[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 26th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14542 9041 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
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
9
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
4
216/18:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 225
8
000/00:00:00
000 0
0 0
0 220
9
Coasting Arc #1 (Orbit 2134)
---------------------------------------
Vector Time (GMT): 2019/207/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929147
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6069029
99 A = 6797631
16 meter
Y = -2722536
40 meter E =
0017500
Z = 1348158
36 I = 51
75165
XDOT = 3065
790979 Wp = 139
04933
YDOT = 3934
383619 meter/sec RA = 165
03273 deg
ZDOT = -5826
153929 TA = 26
29936
MA = 26
21061
Ha = 226
922 n
mi
Hp = 219
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19911515
71 X = 6092474
54
Y = -8932206
05 feet Y = -2654537
28 meter
Z = 4423091
75 Z = 1377695
97
XDOT = 10058
369355 XDOT = 3049
867776
YDOT = 12908
082741 feet/sec YDOT = 3968
578950 meter/sec
ZDOT = -19114
678245 ZDOT = -5811
299861
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18320161
01 X = -5583985
08
Y = -11807500
76 feet Y = -3598926
23 meter
Z = 4557535
49 Z = 1389136
82
XDOT = 4414
023468 XDOT = 1345
394353
YDOT = -14237
447352 feet/sec YDOT = -4339
573953 meter/sec
ZDOT = -19047
421748 ZDOT = -5805
654149
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
53495706
00016717 00000-0 10270-3 0 9005
2 25544 51
6393 166
0584 0006324 184
0196 176
0905 15
50999283 21353
Satellite: ISS
Catalog Number: 25544
Epoch time: 19207
53495706 = yrday
fracday
Element set: 900
Inclination: 51
6393 deg
RA of node: 166
0584 deg
Eccentricity:
0006324
Arg of perigee: 184
0196 deg
Mean anomaly: 176
0905 deg
Mean motion: 15
50999283 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2135
Checksum: 322
Coasting Arc #2 (Orbit 2149)
---------------------------------------
Vector Time (GMT): 2019/208/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929147
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6148882
15 A = 6798181
93 meter
Y = 2812604
83 meter E =
0006110
Z = -698492
89 I = 51
78466
XDOT = -2537
226259 Wp = 74
49110
YDOT = -4076
545457 meter/sec RA = 160
08518 deg
ZDOT = 5965
541545 TA = 277
99401
MA = 278
06334
Ha = 226
844 n
mi
Hp = 219
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20173497
87 X = -6176483
64
Y = 9227706
13 feet Y = 2743689
46 meter
Z = -2291643
35 Z = -728428
40
XDOT = -8324
233133 XDOT = -2520
429685
YDOT = -13374
492968 feet/sec YDOT = -4104
825244 meter/sec
ZDOT = 19571
986697 ZDOT = 5953
257075
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18920154
83 X = 5766863
19
Y = 11554442
06 feet Y = 3521793
94 meter
Z = -2427924
25 Z = -740031
31
XDOT = -5518
243627 XDOT = -1681
960657
YDOT = 13107
633977 feet/sec YDOT = 3995
206836 meter/sec
ZDOT = 19516
415344 ZDOT = 5948
603397
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
50143343
00016717 00000-0 10270-3 0 9011
2 25544 51
6385 161
2637 0006353 187
4911 172
6146 15
51006213 21503
Satellite: ISS
Catalog Number: 25544
Epoch time: 19208
50143343 = yrday
fracday
Element set: 901
Inclination: 51
6385 deg
RA of node: 161
2637 deg
Eccentricity:
0006353
Arg of perigee: 187
4911 deg
Mean anomaly: 172
6146 deg
Mean motion: 15
51006213 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2150
Checksum: 278
Coasting Arc #3 (Orbit 2165)
---------------------------------------
Vector Time (GMT): 2019/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949153
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6157198
95 A = 6798463
15 meter
Y = -2858663
85 meter E =
0016431
Z = 6691
64 I = 51
81764
XDOT = 2006
648828 Wp = 153
52936
YDOT = 4294
672966 meter/sec RA = 155
13992 deg
ZDOT = -6027
689337 TA = 26
39878
MA = 26
31516
Ha = 226
754 n
mi
Hp = 219
696
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20200783
94 X = 6188675
23
Y = -9378818
41 feet Y = -2789633
73 meter
Z = 21954
19 Z = 36676
83
XDOT = 6583
493530 XDOT = 1987
754325
YDOT = 14090
134402 feet/sec YDOT = 4317
007830 meter/sec
ZDOT = -19775
883650 ZDOT = -6017
987228
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19264443
44 X = -5871802
36
Y = -11175441
33 feet Y = -3406274
52 meter
Z = 158488
41 Z = 48307
27
XDOT = 6879
163466 XDOT = 2096
769024
YDOT = -12174
849290 feet/sec YDOT = -3710
894064 meter/sec
ZDOT = -19732
064183 ZDOT = -6014
333163
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
53234192
00016717 00000-0 10270-3 0 9029
2 25544 51
6398 156
1486 0006337 192
2040 167
8958 15
50992959 21665
Satellite: ISS
Catalog Number: 25544
Epoch time: 19209
53234192 = yrday
fracday
Element set: 902
Inclination: 51
6398 deg
RA of node: 156
1486 deg
Eccentricity:
0006337
Arg of perigee: 192
2040 deg
Mean anomaly: 167
8958 deg
Mean motion: 15
50992959 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2166
Checksum: 338
Coasting Arc #4 (Orbit 2180)
---------------------------------------
Vector Time (GMT): 2019/210/10:44:30
000
Vector Time (MET): N/A
Weight (LBS) : 949153
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3607762
79 A = 6787340
31 meter
Y = -2594627
88 meter E =
0009317
Z = 5130482
19 I = 51
80913
XDOT = 5775
935291 Wp = 165
42204
YDOT = -4759
974029 meter/sec RA = 150
46394 deg
ZDOT = 1644
951238 TA = 268
67490
MA = 268
78164
Ha = 226
633 n
mi
Hp = 219
859
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11836492
08 X = -3603401
49
Y = -8512558
66 feet Y = -2634948
71 meter
Z = 16832290
65 Z = 5112967
51
XDOT = 18949
918933 XDOT = 5820
743255
YDOT = -15616
712692 feet/sec YDOT = -4695
133145 meter/sec
ZDOT = 5396
821647 ZDOT = 1673
116408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4637238
99 X = -1413430
45
Y = 13918734
87 feet Y = 4242430
39 meter
Z = 16752821
93 Z = 5106260
12
XDOT = -19457
066624 XDOT = -5930
513907
YDOT = -13170
152505 feet/sec YDOT = -4014
262483 meter/sec
ZDOT = 5525
235174 ZDOT = 1684
091681
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
49881567
00016717 00000-0 10270-3 0 9031
2 25544 51
6398 151
3537 0006324 196
8080 163
2862 15
51027211 21811
Satellite: ISS
Catalog Number: 25544
Epoch time: 19210
49881567 = yrday
fracday
Element set: 903
Inclination: 51
6398 deg
RA of node: 151
3537 deg
Eccentricity:
0006324
Arg of perigee: 196
8080 deg
Mean anomaly: 163
2862 deg
Mean motion: 15
51027211 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2181
Checksum: 306
Coasting Arc #5 (Orbit 2195)
---------------------------------------
Vector Time (GMT): 2019/211/10:44:30
000
Vector Time (MET): N/A
Weight (LBS) : 949153
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3173642
57 A = 6786771
27 meter
Y = 2858318
77 meter E =
0012886
Z = -5284302
25 I = 51
83558
XDOT = -5845
771742 Wp = 108
79002
YDOT = 4861
903785 meter/sec RA = 145
50928 deg
ZDOT = -886
819152 TA = 152
77062
MA = 152
70300
Ha = 226
492 n
mi
Hp = 220
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10412213
15 X = 3167111
89
Y = 9377686
26 feet Y = 2893772
84 meter
Z = -17336949
65 Z = -5268901
66
XDOT = -19179
041149 XDOT = -5895
396884
YDOT = 15951
127902 feet/sec YDOT = 4796
254903 meter/sec
ZDOT = -2909
511655 ZDOT = -915
335110
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5659350
77 X = 1724970
11
Y = -12912934
92 feet Y = -3935862
56 meter
Z = -17267103
58 Z = -5263013
17
XDOT = 20153
966360 XDOT = 6142
928947
YDOT = 12871
757819 feet/sec YDOT = 3923
311783 meter/sec
ZDOT = -3039
552719 ZDOT = -926
455669
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
46529061
00016717 00000-0 10270-3 0 9048
2 25544 51
6400 146
5576 0006205 199
5214 160
5700 15
50996815 21962
Satellite: ISS
Catalog Number: 25544
Epoch time: 19211
46529061 = yrday
fracday
Element set: 904
Inclination: 51
6400 deg
RA of node: 146
5576 deg
Eccentricity:
0006205
Arg of perigee: 199
5214 deg
Mean anomaly: 160
5700 deg
Mean motion: 15
50996815 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2196
Checksum: 304
Coasting Arc #6 (Orbit 2211)
---------------------------------------
Vector Time (GMT): 2019/212/10:44:30
000
Vector Time (MET): N/A
Weight (LBS) : 949153
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2780318
15 A = 6786439
90 meter
Y = -3138447
23 meter E =
0006001
Z = 5336474
18 I = 51
86200
XDOT = 5850
908700 Wp = 181
03089
YDOT = -4947
861493 meter/sec RA = 140
55874 deg
ZDOT = 132
596518 TA = 267
67427
MA = 267
74298
Ha = 226
384 n
mi
Hp = 220
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9121778
70 X = -2770937
51
Y = -10296742
87 feet Y = -3169486
85 meter
Z = 17508117
38 Z = 5322991
17
XDOT = 19195
894685 XDOT = 5905
158196
YDOT = -16233
141380 feet/sec YDOT = -4882
129210 meter/sec
ZDOT = 435
027946 ZDOT = 161
148578
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6725216
41 X = -2049845
96
Y = 12088731
62 feet Y = 3684645
40 meter
Z = 17447004
52 Z = 5317846
98
XDOT = -20717
160419 XDOT = -6314
590496
YDOT = -12368
975196 feet/sec YDOT = -3770
063640 meter/sec
ZDOT = 565
262322 ZDOT = 172
291956
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
49619657
00016717 00000-0 10270-3 0 9054
2 25544 51
6404 141
4442 0006178 204
0505 156
0359 15
51014697 22125
Satellite: ISS
Catalog Number: 25544
Epoch time: 19212
49619657 = yrday
fracday
Element set: 905
Inclination: 51
6404 deg
RA of node: 141
4442 deg
Eccentricity:
0006178
Arg of perigee: 204
0505 deg
Mean anomaly: 156
0359 deg
Mean motion: 15
51014697 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2212
Checksum: 293
Coasting Arc #7 (Orbit 2214)
---------------------------------------
Vector Time (GMT): 2019/212/15:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 949153
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1820864
77 A = 6792459
99 meter
Y = -5380730
80 meter E =
0010003
Z = 3712522
24 I = 51
89001
XDOT = 6264
119950 Wp = 116
27350
YDOT = -874
266404 meter/sec RA = 139
53585 deg
ZDOT = -4334
735075 TA = 19
67543
MA = 19
63686
Ha = 226
180 n
mi
Hp = 220
193
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5973965
78 X = 1862865
38
Y = -17653316
28 feet Y = -5360134
18 meter
Z = 12180191
08 Z = 3721468
53
XDOT = 20551
574639 XDOT = 6294
485915
YDOT = -2868
328098 feet/sec YDOT = -804
046355 meter/sec
ZDOT = -14221
571768 ZDOT = -4304
233402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5324968
24 X = -1623050
32
Y = 17831717
98 feet Y = 5435107
64 meter
Z = 12221270
16 Z = 3725043
15
XDOT = -19244
319533 XDOT = -5865
668594
YDOT = 3915
616736 feet/sec YDOT = 1193
479981 meter/sec
ZDOT = -14082
752145 ZDOT = -4292
422854
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
68949039
00016717 00000-0 10270-3 0 9066
2 25544 51
6428 140
4865 0006108 205
4474 154
6377 15
51037600 22158
Satellite: ISS
Catalog Number: 25544
Epoch time: 19212
68949039 = yrday
fracday
Element set: 906
Inclination: 51
6428 deg
RA of node: 140
4865 deg
Eccentricity:
0006108
Arg of perigee: 205
4474 deg
Mean anomaly: 154
6377 deg
Mean motion: 15
51037600 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2215
Checksum: 308
Coasting Arc #8 (Orbit 2227)
---------------------------------------
Vector Time (GMT): 2019/213/11:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 949153
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 420733
27 A = 6790434
32 meter
Y = -5196975
54 meter E =
0006687
Z = 4343330
51 I = 51
90262
XDOT = 6372
460205 Wp = 111
91352
YDOT = -2418
841390 meter/sec RA = 135
40468 deg
ZDOT = -3509
645607 TA = 13
66642
MA = 13
64832
Ha = 226
201 n
mi
Hp = 220
360
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1380358
50 X = 457719
15
Y = -17050444
68 feet Y = -5192064
18 meter
Z = 14249772
02 Z = 4345463
60
XDOT = 20907
021671 XDOT = 6416
082228
YDOT = -7935
831332 feet/sec YDOT = -2347
335852 meter/sec
ZDOT = -11514
585325 ZDOT = -3478
585671
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14922009
20 X = -4548228
40
Y = 8346825
14 feet Y = 2544112
30 meter
Z = 14259845
99 Z = 4346401
06
XDOT = -17598
103989 XDOT = -5363
902096
YDOT = -12020
378287 feet/sec YDOT = -3663
811302 meter/sec
ZDOT = -11373
099787 ZDOT = -3466
520815
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
52710266
00016717 00000-0 10270-3 0 9079
2 25544 51
6417 136
3301 0006213 208
0884 151
9933 15
51004486 22284
Satellite: ISS
Catalog Number: 25544
Epoch time: 19213
52710266 = yrday
fracday
Element set: 907
Inclination: 51
6417 deg
RA of node: 136
3301 deg
Eccentricity:
0006213
Arg of perigee: 208
0884 deg
Mean anomaly: 151
9933 deg
Mean motion: 15
51004486 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2228
Checksum: 287
Coasting Arc #9 (Orbit 2242)
---------------------------------------
Vector Time (GMT): 2019/214/11:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 949153
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -665765
54 A = 6791910
34 meter
Y = 5512138
26 meter E =
0007685
Z = -3920208
69 I = 51
93108
XDOT = -6084
259573 Wp = 156
66021
YDOT = 2184
412022 meter/sec RA = 130
46046 deg
ZDOT = 4100
634841 TA = 156
23193
MA = 156
19641
Ha = 226
011 n
mi
Hp = 220
512
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2184270
14 X = -708312
69
Y = 18084443
11 feet Y = 5504455
53 meter
Z = -12861577
06 Z = -3923545
67
XDOT = -19961
481539 XDOT = -6128
152172
YDOT = 7166
706110 feet/sec YDOT = 2116
127905 meter/sec
ZDOT = 13453
526382 ZDOT = 4070
974107
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16089089
74 X = 4903954
55
Y = -8518120
28 feet Y = -2596323
06 meter
Z = -12877154
23 Z = -3924956
61
XDOT = 16646
406278 XDOT = 5073
824633
YDOT = 11287
555000 feet/sec YDOT = 3440
446764 meter/sec
ZDOT = 13318
407130 ZDOT = 4059
450493
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
49357483
00016717 00000-0 10270-3 0 9085
2 25544 51
6422 131
5345 0006125 211
6110 148
4674 15
51011122 22434
Satellite: ISS
Catalog Number: 25544
Epoch time: 19214
49357483 = yrday
fracday
Element set: 908
Inclination: 51
6422 deg
RA of node: 131
5345 deg
Eccentricity:
0006125
Arg of perigee: 211
6110 deg
Mean anomaly: 148
4674 deg
Mean motion: 15
51011122 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2243
Checksum: 273
Coasting Arc #10 (Orbit 2258)
---------------------------------------
Vector Time (GMT): 2019/215/11:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 949153
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 850079
88 A = 6793458
79 meter
Y = -5799358
68 meter E =
0010142
Z = 3421764
33 I = 51
95675
XDOT = 5806
413907 Wp = 119
27141
YDOT = -1888
304286 meter/sec RA = 125
52083 deg
ZDOT = -4637
384945 TA = 20
92413
MA = 20
88265
Ha = 225
912 n
mi
Hp = 220
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2788975
97 X = 898246
17
Y = -19026767
33 feet Y = -5789583
28 meter
Z = 11226260
92 Z = 3426010
41
XDOT = 19049
914394 XDOT = 5849
623215
YDOT = -6195
224034 feet/sec YDOT = -1823
131149 meter/sec
ZDOT = -15214
517537 ZDOT = -4609
075366
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17064972
20 X = -5201403
53
Y = 8839649
27 feet Y = 2694325
10 meter
Z = 11246000
22 Z = 3427780
87
XDOT = -15521
482770 XDOT = -4730
947948
YDOT = -10749
162134 feet/sec YDOT = -3276
344619 meter/sec
ZDOT = -15085
554816 ZDOT = -4598
077108
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
52447818
00016717 00000-0 10270-3 0 9093
2 25544 51
6420 126
4206 0006073 215
2651 144
8099 15
51004159 22593
Satellite: ISS
Catalog Number: 25544
Epoch time: 19215
52447818 = yrday
fracday
Element set: 909
Inclination: 51
6420 deg
RA of node: 126
4206 deg
Eccentricity:
0006073
Arg of perigee: 215
2651 deg
Mean anomaly: 144
8099 deg
Mean motion: 15
51004159 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2259
Checksum: 300
Coasting Arc #11 (Orbit 2273)
---------------------------------------
Vector Time (GMT): 2019/216/11:38:30
000
Vector Time (MET): N/A
Weight (LBS) : 949153
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -976993
41 A = 6794864
41 meter
Y = 6078288
37 meter E =
0002724
Z = -2879658
08 I = 51
98020
XDOT = -5518
497762 Wp = 174
74603
YDOT = 1523
239656 meter/sec RA = 120
58278 deg
ZDOT = 5085
231215 TA = 152
71834
MA = 152
70403
Ha = 225
723 n
mi
Hp = 220
820
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3205358
96 X = -1030902
47
Y = 19941890
96 feet Y = 6067061
55 meter
Z = -9447697
10 Z = -2884534
71
XDOT = -18105
307617 XDOT = -5559
821653
YDOT = 4997
505432 feet/sec YDOT = 1461
296815 meter/sec
ZDOT = 16683
829447 ZDOT = 5058
324615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17900952
51 X = 5456210
33
Y = -9331720
30 feet Y = -2844308
35 meter
Z = -9470333
53 Z = -2886557
66
XDOT = 14170
824599 XDOT = 4319
267338
YDOT = 10368
997130 feet/sec YDOT = 3160
470325 meter/sec
ZDOT = 16561
267406 ZDOT = 5047
874305
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 19216
49094963
00016717 00000-0 10270-3 0 9101
2 25544 51
6421 121
6252 0006132 219
2557 140
8150 15
51019162 22748
Satellite: ISS
Catalog Number: 25544
Epoch time: 19216
49094963 = yrday
fracday
Element set: 910
Inclination: 51
6421 deg
RA of node: 121
6252 deg
Eccentricity:
0006132
Arg of perigee: 219
2557 deg
Mean anomaly: 140
8150 deg
Mean motion: 15
51019162 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2274
Checksum: 283
Coasting Arc #12 (Orbit 2278)
---------------------------------------
Vector Time (GMT): 2019/216/18:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949153
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3782299
20 A = 6798207
62 meter
Y = 5600430
17 meter E =
0007128
Z = 713584
97 I = 51
99204
XDOT = -3574
641893 Wp = 64
75367
YDOT = -3181
845202 meter/sec RA = 119
30001 deg
ZDOT = 5981
342723 TA = 302
90497
MA = 302
97353
Ha = 225
805 n
mi
Hp = 220
877
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12409118
12 X = -3848109
85
Y = 18374114
72 feet Y = 5557765
86 meter
Z = 2341158
05 Z = 695052
55
XDOT = -11727
827732 XDOT = -3567
849404
YDOT = -10439
124678 feet/sec YDOT = -3221
781440 meter/sec
ZDOT = 19623
827831 ZDOT = 5963
995247
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3108366
14 X = -947430
00
Y = -21961830
90 feet Y = -6693966
06 meter
Z = 2256406
13 Z = 687752
59
XDOT = 14195
838424 XDOT = 4326
891552
YDOT = 14
162704 feet/sec YDOT = 4
316792 meter/sec
ZDOT = 19545
111821 ZDOT = 5957
350083
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 19216
81310566
00016717 00000-0 10270-3 0 9118
2 25544 51
6385 120
0228 0006389 219
0670 141
0020 15
51010125 22795
Satellite: ISS
Catalog Number: 25544
Epoch time: 19216
81310566 = yrday
fracday
Element set: 911
Inclination: 51
6385 deg
RA of node: 120
0228 deg
Eccentricity:
0006389
Arg of perigee: 219
0670 deg
Mean anomaly: 141
0020 deg
Mean motion: 15
51010125 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2279
Checksum: 267
Coasting Arc #13 (Orbit 2293)
---------------------------------------
Vector Time (GMT): 2019/217/18:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 949153
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3695741
34 A = 6797506
05 meter
Y = -5523631
91 meter E =
0011366
Z = -1392331
03 I = 52
00647
XDOT = 3329
169967 Wp = 174
80249
YDOT = 3694
283397 meter/sec RA = 114
36731 deg
ZDOT = -5833
809733 TA = 20
27868
MA = 20
23357
Ha = 225
587 n
mi
Hp = 220
944
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12125135
63 X = 3763996
58
Y = -18122151
94 feet Y = -5481921
88 meter
Z = -4568015
20 Z = -1374213
03
XDOT = 10922
473646 XDOT = 3315
949005
YDOT = 12120
352354 feet/sec YDOT = 3731
438644 meter/sec
ZDOT = -19139
795712 ZDOT = -5817
670181
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3509970
19 X = 1069838
91
Y = 21537448
46 feet Y = 6564614
29 meter
Z = -4485141
17 Z = -1367071
03
XDOT = -14779
393625 XDOT = -4504
759177
YDOT = -1551
750725 feet/sec YDOT = -472
973621 meter/sec
ZDOT = -19066
616668 ZDOT = -5811
504760
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19217
77957484
00016717 00000-0 10270-3 0 9121
2 25544 51
6396 115
2271 0006144 223
6673 136
3992 15
51049196 22946
Satellite: ISS
Catalog Number: 25544
Epoch time: 19217
77957484 = yrday
fracday
Element set: 912
Inclination: 51
6396 deg
RA of node: 115
2271 deg
Eccentricity:
0006144
Arg of perigee: 223
6673 deg
Mean anomaly: 136
3992 deg
Mean motion: 15
51049196 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2294
Checksum: 331
Coasting Arc #14 (Orbit 2309)
---------------------------------------
Vector Time (GMT): 2019/218/18:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 933877
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3585870
37 A = 6796683
95 meter
Y = 5402371
42 meter E =
0008496
Z = 2028646
93 I = 52
01574
XDOT = -3146
166870 Wp = 85
47589
YDOT = -4193
375248 meter/sec RA = 109
43428 deg
ZDOT = 5586
463359 TA = 296
78568
MA = 296
87257
Ha = 225
530 n
mi
Hp = 221
117
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11764666
57 X = -3655868
67
Y = 17724315
67 feet Y = 5361880
27 meter
Z = 6655665
77 Z = 2011058
38
XDOT = -10322
069783 XDOT = -3126
177165
YDOT = -13757
792808 feet/sec YDOT = -4228
446228 meter/sec
ZDOT = 18328
291859 ZDOT = 5571
229095
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3851982
02 X = -1174084
12
Y = -20947211
76 feet Y = -6384710
14 meter
Z = 6575194
77 Z = 2004119
37
XDOT = 15546
597169 XDOT = 4738
602817
YDOT = 2892
883795 feet/sec YDOT = 881
750981 meter/sec
ZDOT = 18259
275639 ZDOT = 5565
427215
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19218
81047548
00016717 00000-0 10270-3 0 9139
2 25544 51
6391 110
1114 0006298 225
3447 134
7191 15
51020533 23105
Satellite: ISS
Catalog Number: 25544
Epoch time: 19218
81047548 = yrday
fracday
Element set: 913
Inclination: 51
6391 deg
RA of node: 110
1114 deg
Eccentricity:
0006298
Arg of perigee: 225
3447 deg
Mean anomaly: 134
7191 deg
Mean motion: 15
51020533 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2310
Checksum: 278
Coasting Arc #15 (Orbit 2324)
---------------------------------------
Vector Time (GMT): 2019/219/18:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 933877
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3481415
55 A = 6795433
99 meter
Y = -5192926
87 meter E =
0007082
Z = -2651694
97 I = 52
02187
XDOT = 3016
631017 Wp = 185
58749
YDOT = 4699
578301 meter/sec RA = 104
50212 deg
ZDOT = -5248
516673 TA = 24
10636
MA = 24
07323
Ha = 225
424 n
mi
Hp = 221
239
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11421967
02 X = 3552105
96
Y = -17037161
66 feet Y = -5153599
90 meter
Z = -8699786
66 Z = -2634612
18
XDOT = 9897
083388 XDOT = 2989
348941
YDOT = 15418
563981 feet/sec YDOT = 4733
160018 meter/sec
ZDOT = -17219
542889 ZDOT = -5233
929243
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3957531
57 X = 1206255
62
Y = 20159815
55 feet Y = 6144711
78 meter
Z = -8621616
82 Z = -2627868
81
XDOT = -16517
073443 XDOT = -5034
403985
YDOT = -4085
467507 feet/sec YDOT = -1245
250496 meter/sec
ZDOT = -17153
517324 ZDOT = -5228
392080
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19219
77694402
00016717 00000-0 10270-3 0 9143
2 25544 51
6393 105
3167 0006210 229
4013 130
6598 15
51029260 23257
Satellite: ISS
Catalog Number: 25544
Epoch time: 19219
77694402 = yrday
fracday
Element set: 914
Inclination: 51
6393 deg
RA of node: 105
3167 deg
Eccentricity:
0006210
Arg of perigee: 229
4013 deg
Mean anomaly: 130
6598 deg
Mean motion: 15
51029260 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2325
Checksum: 294
Coasting Arc #16 (Orbit 2340)
---------------------------------------
Vector Time (GMT): 2019/220/18:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 933877
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3376570
10 A = 6794043
24 meter
Y = 4940732
71 meter E =
0008276
Z = 3213491
70 I = 52
02560
XDOT = -2950
937648 Wp = 111
41536
YDOT = -5165
177706 meter/sec RA = 99
56818 deg
ZDOT = 4827
837614 TA = 285
46543
MA = 285
55682
Ha = 225
219 n
mi
Hp = 221
408
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11077985
88 X = -3447177
06
Y = 16209752
98 feet Y = 4902578
58 meter
Z = 10542951
76 Z = 3196918
47
XDOT = -9681
553962 XDOT = -2916
410579
YDOT = -16946
121083 feet/sec YDOT = -5197
984346 meter/sec
ZDOT = 15839
362250 ZDOT = 4813
586795
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3938024
66 X = -1200309
92
Y = -19275979
43 feet Y = -5875318
53 meter
Z = 10467104
34 Z = 3190373
40
XDOT = 17588
282444 XDOT = 5360
908489
YDOT = 4995
921306 feet/sec YDOT = 1522
756814 meter/sec
ZDOT = 15774
914859 ZDOT = 4808
194049
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19220
80784283
00016717 00000-0 10270-3 0 9157
2 25544 51
6403 100
2013 0006397 232
9235 127
1331 15
51034254 23417
Satellite: ISS
Catalog Number: 25544
Epoch time: 19220
80784283 = yrday
fracday
Element set: 915
Inclination: 51
6403 deg
RA of node: 100
2013 deg
Eccentricity:
0006397
Arg of perigee: 232
9235 deg
Mean anomaly: 127
1331 deg
Mean motion: 15
51034254 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2341
Checksum: 268
Coasting Arc #17 (Orbit 2355)
---------------------------------------
Vector Time (GMT): 2019/221/18:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 933877
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3302413
33 A = 6792535
68 meter
Y = -4607784
36 meter E =
0002318
Z = -3740108
66 I = 52
02582
XDOT = 2930
341471 Wp = 170
12816
YDOT = 5606
293191 meter/sec RA = 94
63369 deg
ZDOT = -4322
112426 TA = 54
18633
MA = 54
16479
Ha = 225
124 n
mi
Hp = 221
568
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10834689
39 X = 3371860
64
Y = -15117402
76 feet Y = -4570465
92 meter
Z = -12270697
70 Z = -3723898
55
XDOT = 9613
981203 XDOT = 2888
426702
YDOT = 18393
350365 feet/sec YDOT = 5638
828235 meter/sec
ZDOT = -14180
158877 ZDOT = -4307
979529
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3627388
33 X = 1105627
96
Y = 18291622
98 feet Y = 5575286
68 meter
Z = -12196514
46 Z = -3717497
61
XDOT = -18743
982276 XDOT = -5713
165798
YDOT = -5689
633121 feet/sec YDOT = -1734
200175 meter/sec
ZDOT = -14116
294010 ZDOT = -4302
646414
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19221
77430993
00016717 00000-0 10270-3 0 9161
2 25544 51
6412 95
4063 0006235 237
0335 123
0217 15
51022102 23568
Satellite: ISS
Catalog Number: 25544
Epoch time: 19221
77430993 = yrday
fracday
Element set: 916
Inclination: 51
6412 deg
RA of node: 95
4063 deg
Eccentricity:
0006235
Arg of perigee: 237
0335 deg
Mean anomaly: 123
0217 deg
Mean motion: 15
51022102 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2356
Checksum: 273
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