[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 26th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14929 5437 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 69 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 013 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
087/06:36:30
000 0
0 0
0 0
0
N/A 0
0 0
0 224
3
000/00:00:00
000 0
0 0
0 216
6
090/20:25:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
2
000/00:00:00
000 0
0 0
0 216
7
094/11:01:35
000 0
0 0
0 0
0
N/A 0
0 0
0 223
9
000/00:00:00
000 0
0 0
0 216
9
094/14:24:50
000 0
0 0
0 0
0
N/A 0
0 0
0 224
0
000/00:00:00
000 0
0 0
0 216
9
097/20:12:00
000 0
0 0
0 0
0
N/A 0
0 0
0 223
9
000/00:00:00
000 0
0 0
0 216
9
Coasting Arc #1 (Orbit 224)
---------------------------------------
Vector Time (GMT): 2019/084/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4541754
57 A = 6793413
21 meter
Y = -4833571
21 meter E =
0015898
Z = 1434553
63 I = 51
97770
XDOT = 2654
114481 Wp = 118
20257
YDOT = -4232
791722 meter/sec RA = 56
51944 deg
ZDOT = -5817
480433 TA = 46
23111
MA = 46
09966
Ha = 224
405 n
mi
Hp = 216
641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14900769
58 X = -4494334
93
Y = -15858173
26 feet Y = -4884095
04 meter
Z = 4706540
78 Z = 1412606
96
XDOT = 8707
724674 XDOT = 2729
507662
YDOT = -13887
111949 feet/sec YDOT = -4202
690428 meter/sec
ZDOT = -19086
221894 ZDOT = -5804
404286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15415972
06 X = -4698788
28
Y = -15387744
62 feet Y = -4690184
56 meter
Z = 4607736
96 Z = 1404438
23
XDOT = 7278
775470 XDOT = 2218
570763
YDOT = -13031
229690 feet/sec YDOT = -3971
918810 meter/sec
ZDOT = -19026
582768 ZDOT = -5799
302428
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19084
53496800
00016717 00000-0 10270-3 0 9004
2 25544 51
6387 57
0811 0002084 112
5331 247
6042 15
52439279 2255
Satellite: ISS
Catalog Number: 25544
Epoch time: 19084
53496800 = yrday
fracday
Element set: 900
Inclination: 51
6387 deg
RA of node: 57
0811 deg
Eccentricity:
0002084
Arg of perigee: 112
5331 deg
Mean anomaly: 247
6042 deg
Mean motion: 15
52439279 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 225
Checksum: 293
Coasting Arc #2 (Orbit 239)
---------------------------------------
Vector Time (GMT): 2019/085/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4404817
89 A = 6794159
76 meter
Y = 5157153
54 meter E =
0012237
Z = -314710
76 I = 51
96183
XDOT = -3418
562267 Wp = 52
83059
YDOT = 3277
372064 meter/sec RA = 51
57924 deg
ZDOT = 6026
643492 TA = 303
79545
MA = 303
91192
Ha = 224
378 n
mi
Hp = 216
589
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14451502
28 X = 4348350
46
Y = 16919795
07 feet Y = 5206095
55 meter
Z = -1032515
63 Z = -293451
25
XDOT = -11215
755470 XDOT = -3484
230797
YDOT = 10752
533018 feet/sec YDOT = 3238
776478 meter/sec
ZDOT = 19772
452403 ZDOT = 6009
877709
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15256222
06 X = 4650096
48
Y = 16203747
55 feet Y = 4938902
25 meter
Z = -936870
12 Z = -285558
01
XDOT = -9635
164625 XDOT = -2936
798178
YDOT = 10175
410114 feet/sec YDOT = 3101
465003 meter/sec
ZDOT = 19696
211782 ZDOT = 6003
405351
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19085
50055288
00016717 00000-0 10270-3 0 9014
2 25544 51
6394 52
2806 0002183 118
8369 241
3002 15
52455349 2404
Satellite: ISS
Catalog Number: 25544
Epoch time: 19085
50055288 = yrday
fracday
Element set: 901
Inclination: 51
6394 deg
RA of node: 52
2806 deg
Eccentricity:
0002183
Arg of perigee: 118
8369 deg
Mean anomaly: 241
3002 deg
Mean motion: 15
52455349 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 240
Checksum: 292
Coasting Arc #3 (Orbit 255)
---------------------------------------
Vector Time (GMT): 2019/086/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4108070
67 A = 6793901
28 meter
Y = -5335473
52 meter E =
0011904
Z = -864296
27 I = 51
93992
XDOT = 4236
920431 Wp = 136
54920
YDOT = -2306
524823 meter/sec RA = 46
63758 deg
ZDOT = -5956
803757 TA = 52
75575
MA = 52
64722
Ha = 224
320 n
mi
Hp = 216
660
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13477922
14 X = -4043904
31
Y = -17504834
37 feet Y = -5381054
10 meter
Z = -2835617
67 Z = -884095
57
XDOT = 13900
657581 XDOT = 4291
332524
YDOT = -7567
338657 feet/sec YDOT = -2258
840679 meter/sec
ZDOT = -19543
319414 ZDOT = -5936
090166
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14573613
87 X = -4442037
51
Y = -16588269
89 feet Y = -5056104
66 meter
Z = -2924623
03 Z = -891425
10
XDOT = 12297
051521 XDOT = 3748
141304
YDOT = -7406
497104 feet/sec YDOT = -2257
500317 meter/sec
ZDOT = -19449
316451 ZDOT = -5928
151654
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19086
53050777
00016717 00000-0 10270-3 0 9027
2 25544 51
6400 47
1588 0002017 116
9830 243
1528 15
52440774 2566
Satellite: ISS
Catalog Number: 25544
Epoch time: 19086
53050777 = yrday
fracday
Element set: 902
Inclination: 51
6400 deg
RA of node: 47
1588 deg
Eccentricity:
0002017
Arg of perigee: 116
9830 deg
Mean anomaly: 243
1528 deg
Mean motion: 15
52440774 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 256
Checksum: 297
Coasting Arc #4 (Orbit 267)
---------------------------------------
Vector Time (GMT): 2019/087/06:36:30
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3280199
52 A = 6791942
79 meter
Y = -5486196
06 meter E =
0008010
Z = -2291651
68 I = 51
91720
XDOT = 5308
893968 Wp = 131
66515
YDOT = -904
622611 meter/sec RA = 42
80849 deg
ZDOT = -5450
780275 TA = 73
72356
MA = 73
63547
Ha = 224
338 n
mi
Hp = 216
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10761809
44 X = -3207476
01
Y = -17999330
91 feet Y = -5522471
04 meter
Z = -7518542
25 Z = -2307408
67
XDOT = 17417
631128 XDOT = 5345
091887
YDOT = -2967
921953 feet/sec YDOT = -845
052728 meter/sec
ZDOT = -17883
137386 ZDOT = -5424
903819
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14967419
25 X = 4562069
39
Y = -14652675
69 feet Y = -4466135
55 meter
Z = -7589228
50 Z = -2313196
85
XDOT = 5951
148115 XDOT = 1813
909945
YDOT = 15251
310434 feet/sec YDOT = 4648
599420 meter/sec
ZDOT = -17765
927489 ZDOT = -5415
054699
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19087
30297294
00016717 00000-0 10270-3 0 9031
2 25544 51
6418 43
3181 0002228 123
7957 236
3407 15
52450731 2689
Satellite: ISS
Catalog Number: 25544
Epoch time: 19087
30297294 = yrday
fracday
Element set: 903
Inclination: 51
6418 deg
RA of node: 43
3181 deg
Eccentricity:
0002228
Arg of perigee: 123
7957 deg
Mean anomaly: 236
3407 deg
Mean motion: 15
52450731 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 268
Checksum: 304
Coasting Arc #5 (Orbit 283)
---------------------------------------
Vector Time (GMT): 2019/088/06:36:30
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2672617
26 A = 6789745
85 meter
Y = 5315944
51 meter E =
0014597
Z = 3258983
52 I = 51
88329
XDOT = -6001
019917 Wp = 92
51230
YDOT = 78
911931 meter/sec RA = 37
85813 deg
ZDOT = 4773
536447 TA = 305
12038
MA = 305
25711
Ha = 224
396 n
mi
Hp = 216
619
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8768429
32 X = 2597144
00
Y = 17440762
82 feet Y = 5345409
77 meter
Z = 10692203
16 Z = 3271782
39
XDOT = -19688
385556 XDOT = -6024
643352
YDOT = 258
897412 feet/sec YDOT = 11
672513 meter/sec
ZDOT = 15661
208815 ZDOT = 4744
328571
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14681413
53 X = -4474894
84
Y = 12817676
60 feet Y = 3906827
83 meter
Z = 10749513
12 Z = 3276451
60
XDOT = -4313
023045 XDOT = -1314
609424
YDOT = -18015
644236 feet/sec YDOT = -5491
168363 meter/sec
ZDOT = 15529
020000 ZDOT = 4733
245296
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 19088
33292610
00016717 00000-0 10270-3 0 9043
2 25544 51
6407 38
1967 0002289 123
5309 236
6062 15
52424371 2846
Satellite: ISS
Catalog Number: 25544
Epoch time: 19088
33292610 = yrday
fracday
Element set: 904
Inclination: 51
6407 deg
RA of node: 38
1967 deg
Eccentricity:
0002289
Arg of perigee: 123
5309 deg
Mean anomaly: 236
6062 deg
Mean motion: 15
52424371 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 284
Checksum: 303
Coasting Arc #6 (Orbit 298)
---------------------------------------
Vector Time (GMT): 2019/089/06:36:30
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1888499
29 A = 6787011
22 meter
Y = -5067003
96 meter E =
0008819
Z = -4109901
46 I = 51
84943
XDOT = 6587
487554 Wp = 82
54275
YDOT = 661
426660 meter/sec RA = 32
90180 deg
ZDOT = -3848
365453 TA = 147
76347
MA = 147
70954
Ha = 224
282 n
mi
Hp = 216
632
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6195863
81 X = -1811734
81
Y = -16624028
75 feet Y = -5087693
54 meter
Z = -13483928
66 Z = -4118888
21
XDOT = 21612
491974 XDOT = 6598
294764
YDOT = 2170
034974 feet/sec YDOT = 735
152724 meter/sec
ZDOT = -12625
870910 ZDOT = -3816
339980
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14369429
68 X = 4379802
17
Y = -10352973
11 feet Y = -3155586
21 meter
Z = -13524009
41 Z = -4122118
07
XDOT = 2992
874430 XDOT = 912
228126
YDOT = 20432
372990 feet/sec YDOT = 6227
787287 meter/sec
ZDOT = -12481
022926 ZDOT = -3804
215788
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 19089
29850224
00016717 00000-0 10270-3 0 9051
2 25544 51
6425 33
3959 0002160 129
2726 230
8617 15
52457293 2995
Satellite: ISS
Catalog Number: 25544
Epoch time: 19089
29850224 = yrday
fracday
Element set: 905
Inclination: 51
6425 deg
RA of node: 33
3959 deg
Eccentricity:
0002160
Arg of perigee: 129
2726 deg
Mean anomaly: 230
8617 deg
Mean motion: 15
52457293 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 299
Checksum: 320
Coasting Arc #7 (Orbit 314)
---------------------------------------
Vector Time (GMT): 2019/090/06:36:30
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1007397
11 A = 6784698
14 meter
Y = 4749350
32 meter E =
0009890
Z = 4734063
69 I = 51
81129
XDOT = -7039
389362 Wp = 119
68928
YDOT = -1271
665269 meter/sec RA = 27
93848 deg
ZDOT = 2764
625566 TA = 302
96274
MA = 303
05779
Ha = 224
306 n
mi
Hp = 216
663
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3305108
62 X = 931218
40
Y = 15581858
01 feet Y = 4760190
17 meter
Z = 15531705
03 Z = 4738771
81
XDOT = -23095
109457 XDOT = -7038
074960
YDOT = -4172
130148 feet/sec YDOT = -1350
377078 meter/sec
ZDOT = 9070
293852 ZDOT = 2730
434448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14019948
40 X = -4273280
27
Y = 7517582
57 feet Y = 2291359
17 meter
Z = 15552456
47 Z = 4740388
73
XDOT = -2066
177637 XDOT = -629
770944
YDOT = -22360
033449 feet/sec YDOT = -6815
338195 meter/sec
ZDOT = 8915
725819 ZDOT = 2717
513230
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 19090
32844957
00016717 00000-0 10270-3 0 9064
2 25544 51
6408 28
2743 0002210 129
2828 230
8520 15
52447281 3157
Satellite: ISS
Catalog Number: 25544
Epoch time: 19090
32844957 = yrday
fracday
Element set: 906
Inclination: 51
6408 deg
RA of node: 28
2743 deg
Eccentricity:
0002210
Arg of perigee: 129
2828 deg
Mean anomaly: 230
8520 deg
Mean motion: 15
52447281 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 315
Checksum: 295
Coasting Arc #8 (Orbit 323)
---------------------------------------
Vector Time (GMT): 2019/090/20:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3540834
86 A = 6789077
94 meter
Y = 4649794
19 meter E =
0013803
Z = 3444516
51 I = 51
80622
XDOT = -6025
684438 Wp = 97
57050
YDOT = 1171
261799 meter/sec RA = 25
08591 deg
ZDOT = 4595
545384 TA = 302
67340
MA = 302
80646
Ha = 224
158 n
mi
Hp = 216
732
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11616912
28 X = 3471844
97
Y = 15255230
29 feet Y = 4689004
84 meter
Z = 11300907
17 Z = 3461548
44
XDOT = -19769
305900 XDOT = -6060
656404
YDOT = 3842
722437 feet/sec YDOT = 1103
683236 meter/sec
ZDOT = 15077
248634 ZDOT = 4566
190074
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2863369
21 X = 872754
94
Y = -18914025
65 feet Y = -5764995
02 meter
Z = 11377431
84 Z = 3467841
22
XDOT = 15245
912551 XDOT = 4646
954145
YDOT = 11331
925490 feet/sec YDOT = 3453
970889 meter/sec
ZDOT = 14944
283186 ZDOT = 4555
017515
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 19090
90779416
00016717 00000-0 10270-3 0 9076
2 25544 51
6380 25
3904 0002199 141
3621 218
7688 15
52465867 3245
Satellite: ISS
Catalog Number: 25544
Epoch time: 19090
90779416 = yrday
fracday
Element set: 907
Inclination: 51
6380 deg
RA of node: 25
3904 deg
Eccentricity:
0002199
Arg of perigee: 141
3621 deg
Mean anomaly: 218
7688 deg
Mean motion: 15
52465867 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 324
Checksum: 325
Coasting Arc #9 (Orbit 338)
---------------------------------------
Vector Time (GMT): 2019/091/20:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2688811
49 A = 6786427
67 meter
Y = -4557597
41 meter E =
0009246
Z = -4257759
86 I = 51
76878
XDOT = 6719
260874 Wp = 82
19739
YDOT = -580
996194 meter/sec RA = 20
12370 deg
ZDOT = -3626
883353 TA = 150
74735
MA = 150
69554
Ha = 224
182 n
mi
Hp = 216
678
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8821560
02 X = -2616965
61
Y = -14952747
41 feet Y = -4587264
29 meter
Z = -13969028
41 Z = -4270646
06
XDOT = 22044
819139 XDOT = 6742
875620
YDOT = -1906
155491 feet/sec YDOT = -505
725035 meter/sec
ZDOT = -11899
223599 ZDOT = -3594
186512
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4323395
34 X = -1317770
90
Y = 16765902
66 feet Y = 5110247
13 meter
Z = -14026799
05 Z = -4275368
35
XDOT = -15837
010486 XDOT = -4827
120796
YDOT = -13900
144951 feet/sec YDOT = -4236
764181 meter/sec
ZDOT = -11751
218394 ZDOT = -3581
771367
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 19091
87336756
00016717 00000-0 10270-3 0 9080
2 25544 51
6399 20
5897 0002187 140
2414 219
8898 15
52471235 3395
Satellite: ISS
Catalog Number: 25544
Epoch time: 19091
87336756 = yrday
fracday
Element set: 908
Inclination: 51
6399 deg
RA of node: 20
5897 deg
Eccentricity:
0002187
Arg of perigee: 140
2414 deg
Mean anomaly: 219
8898 deg
Mean motion: 15
52471235 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 339
Checksum: 339
Coasting Arc #10 (Orbit 354)
---------------------------------------
Vector Time (GMT): 2019/092/20:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1733433
42 A = 6784170
01 meter
Y = 4423890
58 meter E =
0009021
Z = 4838227
18 I = 51
72963
XDOT = -7246
344866 Wp = 125
84882
YDOT = 87
336712 meter/sec RA = 15
15343 deg
ZDOT = 2507
917576 TA = 299
48869
MA = 299
57864
Ha = 224
074 n
mi
Hp = 216
807
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5687117
52 X = 1660334
06
Y = 14514076
71 feet Y = 4442866
85 meter
Z = 15873448
75 Z = 4846469
49
XDOT = -23774
097331 XDOT = -7258
964954
YDOT = 286
537770 feet/sec YDOT = 6
232719 meter/sec
ZDOT = 8228
076037 ZDOT = 2472
687029
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6004709
54 X = 1830235
47
Y = -14344911
50 feet Y = -4372329
02 meter
Z = 15910219
39 Z = 4849434
87
XDOT = 16367
007813 XDOT = 4988
663981
YDOT = 15830
902402 feet/sec YDOT = 4825
259052 meter/sec
ZDOT = 8068
679113 ZDOT = 2459
333394
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 19092
90330781
00016717 00000-0 10270-3 0 9098
2 25544 51
6399 15
4675 0002144 147
3129 212
8156 15
52476547 3555
Satellite: ISS
Catalog Number: 25544
Epoch time: 19092
90330781 = yrday
fracday
Element set: 909
Inclination: 51
6399 deg
RA of node: 15
4675 deg
Eccentricity:
0002144
Arg of perigee: 147
3129 deg
Mean anomaly: 212
8156 deg
Mean motion: 15
52476547 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 355
Checksum: 317
Coasting Arc #11 (Orbit 369)
---------------------------------------
Vector Time (GMT): 2019/093/20:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -661210
52 A = 6782649
07 meter
Y = -4303430
68 meter E =
0015182
Z = -5213945
37 I = 51
69253
XDOT = 7543
687998 Wp = 88
11284
YDOT = 351
652968 meter/sec RA = 10
17959 deg
ZDOT = -1249
562433 TA = 169
89521
MA = 169
86466
Ha = 224
154 n
mi
Hp = 216
747
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2169325
84 X = -587712
74
Y = -14118867
06 feet Y = -4310414
43 meter
Z = -17106119
97 Z = -5216978
29
XDOT = 24749
632541 XDOT = 7545
264734
YDOT = 1153
717086 feet/sec YDOT = 436
020444 meter/sec
ZDOT = -4099
614280 ZDOT = -1212
914247
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8077637
67 X = -2462063
96
Y = 11762137
36 feet Y = 3585099
47 meter
Z = -17119334
58 Z = -5217973
18
XDOT = -16550
563235 XDOT = -5044
611674
YDOT = -17078
989521 feet/sec YDOT = -5205
676006 meter/sec
ZDOT = -3933
871703 ZDOT = -1199
044095
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 19093
86887551
00016717 00000-0 10270-3 0 9108
2 25544 51
6404 10
6678 0002254 146
6071 213
5223 15
52475899 3701
Satellite: ISS
Catalog Number: 25544
Epoch time: 19093
86887551 = yrday
fracday
Element set: 910
Inclination: 51
6404 deg
RA of node: 10
6678 deg
Eccentricity:
0002254
Arg of perigee: 146
6071 deg
Mean anomaly: 213
5223 deg
Mean motion: 15
52475899 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 370
Checksum: 313
Coasting Arc #12 (Orbit 379)
---------------------------------------
Vector Time (GMT): 2019/094/11:01:35
000
Vector Time (MET): N/A
Weight (LBS) : 914819
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2662528
43 A = 6784622
56 meter
Y = 4087354
18 meter E =
0009363
Z = 4710905
03 I = 51
68042
XDOT = -7015
051605 Wp = 122
45430
YDOT = 1341
414161 meter/sec RA = 7
17016 deg
ZDOT = 2791
974463 TA = 299
84981
MA = 299
94283
Ha = 223
922 n
mi
Hp = 216
872
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8735329
48 X = 2593741
57
Y = 13409954
65 feet Y = 4116744
35 meter
Z = 15455725
17 Z = 4723671
10
XDOT = -23015
261170 XDOT = -7043
092200
YDOT = 4400
965094 feet/sec YDOT = 1262
810469 meter/sec
ZDOT = 9160
021203 ZDOT = 2757
829645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7914789
21 X = 2412427
75
Y = 13846138
40 feet Y = 4220302
99 meter
Z = 15512990
31 Z = 4728359
45
XDOT = -22265
863817 XDOT = -6786
635291
YDOT = 2605
372474 feet/sec YDOT = 794
117530 meter/sec
ZDOT = 9005
413595 ZDOT = 2744
850064
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 19094
51258494
00016717 00000-0 10270-3 0 9110
2 25544 51
6414 7
4711 0001790 148
5925 211
5334 15
52490258 3805
Satellite: ISS
Catalog Number: 25544
Epoch time: 19094
51258494 = yrday
fracday
Element set: 911
Inclination: 51
6414 deg
RA of node: 7
4711 deg
Eccentricity:
0001790
Arg of perigee: 148
5925 deg
Mean anomaly: 211
5334 deg
Mean motion: 15
52490258 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 380
Checksum: 299
Coasting Arc #13 (Orbit 381)
---------------------------------------
Vector Time (GMT): 2019/094/14:24:50
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4844613
39 A = 6787505
97 meter
Y = 2607491
19 meter E =
0011834
Z = 3965331
57 I = 51
68675
XDOT = -5329
323870 Wp = 86
79318
YDOT = -3787
861616 meter/sec RA = 6
42349 deg
ZDOT = -4009
295105 TA = 45
03150
MA = 44
93561
Ha = 224
042 n
mi
Hp = 216
896
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15894400
89 X = -4892672
47
Y = 8554761
11 feet Y = 2553047
05 meter
Z = 13009618
01 Z = 3941681
18
XDOT = -17484
658367 XDOT = -5267
095854
YDOT = -12427
367506 feet/sec YDOT = -3847
110352 meter/sec
ZDOT = -13153
855332 ZDOT = -4035
031472
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4354285
77 X = -1327186
30
Y = 17596478
89 feet Y = 5363406
77 meter
Z = 12902333
29 Z = 3932631
19
XDOT = -19598
077471 XDOT = -5973
494013
YDOT = 4906
915119 feet/sec YDOT = 1495
627728 meter/sec
ZDOT = -13269
823251 ZDOT = -4044
642127
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 19094
64132621
00016717 00000-0 10270-3 0 9128
2 25544 51
6430 6
8319 0001592 145
7392 214
3863 15
52503217 3827
Satellite: ISS
Catalog Number: 25544
Epoch time: 19094
64132621 = yrday
fracday
Element set: 912
Inclination: 51
6430 deg
RA of node: 6
8319 deg
Eccentricity:
0001592
Arg of perigee: 145
7392 deg
Mean anomaly: 214
3863 deg
Mean motion: 15
52503217 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 382
Checksum: 289
Coasting Arc #14 (Orbit 396)
---------------------------------------
Vector Time (GMT): 2019/095/14:24:50
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5574550
60 A = 6790164
16 meter
Y = -2319461
98 meter E =
0004970
Z = -3110921
07 I = 51
66207
XDOT = 4370
784250 Wp = 90
41385
YDOT = 3970
352548 meter/sec RA = 1
45438 deg
ZDOT = 4878
607569 TA = 233
85852
MA = 233
90452
Ha = 223
931 n
mi
Hp = 217
098
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18289208
00 X = 5615184
40
Y = -7609783
40 feet Y = -2256896
58 meter
Z = -10206433
95 Z = -3083742
88
XDOT = 14339
843341 XDOT = 4302
364064
YDOT = 13026
091036 feet/sec YDOT = 4018
847663 meter/sec
ZDOT = 16005
930343 ZDOT = 4899
672749
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6324616
76 X = 1927743
19
Y = -18838863
23 feet Y = -5742085
51 meter
Z = -10083237
66 Z = -3073370
84
XDOT = 17798
107259 XDOT = 5424
863093
YDOT = -2630
547258 feet/sec YDOT = -801
790804 meter/sec
ZDOT = 16100
736444 ZDOT = 4907
504468
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 19095
60688965
00016717 00000-0 10270-3 0 9133
2 25544 51
6429 2
0306 0001540 154
9556 205
1670 15
52467757 3974
Satellite: ISS
Catalog Number: 25544
Epoch time: 19095
60688965 = yrday
fracday
Element set: 913
Inclination: 51
6429 deg
RA of node: 2
0306 deg
Eccentricity:
0001540
Arg of perigee: 154
9556 deg
Mean anomaly: 205
1670 deg
Mean motion: 15
52467757 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 397
Checksum: 321
Coasting Arc #15 (Orbit 412)
---------------------------------------
Vector Time (GMT): 2019/096/14:24:50
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6135395
70 A = 6792369
19 meter
Y = 2021677
19 meter E =
0015112
Z = 2074370
91 I = 51
63640
XDOT = -3260
376219 Wp = 114
64539
YDOT = -4189
275079 meter/sec RA = 356
48745 deg
ZDOT = -5534
867180 TA = 42
40452
MA = 42
28784
Ha = 223
946 n
mi
Hp = 217
011
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20129250
98 X = -6167622
92
Y = 6632799
19 feet Y = 1952886
90 meter
Z = 6805678
83 Z = 2044488
69
XDOT = -10696
772373 XDOT = -3186
402645
YDOT = -13744
340810 feet/sec YDOT = -4225
321780 meter/sec
ZDOT = -18159
013059 ZDOT = -5550
524977
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7917505
10 X = -2413255
55
Y = 19705792
12 feet Y = 6006325
44 meter
Z = 6670300
19 Z = 2033107
50
XDOT = -15888
987350 XDOT = -4842
963344
YDOT = -184
508994 feet/sec YDOT = -56
238341 meter/sec
ZDOT = -18229
327990 ZDOT = -5556
299171
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 19096
63682025
00016717 00000-0 10270-3 0 9149
2 25544 51
6430 356
9090 0001544 152
8370 207
2862 15
52483545 4130
Satellite: ISS
Catalog Number: 25544
Epoch time: 19096
63682025 = yrday
fracday
Element set: 914
Inclination: 51
6430 deg
RA of node: 356
9090 deg
Eccentricity:
0001544
Arg of perigee: 152
8370 deg
Mean anomaly: 207
2862 deg
Mean motion: 15
52483545 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 413
Checksum: 303
Coasting Arc #16 (Orbit 427)
---------------------------------------
Vector Time (GMT): 2019/097/14:24:50
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6489706
79 A = 6793778
61 meter
Y = -1745950
76 meter E =
0009268
Z = -971752
95 I = 51
60600
XDOT = 2068
265942 Wp = 46
60290
YDOT = 4423
653763 meter/sec RA = 351
52148 deg
ZDOT = 5906
277979 TA = 302
87634
MA = 302
96550
Ha = 223
887 n
mi
Hp = 217
061
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21291688
95 X = 6513468
48
Y = -5728184
91 feet Y = -1673245
53 meter
Z = -3188165
85 Z = -940170
15
XDOT = 6785
649417 XDOT = 1989
955883
YDOT = 14513
299747 feet/sec YDOT = 4446
345135 meter/sec
ZDOT = 19377
552424 ZDOT = 5916
134440
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8997428
38 X = 2742416
17
Y = -20151573
68 feet Y = -6142199
66 meter
Z = -3045140
89 Z = -928158
94
XDOT = 13991
809874 XDOT = 4264
703650
YDOT = 3333
962159 feet/sec YDOT = 1016
191666 meter/sec
ZDOT = 19421
597959 ZDOT = 5919
703058
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 19097
60237765
00016717 00000-0 10270-3 0 9155
2 25544 51
6411 352
1075 0001508 159
1609 200
9604 15
52472372 4281
Satellite: ISS
Catalog Number: 25544
Epoch time: 19097
60237765 = yrday
fracday
Element set: 915
Inclination: 51
6411 deg
RA of node: 352
1075 deg
Eccentricity:
0001508
Arg of perigee: 159
1609 deg
Mean anomaly: 200
9604 deg
Mean motion: 15
52472372 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 428
Checksum: 300
Coasting Arc #17 (Orbit 431)
---------------------------------------
Vector Time (GMT): 2019/097/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2093883
89 A = 6782623
74 meter
Y = -3832165
63 meter E =
0014569
Z = -5202496
83 I = 51
56076
XDOT = 7211
727331 Wp = 88
55297
YDOT = -2239
083018 meter/sec RA = 350
33725 deg
ZDOT = -1255
930441 TA = 169
37157
MA = 169
34074
Ha = 223
939 n
mi
Hp = 216
893
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6869697
79 X = -2025604
72
Y = -12572721
88 feet Y = -3855199
49 meter
Z = -17068559
16 Z = -5212502
17
XDOT = 23660
522739 XDOT = 7242
330095
YDOT = -7346
072894 feet/sec YDOT = -2158
265411 meter/sec
ZDOT = -4120
506695 ZDOT = -1220
823630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3411635
77 X = -1039866
58
Y = 13859866
07 feet Y = 4224487
18 meter
Z = -17113347
10 Z = -5216148
20
XDOT = -21494
614454 XDOT = -6551
558485
YDOT = -10171
494605 feet/sec YDOT = -3100
271556 meter/sec
ZDOT = -3961
490405 ZDOT = -1207
462275
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 19097
85986093
00016717 00000-0 10270-3 0 9168
2 25544 51
6408 350
8234 0002122 162
3810 197
7416 15
52486651 4326
Satellite: ISS
Catalog Number: 25544
Epoch time: 19097
85986093 = yrday
fracday
Element set: 916
Inclination: 51
6408 deg
RA of node: 350
8234 deg
Eccentricity:
0002122
Arg of perigee: 162
3810 deg
Mean anomaly: 197
7416 deg
Mean motion: 15
52486651 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 432
Checksum: 318
Coasting Arc #18 (Orbit 447)
---------------------------------------
Vector Time (GMT): 2019/098/20:12:00
000
Vector Time (MET): N/A
Weight (LBS) : 929253
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1008945
65 A = 6782096
32 meter
Y = 4096065
51 meter E =
0003348
Z = 5307995
65 I = 51
52711
XDOT = -7429
708049 Wp = 121
89230
YDOT = 1898
050003 meter/sec RA = 345
34777 deg
ZDOT = -54
149912 TA = 328
61450
MA = 328
63447
Ha = 223
796 n
mi
Hp = 217
044
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3310189
15 X = 937283
65
Y = 13438535
12 feet Y = 4106947
81 meter
Z = 17414683
90 Z = 5312722
55
XDOT = -24375
682577 XDOT = -7450
117357
YDOT = 6227
198172 feet/sec YDOT = 1814
851690 meter/sec
ZDOT = -177
657191 ZDOT = -90
290801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6426212
33 X = 1958709
52
Y = -12228144
43 feet Y = -3727138
42 meter
Z = 17435569
18 Z = 5314361
49
XDOT = 21571
257441 XDOT = 6574
919268
YDOT = 10857
599596 feet/sec YDOT = 3309
396357 meter/sec
ZDOT = -341
298128 ZDOT = -104
027669
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 19098
88978613
00016717 00000-0 10270-3 0 9172
2 25544 51
6414 345
7012 0002042 168
5136 191
6062 15
52499215 4487
Satellite: ISS
Catalog Number: 25544
Epoch time: 19098
88978613 = yrday
fracday
Element set: 917
Inclination: 51
6414 deg
RA of node: 345
7012 deg
Eccentricity:
0002042
Arg of perigee: 168
5136 deg
Mean anomaly: 191
6062 deg
Mean motion: 15
52499215 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 448
Checksum: 323
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