[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 29th 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16464 4774 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 453 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
211/13:59:48
126 -1
5 2
1 2
1
N/A 0
0 -0
2 228
7
000/00:05:36
252 1
5 -0
1 222
7
212/08:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
9
000/00:00:00
000 0
0 0
0 222
7
214/23:32:45
000 0
0 0
0 0
0
N/A 0
0 0
0 228
8
000/00:00:00
000 0
0 0
0 222
8
219/03:44:00
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
5
223/13:07:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
0
000/00:00:00
000 0
0 0
0 222
5
Coasting Arc #1 (Orbit 3825)
---------------------------------------
Vector Time (GMT): 2020/209/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 984330
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5705099
90 A = 6797126
91 meter
Y = -160666
95 meter E =
0006076
Z = -3696918
43 I = 51
84705
XDOT = -2654
594515 Wp = 87
92750
YDOT = 5711
007022 meter/sec RA = 147
79862 deg
ZDOT = -4350
745790 TA = 135
81002
MA = 135
76147
Ha = 228
541 n
mi
Hp = 221
803
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18717519
37 X = 5724429
88
Y = -527122
53 feet Y = -96760
10 meter
Z = -12128997
48 Z = -3669158
59
XDOT = -8709
299589 XDOT = -2697
126154
YDOT = 18736
899678 feet/sec YDOT = 5681
083946 meter/sec
ZDOT = -14274
100361 ZDOT = -4363
743562
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11142874
84 X = -3396348
25
Y = -15150893
71 feet Y = -4617992
40 meter
Z = -12000947
03 Z = -3657888
66
XDOT = 19199
886993 XDOT = 5852
125556
YDOT = -2782
390119 feet/sec YDOT = -848
072508 meter/sec
ZDOT = -14334
172295 ZDOT = -4369
055716
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 20209
52452178
00016717 00000-0 10270-3 0 9004
2 25544 51
6407 148
8185 0000886 134
6482 225
4741 15
49518404 38265
Satellite: ISS
Catalog Number: 25544
Epoch time: 20209
52452178 = yrday
fracday
Element set: 900
Inclination: 51
6407 deg
RA of node: 148
8185 deg
Eccentricity:
0000886
Arg of perigee: 134
6482 deg
Mean anomaly: 225
4741 deg
Mean motion: 15
49518404 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3826
Checksum: 313
Coasting Arc #2 (Orbit 3841)
---------------------------------------
Vector Time (GMT): 2020/210/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 984330
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5601872
27 A = 6796766
01 meter
Y = 492414
74 meter E =
0012116
Z = 3808926
14 I = 51
87416
XDOT = 2358
368958 Wp = 100
22708
YDOT = -5943
801693 meter/sec RA = 142
86389 deg
ZDOT = 4223
402330 TA = 305
24302
MA = 305
35635
Ha = 228
563 n
mi
Hp = 221
783
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18378846
04 X = -5625463
71
Y = 1615533
93 feet Y = 429638
35 meter
Z = 12496476
85 Z = 3781657
38
XDOT = 7737
430963 XDOT = 2404
144323
YDOT = -19500
661722 feet/sec YDOT = -5917
173168 meter/sec
ZDOT = 13856
306856 ZDOT = 4234
968915
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12089410
41 X = 3684852
29
Y = 14048721
92 feet Y = 4282050
44 meter
Z = 12370668
27 Z = 3770579
69
XDOT = -19269
992717 XDOT = -5873
493780
YDOT = 4294
720084 feet/sec YDOT = 1309
030682 meter/sec
ZDOT = 13909
798842 ZDOT = 4239
706687
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 20210
55642450
00016717 00000-0 10270-3 0 9014
2 25544 51
6410 143
7107 0000897 148
9210 211
1994 15
49518899 38424
Satellite: ISS
Catalog Number: 25544
Epoch time: 20210
55642450 = yrday
fracday
Element set: 901
Inclination: 51
6410 deg
RA of node: 143
7107 deg
Eccentricity:
0000897
Arg of perigee: 148
9210 deg
Mean anomaly: 211
1994 deg
Mean motion: 15
49518899 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3842
Checksum: 302
Coasting Arc #3 (Orbit 3856)
---------------------------------------
Vector Time (GMT): 2020/211/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 984330
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5482303
81 A = 6796303
55 meter
Y = -779145
89 meter E =
0006850
Z = -3947166
66 I = 51
89980
XDOT = -2051
817362 Wp = 80
47791
YDOT = 6149
674555 meter/sec RA = 137
92968 deg
ZDOT = -4068
635838 TA = 147
05012
MA = 147
00741
Ha = 228
482 n
mi
Hp = 221
841
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17986561
06 X = 5509781
91
Y = -2556252
93 feet Y = -717684
77 meter
Z = -12950021
86 Z = -3920469
35
XDOT = -6731
684257 XDOT = -2100
669429
YDOT = 20176
097623 feet/sec YDOT = 6126
456980 meter/sec
ZDOT = -13348
542777 ZDOT = -4078
720637
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12851019
65 X = -3916990
79
Y = -12964479
52 feet Y = -3951573
36 meter
Z = -12826824
96 Z = -3909616
25
XDOT = 19199
685152 XDOT = 5852
064034
YDOT = -5794
774207 feet/sec YDOT = -1766
247178 meter/sec
ZDOT = -13395
221525 ZDOT = -4082
863521
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 20211
52383213
00016717 00000-0 10270-3 0 9022
2 25544 51
6419 138
9212 0000784 138
4948 221
6262 15
49526285 38571
Satellite: ISS
Catalog Number: 25544
Epoch time: 20211
52383213 = yrday
fracday
Element set: 902
Inclination: 51
6419 deg
RA of node: 138
9212 deg
Eccentricity:
0000784
Arg of perigee: 138
4948 deg
Mean anomaly: 221
6262 deg
Mean motion: 15
49526285 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3857
Checksum: 307
Coasting Arc #4 (Orbit 3857)
---------------------------------------
Vector Time (GMT): 2020/211/14:02:36
252
Vector Time (MET): N/A
Weight (LBS) : 984095
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3935681
58 A = 6802772
79 meter
Y = 5309005
12 meter E =
0008287
Z = -1597924
78 I = 51
92174
XDOT = -4729
515857 Wp = 32
72315
YDOT = -1780
194939 meter/sec RA = 137
47045 deg
ZDOT = 5754
894881 TA = 309
90564
MA = 309
97846
Ha = 228
717 n
mi
Hp = 222
678
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12912341
16 X = -3986994
22
Y = 17417995
79 feet Y = 5264706
79 meter
Z = -5242535
36 Z = -1617166
63
XDOT = -15516
784307 XDOT = -4737
211422
YDOT = -5840
534577 feet/sec YDOT = -1833
127451 meter/sec
ZDOT = 18880
888718 ZDOT = 5731
902045
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18574972
79 X = 5661651
71
Y = -11142054
79 feet Y = -3396098
30 meter
Z = -5331445
31 Z = -1625024
53
XDOT = 11393
496266 XDOT = 3472
737662
YDOT = 10042
397801 feet/sec YDOT = 3060
922850 meter/sec
ZDOT = 18774
844622 ZDOT = 5722
572641
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 20211
58832533
00016717 00000-0 10270-3 0 9033
2 25544 51
6438 138
6025 0000881 331
7881 28
3221 15
49133009 38589
Satellite: ISS
Catalog Number: 25544
Epoch time: 20211
58832533 = yrday
fracday
Element set: 903
Inclination: 51
6438 deg
RA of node: 138
6025 deg
Eccentricity:
0000881
Arg of perigee: 331
7881 deg
Mean anomaly: 28
3221 deg
Mean motion: 15
49133009 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3858
Checksum: 296
Coasting Arc #5 (Orbit 3869)
---------------------------------------
Vector Time (GMT): 2020/212/08:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 984095
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5414096
97 A = 6802815
01 meter
Y = -3764537
32 meter E =
0007154
Z = -1661177
95 I = 51
93605
XDOT = 1597
728501 Wp = 139
54008
YDOT = 4818
985574 meter/sec RA = 133
81097 deg
ZDOT = -5732
534299 TA = 58
53530
MA = 58
46539
Ha = 228
880 n
mi
Hp = 222
653
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17762785
34 X = 5463859
73
Y = -12350844
22 feet Y = -3703714
57 meter
Z = -5450058
91 Z = -1634758
29
XDOT = 5241
891407 XDOT = 1571
567478
YDOT = 15810
320124 feet/sec YDOT = 4836
706962 meter/sec
ZDOT = -18807
527228 ZDOT = -5724
836175
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4605848
92 X = -1403862
75
Y = -21169815
15 feet Y = -6452559
66 meter
Z = -5328050
33 Z = -1623989
74
XDOT = 15117
603513 XDOT = 4607
845551
YDOT = 1419
357123 feet/sec YDOT = 432
620051 meter/sec
ZDOT = -18772
128975 ZDOT = -5721
744912
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 20212
36244684
00016717 00000-0 10270-3 0 9045
2 25544 51
6401 134
7715 0000831 347
8023 12
3107 15
49119144 38707
Satellite: ISS
Catalog Number: 25544
Epoch time: 20212
36244684 = yrday
fracday
Element set: 904
Inclination: 51
6401 deg
RA of node: 134
7715 deg
Eccentricity:
0000831
Arg of perigee: 347
8023 deg
Mean anomaly: 12
3107 deg
Mean motion: 15
49119144 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3870
Checksum: 276
Coasting Arc #6 (Orbit 3885)
---------------------------------------
Vector Time (GMT): 2020/213/08:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 984095
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5076279
90 A = 6802649
50 meter
Y = 4191106
19 meter E =
0013907
Z = 1687554
22 I = 51
95820
XDOT = -1965
982924 Wp = 61
34944
YDOT = -4698
176299 meter/sec RA = 128
88467 deg
ZDOT = 5725
070804 TA = 317
03009
MA = 317
13863
Ha = 228
764 n
mi
Hp = 222
624
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16654461
61 X = -5130965
87
Y = 13750348
40 feet Y = 4134033
61 meter
Z = 5536595
22 Z = 1662763
76
XDOT = -6450
075210 XDOT = -1941
109081
YDOT = -15413
964234 feet/sec YDOT = -4720
023006 meter/sec
ZDOT = 18783
040696 ZDOT = 5715
580763
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6677390
32 X = 2035268
57
Y = 20569654
35 feet Y = 6269630
65 meter
Z = 5422069
52 Z = 1652646
79
XDOT = -15251
427049 XDOT = -4648
634965
YDOT = -14
448697 feet/sec YDOT = -4
403963 meter/sec
ZDOT = 18739
372585 ZDOT = 5711
760764
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 20213
39460775
00016717 00000-0 10270-3 0 9051
2 25544 51
6398 129
6659 0000651 334
1579 25
9538 15
49164757 38862
Satellite: ISS
Catalog Number: 25544
Epoch time: 20213
39460775 = yrday
fracday
Element set: 905
Inclination: 51
6398 deg
RA of node: 129
6659 deg
Eccentricity:
0000651
Arg of perigee: 334
1579 deg
Mean anomaly: 25
9538 deg
Mean motion: 15
49164757 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3886
Checksum: 347
Coasting Arc #7 (Orbit 3900)
---------------------------------------
Vector Time (GMT): 2020/214/08:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 984095
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4724232
80 A = 6802676
95 meter
Y = -4568609
24 meter E =
0006812
Z = -1747729
89 I = 51
97922
XDOT = 2305
762219 Wp = 138
76523
YDOT = 4559
430627 meter/sec RA = 123
95843 deg
ZDOT = -5703
451916 TA = 60
27526
MA = 60
20749
Ha = 228
869 n
mi
Hp = 222
656
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15499451
44 X = 4783458
54
Y = -14988875
47 feet Y = -4515448
12 meter
Z = -5734021
95 Z = -1724638
62
XDOT = 7564
836678 XDOT = 2282
309480
YDOT = 14958
761899 feet/sec YDOT = 4585
084909 meter/sec
ZDOT = -18712
112586 ZDOT = -5692
308023
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8594467
94 X = -2619593
83
Y = -19805225
06 feet Y = -6036632
60 meter
Z = -5627305
91 Z = -1715202
84
XDOT = 15260
651743 XDOT = 4651
446651
YDOT = -1336
948818 feet/sec YDOT = -407
502000 meter/sec
ZDOT = -18660
807748 ZDOT = -5687
814202
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 20214
36226165
00016717 00000-0 10270-3 0 9063
2 25544 51
6409 124
8780 0000903 347
5623 12
5504 15
49122462 39015
Satellite: ISS
Catalog Number: 25544
Epoch time: 20214
36226165 = yrday
fracday
Element set: 906
Inclination: 51
6409 deg
RA of node: 124
8780 deg
Eccentricity:
0000903
Arg of perigee: 347
5623 deg
Mean anomaly: 12
5504 deg
Mean motion: 15
49122462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3901
Checksum: 282
Coasting Arc #8 (Orbit 3910)
---------------------------------------
Vector Time (GMT): 2020/214/23:32:45
000
Vector Time (MET): N/A
Weight (LBS) : 956537
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4892593
94 A = 6800287
48 meter
Y = -3667803
95 meter E =
0004072
Z = -2976942
53 I = 51
98621
XDOT = 1193
967512 Wp = 110
62385
YDOT = 5658
361820 meter/sec RA = 120
77440 deg
ZDOT = -5016
156414 TA = 103
12735
MA = 103
08191
Ha = 228
796 n
mi
Hp = 222
773
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16051817
40 X = 4947704
75
Y = -12033477
52 feet Y = -3612782
96 meter
Z = -9766871
83 Z = -2953043
36
XDOT = 3917
216248 XDOT = 1154
970340
YDOT = 18564
179201 feet/sec YDOT = 5671
496178 meter/sec
ZDOT = -16457
206083 ZDOT = -5010
450748
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18909067
32 X = 5763483
72
Y = 6859849
79 feet Y = 2090882
22 meter
Z = -9656440
47 Z = -2943283
06
XDOT = -12799
376783 XDOT = -3901
250043
YDOT = 12184
111254 feet/sec YDOT = 3713
717110 meter/sec
ZDOT = -16431
037300 ZDOT = -5008
180169
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 20215
00736143
00016717 00000-0 10270-3 0 9078
2 25544 51
6441 121
6848 0000549 318
1792 41
9316 15
49116318 39119
Satellite: ISS
Catalog Number: 25544
Epoch time: 20215
00736143 = yrday
fracday
Element set: 907
Inclination: 51
6441 deg
RA of node: 121
6848 deg
Eccentricity:
0000549
Arg of perigee: 318
1792 deg
Mean anomaly: 41
9316 deg
Mean motion: 15
49116318 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3911
Checksum: 291
Coasting Arc #9 (Orbit 3926)
---------------------------------------
Vector Time (GMT): 2020/215/23:32:45
000
Vector Time (MET): N/A
Weight (LBS) : 956537
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4563242
98 A = 6800164
40 meter
Y = 4040585
57 meter E =
0013018
Z = 3001490
99 I = 52
00274
XDOT = -1637
593688 Wp = 80
03578
YDOT = -5573
737262 meter/sec RA = 115
85088 deg
ZDOT = 4997
438738 TA = 314
06240
MA = 314
16952
Ha = 228
872 n
mi
Hp = 222
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14971269
61 X = -4622666
01
Y = 13256514
34 feet Y = 3989223
57 meter
Z = 9847411
40 Z = 2979181
21
XDOT = -5372
682704 XDOT = -1599
418849
YDOT = -18286
539573 feet/sec YDOT = -5591
837067 meter/sec
ZDOT = 16395
796384 ZDOT = 4989
576300
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19426018
06 X = -5921050
30
Y = -4952196
57 feet Y = -1509429
52 meter
Z = 9744289
04 Z = 2970059
30
XDOT = 11653
916573 XDOT = 3552
113771
YDOT = -13418
709053 feet/sec YDOT = -4090
022519 meter/sec
ZDOT = 16359
671563 ZDOT = 4986
427892
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 20216
03951991
00016717 00000-0 10270-3 0 9083
2 25544 51
6446 116
5787 0000633 338
5997 21
5126 15
49136140 39271
Satellite: ISS
Catalog Number: 25544
Epoch time: 20216
03951991 = yrday
fracday
Element set: 908
Inclination: 51
6446 deg
RA of node: 116
5787 deg
Eccentricity:
0000633
Arg of perigee: 338
5997 deg
Mean anomaly: 21
5126 deg
Mean motion: 15
49136140 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3927
Checksum: 318
Coasting Arc #10 (Orbit 3941)
---------------------------------------
Vector Time (GMT): 2020/216/23:32:45
000
Vector Time (MET): N/A
Weight (LBS) : 956537
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4224434
74 A = 6800079
53 meter
Y = -4367665
16 meter E =
0004140
Z = -3054965
10 I = 52
01468
XDOT = 2059
359789 Wp = 103
15249
YDOT = 5455
838888 meter/sec RA = 110
92906 deg
ZDOT = -4959
039542 TA = 111
59153
MA = 111
54741
Ha = 228
847 n
mi
Hp = 222
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13859694
03 X = 4287800
18
Y = -14329610
10 feet Y = -4320069
97 meter
Z = -10022851
37 Z = -3034291
46
XDOT = 6756
429755 XDOT = 2022
285428
YDOT = 17899
733886 feet/sec YDOT = 5478
661217 meter/sec
ZDOT = -16269
814770 ZDOT = -4949
125864
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19742877
57 X = 6017629
08
Y = 3091070
40 feet Y = 942158
26 meter
Z = -9927258
59 Z = -3025828
42
XDOT = -10418
116249 XDOT = -3175
441833
YDOT = 14505
448216 feet/sec YDOT = 4421
260616 meter/sec
ZDOT = -16224
218149 ZDOT = -4945
141692
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 20217
00716984
00016717 00000-0 10270-3 0 9093
2 25544 51
6434 111
7926 0000623 338
8399 21
2724 15
49116622 39429
Satellite: ISS
Catalog Number: 25544
Epoch time: 20217
00716984 = yrday
fracday
Element set: 909
Inclination: 51
6434 deg
RA of node: 111
7926 deg
Eccentricity:
0000623
Arg of perigee: 338
8399 deg
Mean anomaly: 21
2724 deg
Mean motion: 15
49116622 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3942
Checksum: 306
Coasting Arc #11 (Orbit 3957)
---------------------------------------
Vector Time (GMT): 2020/217/23:32:45
000
Vector Time (MET): N/A
Weight (LBS) : 956537
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3842974
09 A = 6799953
54 meter
Y = 4680629
38 meter E =
0012928
Z = 3078881
59 I = 52
02561
XDOT = -2489
615145 Wp = 81
08005
YDOT = -5303
526555 meter/sec RA = 106
00698 deg
ZDOT = 4939
440477 TA = 314
01273
MA = 314
11921
Ha = 228
882 n
mi
Hp = 222
625
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12608182
70 X = -3909983
71
Y = 15356395
62 feet Y = 4637279
66 meter
Z = 10101317
56 Z = 3060051
94
XDOT = -8168
028691 XDOT = -2454
116821
YDOT = -17400
021506 feet/sec YDOT = -5331
168999 meter/sec
ZDOT = 16205
513375 ZDOT = 4927
433151
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19880869
77 X = -6059689
11
Y = -1135010
16 feet Y = -345951
10 meter
Z = 10014217
04 Z = 3052333
35
XDOT = 9047
186408 XDOT = 2757
582417
YDOT = -15518
162470 feet/sec YDOT = -4729
935921 meter/sec
ZDOT = 16150
247482 ZDOT = 4922
595432
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 20218
03932762
00016717 00000-0 10270-3 0 9103
2 25544 51
6436 106
6861 0000667 343
1856 16
9272 15
49136715 39588
Satellite: ISS
Catalog Number: 25544
Epoch time: 20218
03932762 = yrday
fracday
Element set: 910
Inclination: 51
6436 deg
RA of node: 106
6861 deg
Eccentricity:
0000667
Arg of perigee: 343
1856 deg
Mean anomaly: 16
9272 deg
Mean motion: 15
49136715 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3958
Checksum: 315
Coasting Arc #12 (Orbit 3972)
---------------------------------------
Vector Time (GMT): 2020/218/23:32:45
000
Vector Time (MET): N/A
Weight (LBS) : 956537
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3460190
59 A = 6799846
63 meter
Y = -4946946
34 meter E =
0004253
Z = -3132429
82 I = 52
03277
XDOT = 2892
335480 Wp = 96
17572
YDOT = 5121
306487 meter/sec RA = 101
08573 deg
ZDOT = -4899
090981 TA = 119
57111
MA = 119
52871
Ha = 228
875 n
mi
Hp = 222
660
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11352331
33 X = 3530466
83
Y = -16230138
91 feet Y = -4907858
97 meter
Z = -10277000
71 Z = -3115451
47
XDOT = 9489
289633 XDOT = 2858
648926
YDOT = 16802
186637 feet/sec YDOT = 5153
462465 meter/sec
ZDOT = -16073
133140 ZDOT = -4885
123135
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19833352
22 X = 6045205
76
Y = -734683
30 feet Y = -223931
47 meter
Z = -10198429
25 Z = -3108481
24
XDOT = -7615
163194 XDOT = -2321
101741
YDOT = 16365
129992 feet/sec YDOT = 4988
091622 meter/sec
ZDOT = -16008
812246 ZDOT = -4879
485973
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 20219
00697530
00016717 00000-0 10270-3 0 9113
2 25544 51
6431 101
8991 0000753 350
5339 9
5797 15
49123415 39738
Satellite: ISS
Catalog Number: 25544
Epoch time: 20219
00697530 = yrday
fracday
Element set: 911
Inclination: 51
6431 deg
RA of node: 101
8991 deg
Eccentricity:
0000753
Arg of perigee: 350
5339 deg
Mean anomaly: 9
5797 deg
Mean motion: 15
49123415 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3973
Checksum: 305
Coasting Arc #13 (Orbit 3975)
---------------------------------------
Vector Time (GMT): 2020/219/03:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 956537
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3480464
91 A = 6793219
86 meter
Y = -2919867
00 meter E =
0006553
Z = 5047573
36 I = 52
01090
XDOT = 2819
621478 Wp = 49
76761
YDOT = -6837
031200 meter/sec RA = 100
18802 deg
ZDOT = -2004
965454 TA = 59
65486
MA = 59
59007
Ha = 229
054 n
mi
Hp = 222
482
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11418848
12 X = -3472073
04
Y = -9579616
13 feet Y = -2958741
28 meter
Z = 16560280
06 Z = 5030687
33
XDOT = 9250
726633 XDOT = 2905
604387
YDOT = -22431
204725 feet/sec YDOT = -6805
019353 meter/sec
ZDOT = -6577
970649 ZDOT = -1991
060555
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13051029
33 X = -3977953
74
Y = -7375830
23 feet Y = -2248153
05 meter
Z = 16482408
05 Z = 5023837
97
XDOT = 4621
128154 XDOT = 1408
519861
YDOT = -22775
155815 feet/sec YDOT = -6941
867492 meter/sec
ZDOT = -6513
523480 ZDOT = -1985
321957
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 20219
20050368
00016717 00000-0 10270-3 0 9128
2 25544 51
6420 100
9424 0000998 6
6646 353
4517 15
49139755 39766
Satellite: ISS
Catalog Number: 25544
Epoch time: 20219
20050368 = yrday
fracday
Element set: 912
Inclination: 51
6420 deg
RA of node: 100
9424 deg
Eccentricity:
0000998
Arg of perigee: 6
6646 deg
Mean anomaly: 353
4517 deg
Mean motion: 15
49139755 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3976
Checksum: 308
Coasting Arc #14 (Orbit 3990)
---------------------------------------
Vector Time (GMT): 2020/220/03:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 956537
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3708956
73 A = 6793382
82 meter
Y = 2660964
93 meter E =
0012642
Z = -5042622
01 I = 52
01528
XDOT = -2253
249777 Wp = 100
14024
YDOT = 7018
247654 meter/sec RA = 95
26693 deg
ZDOT = 2048
380790 TA = 189
70650
MA = 189
73094
Ha = 229
030 n
mi
Hp = 222
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12168493
19 X = 3703419
03
Y = 8730199
90 feet Y = 2702410
27 meter
Z = -16544035
47 Z = -5024619
12
XDOT = -7392
551763 XDOT = -2341
512114
YDOT = 23025
746897 feet/sec YDOT = 6992
556660 meter/sec
ZDOT = 6720
409417 ZDOT = 2037
221376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13745765
48 X = 4189709
32
Y = 6171155
67 feet Y = 1880968
25 meter
Z = -16460999
23 Z = -5017312
57
XDOT = -2362
701246 XDOT = -720
151340
YDOT = 23031
304903 feet/sec YDOT = 7019
941734 meter/sec
ZDOT = 6668
620976 ZDOT = 2032
595674
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 20220
16814974
00016717 00000-0 10270-3 0 9137
2 25544 51
6414 96
1555 0001093 10
1795 349
9377 15
49107391 39914
Satellite: ISS
Catalog Number: 25544
Epoch time: 20220
16814974 = yrday
fracday
Element set: 913
Inclination: 51
6414 deg
RA of node: 96
1555 deg
Eccentricity:
0001093
Arg of perigee: 10
1795 deg
Mean anomaly: 349
9377 deg
Mean motion: 15
49107391 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3991
Checksum: 315
Coasting Arc #15 (Orbit 4006)
---------------------------------------
Vector Time (GMT): 2020/221/03:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 956537
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3901715
05 A = 6793397
54 meter
Y = -2396401
49 meter E =
0006909
Z = 5015226
60 I = 52
01593
XDOT = 1688
339212 Wp = 50
15871
YDOT = -7171
165860 meter/sec RA = 90
34513 deg
ZDOT = -2106
855289 TA = 60
29242
MA = 60
22367
Ha = 229
103 n
mi
Hp = 222
482
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12800902
38 X = -3898988
48
Y = -7862209
62 feet Y = -2440018
08 meter
Z = 16454155
52 Z = 4996280
51
XDOT = 5539
170643 XDOT = 1778
637582
YDOT = -23527
447047 feet/sec YDOT = -7151
780727 meter/sec
ZDOT = -6912
254885 ZDOT = -2098
434913
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14283750
37 X = -4353687
11
Y = -4951807
83 feet Y = -1509311
03 meter
Z = 16366757
47 Z = 4988587
68
XDOT = 121
543475 XDOT = 37
046451
YDOT = -23135
469190 feet/sec YDOT = -7051
691009 meter/sec
ZDOT = -6873
095054 ZDOT = -2094
919372
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 20221
20030504
00016717 00000-0 10270-3 0 9143
2 25544 51
6398 91
0486 0001099 8
3334 351
7834 15
49130060 40073
Satellite: ISS
Catalog Number: 25544
Epoch time: 20221
20030504 = yrday
fracday
Element set: 914
Inclination: 51
6398 deg
RA of node: 91
0486 deg
Eccentricity:
0001099
Arg of perigee: 8
3334 deg
Mean anomaly: 351
7834 deg
Mean motion: 15
49130060 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4007
Checksum: 270
Coasting Arc #16 (Orbit 4021)
---------------------------------------
Vector Time (GMT): 2020/222/03:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 956537
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4092381
80 A = 6793530
36 meter
Y = 2103416
23 meter E =
0012475
Z = -5009329
88 I = 52
01562
XDOT = -1102
793992 Wp = 100
34948
YDOT = 7259
016249 meter/sec RA = 85
42388 deg
ZDOT = 2149
498458 TA = 190
52106
MA = 190
54719
Ha = 229
068 n
mi
Hp = 222
592
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13426449
48 X = 4092888
77
Y = 6900971
88 feet Y = 2149183
07 meter
Z = -16434809
33 Z = -4989449
69
XDOT = -3618
090526 XDOT = -1194
325425
YDOT = 23815
670109 feet/sec YDOT = 7246
172205 meter/sec
ZDOT = 7052
160296 ZDOT = 2143
919373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14756221
95 X = 4497696
45
Y = 3626736
40 feet Y = 1105429
25 meter
Z = -16343090
69 Z = -4981374
04
XDOT = 2132
950340 XDOT = 650
123264
YDOT = 22947
954487 feet/sec YDOT = 6994
536528 meter/sec
ZDOT = 7026
101879 ZDOT = 2141
555853
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 20222
16795070
00016717 00000-0 10270-3 0 9156
2 25544 51
6403 86
2613 0001162 14
2555 345
8627 15
49108458 40227
Satellite: ISS
Catalog Number: 25544
Epoch time: 20222
16795070 = yrday
fracday
Element set: 915
Inclination: 51
6403 deg
RA of node: 86
2613 deg
Eccentricity:
0001162
Arg of perigee: 14
2555 deg
Mean anomaly: 345
8627 deg
Mean motion: 15
49108458 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4022
Checksum: 287
Coasting Arc #17 (Orbit 4037)
---------------------------------------
Vector Time (GMT): 2020/223/03:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 956537
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4246454
57 A = 6793540
47 meter
Y = -1812422
62 meter E =
0007335
Z = 4980107
21 I = 52
01233
XDOT = 524
824724 Wp = 51
09319
YDOT = -7318
457051 meter/sec RA = 80
50184 deg
ZDOT = -2209
253000 TA = 60
40110
MA = 60
32804
Ha = 229
159 n
mi
Hp = 222
426
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13931937
56 X = -4250062
19
Y = -5946268
44 feet Y = -1859929
78 meter
Z = 16338934
41 Z = 4959470
99
XDOT = 1721
865892 XDOT = 617
354082
YDOT = -24010
685863 feet/sec YDOT = -7312
070677 meter/sec
ZDOT = -7248
205379 ZDOT = -2206
479043
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15071918
50 X = -4593920
76
Y = -2323079
21 feet Y = -708074
54 meter
Z = 16243717
11 Z = 4951084
98
XDOT = -4335
716901 XDOT = -1321
526511
YDOT = -22614
009905 feet/sec YDOT = -6892
750219 meter/sec
ZDOT = -7235
080735 ZDOT = -2205
252608
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 20223
20010359
00016717 00000-0 10270-3 0 9163
2 25544 51
6406 81
1542 0001218 13
8672 346
2511 15
49134982 40387
Satellite: ISS
Catalog Number: 25544
Epoch time: 20223
20010359 = yrday
fracday
Element set: 916
Inclination: 51
6406 deg
RA of node: 81
1542 deg
Eccentricity:
0001218
Arg of perigee: 13
8672 deg
Mean anomaly: 346
2511 deg
Mean motion: 15
49134982 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4038
Checksum: 274
Coasting Arc #18 (Orbit 4043)
---------------------------------------
Vector Time (GMT): 2020/223/13:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 956537
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3838983
51 A = 6797894
42 meter
Y = -4150508
06 meter E =
0011868
Z = 3766753
17 I = 52
02669
XDOT = 2212
127827 Wp = 77
44270
YDOT = -5951
369103 meter/sec RA = 78
56700 deg
ZDOT = -4289
265734 TA = 57
86014
MA = 57
74504
Ha = 228
969 n
mi
Hp = 222
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12595090
26 X = -3810582
55
Y = -13617152
44 feet Y = -4193279
61 meter
Z = 12358114
09 Z = 3748173
93
XDOT = 7257
637227 XDOT = 2299
348034
YDOT = -19525
489183 feet/sec YDOT = -5926
143726 meter/sec
ZDOT = -14072
394139 ZDOT = -4278
308476
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5873874
39 X = 1790356
91
Y = 17654162
64 feet Y = 5380988
77 meter
Z = 12272500
33 Z = 3740658
10
XDOT = -13515
644817 XDOT = -4119
568540
YDOT = 14276
020249 feet/sec YDOT = 4351
330972 meter/sec
ZDOT = -14021
533044 ZDOT = -4273
763272
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 20223
58715868
00016717 00000-0 10270-3 0 9172
2 25544 51
6424 79
2383 0001369 1
1765 358
9388 15
49166193 40446
Satellite: ISS
Catalog Number: 25544
Epoch time: 20223
58715868 = yrday
fracday
Element set: 917
Inclination: 51
6424 deg
RA of node: 79
2383 deg
Eccentricity:
0001369
Arg of perigee: 1
1765 deg
Mean anomaly: 358
9388 deg
Mean motion: 15
49166193 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4044
Checksum: 332
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