[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 24th 2019
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14248 1882 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
082/14:24:51
161 -0
8 2
2 2
2
N/A 1
1 -0
2 224
4
000/00:05:42
323 1
8 -0
0 216
6
082/22:28:00
000 0
0 0
0 0
0
N/A 0
0 0
0 224
4
000/00:00:00
000 0
0 0
0 216
7
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
1
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
8
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
Coasting Arc #1 (Orbit 177)
---------------------------------------
Vector Time (GMT): 2019/081/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915052
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4488523
13 A = 6785224
43 meter
Y = 2638766
21 meter E =
0012094
Z = -4363379
76 I = 51
99542
XDOT = -593
572157 Wp = 115
41962
YDOT = 6785
054370 meter/sec RA = 71
35902 deg
ZDOT = 3495
185435 TA = 189
97832
MA = 190
00235
Ha = 224
234 n
mi
Hp = 215
767
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14726125
74 X = 4479876
94
Y = 8657369
45 feet Y = 2688911
08 meter
Z = -14315550
40 Z = -4341597
60
XDOT = -1947
415214 XDOT = -686
378088
YDOT = 22260
677067 feet/sec YDOT = 6777
898198 meter/sec
ZDOT = 11467
143814 ZDOT = 3492
075754
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14639926
90 X = 4462249
72
Y = 8960292
79 feet Y = 2731097
24 meter
Z = -14217225
53 Z = -4333410
34
XDOT = -1829
453671 XDOT = -557
617479
YDOT = 21147
386628 feet/sec YDOT = 6445
723444 meter/sec
ZDOT = 11452
386287 ZDOT = 3490
687340
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 19081
50975240
00016717 00000-0 10270-3 0 9008
2 25544 51
6373 72
1276 0003623 127
8845 232
2635 15
52813371 1786
Satellite: ISS
Catalog Number: 25544
Epoch time: 19081
50975240 = yrday
fracday
Element set: 900
Inclination: 51
6373 deg
RA of node: 72
1276 deg
Eccentricity:
0003623
Arg of perigee: 127
8845 deg
Mean anomaly: 232
2635 deg
Mean motion: 15
52813371 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 178
Checksum: 298
Coasting Arc #2 (Orbit 193)
---------------------------------------
Vector Time (GMT): 2019/082/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915052
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4549709
17 A = 6787998
14 meter
Y = -3633232
47 meter E =
0015112
Z = 3474515
44 I = 51
99377
XDOT = 1286
298378 Wp = 97
99076
YDOT = -6012
573944 meter/sec RA = 66
40640 deg
ZDOT = -4587
928513 TA = 41
44092
MA = 41
32641
Ha = 224
185 n
mi
Hp = 215
682
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14926867
36 X = -4525620
49
Y = -11920054
03 feet Y = -3683975
40 meter
Z = 11399328
87 Z = 3452473
55
XDOT = 4220
139036 XDOT = 1375
722739
YDOT = -19726
292466 feet/sec YDOT = -5997
690194 meter/sec
ZDOT = -15052
258902 ZDOT = -4581
462242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14961931
96 X = -4560396
86
Y = -11970617
58 feet Y = -3648644
24 meter
Z = 11299940
82 Z = 3444221
96
XDOT = 3515
423322 XDOT = 1071
501029
YDOT = -18621
328950 feet/sec YDOT = -5675
781064 meter/sec
ZDOT = -15022
372144 ZDOT = -4578
819029
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 19082
53943782
00016717 00000-0 10270-3 0 9019
2 25544 51
6376 67
0038 0003473 131
1447 229
0005 15
52858072 1947
Satellite: ISS
Catalog Number: 25544
Epoch time: 19082
53943782 = yrday
fracday
Element set: 901
Inclination: 51
6376 deg
RA of node: 67
0038 deg
Eccentricity:
0003473
Arg of perigee: 131
1447 deg
Mean anomaly: 229
0005 deg
Mean motion: 15
52858072 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 194
Checksum: 300
Coasting Arc #3 (Orbit 194)
---------------------------------------
Vector Time (GMT): 2019/082/14:27:42
323
Vector Time (MET): N/A
Weight (LBS) : 914819
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3214963
43 A = 6794101
32 meter
Y = 5944695
23 meter E =
0011722
Z = -652222
02 I = 52
01029
XDOT = -3897
250084 Wp = 49
98608
YDOT = 2756
953875 meter/sec RA = 65
91747 deg
ZDOT = 5996
196839 TA = 303
01305
MA = 303
12563
Ha = 224
442 n
mi
Hp = 216
603
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10547780
27 X = 3151417
36
Y = 19503593
27 feet Y = 5980291
82 meter
Z = -2139836
04 Z = -636759
93
XDOT = -12786
253555 XDOT = -3956
915733
YDOT = 9045
124262 feet/sec YDOT = 2713
039180 meter/sec
ZDOT = 19672
561807 ZDOT = 5977
120185
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20145310
36 X = 6140290
60
Y = 9279242
83 feet Y = 2828313
21 meter
Z = -2070468
62 Z = -631078
83
XDOT = -4239
733693 XDOT = -1292
270830
YDOT = 13515
390438 feet/sec YDOT = 4119
491006 meter/sec
ZDOT = 19585
934980 ZDOT = 5969
792982
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 19082
60379381
00016717 00000-0 10270-3 0 9026
2 25544 51
6392 66
6837 0002117 106
8369 253
3015 15
52429174 1952
Satellite: ISS
Catalog Number: 25544
Epoch time: 19082
60379381 = yrday
fracday
Element set: 902
Inclination: 51
6392 deg
RA of node: 66
6837 deg
Eccentricity:
0002117
Arg of perigee: 106
8369 deg
Mean anomaly: 253
3015 deg
Mean motion: 15
52429174 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 195
Checksum: 312
Coasting Arc #4 (Orbit 200)
---------------------------------------
Vector Time (GMT): 2019/082/22:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 914819
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1658208
13 A = 6785595
29 meter
Y = 4750798
68 meter E =
0010781
Z = 4545985
27 I = 51
97576
XDOT = -5064
773732 Wp = 112
19816
YDOT = -4809
041523 meter/sec RA = 64
29338 deg
ZDOT = 3168
306938 TA = 306
12211
MA = 306
22185
Ha = 224
446 n
mi
Hp = 216
677
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5440315
38 X = -1733291
60
Y = 15586609
84 feet Y = 4731836
11 meter
Z = 14914649
84 Z = 4537747
42
XDOT = -16616
711719 XDOT = -5026
011162
YDOT = -15777
695287 feet/sec YDOT = -4865
462290 meter/sec
ZDOT = 10394
707801 ZDOT = 3143
798766
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11140410
56 X = 3395597
14
Y = -12229317
56 feet Y = -3727495
99 meter
Z = 14876870
05 Z = 4534469
99
XDOT = 8388
847383 XDOT = 2556
920682
YDOT = 20192
490621 feet/sec YDOT = 6154
671141 meter/sec
ZDOT = 10284
285237 ZDOT = 3134
650140
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 19082
99002857
00016717 00000-0 10270-3 0 9030
2 25544 51
6377 64
7608 0001997 111
3030 248
8335 15
52417485 2015
Satellite: ISS
Catalog Number: 25544
Epoch time: 19082
99002857 = yrday
fracday
Element set: 903
Inclination: 51
6377 deg
RA of node: 64
7608 deg
Eccentricity:
0001997
Arg of perigee: 111
3030 deg
Mean anomaly: 248
8335 deg
Mean motion: 15
52417485 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 201
Checksum: 309
Coasting Arc #5 (Orbit 215)
---------------------------------------
Vector Time (GMT): 2019/083/22:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 914819
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2266049
00 A = 6783549
64 meter
Y = -3933458
63 meter E =
0014676
Z = -5053956
24 I = 51
95331
XDOT = 5019
188831 Wp = 81
09287
YDOT = 5429
954576 meter/sec RA = 59
33722 deg
ZDOT = -1978
322548 TA = 169
76300
MA = 169
73309
Ha = 224
437 n
mi
Hp = 216
654
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7434543
96 X = 2334415
02
Y = -12905048
00 feet Y = -3907736
25 meter
Z = -16581221
27 Z = -5042782
21
XDOT = 16467
154956 XDOT = 4967
706126
YDOT = 17814
811601 feet/sec YDOT = 5485
794633 meter/sec
ZDOT = -6490
559542 ZDOT = -1954
066634
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11795615
45 X = -3595303
59
Y = 9185021
01 feet Y = 2799594
40 meter
Z = -16530228
43 Z = -5038413
62
XDOT = -8051
655654 XDOT = -2454
144643
YDOT = -21808
701673 feet/sec YDOT = -6647
292270 meter/sec
ZDOT = -6381
360191 ZDOT = -1945
038586
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 19083
95561603
00016717 00000-0 10270-3 0 9047
2 25544 51
6374 59
9596 0002263 116
6330 243
5053 15
52433590 2162
Satellite: ISS
Catalog Number: 25544
Epoch time: 19083
95561603 = yrday
fracday
Element set: 904
Inclination: 51
6374 deg
RA of node: 59
9596 deg
Eccentricity:
0002263
Arg of perigee: 116
6330 deg
Mean anomaly: 243
5053 deg
Mean motion: 15
52433590 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 216
Checksum: 303
Coasting Arc #6 (Orbit 231)
---------------------------------------
Vector Time (GMT): 2019/084/22:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 914819
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2907754
99 A = 6782548
35 meter
Y = 3068758
05 meter E =
0005222
Z = 5300086
14 I = 51
93202
XDOT = -4888
885851 Wp = 117
42405
YDOT = -5866
169759 meter/sec RA = 54
37673 deg
ZDOT = 711
481791 TA = 325
79196
MA = 325
82559
Ha = 224
567 n
mi
Hp = 216
681
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9539878
58 X = -2967599
53
Y = 10068103
82 feet Y = 3035907
23 meter
Z = 17388734
06 Z = 5285815
78
XDOT = -16039
651742 XDOT = -4826
381316
YDOT = -19245
963777 feet/sec YDOT = -5920
491170 meter/sec
ZDOT = 2334
257846 ZDOT = 687
885568
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12601898
32 X = 3841058
61
Y = -5985124
03 feet Y = -1824265
80 meter
Z = 17323813
65 Z = 5280298
40
XDOT = 7739
789002 XDOT = 2359
087688
YDOT = 22773
059891 feet/sec YDOT = 6941
228655 meter/sec
ZDOT = 2228
107055 ZDOT = 679
127030
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
98557376
00016717 00000-0 10270-3 0 9054
2 25544 51
6378 54
8379 0002200 119
8275 240
3095 15
52395788 2328
Satellite: ISS
Catalog Number: 25544
Epoch time: 19084
98557376 = yrday
fracday
Element set: 905
Inclination: 51
6378 deg
RA of node: 54
8379 deg
Eccentricity:
0002200
Arg of perigee: 119
8275 deg
Mean anomaly: 240
3095 deg
Mean motion: 15
52395788 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 232
Checksum: 336
Coasting Arc #7 (Orbit 246)
---------------------------------------
Vector Time (GMT): 2019/085/22:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 914819
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3606179
07 A = 6782389
42 meter
Y = -2200130
75 meter E =
0016752
Z = -5320693
83 I = 51
91290
XDOT = 4598
453887 Wp = 98
38958
YDOT = 6088
503188 meter/sec RA = 49
41410 deg
ZDOT = 598
278723 TA = 177
31494
MA = 177
30594
Ha = 224
402 n
mi
Hp = 216
694
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11831296
16 X = 3656358
49
Y = -7218276
73 feet Y = -2159523
64 meter
Z = -17456344
60 Z = -5303054
39
XDOT = 15086
790968 XDOT = 4527
122649
YDOT = 19975
404159 feet/sec YDOT = 6139
527509 meter/sec
ZDOT = 1962
856702 ZDOT = 620
442695
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13687496
30 X = -4171948
87
Y = 2743139
41 feet Y = 836108
89 meter
Z = -17376267
90 Z = -5296286
46
XDOT = -7211
703535 XDOT = -2198
127237
YDOT = -22903
631535 feet/sec YDOT = -6981
026892 meter/sec
ZDOT = 2062
486447 ZDOT = 628
645869
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
95115315
00016717 00000-0 10270-3 0 9066
2 25544 51
6391 50
0367 0002346 123
4447 236
6929 15
52447730 2476
Satellite: ISS
Catalog Number: 25544
Epoch time: 19085
95115315 = yrday
fracday
Element set: 906
Inclination: 51
6391 deg
RA of node: 50
0367 deg
Eccentricity:
0002346
Arg of perigee: 123
4447 deg
Mean anomaly: 236
6929 deg
Mean motion: 15
52447730 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 247
Checksum: 306
Coasting Arc #8 (Orbit 262)
---------------------------------------
Vector Time (GMT): 2019/086/22:28:00
000
Vector Time (MET): N/A
Weight (LBS) : 914819
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4295484
18 A = 6783559
60 meter
Y = 1353797
65 meter E =
0006830
Z = 5067557
26 I = 51
89270
XDOT = -4167
197280 Wp = 75
00286
YDOT = -6157
424991 meter/sec RA = 44
45056 deg
ZDOT = -1883
508108 TA = 33
20394
MA = 33
16110
Ha = 224
600 n
mi
Hp = 216
654
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14092795
88 X = -4334918
77
Y = 4441593
35 feet Y = 1305542
31 meter
Z = 16625844
02 Z = 5046595
64
XDOT = -13671
907087 XDOT = -4088
884492
YDOT = -20201
525561 feet/sec YDOT = -6203
587726 meter/sec
ZDOT = -6179
488544 ZDOT = -1903
560197
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14877577
05 X = 4534685
48
Y = 377936
36 feet Y = 115195
00 meter
Z = 16530825
80 Z = 5038595
71
XDOT = 6410
391290 XDOT = 1953
887265
YDOT = 22434
486682 feet/sec YDOT = 6838
031541 meter/sec
ZDOT = -6269
540194 ZDOT = -1910
955851
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
98110333
00016717 00000-0 10270-3 0 9076
2 25544 51
6378 44
9148 0002398 127
6297 232
5072 15
52411573 2634
Satellite: ISS
Catalog Number: 25544
Epoch time: 19086
98110333 = yrday
fracday
Element set: 907
Inclination: 51
6378 deg
RA of node: 44
9148 deg
Eccentricity:
0002398
Arg of perigee: 127
6297 deg
Mean anomaly: 232
5072 deg
Mean motion: 15
52411573 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 263
Checksum: 314
Coasting Arc #9 (Orbit 267)
---------------------------------------
Vector Time (GMT): 2019/087/06:36:30
000
Vector Time (MET): N/A
Weight (LBS) : 914819
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3274419
44 A = 6791902
95 meter
Y = -5487154
71 meter E =
0007997
Z = -2297527
46 I = 51
91687
XDOT = 5313
448808 Wp = 131
64892
YDOT = -897
075221 meter/sec RA = 42
80854 deg
ZDOT = -5447
603854 TA = 73
80977
MA = 73
72178
Ha = 224
321 n
mi
Hp = 216
584
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10742845
94 X = -3201657
10
Y = -18002476
07 feet Y = -5523364
83 meter
Z = -7537819
74 Z = -2313256
28
XDOT = 17432
574828 XDOT = 5349
546562
YDOT = -2943
160173 feet/sec YDOT = -837
454962 meter/sec
ZDOT = -17872
716058 ZDOT = -5421
705516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14974977
84 X = 4564373
25
Y = -14634863
41 feet Y = -4460706
37 meter
Z = -7608378
39 Z = -2319033
73
XDOT = 5931
888794 XDOT = 1808
039704
YDOT = 15271
051224 feet/sec YDOT = 4654
616413 meter/sec
ZDOT = -17755
407991 ZDOT = -5411
848356
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
30296024
00016717 00000-0 10270-3 0 9086
2 25544 51
6415 43
3181 0002229 124
0770 236
0594 15
52460479 2688
Satellite: ISS
Catalog Number: 25544
Epoch time: 19087
30296024 = yrday
fracday
Element set: 908
Inclination: 51
6415 deg
RA of node: 43
3181 deg
Eccentricity:
0002229
Arg of perigee: 124
0770 deg
Mean anomaly: 236
0594 deg
Mean motion: 15
52460479 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 268
Checksum: 298
Coasting Arc #10 (Orbit 283)
---------------------------------------
Vector Time (GMT): 2019/088/06:36:30
000
Vector Time (MET): N/A
Weight (LBS) : 914819
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2662358
81 A = 6789686
51 meter
Y = 5316061
25 meter E =
0014579
Z = 3267091
73 I = 51
88292
XDOT = -6006
849124 Wp = 92
69434
YDOT = 67
358974 meter/sec RA = 37
85805 deg
ZDOT = 4766
399232 TA = 305
04882
MA = 305
18551
Ha = 224
375 n
mi
Hp = 216
601
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8734773
01 X = 2586845
63
Y = 17441145
83 feet Y = 5345411
57 meter
Z = 10718804
89 Z = 3279840
67
XDOT = -19707
510248 XDOT = -6030
308268
YDOT = 220
994010 feet/sec YDOT =
055288 meter/sec
ZDOT = 15637
792757 ZDOT = 4737
163440
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14690326
28 X = -4477611
45
Y = 12785035
71 feet Y = 3896878
88 meter
Z = 10775888
89 Z = 3284490
93
XDOT = -4283
513646 XDOT = -1305
614959
YDOT = -18042
915709 feet/sec YDOT = -5499
480708 meter/sec
ZDOT = 15505
478937 ZDOT = 4726
069980
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
33290588
00016717 00000-0 10270-3 0 9090
2 25544 51
6404 38
1966 0002292 123
9197 236
2173 15
52437052 2844
Satellite: ISS
Catalog Number: 25544
Epoch time: 19088
33290588 = yrday
fracday
Element set: 909
Inclination: 51
6404 deg
RA of node: 38
1966 deg
Eccentricity:
0002292
Arg of perigee: 123
9197 deg
Mean anomaly: 236
2173 deg
Mean motion: 15
52437052 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 284
Checksum: 318
Coasting Arc #11 (Orbit 298)
---------------------------------------
Vector Time (GMT): 2019/089/06:36:30
000
Vector Time (MET): N/A
Weight (LBS) : 914819
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1872079
27 A = 6786933
79 meter
Y = -5065309
91 meter E =
0008851
Z = -4119411
32 I = 51
84902
XDOT = 6593
477172 Wp = 82
50776
YDOT = 677
417414 meter/sec RA = 32
90153 deg
ZDOT = -3835
325312 TA = 147
95933
MA = 147
90549
Ha = 224
256 n
mi
Hp = 216
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6141992
34 X = -1795288
75
Y = -16618470
84 feet Y = -5085815
72 meter
Z = -13515129
01 Z = -4128318
26
XDOT = 21632
142954 XDOT = 6604
041783
YDOT = 2222
498079 feet/sec YDOT = 751
209103 meter/sec
ZDOT = -12583
088294 ZDOT = -3803
271334
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14378627
66 X = 4382605
71
Y = -10299393
07 feet Y = -3139255
01 meter
Z = -13554848
73 Z = -4131517
89
XDOT = 2951
459499 XDOT = 899
604855
YDOT = 20464
467419 feet/sec YDOT = 6237
569669 meter/sec
ZDOT = -12438
113172 ZDOT = -3791
136895
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
29847321
00016717 00000-0 10270-3 0 9101
2 25544 51
6422 33
3957 0002165 129
7905 230
3438 15
52472605 2999
Satellite: ISS
Catalog Number: 25544
Epoch time: 19089
29847321 = yrday
fracday
Element set: 910
Inclination: 51
6422 deg
RA of node: 33
3957 deg
Eccentricity:
0002165
Arg of perigee: 129
7905 deg
Mean anomaly: 230
3438 deg
Mean motion: 15
52472605 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 299
Checksum: 314
Coasting Arc #12 (Orbit 314)
---------------------------------------
Vector Time (GMT): 2019/090/06:36:30
000
Vector Time (MET): N/A
Weight (LBS) : 914819
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 983282
78 A = 6784607
10 meter
Y = 4744950
38 meter E =
0009839
Z = 4743448
38 I = 51
81087
XDOT = -7043
764025 Wp = 120
01856
YDOT = -1292
376764 meter/sec RA = 27
93797 deg
ZDOT = 2743
851146 TA = 302
85554
MA = 302
95022
Ha = 224
275 n
mi
Hp = 216
638
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3225993
38 X = 907109
48
Y = 15567422
51 feet Y = 4755520
60 meter
Z = 15562494
70 Z = 4748039
38
XDOT = -23109
462024 XDOT = -7042
116786
YDOT = -4240
081248 feet/sec YDOT = -1371
135635 meter/sec
ZDOT = 9002
136305 ZDOT = 2709
639587
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14028766
33 X = -4275967
98
Y = 7437444
11 feet Y = 2266932
96 meter
Z = 15582716
66 Z = 4749612
04
XDOT = -2010
863497 XDOT = -612
911194
YDOT = -22392
113037 feet/sec YDOT = -6825
116054 meter/sec
ZDOT = 8847
478193 ZDOT = 2696
711353
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
32840926
00016717 00000-0 10270-3 0 9112
2 25544 51
6405 28
2740 0002214 129
9148 230
2198 15
52465720 3150
Satellite: ISS
Catalog Number: 25544
Epoch time: 19090
32840926 = yrday
fracday
Element set: 911
Inclination: 51
6405 deg
RA of node: 28
2740 deg
Eccentricity:
0002214
Arg of perigee: 129
9148 deg
Mean anomaly: 230
2198 deg
Mean motion: 15
52465720 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 315
Checksum: 286
Coasting Arc #13 (Orbit 323)
---------------------------------------
Vector Time (GMT): 2019/090/20:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 914819
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3516454
17 A = 6788965
13 meter
Y = 4654448
83 meter E =
0013760
Z = 3463006
50 I = 51
80574
XDOT = -6043
887540 Wp = 97
98454
YDOT = 1147
333515 meter/sec RA = 25
08545 deg
ZDOT = 4577
680390 TA = 302
52104
MA = 302
65392
Ha = 224
123 n
mi
Hp = 216
705
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11536923
12 X = 3447324
23
Y = 15270501
42 feet Y = 4693386
05 meter
Z = 11361569
90 Z = 3479919
67
XDOT = -19829
027362 XDOT = -6078
503802
YDOT = 3764
217569 feet/sec YDOT = 1079
553380 meter/sec
ZDOT = 15018
636450 ZDOT = 4548
237523
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2930436
76 X = 893197
12
Y = -18867138
59 feet Y = -5750703
84 meter
Z = 11437556
59 Z = 3486167
25
XDOT = 15234
552198 XDOT = 4643
491510
YDOT = 11424
322908 feet/sec YDOT = 3482
133622 meter/sec
ZDOT = 14885
277613 ZDOT = 4537
032616
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
90774664
00016717 00000-0 10270-3 0 9122
2 25544 51
6377 25
3900 0002208 142
0405 218
0903 15
52486018 3240
Satellite: ISS
Catalog Number: 25544
Epoch time: 19090
90774664 = yrday
fracday
Element set: 912
Inclination: 51
6377 deg
RA of node: 25
3900 deg
Eccentricity:
0002208
Arg of perigee: 142
0405 deg
Mean anomaly: 218
0903 deg
Mean motion: 15
52486018 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 324
Checksum: 286
Coasting Arc #14 (Orbit 338)
---------------------------------------
Vector Time (GMT): 2019/091/20:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 914819
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2653469
99 A = 6786291
78 meter
Y = -4560511
67 meter E =
0009321
Z = -4276656
72 I = 51
76826
XDOT = 6737
133671 Wp = 82
14226
YDOT = -550
655590 meter/sec RA = 20
12293 deg
ZDOT = -3598
354794 TA = 151
14193
MA = 151
09035
Ha = 224
142 n
mi
Hp = 216
646
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8705610
19 X = -2581502
35
Y = -14962308
63 feet Y = -4589782
66 meter
Z = -14031025
97 Z = -4289370
95
XDOT = 22103
456927 XDOT = 6760
269237
YDOT = -1806
612828 feet/sec YDOT = -475
187242 meter/sec
ZDOT = -11805
625964 ZDOT = -3565
572300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4412794
42 X = -1345019
74
Y = 16690806
07 feet Y = 5087357
69 meter
Z = -14088018
18 Z = -4294027
94
XDOT = -15813
639253 XDOT = -4819
997244
YDOT = -14005
173771 feet/sec YDOT = -4268
776965 meter/sec
ZDOT = -11657
236779 ZDOT = -3553
125770
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
87330644
00016717 00000-0 10270-3 0 9136
2 25544 51
6396 20
5893 0002197 141
0389 219
0921 15
52494677 3393
Satellite: ISS
Catalog Number: 25544
Epoch time: 19091
87330644 = yrday
fracday
Element set: 913
Inclination: 51
6396 deg
RA of node: 20
5893 deg
Eccentricity:
0002197
Arg of perigee: 141
0389 deg
Mean anomaly: 219
0921 deg
Mean motion: 15
52494677 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 339
Checksum: 323
Coasting Arc #15 (Orbit 354)
---------------------------------------
Vector Time (GMT): 2019/092/20:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 914819
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1685198
38 A = 6784026
09 meter
Y = 4424318
95 meter E =
0008922
Z = 4854713
01 I = 51
72910
XDOT = -7260
874821 Wp = 126
43435
YDOT = 49
869718 meter/sec RA = 15
15227 deg
ZDOT = 2466
664113 TA = 299
33459
MA = 299
42369
Ha = 224
029 n
mi
Hp = 216
772
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5528866
07 X = 1612017
73
Y = 14515482
13 feet Y = 4442755
36 meter
Z = 15927536
14 Z = 4862720
83
XDOT = -23821
767786 XDOT = -7272
874476
YDOT = 163
614559 feet/sec YDOT = -31
393296 meter/sec
ZDOT = 8092
730031 ZDOT = 2431
364497
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6120268
56 X = 1865457
86
Y = -14236259
51 feet Y = -4339211
90 meter
Z = 15963245
81 Z = 4865597
32
XDOT = 16323
713390 XDOT = 4975
467841
YDOT = 15943
619711 feet/sec YDOT = 4859
615288 meter/sec
ZDOT = 7933
025023 ZDOT = 2417
986027
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
90322984
00016717 00000-0 10270-3 0 9140
2 25544 51
6396 15
4669 0002156 148
1680 211
9602 15
52502980 3556
Satellite: ISS
Catalog Number: 25544
Epoch time: 19092
90322984 = yrday
fracday
Element set: 914
Inclination: 51
6396 deg
RA of node: 15
4669 deg
Eccentricity:
0002156
Arg of perigee: 148
1680 deg
Mean anomaly: 211
9602 deg
Mean motion: 15
52502980 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 355
Checksum: 310
Coasting Arc #16 (Orbit 369)
---------------------------------------
Vector Time (GMT): 2019/093/20:25:00
000
Vector Time (MET): N/A
Weight (LBS) : 914819
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -598882
96 A = 6782517
86 meter
Y = -4300288
53 meter E =
0015234
Z = -5223936
63 I = 51
69207
XDOT = 7550
369588 Wp = 88
58266
YDOT = 396
627987 meter/sec RA = 10
17800 deg
ZDOT = -1194
737441 TA = 169
95948
MA = 169
92901
Ha = 224
100 n
mi
Hp = 216
710
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1964839
12 X = -525376
43
Y = -14108558
17 feet Y = -4306575
24 meter
Z = -17138899
69 Z = -5226666
76
XDOT = 24771
553765 XDOT = 7551
176593
YDOT = 1301
272924 feet/sec YDOT = 481
065884 meter/sec
ZDOT = -3919
742261 ZDOT = -1158
058674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8220935
82 X = -2505741
24
Y = 11615595
12 feet Y = 3540433
39 meter
Z = -17150744
97 Z = -5227547
07
XDOT = -16476
273790 XDOT = -5021
968251
YDOT = -17190
951453 feet/sec YDOT = -5239
802003 meter/sec
ZDOT = -3753
866628 ZDOT = -1144
178548
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
86877952
00016717 00000-0 10270-3 0 9157
2 25544 51
6401 10
6671 0002268 147
6582 212
4710 15
52506351 3701
Satellite: ISS
Catalog Number: 25544
Epoch time: 19093
86877952 = yrday
fracday
Element set: 915
Inclination: 51
6401 deg
RA of node: 10
6671 deg
Eccentricity:
0002268
Arg of perigee: 147
6582 deg
Mean anomaly: 212
4710 deg
Mean motion: 15
52506351 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 370
Checksum: 302
Coasting Arc #17 (Orbit 379)
---------------------------------------
Vector Time (GMT): 2019/094/11:01:35
000
Vector Time (MET): N/A
Weight (LBS) : 914819
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2596981
58 A = 6784423
47 meter
Y = 4099587
98 meter E =
0009218
Z = 4736616
84 I = 51
67977
XDOT = -7046
343268 Wp = 123
33596
YDOT = 1292
823168 meter/sec RA = 7
16853 deg
ZDOT = 2735
604625 TA = 299
57296
MA = 299
66479
Ha = 223
861 n
mi
Hp = 216
832
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8520280
79 X = 2527937
91
Y = 13450091
80 feet Y = 4128243
73 meter
Z = 15540081
49 Z = 4749063
88
XDOT = -23117
924108 XDOT = -7073
564365
YDOT = 4241
545828 feet/sec YDOT = 1213
874127 meter/sec
ZDOT = 8975
080791 ZDOT = 2701
309800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7697368
52 X = 2346157
92
Y = 13874892
50 feet Y = 4229067
23 meter
Z = 15595902
11 Z = 4753630
96
XDOT = -22356
668914 XDOT = -6814
312685
YDOT = 2456
684933 feet/sec YDOT = 748
797568 meter/sec
ZDOT = 8819
800361 ZDOT = 2688
275150
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
51247576
00016717 00000-0 10270-3 0 9164
2 25544 51
6411 7
4703 0001801 150
1017 210
0238 15
52523589 3808
Satellite: ISS
Catalog Number: 25544
Epoch time: 19094
51247576 = yrday
fracday
Element set: 916
Inclination: 51
6411 deg
RA of node: 7
4703 deg
Eccentricity:
0001801
Arg of perigee: 150
1017 deg
Mean anomaly: 210
0238 deg
Mean motion: 15
52523589 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 380
Checksum: 276
Coasting Arc #18 (Orbit 381)
---------------------------------------
Vector Time (GMT): 2019/094/14:24:50
000
Vector Time (MET): N/A
Weight (LBS) : 929253
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4895280
93 A = 6787541
13 meter
Y = 2571103
08 meter E =
0011941
Z = 3926616
82 I = 51
68688
XDOT = -5269
825970 Wp = 87
60690
YDOT = -3819
518746 meter/sec RA = 6
42208 deg
ZDOT = -4057
728576 TA = 44
83891
MA = 44
74249
Ha = 223
983 n
mi
Hp = 216
855
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16060632
96 X = -4942741
28
Y = 8435377
56 feet Y = 2516095
69 meter
Z = 12882601
10 Z = 3902721
75
XDOT = -17289
455283 XDOT = -5207
013114
YDOT = -12531
229481 feet/sec YDOT = -3878
098870 meter/sec
ZDOT = -13312
757795 ZDOT = -4083
174499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4553716
64 X = -1387972
83
Y = 17639276
04 feet Y = 5376451
34 meter
Z = 12774213
96 Z = 3893580
41
XDOT = -19540
592676 XDOT = -5955
972648
YDOT = 4706
160190 feet/sec YDOT = 1434
437626 meter/sec
ZDOT = -13427
408222 ZDOT = -4092
674026
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
64121434
00016717 00000-0 10270-3 0 9173
2 25544 51
6426 6
8310 0001606 147
2500 212
8751 15
52535585 3829
Satellite: ISS
Catalog Number: 25544
Epoch time: 19094
64121434 = yrday
fracday
Element set: 917
Inclination: 51
6426 deg
RA of node: 6
8310 deg
Eccentricity:
0001606
Arg of perigee: 147
2500 deg
Mean anomaly: 212
8751 deg
Mean motion: 15
52535585 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 382
Checksum: 286
Coasting Arc #19 (Orbit 396)
---------------------------------------
Vector Time (GMT): 2019/095/14:24:50
000
Vector Time (MET): N/A
Weight (LBS) : 929253
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5624397
05 A = 6790206
17 meter
Y = -2273525
17 meter E =
0004871
Z = -3054297
18 I = 51
66226
XDOT = 4288
707717 Wp = 88
22689
YDOT = 4004
035365 meter/sec RA = 1
45296 deg
ZDOT = 4923
990244 TA = 236
79144
MA = 236
83816
Ha = 223
864 n
mi
Hp = 217
053
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18452746
21 X = 5664238
42
Y = -7459072
07 feet Y = -2210406
77 meter
Z = -10020660
04 Z = -3026878
78
XDOT = 14070
563375 XDOT = 4219
696534
YDOT = 13136
598967 feet/sec YDOT = 4051
609343 meter/sec
ZDOT = 16154
823634 ZDOT = 4944
655286
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6544872
53 X = 1994877
15
Y = -18862170
57 feet Y = -5749189
59 meter
Z = -9896382
74 Z = -3016417
46
XDOT = 17702
137024 XDOT = 5395
611365
YDOT = -2370
250881 feet/sec YDOT = -722
452469 meter/sec
ZDOT = 16247
815994 ZDOT = 4952
334315
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
60675596
00016717 00000-0 10270-3 0 9184
2 25544 51
6426 2
0296 0001553 156
6885 203
4337 15
52503534 3972
Satellite: ISS
Catalog Number: 25544
Epoch time: 19095
60675596 = yrday
fracday
Element set: 918
Inclination: 51
6426 deg
RA of node: 2
0296 deg
Eccentricity:
0001553
Arg of perigee: 156
6885 deg
Mean anomaly: 203
4337 deg
Mean motion: 15
52503534 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 397
Checksum: 320
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