[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
April 6th 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
098/13:05:00
000 0
0 0
0 0
0
N/A 0
0 0
0 230
9
000/00:00:00
000 0
0 0
0 221
9
100/06:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 231
0
000/00:00:00
000 0
0 0
0 221
9
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
245 0
9 -3
1 3
1
N/A -2
9 -0
0 228
5
000/00:01:02
490 0
6 -0
0 222
2
Coasting Arc #1 (Orbit 2089)
---------------------------------------
Vector Time (GMT): 2020/097/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1692257
31 A = 6793210
92 meter
Y = 3887777
56 meter E =
0006172
Z = 5302168
59 I = 51
51125
XDOT = -7203
195843 Wp = 95
64440
YDOT = 2588
815923 meter/sec RA = 342
61168 deg
ZDOT = 399
768254 TA = 350
52906
MA = 350
54070
Ha = 230
821 n
mi
Hp = 221
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5552025
28 X = 1622902
41
Y = 12755175
71 feet Y = 3906314
30 meter
Z = 17395566
23 Z = 5310220
07
XDOT = -23632
532294 XDOT = -7233
551234
YDOT = 8493
490561 feet/sec YDOT = 2508
094971 meter/sec
ZDOT = 1311
575635 ZDOT = 364
704063
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8423138
18 X = 2567372
52
Y = 11013364
06 feet Y = 3356873
36 meter
Z = 17432205
02 Z = 5313336
09
XDOT = -19998
437412 XDOT = -6095
523723
YDOT = 13468
675315 feet/sec YDOT = 4105
252236 meter/sec
ZDOT = 1150
590276 ZDOT = 350
699916
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 20097
54902275
00016717 00000-0 10270-3 0 9009
2 25544 51
6454 342
9712 0003646 89
4988 270
6580 15
48708136 20902
Satellite: ISS
Catalog Number: 25544
Epoch time: 20097
54902275 = yrday
fracday
Element set: 900
Inclination: 51
6454 deg
RA of node: 342
9712 deg
Eccentricity:
0003646
Arg of perigee: 89
4988 deg
Mean anomaly: 270
6580 deg
Mean motion: 15
48708136 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2090
Checksum: 325
Coasting Arc #2 (Orbit 2104)
---------------------------------------
Vector Time (GMT): 2020/098/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 939740
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2136142
04 A = 6793255
93 meter
Y = -3688391
05 meter E =
0018388
Z = -5305732
39 I = 51
47921
XDOT = 6894
145443 Wp = 86
77221
YDOT = -3267
521085 meter/sec RA = 337
65953 deg
ZDOT = -504
674823 TA = 178
39126
MA = 178
38534
Ha = 230
886 n
mi
Hp = 221
762
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7008340
03 X = -2068966
29
Y = -12101020
51 feet Y = -3711903
84 meter
Z = -17407258
49 Z = -5315945
44
XDOT = 22618
587411 XDOT = 6932
622874
YDOT = -10720
213534 feet/sec YDOT = -3190
210753 meter/sec
ZDOT = -1655
757294 ZDOT = -471
091870
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9842921
58 X = -3000122
50
Y = -9851149
03 feet Y = -3002630
22 meter
Z = -17453822
88 Z = -5319925
21
XDOT = 18273
833155 XDOT = 5569
864346
YDOT = -15601
161634 feet/sec YDOT = -4755
234066 meter/sec
ZDOT = -1501
533857 ZDOT = -457
667520
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 20098
51694599
00016717 00000-0 10270-3 0 9015
2 25544 51
6449 338
1856 0003674 90
4439 269
7132 15
48708806 21059
Satellite: ISS
Catalog Number: 25544
Epoch time: 20098
51694599 = yrday
fracday
Element set: 901
Inclination: 51
6449 deg
RA of node: 338
1856 deg
Eccentricity:
0003674
Arg of perigee: 90
4439 deg
Mean anomaly: 269
7132 deg
Mean motion: 15
48708806 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2105
Checksum: 338
Coasting Arc #3 (Orbit 2105)
---------------------------------------
Vector Time (GMT): 2020/098/13:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 915727
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5149601
18 A = 6803424
40 meter
Y = 3923000
35 meter E =
0017386
Z = 2067943
09 I = 51
51121
XDOT = -4445
848318 Wp = 106
33796
YDOT = -2906
753788 meter/sec RA = 337
41344 deg
ZDOT = -5522
916848 TA = 50
78490
MA = 50
63067
Ha = 230
941 n
mi
Hp = 221
894
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16895016
98 X = -5203131
52
Y = 12870736
07 feet Y = 3865114
75 meter
Z = 6784590
20 Z = 2042797
85
XDOT = -14586
116529 XDOT = -4386
186437
YDOT = -9536
593793 feet/sec YDOT = -2956
137386 meter/sec
ZDOT = -18119
805932 ZDOT = -5544
367922
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7678856
27 X = -2340515
39
Y = 19841562
08 feet Y = 6047708
12 meter
Z = 6669009
72 Z = 2032714
16
XDOT = -15869
109540 XDOT = -4836
904588
YDOT = 19
825074 feet/sec YDOT = 6
042683 meter/sec
ZDOT = -18217
955856 ZDOT = -5552
832945
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 20098
58147405
00016717 00000-0 10270-3 0 9022
2 25544 51
6447 337
8662 0003702 89
8642 270
2932 15
48698173 21069
Satellite: ISS
Catalog Number: 25544
Epoch time: 20098
58147405 = yrday
fracday
Element set: 902
Inclination: 51
6447 deg
RA of node: 337
8662 deg
Eccentricity:
0003702
Arg of perigee: 89
8642 deg
Mean anomaly: 270
2932 deg
Mean motion: 15
48698173 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2106
Checksum: 325
Coasting Arc #4 (Orbit 2120)
---------------------------------------
Vector Time (GMT): 2020/099/13:05:00
000
Vector Time (MET): N/A
Weight (LBS) : 915727
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4702036
13 A = 6803264
10 meter
Y = -4407309
14 meter E =
0008975
Z = -2177606
75 I = 51
47792
XDOT = 4784
132583 Wp = 59
73973
YDOT = 2413
393762 meter/sec RA = 332
45702 deg
ZDOT = 5467
038353 TA = 276
10822
MA = 276
21047
Ha = 230
919 n
mi
Hp = 221
963
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15426627
73 X = 4761548
17
Y = -14459675
65 feet Y = -4354395
06 meter
Z = -7144379
10 Z = -2154620
96
XDOT = 15695
973041 XDOT = 4730
233738
YDOT = 7917
958536 feet/sec YDOT = 2466
592440 meter/sec
ZDOT = 17936
477537 ZDOT = 5490
146891
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5245352
38 X = 1598783
41
Y = -20519466
48 feet Y = -6254333
38 meter
Z = -7038678
12 Z = -2145389
09
XDOT = 15890
281458 XDOT = 4843
357788
YDOT = -2102
555638 feet/sec YDOT = -640
858959 meter/sec
ZDOT = 18042
254263 ZDOT = 5499
279099
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
54939555
00016717 00000-0 10270-3 0 9035
2 25544 51
6426 333
0803 0003581 93
6022 266
5538 15
48682025 21217
Satellite: ISS
Catalog Number: 25544
Epoch time: 20099
54939555 = yrday
fracday
Element set: 903
Inclination: 51
6426 deg
RA of node: 333
0803 deg
Eccentricity:
0003581
Arg of perigee: 93
6022 deg
Mean anomaly: 266
5538 deg
Mean motion: 15
48682025 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2121
Checksum: 306
Coasting Arc #5 (Orbit 2131)
---------------------------------------
Vector Time (GMT): 2020/100/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 915727
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1896603
24 A = 6797951
49 meter
Y = -5027198
68 meter E =
0011332
Z = -4175933
69 I = 51
43733
XDOT = 6666
466650 Wp = 104
84241
YDOT = -561
247255 meter/sec RA = 328
95685 deg
ZDOT = 3709
026011 TA = 203
45552
MA = 203
50724
Ha = 230
970 n
mi
Hp = 221
921
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6222451
58 X = 1972962
44
Y = -16493433
99 feet Y = -5005562
85 meter
Z = -13700569
85 Z = -4166534
82
XDOT = 21871
609743 XDOT = 6654
230674
YDOT = -1841
362386 feet/sec YDOT = -486
766242 meter/sec
ZDOT = 12168
720508 ZDOT = 3741
379796
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17620860
41 X = 5370838
25
Y = 1202567
77 feet Y = 366542
65 meter
Z = -13657122
40 Z = -4162690
91
XDOT = 8234
912402 XDOT = 2510
001300
YDOT = 19006
636544 feet/sec YDOT = 5793
222819 meter/sec
ZDOT = 12317
089139 ZDOT = 3754
248770
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
25920596
00016717 00000-0 10270-3 0 9042
2 25544 51
6405 329
5705 0003750 96
9711 263
1866 15
48673033 21322
Satellite: ISS
Catalog Number: 25544
Epoch time: 20100
25920596 = yrday
fracday
Element set: 904
Inclination: 51
6405 deg
RA of node: 329
5705 deg
Eccentricity:
0003750
Arg of perigee: 96
9711 deg
Mean anomaly: 263
1866 deg
Mean motion: 15
48673033 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2132
Checksum: 298
Coasting Arc #6 (Orbit 2133)
---------------------------------------
Vector Time (GMT): 2020/100/08:05:06
000
Vector Time (MET): N/A
Weight (LBS) : 915727
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3806002
66 A = 6794100
64 meter
Y = 2418536
36 meter E =
0008606
Z = 5075877
24 I = 51
42435
XDOT = -5526
964382 Wp = 113
62672
YDOT = 5013
674107 meter/sec RA = 328
56595 deg
ZDOT = 1749
597391 TA = 319
36423
MA = 319
42842
Ha = 230
715 n
mi
Hp = 221
859
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12486885
37 X = 3754018
99
Y = 7934830
58 feet Y = 2460807
47 meter
Z = 16653140
56 Z = 5094239
11
XDOT = -18133
085244 XDOT = -5591
116639
YDOT = 16449
062032 feet/sec YDOT = 4951
509076 meter/sec
ZDOT = 5740
148919 ZDOT = 1722
593093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3985999
43 X = 1214932
63
Y = 14148871
29 feet Y = 4312575
97 meter
Z = 16737149
78 Z = 5101483
25
XDOT = -23478
105046 XDOT = -7156
126418
YDOT = -51
288613 feet/sec YDOT = -15
632769 meter/sec
ZDOT = 5615
989642 ZDOT = 1711
753643
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
38826109
00016717 00000-0 10270-3 0 9052
2 25544 51
6422 328
9333 0003629 98
7839 261
3721 15
48723431 21347
Satellite: ISS
Catalog Number: 25544
Epoch time: 20100
38826109 = yrday
fracday
Element set: 905
Inclination: 51
6422 deg
RA of node: 328
9333 deg
Eccentricity:
0003629
Arg of perigee: 98
7839 deg
Mean anomaly: 261
3721 deg
Mean motion: 15
48723431 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2134
Checksum: 303
Coasting Arc #7 (Orbit 2137)
---------------------------------------
Vector Time (GMT): 2020/100/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 931644
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3841764
38 A = 6794282
53 meter
Y = 2350531
00 meter E =
0008598
Z = 5081129
61 I = 51
41503
XDOT = -5429
404284 Wp = 113
84010
YDOT = 5126
367066 meter/sec RA = 327
28371 deg
ZDOT = 1727
900837 TA = 319
36518
MA = 319
42931
Ha = 230
833 n
mi
Hp = 221
961
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12604213
86 X = 3790512
99
Y = 7711715
87 feet Y = 2393206
07 meter
Z = 16670372
73 Z = 5099667
01
XDOT = -17813
006181 XDOT = -5494
718571
YDOT = 16818
789587 feet/sec YDOT = 5065
286510 meter/sec
ZDOT = 5668
966002 ZDOT = 1701
367651
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13803293
90 X = 4207243
98
Y = -4997076
51 feet Y = -1523108
92 meter
Z = 16755190
23 Z = 5106981
98
XDOT = 1726
428705 XDOT = 526
215469
YDOT = 23430
545461 feet/sec YDOT = 7141
630257 meter/sec
ZDOT = 5546
961134 ZDOT = 1690
713754
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
64637420
00016717 00000-0 10270-3 0 9068
2 25544 51
6403 327
6549 0003659 99
5129 260
6434 15
48653431 21384
Satellite: ISS
Catalog Number: 25544
Epoch time: 20100
64637420 = yrday
fracday
Element set: 906
Inclination: 51
6403 deg
RA of node: 327
6549 deg
Eccentricity:
0003659
Arg of perigee: 99
5129 deg
Mean anomaly: 260
6434 deg
Mean motion: 15
48653431 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2138
Checksum: 306
Coasting Arc #8 (Orbit 2152)
---------------------------------------
Vector Time (GMT): 2020/101/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 931644
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4110305
40 A = 6794281
36 meter
Y = -1937737
37 meter E =
0016542
Z = -5065908
64 I = 51
38736
XDOT = 4877
936208 Wp = 82
11628
YDOT = -5601
462353 meter/sec RA = 322
32368 deg
ZDOT = -1818
102885 TA = 170
18539
MA = 170
15304
Ha = 230
886 n
mi
Hp = 221
754
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13485253
93 X = -4063723
97
Y = -6357406
08 feet Y = -1983441
42 meter
Z = -16620435
18 Z = -5085761
95
XDOT = 16003
727715 XDOT = 4949
042291
YDOT = -18377
501158 feet/sec YDOT = -5546
516272 meter/sec
ZDOT = -5964
904479 ZDOT = -1794
234624
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13175234
95 X = -4015811
61
Y = 6756687
73 feet Y = 2059438
42 meter
Z = -16711310
72 Z = -5093607
51
XDOT = -4354
262393 XDOT = -1327
179177
YDOT = -22948
591016 feet/sec YDOT = -6994
730542 meter/sec
ZDOT = -5855
091117 ZDOT = -1784
631772
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
61429259
00016717 00000-0 10270-3 0 9076
2 25544 51
6399 322
8681 0003696 104
0732 256
0828 15
48694638 21532
Satellite: ISS
Catalog Number: 25544
Epoch time: 20101
61429259 = yrday
fracday
Element set: 907
Inclination: 51
6399 deg
RA of node: 322
8681 deg
Eccentricity:
0003696
Arg of perigee: 104
0732 deg
Mean anomaly: 256
0828 deg
Mean motion: 15
48694638 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2153
Checksum: 322
Coasting Arc #9 (Orbit 2168)
---------------------------------------
Vector Time (GMT): 2020/102/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 931644
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4327632
88 A = 6794498
95 meter
Y = 1471365
52 meter E =
0009243
Z = 5021137
86 I = 51
36202
XDOT = -4296
951977 Wp = 116
48981
YDOT = 6047
654115 meter/sec RA = 317
36241 deg
ZDOT = 1924
497378 TA = 314
72103
MA = 314
79625
Ha = 230
805 n
mi
Hp = 221
952
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14198270
59 X = 4286467
94
Y = 4827314
69 feet Y = 1519530
03 meter
Z = 16473549
40 Z = 5042060
03
XDOT = -14097
611474 XDOT = -4373
607475
YDOT = 19841
384893 feet/sec YDOT = 5999
173939 meter/sec
ZDOT = 6313
967775 ZDOT = 1903
438061
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12250061
08 X = 3733818
62
Y = -8465467
18 feet Y = -2580274
40 meter
Z = 16569355
86 Z = 5050339
67
XDOT = 6948
577821 XDOT = 2117
926520
YDOT = 22266
926004 feet/sec YDOT = 6786
959046 meter/sec
ZDOT = 6217
006613 ZDOT = 1894
943616
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
64673887
00016717 00000-0 10270-3 0 9089
2 25544 51
6399 317
7625 0003713 106
0122 254
1437 15
48662851 21692
Satellite: ISS
Catalog Number: 25544
Epoch time: 20102
64673887 = yrday
fracday
Element set: 908
Inclination: 51
6399 deg
RA of node: 317
7625 deg
Eccentricity:
0003713
Arg of perigee: 106
0122 deg
Mean anomaly: 254
1437 deg
Mean motion: 15
48662851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2169
Checksum: 315
Coasting Arc #10 (Orbit 2183)
---------------------------------------
Vector Time (GMT): 2020/103/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 931644
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4499807
87 A = 6794512
54 meter
Y = -1009657
58 meter E =
0016124
Z = -5004302
15 I = 51
33819
XDOT = 3667
941695 Wp = 83
06918
YDOT = -6402
041470 meter/sec RA = 312
39982 deg
ZDOT = -2010
204293 TA = 167
27882
MA = 167
23809
Ha = 230
922 n
mi
Hp = 221
699
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14763149
19 X = -4463874
96
Y = -3312524
88 feet Y = -1059776
66 meter
Z = -16418314
14 Z = -5026073
33
XDOT = 12033
929444 XDOT = 3749
023088
YDOT = -21004
073064 feet/sec YDOT = -6360
570559 meter/sec
ZDOT = -6595
158440 ZDOT = -1992
189903
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11196432
26 X = -3412672
55
Y = 10013917
36 feet Y = 3052242
01 meter
Z = -16518044
62 Z = -5034700
00
XDOT = -9375
840752 XDOT = -2857
756261
YDOT = -21204
944538 feet/sec YDOT = -6463
267095 meter/sec
ZDOT = -6512
138751 ZDOT = -1984
899891
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
61465490
00016717 00000-0 10270-3 0 9097
2 25544 51
6396 312
9768 0003913 111
0168 249
1401 15
48700691 21849
Satellite: ISS
Catalog Number: 25544
Epoch time: 20103
61465490 = yrday
fracday
Element set: 909
Inclination: 51
6396 deg
RA of node: 312
9768 deg
Eccentricity:
0003913
Arg of perigee: 111
0168 deg
Mean anomaly: 249
1401 deg
Mean motion: 15
48700691 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2184
Checksum: 300
Coasting Arc #11 (Orbit 2199)
---------------------------------------
Vector Time (GMT): 2020/104/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 931644
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4613935
71 A = 6794704
17 meter
Y = 501992
14 meter E =
0009872
Z = 4956760
90 I = 51
31641
XDOT = -3012
694740 Wp = 119
65885
YDOT = 6722
005307 meter/sec RA = 307
43555 deg
ZDOT = 2115
578545 TA = 309
58863
MA = 309
67577
Ha = 230
739 n
mi
Hp = 221
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15137584
35 X = 4583902
21
Y = 1646955
85 feet Y = 553420
45 meter
Z = 16262338
90 Z = 4979100
70
XDOT = -9884
169095 XDOT = -3097
914572
YDOT = 22053
823187 feet/sec YDOT = 6687
838687 meter/sec
ZDOT = 6940
874493 ZDOT = 2100
737142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9861727
19 X = 3005854
45
Y = -11457100
32 feet Y = -3492124
18 meter
Z = 16364711
40 Z = 4987964
03
XDOT = 11728
550702 XDOT = 3574
862254
YDOT = 19948
707363 feet/sec YDOT = 6080
366004 meter/sec
ZDOT = 6872
388670 ZDOT = 2094
704067
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
64709911
00016717 00000-0 10270-3 0 9102
2 25544 51
6391 307
8716 0003759 115
2647 244
8893 15
48683599 22009
Satellite: ISS
Catalog Number: 25544
Epoch time: 20104
64709911 = yrday
fracday
Element set: 910
Inclination: 51
6391 deg
RA of node: 307
8716 deg
Eccentricity:
0003759
Arg of perigee: 115
2647 deg
Mean anomaly: 244
8893 deg
Mean motion: 15
48683599 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2200
Checksum: 325
Coasting Arc #12 (Orbit 2214)
---------------------------------------
Vector Time (GMT): 2020/105/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 931644
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4681605
93 A = 6794740
50 meter
Y = -12653
45 meter E =
0015395
Z = -4938415
03 I = 51
29925
XDOT = 2332
143914 Wp = 83
96077
YDOT = -6944
191444 meter/sec RA = 302
47032 deg
ZDOT = -2197
427010 TA = 164
46021
MA = 164
41289
Ha = 230
848 n
mi
Hp = 221
743
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15359599
52 X = -4657128
54
Y = -41513
95 feet Y = -64869
60 meter
Z = -16202149
05 Z = -4961096
95
XDOT = 7651
390793 XDOT = 2420
296414
YDOT = -22782
780329 feet/sec YDOT = -6917
618842 meter/sec
ZDOT = -7209
406202 ZDOT = -2185
884340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8446753
90 X = -2574570
59
Y = 12696116
05 feet Y = 3869776
17 meter
Z = -16306122
79 Z = -4970106
23
XDOT = -13830
457141 XDOT = -4215
523337
YDOT = -18373
994957 feet/sec YDOT = -5600
393663 meter/sec
ZDOT = -7156
040995 ZDOT = -2181
161295
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
61501322
00016717 00000-0 10270-3 0 9117
2 25544 51
6410 303
0863 0003903 118
4545 241
6998 15
48714678 22155
Satellite: ISS
Catalog Number: 25544
Epoch time: 20105
61501322 = yrday
fracday
Element set: 911
Inclination: 51
6410 deg
RA of node: 303
0863 deg
Eccentricity:
0003903
Arg of perigee: 118
4545 deg
Mean anomaly: 241
6998 deg
Mean motion: 15
48714678 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2215
Checksum: 286
Coasting Arc #13 (Orbit 2230)
---------------------------------------
Vector Time (GMT): 2020/106/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 931644
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4685071
74 A = 6794890
66 meter
Y = -511556
96 meter E =
0010413
Z = 4889060
03 I = 51
28214
XDOT = -1631
372582 Wp = 121
71488
YDOT = 7126
151014 meter/sec RA = 297
50263 deg
ZDOT = 2299
931294 TA = 305
61563
MA = 305
71258
Ha = 230
651 n
mi
Hp = 221
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15370970
28 X = 4666695
75
Y = -1678336
49 feet Y = -459267
89 meter
Z = 16040223
19 Z = 4911773
56
XDOT = -5352
272250 XDOT = -1722
109772
YDOT = 23379
760545 feet/sec YDOT = 7107
400510 meter/sec
ZDOT = 7545
706345 ZDOT = 2291
786347
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6783149
93 X = 2067504
10
Y = -13773900
86 feet Y = -4198284
98 meter
Z = 16144374
65 Z = 4920805
39
XDOT = 15813
641571 XDOT = 4819
997951
YDOT = 16622
081990 feet/sec YDOT = 5066
410590 meter/sec
ZDOT = 7507
921570 ZDOT = 2288
414494
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
64745256
00016717 00000-0 10270-3 0 9128
2 25544 51
6403 297
9805 0003793 122
8617 237
2898 15
48716372 22311
Satellite: ISS
Catalog Number: 25544
Epoch time: 20106
64745256 = yrday
fracday
Element set: 912
Inclination: 51
6403 deg
RA of node: 297
9805 deg
Eccentricity:
0003793
Arg of perigee: 122
8617 deg
Mean anomaly: 237
2898 deg
Mean motion: 15
48716372 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2231
Checksum: 323
Coasting Arc #14 (Orbit 2245)
---------------------------------------
Vector Time (GMT): 2020/107/14:16:50
000
Vector Time (MET): N/A
Weight (LBS) : 931644
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4645443
45 A = 6795022
32 meter
Y = 1005116
78 meter E =
0014655
Z = -4869336
61 I = 51
26832
XDOT = 927
083327 Wp = 84
89851
YDOT = -7210
056112 meter/sec RA = 292
53580 deg
ZDOT = -2377
678221 TA = 161
64276
MA = 161
58981
Ha = 230
799 n
mi
Hp = 221
813
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15240956
20 X = -4632685
36
Y = 3297627
24 feet Y = 953239
38 meter
Z = -15975513
81 Z = -4891871
29
XDOT = 3041
611964 XDOT = 1019
188755
YDOT = -23655
039739 feet/sec YDOT = -7199
173856 meter/sec
ZDOT = -7800
781565 ZDOT = -2372
950998
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5096906
53 X = -1553537
11
Y = 14624278
15 feet Y = 4457479
98 meter
Z = -16078873
27 Z = -4900840
57
XDOT = -17484
853947 XDOT = -5329
383483
YDOT = -14628
559180 feet/sec YDOT = -4458
784838 meter/sec
ZDOT = -7778
677377 ZDOT = -2370
940865
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
61536449
00016717 00000-0 10270-3 0 9139
2 25544 51
6405 293
1961 0003924 125
0730 235
0789 15
48715712 22469
Satellite: ISS
Catalog Number: 25544
Epoch time: 20107
61536449 = yrday
fracday
Element set: 913
Inclination: 51
6405 deg
RA of node: 293
1961 deg
Eccentricity:
0003924
Arg of perigee: 125
0730 deg
Mean anomaly: 235
0789 deg
Mean motion: 15
48715712 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2246
Checksum: 302
Coasting Arc #15 (Orbit 2253)
---------------------------------------
Vector Time (GMT): 2020/108/01:53:00
000
Vector Time (MET): N/A
Weight (LBS) : 916536
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4613496
75 A = 6795461
89 meter
Y = -1526857
23 meter E =
0011057
Z = 4744035
58 I = 51
26287
XDOT = -364
336037 Wp = 119
83687
YDOT = 7179
651575 meter/sec RA = 290
13888 deg
ZDOT = 2654
984730 TA = 303
74170
MA = 303
84701
Ha = 230
544 n
mi
Hp = 222
060
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15136144
19 X = 4607183
92
Y = -5009374
10 feet Y = -1475301
00 meter
Z = 15564421
20 Z = 4766430
76
XDOT = -1195
328204 XDOT = -457
490292
YDOT = 23555
287320 feet/sec YDOT = 7175
056518 meter/sec
ZDOT = 8710
579823 ZDOT = 2652
988503
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5041970
16 X = -1536792
50
Y = 15018861
87 feet Y = 4577749
10 meter
Z = 15667170
20 Z = 4775353
48
XDOT = -16965
668877 XDOT = -5171
135874
YDOT = -14806
402048 feet/sec YDOT = -4512
991344 meter/sec
ZDOT = 8701
005737 ZDOT = 2652
066549
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
13158255
00016717 00000-0 10270-3 0 9143
2 25544 51
6395 290
6474 0003528 124
1539 235
9946 15
48725235 22549
Satellite: ISS
Catalog Number: 25544
Epoch time: 20108
13158255 = yrday
fracday
Element set: 914
Inclination: 51
6395 deg
RA of node: 290
6474 deg
Eccentricity:
0003528
Arg of perigee: 124
1539 deg
Mean anomaly: 235
9946 deg
Mean motion: 15
48725235 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2254
Checksum: 316
Coasting Arc #16 (Orbit 2268)
---------------------------------------
Vector Time (GMT): 2020/109/01:53:00
000
Vector Time (MET): N/A
Weight (LBS) : 916536
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4469533
93 A = 6795675
71 meter
Y = 2009846
05 meter E =
0013341
Z = -4720187
90 I = 51
25315
XDOT = -333
650034 Wp = 83
69223
YDOT = -7138
063393 meter/sec RA = 285
16848 deg
ZDOT = -2728
690540 TA = 159
11578
MA = 159
06122
Ha = 230
694 n
mi
Hp = 221
975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14663825
24 X = -4468748
52
Y = 6593983
10 feet Y = 1959868
75 meter
Z = -15486180
76 Z = -4741897
26
XDOT = -1094
652343 XDOT = -240
550911
YDOT = -23418
843153 feet/sec YDOT = -7141
274058 meter/sec
ZDOT = -8952
396785 ZDOT = -2730
084890
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3223610
34 X = 982556
43
Y = -15653150
00 feet Y = -4771080
12 meter
Z = -15585807
97 Z = -4750554
27
XDOT = 18412
457497 XDOT = 5612
117045
YDOT = 12694
666211 feet/sec YDOT = 3869
334261 meter/sec
ZDOT = -8958
386746 ZDOT = -2730
516280
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
09949370
00016717 00000-0 10270-3 0 9156
2 25544 51
6398 285
8608 0003589 126
4070 233
7411 15
48699628 22694
Satellite: ISS
Catalog Number: 25544
Epoch time: 20109
09949370 = yrday
fracday
Element set: 915
Inclination: 51
6398 deg
RA of node: 285
8608 deg
Eccentricity:
0003589
Arg of perigee: 126
4070 deg
Mean anomaly: 233
7411 deg
Mean motion: 15
48699628 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2269
Checksum: 344
Coasting Arc #17 (Orbit 2284)
---------------------------------------
Vector Time (GMT): 2020/110/01:53:00
000
Vector Time (MET): N/A
Weight (LBS) : 916536
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4254655
25 A = 6795723
24 meter
Y = -2503472
67 meter E =
0011350
Z = 4664594
30 I = 51
24702
XDOT = 1036
694029 Wp = 120
79828
YDOT = 7047
228601 meter/sec RA = 280
19919 deg
ZDOT = 2825
781930 TA = 300
92664
MA = 301
03815
Ha = 230
426 n
mi
Hp = 222
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13958842
68 X = 4259675
66
Y = -8213493
02 feet Y = -2455865
80 meter
Z = 15303787
09 Z = 4685274
08
XDOT = 3401
227130 XDOT = 944
086741
YDOT = 23120
828742 feet/sec YDOT = 7058
303980 meter/sec
ZDOT = 9270
938091 ZDOT = 2830
592540
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1223700
97 X = -372984
06
Y = 16059227
73 feet Y = 4894852
61 meter
Z = 15398714
77 Z = 4693528
26
XDOT = -19680
557139 XDOT = -5998
633816
YDOT = -10443
995095 feet/sec YDOT = -3183
329705 meter/sec
ZDOT = 9292
611277 ZDOT = 2832
387917
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
13192715
00016717 00000-0 10270-3 0 9167
2 25544 51
6406 280
7566 0003435 132
0097 228
1345 15
48748241 22851
Satellite: ISS
Catalog Number: 25544
Epoch time: 20110
13192715 = yrday
fracday
Element set: 916
Inclination: 51
6406 deg
RA of node: 280
7566 deg
Eccentricity:
0003435
Arg of perigee: 132
0097 deg
Mean anomaly: 228
1345 deg
Mean motion: 15
48748241 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2285
Checksum: 292
Coasting Arc #18 (Orbit 2286)
---------------------------------------
Vector Time (GMT): 2020/110/05:10:04
490
Vector Time (MET): N/A
Weight (LBS) : 916214
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3745872
56 A = 6792182
68 meter
Y = 2450702
49 meter E =
0004345
Z = 5105147
19 I = 51
24174
XDOT = -2471
135700 Wp = 72
61194
YDOT = 7079
289397 meter/sec RA = 279
48540 deg
ZDOT = -1582
803116 TA = 32
76043
MA = 32
73350
Ha = 228
525 n
mi
Hp = 222
156
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12289608
13 X = 3693391
76
Y = 8040362
50 feet Y = 2492298
30 meter
Z = 16749170
59 Z = 5123215
62
XDOT = -8107
400590 XDOT = -2542
426388
YDOT = 23226
015083 feet/sec YDOT = 7051
256714 meter/sec
ZDOT = -5192
923610 ZDOT = -1594
980419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4763691
15 X = -1451973
06
Y = 13791745
36 feet Y = 4203723
99 meter
Z = 16831863
21 Z = 5130351
91
XDOT = -23497
310933 XDOT = -7161
980372
YDOT = -1700
279593 feet/sec YDOT = -518
245220 meter/sec
ZDOT = -5249
119877 ZDOT = -1599
931738
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
26095963
00016717 00000-0 10270-3 0 9179
2 25544 51
6423 280
1193 0001539 176
1499 183
9663 15
49336405 22877
Satellite: ISS
Catalog Number: 25544
Epoch time: 20110
26095963 = yrday
fracday
Element set: 917
Inclination: 51
6423 deg
RA of node: 280
1193 deg
Eccentricity:
0001539
Arg of perigee: 176
1499 deg
Mean anomaly: 183
9663 deg
Mean motion: 15
49336405 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2287
Checksum: 320
Coasting Arc #19 (Orbit 2301)
---------------------------------------
Vector Time (GMT): 2020/111/05:10:04
490
Vector Time (MET): N/A
Weight (LBS) : 916214
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3915815
52 A = 6792393
67 meter
Y = -2257224
45 meter E =
0013830
Z = -5082866
98 I = 51
23837
XDOT = 1939
571005 Wp = 108
93595
YDOT = -7201
297760 meter/sec RA = 274
50841 deg
ZDOT = 1703
172178 TA = 177
65743
MA = 177
65094
Ha = 228
707 n
mi
Hp = 222
038
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12847163
77 X = -3865593
75
Y = -7405592
03 feet Y = -2300733
32 meter
Z = -16676072
75 Z = -5101766
48
XDOT = 6363
421933 XDOT = 2011
680818
YDOT = -23626
304988 feet/sec YDOT = -7179
204824 meter/sec
ZDOT = 5587
835229 ZDOT = 1712
769384
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3765749
25 X = 1147800
37
Y = -14241436
86 feet Y = -4340789
95 meter
Z = -16762589
94 Z = -5109237
41
XDOT = 23419
026677 XDOT = 7138
119331
YDOT = -438
977520 feet/sec YDOT = -133
800348 meter/sec
ZDOT = 5632
193345 ZDOT = 1716
692531
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
22849435
00016717 00000-0 10270-3 0 9188
2 25544 51
6428 275
3306 0001528 175
8007 184
3157 15
49312338 23023
Satellite: ISS
Catalog Number: 25544
Epoch time: 20111
22849435 = yrday
fracday
Element set: 918
Inclination: 51
6428 deg
RA of node: 275
3306 deg
Eccentricity:
0001528
Arg of perigee: 175
8007 deg
Mean anomaly: 184
3157 deg
Mean motion: 15
49312338 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2302
Checksum: 295
Coasting Arc #20 (Orbit 2317)
---------------------------------------
Vector Time (GMT): 2020/112/05:10:04
490
Vector Time (MET): N/A
Weight (LBS) : 916214
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4063140
87 A = 6792422
57 meter
Y = 2049369
15 meter E =
0004706
Z = 5039215
65 I = 51
23697
XDOT = -1410
655607 Wp = 69
98860
YDOT = 7306
448525 meter/sec RA = 269
53245 deg
ZDOT = -1831
017037 TA = 37
87183
MA = 37
83873
Ha = 228
412 n
mi
Hp = 222
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13330514
66 X = 4015444
39
Y = 6723652
06 feet Y = 2094539
60 meter
Z = 16532859
74 Z = 5058837
04
XDOT = -4628
135192 XDOT = -1483
359520
YDOT = 23971
287811 feet/sec YDOT = 7290
266979 meter/sec
ZDOT = -6007
273744 ZDOT = -1838
046404
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2729474
01 X = -831943
68
Y = 14576740
34 feet Y = 4442990
45 meter
Z = 16622700
80 Z = 5066599
20
XDOT = -23229
588903 XDOT = -7080
378698
YDOT = 2548
980862 feet/sec YDOT = 776
929367 meter/sec
ZDOT = -6039
850696 ZDOT = -1840
946492
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
26052922
00016717 00000-0 10270-3 0 9191
2 25544 51
6424 270
2238 0001504 184
9313 175
1822 15
49348474 23186
Satellite: ISS
Catalog Number: 25544
Epoch time: 20112
26052922 = yrday
fracday
Element set: 919
Inclination: 51
6424 deg
RA of node: 270
2238 deg
Eccentricity:
0001504
Arg of perigee: 184
9313 deg
Mean anomaly: 175
1822 deg
Mean motion: 15
49348474 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2318
Checksum: 291
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