[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 30th 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19912 1579 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 884 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
130/00:47:30
000 0
0 0
0 0
0
N/A 0
0 0
0 228
1
000/00:00:00
000 0
0 0
0 222
7
132/16:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
0
000/00:00:00
000 0
0 0
0 222
6
132/22:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
1
000/00:00:00
000 0
0 0
0 222
8
Coasting Arc #1 (Orbit 2445)
---------------------------------------
Vector Time (GMT): 2020/120/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2863180
87 A = 6791415
79 meter
Y = 3160286
12 meter E =
0013816
Z = -5297621
18 I = 51
32936
XDOT = -5314
669120 Wp = 92
79248
YDOT = -5488
408528 meter/sec RA = 228
34256 deg
ZDOT = -403
279869 TA = 173
34543
MA = 173
32707
Ha = 228
299 n
mi
Hp = 222
414
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9393638
02 X = -2872574
38
Y = 10368392
78 feet Y = 3128215
83 meter
Z = -17380646
92 Z = -5311552
07
XDOT = -17436
578478 XDOT = -5250
942201
YDOT = -18006
589659 feet/sec YDOT = -5547
484592 meter/sec
ZDOT = -1323
096683 ZDOT = -428
942173
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1166946
10 X = -355685
17
Y = 13861931
86 feet Y = 4225116
83 meter
Z = -17444654
58 Z = -5317130
72
XDOT = -23744
198101 XDOT = -7237
231581
YDOT = -3805
336281 feet/sec YDOT = -1159
866498 meter/sec
ZDOT = -1440
607574 ZDOT = -439
097189
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 20120
51689854
00016717 00000-0 10270-3 0 9008
2 25544 51
6426 229
3601 0001726 211
7181 148
3866 15
49334338 24461
Satellite: ISS
Catalog Number: 25544
Epoch time: 20120
51689854 = yrday
fracday
Element set: 900
Inclination: 51
6426 deg
RA of node: 229
3601 deg
Eccentricity:
0001726
Arg of perigee: 211
7181 deg
Mean anomaly: 148
3866 deg
Mean motion: 15
49334338 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2446
Checksum: 303
Coasting Arc #2 (Orbit 2461)
---------------------------------------
Vector Time (GMT): 2020/121/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2685973
23 A = 6791262
67 meter
Y = -3290420
13 meter E =
0002430
Z = 5297908
27 I = 51
35301
XDOT = 5712
001726 Wp = 144
75311
YDOT = 5099
897449 meter/sec RA = 223
37250 deg
ZDOT = 269
516937 TA = 302
65381
MA = 302
67725
Ha = 228
084 n
mi
Hp = 222
538
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8812248
13 X = 2696833
79
Y = -10795341
64 feet Y = -3260323
25 meter
Z = 17381588
82 Z = 5310981
90
XDOT = 18740
163142 XDOT = 5653
239473
YDOT = 16731
947012 feet/sec YDOT = 5163
444540 meter/sec
ZDOT = 884
241920 ZDOT = 297
121236
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 207328
15 X = 63193
62
Y = -13858568
02 feet Y = -4224091
53 meter
Z = 17441670
10 Z = 5316221
05
XDOT = 24052
783276 XDOT = 7331
288343
YDOT = 1640
120506 feet/sec YDOT = 499
908730 meter/sec
ZDOT = 1010
701101 ZDOT = 308
061696
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 20121
54891821
00016717 00000-0 10270-3 0 9012
2 25544 51
6431 224
2519 0001723 218
1696 141
9333 15
49372023 24627
Satellite: ISS
Catalog Number: 25544
Epoch time: 20121
54891821 = yrday
fracday
Element set: 901
Inclination: 51
6431 deg
RA of node: 224
2519 deg
Eccentricity:
0001723
Arg of perigee: 218
1696 deg
Mean anomaly: 141
9333 deg
Mean motion: 15
49372023 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2462
Checksum: 283
Coasting Arc #3 (Orbit 2476)
---------------------------------------
Vector Time (GMT): 2020/122/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2522441
55 A = 6791346
27 meter
Y = 3415955
02 meter E =
0013765
Z = -5312016
02 I = 51
37807
XDOT = -6057
658431 Wp = 93
72043
YDOT = -4671
181206 meter/sec RA = 218
40555 deg
ZDOT = -128
508325 TA = 175
05445
MA = 175
04084
Ha = 228
198 n
mi
Hp = 222
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8275726
86 X = -2534649
54
Y = 11207201
49 feet Y = 3387679
24 meter
Z = -17427874
09 Z = -5324298
58
XDOT = -19874
207452 XDOT = -6004
349462
YDOT = -15325
397656 feet/sec YDOT = -4738
624178 meter/sec
ZDOT = -421
615240 ZDOT = -157
804800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 707482
04 X = 215640
53
Y = 13842596
38 feet Y = 4219223
38 meter
Z = -17484330
42 Z = -5329223
91
XDOT = -24078
001222 XDOT = -7338
974772
YDOT = 533
291979 feet/sec YDOT = 162
547395 meter/sec
ZDOT = -555
878193 ZDOT = -169
431673
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 20122
51643515
00016717 00000-0 10270-3 0 9026
2 25544 51
6430 219
4646 0001567 223
3538 136
7489 15
49339550 24770
Satellite: ISS
Catalog Number: 25544
Epoch time: 20122
51643515 = yrday
fracday
Element set: 902
Inclination: 51
6430 deg
RA of node: 219
4646 deg
Eccentricity:
0001567
Arg of perigee: 223
3538 deg
Mean anomaly: 136
7489 deg
Mean motion: 15
49339550 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2477
Checksum: 310
Coasting Arc #4 (Orbit 2492)
---------------------------------------
Vector Time (GMT): 2020/123/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2342700
13 A = 6791216
20 meter
Y = -3529124
42 meter E =
0001694
Z = 5307195
66 I = 51
40513
XDOT = 6389
529525 Wp = 133
60520
YDOT = 4228
687326 meter/sec RA = 213
43955 deg
ZDOT = -9
657616 TA = 316
48052
MA = 316
49388
Ha = 228
018 n
mi
Hp = 222
578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7686024
05 X = 2356210
37
Y = -11578492
20 feet Y = -3502851
26 meter
Z = 17412059
25 Z = 5318608
33
XDOT = 20963
023376 XDOT = 6341
815119
YDOT = 13873
646084 feet/sec YDOT = 4299
872805 meter/sec
ZDOT = -31
685093 ZDOT = 21
264475
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1635862
87 X = -498611
00
Y = -13734281
97 feet Y = -4186209
14 meter
Z = 17464527
08 Z = 5323187
85
XDOT = 23976
557537 XDOT = 7308
054737
YDOT = -2711
073504 feet/sec YDOT = -826
335204 meter/sec
ZDOT = 110
075040 ZDOT = 33
550872
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 20123
54844898
00016717 00000-0 10270-3 0 9038
2 25544 51
6430 214
3571 0001606 227
4151 132
6863 15
49377219 24934
Satellite: ISS
Catalog Number: 25544
Epoch time: 20123
54844898 = yrday
fracday
Element set: 903
Inclination: 51
6430 deg
RA of node: 214
3571 deg
Eccentricity:
0001606
Arg of perigee: 227
4151 deg
Mean anomaly: 132
6863 deg
Mean motion: 15
49377219 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2493
Checksum: 306
Coasting Arc #5 (Orbit 2507)
---------------------------------------
Vector Time (GMT): 2020/124/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2172868
40 A = 6791343
74 meter
Y = 3643005
21 meter E =
0013620
Z = -5315537
35 I = 51
43340
XDOT = -6665
269973 Wp = 95
35178
YDOT = -3752
911489 meter/sec RA = 208
47619 deg
ZDOT = 151
642168 TA = 176
10613
MA = 176
09552
Ha = 228
119 n
mi
Hp = 222
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7128833
34 X = -2187624
11
Y = 11952116
84 feet Y = 3618624
18 meter
Z = -17439427
01 Z = -5326128
16
XDOT = -21867
683638 XDOT = -6623
545022
YDOT = -12312
701735 feet/sec YDOT = -3827
213984 meter/sec
ZDOT = 497
513673 ZDOT = 119
366062
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2537714
69 X = 773495
44
Y = 13621028
95 feet Y = 4151689
63 meter
Z = -17488125
98 Z = -5330380
80
XDOT = -23595
086876 XDOT = -7191
782480
YDOT = 4848
506420 feet/sec YDOT = 1477
824757 meter/sec
ZDOT = 349
504497 ZDOT = 106
528971
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 20124
51596176
00016717 00000-0 10270-3 0 9040
2 25544 51
6426 209
5696 0001578 232
9055 127
1951 15
49338516 25086
Satellite: ISS
Catalog Number: 25544
Epoch time: 20124
51596176 = yrday
fracday
Element set: 904
Inclination: 51
6426 deg
RA of node: 209
5696 deg
Eccentricity:
0001578
Arg of perigee: 232
9055 deg
Mean anomaly: 127
1951 deg
Mean motion: 15
49338516 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2508
Checksum: 320
Coasting Arc #6 (Orbit 2523)
---------------------------------------
Vector Time (GMT): 2020/125/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1990607
77 A = 6791221
29 meter
Y = -3741888
60 meter E =
0001149
Z = 5305297
12 I = 51
46465
XDOT = 6924
072521 Wp = 107
29080
YDOT = 3267
662694 meter/sec RA = 203
51406 deg
ZDOT = -293
551454 TA = 345
51497
MA = 345
51826
Ha = 227
939 n
mi
Hp = 222
637
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6530865
40 X = 2006532
40
Y = -12276537
41 feet Y = -3719539
16 meter
Z = 17405830
43 Z = 5315005
48
XDOT = 22716
773364 XDOT = 6888
443855
YDOT = 10720
678130 feet/sec YDOT = 3344
893390 meter/sec
ZDOT = -963
095322 ZDOT = -260
003244
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3433102
15 X = -1046409
54
Y = -13417263
95 feet Y = -4089582
05 meter
Z = 17450482
64 Z = 5318907
11
XDOT = 23089
802114 XDOT = 7037
771684
YDOT = -6959
299778 feet/sec YDOT = -2121
194572 meter/sec
ZDOT = -809
215640 ZDOT = -246
648927
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 20125
54797002
00016717 00000-0 10270-3 0 9056
2 25544 51
6436 204
4620 0001585 238
7615 121
3380 15
49382172 25249
Satellite: ISS
Catalog Number: 25544
Epoch time: 20125
54797002 = yrday
fracday
Element set: 905
Inclination: 51
6436 deg
RA of node: 204
4620 deg
Eccentricity:
0001585
Arg of perigee: 238
7615 deg
Mean anomaly: 121
3380 deg
Mean motion: 15
49382172 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2524
Checksum: 289
Coasting Arc #7 (Orbit 2538)
---------------------------------------
Vector Time (GMT): 2020/126/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1814599
51 A = 6791382
76 meter
Y = 3845025
82 meter E =
0013502
Z = -5307582
74 I = 51
49508
XDOT = -7123
074181 Wp = 96
26058
YDOT = -2757
671181 meter/sec RA = 198
55463 deg
ZDOT = 437
047786 TA = 177
92842
MA = 177
92282
Ha = 228
075 n
mi
Hp = 222
604
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5953410
48 X = -1831679
29
Y = 12614914
11 feet Y = 3824638
21 meter
Z = -17413329
21 Z = -5316438
95
XDOT = -23369
665948 XDOT = -7093
830640
YDOT = -9047
477629 feet/sec YDOT = -2837
162959 meter/sec
ZDOT = 1433
883811 ZDOT = 402
517187
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4316718
36 X = 1315735
75
Y = 13210767
87 feet Y = 4026642
05 meter
Z = -17454075
27 Z = -5320002
14
XDOT = -22318
328649 XDOT = -6802
626572
YDOT = 8979
898609 feet/sec YDOT = 2737
073096 meter/sec
ZDOT = 1275
464130 ZDOT = 388
761467
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 20126
51547730
00016717 00000-0 10270-3 0 9066
2 25544 51
6427 199
6744 0001429 245
8577 114
2424 15
49340988 25399
Satellite: ISS
Catalog Number: 25544
Epoch time: 20126
51547730 = yrday
fracday
Element set: 906
Inclination: 51
6427 deg
RA of node: 199
6744 deg
Eccentricity:
0001429
Arg of perigee: 245
8577 deg
Mean anomaly: 114
2424 deg
Mean motion: 15
49340988 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2539
Checksum: 329
Coasting Arc #8 (Orbit 2554)
---------------------------------------
Vector Time (GMT): 2020/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1628945
25 A = 6791296
07 meter
Y = -3931960
16 meter E =
0001344
Z = 5291213
85 I = 51
52723
XDOT = 7303
514578 Wp = 67
96315
YDOT = 2242
135359 meter/sec RA = 193
59749 deg
ZDOT = -581
681061 TA = 27
60506
MA = 27
59793
Ha = 227
934 n
mi
Hp = 222
640
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5344308
55 X = 1647090
35
Y = -12900131
76 feet Y = -3913642
81 meter
Z = 17359625
50 Z = 5299170
75
XDOT = 23961
662002 XDOT = 7280
725068
YDOT = 7356
087137 feet/sec YDOT = 2323
681049 meter/sec
ZDOT = -1908
402432 ZDOT = -546
258075
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5179692
00 X = -1578770
12
Y = -12917928
95 feet Y = -3937384
74 meter
Z = 17396250
54 Z = 5302377
17
XDOT = 21432
267146 XDOT = 6532
555026
YDOT = -10947
477885 feet/sec YDOT = -3336
791259 meter/sec
ZDOT = -1745
854853 ZDOT = -532
136559
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 20127
54748159
00016717 00000-0 10270-3 0 9079
2 25544 51
6424 194
5675 0001460 248
4593 111
6402 15
49381954 25558
Satellite: ISS
Catalog Number: 25544
Epoch time: 20127
54748159 = yrday
fracday
Element set: 907
Inclination: 51
6424 deg
RA of node: 194
5675 deg
Eccentricity:
0001460
Arg of perigee: 248
4593 deg
Mean anomaly: 111
6402 deg
Mean motion: 15
49381954 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2555
Checksum: 321
Coasting Arc #9 (Orbit 2569)
---------------------------------------
Vector Time (GMT): 2020/128/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1443696
67 A = 6791483
54 meter
Y = 4025673
17 meter E =
0013316
Z = -5287423
40 I = 51
55917
XDOT = -7422
053094 Wp = 97
91262
YDOT = -1709
770296 meter/sec RA = 188
64201 deg
ZDOT = 724
558303 TA = 179
03332
MA = 179
03075
Ha = 228
055 n
mi
Hp = 222
632
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4736537
63 X = -1462921
84
Y = 13207589
13 feet Y = 4009421
52 meter
Z = -17347189
62 Z = -5294482
92
XDOT = -24350
567893 XDOT = -7405
901872
YDOT = -5609
482597 feet/sec YDOT = -1792
678708 meter/sec
ZDOT = 2377
159787 ZDOT = 688
543276
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6048630
58 X = 1843622
60
Y = 12615868
30 feet Y = 3845316
66 meter
Z = -17379704
32 Z = -5297333
88
XDOT = -20301
260080 XDOT = -6187
824072
YDOT = 12781
433547 feet/sec YDOT = 3895
780945 meter/sec
ZDOT = 2211
859360 ZDOT = 674
174733
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 20128
51498610
00016717 00000-0 10270-3 0 9082
2 25544 51
6412 189
7793 0001390 253
6313 106
4684 15
49341002 25703
Satellite: ISS
Catalog Number: 25544
Epoch time: 20128
51498610 = yrday
fracday
Element set: 908
Inclination: 51
6412 deg
RA of node: 189
7793 deg
Eccentricity:
0001390
Arg of perigee: 253
6313 deg
Mean anomaly: 106
4684 deg
Mean motion: 15
49341002 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2570
Checksum: 299
Coasting Arc #10 (Orbit 2585)
---------------------------------------
Vector Time (GMT): 2020/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1253599
70 A = 6791415
53 meter
Y = -4101601
30 meter E =
0002016
Z = 5264668
14 I = 51
59310
XDOT = 7520
660057 Wp = 48
33950
YDOT = 1177
511801 meter/sec RA = 183
68877 deg
ZDOT = -871
883652 TA = 50
01902
MA = 50
00133
Ha = 227
932 n
mi
Hp = 222
635
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4112859
90 X = 1273798
63
Y = -13456697
17 feet Y = -4087470
17 meter
Z = 17272533
28 Z = 5270806
46
XDOT = 24674
081552 XDOT = 7511
169008
YDOT = 3863
227693 feet/sec YDOT = 1261
560180 meter/sec
ZDOT = -2860
510668 ZDOT = -835
373495
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6877416
77 X = -2096236
63
Y = -12236061
58 feet Y = -3729551
57 meter
Z = 17300828
21 Z = 5273292
44
XDOT = 19072
346548 XDOT = 5813
251228
YDOT = -14534
442073 feet/sec YDOT = -4430
097944 meter/sec
ZDOT = -2692
897818 ZDOT = -820
795255
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 20129
54698550
00016717 00000-0 10270-3 0 9092
2 25544 51
6415 184
6718 0001379 259
9565 100
1430 15
49385552 25867
Satellite: ISS
Catalog Number: 25544
Epoch time: 20129
54698550 = yrday
fracday
Element set: 909
Inclination: 51
6415 deg
RA of node: 184
6718 deg
Eccentricity:
0001379
Arg of perigee: 259
9565 deg
Mean anomaly: 100
1430 deg
Mean motion: 15
49385552 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2586
Checksum: 333
Coasting Arc #11 (Orbit 2593)
---------------------------------------
Vector Time (GMT): 2020/130/00:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6598833
10 A = 6802702
30 meter
Y = 1089098
36 meter E =
0008386
Z = -1220534
31 I = 51
64853
XDOT = -1835
212560 Wp = 149
74452
YDOT = 4593
463963 meter/sec RA = 181
06983 deg
ZDOT = -5847
898512 TA = 43
48934
MA = 43
42323
Ha = 228
062 n
mi
Hp = 222
740
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21649714
90 X = 6592092
79
Y = 3573157
36 feet Y = 1162853
65 meter
Z = -4004377
66 Z = -1188495
49
XDOT = -6021
038584 XDOT = -1858
035421
YDOT = 15070
419825 feet/sec YDOT = 4572
814287 meter/sec
ZDOT = -19186
018740 ZDOT = -5856
868377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14437090
12 X = -4400425
07
Y = 16559120
28 feet Y = 5047219
86 meter
Z = -3857280
61 Z = -1175699
13
XDOT = -8513
079796 XDOT = -2594
786722
YDOT = -11881
430992 feet/sec YDOT = -3621
460166 meter/sec
ZDOT = -19227
333945 ZDOT = -5860
491386
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 20130
06298574
00016717 00000-0 10270-3 0 9105
2 25544 51
6419 182
1194 0001408 272
3386 87
7603 15
49339007 25940
Satellite: ISS
Catalog Number: 25544
Epoch time: 20130
06298574 = yrday
fracday
Element set: 910
Inclination: 51
6419 deg
RA of node: 182
1194 deg
Eccentricity:
0001408
Arg of perigee: 272
3386 deg
Mean anomaly: 87
7603 deg
Mean motion: 15
49339007 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2594
Checksum: 309
Coasting Arc #12 (Orbit 2609)
---------------------------------------
Vector Time (GMT): 2020/131/00:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6636234
54 A = 6802433
37 meter
Y = -606246
54 meter E =
0012690
Z = 1333344
84 I = 51
68015
XDOT = 1606
808525 Wp = 55
86173
YDOT = -4718
474985 meter/sec RA = 176
12130 deg
ZDOT = 5819
167959 TA = 318
62005
MA = 318
71611
Ha = 227
979 n
mi
Hp = 222
660
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21772423
04 X = -6635438
80
Y = -1988997
83 feet Y = -680453
34 meter
Z = 4374490
95 Z = 1301110
08
XDOT = 5271
681513 XDOT = 1631
185967
YDOT = -15480
560976 feet/sec YDOT = -4700
370895 meter/sec
ZDOT = 19091
758397 ZDOT = 5827
031951
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12852494
60 X = 3917440
36
Y = -17722334
77 feet Y = -5401767
64 meter
Z = 4226454
89 Z = 1288223
45
XDOT = 9384
502142 XDOT = 2860
396253
YDOT = 11393
966080 feet/sec YDOT = 3472
880861 meter/sec
ZDOT = 19128
008382 ZDOT = 5830
216955
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 20131
09498159
00016717 00000-0 10270-3 0 9111
2 25544 51
6403 177
0109 0001369 277
8999 82
1996 15
49392980 26100
Satellite: ISS
Catalog Number: 25544
Epoch time: 20131
09498159 = yrday
fracday
Element set: 911
Inclination: 51
6403 deg
RA of node: 177
0109 deg
Eccentricity:
0001369
Arg of perigee: 277
8999 deg
Mean anomaly: 82
1996 deg
Mean motion: 15
49392980 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2610
Checksum: 335
Coasting Arc #13 (Orbit 2624)
---------------------------------------
Vector Time (GMT): 2020/132/00:47:30
000
Vector Time (MET): N/A
Weight (LBS) : 936290
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6635150
26 A = 6802379
41 meter
Y = 148665
56 meter E =
0007465
Z = -1475419
45 I = 51
71266
XDOT = -1388
899089 Wp = 150
25661
YDOT = 4831
428362 meter/sec RA = 171
17644 deg
ZDOT = -5778
110463 TA = 45
79345
MA = 45
73215
Ha = 228
036 n
mi
Hp = 222
735
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21768865
69 X = 6640161
49
Y = 487747
91 feet Y = 222892
73 meter
Z = -4840614
99 Z = -1443176
07
XDOT = -4556
755541 XDOT = -1414
755383
YDOT = 15851
142919 feet/sec YDOT = 4815
752842 meter/sec
ZDOT = -18957
055326 ZDOT = -5784
919445
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11242179
45 X = -3426616
30
Y = 18685470
64 feet Y = 5695331
45 meter
Z = -4692499
66 Z = -1430273
90
XDOT = -10200
864682 XDOT = -3109
223555
YDOT = -10889
935813 feet/sec YDOT = -3319
252436 meter/sec
ZDOT = -18988
470934 ZDOT = -5787
685941
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 20132
06247941
00016717 00000-0 10270-3 0 9121
2 25544 51
6399 172
2229 0001452 280
4617 79
6369 15
49353685 26254
Satellite: ISS
Catalog Number: 25544
Epoch time: 20132
06247941 = yrday
fracday
Element set: 912
Inclination: 51
6399 deg
RA of node: 172
2229 deg
Eccentricity:
0001452
Arg of perigee: 280
4617 deg
Mean anomaly: 79
6369 deg
Mean motion: 15
49353685 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2625
Checksum: 319
Coasting Arc #14 (Orbit 2634)
---------------------------------------
Vector Time (GMT): 2020/132/16:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3880241
44 A = 6796644
41 meter
Y = -3977488
80 meter E =
0009966
Z = 3907044
05 I = 51
71332
XDOT = 6167
366971 Wp = 77
75402
YDOT = 1989
313728 meter/sec RA = 168
00370 deg
ZDOT = -4088
991217 TA = 55
12569
MA = 55
03204
Ha = 227
971 n
mi
Hp = 222
570
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12730450
90 X = 3905452
25
Y = -13049503
95 feet Y = -3933956
69 meter
Z = 12818386
00 Z = 3925953
58
XDOT = 20234
143606 XDOT = 6164
525562
YDOT = 6526
619841 feet/sec YDOT = 2058
266214 meter/sec
ZDOT = -13415
325514 ZDOT = -4059
039101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16453651
48 X = -5015072
97
Y = -7706723
13 feet Y = -2349009
21 meter
Z = 12905375
80 Z = 3933558
54
XDOT = -1007
711591 XDOT = -307
150493
YDOT = -20142
401236 feet/sec YDOT = -6139
403897 meter/sec
ZDOT = -13277
772598 ZDOT = -4047
065088
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 20132
70747684
00016717 00000-0 10270-3 0 9132
2 25544 51
6382 169
0298 0001251 286
1320 73
9693 15
49379385 26350
Satellite: ISS
Catalog Number: 25544
Epoch time: 20132
70747684 = yrday
fracday
Element set: 913
Inclination: 51
6382 deg
RA of node: 169
0298 deg
Eccentricity:
0001251
Arg of perigee: 286
1320 deg
Mean anomaly: 73
9693 deg
Mean motion: 15
49379385 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2635
Checksum: 326
Coasting Arc #15 (Orbit 2638)
---------------------------------------
Vector Time (GMT): 2020/132/22:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6422565
80 A = 6801273
76 meter
Y = 277640
95 meter E =
0005102
Z = -2214746
72 I = 51
74131
XDOT = -2096
670819 Wp = 147
60214
YDOT = 4929
269464 meter/sec RA = 166
71105 deg
ZDOT = -5472
268329 TA = 56
90598
MA = 56
85701
Ha = 228
052 n
mi
Hp = 222
769
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21071410
10 X = 6429741
80
Y = 910895
51 feet Y = 349503
03 meter
Z = -7266229
41 Z = -2183530
86
XDOT = -6878
841271 XDOT = -2125
054318
YDOT = 16172
143912 feet/sec YDOT = 4905
664937 meter/sec
ZDOT = -17953
636251 ZDOT = -5482
521529
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19267694
89 X = -5872793
40
Y = 8697906
92 feet Y = 2651122
03 meter
Z = -7122814
98 Z = -2171034
00
XDOT = -615
159928 XDOT = -187
500746
YDOT = -16076
305000 feet/sec YDOT = -4900
057764 meter/sec
ZDOT = -18000
885697 ZDOT = -5486
669960
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 20132
96547544
00016717 00000-0 10270-3 0 9144
2 25544 51
6425 167
7548 0001454 282
7243 77
3744 15
49347322 26397
Satellite: ISS
Catalog Number: 25544
Epoch time: 20132
96547544 = yrday
fracday
Element set: 914
Inclination: 51
6425 deg
RA of node: 167
7548 deg
Eccentricity:
0001454
Arg of perigee: 282
7243 deg
Mean anomaly: 77
3744 deg
Mean motion: 15
49347322 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2639
Checksum: 325
Coasting Arc #16 (Orbit 2654)
---------------------------------------
Vector Time (GMT): 2020/133/22:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6382879
13 A = 6800990
99 meter
Y = 176468
73 meter E =
0012801
Z = 2322375
60 I = 51
77306
XDOT = 1837
295632 Wp = 67
98405
YDOT = -5098
255596 meter/sec RA = 161
76870 deg
ZDOT = 5417
813211 TA = 317
80767
MA = 317
90612
Ha = 228
083 n
mi
Hp = 222
670
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20941204
49 X = -6395658
84
Y = 578965
66 feet Y = 105019
14 meter
Z = 7619342
52 Z = 2291339
04
XDOT = 6027
872807 XDOT = 1867
852649
YDOT = -16726
560354 feet/sec YDOT = -5077
539353 meter/sec
ZDOT = 17774
977728 ZDOT = 5426
811767
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18308425
58 X = 5580408
12
Y = -10287074
85 feet Y = -3135500
41 meter
Z = 7476715
24 Z = 2278902
80
XDOT = 1809
952878 XDOT = 551
673637
YDOT = 16217
193224 feet/sec YDOT = 4943
000495 meter/sec
ZDOT = 17816
475693 ZDOT = 5430
461791
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 20133
99746657
00016717 00000-0 10270-3 0 9155
2 25544 51
6424 162
6462 0001470 296
8297 63
2703 15
49376766 26559
Satellite: ISS
Catalog Number: 25544
Epoch time: 20133
99746657 = yrday
fracday
Element set: 915
Inclination: 51
6424 deg
RA of node: 162
6462 deg
Eccentricity:
0001470
Arg of perigee: 296
8297 deg
Mean anomaly: 63
2703 deg
Mean motion: 15
49376766 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2655
Checksum: 338
Coasting Arc #17 (Orbit 2669)
---------------------------------------
Vector Time (GMT): 2020/134/22:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 921014
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6312045
48 A = 6800786
83 meter
Y = -598815
28 meter E =
0004175
Z = -2456729
96 I = 51
80283
XDOT = -1579
046240 Wp = 139
69579
YDOT = 5250
463902 meter/sec RA = 156
82968 deg
ZDOT = -5344
979954 TA = 67
67417
MA = 67
62993
Ha = 228
082 n
mi
Hp = 222
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20708810
62 X = 6330205
86
Y = -1964617
07 feet Y = -528127
74 meter
Z = -8060137
65 Z = -2426024
48
XDOT = -5180
597900 XDOT = -1611
678301
YDOT = 17225
931436 feet/sec YDOT = 5232
623891 meter/sec
ZDOT = -17536
023472 ZDOT = -5352
729135
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17261443
99 X = -5261288
13
Y = 11705229
39 feet Y = 3567753
92 meter
Z = -7918998
20 Z = -2413710
65
XDOT = -2989
666137 XDOT = -911
250239
YDOT = -16278
242031 feet/sec YDOT = -4961
608171 meter/sec
ZDOT = -17571
791572 ZDOT = -5355
882071
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 20134
96495748
00016717 00000-0 10270-3 0 9166
2 25544 51
6415 157
8580 0001466 294
9197 65
1801 15
49353626 26706
Satellite: ISS
Catalog Number: 25544
Epoch time: 20134
96495748 = yrday
fracday
Element set: 916
Inclination: 51
6415 deg
RA of node: 157
8580 deg
Eccentricity:
0001466
Arg of perigee: 294
9197 deg
Mean anomaly: 65
1801 deg
Mean motion: 15
49353626 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2670
Checksum: 336
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