[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 22nd 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14481 7651 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
203/20:55:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
4
000/00:00:00
000 0
0 0
0 219
0
204/11:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
4
000/00:00:00
000 0
0 0
0 218
9
205/22:24:29
000 0
0 0
0 0
0
N/A 0
0 0
0 227
2
000/00:00:00
000 0
0 0
0 219
2
207/04:36:00
000 0
0 0
0 0
0
N/A 0
0 0
0 227
1
000/00:00:00
000 0
0 0
0 219
4
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 2072)
---------------------------------------
Vector Time (GMT): 2019/203/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929147
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5123823
74 A = 6792574
74 meter
Y = -2492837
07 meter E =
0013910
Z = 3681528
13 I = 51
60183
XDOT = 5004
341998 Wp = 112
61470
YDOT = 3872
963914 meter/sec RA = 184
85742 deg
ZDOT = -4334
559540 TA = 23
56064
MA = 23
49699
Ha = 227
268 n
mi
Hp = 218
742
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16810445
33 X = 5133436
01
Y = -8178599
30 feet Y = -2435485
35 meter
Z = 12078504
38 Z = 3706440
56
XDOT = 16418
444874 XDOT = 4981
716028
YDOT = 12706
574522 feet/sec YDOT = 3928
799733 meter/sec
ZDOT = -14220
995867 ZDOT = -4310
305418
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15274449
68 X = -4655652
26
Y = -10649918
40 feet Y = -3246095
13 meter
Z = 12191851
86 Z = 3716076
45
XDOT = 2307
377129 XDOT = 703
288549
YDOT = -19492
628050 feet/sec YDOT = -5941
353030 meter/sec
ZDOT = -14111
060123 ZDOT = -4301
051126
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19203
54017763
00016717 00000-0 10270-3 0 9005
2 25544 51
6388 185
8785 0006487 168
9886 191
1408 15
51007000 20731
Satellite: ISS
Catalog Number: 25544
Epoch time: 19203
54017763 = yrday
fracday
Element set: 900
Inclination: 51
6388 deg
RA of node: 185
8785 deg
Eccentricity:
0006487
Arg of perigee: 168
9886 deg
Mean anomaly: 191
1408 deg
Mean motion: 15
51007000 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2073
Checksum: 320
Coasting Arc #2 (Orbit 2078)
---------------------------------------
Vector Time (GMT): 2019/203/20:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 929147
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4012480
37 A = 6791220
63 meter
Y = -3534074
52 meter E =
0014070
Z = 4183574
95 I = 51
61067
XDOT = 6179
742290 Wp = 129
13263
YDOT = -2609
410903 meter/sec RA = 183
06342 deg
ZDOT = 3705
646529 TA = 282
69775
MA = 282
85500
Ha = 227
384 n
mi
Hp = 218
955
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13164305
69 X = -3992984
32
Y = -11594732
69 feet Y = -3578836
13 meter
Z = 13725639
60 Z = 4164131
25
XDOT = 20274
745046 XDOT = 6190
462467
YDOT = -8561
059393 feet/sec YDOT = -2540
244959 meter/sec
ZDOT = 12157
632968 ZDOT = 3735
690862
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14933925
27 X = 4551860
42
Y = -9334107
23 feet Y = -2845035
88 meter
Z = 13637531
71 Z = 4156719
67
XDOT = 1669
997850 XDOT = 509
015345
YDOT = 20716
722112 feet/sec YDOT = 6314
456900 meter/sec
ZDOT = 12294
308692 ZDOT = 3747
305289
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19203
92677024
00016717 00000-0 10270-3 0 9010
2 25544 51
6404 183
9602 0006315 171
4996 188
6263 15
50973135 20794
Satellite: ISS
Catalog Number: 25544
Epoch time: 19203
92677024 = yrday
fracday
Element set: 901
Inclination: 51
6404 deg
RA of node: 183
9602 deg
Eccentricity:
0006315
Arg of perigee: 171
4996 deg
Mean anomaly: 188
6263 deg
Mean motion: 15
50973135 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2079
Checksum: 318
Coasting Arc #3 (Orbit 2087)
---------------------------------------
Vector Time (GMT): 2019/204/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929147
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 73181
09 A = 6786501
53 meter
Y = -4212507
64 meter E =
0007258
Z = 5317479
33 I = 51
61273
XDOT = 7665
853658 Wp = 153
48806
YDOT = 64
853637 meter/sec RA = 180
12682 deg
ZDOT = -60
443969 TA = 297
05125
MA = 297
12530
Ha = 227
356 n
mi
Hp = 218
892
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 240095
44 X = 94452
07
Y = -13820563
11 feet Y = -4211570
65 meter
Z = 17445798
34 Z = 5317886
24
XDOT = 25150
438511 XDOT = 7664
852307
YDOT = 212
774399 feet/sec YDOT = 150
573002 meter/sec
ZDOT = -198
306986 ZDOT = -23
209003
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13379852
08 X = -4078178
91
Y = 3459913
75 feet Y = 1054581
71 meter
Z = 17447923
82 Z = 5318127
18
XDOT = -6054
939430 XDOT = -1845
545538
YDOT = -23372
775978 feet/sec YDOT = -7124
022118 meter/sec
ZDOT = -29
125816 ZDOT = -8
877549
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19204
50665823
00016717 00000-0 10270-3 0 9020
2 25544 51
6383 181
0835 0006539 172
4086 187
7165 15
50989319 20888
Satellite: ISS
Catalog Number: 25544
Epoch time: 19204
50665823 = yrday
fracday
Element set: 902
Inclination: 51
6383 deg
RA of node: 181
0835 deg
Eccentricity:
0006539
Arg of perigee: 172
4086 deg
Mean anomaly: 187
7165 deg
Mean motion: 15
50989319 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2088
Checksum: 332
Coasting Arc #4 (Orbit 2102)
---------------------------------------
Vector Time (GMT): 2019/205/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929147
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -584740
79 A = 6786764
20 meter
Y = 4241803
50 meter E =
0016955
Z = -5279343
51 I = 51
64679
XDOT = -7606
750402 Wp = 118
73068
YDOT = -12
348496 meter/sec RA = 175
16002 deg
ZDOT = 826
667975 TA = 159
22267
MA = 159
15366
Ha = 227
257 n
mi
Hp = 219
035
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1918440
90 X = -606486
50
Y = 13916678
14 feet Y = 4235143
25 meter
Z = -17320680
80 Z = -5282236
49
XDOT = -24956
530189 XDOT = -7610
062429
YDOT = -40
513437 feet/sec YDOT = -97
431092 meter/sec
ZDOT = 2712
165271 ZDOT = 789
709512
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13873399
37 X = 4228612
13
Y = -2101881
15 feet Y = -640653
37 meter
Z = -17334105
53 Z = -5283435
37
XDOT = 6688
848133 XDOT = 2038
760911
YDOT = 23007
041745 feet/sec YDOT = 7012
546324 meter/sec
ZDOT = 2544
217075 ZDOT = 775
477364
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19205
47313881
00016717 00000-0 10270-3 0 9032
2 25544 51
6383 176
2887 0006520 175
7692 184
3515 15
50973280 21030
Satellite: ISS
Catalog Number: 25544
Epoch time: 19205
47313881 = yrday
fracday
Element set: 903
Inclination: 51
6383 deg
RA of node: 176
2887 deg
Eccentricity:
0006520
Arg of perigee: 175
7692 deg
Mean anomaly: 184
3515 deg
Mean motion: 15
50973280 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2103
Checksum: 316
Coasting Arc #5 (Orbit 2110)
---------------------------------------
Vector Time (GMT): 2019/205/22:24:29
000
Vector Time (MET): N/A
Weight (LBS) : 929147
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4421323
51 A = 6790748
92 meter
Y = -2858876
38 meter E =
0013538
Z = 4286562
04 I = 51
67549
XDOT = 5773
481166 Wp = 135
19938
YDOT = -3563
851377 meter/sec RA = 172
83087 deg
ZDOT = 3561
864522 TA = 278
38995
MA = 278
54339
Ha = 227
236 n
mi
Hp = 219
155
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14505654
55 X = -4409847
71
Y = -9379515
67 feet Y = -2908254
84 meter
Z = 14063523
76 Z = 4265112
75
XDOT = 18941
867342 XDOT = 5795
602653
YDOT = -11692
425777 feet/sec YDOT = -3499
164803 meter/sec
ZDOT = 11685
907223 ZDOT = 3589
963209
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7370117
78 X = 2246411
90
Y = -15709795
66 feet Y = -4788345
72 meter
Z = 13966234
74 Z = 4256908
35
XDOT = 12932
819266 XDOT = 3941
923312
YDOT = 16617
725784 feet/sec YDOT = 5065
082819 meter/sec
ZDOT = 11813
836630 ZDOT = 3600
857405
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19205
98859355
00016717 00000-0 10270-3 0 9040
2 25544 51
6377 173
7280 0006714 179
8502 180
2652 15
51012961 21119
Satellite: ISS
Catalog Number: 25544
Epoch time: 19205
98859355 = yrday
fracday
Element set: 904
Inclination: 51
6377 deg
RA of node: 173
7280 deg
Eccentricity:
0006714
Arg of perigee: 179
8502 deg
Mean anomaly: 180
2652 deg
Mean motion: 15
51012961 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2111
Checksum: 313
Coasting Arc #6 (Orbit 2125)
---------------------------------------
Vector Time (GMT): 2019/206/22:24:29
000
Vector Time (MET): N/A
Weight (LBS) : 929147
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3983348
19 A = 6789301
12 meter
Y = 2914524
44 meter E =
0010181
Z = -4668690
34 I = 51
70511
XDOT = -6069
591805 Wp = 108
45194
YDOT = 3652
229696 meter/sec RA = 167
87074 deg
ZDOT = -2906
973650 TA = 132
66136
MA = 132
57552
Ha = 227
163 n
mi
Hp = 219
258
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13068727
67 X = 3973138
86
Y = 9562088
05 feet Y = 2959012
33 meter
Z = -15317225
51 Z = -4649365
39
XDOT = -19913
358941 XDOT = -6095
860604
YDOT = 11982
380893 feet/sec YDOT = 3584
208617 meter/sec
ZDOT = -9537
315126 ZDOT = -2936
520786
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7492065
75 X = -2283581
64
Y = 14448919
49 feet Y = 4404030
66 meter
Z = -15229584
52 Z = -4641977
36
XDOT = -13751
515178 XDOT = -4191
461826
YDOT = -17295
827725 feet/sec YDOT = -5271
768290 meter/sec
ZDOT = -9671
852102 ZDOT = -2947
980521
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 19206
95507224
00016717 00000-0 10270-3 0 9054
2 25544 51
6391 168
9327 0006650 180
6268 179
4875 15
51015556 21267
Satellite: ISS
Catalog Number: 25544
Epoch time: 19206
95507224 = yrday
fracday
Element set: 905
Inclination: 51
6391 deg
RA of node: 168
9327 deg
Eccentricity:
0006650
Arg of perigee: 180
6268 deg
Mean anomaly: 179
4875 deg
Mean motion: 15
51015556 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2126
Checksum: 325
Coasting Arc #7 (Orbit 2129)
---------------------------------------
Vector Time (GMT): 2019/207/04:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 929147
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3905746
88 A = 6789123
09 meter
Y = 2911649
59 meter E =
0010180
Z = -4735487
51 I = 51
71470
XDOT = -6104
982106 Wp = 108
58290
YDOT = 3701
021204 meter/sec RA = 166
59341 deg
ZDOT = -2767
726672 TA = 134
03936
MA = 133
95546
Ha = 227
135 n
mi
Hp = 219
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12814130
20 X = 3895899
94
Y = 9552656
12 feet Y = 2955271
74 meter
Z = -15536376
34 Z = -4716538
63
XDOT = -20029
468853 XDOT = -6132
470254
YDOT = 12142
458019 feet/sec YDOT = 3632
597549 meter/sec
ZDOT = -9080
468085 ZDOT = -2797
448666
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14587075
16 X = 4446140
51
Y = 6733145
19 feet Y = 2052262
65 meter
Z = -15450441
93 Z = -4709294
70
XDOT = -16599
449477 XDOT = -5059
512200
YDOT = 14875
541076 feet/sec YDOT = 4534
064920 meter/sec
ZDOT = -9215
808449 ZDOT = -2808
978415
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
21279851
00016717 00000-0 10270-3 0 9067
2 25544 51
6412 167
6560 0006738 184
2593 175
8502 15
50985722 21306
Satellite: ISS
Catalog Number: 25544
Epoch time: 19207
21279851 = yrday
fracday
Element set: 906
Inclination: 51
6412 deg
RA of node: 167
6560 deg
Eccentricity:
0006738
Arg of perigee: 184
2593 deg
Mean anomaly: 175
8502 deg
Mean motion: 15
50985722 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2130
Checksum: 317
Coasting Arc #8 (Orbit 2145)
---------------------------------------
Vector Time (GMT): 2019/208/04:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 949153
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3476439
49 A = 6787924
94 meter
Y = -2999277
27 meter E =
0010863
Z = 4998970
65 I = 51
74317
XDOT = 6307
238161 Wp = 156
94801
YDOT = -3823
028728 meter/sec RA = 161
63505 deg
ZDOT = 2081
222630 TA = 272
75599
MA = 272
88032
Ha = 226
999 n
mi
Hp = 219
473
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11405641
38 X = -3466924
42
Y = -9840148
51 feet Y = -3038100
57 meter
Z = 16400822
36 Z = 4982106
31
XDOT = 20693
038585 XDOT = 6339
410238
YDOT = -12542
745172 feet/sec YDOT = -3752
317095 meter/sec
ZDOT = 6828
158234 ZDOT = 2111
938389
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13395473
75 X = -4082940
40
Y = -7069702
75 feet Y = -2154845
40 meter
Z = 16324360
26 Z = 4975665
01
XDOT = 16872
391202 XDOT = 5142
704839
YDOT = -15793
772064 feet/sec YDOT = -4813
941725 meter/sec
ZDOT = 6968
046897 ZDOT = 2123
860694
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
24370544
00016717 00000-0 10270-3 0 9073
2 25544 51
6411 162
5413 0006654 187
9083 172
1964 15
51017746 21469
Satellite: ISS
Catalog Number: 25544
Epoch time: 19208
24370544 = yrday
fracday
Element set: 907
Inclination: 51
6411 deg
RA of node: 162
5413 deg
Eccentricity:
0006654
Arg of perigee: 187
9083 deg
Mean anomaly: 172
1964 deg
Mean motion: 15
51017746 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2146
Checksum: 306
Coasting Arc #9 (Orbit 2160)
---------------------------------------
Vector Time (GMT): 2019/209/04:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 949153
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3006688
58 A = 6787161
49 meter
Y = 3168484
16 meter E =
0012985
Z = -5204647
46 I = 51
77074
XDOT = -6436
382741 Wp = 108
46449
YDOT = 3922
131517 meter/sec RA = 156
67742 deg
ZDOT = -1337
283372 TA = 148
72485
MA = 148
64753
Ha = 226
898 n
mi
Hp = 219
751
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9864463
84 X = 2996315
30
Y = 10395289
23 feet Y = 3202049
69 meter
Z = -17075615
01 Z = -5190067
01
XDOT = -21116
741276 XDOT = -6473
267052
YDOT = 12867
885555 feet/sec YDOT = 3849
949295 meter/sec
ZDOT = -4387
412639 ZDOT = -1368
637772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12153257
97 X = 3704313
03
Y = 7740813
40 feet Y = 2359399
92 meter
Z = -17009539
72 Z = -5184507
71
XDOT = -16883
152091 XDOT = -5145
984757
YDOT = 16601
082973 feet/sec YDOT = 5060
010090 meter/sec
ZDOT = -4530
237080 ZDOT = -1380
816262
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
21018242
00016717 00000-0 10270-3 0 9086
2 25544 51
6403 157
7464 0006668 191
1615 168
9389 15
50981359 21615
Satellite: ISS
Catalog Number: 25544
Epoch time: 19209
21018242 = yrday
fracday
Element set: 908
Inclination: 51
6403 deg
RA of node: 157
7464 deg
Eccentricity:
0006668
Arg of perigee: 191
1615 deg
Mean anomaly: 168
9389 deg
Mean motion: 15
50981359 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2161
Checksum: 325
Coasting Arc #10 (Orbit 2176)
---------------------------------------
Vector Time (GMT): 2019/210/04:36:00
000
Vector Time (MET): N/A
Weight (LBS) : 949153
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2570179
80 A = 6786550
02 meter
Y = -3359448
31 meter E =
0007669
Z = 5306976
49 I = 51
80013
XDOT = 6496
047450 Wp = 173
10945
YDOT = -4023
329501 meter/sec RA = 151
72136 deg
ZDOT = 591
667265 TA = 271
20888
MA = 271
29674
Ha = 226
752 n
mi
Hp = 219
777
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8432348
43 X = -2558200
50
Y = -11021812
05 feet Y = -3388123
58 meter
Z = 17411340
20 Z = 5294520
32
XDOT = 21312
491634 XDOT = 6537
680722
YDOT = -13199
899937 feet/sec YDOT = -3950
453429 meter/sec
ZDOT = 1941
165567 ZDOT = 623
322854
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11059870
90 X = -3371048
65
Y = -8498544
72 feet Y = -2590356
43 meter
Z = 17354930
19 Z = 5289782
72
XDOT = 16645
750319 XDOT = 5073
624697
YDOT = -17353
411244 feet/sec YDOT = -5289
319747 meter/sec
ZDOT = 2085
393759 ZDOT = 635
628018
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
24108698
00016717 00000-0 10270-3 0 9097
2 25544 51
6411 152
6316 0006570 195
1857 164
9098 15
51019942 21779
Satellite: ISS
Catalog Number: 25544
Epoch time: 19210
24108698 = yrday
fracday
Element set: 909
Inclination: 51
6411 deg
RA of node: 152
6316 deg
Eccentricity:
0006570
Arg of perigee: 195
1857 deg
Mean anomaly: 164
9098 deg
Mean motion: 15
51019942 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2177
Checksum: 320
Coasting Arc #11 (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 = -3606766
29 A = 6787330
49 meter
Y = -2595422
71 meter E =
0009297
Z = 5130758
65 I = 51
80927
XDOT = 5776
724776 Wp = 165
37283
YDOT = -4759
413544 meter/sec RA = 150
46405 deg
ZDOT = 1643
862551 TA = 268
73505
MA = 268
84156
Ha = 226
622 n
mi
Hp = 219
855
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11833222
75 X = -3602397
52
Y = -8515166
36 feet Y = -2635732
35 meter
Z = 16833197
66 Z = 5113248
82
XDOT = 18952
509109 XDOT = 5821
531703
YDOT = -15614
873832 feet/sec YDOT = -4694
563838 meter/sec
ZDOT = 5393
249840 ZDOT = 1672
031554
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4640688
20 X = -1414481
76
Y = 13916378
84 feet Y = 4241712
27 meter
Z = 16753751
09 Z = 5106543
33
XDOT = -19456
246326 XDOT = -5930
263880
YDOT = -13172
939087 feet/sec YDOT = -4015
111834 meter/sec
ZDOT = 5521
680756 ZDOT = 1683
008295
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
49881366
00016717 00000-0 10270-3 0 9106
2 25544 51
6401 151
3537 0006303 196
8202 163
2741 15
51030120 21818
Satellite: ISS
Catalog Number: 25544
Epoch time: 19210
49881366 = yrday
fracday
Element set: 910
Inclination: 51
6401 deg
RA of node: 151
3537 deg
Eccentricity:
0006303
Arg of perigee: 196
8202 deg
Mean anomaly: 163
2741 deg
Mean motion: 15
51030120 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2181
Checksum: 268
Coasting Arc #12 (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 = 3171554
70 A = 6786758
20 meter
Y = 2860034
20 meter E =
0012889
Z = -5284621
83 I = 51
83572
XDOT = -5847
214454 Wp = 108
71599
YDOT = 4860
600008 meter/sec RA = 145
50936 deg
ZDOT = -884
431440 TA = 152
86754
MA = 152
80013
Ha = 226
480 n
mi
Hp = 220
118
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10405363
19 X = 3165006
55
Y = 9383314
29 feet Y = 2895464
82 meter
Z = -17337998
14 Z = -5269231
42
XDOT = -19183
774457 XDOT = -5896
836508
YDOT = 15946
850419 feet/sec YDOT = 4794
935010 meter/sec
ZDOT = -2901
677952 ZDOT = -912
954398
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5666819
56 X = 1727246
60
Y = -12908168
96 feet Y = -3934409
90 meter
Z = -17268198
51 Z = -5263346
91
XDOT = 20151
727350 XDOT = 6142
246496
YDOT = 12877
087473 feet/sec YDOT = 3924
936262 meter/sec
ZDOT = -3031
750765 ZDOT = -924
077633
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
46528643
00016717 00000-0 10270-3 0 9111
2 25544 51
6402 146
5576 0006185 199
5356 160
5558 15
51000768 21963
Satellite: ISS
Catalog Number: 25544
Epoch time: 19211
46528643 = yrday
fracday
Element set: 911
Inclination: 51
6402 deg
RA of node: 146
5576 deg
Eccentricity:
0006185
Arg of perigee: 199
5356 deg
Mean anomaly: 160
5558 deg
Mean motion: 15
51000768 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2196
Checksum: 318
Coasting Arc #13 (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 = -2776723
67 A = 6786424
92 meter
Y = -3141452
94 meter E =
0005976
Z = 5336549
77 I = 51
86215
XDOT = 5853
079963 Wp = 180
98756
YDOT = -4945
426688 meter/sec RA = 140
55879 deg
ZDOT = 128
454616 TA = 267
75712
MA = 267
82555
Ha = 226
371 n
mi
Hp = 220
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9109985
80 X = -2767310
06
Y = -10306604
14 feet Y = -3172452
19 meter
Z = 17508365
40 Z = 5323084
31
XDOT = 19203
018250 XDOT = 5907
322189
YDOT = -16225
153177 feet/sec YDOT = -4879
670165 meter/sec
ZDOT = 421
439030 ZDOT = 157
017206
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6738380
09 X = -2053858
25
Y = 12080795
10 feet Y = 3682226
35 meter
Z = 17447332
54 Z = 5317946
96
XDOT = -20712
537030 XDOT = -6313
181287
YDOT = -12377
438090 feet/sec YDOT = -3772
643130 meter/sec
ZDOT = 551
721133 ZDOT = 168
164601
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
49618940
00016717 00000-0 10270-3 0 9126
2 25544 51
6406 141
4442 0006160 204
0657 156
0207 15
51019631 22121
Satellite: ISS
Catalog Number: 25544
Epoch time: 19212
49618940 = yrday
fracday
Element set: 912
Inclination: 51
6406 deg
RA of node: 141
4442 deg
Eccentricity:
0006160
Arg of perigee: 204
0657 deg
Mean anomaly: 156
0207 deg
Mean motion: 15
51019631 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2212
Checksum: 271
Coasting Arc #14 (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 = 1825060
65 A = 6792453
90 meter
Y = -5381294
10 meter E =
0010013
Z = 3709629
83 I = 51
89019
XDOT = 6262
568859 Wp = 116
20281
YDOT = -869
693277 meter/sec RA = 139
53593 deg
ZDOT = -4337
904848 TA = 19
78935
MA = 19
75054
Ha = 226
167 n
mi
Hp = 220
186
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5987731
80 X = 1867081
30
Y = -17655164
37 feet Y = -5360650
44 meter
Z = 12170701
53 Z = 3718596
55
XDOT = 20546
485757 XDOT = 6292
899198
YDOT = -2853
324398 feet/sec YDOT = -799
490772 meter/sec
ZDOT = -14231
971287 ZDOT = -4307
410796
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5338731
70 X = -1627245
42
Y = 17834007
51 feet Y = 5435805
49 meter
Z = 12211873
60 Z = 3722179
07
XDOT = -19239
615610 XDOT = -5864
234838
YDOT = 3901
464703 feet/sec YDOT = 1189
166441 meter/sec
ZDOT = -14093
186654 ZDOT = -4295
603292
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
68948257
00016717 00000-0 10270-3 0 9135
2 25544 51
6430 140
4865 0006090 205
4656 154
6196 15
51042772 22158
Satellite: ISS
Catalog Number: 25544
Epoch time: 19212
68948257 = yrday
fracday
Element set: 913
Inclination: 51
6430 deg
RA of node: 140
4865 deg
Eccentricity:
0006090
Arg of perigee: 205
4656 deg
Mean anomaly: 154
6196 deg
Mean motion: 15
51042772 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2215
Checksum: 307
Coasting Arc #15 (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 = 426683
14 A = 6790428
18 meter
Y = -5199204
56 meter E =
0006704
Z = 4340059
73 I = 51
90281
XDOT = 6371
962471 Wp = 111
77709
YDOT = -2412
682882 meter/sec RA = 135
40473 deg
ZDOT = -3514
810793 TA = 13
86315
MA = 13
84476
Ha = 226
187 n
mi
Hp = 220
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1399879
05 X = 463709
39
Y = -17057757
75 feet Y = -5194226
44 meter
Z = 14239041
12 Z = 4342221
82
XDOT = 20905
388684 XDOT = 6415
540753
YDOT = -7915
626252 feet/sec YDOT = -2341
183154 meter/sec
ZDOT = -11531
531473 ZDOT = -3483
753380
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14938928
05 X = -4553385
27
Y = 8334532
75 feet Y = 2540365
58 meter
Z = 14249247
19 Z = 4343170
54
XDOT = -17581
319270 XDOT = -5358
786113
YDOT = -12029
038318 feet/sec YDOT = -3666
450879 meter/sec
ZDOT = -11390
057853 ZDOT = -3471
689633
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
52709176
00016717 00000-0 10270-3 0 9145
2 25544 51
6419 136
3301 0006196 208
1115 151
9703 15
51010640 22288
Satellite: ISS
Catalog Number: 25544
Epoch time: 19213
52709176 = yrday
fracday
Element set: 914
Inclination: 51
6419 deg
RA of node: 136
3301 deg
Eccentricity:
0006196
Arg of perigee: 208
1115 deg
Mean anomaly: 151
9703 deg
Mean motion: 15
51010640 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2228
Checksum: 277
Coasting Arc #16 (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 = -673693
97 A = 6791906
37 meter
Y = 5514945
77 meter E =
0007651
Z = -3914863
71 I = 51
93129
XDOT = -6083
162424 Wp = 156
65787
YDOT = 2175
307379 meter/sec RA = 130
46048 deg
ZDOT = 4107
139584 TA = 156
31826
MA = 156
28303
Ha = 225
995 n
mi
Hp = 220
501
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2210282
07 X = -716297
90
Y = 18093654
10 feet Y = 5507174
06 meter
Z = -12844041
05 Z = -3918239
34
XDOT = -19957
881969 XDOT = -6126
984890
YDOT = 7136
835232 feet/sec YDOT = 2107
035922 meter/sec
ZDOT = 13474
867402 ZDOT = 4077
484349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16111485
77 X = 4910780
86
Y = -8501810
01 feet Y = -2591351
69 meter
Z = -12859794
29 Z = -3919665
30
XDOT = 16621
025647 XDOT = 5066
088617
YDOT = 11299
998976 feet/sec YDOT = 3444
239688 meter/sec
ZDOT = 13339
773822 ZDOT = 4065
963061
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
49355972
00016717 00000-0 10270-3 0 9154
2 25544 51
6424 131
5345 0006110 211
6371 148
4413 15
51018442 22432
Satellite: ISS
Catalog Number: 25544
Epoch time: 19214
49355972 = yrday
fracday
Element set: 915
Inclination: 51
6424 deg
RA of node: 131
5345 deg
Eccentricity:
0006110
Arg of perigee: 211
6371 deg
Mean anomaly: 148
4413 deg
Mean motion: 15
51018442 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2243
Checksum: 280
Coasting Arc #17 (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 = 860257
91 A = 6793456
84 meter
Y = -5802629
46 meter E =
0010171
Z = 3413633
84 I = 51
95697
XDOT = 5804
506789 Wp = 119
30197
YDOT = -1875
367361 meter/sec RA = 125
52083 deg
ZDOT = -4645
044263 TA = 21
00695
MA = 20
96521
Ha = 225
895 n
mi
Hp = 220
637
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2822368
47 X = 908499
51
Y = -19037498
24 feet Y = -5792739
82 meter
Z = 11199586
07 Z = 3417929
54
XDOT = 19043
657444 XDOT = 5847
608778
YDOT = -6152
780056 feet/sec YDOT = -1810
216151 meter/sec
ZDOT = -15239
646532 ZDOT = -4616
744207
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17093204
91 X = -5210008
86
Y = 8818551
07 feet Y = 2687894
37 meter
Z = 11219551
42 Z = 3419719
27
XDOT = -15484
933335 XDOT = -4719
807680
YDOT = -10766
794045 feet/sec YDOT = -3281
718825 meter/sec
ZDOT = -15110
728081 ZDOT = -4605
749919
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
52445773
00016717 00000-0 10270-3 0 9169
2 25544 51
6422 126
4206 0006061 215
2934 144
7816 15
51012817 22592
Satellite: ISS
Catalog Number: 25544
Epoch time: 19215
52445773 = yrday
fracday
Element set: 916
Inclination: 51
6422 deg
RA of node: 126
4206 deg
Eccentricity:
0006061
Arg of perigee: 215
2934 deg
Mean anomaly: 144
7816 deg
Mean motion: 15
51012817 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2259
Checksum: 295
Coasting Arc #18 (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 = -989487
53 A = 6794863
32 meter
Y = 6081681
42 meter E =
0002669
Z = -2868131
28 I = 51
98043
XDOT = -5515
676871 Wp = 174
71432
YDOT = 1505
764952 meter/sec RA = 120
58276 deg
ZDOT = 5093
541341 TA = 152
89619
MA = 152
88225
Ha = 225
704 n
mi
Hp = 220
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3246350
17 X = -1043489
59
Y = 19953023
04 feet Y = 6070314
37 meter
Z = -9409879
52 Z = -2873068
82
XDOT = -18096
052728 XDOT = -5556
845931
YDOT = 4940
173727 feet/sec YDOT = 1443
854523 meter/sec
ZDOT = 16711
093639 ZDOT = 5066
648819
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17934429
98 X = 5466414
26
Y = -9305180
30 feet Y = -2836218
95 meter
Z = -9432793
42 Z = -2875115
43
XDOT = 14121
272616 XDOT = 4304
163893
YDOT = 10393
352684 feet/sec YDOT = 3167
893898 meter/sec
ZDOT = 16588
596941 ZDOT = 5056
204348
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
49092339
00016717 00000-0 10270-3 0 9173
2 25544 51
6423 121
6251 0006121 219
2887 140
7820 15
51029037 22748
Satellite: ISS
Catalog Number: 25544
Epoch time: 19216
49092339 = yrday
fracday
Element set: 917
Inclination: 51
6423 deg
RA of node: 121
6251 deg
Eccentricity:
0006121
Arg of perigee: 219
2887 deg
Mean anomaly: 140
7820 deg
Mean motion: 15
51029037 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2274
Checksum: 295
Coasting Arc #19 (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 = -3790893
45 A = 6798169
62 meter
Y = 5592698
47 meter E =
0007161
Z = 728012
44 I = 51
99216
XDOT = -3563
015256 Wp = 64
93721
YDOT = -3199
029454 meter/sec RA = 119
30006 deg
ZDOT = 5979
155841 TA = 302
87726
MA = 302
94616
Ha = 225
786 n
mi
Hp = 220
861
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12437314
46 X = -3856687
08
Y = 18348748
25 feet Y = 5549938
15 meter
Z = 2388492
25 Z = 709438
30
XDOT = -11689
682598 XDOT = -3556
020850
YDOT = -10495
503458 feet/sec YDOT = -3238
834546 meter/sec
ZDOT = 19616
653022 ZDOT = 5961
865332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3070205
00 X = -935798
48
Y = -21962143
38 feet Y = -6694061
30 meter
Z = 2303551
09 Z = 702122
37
XDOT = 14205
301981 XDOT = 4329
776044
YDOT = 78
813605 feet/sec YDOT = 24
022387 meter/sec
ZDOT = 19538
197529 ZDOT = 5955
242607
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
81307733
00016717 00000-0 10270-3 0 9187
2 25544 51
6387 120
0227 0006378 219
0991 140
9700 15
51020273 22798
Satellite: ISS
Catalog Number: 25544
Epoch time: 19216
81307733 = yrday
fracday
Element set: 918
Inclination: 51
6387 deg
RA of node: 120
0227 deg
Eccentricity:
0006378
Arg of perigee: 219
0991 deg
Mean anomaly: 140
9700 deg
Mean motion: 15
51020273 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2279
Checksum: 299
Coasting Arc #20 (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 = 3705752
48 A = 6797452
82 meter
Y = -5512427
87 meter E =
0011316
Z = -1409927
95 I = 52
00655
XDOT = 3314
923979 Wp = 174
92693
YDOT = 3715
511026 meter/sec RA = 114
36731 deg
ZDOT = -5828
425315 TA = 20
34947
MA = 20
30442
Ha = 225
567 n
mi
Hp = 220
926
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12157980
57 X = 3773967
17
Y = -18085393
28 feet Y = -5470606
12 meter
Z = -4625747
85 Z = -1391761
41
XDOT = 10875
734840 XDOT = 3301
440548
YDOT = 12189
996805 feet/sec YDOT = 3752
505496 meter/sec
ZDOT = -19122
130297 ZDOT = -5812
355601
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3460590
57 X = 1054788
01
Y = 21533325
21 feet Y = 6563357
52 meter
Z = -4542653
78 Z = -1384600
87
XDOT = -14793
079670 XDOT = -4508
930683
YDOT = -1631
016555 feet/sec YDOT = -497
133846 meter/sec
ZDOT = -19049
270695 ZDOT = -5806
217708
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
77953971
00016717 00000-0 10270-3 0 9195
2 25544 51
6398 115
2271 0006135 223
6891 136
3775 15
51060440 22944
Satellite: ISS
Catalog Number: 25544
Epoch time: 19217
77953971 = yrday
fracday
Element set: 919
Inclination: 51
6398 deg
RA of node: 115
2271 deg
Eccentricity:
0006135
Arg of perigee: 223
6891 deg
Mean anomaly: 136
3775 deg
Mean motion: 15
51060440 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2294
Checksum: 323
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