[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 3rd 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19800 2132 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 68 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 884 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
184/00:18:16
773 0
9 1
7 1
7
N/A -0
4 -0
2 228
6
000/00:00:33
545 1
3 0
1 217
1
184/09:50:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
5
000/00:00:00
000 0
0 0
0 217
0
187/16:56:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
4
000/00:00:00
000 0
0 0
0 217
2
194/07:45:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
2
000/00:00:00
000 0
0 0
0 217
7
Coasting Arc #1 (Orbit 1746)
---------------------------------------
Vector Time (GMT): 2019/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -993620
60 A = 6796748
56 meter
Y = 6532971
43 meter E =
0021995
Z = 1547931
73 I = 51
29734
XDOT = -5072
581877 Wp = 113
71612
YDOT = 597
239036 meter/sec RA = 289
46577 deg
ZDOT = -5720
736798 TA = 49
29106
MA = 49
10021
Ha = 228
488 n
mi
Hp = 216
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3259910
12 X = -1074119
29
Y = 21433633
30 feet Y = 6521409
67 meter
Z = 5078516
19 Z = 1542910
86
XDOT = -16642
328992 XDOT = -5051
095281
YDOT = 1959
445656 feet/sec YDOT = 540
635123 meter/sec
ZDOT = -18768
821516 ZDOT = -5745
325143
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21685152
24 X = 6609634
40
Y = 140729
03 feet Y = 42894
21 meter
Z = 5055031
63 Z = 1540773
64
XDOT = 4350
291663 XDOT = 1325
968899
YDOT = 14473
941132 feet/sec YDOT = 4411
657257 meter/sec
ZDOT = -18880
370152 ZDOT = -5754
736822
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 19182
53529039
00016717 00000-0 10270-3 0 9004
2 25544 51
6427 290
0903 0008200 107
5802 252
6245 15
51237824 17476
Satellite: ISS
Catalog Number: 25544
Epoch time: 19182
53529039 = yrday
fracday
Element set: 900
Inclination: 51
6427 deg
RA of node: 290
0903 deg
Eccentricity:
0008200
Arg of perigee: 107
5802 deg
Mean anomaly: 252
6245 deg
Mean motion: 15
51237824 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1747
Checksum: 294
Coasting Arc #2 (Orbit 1761)
---------------------------------------
Vector Time (GMT): 2019/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 916459
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1027554
44 A = 6797436
38 meter
Y = -6664799
37 meter E =
0014987
Z = -838612
39 I = 51
29039
XDOT = 4880
930654 Wp = 69
97220
YDOT = 21
212266 meter/sec RA = 284
48444 deg
ZDOT = 5903
346471 TA = 280
92837
MA = 281
09695
Ha = 228
446 n
mi
Hp = 216
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3371241
62 X = 1106079
25
Y = -21866139
66 feet Y = -6652869
31 meter
Z = -2751352
97 Z = -833431
56
XDOT = 16013
552015 XDOT = 4851
655740
YDOT = 69
594050 feet/sec YDOT = 75
629389 meter/sec
ZDOT = 19367
934615 ZDOT = 5926
984929
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22126514
77 X = -6744161
70
Y = 208131
15 feet Y = 63438
38 meter
Z = -2727141
81 Z = -831232
82
XDOT = -2495
448659 XDOT = -760
612751
YDOT = -14070
011932 feet/sec YDOT = -4288
539637 meter/sec
ZDOT = 19475
114339 ZDOT = 5936
014850
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 19183
50161033
00016717 00000-0 10270-3 0 9019
2 25544 51
6435 285
2952 0008092 109
9256 250
2768 15
51241213 17621
Satellite: ISS
Catalog Number: 25544
Epoch time: 19183
50161033 = yrday
fracday
Element set: 901
Inclination: 51
6435 deg
RA of node: 285
2952 deg
Eccentricity:
0008092
Arg of perigee: 109
9256 deg
Mean anomaly: 250
2768 deg
Mean motion: 15
51241213 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1762
Checksum: 294
Coasting Arc #3 (Orbit 1769)
---------------------------------------
Vector Time (GMT): 2019/184/00:18:33
545
Vector Time (MET): N/A
Weight (LBS) : 916291
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -327874
77 A = 6796771
18 meter
Y = -6467560
05 meter E =
0011839
Z = -2066167
20 I = 51
28065
XDOT = 4932
623393 Wp = 72
27024
YDOT = -1999
244375 meter/sec RA = 281
91822 deg
ZDOT = 5505
035712 TA = 264
80119
MA = 264
93631
Ha = 228
591 n
mi
Hp = 217
069
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1075704
62 X = -245492
11
Y = -21219029
04 feet Y = -6470765
54 meter
Z = -6778763
78 Z = -2067561
07
XDOT = 16183
147614 XDOT = 4927
872796
YDOT = -6559
200705 feet/sec YDOT = -1944
111975 meter/sec
ZDOT = 18061
140788 ZDOT = 5528
984367
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20286129
97 X = 6183212
42
Y = -6308795
88 feet Y = -1922920
98 meter
Z = -6784393
67 Z = -2067883
19
XDOT = 9909
488862 XDOT = 3020
412205
YDOT = 12429
270982 feet/sec YDOT = 3788
441795 meter/sec
ZDOT = 18169
946339 ZDOT = 5538
199644
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 19184
01698103
00016717 00000-0 10270-3 0 9020
2 25544 51
6428 282
7403 0007133 100
9727 259
2227 15
50950203 17708
Satellite: ISS
Catalog Number: 25544
Epoch time: 19184
01698103 = yrday
fracday
Element set: 902
Inclination: 51
6428 deg
RA of node: 282
7403 deg
Eccentricity:
0007133
Arg of perigee: 100
9727 deg
Mean anomaly: 259
2227 deg
Mean motion: 15
50950203 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1770
Checksum: 292
Coasting Arc #4 (Orbit 1776)
---------------------------------------
Vector Time (GMT): 2019/184/09:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 916291
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3324596
90 A = 6794679
10 meter
Y = -5113194
45 meter E =
0019952
Z = 2978264
30 I = 51
27137
XDOT = 3152
812342 Wp = 91
46441
YDOT = 4944
395446 meter/sec RA = 279
97660 deg
ZDOT = 4939
992247 TA = 302
76284
MA = 302
95495
Ha = 228
504 n
mi
Hp = 217
013
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10907470
13 X = 3367060
44
Y = -16775572
33 feet Y = -5075779
63 meter
Z = 9771208
32 Z = 2994515
88
XDOT = 10343
872514 XDOT = 3073
292947
YDOT = 16221
769835 feet/sec YDOT = 4979
206820 meter/sec
ZDOT = 16207
323644 ZDOT = 4955
115063
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11419929
55 X = -3480794
53
Y = -16386632
85 feet Y = -4994645
69 meter
Z = 9845441
42 Z = 3000890
54
XDOT = 17695
515798 XDOT = 5393
593215
YDOT = -2496
207216 feet/sec YDOT = -760
843959 meter/sec
ZDOT = 16275
375454 ZDOT = 4960
734438
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 19184
46801674
00016717 00000-0 10270-3 0 9039
2 25544 51
6428 280
4979 0007236 107
3224 252
8719 15
50985924 17778
Satellite: ISS
Catalog Number: 25544
Epoch time: 19184
46801674 = yrday
fracday
Element set: 903
Inclination: 51
6428 deg
RA of node: 280
4979 deg
Eccentricity:
0007236
Arg of perigee: 107
3224 deg
Mean anomaly: 252
8719 deg
Mean motion: 15
50985924 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1777
Checksum: 341
Coasting Arc #5 (Orbit 1791)
---------------------------------------
Vector Time (GMT): 2019/185/09:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 916291
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3260871
85 A = 6793265
94 meter
Y = 4809513
52 meter E =
0012209
Z = -3527646
45 I = 51
26145
XDOT = -3123
388798 Wp = 99
16608
YDOT = -5379
164230 meter/sec RA = 274
99108 deg
ZDOT = -4461
837431 TA = 122
53978
MA = 122
42178
Ha = 228
589 n
mi
Hp = 217
027
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10698398
45 X = -3297275
81
Y = 15779243
82 feet Y = 4772845
25 meter
Z = -11573643
22 Z = -3543573
83
XDOT = -10247
338577 XDOT = -3041
332563
YDOT = -17648
176609 feet/sec YDOT = -5413
632551 meter/sec
ZDOT = -14638
574250 ZDOT = -4476
811087
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10851750
20 X = 3307613
46
Y = 15620217
53 feet Y = 4761042
30 meter
Z = -11646364
42 Z = -3549811
88
XDOT = -18989
319327 XDOT = -5787
944531
YDOT = 2264
607279 feet/sec YDOT = 690
252299 meter/sec
ZDOT = -14705
924551 ZDOT = -4482
365803
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 19185
43452582
00016717 00000-0 10270-3 0 9048
2 25544 51
6426 275
7034 0007310 109
6742 250
5198 15
50949998 17922
Satellite: ISS
Catalog Number: 25544
Epoch time: 19185
43452582 = yrday
fracday
Element set: 904
Inclination: 51
6426 deg
RA of node: 275
7034 deg
Eccentricity:
0007310
Arg of perigee: 109
6742 deg
Mean anomaly: 250
5198 deg
Mean motion: 15
50949998 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1792
Checksum: 334
Coasting Arc #6 (Orbit 1807)
---------------------------------------
Vector Time (GMT): 2019/186/09:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 916291
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3185076
73 A = 6791737
42 meter
Y = -4487950
28 meter E =
0018075
Z = 3968758
89 I = 51
25446
XDOT = 3168
775524 Wp = 105
89346
YDOT = 5758
950910 meter/sec RA = 270
00407 deg
ZDOT = 3949
351880 TA = 302
69398
MA = 302
86816
Ha = 228
455 n
mi
Hp = 217
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10449726
80 X = 3215747
92
Y = -14724246
32 feet Y = -4452161
64 meter
Z = 13020862
50 Z = 3984304
30
XDOT = 10396
245159 XDOT = 3084
958406
YDOT = 18894
195898 feet/sec YDOT = 5793
917121 meter/sec
ZDOT = 12957
191208 ZDOT = 3964
541614
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10218725
88 X = -3114667
65
Y = -14823133
44 feet Y = -4518091
07 meter
Z = 13091808
00 Z = 3990383
08
XDOT = 20216
086476 XDOT = 6161
863158
YDOT = -2374
947254 feet/sec YDOT = -723
883923 meter/sec
ZDOT = 13025
505588 ZDOT = 3970
174103
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 19186
46546460
00016717 00000-0 10270-3 0 9052
2 25544 51
6422 270
5895 0007281 113
6717 246
5199 15
50989459 18080
Satellite: ISS
Catalog Number: 25544
Epoch time: 19186
46546460 = yrday
fracday
Element set: 905
Inclination: 51
6422 deg
RA of node: 270
5895 deg
Eccentricity:
0007281
Arg of perigee: 113
6717 deg
Mean anomaly: 246
5199 deg
Mean motion: 15
50989459 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1808
Checksum: 346
Coasting Arc #7 (Orbit 1822)
---------------------------------------
Vector Time (GMT): 2019/187/09:50:00
000
Vector Time (MET): N/A
Weight (LBS) : 916291
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3186044
21 A = 6790366
62 meter
Y = 4090462
71 meter E =
0014909
Z = -4397679
64 I = 51
25066
XDOT = -3220
180495 Wp = 90
56530
YDOT = -6086
356197 meter/sec RA = 265
01509 deg
ZDOT = -3338
213479 TA = 145
47170
MA = 145
37478
Ha = 228
522 n
mi
Hp = 217
130
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10452900
94 X = -3210187
08
Y = 13420153
24 feet Y = 4054699
69 meter
Z = -14428082
80 Z = -4413214
06
XDOT = -10564
896636 XDOT = -3135
666924
YDOT = -19968
360226 feet/sec YDOT = -6121
893548 meter/sec
ZDOT = -10952
143961 ZDOT = -3353
651106
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9243349
31 X = 2817372
87
Y = 14208264
44 feet Y = 4330679
00 meter
Z = -14498928
91 Z = -4419273
53
XDOT = -21277
975897 XDOT = -6485
527054
YDOT = 2628
931187 feet/sec YDOT = 801
298226 meter/sec
ZDOT = -11021
574011 ZDOT = -3359
375758
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 19187
43197118
00016717 00000-0 10270-3 0 9063
2 25544 51
6422 265
7950 0007244 117
2702 242
9188 15
50946063 18230
Satellite: ISS
Catalog Number: 25544
Epoch time: 19187
43197118 = yrday
fracday
Element set: 906
Inclination: 51
6422 deg
RA of node: 265
7950 deg
Eccentricity:
0007244
Arg of perigee: 117
2702 deg
Mean anomaly: 242
9188 deg
Mean motion: 15
50946063 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1823
Checksum: 317
Coasting Arc #8 (Orbit 1827)
---------------------------------------
Vector Time (GMT): 2019/187/16:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 916291
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4200750
66 A = 6786587
87 meter
Y = -624274
74 meter E =
0009558
Z = 5285799
48 I = 51
23639
XDOT = 966
748149 Wp = 109
94412
YDOT = 7608
395647 meter/sec RA = 263
51980 deg
ZDOT = 126
890213 TA = 338
82047
MA = 338
86002
Ha = 228
389 n
mi
Hp = 217
176
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13781990
35 X = 4181744
29
Y = -2048145
47 feet Y = -577405
90 meter
Z = 17341861
80 Z = 5306158
52
XDOT = 3171
745895 XDOT = 880
980689
YDOT = 24961
927976 feet/sec YDOT = 7618
726932 meter/sec
ZDOT = 416
306474 ZDOT = 131
378815
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13741489
30 X = -4188405
94
Y = 1447924
36 feet Y = 441327
34 meter
Z = 17434256
95 Z = 5313961
52
XDOT = -1969
556604 XDOT = -600
320853
YDOT = -24074
535029 feet/sec YDOT = -7337
918277 meter/sec
ZDOT = 435
940897 ZDOT = 132
874785
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 19187
75413806
00016717 00000-0 10270-3 0 9074
2 25544 51
6395 264
1995 0007213 114
6038 245
5865 15
50960168 18288
Satellite: ISS
Catalog Number: 25544
Epoch time: 19187
75413806 = yrday
fracday
Element set: 907
Inclination: 51
6395 deg
RA of node: 264
1995 deg
Eccentricity:
0007213
Arg of perigee: 114
6038 deg
Mean anomaly: 245
5865 deg
Mean motion: 15
50960168 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1828
Checksum: 336
Coasting Arc #9 (Orbit 1842)
---------------------------------------
Vector Time (GMT): 2019/188/16:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 916291
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4291633
79 A = 6786791
75 meter
Y = 143196
17 meter E =
0021521
Z = -5274391
73 I = 51
24206
XDOT = -1021
864211 Wp = 102
25000
YDOT = -7552
969938 meter/sec RA = 258
52589 deg
ZDOT = 624
098273 TA = 173
77075
MA = 173
74394
Ha = 228
558 n
mi
Hp = 217
058
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14080163
34 X = -4267296
44
Y = 469803
71 feet Y = 95340
70 meter
Z = -17304434
80 Z = -5295179
42
XDOT = -3352
572870 XDOT = -940
360264
YDOT = -24780
085100 feet/sec YDOT = -7563
941485 meter/sec
ZDOT = 2047
566514 ZDOT = 619
331741
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13971028
24 X = 4258369
41
Y = -98392
12 feet Y = -29989
92 meter
Z = -17398731
79 Z = -5303133
45
XDOT = 2701
150747 XDOT = 823
310748
YDOT = 23841
678817 feet/sec YDOT = 7266
943703 meter/sec
ZDOT = 2026
642169 ZDOT = 617
720533
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 19188
72064098
00016717 00000-0 10270-3 0 9088
2 25544 51
6399 259
4046 0007245 117
2278 242
9611 15
50939671 18438
Satellite: ISS
Catalog Number: 25544
Epoch time: 19188
72064098 = yrday
fracday
Element set: 908
Inclination: 51
6399 deg
RA of node: 259
4046 deg
Eccentricity:
0007245
Arg of perigee: 117
2278 deg
Mean anomaly: 242
9611 deg
Mean motion: 15
50939671 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1843
Checksum: 340
Coasting Arc #10 (Orbit 1858)
---------------------------------------
Vector Time (GMT): 2019/189/16:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 916291
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4401455
14 A = 6787189
31 meter
Y = 313822
48 meter E =
0009776
Z = 5148319
33 I = 51
25008
XDOT = 1065
936067 Wp = 96
72806
YDOT = 7472
699928 meter/sec RA = 253
53250 deg
ZDOT = -1365
696712 TA = 6
47438
MA = 6
46176
Ha = 228
293 n
mi
Hp = 217
307
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14440469
61 X = 4372611
38
Y = 1029601
32 feet Y = 362880
92 meter
Z = 16890811
44 Z = 5169629
67
XDOT = 3497
165573 XDOT = 988
928689
YDOT = 24516
732046 feet/sec YDOT = 7484
189517 meter/sec
ZDOT = -4480
632256 ZDOT = -1360
705236
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14316378
67 X = -4363632
22
Y = -1163990
54 feet Y = -354784
32 meter
Z = 16987441
85 Z = 5177772
28
XDOT = -3383
829181 XDOT = -1031
391134
YDOT = -23504
223972 feet/sec YDOT = -7164
087467 meter/sec
ZDOT = -4458
659314 ZDOT = -1358
999359
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 19189
75157562
00016717 00000-0 10270-3 0 9092
2 25544 51
6386 254
2896 0007108 120
7527 239
4335 15
50961510 18592
Satellite: ISS
Catalog Number: 25544
Epoch time: 19189
75157562 = yrday
fracday
Element set: 909
Inclination: 51
6386 deg
RA of node: 254
2896 deg
Eccentricity:
0007108
Arg of perigee: 120
7527 deg
Mean anomaly: 239
4335 deg
Mean motion: 15
50961510 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1859
Checksum: 338
Coasting Arc #11 (Orbit 1873)
---------------------------------------
Vector Time (GMT): 2019/190/16:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 916291
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4579609
97 A = 6788090
13 meter
Y = -746287
64 meter E =
0019489
Z = -4972734
82 I = 51
26341
XDOT = -1070
889300 Wp = 112
15529
YDOT = -7281
865594 meter/sec RA = 248
54092 deg
ZDOT = 2078
433260 TA = 178
23749
MA = 178
23061
Ha = 228
455 n
mi
Hp = 217
226
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15024967
08 X = -4546769
80
Y = -2448450
25 feet Y = -797315
98 meter
Z = -16314746
78 Z = -4994900
98
XDOT = -3513
416338 XDOT = -999
477596
YDOT = -23890
635150 feet/sec YDOT = -7293
441929 meter/sec
ZDOT = 6819
006759 ZDOT = 2073
404108
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14933824
26 X = 4551829
64
Y = 2331676
69 feet Y = 710695
06 meter
Z = -16415227
18 Z = -5003361
25
XDOT = 3917
776650 XDOT = 1194
138323
YDOT = 22772
334854 feet/sec YDOT = 6941
007664 meter/sec
ZDOT = 6796
828416 ZDOT = 2071
673301
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 19190
71807693
00016717 00000-0 10270-3 0 9109
2 25544 51
6386 249
4949 0007118 123
9058 236
2771 15
50938562 18749
Satellite: ISS
Catalog Number: 25544
Epoch time: 19190
71807693 = yrday
fracday
Element set: 910
Inclination: 51
6386 deg
RA of node: 249
4949 deg
Eccentricity:
0007118
Arg of perigee: 123
9058 deg
Mean anomaly: 236
2771 deg
Mean motion: 15
50938562 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1874
Checksum: 342
Coasting Arc #12 (Orbit 1889)
---------------------------------------
Vector Time (GMT): 2019/191/16:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 916291
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4765720
77 A = 6789096
86 meter
Y = 1143900
52 meter E =
0012549
Z = 4686751
53 I = 51
28071
XDOT = 1035
781314 Wp = 93
59085
YDOT = 7076
357382 meter/sec RA = 243
55070 deg
ZDOT = -2774
696385 TA = 24
05769
MA = 23
99912
Ha = 228
179 n
mi
Hp = 217
456
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15635566
82 X = 4729809
62
Y = 3752954
46 feet Y = 1196992
88 meter
Z = 15376481
38 Z = 4709814
40
XDOT = 3398
232656 XDOT = 970
052343
YDOT = 23216
395611 feet/sec YDOT = 7087
572988 meter/sec
ZDOT = -9103
334596 ZDOT = -2769
823883
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15621157
30 X = -4761328
75
Y = -3362999
32 feet Y = -1025042
19 meter
Z = 15481003
74 Z = 4718609
94
XDOT = -4286
158160 XDOT = -1306
421007
YDOT = -21982
542157 feet/sec YDOT = -6700
278849 meter/sec
ZDOT = -9081
834308 ZDOT = -2768
143097
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 19191
74900951
00016717 00000-0 10270-3 0 9115
2 25544 51
6390 244
3799 0007020 127
9084 232
2703 15
50968816 18900
Satellite: ISS
Catalog Number: 25544
Epoch time: 19191
74900951 = yrday
fracday
Element set: 911
Inclination: 51
6390 deg
RA of node: 244
3799 deg
Eccentricity:
0007020
Arg of perigee: 127
9084 deg
Mean anomaly: 232
2703 deg
Mean motion: 15
50968816 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1890
Checksum: 319
Coasting Arc #13 (Orbit 1904)
---------------------------------------
Vector Time (GMT): 2019/192/16:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 916291
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5003398
40 A = 6790471
08 meter
Y = -1489554
93 meter E =
0015648
Z = -4359073
61 I = 51
30146
XDOT = -947
418153 Wp = 119
45744
YDOT = -6783
173441 meter/sec RA = 238
56325 deg
ZDOT = 3407
099540 TA = 185
33249
MA = 185
34917
Ha = 228
326 n
mi
Hp = 217
406
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16415349
10 X = -4965196
04
Y = -4886991
26 feet Y = -1545292
31 meter
Z = -14301422
61 Z = -4383285
55
XDOT = -3108
327272 XDOT = -888
046081
YDOT = -22254
506040 feet/sec YDOT = -6793
436579 meter/sec
ZDOT = 11178
148096 ZDOT = 3402
640734
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16510933
71 X = 5032532
60
Y = 4193467
79 feet Y = 1278168
98 meter
Z = -14411139
92 Z = -4392515
45
XDOT = 4427
458800 XDOT = 1349
489442
YDOT = 20895
229248 feet/sec YDOT = 6368
865875 meter/sec
ZDOT = 11158
486883 ZDOT = 3401
106802
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 19192
71550725
00016717 00000-0 10270-3 0 9124
2 25544 51
6395 239
5850 0007001 130
2895 229
8869 15
50947218 19050
Satellite: ISS
Catalog Number: 25544
Epoch time: 19192
71550725 = yrday
fracday
Element set: 912
Inclination: 51
6395 deg
RA of node: 239
5850 deg
Eccentricity:
0007001
Arg of perigee: 130
2895 deg
Mean anomaly: 229
8869 deg
Mean motion: 15
50947218 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1905
Checksum: 328
Coasting Arc #14 (Orbit 1920)
---------------------------------------
Vector Time (GMT): 2019/193/16:56:00
000
Vector Time (MET): N/A
Weight (LBS) : 916291
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5230650
65 A = 6791866
78 meter
Y = 1793809
17 meter E =
0016015
Z = 3927633
01 I = 51
32398
XDOT = 796
153139 Wp = 100
42714
YDOT = 6489
290165 meter/sec RA = 233
57847 deg
ZDOT = -4012
908185 TA = 31
69260
MA = 31
59629
Ha = 228
065 n
mi
Hp = 217
617
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17160927
34 X = 5191124
85
Y = 5885200
69 feet Y = 1852080
42 meter
Z = 12885935
06 Z = 3952945
68
XDOT = 2612
050982 XDOT = 743
021248
YDOT = 21290
322064 feet/sec YDOT = 6497
896789 meter/sec
ZDOT = -13165
709270 ZDOT = -4009
168931
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17393718
85 X = -5301605
51
Y = -4860283
37 feet Y = -1481414
37 meter
Z = 13000635
63 Z = 3962593
74
XDOT = -4316
220092 XDOT = -1315
583884
YDOT = -19822
793410 feet/sec YDOT = -6041
987431 meter/sec
ZDOT = -13149
276412 ZDOT = -4007
899450
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 19193
74643726
00016717 00000-0 10270-3 0 9133
2 25544 51
6388 234
4704 0006895 134
1181 226
0538 15
50974326 19215
Satellite: ISS
Catalog Number: 25544
Epoch time: 19193
74643726 = yrday
fracday
Element set: 913
Inclination: 51
6388 deg
RA of node: 234
4704 deg
Eccentricity:
0006895
Arg of perigee: 134
1181 deg
Mean anomaly: 226
0538 deg
Mean motion: 15
50974326 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1921
Checksum: 322
Coasting Arc #15 (Orbit 1929)
---------------------------------------
Vector Time (GMT): 2019/194/07:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 916291
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5147178
97 A = 6797313
86 meter
Y = -4101590
21 meter E =
0009341
Z = -1705948
58 I = 51
35770
XDOT = 1935
097080 Wp = 86
95670
YDOT = -4772
950716 meter/sec RA = 230
51020 deg
ZDOT = 5664
425190 TA = 254
30512
MA = 254
40819
Ha = 228
237 n
mi
Hp = 217
702
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16887070
11 X = -5092644
77
Y = -13456660
78 feet Y = -4158844
40 meter
Z = -5596944
16 Z = -1730819
65
XDOT = 6348
743702 XDOT = 1960
811309
YDOT = -15659
287126 feet/sec YDOT = -4751
168171 meter/sec
ZDOT = 18584
072146 ZDOT = 5673
886852
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21371332
04 X = -6513982
00
Y = 2872077
44 feet Y = 875409
20 meter
Z = -5709463
94 Z = -1740244
61
XDOT = -6802
405419 XDOT = -2073
373172
YDOT = -13762
867540 feet/sec YDOT = -4194
922026 meter/sec
ZDOT = 18627
391958 ZDOT = 5677
629069
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 19194
32633497
00016717 00000-0 10270-3 0 9143
2 25544 51
6421 231
5914 0007106 139
1479 221
0206 15
50944564 19303
Satellite: ISS
Catalog Number: 25544
Epoch time: 19194
32633497 = yrday
fracday
Element set: 914
Inclination: 51
6421 deg
RA of node: 231
5914 deg
Eccentricity:
0007106
Arg of perigee: 139
1479 deg
Mean anomaly: 221
0206 deg
Mean motion: 15
50944564 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1930
Checksum: 300
Coasting Arc #16 (Orbit 1945)
---------------------------------------
Vector Time (GMT): 2019/195/07:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 916291
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5252909
43 A = 6798084
23 meter
Y = 4171220
92 meter E =
0020579
Z = 1035361
95 I = 51
38188
XDOT = -2294
086327 Wp = 130
70314
YDOT = 4363
238151 meter/sec RA = 225
53496 deg
ZDOT = -5875
725208 TA = 38
03782
MA = 37
89269
Ha = 228
181 n
mi
Hp = 217
764
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17233954
82 X = 5200846
07
Y = 13685107
99 feet Y = 4229671
36 meter
Z = 3396856
79 Z = 1060752
59
XDOT = -7526
529943 XDOT = -2314
166075
YDOT = 14315
085796 feet/sec YDOT = 4337
472732 meter/sec
ZDOT = -19277
313676 ZDOT = -5886
916989
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21731906
64 X = 6623885
14
Y = -3349904
11 feet Y = -1021050
77 meter
Z = 3511750
56 Z = 1070381
57
XDOT = 5246
661361 XDOT = 1599
182383
YDOT = 13562
750303 feet/sec YDOT = 4133
926292 meter/sec
ZDOT = -19328
450723 ZDOT = -5891
311780
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 19195
35726350
00016717 00000-0 10270-3 0 9159
2 25544 51
6416 226
4768 0007284 143
6598 216
5049 15
50958017 19465
Satellite: ISS
Catalog Number: 25544
Epoch time: 19195
35726350 = yrday
fracday
Element set: 915
Inclination: 51
6416 deg
RA of node: 226
4768 deg
Eccentricity:
0007284
Arg of perigee: 143
6598 deg
Mean anomaly: 216
5049 deg
Mean motion: 15
50958017 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1946
Checksum: 338
Coasting Arc #17 (Orbit 1960)
---------------------------------------
Vector Time (GMT): 2019/196/07:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 916291
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5355969
48 A = 6798472
86 meter
Y = -4166536
83 meter E =
0011718
Z = -397772
32 I = 51
40771
XDOT = 2669
036696 Wp = 78
04088
YDOT = -3986
361752 meter/sec RA = 220
56158 deg
ZDOT = 5969
469091 TA = 277
66540
MA = 277
79846
Ha = 228
083 n
mi
Hp = 217
926
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17572078
35 X = -5307047
88
Y = -13669740
27 feet Y = -4226157
44 meter
Z = -1305027
29 Z = -423671
12
XDOT = 8756
682073 XDOT = 2684
418998
YDOT = -13078
614671 feet/sec YDOT = -3956
429669 meter/sec
ZDOT = 19584
872346 ZDOT = 5982
470815
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21894062
11 X = -6673310
13
Y = 3996257
87 feet Y = 1218059
40 meter
Z = -1422251
79 Z = -433502
35
XDOT = -3719
027345 XDOT = -1133
559535
YDOT = -13546
737191 feet/sec YDOT = -4129
045496 meter/sec
ZDOT = 19644
194948 ZDOT = 5987
550620
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 19196
32375565
00016717 00000-0 10270-3 0 9166
2 25544 51
6420 221
6820 0007015 145
6028 214
5578 15
50958567 19610
Satellite: ISS
Catalog Number: 25544
Epoch time: 19196
32375565 = yrday
fracday
Element set: 916
Inclination: 51
6420 deg
RA of node: 221
6820 deg
Eccentricity:
0007015
Arg of perigee: 145
6028 deg
Mean anomaly: 214
5578 deg
Mean motion: 15
50958567 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1961
Checksum: 320
Coasting Arc #18 (Orbit 1976)
---------------------------------------
Vector Time (GMT): 2019/197/07:45:00
000
Vector Time (MET): N/A
Weight (LBS) : 916291
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5373619
30 A = 6798512
09 meter
Y = 4138322
44 meter E =
0018584
Z = -298284
55 I = 51
43246
XDOT = -3120
723740 Wp = 142
01516
YDOT = 3636
169363 meter/sec RA = 215
59091 deg
ZDOT = -5986
174480 TA = 41
20620
MA = 41
06606
Ha = 228
056 n
mi
Hp = 217
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17629984
57 X = 5328392
89
Y = 13577173
36 feet Y = 4198161
19 meter
Z = -978623
86 Z = -272291
17
XDOT = -10238
594946 XDOT = -3132
075485
YDOT = 11929
689510 feet/sec YDOT = 3601
208699 meter/sec
ZDOT = -19639
680051 ZDOT = -6001
360534
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21799714
70 X = 6644553
04
Y = -4488308
65 feet Y = -1368036
48 meter
Z = -860942
45 Z = -262415
26
XDOT = 2105
421394 XDOT = 641
732441
YDOT = 13853
939696 feet/sec YDOT = 4222
680819 meter/sec
ZDOT = -19708
893233 ZDOT = -6007
270658
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 19197
35468118
00016717 00000-0 10270-3 0 9178
2 25544 51
6406 216
5677 0007148 149
8314 210
3250 15
50966140 19772
Satellite: ISS
Catalog Number: 25544
Epoch time: 19197
35468118 = yrday
fracday
Element set: 917
Inclination: 51
6406 deg
RA of node: 216
5677 deg
Eccentricity:
0007148
Arg of perigee: 149
8314 deg
Mean anomaly: 210
3250 deg
Mean motion: 15
50966140 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1977
Checksum: 324
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