790823
78 meter
Y = -3356509
90 meter E =
0002765
Z = -4248082
36 I = 52
01129
XDOT = 1549
703061 Wp = 106
77083
YDOT = 6540
297366 meter/sec RA = 101
94265 deg
ZDOT = -3674
360763 TA = 125
75234
MA = 125
72663
Ha = 225
201 n
mi
Hp = 221
423
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13454571
76 X = 4158816
79
Y = -11012171
58 feet Y = -3310326
45 meter
Z = -13937278
07 Z = -4228021
23
XDOT = 5084
327627 XDOT = 1494
300253
YDOT = 21457
668525 feet/sec YDOT = 6557
317610 meter/sec
ZDOT = -12054
989379 ZDOT = -3666
967242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -517425
51 X = -157711
30
Y = -17451942
00 feet Y = -5319351
92 meter
Z = -13845690
15 Z = -4220166
36
XDOT = 18908
978174 XDOT = 5763
456547
YDOT = 8969
851958 feet/sec YDOT = 2734
010877 meter/sec
ZDOT = -12021
862720 ZDOT = -3664
263757
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 19220
29229753
00016717 00000-0 10270-3 0 9044
2 25544 51
6398 102
7620 0005994 234
2638 125
7956 15
51032085 23333
Satellite: ISS
Catalog Number: 25544
Epoch time: 19220
29229753 = yrday
fracday
Element set: 904
Inclination: 51
6398 deg
RA of node: 102
7620 deg
Eccentricity:
0005994
Arg of perigee: 234
2638 deg
Mean anomaly: 125
7956 deg
Mean motion: 15
51032085 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2333
Checksum: 311
Coasting Arc #6 (Orbit 2348)
---------------------------------------
Vector Time (GMT): 2019/221/06:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 937301
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4001355
70 A = 6789297
62 meter
Y = 2950315
92 meter E =
0007143
Z = 4625015
69 I = 52
01371
XDOT = -1544
035118 Wp = 159
81975
YDOT = -6863
253453 meter/sec RA = 97
00504 deg
ZDOT = 3034
354856 TA = 259
97332
MA = 260
05392
Ha = 224
909 n
mi
Hp = 221
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13127807
40 X = -4056515
14
Y = 9679514
19 feet Y = 2905261
28 meter
Z = 15173935
99 Z = 4605444
98
XDOT = -5065
732013 XDOT = -1481
912561
YDOT = -22517
235738 feet/sec YDOT = -6880
172759 meter/sec
ZDOT = 9955
232466 ZDOT = 3027
005081
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -65649
82 X = -20010
06
Y = 16393022
37 feet Y = 4996593
22 meter
Z = 15084600
19 Z = 4597786
14
XDOT = -19970
113272 XDOT = -6086
890525
YDOT = -9234
389015 feet/sec YDOT = -2814
641772 meter/sec
ZDOT = 9922
346046 ZDOT = 3024
331075
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 19221
32318249
00016717 00000-0 10270-3 0 9059
2 25544 51
6411 97
6477 0006208 238
7482 121
3061 15
51073536 23498
Satellite: ISS
Catalog Number: 25544
Epoch time: 19221
32318249 = yrday
fracday
Element set: 905
Inclination: 51
6411 deg
RA of node: 97
6477 deg
Eccentricity:
0006208
Arg of perigee: 238
7482 deg
Mean anomaly: 121
3061 deg
Mean motion: 15
51073536 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2349
Checksum: 301
Coasting Arc #7 (Orbit 2363)
---------------------------------------
Vector Time (GMT): 2019/222/06:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 937301
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3948197
23 A = 6788144
71 meter
Y = -2482576
70 meter E =
0006281
Z = -4937936
38 I = 52
01259
XDOT = 1565
479198 Wp = 82
90741
YDOT = 7124
610590 meter/sec RA = 92
06471 deg
ZDOT = -2332
022106 TA = 164
37393
MA = 164
35454
Ha = 224
789 n
mi
Hp = 221
692
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12953402
97 X = 3999650
14
Y = -8144936
68 feet Y = -2438137
17 meter
Z = -16200578
69 Z = -4918632
94
XDOT = 5136
086606 XDOT = 1497
020936
YDOT = 23374
706659 feet/sec YDOT = 7141
734259 meter/sec
ZDOT = -7650
991162 ZDOT = -2324
583483
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 936785
63 X = 285532
26
Y = -15365532
44 feet Y = -4683414
29 meter
Z = -16112487
00 Z = -4911086
04
XDOT = 20931
374417 XDOT = 6379
882922
YDOT = 9258
001083 feet/sec YDOT = 2821
838730 meter/sec
ZDOT = -7617
736685 ZDOT = -2321
886141
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 19222
28963804
00016717 00000-0 10270-3 0 9069
2 25544 51
6412 92
8518 0005959 243
0247 117
0295 15
51039389 23648
Satellite: ISS
Catalog Number: 25544
Epoch time: 19222
28963804 = yrday
fracday
Element set: 906
Inclination: 51
6412 deg
RA of node: 92
8518 deg
Eccentricity:
0005959
Arg of perigee: 243
0247 deg
Mean anomaly: 117
0295 deg
Mean motion: 15
51039389 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2364
Checksum: 321
Coasting Arc #8 (Orbit 2379)
---------------------------------------
Vector Time (GMT): 2019/223/06:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 937301
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3933351
10 A = 6787110
58 meter
Y = 2002730
08 meter E =
0005415
Z = 5158443
37 I = 52
00951
XDOT = -1619
153993 Wp = 197
17552
YDOT = -7315
092741 meter/sec RA = 87
12542 deg
ZDOT = 1600
814939 TA = 237
42387
MA = 237
47618
Ha = 224
523 n
mi
Hp = 221
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12904695
22 X = -3980510
34
Y = 6570636
74 feet Y = 1958480
54 meter
Z = 16924026
79 Z = 5139222
51
XDOT = -5312
185016 XDOT = -1545
009934
YDOT = -23999
648099 feet/sec YDOT = -7332
784805 meter/sec
ZDOT = 5252
017517 ZDOT = 1593
129383
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1945673
20 X = -593041
19
Y = 14452647
94 feet Y = 4405167
09 meter
Z = 16836342
59 Z = 5131717
22
XDOT = -21761
042838 XDOT = -6632
765857
YDOT = -9025
466451 feet/sec YDOT = -2750
962174 meter/sec
ZDOT = 5217
668570 ZDOT = 1590
345380
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 19223
32052054
00016717 00000-0 10270-3 0 9072
2 25544 51
6412 87
7381 0006100 247
5148 112
5358 15
51070198 23808
Satellite: ISS
Catalog Number: 25544
Epoch time: 19223
32052054 = yrday
fracday
Element set: 907
Inclination: 51
6412 deg
RA of node: 87
7381 deg
Eccentricity:
0006100
Arg of perigee: 247
5148 deg
Mean anomaly: 112
5358 deg
Mean motion: 15
51070198 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2380
Checksum: 284
Coasting Arc #9 (Orbit 2394)
---------------------------------------
Vector Time (GMT): 2019/224/06:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 937301
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3975331
91 A = 6786581
21 meter
Y = -1492102
28 meter E =
0008713
Z = -5301607
47 I = 52
00498
XDOT = 1676
759710 Wp = 92
38760
YDOT = 7424
700467 meter/sec RA = 82
18321 deg
ZDOT = -833
872070 TA = 169
67841
MA = 169
66051
Ha = 224
390 n
mi
Hp = 221
898
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13042427
51 X = 4017473
35
Y = -4895348
68 feet Y = -1447411
35 meter
Z = -17393725
31 Z = -5282194
91
XDOT = 5501
180150 XDOT = 1597
660365
YDOT = 24359
253502 feet/sec YDOT = 7443
008956 meter/sec
ZDOT = -2735
800755 ZDOT = -825
918778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3171994
78 X = 966824
01
Y = -13677694
87 feet Y = -4168961
40 meter
Z = -17305205
76 Z = -5274626
72
XDOT = 22366
866398 XDOT = 6817
420878
YDOT = 8597
104187 feet/sec YDOT = 2620
397356 meter/sec
ZDOT = -2700
254223 ZDOT = -823
037487
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 19224
28697397
00016717 00000-0 10270-3 0 9084
2 25544 51
6415 82
9424 0006039 250
9648 109
0849 15
51041101 23954
Satellite: ISS
Catalog Number: 25544
Epoch time: 19224
28697397 = yrday
fracday
Element set: 908
Inclination: 51
6415 deg
RA of node: 82
9424 deg
Eccentricity:
0006039
Arg of perigee: 250
9648 deg
Mean anomaly: 109
0849 deg
Mean motion: 15
51041101 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2395
Checksum: 322
Coasting Arc #10 (Orbit 2410)
---------------------------------------
Vector Time (GMT): 2019/225/06:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 937301
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4061587
35 A = 6786270
69 meter
Y = 987589
75 meter E =
0003867
Z = 5349228
46 I = 51
99913
XDOT = -1736
000515 Wp = 245
68038
YDOT = -7461
750156 meter/sec RA = 77
24171 deg
ZDOT = 57
975531 TA = 203
76045
MA = 203
77831
Ha = 224
137 n
mi
Hp = 221
750
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13325417
81 X = -4098312
02
Y = 3240123
86 feet Y = 941964
60 meter
Z = 17549962
13 Z = 5329410
07
XDOT = -5695
539746 XDOT = -1652
713662
YDOT = -24480
807597 feet/sec YDOT = -7480
697651 meter/sec
ZDOT = 190
208435 ZDOT = 49
744755
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4485080
21 X = -1367052
45
Y = 13080960
66 feet Y = 3987076
81 meter
Z = 17459635
07 Z = 5321696
77
XDOT = -22756
629374 XDOT = -6936
220633
YDOT = -8014
019687 feet/sec YDOT = -2442
673201 meter/sec
ZDOT = 153
411968 ZDOT = 46
759968
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 19225
31785291
00016717 00000-0 10270-3 0 9091
2 25544 51
6421 77
8282 0006124 256
0956 103
9514 15
51070014 24116
Satellite: ISS
Catalog Number: 25544
Epoch time: 19225
31785291 = yrday
fracday
Element set: 909
Inclination: 51
6421 deg
RA of node: 77
8282 deg
Eccentricity:
0006124
Arg of perigee: 256
0956 deg
Mean anomaly: 103
9514 deg
Mean motion: 15
51070014 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2411
Checksum: 291
Coasting Arc #11 (Orbit 2425)
---------------------------------------
Vector Time (GMT): 2019/226/06:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 937301
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4203904
49 A = 6786527
45 meter
Y = -485566
18 meter E =
0008987
Z = -5313204
40 I = 51
99085
XDOT = 1772
661646 Wp = 105
98571
YDOT = 7413
769934 meter/sec RA = 72
29797 deg
ZDOT = 723
637639 TA = 170
91138
MA = 170
89510
Ha = 223
924 n
mi
Hp = 221
895
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13792337
56 X = 4234829
78
Y = -1593064
88 feet Y = -438382
05 meter
Z = -17431772
98 Z = -5292708
79
XDOT = 5815
819047 XDOT = 1686
112041
YDOT = 24323
392172 feet/sec YDOT = 7433
109128 meter/sec
ZDOT = 2374
139235 ZDOT = 732
038427
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5907350
05 X = 1800560
29
Y = -12693149
68 feet Y = -3868872
02 meter
Z = -17338405
55 Z = -5284746
01
XDOT = 22844
606778 XDOT = 6963
036146
YDOT = 7331
231933 feet/sec YDOT = 2234
559493 meter/sec
ZDOT = 2411
705222 ZDOT = 735
087752
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 19226
28430210
00016717 00000-0 10270-3 0 9108
2 25544 51
6417 73
0322 0005960 259
8709 100
1770 15
51044413 24261
Satellite: ISS
Catalog Number: 25544
Epoch time: 19226
28430210 = yrday
fracday
Element set: 910
Inclination: 51
6417 deg
RA of node: 73
0322 deg
Eccentricity:
0005960
Arg of perigee: 259
8709 deg
Mean anomaly: 100
1770 deg
Mean motion: 15
51044413 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2426
Checksum: 273
Coasting Arc #12 (Orbit 2440)
---------------------------------------
Vector Time (GMT): 2019/227/05:47:34
629
Vector Time (MET): N/A
Weight (LBS) : 937115
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4649405
23 A = 6791821
38 meter
Y = 2545987
77 meter E =
0002932
Z = -4248198
88 I = 51
99346
XDOT = -320
980537 Wp = 177
48456
YDOT = 6715
040552 meter/sec RA = 67
48135 deg
ZDOT = 3670
344055 TA = 129
98504
MA = 129
95929
Ha = 223
724 n
mi
Hp = 222
898
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15253954
17 X = 4641224
62
Y = 8352978
25 feet Y = 2597935
03 meter
Z = -13937660
35 Z = -4225634
17
XDOT = -1053
085752 XDOT = -413
874270
YDOT = 22030
972940 feet/sec YDOT = 6710
931657 meter/sec
ZDOT = 12041
811203 ZDOT = 3668
559389
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16333913
30 X = 4978576
78
Y = -6205281
14 feet Y = -1891369
69 meter
Z = -13835154
57 Z = -4216955
11
XDOT = 15526
066474 XDOT = 4732
345061
YDOT = 14019
732495 feet/sec YDOT = 4273
214465 meter/sec
ZDOT = 12033
056791 ZDOT = 3667
675710
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 19227
25074994
00016717 00000-0 10270-3 0 9110
2 25544 51
6409 68
2372 0007374 268
2699 91
7607 15
50695700 24417
Satellite: ISS
Catalog Number: 25544
Epoch time: 19227
25074994 = yrday
fracday
Element set: 911
Inclination: 51
6409 deg
RA of node: 68
2372 deg
Eccentricity:
0007374
Arg of perigee: 268
2699 deg
Mean anomaly: 91
7607 deg
Mean motion: 15
50695700 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2441
Checksum: 331
Coasting Arc #13 (Orbit 2442)
---------------------------------------
Vector Time (GMT): 2019/227/08:49:34
515
Vector Time (MET): N/A
Weight (LBS) : 936929
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4592029
35 A = 6790248
69 meter
Y = 983184
30 meter E =
0004276
Z = -4907881
32 I = 51
98563
XDOT = 1031
462558 Wp = 146
14088
YDOT = 7198
161128 meter/sec RA = 66
86471 deg
ZDOT = 2404
626305 TA = 147
35692
MA = 147
33049
Ha = 224
020 n
mi
Hp = 223
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15065713
08 X = 4604533
01
Y = 3225670
27 feet Y = 1034605
59 meter
Z = -16101972
84 Z = -4885545
11
XDOT = 3384
063511 XDOT = 939
213924
YDOT = 23616
014201 feet/sec YDOT = 7209
179838 meter/sec
ZDOT = 7889
193913 ZDOT = 2409
412703
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1895000
86 X = 577596
26
Y = -15396479
86 feet Y = -4692847
06 meter
Z = -16000361
51 Z = -4876910
19
XDOT = 22115
389895 XDOT = 6740
770840
YDOT = -5506
999663 feet/sec YDOT = -1678
533497 meter/sec
ZDOT = 7910
313369 ZDOT = 2411
063515
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 19227
37963813
00016717 00000-0 10270-3 0 9121
2 25544 51
6431 67
5993 0008921 269
8088 90
2040 15
50367836 24434
Satellite: ISS
Catalog Number: 25544
Epoch time: 19227
37963813 = yrday
fracday
Element set: 912
Inclination: 51
6431 deg
RA of node: 67
5993 deg
Eccentricity:
0008921
Arg of perigee: 269
8088 deg
Mean anomaly: 90
2040 deg
Mean motion: 15
50367836 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2443
Checksum: 329
Coasting Arc #14 (Orbit 2458)
---------------------------------------
Vector Time (GMT): 2019/228/08:49:34
515
Vector Time (MET): N/A
Weight (LBS) : 936929
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4769395
78 A = 6790959
60 meter
Y = -1124062
62 meter E =
0004509
Z = 4705175
51 I = 51
97481
XDOT = -1187
177986 Wp = 337
71733
YDOT = -6999
613709 meter/sec RA = 61
92926 deg
ZDOT = -2872
426520 TA = 140
73116
MA = 140
69845
Ha = 224
925 n
mi
Hp = 224
501
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15647623
97 X = -4779326
34
Y = -3687869
50 feet Y = -1177452
87 meter
Z = 15436927
52 Z = 4681983
97
XDOT = -3894
940898 XDOT = -1094
865715
YDOT = -22964
611906 feet/sec YDOT = -7012
373429 meter/sec
ZDOT = -9423
971521 ZDOT = -2877
969026
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2029599
13 X = -618621
82
Y = 16049142
66 feet Y = 4891778
68 meter
Z = 15331438
15 Z = 4673022
35
XDOT = -21272
198749 XDOT = -6483
766179
YDOT = 6345
861384 feet/sec YDOT = 1934
218550 meter/sec
ZDOT = -9448
544382 ZDOT = -2879
916328
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 19228
41097339
00016717 00000-0 10270-3 0 9139
2 25544 51
6437 62
4874 0009038 274
2803 85
7315 15
50406477 24593
Satellite: ISS
Catalog Number: 25544
Epoch time: 19228
41097339 = yrday
fracday
Element set: 913
Inclination: 51
6437 deg
RA of node: 62
4874 deg
Eccentricity:
0009038
Arg of perigee: 274
2803 deg
Mean anomaly: 85
7315 deg
Mean motion: 15
50406477 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2459
Checksum: 326
Coasting Arc #15 (Orbit 2473)
---------------------------------------
Vector Time (GMT): 2019/229/08:49:34
515
Vector Time (MET): N/A
Weight (LBS) : 936929
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4967186
76 A = 6791972
74 meter
Y = 1232081
32 meter E =
0001993
Z = -4466224
33 I = 51
96103
XDOT = 1305
807535 Wp = 190
22548
YDOT = 6778
600655 meter/sec RA = 56
99230 deg
ZDOT = 3320
129060 TA = 113
17412
MA = 113
15312
Ha = 225
323 n
mi
Hp = 224
266
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16296544
47 X = 4974734
11
Y = 4042261
54 feet Y = 1287670
01 meter
Z = -14652966
98 Z = -4442077
77
XDOT = 4284
145457 XDOT = 1213
783196
YDOT = 22239
503461 feet/sec YDOT = 6792
688638 meter/sec
ZDOT = 10892
811875 ZDOT = 3326
248419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2027164
92 X = 617879
87
Y = -16763478
77 feet Y = -5109508
33 meter
Z = -14543144
89 Z = -4432750
56
XDOT = 20344
576896 XDOT = 6201
027038
YDOT = -7019
564494 feet/sec YDOT = -2139
563258 meter/sec
ZDOT = 10920
023858 ZDOT = 3328
423272
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 19229
37785002
00016717 00000-0 10270-3 0 9147
2 25544 51
6435 57
6940 0009007 277
9623 82
0505 15
50373852 24745
Satellite: ISS
Catalog Number: 25544
Epoch time: 19229
37785002 = yrday
fracday
Element set: 914
Inclination: 51
6435 deg
RA of node: 57
6940 deg
Eccentricity:
0009007
Arg of perigee: 277
9623 deg
Mean anomaly: 82
0505 deg
Mean motion: 15
50373852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2474
Checksum: 316
Coasting Arc #16 (Orbit 2489)
---------------------------------------
Vector Time (GMT): 2019/230/08:49:34
515
Vector Time (MET): N/A
Weight (LBS) : 936929
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5183181
08 A = 6792878
01 meter
Y = -1309435
43 meter E =
0004651
Z = 4192881
13 I = 51
94478
XDOT = -1381
069137 Wp = 14
97035
YDOT = -6537
277671 meter/sec RA = 52
05588 deg
ZDOT = -3743
551045 TA = 113
42507
MA = 113
37616
Ha = 225
514 n
mi
Hp = 224
188
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17005187
26 X = -5188519
73
Y = -4296048
01 feet Y = -1367427
13 meter
Z = 13756171
68 Z = 4167690
66
XDOT = -4531
066721 XDOT = -1289
680975
YDOT = -21447
761388 feet/sec YDOT = -6552
210892 meter/sec
ZDOT = -12281
991618 ZDOT = -3750
037485
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1892897
12 X = -576955
04
Y = 17526781
07 feet Y = 5342162
87 meter
Z = 13641611
61 Z = 4157963
22
XDOT = -19350
642948 XDOT = -5898
075971
YDOT = 7505
694011 feet/sec YDOT = 2287
735535 meter/sec
ZDOT = -12310
889012 ZDOT = -3752
358971
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 19230
40918242
00016717 00000-0 10270-3 0 9158
2 25544 51
6430 52
5821 0009027 282
6137 77
4004 15
50406692 24906
Satellite: ISS
Catalog Number: 25544
Epoch time: 19230
40918242 = yrday
fracday
Element set: 915
Inclination: 51
6430 deg
RA of node: 52
5821 deg
Eccentricity:
0009027
Arg of perigee: 282
6137 deg
Mean anomaly: 77
4004 deg
Mean motion: 15
50406692 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2490
Checksum: 288
Coasting Arc #17 (Orbit 2504)
---------------------------------------
Vector Time (GMT): 2019/231/08:49:34
515
Vector Time (MET): N/A
Weight (LBS) : 936929
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5404433
80 A = 6794000
81 meter
Y = 1342616
03 meter E =
0002820
Z = -3889051
00 I = 51
92634
XDOT = 1416
811475 Wp = 286
40485
YDOT = 6289
936383 meter/sec RA = 47
11827 deg
ZDOT = 4138
641680 TA = 26
93207
MA = 26
91744
Ha = 225
828 n
mi
Hp = 223
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17731082
03 X = 5407909
23
Y = 4404908
25 feet Y = 1403071
50 meter
Z = -12759353
68 Z = -3862790
22
XDOT = 4648
331612 XDOT = 1326
267319
YDOT = 20636
274222 feet/sec YDOT = 6305
274058 meter/sec
ZDOT = 13578
220734 ZDOT = 4145
303784
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1587185
32 X = 483774
09
Y = -18284105
80 feet Y = -5572995
45 meter
Z = -12639933
19 Z = -3852651
64
XDOT = 18347
210039 XDOT = 5592
229620
YDOT = -7818
509367 feet/sec YDOT = -2383
081655 meter/sec
ZDOT = 13607
932056 ZDOT = 4147
697691
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 19231
37605761
00016717 00000-0 10270-3 0 9165
2 25544 51
6426 47
7892 0009074 285
3578 74
6570 15
50373154 25056
Satellite: ISS
Catalog Number: 25544
Epoch time: 19231
37605761 = yrday
fracday
Element set: 916
Inclination: 51
6426 deg
RA of node: 47
7892 deg
Eccentricity:
0009074
Arg of perigee: 285
3578 deg
Mean anomaly: 74
6570 deg
Mean motion: 15
50373154 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2505
Checksum: 325
Coasting Arc #18 (Orbit 2520)
---------------------------------------
Vector Time (GMT): 2019/232/08:49:34
515
Vector Time (MET): N/A
Weight (LBS) : 936929
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5633685
42 A = 6794953
49 meter
Y = -1346443
87 meter E =
0004968
Z = 3552877
67 I = 51
90744
XDOT = -1402
321509 Wp = 44
75332
YDOT = -6034
276671 meter/sec RA = 42
18033 deg
ZDOT = -4503
179961 TA = 93
61417
MA = 93
55735
Ha = 225
936 n
mi
Hp = 223
747
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18483219
89 X = -5635468
15
Y = -4417466
76 feet Y = -1409453
54 meter
Z = 11656422
81 Z = 3525507
29
XDOT = -4600
792351 XDOT = -1312
866501
YDOT = -19797
495639 feet/sec YDOT = -6049
458410 meter/sec
ZDOT = -14774
212472 ZDOT = -4509
774364
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1156728
22 X = -352570
76
Y = 19044460
12 feet Y = 5804751
44 meter
Z = 11531961
72 Z = 3514941
93
XDOT = -17339
727777 XDOT = -5285
149026
YDOT = 7925
418366 feet/sec YDOT = 2415
667518 meter/sec
ZDOT = -14803
630315 ZDOT = -4512
146520
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 19232
40738739
00016717 00000-0 10270-3 0 9173
2 25544 51
6437 42
6770 0009210 290
0708 69
9452 15
50408645 25215
Satellite: ISS
Catalog Number: 25544
Epoch time: 19232
40738739 = yrday
fracday
Element set: 917
Inclination: 51
6437 deg
RA of node: 42
6770 deg
Eccentricity:
0009210
Arg of perigee: 290
0708 deg
Mean anomaly: 69
9452 deg
Mean motion: 15
50408645 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2521
Checksum: 312
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