[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 3rd 2020
- spaceflight nasa gov will be taken offline in the next 30 days *
- *
- Current information about the International Space Station can be *
- found at www nasa gov/station *
- *
- Predicted ISS and visiting vehicle sightings opportunities can be *
- found at spotthestation nasa gov *
- *
- Updated ISS trajectory information will be made available as a CCSDS *
- Orbital Ephemeris Message (OEM) in the Mean of J2000 (J2K) reference *
- system *
- Included in the OEM are a sequence of events with ISS maneuver *
- details (in the comment section), predicted post-maneuver state *
- vectors, predicted coasting state vectors at 4-minute intervals, *
- and ISS ballistic details *
- *
- OEMs will be provided in xml and txt formats *
- Links to the OEMs and more details to follow *
- *
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) : 74 2 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
311/18:30:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
2
000/00:00:00
000 0
0 0
0 221
4
317/19:37:58
974 1
8 2
1 2
1
N/A -1
1 -0
2 229
1
000/00:05:57
948 0
2 0
1 222
5
320/00:49:48
000 0
0 0
0 0
0
N/A 0
0 0
0 228
9
000/00:00:00
000 0
0 0
0 222
6
320/09:04:15
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
6
Coasting Arc #1 (Orbit 1344)
---------------------------------------
Vector Time (GMT): 2020/307/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2707764
62 A = 6791628
05 meter
Y = -3346033
21 meter E =
0015831
Z = -5267262
16 I = 51
78404
XDOT = 6596
131390 Wp = 95
56839
YDOT = 3736
076838 meter/sec RA = 23
45371 deg
ZDOT = 1018
698805 TA = 184
18444
MA = 184
19770
Ha = 229
102 n
mi
Hp = 221
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8883742
19 X = 2770565
83
Y = -10977799
24 feet Y = -3315401
74 meter
Z = -17281043
83 Z = -5253956
07
XDOT = 21640
851017 XDOT = 6548
914805
YDOT = 12257
469941 feet/sec YDOT = 3809
575477 meter/sec
ZDOT = 3342
187679 ZDOT = 1050
626606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 486862
24 X = 148395
61
Y = 14188940
92 feet Y = 4324789
19 meter
Z = -17219301
62 Z = -5248443
13
XDOT = -23294
481096 XDOT = -7100
157838
YDOT = 5029
722196 feet/sec YDOT = 1533
059325 meter/sec
ZDOT = 3489
689886 ZDOT = 1063
657477
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 20307
51431578
00016717 00000-0 10270-3 0 9003
2 25544 51
6449 24
0155 0001679 77
5371 282
5967 15
49368251 13457
Satellite: ISS
Catalog Number: 25544
Epoch time: 20307
51431578 = yrday
fracday
Element set: 900
Inclination: 51
6449 deg
RA of node: 24
0155 deg
Eccentricity:
0001679
Arg of perigee: 77
5371 deg
Mean anomaly: 282
5967 deg
Mean motion: 15
49368251 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1345
Checksum: 314
Coasting Arc #2 (Orbit 1360)
---------------------------------------
Vector Time (GMT): 2020/308/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2561217
39 A = 6791607
64 meter
Y = 3489584
21 meter E =
0005502
Z = 5229660
80 I = 51
75326
XDOT = -6836
692238 Wp = 62
40272
YDOT = -3260
958631 meter/sec RA = 18
51337 deg
ZDOT = -1168
896089 TA = 38
81485
MA = 38
77535
Ha = 229
088 n
mi
Hp = 221
537
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8402944
21 X = -2625452
03
Y = 11448767
08 feet Y = 3460583
42 meter
Z = 17157679
78 Z = 5217063
21
XDOT = -22430
092643 XDOT = -6794
041105
YDOT = -10698
683172 feet/sec YDOT = -3337
172894 meter/sec
ZDOT = -3834
960921 ZDOT = -1202
003557
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1404050
40 X = -427954
56
Y = -14202660
20 feet Y = -4328970
83 meter
Z = 17099204
66 Z = 5211837
58
XDOT = 22734
904592 XDOT = 6929
598920
YDOT = -7062
373760 feet/sec YDOT = -2152
611522 meter/sec
ZDOT = -3987
933372 ZDOT = -1215
522092
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 20308
54630826
00016717 00000-0 10270-3 0 9015
2 25544 51
6453 18
9082 0001551 81
4773 278
6553 15
49410029 13618
Satellite: ISS
Catalog Number: 25544
Epoch time: 20308
54630826 = yrday
fracday
Element set: 901
Inclination: 51
6453 deg
RA of node: 18
9082 deg
Eccentricity:
0001551
Arg of perigee: 81
4773 deg
Mean anomaly: 278
6553 deg
Mean motion: 15
49410029 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1361
Checksum: 297
Coasting Arc #3 (Orbit 1375)
---------------------------------------
Vector Time (GMT): 2020/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2408083
20 A = 6791847
28 meter
Y = -3649275
97 meter E =
0015487
Z = -5211101
77 I = 51
72056
XDOT = 7013
191172 Wp = 97
71096
YDOT = 2757
386331 meter/sec RA = 13
57098 deg
ZDOT = 1311
195012 TA = 184
89478
MA = 184
90994
Ha = 229
106 n
mi
Hp = 221
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7900535
44 X = 2474024
72
Y = -11972690
18 feet Y = -3621978
02 meter
Z = -17096790
58 Z = -5199244
02
XDOT = 23009
157387 XDOT = 6975
466812
YDOT = 9046
543080 feet/sec YDOT = 2835
601852 meter/sec
ZDOT = 4301
820907 ZDOT = 1345
171749
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2373384
17 X = 723407
49
Y = 14213043
77 feet Y = 4332135
74 meter
Z = -17041726
82 Z = -5194318
33
XDOT = -21893
808118 XDOT = -6673
232714
YDOT = 8996
981955 feet/sec YDOT = 2742
280100 meter/sec
ZDOT = 4458
832537 ZDOT = 1359
052157
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 20309
51379895
00016717 00000-0 10270-3 0 9020
2 25544 51
6447 14
1202 0001703 80
3078 279
8264 15
49374210 13767
Satellite: ISS
Catalog Number: 25544
Epoch time: 20309
51379895 = yrday
fracday
Element set: 902
Inclination: 51
6447 deg
RA of node: 14
1202 deg
Eccentricity:
0001703
Arg of perigee: 80
3078 deg
Mean anomaly: 279
8264 deg
Mean motion: 15
49374210 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1376
Checksum: 301
Coasting Arc #4 (Orbit 1391)
---------------------------------------
Vector Time (GMT): 2020/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2251705
73 A = 6791860
40 meter
Y = 3786214
64 meter E =
0006280
Z = 5165368
33 I = 51
68804
XDOT = -7175
079285 Wp = 61
65837
YDOT = -2260
479996 meter/sec RA = 8
62621 deg
ZDOT = -1466
584091 TA = 42
48093
MA = 42
43234
Ha = 229
115 n
mi
Hp = 221
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7387485
99 X = -2318967
91
Y = 12421964
03 feet Y = 3760657
99 meter
Z = 16946746
49 Z = 5154267
09
XDOT = -23540
286367 XDOT = -7142
144668
YDOT = -7416
272953 feet/sec YDOT = -2340
532626 meter/sec
ZDOT = -4811
627595 ZDOT = -1501
358722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3299217
92 X = -1005601
62
Y = -14132962
61 feet Y = -4307727
00 meter
Z = 16895173
44 Z = 5149648
86
XDOT = 20978
300121 XDOT = 6394
185877
YDOT = -10858
171646 feet/sec YDOT = -3309
570718 meter/sec
ZDOT = -4972
350449 ZDOT = -1515
572417
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 20310
54578242
00016717 00000-0 10270-3 0 9033
2 25544 51
6449 9
0128 0001689 82
8119 277
3223 15
49416673 13921
Satellite: ISS
Catalog Number: 25544
Epoch time: 20310
54578242 = yrday
fracday
Element set: 903
Inclination: 51
6449 deg
RA of node: 9
0128 deg
Eccentricity:
0001689
Arg of perigee: 82
8119 deg
Mean anomaly: 277
3223 deg
Mean motion: 15
49416673 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1392
Checksum: 308
Coasting Arc #5 (Orbit 1406)
---------------------------------------
Vector Time (GMT): 2020/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2081869
80 A = 6792137
15 meter
Y = -3940134
32 meter E =
0015185
Z = -5139436
37 I = 51
65382
XDOT = 7271
514604 Wp = 99
88569
YDOT = 1743
908151 meter/sec RA = 3
67937 deg
ZDOT = 1610
086681 TA = 185
67433
MA = 185
69156
Ha = 229
162 n
mi
Hp = 221
524
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6830281
50 X = 2150739
71
Y = -12926949
86 feet Y = -3916467
92 meter
Z = -16861667
87 Z = -5129156
29
XDOT = 23856
675210 XDOT = 7243
652247
YDOT = 5721
483434 feet/sec YDOT = 1825
067542 meter/sec
ZDOT = 5282
436618 ZDOT = 1645
341905
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4293137
25 X = 1308548
23
Y = 14033419
48 feet Y = 4277386
26 meter
Z = -16813885
08 Z = -5124872
17
XDOT = -19808
071618 XDOT = -6037
500229
YDOT = 12578
044828 feet/sec YDOT = 3833
788064 meter/sec
ZDOT = 5445
405555 ZDOT = 1659
759613
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 20311
51326681
00016717 00000-0 10270-3 0 9040
2 25544 51
6439 4
2249 0001858 84
8443 275
2919 15
49377859 14079
Satellite: ISS
Catalog Number: 25544
Epoch time: 20311
51326681 = yrday
fracday
Element set: 904
Inclination: 51
6439 deg
RA of node: 4
2249 deg
Eccentricity:
0001858
Arg of perigee: 84
8443 deg
Mean anomaly: 275
2919 deg
Mean motion: 15
49377859 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1407
Checksum: 323
Coasting Arc #6 (Orbit 1410)
---------------------------------------
Vector Time (GMT): 2020/311/18:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6791845
64 A = 6803078
96 meter
Y = 67136
07 meter E =
0013218
Z = -267648
07 I = 51
67983
XDOT = 181
652576 Wp = 48
41967
YDOT = 4755
848101 meter/sec RA = 2
35099 deg
ZDOT = 6003
097742 TA = 308
70361
MA = 308
82174
Ha = 229
174 n
mi
Hp = 221
390
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22282958
15 X = 6791890
22
Y = 220262
71 feet Y = 143087
63 meter
Z = -878110
46 Z = -234655
30
XDOT = 595
973019 XDOT = 99
297666
YDOT = 15603
176185 feet/sec YDOT = 4757
418582 meter/sec
ZDOT = 19695
202565 ZDOT = 6003
780453
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17673600
70 X = 5386913
49
Y = 13581873
67 feet Y = 4139755
10 meter
Z = -725509
22 Z = -221135
21
XDOT = -8026
711565 XDOT = -2446
541685
YDOT = 11454
554318 feet/sec YDOT = 3491
348156 meter/sec
ZDOT = 19698
079504 ZDOT = 6003
974633
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 20311
77126225
00016717 00000-0 10270-3 0 9051
2 25544 51
6422 2
9486 0001944 81
5697 278
5674 15
49402683 14113
Satellite: ISS
Catalog Number: 25544
Epoch time: 20311
77126225 = yrday
fracday
Element set: 905
Inclination: 51
6422 deg
RA of node: 2
9486 deg
Eccentricity:
0001944
Arg of perigee: 81
5697 deg
Mean anomaly: 278
5674 deg
Mean motion: 15
49402683 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1411
Checksum: 308
Coasting Arc #7 (Orbit 1426)
---------------------------------------
Vector Time (GMT): 2020/312/18:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6785457
23 A = 6803119
26 meter
Y = 390244
38 meter E =
0013424
Z = 104148
36 I = 51
64747
XDOT = -372
918437 Wp = 127
05044
YDOT = -4740
495107 meter/sec RA = 357
40314 deg
ZDOT = -6006
407386 TA = 51
83006
MA = 51
70919
Ha = 229
118 n
mi
Hp = 221
459
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22261998
79 X = -6789822
65
Y = 1280329
32 feet Y = 314340
11 meter
Z = 341694
10 Z = 71176
26
XDOT = -1223
485686 XDOT = -290
705005
YDOT = -15552
805468 feet/sec YDOT = -4744
205314 meter/sec
ZDOT = -19706
060978 ZDOT = -6008
019494
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18766480
05 X = -5720023
12
Y = -12047241
59 feet Y = -3671999
24 meter
Z = 189169
04 Z = 57658
72
XDOT = 7380
826913 XDOT = 2249
676043
YDOT = -11856
021453 feet/sec YDOT = -3613
715339 meter/sec
ZDOT = -19713
239003 ZDOT = -6008
595248
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 20312
80323953
00016717 00000-0 10270-3 0 9064
2 25544 51
6437 357
8406 0001875 82
1878 277
9478 15
49395986 14273
Satellite: ISS
Catalog Number: 25544
Epoch time: 20312
80323953 = yrday
fracday
Element set: 906
Inclination: 51
6437 deg
RA of node: 357
8406 deg
Eccentricity:
0001875
Arg of perigee: 82
1878 deg
Mean anomaly: 277
9478 deg
Mean motion: 15
49395986 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1427
Checksum: 351
Coasting Arc #8 (Orbit 1442)
---------------------------------------
Vector Time (GMT): 2020/313/18:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6739982
33 A = 6803076
63 meter
Y = -879262
32 meter E =
0013745
Z = 17118
17 I = 51
61355
XDOT = 592
361784 Wp = 50
62613
YDOT = 4720
365238 meter/sec RA = 352
45316 deg
ZDOT = 6005
105274 TA = 309
55796
MA = 309
67931
Ha = 229
143 n
mi
Hp = 221
380
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22112802
93 X = 6749230
43
Y = -2884718
90 feet Y = -803839
29 meter
Z = 56161
97 Z = 49881
17
XDOT = 1943
444172 XDOT = 510
363505
YDOT = 15486
762593 feet/sec YDOT = 4726
530719 meter/sec
ZDOT = 19701
788957 ZDOT = 6007
783807
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19766824
66 X = 6024928
16
Y = 10321351
57 feet Y = 3145947
96 meter
Z = 207738
98 Z = 63318
84
XDOT = -6650
364603 XDOT = -2027
031131
YDOT = 12282
090816 feet/sec YDOT = 3743
581281 meter/sec
ZDOT = 19713
903509 ZDOT = 6008
797790
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 20313
83521233
00016717 00000-0 10270-3 0 9070
2 25544 51
6435 352
7333 0001907 84
6017 275
5351 15
49410973 14438
Satellite: ISS
Catalog Number: 25544
Epoch time: 20313
83521233 = yrday
fracday
Element set: 907
Inclination: 51
6435 deg
RA of node: 352
7333 deg
Eccentricity:
0001907
Arg of perigee: 84
6017 deg
Mean anomaly: 275
5351 deg
Mean motion: 15
49410973 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1443
Checksum: 292
Coasting Arc #9 (Orbit 1457)
---------------------------------------
Vector Time (GMT): 2020/314/18:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6664376
60 A = 6803084
45 meter
Y = 1327270
59 meter E =
0012929
Z = -184701
24 I = 51
58029
XDOT = -777
988588 Wp = 129
10131
YDOT = -4700
684014 meter/sec RA = 347
50110 deg
ZDOT = -5998
423132 TA = 52
88609
MA = 52
76802
Ha = 229
136 n
mi
Hp = 221
410
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21864752
62 X = -6677826
04
Y = 4354562
31 feet Y = 1252669
55 meter
Z = -605975
20 Z = -217107
20
XDOT = -2552
455999 XDOT = -696
229035
YDOT = -15422
191648 feet/sec YDOT = -4708
926752 meter/sec
ZDOT = -19679
865920 ZDOT = -6002
003873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20555037
19 X = -6265175
33
Y = -8620664
99 feet Y = -2627578
69 meter
Z = -755914
84 Z = -230402
84
XDOT = 5996
204494 XDOT = 1827
643130
YDOT = -12637
194882 feet/sec YDOT = -3851
817000 meter/sec
ZDOT = -19696
158000 ZDOT = -6003
388958
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 20314
80268498
00016717 00000-0 10270-3 0 9080
2 25544 51
6437 347
9451 0001955 85
4965 274
6409 15
49400431 14589
Satellite: ISS
Catalog Number: 25544
Epoch time: 20314
80268498 = yrday
fracday
Element set: 908
Inclination: 51
6437 deg
RA of node: 347
9451 deg
Eccentricity:
0001955
Arg of perigee: 85
4965 deg
Mean anomaly: 274
6409 deg
Mean motion: 15
49400431 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1458
Checksum: 333
Coasting Arc #10 (Orbit 1473)
---------------------------------------
Vector Time (GMT): 2020/315/18:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6546502
41 A = 6803025
42 meter
Y = -1801409
93 meter E =
0014188
Z = 308481
10 I = 51
54678
XDOT = 994
961869 Wp = 53
47178
YDOT = 4672
893131 meter/sec RA = 342
54703 deg
ZDOT = 5989
370991 TA = 309
85070
MA = 309
97543
Ha = 229
131 n
mi
Hp = 221
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21478026
27 X = 6564661
32
Y = -5910137
57 feet Y = -1728100
71 meter
Z = 1012077
12 Z = 340326
01
XDOT = 3264
310593 XDOT = 913
540849
YDOT = 15331
014209 feet/sec YDOT = 4683
564208 meter/sec
ZDOT = 19650
167292 ZDOT = 5994
006475
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21221715
37 X = 6468378
84
Y = 6749381
17 feet Y = 2057211
38 meter
Z = 1159434
84 Z = 353395
74
XDOT = -5241
874909 XDOT = -1597
723472
YDOT = 13012
151130 feet/sec YDOT = 3966
103664 meter/sec
ZDOT = 19671
342237 ZDOT = 5995
825114
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 20315
83465310
00016717 00000-0 10270-3 0 9097
2 25544 51
6431 342
8382 0001896 89
7959 270
3408 15
49411313 14745
Satellite: ISS
Catalog Number: 25544
Epoch time: 20315
83465310 = yrday
fracday
Element set: 909
Inclination: 51
6431 deg
RA of node: 342
8382 deg
Eccentricity:
0001896
Arg of perigee: 89
7959 deg
Mean anomaly: 270
3408 deg
Mean motion: 15
49411313 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1474
Checksum: 316
Coasting Arc #11 (Orbit 1488)
---------------------------------------
Vector Time (GMT): 2020/316/18:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6404169
32 A = 6802961
52 meter
Y = 2229271
62 meter E =
0012312
Z = -478673
01 I = 51
51583
XDOT = -1180
016815 Wp = 131
82849
YDOT = -4649
274972 meter/sec RA = 337
59016 deg
ZDOT = -5972
467179 TA = 53
33248
MA = 53
21937
Ha = 229
081 n
mi
Hp = 221
417
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21011054
21 X = -6426296
58
Y = 7313883
26 feet Y = 2157531
88 meter
Z = -1570449
52 Z = -509836
30
XDOT = -3871
446244 XDOT = -1098
928132
YDOT = -15253
526810 feet/sec YDOT = -4662
017372 meter/sec
ZDOT = -19594
708594 ZDOT = -5978
002396
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21680477
17 X = -6608209
44
Y = -4943726
99 feet Y = -1506847
99 meter
Z = -1714663
90 Z = -522629
56
XDOT = 4566
211761 XDOT = 1391
781345
YDOT = -13331
847662 feet/sec YDOT = -4063
547167 meter/sec
ZDOT = -19620
047852 ZDOT = -5980
190585
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 20316
80212009
00016717 00000-0 10270-3 0 9102
2 25544 51
6443 338
0497 0001861 92
5544 267
5820 15
49410513 14899
Satellite: ISS
Catalog Number: 25544
Epoch time: 20316
80212009 = yrday
fracday
Element set: 910
Inclination: 51
6443 deg
RA of node: 338
0497 deg
Eccentricity:
0001861
Arg of perigee: 92
5544 deg
Mean anomaly: 267
5820 deg
Mean motion: 15
49410513 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1489
Checksum: 295
Coasting Arc #12 (Orbit 1504)
---------------------------------------
Vector Time (GMT): 2020/317/18:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6218146
19 A = 6802894
87 meter
Y = -2675648
66 meter E =
0014632
Z = 606199
05 I = 51
48423
XDOT = 1395
677740 Wp = 56
35985
YDOT = 4614
443794 meter/sec RA = 332
63091 deg
ZDOT = 5955
055106 TA = 310
18577
MA = 310
31377
Ha = 229
123 n
mi
Hp = 221
360
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20400742
09 X = 6244659
31
Y = -8778374
86 feet Y = -2605964
64 meter
Z = 1988842
02 Z = 636469
48
XDOT = 4578
995211 XDOT = 1315
046953
YDOT = 15139
251292 feet/sec YDOT = 4629
600400 meter/sec
ZDOT = 19537
582369 ZDOT = 5961
639107
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21992680
50 X = 6703369
02
Y = 2999210
37 feet Y = 914159
32 meter
Z = 2128938
04 Z = 648900
31
XDOT = -3785
383416 XDOT = -1153
784865
YDOT = 13658
992644 feet/sec YDOT = 4163
260958 meter/sec
ZDOT = 19567
773755 ZDOT = 5964
257440
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 20317
83408123
00016717 00000-0 10270-3 0 9111
2 25544 51
6437 332
9420 0001908 92
2711 267
8658 15
49413528 15056
Satellite: ISS
Catalog Number: 25544
Epoch time: 20317
83408123 = yrday
fracday
Element set: 911
Inclination: 51
6437 deg
RA of node: 332
9420 deg
Eccentricity:
0001908
Arg of perigee: 92
2711 deg
Mean anomaly: 267
8658 deg
Mean motion: 15
49413528 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1505
Checksum: 301
Coasting Arc #13 (Orbit 1504)
---------------------------------------
Vector Time (GMT): 2020/317/19:40:57
948
Vector Time (MET): N/A
Weight (LBS) : 938222
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -700502
01 A = 6792718
40 meter
Y = -4318725
16 meter E =
0014245
Z = -5208682
03 I = 51
44673
XDOT = 7085
016625 Wp = 99
34475
YDOT = -2614
940285 meter/sec RA = 332
36998 deg
ZDOT = 1215
897141 TA = 182
37932
MA = 182
38610
Ha = 229
086 n
mi
Hp = 222
538
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2298234
95 X = -626855
24
Y = -14169045
79 feet Y = -4326146
86 meter
Z = -17088851
80 Z = -5211906
02
XDOT = 23244
805200 XDOT = 7107
824825
YDOT = -8579
200409 feet/sec YDOT = -2535
583019 meter/sec
ZDOT = 3989
163849 ZDOT = 1250
369602
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1130121
94 X = 344461
17
Y = -14292125
90 feet Y = -4356239
97 meter
Z = -17103524
78 Z = -5213154
35
XDOT = 23524
153360 XDOT = 7170
161944
YDOT = -3102
322045 feet/sec YDOT = -945
587759 meter/sec
ZDOT = 4148
683390 ZDOT = 1264
518697
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 20317
83408092
00016717 00000-0 10270-3 0 9127
2 25544 51
6453 332
9421 0000243 106
7194 253
3983 15
49048324 15051
Satellite: ISS
Catalog Number: 25544
Epoch time: 20317
83408092 = yrday
fracday
Element set: 912
Inclination: 51
6453 deg
RA of node: 332
9421 deg
Eccentricity:
0000243
Arg of perigee: 106
7194 deg
Mean anomaly: 253
3983 deg
Mean motion: 15
49048324 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1505
Checksum: 292
Coasting Arc #14 (Orbit 1520)
---------------------------------------
Vector Time (GMT): 2020/318/19:40:57
948
Vector Time (MET): N/A
Weight (LBS) : 938222
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1040148
07 A = 6792631
72 meter
Y = 4251343
60 meter E =
0004317
Z = 5191923
75 I = 51
41654
XDOT = -6850
197240 Wp = 56
55303
YDOT = 3200
245406 meter/sec RA = 327
41011 deg
ZDOT = -1245
033439 TA = 45
46124
MA = 45
42599
Ha = 228
954 n
mi
Hp = 222
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3412559
27 X = 967310
83
Y = 13947977
68 feet Y = 4262567
89 meter
Z = 17033870
56 Z = 5196799
72
XDOT = -22474
400395 XDOT = -6879
426394
YDOT = 10499
492802 feet/sec YDOT = 3123
478184 meter/sec
ZDOT = -4084
755376 ZDOT = -1278
380880
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 252073
42 X = 76831
98
Y = 14330645
24 feet Y = 4367980
67 meter
Z = 17056185
23 Z = 5198725
26
XDOT = -23121
010599 XDOT = -7047
284031
YDOT = 5464
038953 feet/sec YDOT = 1665
439073 meter/sec
ZDOT = -4239
091990 ZDOT = -1292
075239
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 20318
86629564
00016717 00000-0 10270-3 0 9131
2 25544 51
6445 327
8363 0000139 107
3370 252
7796 15
49082296 15216
Satellite: ISS
Catalog Number: 25544
Epoch time: 20318
86629564 = yrday
fracday
Element set: 913
Inclination: 51
6445 deg
RA of node: 327
8363 deg
Eccentricity:
0000139
Arg of perigee: 107
3370 deg
Mean anomaly: 252
7796 deg
Mean motion: 15
49082296 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1521
Checksum: 321
Coasting Arc #15 (Orbit 1535)
---------------------------------------
Vector Time (GMT): 2020/319/19:40:57
948
Vector Time (MET): N/A
Weight (LBS) : 938222
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1385571
17 A = 6792729
14 meter
Y = -4167451
02 meter E =
0014056
Z = -5194555
27 I = 51
38873
XDOT = 6543
475689 Wp = 99
81899
YDOT = -3754
119623 meter/sec RA = 322
44784 deg
ZDOT = 1267
046983 TA = 182
41570
MA = 182
42250
Ha = 229
023 n
mi
Hp = 222
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4545837
18 X = -1313633
56
Y = -13672739
57 feet Y = -4182542
95 meter
Z = -17042504
16 Z = -5201111
54
XDOT = 21468
096093 XDOT = 6578
814286
YDOT = -12316
665431 feet/sec YDOT = -3680
748262 meter/sec
ZDOT = 4156
978291 ZDOT = 1298
919211
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1663694
18 X = -507093
98
Y = -14276349
09 feet Y = -4351431
20 meter
Z = -17072591
18 Z = -5203725
79
XDOT = 22395
919629 XDOT = 6826
276303
YDOT = -7755
201584 feet/sec YDOT = -2363
785443 meter/sec
ZDOT = 4304
515564 ZDOT = 1312
016344
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 20319
83399727
00016717 00000-0 10270-3 0 9145
2 25544 51
6445 323
0493 0000127 122
6812 237
4350 15
49058548 15361
Satellite: ISS
Catalog Number: 25544
Epoch time: 20319
83399727 = yrday
fracday
Element set: 914
Inclination: 51
6445 deg
RA of node: 323
0493 deg
Eccentricity:
0000127
Arg of perigee: 122
6812 deg
Mean anomaly: 237
4350 deg
Mean motion: 15
49058548 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1536
Checksum: 310
Coasting Arc #16 (Orbit 1539)
---------------------------------------
Vector Time (GMT): 2020/320/00:49:48
000
Vector Time (MET): N/A
Weight (LBS) : 938222
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5791929
08 A = 6799289
07 meter
Y = -1212321
28 meter E =
0012585
Z = 3338054
36 I = 51
40045
XDOT = -1453
363275 Wp = 91
04334
YDOT = 5911
763245 meter/sec RA = 321
41433 deg
ZDOT = 4653
333176 TA = 307
90877
MA = 308
02249
Ha = 228
935 n
mi
Hp = 222
567
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19002391
99 X = 5788840
31
Y = -3977432
03 feet Y = -1147569
26 meter
Z = 10951621
93 Z = 3366182
56
XDOT = -4768
252215 XDOT = -1541
966292
YDOT = 19395
548703 feet/sec YDOT = 5895
014987 meter/sec
ZDOT = 15266
841129 ZDOT = 4646
058262
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4025823
06 X = 1227070
87
Y = -18916585
88 feet Y = -5765775
38 meter
Z = 11081715
44 Z = 3377706
87
XDOT = 14383
703716 XDOT = 4384
152893
YDOT = 12014
265570 feet/sec YDOT = 3661
948146 meter/sec
ZDOT = 15232
897730 ZDOT = 4642
987228
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 20320
09204948
00016717 00000-0 10270-3 0 9156
2 25544 51
6399 321
7678 0000480 166
0935 194
0228 15
49062300 15407
Satellite: ISS
Catalog Number: 25544
Epoch time: 20320
09204948 = yrday
fracday
Element set: 915
Inclination: 51
6399 deg
RA of node: 321
7678 deg
Eccentricity:
0000480
Arg of perigee: 166
0935 deg
Mean anomaly: 194
0228 deg
Mean motion: 15
49062300 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1540
Checksum: 297
Coasting Arc #17 (Orbit 1544)
---------------------------------------
Vector Time (GMT): 2020/320/09:04:15
000
Vector Time (MET): N/A
Weight (LBS) : 965317
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3554408
34 A = 6802012
23 meter
Y = 5347273
26 meter E =
0014058
Z = 2224828
70 I = 51
40372
XDOT = -5260
230069 Wp = 109
19724
YDOT = -1225
198331 meter/sec RA = 319
66824 deg
ZDOT = -5435
428249 TA = 46
03697
MA = 45
92109
Ha = 229
030 n
mi
Hp = 222
582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11661444
70 X = -3624746
26
Y = 17543547
45 feet Y = 5307131
87 meter
Z = 7299306
77 Z = 2207391
82
XDOT = -17257
972667 XDOT = -5219
735595
YDOT = -4019
679563 feet/sec YDOT = -1283
795174 meter/sec
ZDOT = -17832
769847 ZDOT = -5460
882882
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8463118
95 X = 2579558
66
Y = -19321368
38 feet Y = -5889153
08 meter
Z = 7218418
84 Z = 2200174
06
XDOT = 16165
505497 XDOT = 4927
246076
YDOT = 345
248938 feet/sec YDOT = 105
231876 meter/sec
ZDOT = -17950
373883 ZDOT = -5471
273959
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 20320
41461535
00016717 00000-0 10270-3 0 9160
2 25544 51
6431 320
1748 0000261 143
4756 216
6412 15
49078331 15454
Satellite: ISS
Catalog Number: 25544
Epoch time: 20320
41461535 = yrday
fracday
Element set: 916
Inclination: 51
6431 deg
RA of node: 320
1748 deg
Eccentricity:
0000261
Arg of perigee: 143
4756 deg
Mean anomaly: 216
6412 deg
Mean motion: 15
49078331 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1545
Checksum: 278
Coasting Arc #18 (Orbit 1559)
---------------------------------------
Vector Time (GMT): 2020/321/09:04:15
000
Vector Time (MET): N/A
Weight (LBS) : 965317
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3089226
14 A = 6802030
95 meter
Y = -5638528
90 meter E =
0006177
Z = -2216388
55 I = 51
37933
XDOT = 5331
737767 Wp = 46
04542
YDOT = 788
864317 meter/sec RA = 314
70314 deg
ZDOT = 5438
241972 TA = 289
30048
MA = 289
36727
Ha = 229
089 n
mi
Hp = 222
532
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10135256
35 X = 3162814
50
Y = -18499110
58 feet Y = -5603571
27 meter
Z = -7271615
97 Z = -2201203
75
XDOT = 17492
577977 XDOT = 5296
103629
YDOT = 2588
137523 feet/sec YDOT = 848
287830 meter/sec
ZDOT = 17842
001221 ZDOT = 5464
055672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6448258
14 X = -1965429
08
Y = 20109217
81 feet Y = 6129289
59 meter
Z = -7201127
57 Z = -2194903
68
XDOT = -16077
665923 XDOT = -4900
472573
YDOT = 1260
214128 feet/sec YDOT = 384
113266 meter/sec
ZDOT = 17961
287371 ZDOT = 5474
600391
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 20321
38231219
00016717 00000-0 10270-3 0 9172
2 25544 51
6437 315
3877 0000400 131
4161 228
7024 15
49072947 15608
Satellite: ISS
Catalog Number: 25544
Epoch time: 20321
38231219 = yrday
fracday
Element set: 917
Inclination: 51
6437 deg
RA of node: 315
3877 deg
Eccentricity:
0000400
Arg of perigee: 131
4161 deg
Mean anomaly: 228
7024 deg
Mean motion: 15
49072947 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1560
Checksum: 284
Coasting Arc #19 (Orbit 1575)
---------------------------------------
Vector Time (GMT): 2020/322/09:04:15
000
Vector Time (MET): N/A
Weight (LBS) : 965317
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2628214
38 A = 6802111
44 meter
Y = 5878167
98 meter E =
0014182
Z = 2172056
83 I = 51
35647
XDOT = -5365
045708 Wp = 109
41976
YDOT = -372
834677 meter/sec RA = 309
73692 deg
ZDOT = -5458
171528 TA = 46
42326
MA = 46
30561
Ha = 229
077 n
mi
Hp = 222
533
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8622750
58 X = -2704301
31
Y = 19285328
02 feet Y = 5848351
71 meter
Z = 7126170
71 Z = 2159105
63
XDOT = -17601
855998 XDOT = -5333
964608
YDOT = -1223
210883 feet/sec YDOT = -432
656030 meter/sec
ZDOT = -17907
386904 ZDOT = -5484
157902
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4457217
83 X = 1358559
99
Y = -20670337
57 feet Y = -6300318
89 meter
Z = 7066000
80 Z = 2153717
05
XDOT = 15842
239384 XDOT = 4828
714564
YDOT = -2774
278552 feet/sec YDOT = -845
600103 meter/sec
ZDOT = -18027
494570 ZDOT = -5494
780345
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 20322
41451797
00016717 00000-0 10270-3 0 9183
2 25544 51
6435 310
2816 0000325 114
8706 245
2478 15
49073582 15769
Satellite: ISS
Catalog Number: 25544
Epoch time: 20322
41451797 = yrday
fracday
Element set: 918
Inclination: 51
6435 deg
RA of node: 310
2816 deg
Eccentricity:
0000325
Arg of perigee: 114
8706 deg
Mean anomaly: 245
2478 deg
Mean motion: 15
49073582 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1576
Checksum: 306
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