[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 10th 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16491 3871 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 70 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 865 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
100/08:05:06
000 0
0 0
0 0
0
N/A 0
0 0
0 230
7
000/00:00:00
000 0
0 0
0 221
9
100/14:16:50
000 0
0 0
0 0
0
N/A 0
0 0
0 230
8
000/00:00:00
000 0
0 0
0 222
0
108/01:53:00
000 0
0 0
0 0
0
N/A 0
0 0
0 230
5
000/00:00:00
000 0
0 0
0 222
1
110/05:09:33
438 0
9 -3
1 3
1
N/A -2
9 -0
0 228
5
000/00:01:02
876 0
6 -0
0 222
2
113/03:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
6
000/00:00:00
000 0
0 0
0 222
3
Coasting Arc #1 (Orbit 2120)
---------------------------------------
Vector Time (GMT): 2020/099/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 921212
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2549012
49 A = 6793318
96 meter
Y = 3420846
99 meter E =
0006499
Z = 5281340
95 I = 51
44759
XDOT = -6551
237994 Wp = 102
34464
YDOT = 3930
964282 meter/sec RA = 332
70534 deg
ZDOT = 613
742779 TA = 341
76684
MA = 341
79013
Ha = 230
838 n
mi
Hp = 221
864
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8362901
86 X = 2484916
15
Y = 11223251
29 feet Y = 3448993
94 meter
Z = 17327234
08 Z = 5293567
19
XDOT = -21493
562974 XDOT = -6597
689536
YDOT = 12896
864442 feet/sec YDOT = 3857
444002 meter/sec
ZDOT = 2013
591795 ZDOT = 581
805979
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11064999
86 X = 3372611
96
Y = 8457425
44 feet Y = 2577823
27 meter
Z = 17383045
51 Z = 5298352
27
XDOT = -16403
344591 XDOT = -4999
739431
YDOT = 17610
208619 feet/sec YDOT = 5367
591587 meter/sec
ZDOT = 1866
885073 ZDOT = 569
026570
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 20099
54939684
00016717 00000-0 10270-3 0 9005
2 25544 51
6438 333
0809 0003728 94
9762 265
1813 15
48694245 21212
Satellite: ISS
Catalog Number: 25544
Epoch time: 20099
54939684 = yrday
fracday
Element set: 900
Inclination: 51
6438 deg
RA of node: 333
0809 deg
Eccentricity:
0003728
Arg of perigee: 94
9762 deg
Mean anomaly: 265
1813 deg
Mean motion: 15
48694245 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2121
Checksum: 331
Coasting Arc #2 (Orbit 2133)
---------------------------------------
Vector Time (GMT): 2020/100/08:05:06
000
Vector Time (MET): N/A
Weight (LBS) : 921212
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3806464
72 A = 6794101
83 meter
Y = 2418133
31 meter E =
0008616
Z = 5075720
40 I = 51
42416
XDOT = -5526
561748 Wp = 113
65642
YDOT = 5013
942427 meter/sec RA = 328
56580 deg
ZDOT = 1750
112007 TA = 319
32928
MA = 319
39360
Ha = 230
718 n
mi
Hp = 221
857
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12488401
32 X = 3754486
29
Y = 7933508
24 feet Y = 2460409
61 meter
Z = 16652625
99 Z = 5094084
53
XDOT = -18131
764266 XDOT = -5590
719535
YDOT = 16449
942346 feet/sec YDOT = 4951
781868 meter/sec
ZDOT = 5741
837293 ZDOT = 1723
109652
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3988013
60 X = 1215546
55
Y = 14148890
93 feet Y = 4312581
96 meter
Z = 16736645
59 Z = 5101329
58
XDOT = -23477
708709 XDOT = -7156
005615
YDOT = -49
907778 feet/sec YDOT = -15
211891 meter/sec
ZDOT = 5617
686903 ZDOT = 1712
270968
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 20100
38826202
00016717 00000-0 10270-3 0 9012
2 25544 51
6420 328
9331 0003636 98
8886 261
2675 15
48723244 21343
Satellite: ISS
Catalog Number: 25544
Epoch time: 20100
38826202 = yrday
fracday
Element set: 901
Inclination: 51
6420 deg
RA of node: 328
9331 deg
Eccentricity:
0003636
Arg of perigee: 98
8886 deg
Mean anomaly: 261
2675 deg
Mean motion: 15
48723244 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2134
Checksum: 299
Coasting Arc #3 (Orbit 2137)
---------------------------------------
Vector Time (GMT): 2020/100/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 937130
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3842233
20 A = 6794283
83 meter
Y = 2350104
82 meter E =
0008608
Z = 5080970
08 I = 51
41484
XDOT = -5428
984292 Wp = 113
87037
YDOT = 5126
636311 meter/sec RA = 327
28355 deg
ZDOT = 1728
432920 TA = 319
32950
MA = 319
39376
Ha = 230
836 n
mi
Hp = 221
959
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12605751
98 X = 3790987
32
Y = 7710317
67 feet Y = 2392785
17 meter
Z = 16669849
36 Z = 5099509
78
XDOT = -17811
628254 XDOT = -5494
304205
YDOT = 16819
672937 feet/sec YDOT = 5065
560420 meter/sec
ZDOT = 5670
711681 ZDOT = 1701
901760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13803155
87 X = 4207201
91
Y = -4999153
21 feet Y = -1523741
90 meter
Z = 16754677
39 Z = 5106825
67
XDOT = 1727
818172 XDOT = 526
638979
YDOT = 23430
033846 feet/sec YDOT = 7141
474316 meter/sec
ZDOT = 5548
716085 ZDOT = 1691
248663
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 20100
64637517
00016717 00000-0 10270-3 0 9021
2 25544 51
6402 327
6548 0003667 99
6164 260
5400 15
48653212 21380
Satellite: ISS
Catalog Number: 25544
Epoch time: 20100
64637517 = yrday
fracday
Element set: 902
Inclination: 51
6402 deg
RA of node: 327
6548 deg
Eccentricity:
0003667
Arg of perigee: 99
6164 deg
Mean anomaly: 260
5400 deg
Mean motion: 15
48653212 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2138
Checksum: 295
Coasting Arc #4 (Orbit 2152)
---------------------------------------
Vector Time (GMT): 2020/101/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 937130
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4110786
68 A = 6794283
15 meter
Y = -1937206
93 meter E =
0016546
Z = -5065724
97 I = 51
38717
XDOT = 4877
416260 Wp = 82
14422
YDOT = -5601
714512 meter/sec RA = 322
32350 deg
ZDOT = -1818
711005 TA = 170
15133
MA = 170
11886
Ha = 230
889 n
mi
Hp = 221
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13486832
95 X = -4064212
04
Y = -6355665
78 feet Y = -1982916
40 meter
Z = -16619832
59 Z = -5085580
64
XDOT = 16002
021850 XDOT = 4948
528156
YDOT = -18378
328452 feet/sec YDOT = -5546
774213 meter/sec
ZDOT = -5966
899623 ZDOT = -1794
845255
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13174814
70 X = -4015683
52
Y = 6759002
52 feet Y = 2060143
97 meter
Z = -16710718
97 Z = -5093427
14
XDOT = -4355
779022 XDOT = -1327
641446
YDOT = -22947
780399 feet/sec YDOT = -6994
483465 meter/sec
ZDOT = -5857
097757 ZDOT = -1785
243396
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 20101
61429372
00016717 00000-0 10270-3 0 9038
2 25544 51
6397 322
8679 0003704 104
1742 255
9819 15
48694289 21539
Satellite: ISS
Catalog Number: 25544
Epoch time: 20101
61429372 = yrday
fracday
Element set: 903
Inclination: 51
6397 deg
RA of node: 322
8679 deg
Eccentricity:
0003704
Arg of perigee: 104
1742 deg
Mean anomaly: 255
9819 deg
Mean motion: 15
48694289 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2153
Checksum: 321
Coasting Arc #5 (Orbit 2168)
---------------------------------------
Vector Time (GMT): 2020/102/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 937130
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4328164
87 A = 6794501
31 meter
Y = 1470636
53 meter E =
0009253
Z = 5020893
17 I = 51
36183
XDOT = -4296
272053 Wp = 116
52057
YDOT = 6047
897514 meter/sec RA = 317
36222 deg
ZDOT = 1925
254661 TA = 314
68250
MA = 314
75785
Ha = 230
808 n
mi
Hp = 221
951
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14200015
97 X = 4287009
23
Y = 4824923
01 feet Y = 1518807
05 meter
Z = 16472746
61 Z = 5041817
94
XDOT = -14095
380752 XDOT = -4372
934002
YDOT = 19842
183445 feet/sec YDOT = 5999
424905 meter/sec
ZDOT = 6316
452301 ZDOT = 1904
198631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12249176
61 X = 3733549
03
Y = -8468296
19 feet Y = -2581136
68 meter
Z = 16568565
07 Z = 5050098
63
XDOT = 6950
328855 XDOT = 2118
460235
YDOT = 22265
683730 feet/sec YDOT = 6786
580401 meter/sec
ZDOT = 6219
506192 ZDOT = 1895
705487
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 20102
64674026
00016717 00000-0 10270-3 0 9041
2 25544 51
6398 317
7624 0003721 106
1159 254
0401 15
48662392 21690
Satellite: ISS
Catalog Number: 25544
Epoch time: 20102
64674026 = yrday
fracday
Element set: 904
Inclination: 51
6398 deg
RA of node: 317
7624 deg
Eccentricity:
0003721
Arg of perigee: 106
1159 deg
Mean anomaly: 254
0401 deg
Mean motion: 15
48662392 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2169
Checksum: 295
Coasting Arc #6 (Orbit 2183)
---------------------------------------
Vector Time (GMT): 2020/103/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 937130
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4500358
62 A = 6794515
55 meter
Y = -1008722
25 meter E =
0016126
Z = -5003999
10 I = 51
33800
XDOT = 3667
081351 Wp = 83
09928
YDOT = -6402
244105 meter/sec RA = 312
39962 deg
ZDOT = -2011
123522 TA = 167
23936
MA = 167
19850
Ha = 230
926 n
mi
Hp = 221
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14764956
11 X = -4464437
61
Y = -3309456
20 feet Y = -1058847
55 meter
Z = -16417319
88 Z = -5025772
98
XDOT = 12031
106795 XDOT = 3748
169539
YDOT = -21004
737876 feet/sec YDOT = -6360
782776 meter/sec
ZDOT = -6598
174284 ZDOT = -1993
113295
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11194984
17 X = -3412231
18
Y = 10017174
58 feet Y = 3053234
81 meter
Z = -16517062
82 Z = -5034400
75
XDOT = -9377
770059 XDOT = -2858
344314
YDOT = -21203
153083 feet/sec YDOT = -6462
721060 meter/sec
ZDOT = -6515
173664 ZDOT = -1985
824933
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 20103
61465662
00016717 00000-0 10270-3 0 9054
2 25544 51
6395 312
9766 0003921 111
1123 249
0446 15
48700093 21841
Satellite: ISS
Catalog Number: 25544
Epoch time: 20103
61465662 = yrday
fracday
Element set: 905
Inclination: 51
6395 deg
RA of node: 312
9766 deg
Eccentricity:
0003921
Arg of perigee: 111
1123 deg
Mean anomaly: 249
0446 deg
Mean motion: 15
48700093 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2184
Checksum: 289
Coasting Arc #7 (Orbit 2199)
---------------------------------------
Vector Time (GMT): 2020/104/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 937130
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4614508
28 A = 6794707
88 meter
Y = 500741
09 meter E =
0009884
Z = 4956357
65 I = 51
31623
XDOT = -3011
583821 Wp = 119
68831
YDOT = 6722
138912 meter/sec RA = 307
43533 deg
ZDOT = 2116
733370 TA = 309
54721
MA = 309
63451
Ha = 230
743 n
mi
Hp = 221
965
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15139462
86 X = 4584490
69
Y = 1642851
33 feet Y = 552175
89 meter
Z = 16261015
92 Z = 4978700
27
XDOT = -9880
524348 XDOT = -3096
810839
YDOT = 22054
261523 feet/sec YDOT = 6687
984674 meter/sec
ZDOT = 6944
663287 ZDOT = 2101
897345
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9859411
00 X = 3005148
47
Y = -11460979
16 feet Y = -3493306
45 meter
Z = 16363401
42 Z = 4987564
75
XDOT = 11730
677244 XDOT = 3575
510424
YDOT = 19946
140616 feet/sec YDOT = 6079
583660 meter/sec
ZDOT = 6876
202113 ZDOT = 2095
866404
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 20104
64710126
00016717 00000-0 10270-3 0 9067
2 25544 51
6389 307
8714 0003767 115
3642 244
7898 15
48682902 22000
Satellite: ISS
Catalog Number: 25544
Epoch time: 20104
64710126 = yrday
fracday
Element set: 906
Inclination: 51
6389 deg
RA of node: 307
8714 deg
Eccentricity:
0003767
Arg of perigee: 115
3642 deg
Mean anomaly: 244
7898 deg
Mean motion: 15
48682902 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2200
Checksum: 311
Coasting Arc #8 (Orbit 2214)
---------------------------------------
Vector Time (GMT): 2020/105/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 937130
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4682144
05 A = 6794745
07 meter
Y = -11085
68 meter E =
0015394
Z = -4937911
47 I = 51
29907
XDOT = 2330
776931 Wp = 83
99388
YDOT = -6944
207598 meter/sec RA = 302
47009 deg
ZDOT = -2198
826718 TA = 164
41265
MA = 164
36520
Ha = 230
852 n
mi
Hp = 221
743
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15361365
01 X = -4657686
59
Y = -36370
35 feet Y = -63307
95 meter
Z = -16200496
95 Z = -4960596
06
XDOT = 7646
905941 XDOT = 2418
936512
YDOT = -22782
833327 feet/sec YDOT = -6917
650242 meter/sec
ZDOT = -7213
998418 ZDOT = -2187
290670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8443443
50 X = -2573561
58
Y = 12700435
23 feet Y = 3871092
66 meter
Z = -16304483
00 Z = -4969606
42
XDOT = -13832
643159 XDOT = -4216
189635
YDOT = -18370
550972 feet/sec YDOT = -5599
343936 meter/sec
ZDOT = -7160
663572 ZDOT = -2182
570257
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 20105
61501585
00016717 00000-0 10270-3 0 9073
2 25544 51
6408 303
0861 0003911 118
5504 241
6040 15
48713824 22155
Satellite: ISS
Catalog Number: 25544
Epoch time: 20105
61501585 = yrday
fracday
Element set: 907
Inclination: 51
6408 deg
RA of node: 303
0861 deg
Eccentricity:
0003911
Arg of perigee: 118
5504 deg
Mean anomaly: 241
6040 deg
Mean motion: 15
48713824 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2215
Checksum: 272
Coasting Arc #9 (Orbit 2230)
---------------------------------------
Vector Time (GMT): 2020/106/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 937130
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4685539
16 A = 6794896
15 meter
Y = -513553
38 meter E =
0010426
Z = 4888409
52 I = 51
28196
XDOT = -1629
682879 Wp = 121
74227
YDOT = 7125
980208 meter/sec RA = 297
50238 deg
ZDOT = 2301
649745 TA = 305
57024
MA = 305
66737
Ha = 230
655 n
mi
Hp = 221
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15372503
79 X = 4667188
62
Y = -1684886
42 feet Y = -461258
93 meter
Z = 16038088
99 Z = 4911125
39
XDOT = -5346
728605 XDOT = -1720
426632
YDOT = 23379
200159 feet/sec YDOT = 7107
248563 meter/sec
ZDOT = 7551
344307 ZDOT = 2293
512990
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6778456
66 X = 2066073
59
Y = -13778725
01 feet Y = -4199755
38 meter
Z = 16142251
27 Z = 4920158
19
XDOT = 15815
774594 XDOT = 4820
648096
YDOT = 16617
479859 feet/sec YDOT = 5065
007861 meter/sec
ZDOT = 7513
597096 ZDOT = 2290
144395
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 20106
64745579
00016717 00000-0 10270-3 0 9081
2 25544 51
6402 297
9803 0003802 122
9612 237
1903 15
48715419 22312
Satellite: ISS
Catalog Number: 25544
Epoch time: 20106
64745579 = yrday
fracday
Element set: 908
Inclination: 51
6402 deg
RA of node: 297
9803 deg
Eccentricity:
0003802
Arg of perigee: 122
9612 deg
Mean anomaly: 237
1903 deg
Mean motion: 15
48715419 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2231
Checksum: 307
Coasting Arc #10 (Orbit 2245)
---------------------------------------
Vector Time (GMT): 2020/107/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 937130
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4645762
02 A = 6795028
86 meter
Y = 1007524
86 meter E =
0014652
Z = -4868536
80 I = 51
26814
XDOT = 925
089444 Wp = 84
93550
YDOT = -7209
640532 meter/sec RA = 292
53554 deg
ZDOT = -2379
721188 TA = 161
58439
MA = 161
53130
Ha = 230
803 n
mi
Hp = 221
813
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15242001
36 X = -4633034
71
Y = 3305527
76 feet Y = 955643
72 meter
Z = -15972889
77 Z = -4891073
10
XDOT = 3035
070355 XDOT = 1017
200298
YDOT = -23653
676285 feet/sec YDOT = -7198
780542 meter/sec
ZDOT = -7807
484214 ZDOT = -2375
003637
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5090725
98 X = -1551653
28
Y = 14629313
14 feet Y = 4459014
65 meter
Z = -16076256
81 Z = -4900043
08
XDOT = -17486
719260 XDOT = -5329
952031
YDOT = -14622
759188 feet/sec YDOT = -4457
017000 meter/sec
ZDOT = -7785
424390 ZDOT = -2372
997354
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 20107
61536837
00016717 00000-0 10270-3 0 9095
2 25544 51
6404 293
1959 0003933 125
1706 234
9812 15
48714591 22468
Satellite: ISS
Catalog Number: 25544
Epoch time: 20107
61536837 = yrday
fracday
Element set: 909
Inclination: 51
6404 deg
RA of node: 293
1959 deg
Eccentricity:
0003933
Arg of perigee: 125
1706 deg
Mean anomaly: 234
9812 deg
Mean motion: 15
48714591 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2246
Checksum: 317
Coasting Arc #11 (Orbit 2253)
---------------------------------------
Vector Time (GMT): 2020/108/01:53:00
000
Vector Time (MET): N/A
Weight (LBS) : 922021
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4613639
68 A = 6795469
18 meter
Y = -1529503
06 meter E =
0011071
Z = 4743054
65 I = 51
26269
XDOT = -362
152941 Wp = 119
86072
YDOT = 7178
945256 meter/sec RA = 290
13861 deg
ZDOT = 2657
180513 TA = 303
69417
MA = 303
79967
Ha = 230
548 n
mi
Hp = 222
060
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15136613
12 X = 4607361
19
Y = -5018054
64 feet Y = -1477945
04 meter
Z = 15561202
91 Z = 4765450
60
XDOT = -1188
165818 XDOT = -455
310127
YDOT = 23552
969999 feet/sec YDOT = 7174
374595 meter/sec
ZDOT = 8717
783834 ZDOT = 2655
194883
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5035331
55 X = -1534769
06
Y = 15024476
54 feet Y = 4579460
45 meter
Z = 15663955
64 Z = 4774373
68
XDOT = -16967
688365 XDOT = -5171
751414
YDOT = -14799
810324 feet/sec YDOT = -4510
982187 meter/sec
ZDOT = 8708
258370 ZDOT = 2654
277151
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 20108
13158681
00016717 00000-0 10270-3 0 9102
2 25544 51
6394 290
6472 0003536 124
2722 235
8763 15
48724100 22546
Satellite: ISS
Catalog Number: 25544
Epoch time: 20108
13158681 = yrday
fracday
Element set: 910
Inclination: 51
6394 deg
RA of node: 290
6472 deg
Eccentricity:
0003536
Arg of perigee: 124
2722 deg
Mean anomaly: 235
8763 deg
Mean motion: 15
48724100 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2254
Checksum: 292
Coasting Arc #12 (Orbit 2268)
---------------------------------------
Vector Time (GMT): 2020/109/01:53:00
000
Vector Time (MET): N/A
Weight (LBS) : 922021
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4469395
24 A = 6795684
20 meter
Y = 2012937
85 meter E =
0013335
Z = -4719002
10 I = 51
25297
XDOT = -336
131608 Wp = 83
73847
YDOT = -7136
968605 meter/sec RA = 285
16821 deg
ZDOT = -2731
260735 TA = 159
04180
MA = 158
98709
Ha = 230
698 n
mi
Hp = 221
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14663370
20 X = -4468650
17
Y = 6604126
80 feet Y = 1962961
88 meter
Z = -15482290
35 Z = -4740710
89
XDOT = -1102
793989 XDOT = -243
032058
YDOT = -23415
251329 feet/sec YDOT = -7140
207018 meter/sec
ZDOT = -8960
829183 ZDOT = -2732
667138
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3215151
99 X = 979978
33
Y = -15658765
94 feet Y = -4772791
86 meter
Z = -15581915
09 Z = -4749367
72
XDOT = 18413
894496 XDOT = 5612
555042
YDOT = 12686
631875 feet/sec YDOT = 3866
885395 meter/sec
ZDOT = -8966
874459 ZDOT = -2733
103335
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 20109
09949872
00016717 00000-0 10270-3 0 9119
2 25544 51
6396 285
8606 0003597 126
5239 233
6242 15
48698334 22691
Satellite: ISS
Catalog Number: 25544
Epoch time: 20109
09949872 = yrday
fracday
Element set: 911
Inclination: 51
6396 deg
RA of node: 285
8606 deg
Eccentricity:
0003597
Arg of perigee: 126
5239 deg
Mean anomaly: 233
6242 deg
Mean motion: 15
48698334 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2269
Checksum: 344
Coasting Arc #13 (Orbit 2284)
---------------------------------------
Vector Time (GMT): 2020/110/01:53:00
000
Vector Time (MET): N/A
Weight (LBS) : 922021
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4254130
87 A = 6795733
18 meter
Y = -2507090
41 meter E =
0011365
Z = 4663144
60 I = 51
24685
XDOT = 1039
492621 Wp = 120
81584
YDOT = 7045
600322 meter/sec RA = 280
19891 deg
ZDOT = 2828
795617 TA = 300
87608
MA = 300
98781
Ha = 230
430 n
mi
Hp = 222
147
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13957122
26 X = 4259198
81
Y = -8225362
24 feet Y = -2459489
14 meter
Z = 15299030
83 Z = 4683821
94
XDOT = 3410
408861 XDOT = 946
888694
YDOT = 23115
486621 feet/sec YDOT = 7056
707016 meter/sec
ZDOT = 9280
825515 ZDOT = 2833
619830
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1213011
35 X = -369725
86
Y = 16064656
00 feet Y = 4896507
15 meter
Z = 15393947
56 Z = 4692075
22
XDOT = -19681
016443 XDOT = -5998
773812
YDOT = -10434
244993 feet/sec YDOT = -3180
357874 meter/sec
ZDOT = 9302
561143 ZDOT = 2835
420636
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 20110
13193309
00016717 00000-0 10270-3 0 9123
2 25544 51
6405 280
7564 0003444 132
1316 228
0127 15
48746818 22858
Satellite: ISS
Catalog Number: 25544
Epoch time: 20110
13193309 = yrday
fracday
Element set: 912
Inclination: 51
6405 deg
RA of node: 280
7564 deg
Eccentricity:
0003444
Arg of perigee: 132
1316 deg
Mean anomaly: 228
0127 deg
Mean motion: 15
48746818 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2285
Checksum: 285
Coasting Arc #14 (Orbit 2286)
---------------------------------------
Vector Time (GMT): 2020/110/05:10:04
876
Vector Time (MET): N/A
Weight (LBS) : 921697
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3746237
20 A = 6792186
02 meter
Y = 2449728
85 meter E =
0004341
Z = 5105347
85 I = 51
24155
XDOT = -2470
463449 Wp = 72
78234
YDOT = 7079
720701 meter/sec RA = 279
48508 deg
ZDOT = -1581
928451 TA = 32
58129
MA = 32
55451
Ha = 228
529 n
mi
Hp = 222
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12290804
47 X = 3693766
29
Y = 8037168
14 feet Y = 2491328
79 meter
Z = 16749828
91 Z = 5123418
07
XDOT = -8105
195044 XDOT = -2541
763259
YDOT = 23227
430121 feet/sec YDOT = 7051
695484 meter/sec
ZDOT = -5190
053972 ZDOT = -1594
102510
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4759912
64 X = -1450821
37
Y = 13792240
08 feet Y = 4203874
78 meter
Z = 16832529
81 Z = 5130555
09
XDOT = -23498
160045 XDOT = -7162
239182
YDOT = -1697
396324 feet/sec YDOT = -517
366400 meter/sec
ZDOT = -5246
235394 ZDOT = -1599
052548
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 20110
26096568
00016717 00000-0 10270-3 0 9137
2 25544 51
6421 280
1191 0001551 176
1228 183
9935 15
49334957 22879
Satellite: ISS
Catalog Number: 25544
Epoch time: 20110
26096568 = yrday
fracday
Element set: 913
Inclination: 51
6421 deg
RA of node: 280
1191 deg
Eccentricity:
0001551
Arg of perigee: 176
1228 deg
Mean anomaly: 183
9935 deg
Mean motion: 15
49334957 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2287
Checksum: 310
Coasting Arc #15 (Orbit 2301)
---------------------------------------
Vector Time (GMT): 2020/111/05:10:04
876
Vector Time (MET): N/A
Weight (LBS) : 921697
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3916267
55 A = 6792396
81 meter
Y = -2255654
97 meter E =
0013838
Z = -5083225
71 I = 51
23817
XDOT = 1938
461801 Wp = 108
97377
YDOT = -7201
919754 meter/sec RA = 274
50809 deg
ZDOT = 1701
773530 TA = 177
60573
MA = 177
59910
Ha = 228
711 n
mi
Hp = 222
040
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12848646
81 X = -3866061
55
Y = -7400442
81 feet Y = -2299168
98 meter
Z = -16677249
70 Z = -5102127
45
XDOT = 6359
782812 XDOT = 2010
585445
YDOT = -23628
345649 feet/sec YDOT = -7179
839145 meter/sec
ZDOT = 5583
246491 ZDOT = 1711
365382
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3759992
44 X = 1146045
70
Y = -14241599
86 feet Y = -4340839
64 meter
Z = -16763777
21 Z = -5109599
29
XDOT = 23420
021462 XDOT = 7138
422542
YDOT = -443
265990 feet/sec YDOT = -135
107474 meter/sec
ZDOT = 5627
580094 ZDOT = 1715
286413
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 20111
22850135
00016717 00000-0 10270-3 0 9143
2 25544 51
6427 275
3304 0001541 175
7979 184
3185 15
49310743 23021
Satellite: ISS
Catalog Number: 25544
Epoch time: 20111
22850135 = yrday
fracday
Element set: 914
Inclination: 51
6427 deg
RA of node: 275
3304 deg
Eccentricity:
0001541
Arg of perigee: 175
7979 deg
Mean anomaly: 184
3185 deg
Mean motion: 15
49310743 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2302
Checksum: 288
Coasting Arc #16 (Orbit 2317)
---------------------------------------
Vector Time (GMT): 2020/112/05:10:04
876
Vector Time (MET): N/A
Weight (LBS) : 921697
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4063611
04 A = 6792425
22 meter
Y = 2047066
69 meter E =
0004697
Z = 5039774
35 I = 51
23678
XDOT = -1409
012929 Wp = 70
14419
YDOT = 7307
265834 meter/sec RA = 269
53212 deg
ZDOT = -1829
018402 TA = 37
69606
MA = 37
66315
Ha = 228
416 n
mi
Hp = 222
225
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13332057
22 X = 4015937
56
Y = 6716098
08 feet Y = 2092242
54 meter
Z = 16534692
75 Z = 5059398
08
XDOT = -4622
745831 XDOT = -1481
735813
YDOT = 23973
969273 feet/sec YDOT = 7291
102552 meter/sec
ZDOT = -6000
716543 ZDOT = -1836
039836
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2721384
71 X = -829478
06
Y = 14576157
51 feet Y = 4442812
81 meter
Z = 16624544
65 Z = 5067161
21
XDOT = -23230
632991 XDOT = -7080
696936
YDOT = 2554
958427 feet/sec YDOT = 778
751329 meter/sec
ZDOT = -6033
257168 ZDOT = -1838
936785
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 20112
26053732
00016717 00000-0 10270-3 0 9157
2 25544 51
6422 270
2235 0001516 184
8797 175
2339 15
49346743 23180
Satellite: ISS
Catalog Number: 25544
Epoch time: 20112
26053732 = yrday
fracday
Element set: 915
Inclination: 51
6422 deg
RA of node: 270
2235 deg
Eccentricity:
0001516
Arg of perigee: 184
8797 deg
Mean anomaly: 175
2339 deg
Mean motion: 15
49346743 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2318
Checksum: 301
Coasting Arc #17 (Orbit 2331)
---------------------------------------
Vector Time (GMT): 2020/113/03:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 921697
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1116811
56 A = 6801527
90 meter
Y = 6374986
44 meter E =
0007570
Z = -2081722
57 I = 51
26786
XDOT = -4653
926860 Wp = 147
41013
YDOT = -2604
999339 meter/sec RA = 264
98613 deg
ZDOT = -5496
324156 TA = 55
70133
MA = 55
62969
Ha = 228
581 n
mi
Hp = 222
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3664079
92 X = -1177903
60
Y = 20915309
83 feet Y = 6362155
80 meter
Z = -6829798
47 Z = -2087296
26
XDOT = -15268
788912 XDOT = -4597
752763
YDOT = -8546
585759 feet/sec YDOT = -2656
728951 meter/sec
ZDOT = -18032
559568 ZDOT = -5518
794871
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19773426
13 X = -6026940
29
Y = -7715798
39 feet Y = -2351775
35 meter
Z = -6855646
44 Z = -2089601
04
XDOT = 10833
623632 XDOT = 3302
088483
YDOT = -11695
227235 feet/sec YDOT = -3564
705261 meter/sec
ZDOT = -18135
439689 ZDOT = -5527
682017
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 20113
16356984
00016717 00000-0 10270-3 0 9163
2 25544 51
6421 265
7533 0001519 186
7774 173
3356 15
49310272 23320
Satellite: ISS
Catalog Number: 25544
Epoch time: 20113
16356984 = yrday
fracday
Element set: 916
Inclination: 51
6421 deg
RA of node: 265
7533 deg
Eccentricity:
0001519
Arg of perigee: 186
7774 deg
Mean anomaly: 173
3356 deg
Mean motion: 15
49310272 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2332
Checksum: 307
Coasting Arc #18 (Orbit 2347)
---------------------------------------
Vector Time (GMT): 2020/114/03:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 921697
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 639556
63 A = 6801388
95 meter
Y = -6407794
91 meter E =
0013232
Z = 2171335
59 I = 51
27164
XDOT = 4850
155875 Wp = 76
24414
YDOT = 2339
403890 meter/sec RA = 260
01117 deg
ZDOT = 5450
182987 TA = 307
93329
MA = 308
05280
Ha = 228
572 n
mi
Hp = 222
318
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2098282
92 X = 700615
69
Y = -21022949
19 feet Y = -6400301
49 meter
Z = 7123804
41 Z = 2174590
76
XDOT = 15912
584891 XDOT = 4797
161209
YDOT = 7675
209613 feet/sec YDOT = 2393
345568 meter/sec
ZDOT = 17881
177780 ZDOT = 5473
614756
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20295209
11 X = 6185979
74
Y = 5852752
83 feet Y = 1783919
06 meter
Z = 7139015
65 Z = 2175971
97
XDOT = -10002
776063 XDOT = -3048
846144
YDOT = 12644
298225 feet/sec YDOT = 3853
982099 meter/sec
ZDOT = 17988
482247 ZDOT = 5482
889389
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 20114
19560351
00016717 00000-0 10270-3 0 9173
2 25544 51
6423 260
6458 0001436 189
2710 170
8414 15
49306947 23486
Satellite: ISS
Catalog Number: 25544
Epoch time: 20114
19560351 = yrday
fracday
Element set: 917
Inclination: 51
6423 deg
RA of node: 260
6458 deg
Eccentricity:
0001436
Arg of perigee: 189
2710 deg
Mean anomaly: 170
8414 deg
Mean motion: 15
49306947 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2348
Checksum: 303
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