[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 31st 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19920 769 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
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 3887)
---------------------------------------
Vector Time (GMT): 2020/213/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 984330
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5249250
94 A = 6797200
45 meter
Y = -1599855
01 meter E =
0006950
Z = -4018624
01 I = 51
94668
XDOT = -1084
865339 Wp = 65
17005
YDOT = 6442
812657 meter/sec RA = 128
07364 deg
ZDOT = -3984
600126 TA = 163
44738
MA = 163
42468
Ha = 228
835 n
mi
Hp = 222
717
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17221951
92 X = 5286270
73
Y = -5248868
13 feet Y = -1540946
61 meter
Z = -13184461
99 Z = -3993035
92
XDOT = -3559
269484 XDOT = -1137
475577
YDOT = 21137
836802 feet/sec YDOT = 6430
387286 meter/sec
ZDOT = -13072
835058 ZDOT = -3989
996813
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14915015
99 X = -4546096
87
Y = -10236687
75 feet Y = -3120142
43 meter
Z = -13066323
29 Z = -3982615
34
XDOT = 17925
131627 XDOT = 5463
580120
YDOT = -9409
583262 feet/sec YDOT = -2868
040978 meter/sec
ZDOT = -13097
920991 ZDOT = -3992
246318
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
52362666
00016717 00000-0 10270-3 0 9001
2 25544 51
6432 129
0278 0000976 348
3479 11
7648 15
49138100 38888
Satellite: ISS
Catalog Number: 25544
Epoch time: 20213
52362666 = yrday
fracday
Element set: 900
Inclination: 51
6432 deg
RA of node: 129
0278 deg
Eccentricity:
0000976
Arg of perigee: 348
3479 deg
Mean anomaly: 11
7648 deg
Mean motion: 15
49138100 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3888
Checksum: 313
Coasting Arc #2 (Orbit 3903)
---------------------------------------
Vector Time (GMT): 2020/214/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 984330
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5080986
30 A = 6797165
19 meter
Y = 2003326
67 meter E =
0010518
Z = 4038073
26 I = 51
96660
XDOT = 574
050557 Wp = 96
51600
YDOT = -6538
096581 meter/sec RA = 123
14804 deg
ZDOT = 3955
932408 TA = 312
49026
MA = 312
57909
Ha = 228
976 n
mi
Hp = 222
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16669902
55 X = -5122624
71
Y = 6572594
07 feet Y = 1946274
13 meter
Z = 13248271
86 Z = 4013291
46
XDOT = 1883
367968 XDOT = 627
903590
YDOT = -21450
448099 feet/sec YDOT = -6531
376530 meter/sec
ZDOT = 12978
780867 ZDOT = 3958
850826
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15756068
02 X = 4802449
53
Y = 8709209
48 feet Y = 2654567
05 meter
Z = 13133824
35 Z = 4003189
66
XDOT = -17024
855283 XDOT = -5189
175890
YDOT = 11157
163971 feet/sec YDOT = 3400
703578 meter/sec
ZDOT = 12992
443325 ZDOT = 3960
096726
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
55578608
00016717 00000-0 10270-3 0 9011
2 25544 51
6435 123
9216 0000956 347
7464 12
3663 15
49121386 39042
Satellite: ISS
Catalog Number: 25544
Epoch time: 20214
55578608 = yrday
fracday
Element set: 901
Inclination: 51
6435 deg
RA of node: 123
9216 deg
Eccentricity:
0000956
Arg of perigee: 347
7464 deg
Mean anomaly: 12
3663 deg
Mean motion: 15
49121386 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3904
Checksum: 307
Coasting Arc #3 (Orbit 3910)
---------------------------------------
Vector Time (GMT): 2020/214/23:32:45
000
Vector Time (MET): N/A
Weight (LBS) : 956773
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4893396
90 A = 6800264
66 meter
Y = -3663939
71 meter E =
0004103
Z = -2980408
08 I = 51
98638
XDOT = 1189
719988 Wp = 110
02185
YDOT = 5661
521565 meter/sec RA = 120
77411 deg
ZDOT = -5013
558406 TA = 103
77378
MA = 103
72811
Ha = 228
803 n
mi
Hp = 222
751
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16054451
77 X = 4948481
27
Y = -12020799
57 feet Y = -3608909
89 meter
Z = -9778241
74 Z = -2956505
07
XDOT = 3903
280800 XDOT = 1150
675178
YDOT = 18574
545817 feet/sec YDOT = 5674
608157 meter/sec
ZDOT = -16448
682435 ZDOT = -5007
873488
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18899962
77 X = 5760708
65
Y = 6869078
94 feet Y = 2093695
26 meter
Z = -9667792
79 Z = -2946743
24
XDOT = -12815
052833 XDOT = -3906
028103
YDOT = 12178
775409 feet/sec YDOT = 3712
090745 meter/sec
ZDOT = -16422
609520 ZDOT = -5005
611382
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
00735351
00016717 00000-0 10270-3 0 9023
2 25544 51
6442 121
6846 0000535 322
6350 37
4762 15
49121187 39118
Satellite: ISS
Catalog Number: 25544
Epoch time: 20215
00735351 = yrday
fracday
Element set: 902
Inclination: 51
6442 deg
RA of node: 121
6846 deg
Eccentricity:
0000535
Arg of perigee: 322
6350 deg
Mean anomaly: 37
4762 deg
Mean motion: 15
49121187 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3911
Checksum: 275
Coasting Arc #4 (Orbit 3926)
---------------------------------------
Vector Time (GMT): 2020/215/23:32:45
000
Vector Time (MET): N/A
Weight (LBS) : 956773
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4564786
74 A = 6800134
90 meter
Y = 4035136
21 meter E =
0013053
Z = 3006364
60 I = 52
00289
XDOT = -1631
926748 Wp = 80
09160
YDOT = -5578
777809 meter/sec RA = 115
85058 deg
ZDOT = 4993
722214 TA = 314
06978
MA = 314
17717
Ha = 228
879 n
mi
Hp = 222
620
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14976334
45 X = -4624172
40
Y = 13238635
85 feet Y = 3983757
15 meter
Z = 9863400
91 Z = 2984047
41
XDOT = -5354
090382 XDOT = -1593
677913
YDOT = -18303
076800 feet/sec YDOT = -5596
813828 meter/sec
ZDOT = 16383
603064 ZDOT = 4985
887482
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19414165
06 X = -5917437
51
Y = -4966545
31 feet Y = -1513803
01 meter
Z = 9760244
52 Z = 2974922
53
XDOT = 11677
056096 XDOT = 3559
166698
YDOT = -13413
465548 feet/sec YDOT = -4088
424299 meter/sec
ZDOT = 16347
606310 ZDOT = 4982
750403
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
03950839
00016717 00000-0 10270-3 0 9038
2 25544 51
6448 116
5786 0000631 342
4770 17
6359 15
49142047 39270
Satellite: ISS
Catalog Number: 25544
Epoch time: 20216
03950839 = yrday
fracday
Element set: 903
Inclination: 51
6448 deg
RA of node: 116
5786 deg
Eccentricity:
0000631
Arg of perigee: 342
4770 deg
Mean anomaly: 17
6359 deg
Mean motion: 15
49142047 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3927
Checksum: 312
Coasting Arc #5 (Orbit 3941)
---------------------------------------
Vector Time (GMT): 2020/216/23:32:45
000
Vector Time (MET): N/A
Weight (LBS) : 956773
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4227160
66 A = 6800042
68 meter
Y = -4360371
12 meter E =
0004179
Z = -3061616
99 I = 52
01482
XDOT = 2052
203229 Wp = 102
54698
YDOT = 5463
212841 meter/sec RA = 110
92874 deg
ZDOT = -4953
845407 TA = 112
28351
MA = 112
23920
Ha = 228
852 n
mi
Hp = 222
691
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13868637
34 X = 4290476
64
Y = -14305679
54 feet Y = -4312745
73 meter
Z = -10044675
17 Z = -3040930
23
XDOT = 6732
950225 XDOT = 2015
021712
YDOT = 17923
926644 feet/sec YDOT = 5485
954540 meter/sec
ZDOT = -16252
773644 ZDOT = -4943
966751
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19728596
58 X = 6013276
24
Y = 3112315
13 feet Y = 948633
65 meter
Z = -9949022
04 Z = -3032461
92
XDOT = -10449
945830 XDOT = -3185
143489
YDOT = 14501
204859 feet/sec YDOT = 4419
967241 meter/sec
ZDOT = -16207
338963 ZDOT = -4939
996916
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
00715425
00016717 00000-0 10270-3 0 9047
2 25544 51
6435 111
7924 0000618 342
6189 17
4932 15
49123437 39422
Satellite: ISS
Catalog Number: 25544
Epoch time: 20217
00715425 = yrday
fracday
Element set: 904
Inclination: 51
6435 deg
RA of node: 111
7924 deg
Eccentricity:
0000618
Arg of perigee: 342
6189 deg
Mean anomaly: 17
4932 deg
Mean motion: 15
49123437 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3942
Checksum: 293
Coasting Arc #6 (Orbit 3957)
---------------------------------------
Vector Time (GMT): 2020/217/23:32:45
000
Vector Time (MET): N/A
Weight (LBS) : 956773
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3847236
96 A = 6799908
47 meter
Y = 4671397
02 meter E =
0012954
Z = 3087448
68 I = 52
02573
XDOT = -2481
130113 Wp = 81
22050
YDOT = -5313
877767 meter/sec RA = 106
00663 deg
ZDOT = 4932
634921 TA = 313
98463
MA = 314
09136
Ha = 228
885 n
mi
Hp = 222
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12622168
52 X = -3914184
65
Y = 15326105
72 feet Y = 4627999
97 meter
Z = 10129424
81 Z = 3068598
47
XDOT = -8140
190659 XDOT = -2445
483612
YDOT = -17433
982176 feet/sec YDOT = -5341
424496 meter/sec
ZDOT = 16183
185436 ZDOT = 4920
669170
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19864838
08 X = -6054802
65
Y = -1164359
35 feet Y = -354896
73 meter
Z = 10042229
68 Z = 3060871
61
XDOT = 9088
986130 XDOT = 2770
322972
YDOT = -15516
857756 feet/sec YDOT = -4729
538244 meter/sec
ZDOT = 16128
111858 ZDOT = 4915
848494
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
03930722
00016717 00000-0 10270-3 0 9051
2 25544 51
6438 106
6860 0000662 346
5801 13
5331 15
49144581 39580
Satellite: ISS
Catalog Number: 25544
Epoch time: 20218
03930722 = yrday
fracday
Element set: 905
Inclination: 51
6438 deg
RA of node: 106
6860 deg
Eccentricity:
0000662
Arg of perigee: 346
5801 deg
Mean anomaly: 13
5331 deg
Mean motion: 15
49144581 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3958
Checksum: 295
Coasting Arc #7 (Orbit 3972)
---------------------------------------
Vector Time (GMT): 2020/218/23:32:45
000
Vector Time (MET): N/A
Weight (LBS) : 956773
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3466531
64 A = 6799792
89 meter
Y = -4935626
49 meter E =
0004300
Z = -3143251
05 I = 52
03287
XDOT = 2882
659363 Wp = 95
52042
YDOT = 5135
103657 meter/sec RA = 101
08535 deg
ZDOT = -4890
301100 TA = 120
36897
MA = 120
32645
Ha = 228
876 n
mi
Hp = 222
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11373135
30 X = 3536733
39
Y = -16193000
29 feet Y = -4896468
62 meter
Z = -10312503
43 Z = -3126242
08
XDOT = 9457
543842 XDOT = 2848
776549
YDOT = 16847
452942 feet/sec YDOT = 5167
150332 meter/sec
ZDOT = -16044
294946 ZDOT = -4876
380731
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19816535
11 X = 6040079
90
Y = -695449
91 feet Y = -211973
13 meter
Z = -10233790
97 Z = -3119259
49
XDOT = -7667
669494 XDOT = -2337
105662
YDOT = 16368
337702 feet/sec YDOT = 4989
069332 meter/sec
ZDOT = -15980
193766 ZDOT = -4870
763060
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
00694970
00016717 00000-0 10270-3 0 9062
2 25544 51
6432 101
8989 0000750 353
4506 6
6634 15
49132132 39735
Satellite: ISS
Catalog Number: 25544
Epoch time: 20219
00694970 = yrday
fracday
Element set: 906
Inclination: 51
6432 deg
RA of node: 101
8989 deg
Eccentricity:
0000750
Arg of perigee: 353
4506 deg
Mean anomaly: 6
6634 deg
Mean motion: 15
49132132 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3973
Checksum: 301
Coasting Arc #8 (Orbit 3975)
---------------------------------------
Vector Time (GMT): 2020/219/03:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 956773
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3473959
83 A = 6793212
47 meter
Y = -2935494
24 meter E =
0006618
Z = 5042934
09 I = 52
01116
XDOT = 2829
713156 Wp = 50
07205
YDOT = -6828
564765 meter/sec RA = 100
18749 deg
ZDOT = -2019
705029 TA = 59
49882
MA = 59
43350
Ha = 229
053 n
mi
Hp = 222
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11397506
01 X = -3465371
16
Y = -9630886
61 feet Y = -2974294
68 meter
Z = 16545059
34 Z = 5026080
13
XDOT = 9283
835815 XDOT = 2915
672236
YDOT = -22403
427707 feet/sec YDOT = -6796
440198 meter/sec
ZDOT = -6626
328836 ZDOT = -2005
751167
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13039041
54 X = -3974299
86
Y = -7430097
57 feet Y = -2264693
74 meter
Z = 16467335
98 Z = 5019244
01
XDOT = 4655
015061 XDOT = 1418
848591
YDOT = -22754
643326 feet/sec YDOT = -6935
615286 meter/sec
ZDOT = -6561
655867 ZDOT = -1999
992708
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
20047697
00016717 00000-0 10270-3 0 9073
2 25544 51
6421 100
9422 0001005 8
8136 351
3032 15
49148893 39765
Satellite: ISS
Catalog Number: 25544
Epoch time: 20219
20047697 = yrday
fracday
Element set: 907
Inclination: 51
6421 deg
RA of node: 100
9422 deg
Eccentricity:
0001005
Arg of perigee: 8
8136 deg
Mean anomaly: 351
3032 deg
Mean motion: 15
49148893 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3976
Checksum: 292
Coasting Arc #9 (Orbit 3990)
---------------------------------------
Vector Time (GMT): 2020/220/03:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 956773
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3702605
42 A = 6793378
54 meter
Y = 2680639
67 meter E =
0012639
Z = -5036853
25 I = 52
01555
XDOT = -2266
357280 Wp = 100
21237
YDOT = 7008
768745 meter/sec RA = 95
26633 deg
ZDOT = 2066
326358 TA = 189
81555
MA = 189
84026
Ha = 229
029 n
mi
Hp = 222
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12147655
59 X = 3696820
17
Y = 8794749
57 feet Y = 2722012
60 meter
Z = -16525109
08 Z = -5018881
81
XDOT = -7435
555379 XDOT = -2354
599814
YDOT = 22994
648112 feet/sec YDOT = 6982
931283 meter/sec
ZDOT = 6779
285950 ZDOT = 2055
103321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13737768
46 X = 4187271
83
Y = 6238553
12 feet Y = 1901510
99 meter
Z = -16442218
80 Z = -5011588
29
XDOT = -2406
414928 XDOT = -733
475270
YDOT = 23009
838241 feet/sec YDOT = 7013
398696 meter/sec
ZDOT = 6727
204061 ZDOT = 2050
451798
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
16811719
00016717 00000-0 10270-3 0 9085
2 25544 51
6415 96
1553 0001100 12
0851 348
0325 15
49117078 39912
Satellite: ISS
Catalog Number: 25544
Epoch time: 20220
16811719 = yrday
fracday
Element set: 908
Inclination: 51
6415 deg
RA of node: 96
1553 deg
Eccentricity:
0001100
Arg of perigee: 12
0851 deg
Mean anomaly: 348
0325 deg
Mean motion: 15
49117078 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3991
Checksum: 281
Coasting Arc #10 (Orbit 4006)
---------------------------------------
Vector Time (GMT): 2020/221/03:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 956773
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3895952
36 A = 6793396
13 meter
Y = -2420556
26 meter E =
0006985
Z = 5008048
80 I = 52
01622
XDOT = 1705
009723 Wp = 50
54178
YDOT = -7160
894069 meter/sec RA = 90
34445 deg
ZDOT = -2128
414025 TA = 60
12785
MA = 60
05846
Ha = 229
098 n
mi
Hp = 222
452
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12781995
92 X = -3892921
25
Y = -7941457
53 feet Y = -2464106
70 meter
Z = 16430606
31 Z = 4989131
44
XDOT = 5593
863920 XDOT = 1795
296710
YDOT = -23493
746947 feet/sec YDOT = -7141
322578 meter/sec
ZDOT = -6982
985646 ZDOT = -2119
912699
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14281879
79 X = -4353116
96
Y = -5033296
86 feet Y = -1534148
88 meter
Z = 16343341
88 Z = 4981450
61
XDOT = 176
655800 XDOT = 53
844688
YDOT = -23114
343593 feet/sec YDOT = -7045
251927 meter/sec
ZDOT = -6943
452392 ZDOT = -2116
364289
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
20026572
00016717 00000-0 10270-3 0 9097
2 25544 51
6400 91
0483 0001102 10
1694 349
9478 15
49140761 40071
Satellite: ISS
Catalog Number: 25544
Epoch time: 20221
20026572 = yrday
fracday
Element set: 909
Inclination: 51
6400 deg
RA of node: 91
0483 deg
Eccentricity:
0001102
Arg of perigee: 10
1694 deg
Mean anomaly: 349
9478 deg
Mean motion: 15
49140761 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4007
Checksum: 272
Coasting Arc #11 (Orbit 4021)
---------------------------------------
Vector Time (GMT): 2020/222/03:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 956773
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4087940
02 A = 6793533
18 meter
Y = 2132276
44 meter E =
0012451
Z = -5000724
95 I = 52
01593
XDOT = -1123
325739 Wp = 100
47579
YDOT = 7248
356028 meter/sec RA = 85
42312 deg
ZDOT = 2174
764943 TA = 190
65165
MA = 190
67804
Ha = 229
062 n
mi
Hp = 222
561
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13411876
71 X = 4088082
80
Y = 6995657
60 feet Y = 2177991
57 meter
Z = -16406577
92 Z = -4980867
22
XDOT = -3685
451899 XDOT = -1214
859168
YDOT = 23780
695630 feet/sec YDOT = 7235
282371 meter/sec
ZDOT = 7135
055587 ZDOT = 2169
086119
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14763466
25 X = 4499904
51
Y = 3722293
62 feet Y = 1134555
10 meter
Z = -16314964
17 Z = -4972801
08
XDOT = 2065
802292 XDOT = 629
656539
YDOT = 22928
888801 feet/sec YDOT = 6988
725306 meter/sec
ZDOT = 7108
537018 ZDOT = 2166
682083
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
16790456
00016717 00000-0 10270-3 0 9104
2 25544 51
6405 86
2610 0001166 15
9601 344
1586 15
49119709 40227
Satellite: ISS
Catalog Number: 25544
Epoch time: 20222
16790456 = yrday
fracday
Element set: 910
Inclination: 51
6405 deg
RA of node: 86
2610 deg
Eccentricity:
0001166
Arg of perigee: 15
9601 deg
Mean anomaly: 344
1586 deg
Mean motion: 15
49119709 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4022
Checksum: 285
Coasting Arc #12 (Orbit 4037)
---------------------------------------
Vector Time (GMT): 2020/223/03:44:00
000
Vector Time (MET): N/A
Weight (LBS) : 956773
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4243922
94 A = 6793547
85 meter
Y = -1846295
54 meter E =
0007426
Z = 4969763
54 I = 52
01266
XDOT = 549
764484 Wp = 51
55401
YDOT = -7307
732295 meter/sec RA = 80
50099 deg
ZDOT = -2238
646312 TA = 60
24038
MA = 60
16653
Ha = 229
150 n
mi
Hp = 222
395
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13923631
68 X = -4247101
73
Y = -6057400
07 feet Y = -1893771
99 meter
Z = 16304998
49 Z = 4949140
66
XDOT = 1803
689252 XDOT = 642
314836
YDOT = -23975
499654 feet/sec YDOT = -7301
066908 meter/sec
ZDOT = -7344
640131 ZDOT = -2235
751158
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15090873
32 X = -4599698
19
Y = -2432916
44 feet Y = -741552
93 meter
Z = 16209844
24 Z = 4940760
53
XDOT = -4255
140141 XDOT = -1296
966715
YDOT = -22598
729608 feet/sec YDOT = -6888
092784 meter/sec
ZDOT = -7330
956270 ZDOT = -2234
475471
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
20004963
00016717 00000-0 10270-3 0 9112
2 25544 51
6407 81
1539 0001219 15
4502 344
6685 15
49147152 40382
Satellite: ISS
Catalog Number: 25544
Epoch time: 20223
20004963 = yrday
fracday
Element set: 911
Inclination: 51
6407 deg
RA of node: 81
1539 deg
Eccentricity:
0001219
Arg of perigee: 15
4502 deg
Mean anomaly: 344
6685 deg
Mean motion: 15
49147152 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4038
Checksum: 278
Coasting Arc #13 (Orbit 4043)
---------------------------------------
Vector Time (GMT): 2020/223/13:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 956773
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3828055
66 A = 6797923
64 meter
Y = -4179589
61 meter E =
0011944
Z = 3745626
26 I = 52
02710
XDOT = 2235
973274 Wp = 77
92522
YDOT = -5925
459221 meter/sec RA = 78
56632 deg
ZDOT = -4312
774618 TA = 57
69489
MA = 57
57927
Ha = 228
960 n
mi
Hp = 222
455
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12559237
74 X = -3799227
69
Y = -13712564
35 feet Y = -4222236
57 meter
Z = 12288800
07 Z = 3727101
14
XDOT = 7335
870323 XDOT = 2323
016169
YDOT = -19440
483010 feet/sec YDOT = -5899
968178 meter/sec
ZDOT = -14149
523026 ZDOT = -4301
701960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5801182
85 X = 1768200
53
Y = 17725853
19 feet Y = 5402840
05 meter
Z = 12203437
51 Z = 3719607
75
XDOT = -13546
727843 XDOT = -4129
042647
YDOT = 14171
276733 feet/sec YDOT = 4319
405148 meter/sec
ZDOT = -14098
130163 ZDOT = -4297
110074
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
58710165
00016717 00000-0 10270-3 0 9122
2 25544 51
6426 79
2380 0001363 2
5426 357
5730 15
49178848 40444
Satellite: ISS
Catalog Number: 25544
Epoch time: 20223
58710165 = yrday
fracday
Element set: 912
Inclination: 51
6426 deg
RA of node: 79
2380 deg
Eccentricity:
0001363
Arg of perigee: 2
5426 deg
Mean anomaly: 357
5730 deg
Mean motion: 15
49178848 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4044
Checksum: 300
Coasting Arc #14 (Orbit 4058)
---------------------------------------
Vector Time (GMT): 2020/224/13:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 956773
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4166502
06 A = 6798094
32 meter
Y = 3878258
94 meter E =
0005834
Z = -3721541
77 I = 52
01754
XDOT = -1758
615810 Wp = 88
52814
YDOT = 6051
919425 meter/sec RA = 73
64403 deg
ZDOT = 4343
907933 TA = 227
50275
MA = 227
55206
Ha = 229
029 n
mi
Hp = 222
481
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13669626
18 X = 4140901
55
Y = 12723946
65 feet Y = 3924708
74 meter
Z = -12209782
72 Z = -3701364
70
XDOT = -5769
736910 XDOT = -1847
259562
YDOT = 19855
378690 feet/sec YDOT = 6031
757522 meter/sec
ZDOT = 14251
666446 ZDOT = 4335
150254
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7517780
66 X = -2291419
55
Y = -17161081
06 feet Y = -5230697
51 meter
Z = -12116788
48 Z = -3693197
13
XDOT = 12065
774626 XDOT = 3677
648106
YDOT = -15305
429519 feet/sec YDOT = -4665
094918 meter/sec
ZDOT = 14210
942778 ZDOT = 4331
495359
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 20224
55473777
00016717 00000-0 10270-3 0 9136
2 25544 51
6406 74
4501 0001184 14
4450 345
6734 15
49150430 40599
Satellite: ISS
Catalog Number: 25544
Epoch time: 20224
55473777 = yrday
fracday
Element set: 913
Inclination: 51
6406 deg
RA of node: 74
4501 deg
Eccentricity:
0001184
Arg of perigee: 14
4450 deg
Mean anomaly: 345
6734 deg
Mean motion: 15
49150430 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4059
Checksum: 289
Coasting Arc #15 (Orbit 4074)
---------------------------------------
Vector Time (GMT): 2020/225/13:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 956773
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4465177
41 A = 6798221
61 meter
Y = -3573680
66 meter E =
0012186
Z = 3666669
95 I = 52
00803
XDOT = 1293
204528 Wp = 80
33938
YDOT = -6141
143146 meter/sec RA = 68
72160 deg
ZDOT = -4396
161409 TA = 56
43750
MA = 56
32119
Ha = 229
011 n
mi
Hp = 222
446
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14649532
20 X = -4442694
06
Y = -11724674
10 feet Y = -3623487
96 meter
Z = 12029757
05 Z = 3645034
42
XDOT = 4242
797007 XDOT = 1383
134414
YDOT = -20148
107436 feet/sec YDOT = -6126
178540 meter/sec
ZDOT = -14423
101736 ZDOT = -4389
661481
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9099227
34 X = 2773444
49
Y = 16482428
61 feet Y = 5023844
24 meter
Z = 11930022
64 Z = 3636270
90
XDOT = -10544
277774 XDOT = -3213
895866
YDOT = 16273
063861 feet/sec YDOT = 4960
029865 meter/sec
ZDOT = -14392
784137 ZDOT = -4386
920605
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
58688030
00016717 00000-0 10270-3 0 9141
2 25544 51
6412 69
3434 0001202 7
6736 352
4432 15
49165396 40752
Satellite: ISS
Catalog Number: 25544
Epoch time: 20225
58688030 = yrday
fracday
Element set: 914
Inclination: 51
6412 deg
RA of node: 69
3434 deg
Eccentricity:
0001202
Arg of perigee: 7
6736 deg
Mean anomaly: 352
4432 deg
Mean motion: 15
49165396 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4075
Checksum: 297
Coasting Arc #16 (Orbit 4089)
---------------------------------------
Vector Time (GMT): 2020/226/13:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 956773
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4756146
83 A = 6798340
42 meter
Y = 3220491
03 meter E =
0005760
Z = -3641248
90 I = 51
99453
XDOT = -808
390435 Wp = 86
56062
YDOT = 6191
849549 meter/sec RA = 63
79757 deg
ZDOT = 4426
822171 TA = 230
63483
MA = 230
68587
Ha = 229
070 n
mi
Hp = 222
428
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15604156
28 X = 4737467
81
Y = 10565915
46 feet Y = 3273573
48 meter
Z = -11946354
67 Z = -3618190
73
XDOT = -2652
199589 XDOT = -899
072264
YDOT = 20314
467023 feet/sec YDOT = 6182
302206 meter/sec
ZDOT = 14523
694786 ZDOT = 4422
675542
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10694986
31 X = -3259831
83
Y = -15597254
85 feet Y = -4754043
28 meter
Z = -11840040
61 Z = -3608844
38
XDOT = 8898
755419 XDOT = 2712
340652
YDOT = -17096
155735 feet/sec YDOT = -5210
908268 meter/sec
ZDOT = 14504
226885 ZDOT = 4420
888354
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
55451474
00016717 00000-0 10270-3 0 9150
2 25544 51
6408 64
5552 0001120 23
3404 336
7796 15
49154796 40908
Satellite: ISS
Catalog Number: 25544
Epoch time: 20226
55451474 = yrday
fracday
Element set: 915
Inclination: 51
6408 deg
RA of node: 64
5552 deg
Eccentricity:
0001120
Arg of perigee: 23
3404 deg
Mean anomaly: 336
7796 deg
Mean motion: 15
49154796 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4090
Checksum: 302
Coasting Arc #17 (Orbit 4105)
---------------------------------------
Vector Time (GMT): 2020/227/13:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 956773
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5006850
92 A = 6798508
86 meter
Y = -2871491
28 meter E =
0012605
Z = 3583232
24 I = 51
97926
XDOT = 343
191792 Wp = 82
51744
YDOT = -6207
214308 meter/sec RA = 58
87317 deg
ZDOT = -4479
655361 TA = 55
45259
MA = 55
33368
Ha = 229
115 n
mi
Hp = 222
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16426676
24 X = -4991774
02
Y = -9420903
16 feet Y = -2927397
45 meter
Z = 11756011
27 Z = 3558947
58
XDOT = 1125
957324 XDOT = 434
336574
YDOT = -20364
876338 feet/sec YDOT = -6202
866515 meter/sec
ZDOT = -14697
032023 ZDOT = -4477
767408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12133428
21 X = 3698268
92
Y = 14628383
67 feet Y = 4458731
34 meter
Z = 11644020
81 Z = 3549097
54
XDOT = -7250
792119 XDOT = -2210
041438
YDOT = 17745
325621 feet/sec YDOT = 5408
775249 meter/sec
ZDOT = -14687
980332 ZDOT = -4476
896405
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
58665389
00016717 00000-0 10270-3 0 9167
2 25544 51
6409 59
4483 0001168 21
1226 338
9972 15
49157533 41065
Satellite: ISS
Catalog Number: 25544
Epoch time: 20227
58665389 = yrday
fracday
Element set: 916
Inclination: 51
6409 deg
RA of node: 59
4483 deg
Eccentricity:
0001168
Arg of perigee: 21
1226 deg
Mean anomaly: 338
9972 deg
Mean motion: 15
49157533 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4106
Checksum: 326
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