[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 21st 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14504 3693 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
201/16:28:21
000 0
0 0
0 0
0
N/A 0
0 0
0 227
5
000/00:00:00
000 0
0 0
0 218
5
201/22:50:29
000 0
0 -0
0 0
0
N/A -0
0 0
0 227
4
000/00:00:58
000 0
0 -0
0 218
6
203/20:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
4
000/00:00:00
000 0
0 0
0 218
9
203/23:12:38
000 0
0 0
0 0
0
N/A 0
0 0
0 227
5
000/00:00:00
000 0
0 0
0 218
8
204/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
4
000/00:00:00
000 0
0 0
0 218
9
210/10:44:30
000 0
0 0
0 0
0
N/A 0
0 0
0 226
6
000/00:00:00
000 0
0 0
0 219
8
212/15:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 226
2
000/00:00:00
000 0
0 0
0 220
2
213/11:38:30
000 0
0 0
0 0
0
N/A 0
0 0
0 226
2
000/00:00:00
000 0
0 0
0 220
3
Coasting Arc #1 (Orbit 2025)
---------------------------------------
Vector Time (GMT): 2019/200/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3942658
45 A = 6788550
53 meter
Y = 2682010
11 meter E =
0016953
Z = -4847685
52 I = 51
49056
XDOT = -5896
314466 Wp = 125
58905
YDOT = -4204
001225 meter/sec RA = 199
76622 deg
ZDOT = 2466
075820 TA = 168
75826
MA = 168
72034
Ha = 227
781 n
mi
Hp = 218
222
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12935231
15 X = -3948809
60
Y = 8799245
76 feet Y = 2637886
63 meter
Z = -15904480
05 Z = -4866851
72
XDOT = -19344
863734 XDOT = -5860
844453
YDOT = -13792
654939 feet/sec YDOT = -4269
739878 meter/sec
ZDOT = 8090
799935 ZDOT = 2437
520094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13545340
62 X = 4128619
82
Y = 7647765
20 feet Y = 2331038
83 meter
Z = -15991711
95 Z = -4874273
80
XDOT = -3291
239270 XDOT = -1003
169730
YDOT = 22501
062246 feet/sec YDOT = 6858
323772 meter/sec
ZDOT = 7961
406939 ZDOT = 2426
636835
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 19200
51186303
00016717 00000-0 10270-3 0 9006
2 25544 51
6388 200
9039 0006757 157
1527 202
9926 15
50962425 20268
Satellite: ISS
Catalog Number: 25544
Epoch time: 19200
51186303 = yrday
fracday
Element set: 900
Inclination: 51
6388 deg
RA of node: 200
9039 deg
Eccentricity:
0006757
Arg of perigee: 157
1527 deg
Mean anomaly: 202
9926 deg
Mean motion: 15
50962425 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2026
Checksum: 298
Coasting Arc #2 (Orbit 2041)
---------------------------------------
Vector Time (GMT): 2019/201/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4354233
11 A = 6789665
25 meter
Y = -2567560
29 meter E =
0010504
Z = 4522641
70 I = 51
52530
XDOT = 5678
750789 Wp = 106
70630
YDOT = 4084
847614 meter/sec RA = 194
79297 deg
ZDOT = -3145
170269 TA = 14
89634
MA = 14
86542
Ha = 227
492 n
mi
Hp = 218
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14285541
69 X = 4360652
67
Y = -8423754
25 feet Y = -2518832
69 meter
Z = 14838063
33 Z = 4543807
87
XDOT = 18631
072141 XDOT = 5647
927964
YDOT = 13401
731018 feet/sec YDOT = 4148
179316 meter/sec
ZDOT = -10318
800096 ZDOT = -3117
660124
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13958864
96 X = -4254662
04
Y = -8793116
16 feet Y = -2680141
80 meter
Z = 14934378
37 Z = 4551998
53
XDOT = 2773
187974 XDOT = 845
267694
YDOT = -21733
424969 feet/sec YDOT = -6624
347931 meter/sec
ZDOT = -10194
124598 ZDOT = -3107
169178
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 19201
54277955
00016717 00000-0 10270-3 0 9015
2 25544 51
6376 195
7889 0006680 161
9844 198
1545 15
50999599 20422
Satellite: ISS
Catalog Number: 25544
Epoch time: 19201
54277955 = yrday
fracday
Element set: 901
Inclination: 51
6376 deg
RA of node: 195
7889 deg
Eccentricity:
0006680
Arg of perigee: 161
9844 deg
Mean anomaly: 198
1545 deg
Mean motion: 15
50999599 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2042
Checksum: 361
Coasting Arc #3 (Orbit 2044)
---------------------------------------
Vector Time (GMT): 2019/201/16:28:21
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 169138
26 A = 6786614
51 meter
Y = -4271292
62 meter E =
0009170
Z = 5268064
81 I = 51
52348
XDOT = 7527
183701 Wp = 149
69026
YDOT = 1242
391846 meter/sec RA = 193
89745 deg
ZDOT = 757
318362 TA = 293
01244
MA = 293
10913
Ha = 227
498 n
mi
Hp = 218
515
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 554915
56 X = 191299
71
Y = -14013427
24 feet Y = -4269277
71 meter
Z = 17283677
21 Z = 5268939
89
XDOT = 24695
484582 XDOT = 7509
052932
YDOT = 4076
088732 feet/sec YDOT = 1326
464662 meter/sec
ZDOT = 2484
640296 ZDOT = 793
837911
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 628574
43 X = 191589
49
Y = 14005052
58 feet Y = 4268740
03 meter
Z = 17287942
86 Z = 5269364
98
XDOT = -23895
527887 XDOT = -7283
356900
YDOT = -2232
966495 feet/sec YDOT = -680
608188 meter/sec
ZDOT = 2650
436085 ZDOT = 807
852919
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 19201
73607669
00016717 00000-0 10270-3 0 9026
2 25544 51
6399 194
8308 0006564 163
7824 196
3538 15
51025570 20457
Satellite: ISS
Catalog Number: 25544
Epoch time: 19201
73607669 = yrday
fracday
Element set: 902
Inclination: 51
6399 deg
RA of node: 194
8308 deg
Eccentricity:
0006564
Arg of perigee: 163
7824 deg
Mean anomaly: 196
3538 deg
Mean motion: 15
51025570 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2045
Checksum: 327
Coasting Arc #4 (Orbit 2048)
---------------------------------------
Vector Time (GMT): 2019/201/22:50:58
000
Vector Time (MET): N/A
Weight (LBS) : 931973
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4749313
92 A = 6790787
20 meter
Y = -2376617
91 meter E =
0011764
Z = 4219955
44 I = 51
54454
XDOT = 5320
707357 Wp = 108
27869
YDOT = 4150
203487 meter/sec RA = 192
54351 deg
ZDOT = -3646
066182 TA = 19
11943
MA = 19
07531
Ha = 227
379 n
mi
Hp = 218
624
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15581738
59 X = 4755039
18
Y = -7797302
86 feet Y = -2323476
06 meter
Z = 13844998
15 Z = 4243039
08
XDOT = 17456
388966 XDOT = 5291
613355
YDOT = 13616
153174 feet/sec YDOT = 4209
540979 meter/sec
ZDOT = -11962
159391 ZDOT = -3620
291041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10434973
28 X = 3180579
86
Y = 13848499
09 feet Y = 4221022
52 meter
Z = 13950013
94 Z = 4251964
25
XDOT = -9257
814929 XDOT = -2821
781990
YDOT = 18923
605278 feet/sec YDOT = 5767
914889 meter/sec
ZDOT = -11845
359783 ZDOT = -3610
465662
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 19201
99380444
00016717 00000-0 10270-3 0 9034
2 25544 51
6385 193
5493 0006607 165
9564 194
1772 15
50999060 20499
Satellite: ISS
Catalog Number: 25544
Epoch time: 19201
99380444 = yrday
fracday
Element set: 903
Inclination: 51
6385 deg
RA of node: 193
5493 deg
Eccentricity:
0006607
Arg of perigee: 165
9564 deg
Mean anomaly: 194
1772 deg
Mean motion: 15
50999060 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2049
Checksum: 337
Coasting Arc #5 (Orbit 2063)
---------------------------------------
Vector Time (GMT): 2019/202/22:50:58
000
Vector Time (MET): N/A
Weight (LBS) : 931973
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5132431
31 A = 6792273
27 meter
Y = 2350356
00 meter E =
0010928
Z = -3790731
04 I = 51
58206
XDOT = -4957
253689 Wp = 138
22073
YDOT = -4029
561244 meter/sec RA = 187
57509 deg
ZDOT = 4212
460703 TA = 176
41937
MA = 176
41154
Ha = 227
488 n
mi
Hp = 218
571
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16838685
41 X = -5139919
27
Y = 7711141
73 feet Y = 2292919
93 meter
Z = -12436781
64 Z = -3815680
08
XDOT = -16263
955671 XDOT = -4932
286987
YDOT = -13220
345288 feet/sec YDOT = -4084
857411 meter/sec
ZDOT = 13820
409132 ZDOT = 4188
441016
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10834607
81 X = -3302388
46
Y = -14925760
30 feet Y = -4549371
74 meter
Z = -12550279
82 Z = -3825325
29
XDOT = 8681
319929 XDOT = 2646
066314
YDOT = -17833
654212 feet/sec YDOT = -5435
697804 meter/sec
ZDOT = 13711
557641 ZDOT = 4179
282769
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 19202
96028664
00016717 00000-0 10270-3 0 9046
2 25544 51
6382 188
7530 0006755 168
0131 192
1182 15
50999691 20642
Satellite: ISS
Catalog Number: 25544
Epoch time: 19202
96028664 = yrday
fracday
Element set: 904
Inclination: 51
6382 deg
RA of node: 188
7530 deg
Eccentricity:
0006755
Arg of perigee: 168
0131 deg
Mean anomaly: 192
1182 deg
Mean motion: 15
50999691 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2064
Checksum: 322
Coasting Arc #6 (Orbit 2078)
---------------------------------------
Vector Time (GMT): 2019/203/20:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 931973
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4009952
23 A = 6791201
96 meter
Y = -3535161
99 meter E =
0014108
Z = 4185069
24 I = 51
61052
XDOT = 6181
843148 Wp = 129
26787
YDOT = -2607
543107 meter/sec RA = 183
06369 deg
ZDOT = 3703
450113 TA = 282
58877
MA = 282
74650
Ha = 227
393 n
mi
Hp = 218
937
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13156011
24 X = -3990451
46
Y = -11598300
48 feet Y = -3579895
30 meter
Z = 13730542
12 Z = 4165637
83
XDOT = 20281
637626 XDOT = 6192
552952
YDOT = -8554
931453 feet/sec YDOT = -2538
353728 meter/sec
ZDOT = 12150
426880 ZDOT = 3733
504626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14934949
43 X = 4552172
59
Y = -9325167
06 feet Y = -2842310
92 meter
Z = 13642490
15 Z = 4158231
00
XDOT = 1662
775909 XDOT = 506
814097
YDOT = 20721
518176 feet/sec YDOT = 6315
918740 meter/sec
ZDOT = 12287
148732 ZDOT = 3745
122934
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 19203
92676530
00016717 00000-0 10270-3 0 9055
2 25544 51
6403 183
9604 0006362 171
4264 188
6997 15
50977705 20796
Satellite: ISS
Catalog Number: 25544
Epoch time: 19203
92676530 = yrday
fracday
Element set: 905
Inclination: 51
6403 deg
RA of node: 183
9604 deg
Eccentricity:
0006362
Arg of perigee: 171
4264 deg
Mean anomaly: 188
6997 deg
Mean motion: 15
50977705 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2079
Checksum: 335
Coasting Arc #7 (Orbit 2079)
---------------------------------------
Vector Time (GMT): 2019/203/23:12:38
000
Vector Time (MET): N/A
Weight (LBS) : 931973
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4565199
66 A = 6792262
19 meter
Y = 3250661
64 meter E =
0008801
Z = -3839332
22 I = 51
61591
XDOT = -5661
141022 Wp = 126
52181
YDOT = 3046
130475 meter/sec RA = 182
58713 deg
ZDOT = -4164
123921 TA = 99
61539
MA = 99
51595
Ha = 227
471 n
mi
Hp = 218
791
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14977689
17 X = 4547159
62
Y = 10664900
40 feet Y = 3301612
26 meter
Z = -12596234
32 Z = -3817200
13
XDOT = -18573
297315 XDOT = -5674
556262
YDOT = 9993
866389 feet/sec YDOT = 2982
748852 meter/sec
ZDOT = -13661
823887 ZDOT = -4191
655649
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5585539
02 X = -1702472
29
Y = 17589509
08 feet Y = 5361282
37 meter
Z = -12495892
00 Z = -3808747
88
XDOT = -13851
409092 XDOT = -4221
909491
YDOT = -14165
478959 feet/sec YDOT = -4317
637987 meter/sec
ZDOT = -13787
113825 ZDOT = -4202
312294
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 19203
99119734
00016717 00000-0 10270-3 0 9061
2 25544 51
6386 183
6379 0006724 169
6948 190
4342 15
51016624 20804
Satellite: ISS
Catalog Number: 25544
Epoch time: 19203
99119734 = yrday
fracday
Element set: 906
Inclination: 51
6386 deg
RA of node: 183
6379 deg
Eccentricity:
0006724
Arg of perigee: 169
6948 deg
Mean anomaly: 190
4342 deg
Mean motion: 15
51016624 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2080
Checksum: 329
Coasting Arc #8 (Orbit 2087)
---------------------------------------
Vector Time (GMT): 2019/204/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931973
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 77593
95 A = 6786485
02 meter
Y = -4212465
63 meter E =
0007299
Z = 5317414
21 I = 51
61260
XDOT = 7665
817050 Wp = 153
53797
YDOT = 67
985426 meter/sec RA = 180
12703 deg
ZDOT = -64
361569 TA = 297
03848
MA = 297
11296
Ha = 227
363 n
mi
Hp = 218
873
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 254573
34 X = 98864
46
Y = -13820425
29 feet Y = -4211479
29 meter
Z = 17445584
67 Z = 5317842
55
XDOT = 25150
318405 XDOT = 7664
799710
YDOT = 223
049297 feet/sec YDOT = 153
704292 meter/sec
ZDOT = -211
160004 ZDOT = -27
126819
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13383468
22 X = -4079281
11
Y = 3445892
90 feet Y = 1050308
16 meter
Z = 17447807
54 Z = 5318091
74
XDOT = -6046
029504 XDOT = -1842
829793
YDOT = -23375
140200 feet/sec YDOT = -7124
742733 meter/sec
ZDOT = -41
980024 ZDOT = -12
795511
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 19204
50665133
00016717 00000-0 10270-3 0 9079
2 25544 51
6382 181
0836 0006588 172
3543 187
7709 15
50994983 20886
Satellite: ISS
Catalog Number: 25544
Epoch time: 19204
50665133 = yrday
fracday
Element set: 907
Inclination: 51
6382 deg
RA of node: 181
0836 deg
Eccentricity:
0006588
Arg of perigee: 172
3543 deg
Mean anomaly: 187
7709 deg
Mean motion: 15
50994983 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2088
Checksum: 339
Coasting Arc #9 (Orbit 2102)
---------------------------------------
Vector Time (GMT): 2019/205/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 931973
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -592015
77 A = 6786745
94 meter
Y = 4241791
87 meter E =
0016987
Z = -5278533
34 I = 51
64667
XDOT = -7606
043278 Wp = 118
90856
YDOT = -17
481323 meter/sec RA = 175
16014 deg
ZDOT = 833
031868 TA = 159
10641
MA = 159
03690
Ha = 227
262 n
mi
Hp = 219
013
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1942308
97 X = -613764
76
Y = 13916640
00 feet Y = 4235050
25 meter
Z = -17318022
76 Z = -5281461
67
XDOT = -24954
210230 XDOT = -7609
328873
YDOT = -57
353422 feet/sec YDOT = -102
555864 meter/sec
ZDOT = 2733
044187 ZDOT = 796
076905
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13879943
78 X = 4230606
86
Y = -2078909
75 feet Y = -633651
69 meter
Z = -17331608
13 Z = -5282674
16
XDOT = 6673
735869 XDOT = 2034
154693
YDOT = 23009
108809 feet/sec YDOT = 7013
176365 meter/sec
ZDOT = 2565
112228 ZDOT = 781
846207
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 19205
47312779
00016717 00000-0 10270-3 0 9082
2 25544 51
6382 176
2887 0006570 175
7220 184
3988 15
50980688 21035
Satellite: ISS
Catalog Number: 25544
Epoch time: 19205
47312779 = yrday
fracday
Element set: 908
Inclination: 51
6382 deg
RA of node: 176
2887 deg
Eccentricity:
0006570
Arg of perigee: 175
7220 deg
Mean anomaly: 184
3988 deg
Mean motion: 15
50980688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2103
Checksum: 341
Coasting Arc #10 (Orbit 2118)
---------------------------------------
Vector Time (GMT): 2019/206/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 951979
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1064132
69 A = 6787219
95 meter
Y = -4302722
92 meter E =
0005425
Z = 5135858
27 I = 51
68197
XDOT = 7502
215441 Wp = 134
69101
YDOT = -28
491810 meter/sec RA = 170
19583 deg
ZDOT = -1581
005417 TA = 330
53148
MA = 330
56205
Ha = 227
096 n
mi
Hp = 219
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3491248
97 X = 1087220
90
Y = -14116545
01 feet Y = -4290694
33 meter
Z = 16849928
70 Z = 5141083
15
XDOT = 24613
567721 XDOT = 7509
656063
YDOT = -93
477068 feet/sec YDOT = 55
444952 meter/sec
ZDOT = -5187
025646 ZDOT = -1544
544631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14486572
97 X = -4415507
44
Y = 891336
81 feet Y = 271679
46 meter
Z = 16873958
69 Z = 5143182
61
XDOT = -7222
283346 XDOT = -2201
351964
YDOT = -22489
824213 feet/sec YDOT = -6854
898420 meter/sec
ZDOT = -5021
315635 ZDOT = -1530
497006
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 19206
50403257
00016717 00000-0 10270-3 0 9090
2 25544 51
6384 171
1737 0006519 180
2684 179
8465 15
51007643 21191
Satellite: ISS
Catalog Number: 25544
Epoch time: 19206
50403257 = yrday
fracday
Element set: 909
Inclination: 51
6384 deg
RA of node: 171
1737 deg
Eccentricity:
0006519
Arg of perigee: 180
2684 deg
Mean anomaly: 179
8465 deg
Mean motion: 15
51007643 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2119
Checksum: 315
Coasting Arc #11 (Orbit 2133)
---------------------------------------
Vector Time (GMT): 2019/207/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 951979
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1538858
06 A = 6788201
15 meter
Y = 4425500
36 meter E =
0015003
Z = -4925187
70 I = 51
71813
XDOT = -7295
284535 Wp = 131
46039
YDOT = 38
413836 meter/sec RA = 165
23431 deg
ZDOT = 2308
782440 TA = 161
17225
MA = 161
11671
Ha = 226
993 n
mi
Hp = 219
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5048746
93 X = -1564307
22
Y = 14519358
15 feet Y = 4408149
92 meter
Z = -16158752
30 Z = -4932724
26
XDOT = -23934
660547 XDOT = -7306
386610
YDOT = 126
029645 feet/sec YDOT = -43
229445 meter/sec
ZDOT = 7574
745539 ZDOT = 2273
317916
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15334105
83 X = 4673835
46
Y = 221310
77 feet Y = 67455
52 meter
Z = -16193304
25 Z = -4935719
13
XDOT = 7534
050264 XDOT = 2296
378521
YDOT = 21658
584636 feet/sec YDOT = 6601
536597 meter/sec
ZDOT = 7413
541030 ZDOT = 2259
647306
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 19207
47050299
00016717 00000-0 10270-3 0 9103
2 25544 51
6388 166
3783 0006395 183
2636 176
8474 15
50992958 21349
Satellite: ISS
Catalog Number: 25544
Epoch time: 19207
47050299 = yrday
fracday
Element set: 910
Inclination: 51
6388 deg
RA of node: 166
3783 deg
Eccentricity:
0006395
Arg of perigee: 183
2636 deg
Mean anomaly: 176
8474 deg
Mean motion: 15
50992958 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2134
Checksum: 346
Coasting Arc #12 (Orbit 2149)
---------------------------------------
Vector Time (GMT): 2019/208/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 951979
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1956571
94 A = 6789307
88 meter
Y = -4568605
94 meter E =
0007236
Z = 4618240
38 I = 51
75347
XDOT = 7055
287281 Wp = 113
18505
YDOT = -14
923463 meter/sec RA = 160
27657 deg
ZDOT = -3002
864014 TA = 6
73098
MA = 6
72126
Ha = 226
799 n
mi
Hp = 219
490
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6419199
28 X = 1985081
29
Y = -14988864
62 feet Y = -4546567
27 meter
Z = 15151707
29 Z = 4627813
36
XDOT = 23147
267982 XDOT = 7069
515950
YDOT = -48
961492 feet/sec YDOT = 64
053600 meter/sec
ZDOT = -9851
916056 ZDOT = -2968
557728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16226995
68 X = -4945988
28
Y = -1107574
32 feet Y = -337588
65 meter
Z = 15195535
74 Z = 4631599
29
XDOT = -7665
890157 XDOT = -2336
563320
YDOT = -20755
555673 feet/sec YDOT = -6326
293369 meter/sec
ZDOT = -9695
955088 ZDOT = -2955
327111
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 19208
50140278
00016717 00000-0 10270-3 0 9116
2 25544 51
6381 161
2635 0006355 187
9560 172
1491 15
51017646 21504
Satellite: ISS
Catalog Number: 25544
Epoch time: 19208
50140278 = yrday
fracday
Element set: 911
Inclination: 51
6381 deg
RA of node: 161
2635 deg
Eccentricity:
0006355
Arg of perigee: 187
9560 deg
Mean anomaly: 172
1491 deg
Mean motion: 15
51017646 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2150
Checksum: 294
Coasting Arc #13 (Orbit 2164)
---------------------------------------
Vector Time (GMT): 2019/209/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936703
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2345059
87 A = 6790767
14 meter
Y = 4759340
42 meter E =
0011087
Z = -4249855
52 I = 51
78961
XDOT = -6731
370757 Wp = 145
11522
YDOT = -61
583215 meter/sec RA = 155
32196 deg
ZDOT = 3641
227545 TA = 162
16918
MA = 162
13024
Ha = 226
729 n
mi
Hp = 219
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7693765
96 X = -2377462
63
Y = 15614633
93 feet Y = 4732935
67 meter
Z = -13943095
54 Z = -4261324
95
XDOT = -22084
549729 XDOT = -6747
868732
YDOT = -202
044670 feet/sec YDOT = -136
950829 meter/sec
ZDOT = 11946
284595 ZDOT = 3608
489274
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17269330
77 X = 5263692
02
Y = 1820697
46 feet Y = 554948
58 meter
Z = -13995571
32 Z = -4265850
14
XDOT = 7500
779886 XDOT = 2286
237709
YDOT = 19645
599949 feet/sec YDOT = 5987
978864 meter/sec
ZDOT = 11797
433849 ZDOT = 3595
857837
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 19209
46786969
00016717 00000-0 10270-3 0 9126
2 25544 51
6385 156
4681 0006355 191
7397 168
3606 15
51001391 21657
Satellite: ISS
Catalog Number: 25544
Epoch time: 19209
46786969 = yrday
fracday
Element set: 912
Inclination: 51
6385 deg
RA of node: 156
4681 deg
Eccentricity:
0006355
Arg of perigee: 191
7397 deg
Mean anomaly: 168
3606 deg
Mean motion: 15
51001391 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2165
Checksum: 337
Coasting Arc #14 (Orbit 2180)
---------------------------------------
Vector Time (GMT): 2019/210/10:44:30
000
Vector Time (MET): N/A
Weight (LBS) : 936703
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3581942
44 A = 6787251
61 meter
Y = -2615798
90 meter E =
0009304
Z = 5137717
78 I = 51
80904
XDOT = 5796
340792 Wp = 165
82610
YDOT = -4745
205492 meter/sec RA = 150
46350 deg
ZDOT = 1615
752108 TA = 268
55952
MA = 268
66610
Ha = 226
613 n
mi
Hp = 219
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11751779
65 X = -3577381
46
Y = -8582017
39 feet Y = -2655829
87 meter
Z = 16856029
46 Z = 5120329
00
XDOT = 19016
866117 XDOT = 5841
123926
YDOT = -15568
259487 feet/sec YDOT = -4680
136555 meter/sec
ZDOT = 5301
023978 ZDOT = 1644
016341
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4728418
91 X = -1441222
09
Y = 13858242
32 feet Y = 4223992
26 meter
Z = 16777134
78 Z = 5113670
68
XDOT = -19434
958051 XDOT = -5923
775214
YDOT = -13242
321419 feet/sec YDOT = -4036
259569 meter/sec
ZDOT = 5429
886974 ZDOT = 1655
029550
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 19210
49876332
00016717 00000-0 10270-3 0 9136
2 25544 51
6400 151
3534 0006364 196
7691 163
3251 15
51046508 21816
Satellite: ISS
Catalog Number: 25544
Epoch time: 19210
49876332 = yrday
fracday
Element set: 913
Inclination: 51
6400 deg
RA of node: 151
3534 deg
Eccentricity:
0006364
Arg of perigee: 196
7691 deg
Mean anomaly: 163
3251 deg
Mean motion: 15
51046508 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2181
Checksum: 296
Coasting Arc #15 (Orbit 2195)
---------------------------------------
Vector Time (GMT): 2019/211/10:44:30
000
Vector Time (MET): N/A
Weight (LBS) : 936703
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3140418
57 A = 6786681
42 meter
Y = 2885771
61 meter E =
0012950
Z = -5289157
13 I = 51
83552
XDOT = -5868
459899 Wp = 109
21459
YDOT = 4841
335611 meter/sec RA = 145
50859 deg
ZDOT = -848
782931 TA = 152
71222
MA = 152
64412
Ha = 226
467 n
mi
Hp = 220
085
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10303210
53 X = 3133606
96
Y = 9467754
61 feet Y = 2920852
57 meter
Z = -17352877
71 Z = -5273918
60
XDOT = -19253
477358 XDOT = -5918
038111
YDOT = 15883
647018 feet/sec YDOT = 4775
433272 meter/sec
ZDOT = -2784
720901 ZDOT = -877
408985
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5778687
48 X = 1761343
94
Y = -12837247
80 feet Y = -3912793
13 meter
Z = -17283770
69 Z = -5268093
31
XDOT = 20118
610227 XDOT = 6132
152397
YDOT = 12955
511028 feet/sec YDOT = 3948
839761 meter/sec
ZDOT = -2915
261280 ZDOT = -888
571638
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 19211
46522480
00016717 00000-0 10270-3 0 9147
2 25544 51
6401 146
5573 0006251 199
5121 160
5792 15
51019794 21962
Satellite: ISS
Catalog Number: 25544
Epoch time: 19211
46522480 = yrday
fracday
Element set: 914
Inclination: 51
6401 deg
RA of node: 146
5573 deg
Eccentricity:
0006251
Arg of perigee: 199
5121 deg
Mean anomaly: 160
5792 deg
Mean motion: 15
51019794 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2196
Checksum: 303
Coasting Arc #16 (Orbit 2211)
---------------------------------------
Vector Time (GMT): 2019/212/10:44:30
000
Vector Time (MET): N/A
Weight (LBS) : 936703
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2739096
46 A = 6786360
70 meter
Y = -3173081
81 meter E =
0005953
Z = 5337189
53 I = 51
86201
XDOT = 5875
588841 Wp = 181
28270
YDOT = -4919
682646 meter/sec RA = 140
55777 deg
ZDOT = 84
746491 TA = 267
87764
MA = 267
94581
Ha = 226
356 n
mi
Hp = 220
133
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8986536
93 X = -2729335
07
Y = -10410373
40 feet Y = -3203658
34 meter
Z = 17510464
35 Z = 5323907
68
XDOT = 19276
866277 XDOT = 5929
753822
YDOT = -16140
691097 feet/sec YDOT = -4853
674840 meter/sec
ZDOT = 278
039669 ZDOT = 113
418234
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6876690
89 X = -2096015
38
Y = 11997887
99 feet Y = 3656956
26 meter
Z = 17450269
00 Z = 5318841
99
XDOT = -20663
098772 XDOT = -6298
112506
YDOT = -12465
589508 feet/sec YDOT = -3799
511682 meter/sec
ZDOT = 408
816494 ZDOT = 124
607267
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 19212
49611430
00016717 00000-0 10270-3 0 9156
2 25544 51
6406 141
4438 0006228 204
0095 156
0767 15
51040120 22125
Satellite: ISS
Catalog Number: 25544
Epoch time: 19212
49611430 = yrday
fracday
Element set: 915
Inclination: 51
6406 deg
RA of node: 141
4438 deg
Eccentricity:
0006228
Arg of perigee: 204
0095 deg
Mean anomaly: 156
0767 deg
Mean motion: 15
51040120 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2212
Checksum: 265
Coasting Arc #17 (Orbit 2214)
---------------------------------------
Vector Time (GMT): 2019/212/15:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 936703
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1866658
88 A = 6792482
22 meter
Y = -5386884
43 meter E =
0010142
Z = 3680584
25 I = 51
89036
XDOT = 6246
936084 Wp = 116
90946
YDOT = -823
983568 meter/sec RA = 139
53526 deg
ZDOT = -4369
412953 TA = 19
51408
MA = 19
47529
Ha = 226
151 n
mi
Hp = 220
151
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6124208
91 X = 1908880
03
Y = -17673505
35 feet Y = -5365774
47 meter
Z = 12075407
63 Z = 3689753
51
XDOT = 20495
197125 XDOT = 6276
909491
YDOT = -2703
358162 feet/sec YDOT = -753
957872 meter/sec
ZDOT = -14335
344333 ZDOT = -4338
995699
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5475191
00 X = -1668838
22
Y = 17856725
22 feet Y = 5442729
85 meter
Z = 12117501
53 Z = 3693414
47
XDOT = -19192
183283 XDOT = -5849
777465
YDOT = 3759
916444 feet/sec YDOT = 1146
022532 meter/sec
ZDOT = -14196
912302 ZDOT = -4327
218870
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 19212
68940476
00016717 00000-0 10270-3 0 9163
2 25544 51
6429 140
4861 0006160 205
4021 154
6828 15
51063957 22156
Satellite: ISS
Catalog Number: 25544
Epoch time: 19212
68940476 = yrday
fracday
Element set: 916
Inclination: 51
6429 deg
RA of node: 140
4861 deg
Eccentricity:
0006160
Arg of perigee: 205
4021 deg
Mean anomaly: 154
6828 deg
Mean motion: 15
51063957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2215
Checksum: 303
Coasting Arc #18 (Orbit 2227)
---------------------------------------
Vector Time (GMT): 2019/213/11:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 936703
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 475796
99 A = 6790456
77 meter
Y = -5217579
22 meter E =
0006846
Z = 4312710
16 I = 51
90301
XDOT = 6367
550467 Wp = 112
45041
YDOT = -2361
494935 meter/sec RA = 135
40374 deg
ZDOT = -3557
513629 TA = 13
68980
MA = 13
67124
Ha = 226
165 n
mi
Hp = 220
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1561013
75 X = 513157
91
Y = -17118042
06 feet Y = -5212050
00 meter
Z = 14149311
56 Z = 4315111
63
XDOT = 20890
913605 XDOT = 6410
764100
YDOT = -7747
686794 feet/sec YDOT = -2290
046580 meter/sec
ZDOT = -11671
632640 ZDOT = -3526
478529
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15078522
48 X = -4595933
65
Y = 8233011
91 feet Y = 2509422
03 meter
Z = 14160608
05 Z = 4316153
33
XDOT = -17441
260440 XDOT = -5316
096182
YDOT = -12100
337270 feet/sec YDOT = -3688
182800 meter/sec
ZDOT = -11530
264166 ZDOT = -3514
424518
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 19213
52700155
00016717 00000-0 10270-3 0 9176
2 25544 51
6419 136
3295 0006269 208
1012 151
9802 15
51034680 22287
Satellite: ISS
Catalog Number: 25544
Epoch time: 19213
52700155 = yrday
fracday
Element set: 917
Inclination: 51
6419 deg
RA of node: 136
3295 deg
Eccentricity:
0006269
Arg of perigee: 208
1012 deg
Mean anomaly: 151
9802 deg
Mean motion: 15
51034680 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2228
Checksum: 287
Coasting Arc #19 (Orbit 2242)
---------------------------------------
Vector Time (GMT): 2019/214/11:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 936703
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -729192
49 A = 6791952
89 meter
Y = 5534495
01 meter E =
0007529
Z = -3877073
07 I = 51
93156
XDOT = -6075
048403 Wp = 157
66092
YDOT = 2111
362578 meter/sec RA = 130
45941 deg
ZDOT = 4152
410921 TA = 155
90540
MA = 155
87016
Ha = 225
971 n
mi
Hp = 220
463
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2392363
80 X = -772194
45
Y = 18157792
02 feet Y = 5526100
45 meter
Z = -12720056
00 Z = -3880719
24
XDOT = -19931
261166 XDOT = -6118
376320
YDOT = 6927
042579 feet/sec YDOT = 2043
184621 meter/sec
ZDOT = 13623
395411 ZDOT = 4122
796298
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16267982
32 X = 4958481
01
Y = -8387440
63 feet Y = -2556491
90 meter
Z = -12737041
69 Z = -3882250
31
XDOT = 16441
991662 XDOT = 5011
519059
YDOT = 11386
343658 feet/sec YDOT = 3470
557547 meter/sec
ZDOT = 13488
491179 ZDOT = 4111
292111
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 19214
49345386
00016717 00000-0 10270-3 0 9185
2 25544 51
6424 131
5338 0006186 211
6253 148
4527 15
51044567 22439
Satellite: ISS
Catalog Number: 25544
Epoch time: 19214
49345386 = yrday
fracday
Element set: 918
Inclination: 51
6424 deg
RA of node: 131
5338 deg
Eccentricity:
0006186
Arg of perigee: 211
6253 deg
Mean anomaly: 148
4527 deg
Mean motion: 15
51044567 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2243
Checksum: 308
Coasting Arc #20 (Orbit 2257)
---------------------------------------
Vector Time (GMT): 2019/215/11:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 936703
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 921981
28 A = 6793513
51 meter
Y = -5822128
71 meter E =
0010343
Z = 3363816
98 I = 51
95732
XDOT = 5792
427411 Wp = 120
38789
YDOT = -1796
424960 meter/sec RA = 125
51967 deg
ZDOT = -4691
277279 TA = 20
61130
MA = 20
56961
Ha = 225
865 n
mi
Hp = 220
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3024872
97 X = 970678
32
Y = -19101472
16 feet Y = -5811546
29 meter
Z = 11036144
95 Z = 3368413
61
XDOT = 19004
026939 XDOT = 5834
872110
YDOT = -5893
782676 feet/sec YDOT = -1731
412503 meter/sec
ZDOT = -15391
329655 ZDOT = -4663
037493
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17263527
80 X = -5261923
27
Y = 8689954
54 feet Y = 2648698
14 meter
Z = 11057481
11 Z = 3370320
24
XDOT = -15261
045780 XDOT = -4651
566754
YDOT = -10873
338922 feet/sec YDOT = -3314
193703 meter/sec
ZDOT = -15262
691141 ZDOT = -4652
068260
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 19215
52433335
00016717 00000-0 10270-3 0 9193
2 25544 51
6422 126
4198 0006141 215
2873 144
7872 15
51041991 22589
Satellite: ISS
Catalog Number: 25544
Epoch time: 19215
52433335 = yrday
fracday
Element set: 919
Inclination: 51
6422 deg
RA of node: 126
4198 deg
Eccentricity:
0006141
Arg of perigee: 215
2873 deg
Mean anomaly: 144
7872 deg
Mean motion: 15
51041991 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2258
Checksum: 306
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