[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 15th 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14538 8138 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 475 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
231/17:35:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
2
000/00:00:00
000 0
0 0
0 222
2
234/09:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
1
000/00:00:00
000 0
0 0
0 222
1
238/20:27:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
4
000/00:00:00
000 0
0 0
0 221
8
Coasting Arc #1 (Orbit 73)
---------------------------------------
Vector Time (GMT): 2020/225/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1832476
05 A = 6795687
70 meter
Y = -4842973
89 meter E =
0009644
Z = -4411058
15 I = 52
00064
XDOT = 4755
114894 Wp = 62
52374
YDOT = 4918
602475 meter/sec RA = 69
00169 deg
ZDOT = -3426
225266 TA = 172
85451
MA = 172
84075
Ha = 228
976 n
mi
Hp = 222
465
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6012060
52 X = 1907921
69
Y = -15889021
94 feet Y = -4822059
75 meter
Z = -14471975
57 Z = -4401973
78
XDOT = 15600
770651 XDOT = 4716
402734
YDOT = 16137
147228 feet/sec YDOT = 4971
561299 meter/sec
ZDOT = -11240
896541 ZDOT = -3403
220686
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14823078
98 X = -4518074
47
Y = 8372665
02 feet Y = 2551988
30 meter
Z = -14429787
82 Z = -4398199
33
XDOT = -1220
187247 XDOT = -371
913073
YDOT = -21342
545455 feet/sec YDOT = -6505
207855 meter/sec
ZDOT = -11134
905445 ZDOT = -3393
919180
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 20225
52232684
00016717 00000-0 10270-3 0 9000
2 25544 51
6415 69
6636 0001326 10
2223 349
8954 15
49155900 744
Satellite: ISS
Catalog Number: 25544
Epoch time: 20225
52232684 = yrday
fracday
Element set: 900
Inclination: 51
6415 deg
RA of node: 69
6636 deg
Eccentricity:
0001326
Arg of perigee: 10
2223 deg
Mean anomaly: 349
8954 deg
Mean motion: 15
49155900 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 74
Checksum: 288
Coasting Arc #2 (Orbit 89)
---------------------------------------
Vector Time (GMT): 2020/226/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1450632
06 A = 6795636
71 meter
Y = 4937960
33 meter E =
0009237
Z = 4430877
18 I = 51
98767
XDOT = -5152
699905 Wp = 101
02129
YDOT = -4554
880347 meter/sec RA = 64
07775 deg
ZDOT = 3381
521681 TA = 314
88296
MA = 314
95791
Ha = 229
105 n
mi
Hp = 222
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4759291
54 X = -1527264
49
Y = 16200657
25 feet Y = 4921309
54 meter
Z = 14536998
63 Z = 4423644
85
XDOT = -16905
183414 XDOT = -5117
808277
YDOT = -14943
833160 feet/sec YDOT = -4612
306662 meter/sec
ZDOT = 11094
231238 ZDOT = 3356
576510
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13891161
25 X = 4234025
95
Y = -9650132
47 feet Y = -2941360
38 meter
Z = 14503346
60 Z = 4420620
04
XDOT = 3275
407159 XDOT = 998
344102
YDOT = 21253
779344 feet/sec YDOT = 6478
151944 meter/sec
ZDOT = 10979
271423 ZDOT = 3346
481930
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 20226
55446480
00016717 00000-0 10270-3 0 9016
2 25544 51
6422 64
5564 0001409 12
5879 347
5306 15
49135563 907
Satellite: ISS
Catalog Number: 25544
Epoch time: 20226
55446480 = yrday
fracday
Element set: 901
Inclination: 51
6422 deg
RA of node: 64
5564 deg
Eccentricity:
0001409
Arg of perigee: 12
5879 deg
Mean anomaly: 347
5306 deg
Mean motion: 15
49135563 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 90
Checksum: 297
Coasting Arc #3 (Orbit 104)
---------------------------------------
Vector Time (GMT): 2020/227/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1085447
80 A = 6795410
69 meter
Y = -5007410
73 meter E =
0010274
Z = -4474316
24 I = 51
97025
XDOT = 5502
534459 Wp = 63
47168
YDOT = 4154
753049 meter/sec RA = 59
15260 deg
ZDOT = -3316
311390 TA = 173
14933
MA = 173
13528
Ha = 229
063 n
mi
Hp = 222
330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3561180
45 X = 1163094
92
Y = -16428512
89 feet Y = -4994837
97 meter
Z = -14679515
22 Z = -4468855
42
XDOT = 18052
934577 XDOT = 5471
774374
YDOT = 13631
079556 feet/sec YDOT = 4216
114592 meter/sec
ZDOT = -10880
286711 ZDOT = -3289
656905
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12912637
44 X = -3935771
89
Y = 10797658
42 feet Y = 3291126
28 meter
Z = -14654029
34 Z = -4466548
14
XDOT = -5282
902412 XDOT = -1610
228655
YDOT = -20910
741207 feet/sec YDOT = -6373
593920 meter/sec
ZDOT = -10757
421021 ZDOT = -3278
861927
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 20227
52209074
00016717 00000-0 10270-3 0 9021
2 25544 51
6411 59
7683 0001396 21
7448 338
3761 15
49163833 1053
Satellite: ISS
Catalog Number: 25544
Epoch time: 20227
52209074 = yrday
fracday
Element set: 902
Inclination: 51
6411 deg
RA of node: 59
7683 deg
Eccentricity:
0001396
Arg of perigee: 21
7448 deg
Mean anomaly: 338
3761 deg
Mean motion: 15
49163833 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 105
Checksum: 298
Coasting Arc #4 (Orbit 120)
---------------------------------------
Vector Time (GMT): 2020/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -700693
76 A = 6795347
53 meter
Y = 5043447
55 meter E =
0009128
Z = 4493342
17 I = 51
95095
XDOT = -5841
771641 Wp = 102
48831
YDOT = -3730
887155 meter/sec RA = 54
22689 deg
ZDOT = 3269
166012 TA = 314
67554
MA = 314
74988
Ha = 229
132 n
mi
Hp = 222
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2298864
06 X = -778864
78
Y = 16546743
93 feet Y = 5035174
45 meter
Z = 14741936
26 Z = 4489749
07
XDOT = -19165
917456 XDOT = -5815
497071
YDOT = -12240
443423 feet/sec YDOT = -3796
067371 meter/sec
ZDOT = 10725
610275 ZDOT = 3240
852914
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11781684
12 X = 3591057
32
Y = -11864594
05 feet Y = -3616328
27 meter
Z = 14725064
44 Z = 4488199
64
XDOT = 7301
465191 XDOT = 2225
486590
YDOT = 20430
534833 feet/sec YDOT = 6227
227017 meter/sec
ZDOT = 10595
068365 ZDOT = 3229
376838
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 20228
55422589
00016717 00000-0 10270-3 0 9034
2 25544 51
6405 54
6614 0001379 21
9435 338
1774 15
49147344 1212
Satellite: ISS
Catalog Number: 25544
Epoch time: 20228
55422589 = yrday
fracday
Element set: 903
Inclination: 51
6405 deg
RA of node: 54
6614 deg
Eccentricity:
0001379
Arg of perigee: 21
9435 deg
Mean anomaly: 338
1774 deg
Mean motion: 15
49147344 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 121
Checksum: 300
Coasting Arc #5 (Orbit 135)
---------------------------------------
Vector Time (GMT): 2020/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 335502
27 A = 6795139
97 meter
Y = -5058253
91 meter E =
0010799
Z = -4535901
80 I = 51
92924
XDOT = 6127
127438 Wp = 65
15529
YDOT = 3276
716641 meter/sec RA = 49
29952 deg
ZDOT = -3202
431887 TA = 172
73248
MA = 172
71682
Ha = 229
125 n
mi
Hp = 222
212
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1100729
25 X = 414072
64
Y = -16595321
21 feet Y = -5054062
45 meter
Z = -14881567
58 Z = -4534081
62
XDOT = 20102
124140 XDOT = 6105
586114
YDOT = 10750
382681 feet/sec YDOT = 3345
114340 meter/sec
ZDOT = -10506
666295 ZDOT = -3172
721361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10630255
01 X = -3240101
73
Y = 12801273
06 feet Y = 3901828
03 meter
Z = -14872875
69 Z = -4533252
51
XDOT = -9225
120536 XDOT = -2811
816739
YDOT = -19702
360533 feet/sec YDOT = -6005
279490 meter/sec
ZDOT = -10369
650302 ZDOT = -3160
669412
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 20229
52185183
00016717 00000-0 10270-3 0 9049
2 25544 51
6400 49
8735 0001352 34
1830 325
9407 15
49170345 1363
Satellite: ISS
Catalog Number: 25544
Epoch time: 20229
52185183 = yrday
fracday
Element set: 904
Inclination: 51
6400 deg
RA of node: 49
8735 deg
Eccentricity:
0001352
Arg of perigee: 34
1830 deg
Mean anomaly: 325
9407 deg
Mean motion: 15
49170345 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 136
Checksum: 286
Coasting Arc #6 (Orbit 151)
---------------------------------------
Vector Time (GMT): 2020/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 43907
60 A = 6795036
27 meter
Y = 5037200
10 meter E =
0008949
Z = 4554107
17 I = 51
90629
XDOT = -6398
612420 Wp = 104
55421
YDOT = -2801
608401 meter/sec RA = 44
37022 deg
ZDOT = 3153
124258 TA = 313
88969
MA = 313
96356
Ha = 229
106 n
mi
Hp = 222
243
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 144053
80 X = -34543
88
Y = 16526247
06 feet Y = 5037252
22 meter
Z = 14941296
49 Z = 4554130
18
XDOT = -20992
822899 XDOT = -6382
124162
YDOT = -9191
628613 feet/sec YDOT = -2873
070232 meter/sec
ZDOT = 10344
895858 ZDOT = 3122
082915
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9344738
53 X = 2848276
30
Y = -13631541
55 feet Y = -4154893
86 meter
Z = 14941113
45 Z = 4554051
38
XDOT = 11132
368963 XDOT = 3393
146060
YDOT = 18839
767272 feet/sec YDOT = 5742
361064 meter/sec
ZDOT = 10201
711447 ZDOT = 3109
481649
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 20230
55398432
00016717 00000-0 10270-3 0 9058
2 25544 51
6404 44
7659 0001266 30
0257 330
0965 15
49167681 1521
Satellite: ISS
Catalog Number: 25544
Epoch time: 20230
55398432 = yrday
fracday
Element set: 905
Inclination: 51
6404 deg
RA of node: 44
7659 deg
Eccentricity:
0001266
Arg of perigee: 30
0257 deg
Mean anomaly: 330
0965 deg
Mean motion: 15
49167681 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 152
Checksum: 293
Coasting Arc #7 (Orbit 166)
---------------------------------------
Vector Time (GMT): 2020/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 958140
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -399451
71 A = 6794855
07 meter
Y = -4998589
66 meter E =
0011414
Z = -4596651
37 I = 51
88164
XDOT = 6611
110065 Wp = 66
46294
YDOT = 2305
583424 meter/sec RA = 39
43982 deg
ZDOT = -3083
333788 TA = 172
72983
MA = 172
71326
Ha = 229
206 n
mi
Hp = 222
066
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1310537
11 X = -321198
95
Y = -16399572
37 feet Y = -5002618
95 meter
Z = -15080877
21 Z = -4598401
79
XDOT = 21689
993651 XDOT = 6599
813693
YDOT = 7564
250079 feet/sec YDOT = 2379
450507 meter/sec
ZDOT = -10115
924500 ZDOT = -3051
247772
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8067927
93 X = -2459104
43
Y = 14329580
69 feet Y = 4367656
19 meter
Z = -15088671
09 Z = -4599026
95
XDOT = -12895
263527 XDOT = -3930
476323
YDOT = -17750
645690 feet/sec YDOT = -5410
396806 meter/sec
ZDOT = -9967
893072 ZDOT = -3038
213808
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 20231
52160768
00016717 00000-0 10270-3 0 9066
2 25544 51
6412 39
9781 0001475 45
4072 314
7198 15
49181743 1677
Satellite: ISS
Catalog Number: 25544
Epoch time: 20231
52160768 = yrday
fracday
Element set: 906
Inclination: 51
6412 deg
RA of node: 39
9781 deg
Eccentricity:
0001475
Arg of perigee: 45
4072 deg
Mean anomaly: 314
7198 deg
Mean motion: 15
49181743 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 167
Checksum: 307
Coasting Arc #8 (Orbit 170)
---------------------------------------
Vector Time (GMT): 2020/231/17:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 928399
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3267133
25 A = 6791938
26 meter
Y = 2717303
64 meter E =
0004342
Z = 5295610
23 I = 51
86955
XDOT = -5586
051496 Wp = 53
92148
YDOT = -5187
429519 meter/sec RA = 38
26485 deg
ZDOT = -781
589715 TA = 43
54571
MA = 43
51144
Ha = 229
154 n
mi
Hp = 222
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10718941
10 X = -3322998
54
Y = 8915038
19 feet Y = 2680455
74 meter
Z = 17374049
30 Z = 5279604
54
XDOT = -18326
940604 XDOT = -5523
832520
YDOT = -17019
125718 feet/sec YDOT = -5249
548837 meter/sec
ZDOT = -2564
270719 ZDOT = -808
572887
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 41184
13 X = 12552
92
Y = -14033534
55 feet Y = -4277421
33 meter
Z = 17299982
80 Z = 5273034
76
XDOT = 23761
508952 XDOT = 7242
507929
YDOT = -3256
563521 feet/sec YDOT = -992
600561 meter/sec
ZDOT = -2688
570210 ZDOT = -819
476200
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 20231
77963806
00016717 00000-0 10270-3 0 9078
2 25544 51
6448 38
7024 0001156 36
0254 324
0974 15
49206016 1719
Satellite: ISS
Catalog Number: 25544
Epoch time: 20231
77963806 = yrday
fracday
Element set: 907
Inclination: 51
6448 deg
RA of node: 38
7024 deg
Eccentricity:
0001156
Arg of perigee: 36
0254 deg
Mean anomaly: 324
0974 deg
Mean motion: 15
49206016 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 171
Checksum: 291
Coasting Arc #9 (Orbit 185)
---------------------------------------
Vector Time (GMT): 2020/232/17:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 928399
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3085491
77 A = 6792112
41 meter
Y = -2951017
51 meter E =
0015150
Z = -5295588
27 I = 51
84128
XDOT = 5961
697552 Wp = 92
50841
YDOT = 4717
080639 meter/sec RA = 33
33321 deg
ZDOT = 846
411810 TA = 185
57312
MA = 185
59000
Ha = 229
145 n
mi
Hp = 222
285
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10123004
49 X = 3143983
95
Y = -9681815
96 feet Y = -2916186
31 meter
Z = -17373977
25 Z = -5280458
43
XDOT = 19559
375171 XDOT = 5904
395373
YDOT = 15475
986348 feet/sec YDOT = 4783
428214 meter/sec
ZDOT = 2776
941634 ZDOT = 875
231523
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1171241
58 X = 356994
43
Y = 14045267
25 feet Y = 4280997
46 meter
Z = -17303945
41 Z = -5274242
56
XDOT = -23263
893034 XDOT = -7090
834597
YDOT = 5518
947745 feet/sec YDOT = 1682
175273 meter/sec
ZDOT = 2909
740268 ZDOT = 886
888834
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 20232
74726153
00016717 00000-0 10270-3 0 9089
2 25544 51
6437 33
9158 0001243 40
5850 319
5393 15
49163676 1865
Satellite: ISS
Catalog Number: 25544
Epoch time: 20232
74726153 = yrday
fracday
Element set: 908
Inclination: 51
6437 deg
RA of node: 33
9158 deg
Eccentricity:
0001243
Arg of perigee: 40
5850 deg
Mean anomaly: 319
5393 deg
Mean motion: 15
49163676 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 186
Checksum: 308
Coasting Arc #10 (Orbit 201)
---------------------------------------
Vector Time (GMT): 2020/233/17:35:00
000
Vector Time (MET): N/A
Weight (LBS) : 928399
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2887336
44 A = 6792036
06 meter
Y = 3154531
52 meter E =
0004637
Z = 5273863
38 I = 51
81327
XDOT = -6317
631131 Wp = 53
95520
YDOT = -4238
602431 meter/sec RA = 28
39876 deg
ZDOT = -920
256905 TA = 44
85176
MA = 44
81429
Ha = 229
169 n
mi
Hp = 222
147
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9472888
60 X = -2948013
68
Y = 10349512
85 feet Y = 3121904
13 meter
Z = 17302701
38 Z = 5259690
65
XDOT = -20727
136257 XDOT = -6265
294277
YDOT = -13906
175956 feet/sec YDOT = -4308
958095 meter/sec
ZDOT = -3019
215568 ZDOT = -950
817650
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2338697
15 X = -712834
89
Y = -13915639
17 feet Y = -4241486
82 meter
Z = 17237081
89 Z = 5253862
56
XDOT = 22642
437343 XDOT = 6901
414902
YDOT = -7732
831269 feet/sec YDOT = -2356
966971 meter/sec
ZDOT = -3160
068845 ZDOT = -963
188984
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 20233
77939013
00016717 00000-0 10270-3 0 9095
2 25544 51
6444 28
8091 0001136 41
8897 318
2340 15
49201700 2026
Satellite: ISS
Catalog Number: 25544
Epoch time: 20233
77939013 = yrday
fracday
Element set: 909
Inclination: 51
6444 deg
RA of node: 28
8091 deg
Eccentricity:
0001136
Arg of perigee: 41
8897 deg
Mean anomaly: 318
2340 deg
Mean motion: 15
49201700 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 202
Checksum: 285
Coasting Arc #11 (Orbit 211)
---------------------------------------
Vector Time (GMT): 2020/234/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 928399
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5177415
44 A = 6802284
42 meter
Y = -4014824
39 meter E =
0006956
Z = -1823815
88 I = 51
82488
XDOT = 4251
005408 Wp = 128
31405
YDOT = -2919
672810 meter/sec RA = 25
14951 deg
ZDOT = -5659
352038 TA = 71
63215
MA = 71
55652
Ha = 229
147 n
mi
Hp = 222
095
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16986271
12 X = -5123276
76
Y = -13171996
02 feet Y = -4072419
31 meter
Z = -5983647
92 Z = -1848833
70
XDOT = 13946
868138 XDOT = 4310
827578
YDOT = -9578
979037 feet/sec YDOT = -2871
800749 meter/sec
ZDOT = -18567
427946 ZDOT = -5638
557248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5950894
75 X = -1813832
72
Y = 20621082
03 feet Y = 6285305
80 meter
Z = -6098914
29 Z = -1858949
08
XDOT = -12611
266712 XDOT = -3843
914094
YDOT = -9084
536308 feet/sec YDOT = -2768
966667 meter/sec
ZDOT = -18471
253068 ZDOT = -5630
037935
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 20234
42447094
00016717 00000-0 10270-3 0 9103
2 25544 51
6418 25
6170 0001522 36
9132 323
2122 15
49182509 2126
Satellite: ISS
Catalog Number: 25544
Epoch time: 20234
42447094 = yrday
fracday
Element set: 910
Inclination: 51
6418 deg
RA of node: 25
6170 deg
Eccentricity:
0001522
Arg of perigee: 36
9132 deg
Mean anomaly: 323
2122 deg
Mean motion: 15
49182509 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 212
Checksum: 263
Coasting Arc #12 (Orbit 227)
---------------------------------------
Vector Time (GMT): 2020/235/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 928399
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5467594
20 A = 6802242
32 meter
Y = 3577191
07 meter E =
0015282
Z = 1864917
92 I = 51
79325
XDOT = -4052
859399 Wp = 64
48838
YDOT = 3238
720844 meter/sec RA = 20
21185 deg
ZDOT = 5640
252146 TA = 315
95532
MA = 316
07696
Ha = 229
188 n
mi
Hp = 222
048
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17938301
17 X = 5418128
00
Y = 11736191
19 feet Y = 3638057
12 meter
Z = 6118497
11 Z = 1891356
78
XDOT = -13296
782805 XDOT = -4116
171364
YDOT = 10625
724554 feet/sec YDOT = 3193
045100 meter/sec
ZDOT = 18504
764260 ZDOT = 5620
411246
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3903423
42 X = 1189763
46
Y = -21042298
75 feet Y = -6413692
66 meter
Z = 6240335
59 Z = 1902054
29
XDOT = 13455
974193 XDOT = 4101
380934
YDOT = 7984
981422 feet/sec YDOT = 2433
822337 meter/sec
ZDOT = 18412
981952 ZDOT = 5612
276899
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 20235
45659778
00016717 00000-0 10270-3 0 9112
2 25544 51
6415 20
5095 0001463 45
6958 314
4312 15
49176374 2283
Satellite: ISS
Catalog Number: 25544
Epoch time: 20235
45659778 = yrday
fracday
Element set: 911
Inclination: 51
6415 deg
RA of node: 20
5095 deg
Eccentricity:
0001463
Arg of perigee: 45
6958 deg
Mean anomaly: 314
4312 deg
Mean motion: 15
49176374 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 228
Checksum: 309
Coasting Arc #13 (Orbit 242)
---------------------------------------
Vector Time (GMT): 2020/236/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 928399
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5707077
73 A = 6802039
31 meter
Y = -3146603
12 meter E =
0006956
Z = -1944173
73 I = 51
76040
XDOT = 3846
664517 Wp = 125
77407
YDOT = -3526
312771 meter/sec RA = 15
27327 deg
ZDOT = -5602
573394 TA = 75
57008
MA = 75
49290
Ha = 229
230 n
mi
Hp = 221
942
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18724008
29 X = -5662023
68
Y = -10323501
04 feet Y = -3210171
89 meter
Z = -6378522
74 Z = -1971786
79
XDOT = 12620
290411 XDOT = 3913
024852
YDOT = -11569
267621 feet/sec YDOT = -3482
925747 meter/sec
ZDOT = -18381
146306 ZDOT = -5583
726628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1932174
50 X = -588926
79
Y = 21255354
18 feet Y = 6478631
95 meter
Z = -6505792
24 Z = -1982965
48
XDOT = -14171
592028 XDOT = -4319
501250
YDOT = -6869
849770 feet/sec YDOT = -2093
930210 meter/sec
ZDOT = -18293
941862 ZDOT = -5575
993480
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 20236
42421585
00016717 00000-0 10270-3 0 9124
2 25544 51
6412 15
7222 0001653 48
9219 311
2074 15
49197688 2433
Satellite: ISS
Catalog Number: 25544
Epoch time: 20236
42421585 = yrday
fracday
Element set: 912
Inclination: 51
6412 deg
RA of node: 15
7222 deg
Eccentricity:
0001653
Arg of perigee: 48
9219 deg
Mean anomaly: 311
2074 deg
Mean motion: 15
49197688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 243
Checksum: 291
Coasting Arc #14 (Orbit 258)
---------------------------------------
Vector Time (GMT): 2020/237/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 928399
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5923414
22 A = 6802042
27 meter
Y = 2672038
98 meter E =
0015336
Z = 1985257
13 I = 51
72668
XDOT = -3603
263464 Wp = 67
13232
YDOT = 3819
561941 meter/sec RA = 10
33178 deg
ZDOT = 5581
605467 TA = 314
71719
MA = 314
84196
Ha = 229
239 n
mi
Hp = 221
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19433773
70 X = 5883451
23
Y = 8766532
08 feet Y = 2738055
41 meter
Z = 6513310
79 Z = 2013933
56
XDOT = -11821
730525 XDOT = -3672
819308
YDOT = 12531
371197 feet/sec YDOT = 3778
878830 meter/sec
ZDOT = 18312
353894 ZDOT = 5563
933295
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -144437
26 X = -44024
48
Y = -21278235
03 feet Y = -6485606
04 meter
Z = 6645503
32 Z = 2025549
41
XDOT = 14828
005895 XDOT = 4519
576197
YDOT = 5621
689391 feet/sec YDOT = 1713
490926 meter/sec
ZDOT = 18230
557235 ZDOT = 5556
673845
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 20237
45634175
00016717 00000-0 10270-3 0 9130
2 25544 51
6406 10
6151 0001462 58
3153 301
8139 15
49174851 2592
Satellite: ISS
Catalog Number: 25544
Epoch time: 20237
45634175 = yrday
fracday
Element set: 913
Inclination: 51
6406 deg
RA of node: 10
6151 deg
Eccentricity:
0001462
Arg of perigee: 58
3153 deg
Mean anomaly: 301
8139 deg
Mean motion: 15
49174851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 259
Checksum: 286
Coasting Arc #15 (Orbit 273)
---------------------------------------
Vector Time (GMT): 2020/238/09:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 928399
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6089701
76 A = 6801793
78 meter
Y = -2213473
13 meter E =
0006839
Z = -2065832
32 I = 51
69415
XDOT = 3356
949598 Wp = 124
40992
YDOT = -4079
844051 meter/sec RA = 5
38830 deg
ZDOT = -5541
143118 TA = 78
36412
MA = 78
28736
Ha = 229
243 n
mi
Hp = 221
873
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19979336
50 X = -6054462
85
Y = -7262050
94 feet Y = -2281375
48 meter
Z = -6777665
08 Z = -2095328
04
XDOT = 11013
614168 XDOT = 3429
237762
YDOT = -13385
315127 feet/sec YDOT = -4041
900002 meter/sec
ZDOT = -18179
603404 ZDOT = -5524
660884
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2101855
14 X = 640645
45
Y = 21109987
87 feet Y = 6434324
30 meter
Z = -6913655
46 Z = -2107282
18
XDOT = -15352
907774 XDOT = -4679
566289
YDOT = -4382
517370 feet/sec YDOT = -1335
791294 meter/sec
ZDOT = -18103
285211 ZDOT = -5517
881332
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 20238
42395688
00016717 00000-0 10270-3 0 9142
2 25544 51
6420 5
8274 0001634 56
8302 303
3005 15
49208435 2742
Satellite: ISS
Catalog Number: 25544
Epoch time: 20238
42395688 = yrday
fracday
Element set: 914
Inclination: 51
6420 deg
RA of node: 5
8274 deg
Eccentricity:
0001634
Arg of perigee: 56
8302 deg
Mean anomaly: 303
3005 deg
Mean motion: 15
49208435 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 274
Checksum: 288
Coasting Arc #16 (Orbit 280)
---------------------------------------
Vector Time (GMT): 2020/238/20:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 928399
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4105587
38 A = 6796466
75 meter
Y = -3504278
12 meter E =
0009425
Z = -4139984
40 I = 51
66117
XDOT = 6090
550816 Wp = 67
82110
YDOT = -2665
494761 meter/sec RA = 3
14012 deg
ZDOT = -3787
201236 TA = 163
06643
MA = 163
03495
Ha = 229
375 n
mi
Hp = 221
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13469774
88 X = -4045986
76
Y = -11496975
44 feet Y = -3549856
41 meter
Z = -13582625
99 Z = -4159782
96
XDOT = 19982
122100 XDOT = 6138
300502
YDOT = -8745
061552 feet/sec YDOT = -2597
118812 meter/sec
ZDOT = -12425
200905 ZDOT = -3757
499912
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8859382
04 X = 2700339
65
Y = -15252609
46 feet Y = -4648995
36 meter
Z = -13673780
13 Z = -4167768
18
XDOT = 11153
351529 XDOT = 3399
541546
YDOT = 17484
274118 feet/sec YDOT = 5329
206751 meter/sec
ZDOT = -12287
964956 ZDOT = -3745
371718
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 20238
87551000
00016717 00000-0 10270-3 0 9154
2 25544 51
6424 3
5966 0001782 58
6086 301
5239 15
49172892 2816
Satellite: ISS
Catalog Number: 25544
Epoch time: 20238
87551000 = yrday
fracday
Element set: 915
Inclination: 51
6424 deg
RA of node: 3
5966 deg
Eccentricity:
0001782
Arg of perigee: 58
6086 deg
Mean anomaly: 301
5239 deg
Mean motion: 15
49172892 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 281
Checksum: 304
Coasting Arc #17 (Orbit 296)
---------------------------------------
Vector Time (GMT): 2020/239/20:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 928399
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4329105
01 A = 6796293
17 meter
Y = 3164539
04 meter E =
0011389
Z = 4166753
32 I = 51
62599
XDOT = -5906
098667 Wp = 98
11148
YDOT = 3146
369682 meter/sec RA = 358
19332 deg
ZDOT = 3736
307430 TA = 313
39171
MA = 313
48649
Ha = 229
224 n
mi
Hp = 221
909
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14203100
41 X = 4273156
87
Y = 10382345
94 feet Y = 3212637
23 meter
Z = 13670450
53 Z = 4187646
49
XDOT = -19376
964131 XDOT = -5958
992083
YDOT = 10322
735176 feet/sec YDOT = 3080
027597 meter/sec
ZDOT = 12258
226475 ZDOT = 3707
489744
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7357244
38 X = -2242488
09
Y = 15898179
09 feet Y = 4845764
99 meter
Z = 13766671
47 Z = 4196081
46
XDOT = -12841
198054 XDOT = -3913
997167
YDOT = -16471
107811 feet/sec YDOT = -5020
393661 meter/sec
ZDOT = 12125
044822 ZDOT = 3695
713662
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 20239
90763003
00016717 00000-0 10270-3 0 9168
2 25544 51
6414 358
4903 0001692 56
4205 303
7107 15
49190309 2975
Satellite: ISS
Catalog Number: 25544
Epoch time: 20239
90763003 = yrday
fracday
Element set: 916
Inclination: 51
6414 deg
RA of node: 358
4903 deg
Eccentricity:
0001692
Arg of perigee: 56
4205 deg
Mean anomaly: 303
7107 deg
Mean motion: 15
49190309 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 297
Checksum: 297
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