[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 20th 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) : 16464 4774 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 497 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
328/13:07:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
6
000/00:00:00
000 0
0 0
0 222
1
335/15:02:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
6
000/00:00:00
000 0
0 0
0 221
8
337/17:50:56
000 0
0 0
0 0
0
N/A 0
0 0
0 229
7
000/00:00:00
000 0
0 0
0 221
9
338/19:27:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
6
000/00:00:00
000 0
0 0
0 221
9
Coasting Arc #1 (Orbit 1599)
---------------------------------------
Vector Time (GMT): 2020/323/21:45:59
942
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5093721
52 A = 6797699
43 meter
Y = -2223961
22 meter E =
0012173
Z = 3903727
48 I = 51
30903
XDOT = -267
630139 Wp = 93
81926
YDOT = 6505
036025 meter/sec RA = 302
18393 deg
ZDOT = 4043
400851 TA = 313
60349
MA = 313
70444
Ha = 229
419 n
mi
Hp = 222
241
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16711684
77 X = 5099249
66
Y = -7296460
69 feet Y = -2166969
11 meter
Z = 12807504
86 Z = 3928484
24
XDOT = -878
051636 XDOT = -359
992277
YDOT = 21341
981710 feet/sec YDOT = 6501
526292 meter/sec
ZDOT = 13265
750823 ZDOT = 4041
877219
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12222231
06 X = 3725336
03
Y = -13423426
88 feet Y = -4091460
51 meter
Z = 12922058
90 Z = 3938643
55
XDOT = 6811
847220 XDOT = 2076
251033
YDOT = 19002
240621 feet/sec YDOT = 5791
882941 meter/sec
ZDOT = 13258
392771 ZDOT = 4041
158117
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 20323
96292059
00016717 00000-0 10270-3 0 9009
2 25544 51
6421 302
6218 0001595 51
2603 308
8689 15
49012552 16003
Satellite: ISS
Catalog Number: 25544
Epoch time: 20323
96292059 = yrday
fracday
Element set: 900
Inclination: 51
6421 deg
RA of node: 302
6218 deg
Eccentricity:
0001595
Arg of perigee: 51
2603 deg
Mean anomaly: 308
8689 deg
Mean motion: 15
49012552 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1600
Checksum: 286
Coasting Arc #2 (Orbit 1614)
---------------------------------------
Vector Time (GMT): 2020/324/21:45:59
942
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4892174
61 A = 6797591
25 meter
Y = 2628894
80 meter E =
0008414
Z = -3928717
94 I = 51
29147
XDOT = -273
976185 Wp = 69
88638
YDOT = -6506
634473 meter/sec RA = 297
21329 deg
ZDOT = -4016
944807 TA = 157
85133
MA = 157
81496
Ha = 229
593 n
mi
Hp = 222
024
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16050441
62 X = -4902124
50
Y = 8624982
95 feet Y = 2574131
76 meter
Z = -12889494
54 Z = -3952506
28
XDOT = -898
871998 XDOT = -181
684505
YDOT = -21347
225961 feet/sec YDOT = -6509
181827 meter/sec
ZDOT = -13178
952779 ZDOT = -4018
052187
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10828738
05 X = -3300599
36
Y = 14556621
93 feet Y = 4436858
36 meter
Z = -12999587
18 Z = -3962274
17
XDOT = -8683
778665 XDOT = -2646
815737
YDOT = -18221
267670 feet/sec YDOT = -5553
842386 meter/sec
ZDOT = -13183
773470 ZDOT = -4018
414154
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 20324
93063844
00016717 00000-0 10270-3 0 9016
2 25544 51
6417 297
8343 0001767 58
2646 301
8676 15
49028315 16156
Satellite: ISS
Catalog Number: 25544
Epoch time: 20324
93063844 = yrday
fracday
Element set: 901
Inclination: 51
6417 deg
RA of node: 297
8343 deg
Eccentricity:
0001767
Arg of perigee: 58
2646 deg
Mean anomaly: 301
8676 deg
Mean motion: 15
49028315 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1615
Checksum: 316
Coasting Arc #3 (Orbit 1630)
---------------------------------------
Vector Time (GMT): 2020/325/21:45:59
942
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4640117
38 A = 6797568
61 meter
Y = -3031946
25 meter E =
0012328
Z = 3925111
73 I = 51
27674
XDOT = 827
484690 Wp = 95
26946
YDOT = 6476
847224 meter/sec RA = 292
24184 deg
ZDOT = 4012
770728 TA = 312
52534
MA = 312
62939
Ha = 229
449 n
mi
Hp = 222
135
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15223482
21 X = 4654610
61
Y = -9947330
22 feet Y = -2979976
42 meter
Z = 12877663
15 Z = 3947686
67
XDOT = 2714
844782 XDOT = 735
505275
YDOT = 21249
498766 feet/sec YDOT = 6485
586126 meter/sec
ZDOT = 13165
258295 ZDOT = 4016
567488
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9254503
77 X = 2820772
75
Y = -15567778
60 feet Y = -4745058
92 meter
Z = 12982158
01 Z = 3956961
76
XDOT = 10525
664748 XDOT = 3208
222615
YDOT = 17282
885589 feet/sec YDOT = 5267
823528 meter/sec
ZDOT = 13182
531273 ZDOT = 4018
035532
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 20325
96286668
00016717 00000-0 10270-3 0 9022
2 25544 51
6414 292
7278 0001625 62
4493 297
6822 15
49036388 16316
Satellite: ISS
Catalog Number: 25544
Epoch time: 20325
96286668 = yrday
fracday
Element set: 902
Inclination: 51
6414 deg
RA of node: 292
7278 deg
Eccentricity:
0001625
Arg of perigee: 62
4493 deg
Mean anomaly: 297
6822 deg
Mean motion: 15
49036388 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1631
Checksum: 332
Coasting Arc #4 (Orbit 1645)
---------------------------------------
Vector Time (GMT): 2020/326/21:45:59
942
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4375301
50 A = 6797492
94 meter
Y = 3393005
97 meter E =
0008704
Z = -3952680
56 I = 51
26412
XDOT = -1360
188245 Wp = 72
10030
YDOT = -6389
473514 meter/sec RA = 287
26985 deg
ZDOT = -3983
801831 TA = 156
04779
MA = 156
00727
Ha = 229
673 n
mi
Hp = 221
908
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14354663
70 X = -4393717
97
Y = 11131909
34 feet Y = 3343975
50 meter
Z = -12968112
07 Z = -3973978
68
XDOT = -4462
559859 XDOT = -1269
286993
YDOT = -20962
839612 feet/sec YDOT = -6404
175587 meter/sec
ZDOT = -13070
215982 ZDOT = -3990
188775
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7673564
27 X = -2338902
39
Y = 16386738
10 feet Y = 4994677
77 meter
Z = -13066710
84 Z = -3982733
46
XDOT = -12201
791254 XDOT = -3719
105974
YDOT = -16147
220921 feet/sec YDOT = -4921
672937 meter/sec
ZDOT = -13099
485757 ZDOT = -3992
723259
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 20326
93058046
00016717 00000-0 10270-3 0 9038
2 25544 51
6407 287
9410 0001919 70
0338 290
1018 15
49038568 16464
Satellite: ISS
Catalog Number: 25544
Epoch time: 20326
93058046 = yrday
fracday
Element set: 903
Inclination: 51
6407 deg
RA of node: 287
9410 deg
Eccentricity:
0001919
Arg of perigee: 70
0338 deg
Mean anomaly: 290
1018 deg
Mean motion: 15
49038568 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1646
Checksum: 306
Coasting Arc #5 (Orbit 1661)
---------------------------------------
Vector Time (GMT): 2020/327/21:45:59
942
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4060919
20 A = 6797462
22 meter
Y = -3746260
44 meter E =
0012448
Z = 3950274
16 I = 51
25470
XDOT = 1900
929595 Wp = 97
36857
YDOT = 6268
583480 meter/sec RA = 282
29668 deg
ZDOT = 3978
269375 TA = 310
85239
MA = 310
96022
Ha = 229
484 n
mi
Hp = 222
066
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13323225
71 X = 4083320
89
Y = -12290880
72 feet Y = -3700723
29 meter
Z = 12960217
07 Z = 3970054
86
XDOT = 6236
645653 XDOT = 1811
366824
YDOT = 20566
218767 feet/sec YDOT = 6289
340047 meter/sec
ZDOT = 13052
064880 ZDOT = 3987
286220
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5936488
25 X = 1809441
62
Y = -17057251
23 feet Y = -5199050
17 meter
Z = 13051804
72 Z = 3978190
08
XDOT = 13820
068608 XDOT = 4212
356912
YDOT = 14859
592005 feet/sec YDOT = 4529
203643 meter/sec
ZDOT = 13093
515618 ZDOT = 3990
903560
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 20327
96280431
00016717 00000-0 10270-3 0 9048
2 25544 51
6402 282
8345 0001631 76
8127 283
3205 15
49048524 16624
Satellite: ISS
Catalog Number: 25544
Epoch time: 20327
96280431 = yrday
fracday
Element set: 904
Inclination: 51
6402 deg
RA of node: 282
8345 deg
Eccentricity:
0001631
Arg of perigee: 76
8127 deg
Mean anomaly: 283
3205 deg
Mean motion: 15
49048524 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1662
Checksum: 296
Coasting Arc #6 (Orbit 1671)
---------------------------------------
Vector Time (GMT): 2020/328/13:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2393643
03 A = 6802889
42 meter
Y = -6117434
67 meter E =
0015711
Z = 1739537
53 I = 51
27103
XDOT = 4070
560920 Wp = 65
31930
YDOT = 3207
498374 meter/sec RA = 279
10819 deg
ZDOT = 5644
744034 TA = 313
83646
MA = 313
96621
Ha = 229
625 n
mi
Hp = 222
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7853159
54 X = 2453422
38
Y = -20070323
72 feet Y = -6090333
07 meter
Z = 5707144
14 Z = 1751309
91
XDOT = 13354
858662 XDOT = 4006
971994
YDOT = 10523
288627 feet/sec YDOT = 3252
662486 meter/sec
ZDOT = 18519
501424 ZDOT = 5664
363108
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18197109
95 X = 5546479
11
Y = 11520785
69 feet Y = 3511535
48 meter
Z = 5761787
01 Z = 1756192
68
XDOT = -12027
277083 XDOT = -3665
914055
YDOT = 9634
743498 feet/sec YDOT = 2936
669818 meter/sec
ZDOT = 18610
087216 ZDOT = 5672
354583
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 20328
60794448
00016717 00000-0 10270-3 0 9059
2 25544 51
6428 279
6468 0001807 68
3174 291
8168 15
49032069 16725
Satellite: ISS
Catalog Number: 25544
Epoch time: 20328
60794448 = yrday
fracday
Element set: 905
Inclination: 51
6428 deg
RA of node: 279
6468 deg
Eccentricity:
0001807
Arg of perigee: 68
3174 deg
Mean anomaly: 291
8168 deg
Mean motion: 15
49032069 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1672
Checksum: 338
Coasting Arc #7 (Orbit 1686)
---------------------------------------
Vector Time (GMT): 2020/329/13:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1887667
58 A = 6802803
59 meter
Y = 6286013
92 meter E =
0008134
Z = -1782298
07 I = 51
26754
XDOT = -4316
665739 Wp = 128
41049
YDOT = -2885
399205 meter/sec RA = 274
13448 deg
ZDOT = -5627
185652 TA = 71
21958
MA = 71
13135
Ha = 229
666 n
mi
Hp = 222
007
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6193135
09 X = -1949161
90
Y = 20623405
25 feet Y = 6264560
91 meter
Z = -5847434
61 Z = -1791616
81
XDOT = -14162
289170 XDOT = -4256
745530
YDOT = -9466
532825 feet/sec YDOT = -2933
335975 meter/sec
ZDOT = -18461
895185 ZDOT = -5648
009171
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19227841
01 X = -5860645
94
Y = -9667561
96 feet Y = -2946672
89 meter
Z = -5890724
38 Z = -1795492
79
XDOT = 11072
898862 XDOT = 3375
019573
YDOT = -10759
592141 feet/sec YDOT = -3279
523685 meter/sec
ZDOT = -18558
068613 ZDOT = -5656
499313
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 20329
57564948
00016717 00000-0 10270-3 0 9067
2 25544 51
6436 274
8595 0001906 68
6032 291
5321 15
49038318 16875
Satellite: ISS
Catalog Number: 25544
Epoch time: 20329
57564948 = yrday
fracday
Element set: 906
Inclination: 51
6436 deg
RA of node: 274
8595 deg
Eccentricity:
0001906
Arg of perigee: 68
6032 deg
Mean anomaly: 291
5321 deg
Mean motion: 15
49038318 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1687
Checksum: 336
Coasting Arc #8 (Orbit 1702)
---------------------------------------
Vector Time (GMT): 2020/330/13:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1338198
80 A = 6802821
20 meter
Y = -6418710
31 meter E =
0015834
Z = 1785258
04 I = 51
26570
XDOT = 4550
235769 Wp = 66
36319
YDOT = 2522
769632 meter/sec RA = 269
16123 deg
ZDOT = 5626
012212 TA = 313
31822
MA = 313
45012
Ha = 229
683 n
mi
Hp = 221
995
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4390416
01 X = 1401203
41
Y = -21058760
85 feet Y = -6403393
41 meter
Z = 5857145
79 Z = 1791911
31
XDOT = 14928
595042 XDOT = 4494
358837
YDOT = 8276
803254 feet/sec YDOT = 2573
340941 meter/sec
ZDOT = 18458
045315 ZDOT = 5647
980225
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20106126
81 X = 6128347
45
Y = 7624121
35 feet Y = 2323832
19 meter
Z = 5888102
92 Z = 1794693
77
XDOT = -9957
324810 XDOT = -3034
992602
YDOT = 11841
076372 feet/sec YDOT = 3609
160078 meter/sec
ZDOT = 18559
528997 ZDOT = 5656
944438
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 20330
60786565
00016717 00000-0 10270-3 0 9075
2 25544 51
6430 269
7538 0001936 72
3863 287
7498 15
49035713 17033
Satellite: ISS
Catalog Number: 25544
Epoch time: 20330
60786565 = yrday
fracday
Element set: 907
Inclination: 51
6430 deg
RA of node: 269
7538 deg
Eccentricity:
0001936
Arg of perigee: 72
3863 deg
Mean anomaly: 287
7498 deg
Mean motion: 15
49035713 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1703
Checksum: 332
Coasting Arc #9 (Orbit 1717)
---------------------------------------
Vector Time (GMT): 2020/331/13:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -814247
26 A = 6802734
26 meter
Y = 6499106
39 meter E =
0008203
Z = -1830526
39 I = 51
26821
XDOT = -4741
564952 Wp = 129
35553
YDOT = -2167
297928 meter/sec RA = 264
18796 deg
ZDOT = -5607
691919 TA = 70
82867
MA = 70
73990
Ha = 229
670 n
mi
Hp = 221
999
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2671414
91 X = -877969
91
Y = 21322527
53 feet Y = 6489644
70 meter
Z = -6005664
00 Z = -1834636
16
XDOT = -15556
315458 XDOT = -4689
737695
YDOT = -7110
557506 feet/sec YDOT = -2220
031407 meter/sec
ZDOT = -18397
939367 ZDOT = -5630
599263
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20738036
09 X = -6320953
40
Y = -5611564
54 feet Y = -1710404
87 meter
Z = -6024851
90 Z = -1836374
86
XDOT = 8807
640179 XDOT = 2684
568727
YDOT = -12760
213249 feet/sec YDOT = -3889
312998 meter/sec
ZDOT = -18503
783742 ZDOT = -5639
953285
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 20331
57556590
00016717 00000-0 10270-3 0 9086
2 25544 51
6440 264
9671 0001858 76
3199 283
8158 15
49040660 17181
Satellite: ISS
Catalog Number: 25544
Epoch time: 20331
57556590 = yrday
fracday
Element set: 908
Inclination: 51
6440 deg
RA of node: 264
9671 deg
Eccentricity:
0001858
Arg of perigee: 76
3199 deg
Mean anomaly: 283
8158 deg
Mean motion: 15
49040660 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1718
Checksum: 331
Coasting Arc #10 (Orbit 1733)
---------------------------------------
Vector Time (GMT): 2020/332/13:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 253463
13 A = 6802737
72 meter
Y = -6537812
10 meter E =
0015726
Z = 1836102
97 I = 51
27299
XDOT = 4914
120478 Wp = 67
58505
YDOT = 1774
031233 meter/sec RA = 259
21456 deg
ZDOT = 5605
675612 TA = 312
67878
MA = 312
81115
Ha = 229
662 n
mi
Hp = 222
007
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 831571
96 X = 317633
17
Y = -21449514
77 feet Y = -6534619
03 meter
Z = 6023959
88 Z = 1837489
61
XDOT = 16122
442514 XDOT = 4866
687755
YDOT = 5820
312443 feet/sec YDOT = 1828
718835 meter/sec
ZDOT = 18391
324187 ZDOT = 5629
431914
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21185665
06 X = 6457390
71
Y = 3444035
34 feet Y = 1049741
97 meter
Z = 6030547
66 Z = 1838110
93
XDOT = -7508
754663 XDOT = -2288
668421
YDOT = 13605
787419 feet/sec YDOT = 4147
044005 meter/sec
ZDOT = 18501
112559 ZDOT = 5639
139108
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 20332
60777643
00016717 00000-0 10270-3 0 9096
2 25544 51
6441 259
8611 0001849 78
1086 282
0271 15
49041513 17347
Satellite: ISS
Catalog Number: 25544
Epoch time: 20332
60777643 = yrday
fracday
Element set: 909
Inclination: 51
6441 deg
RA of node: 259
8611 deg
Eccentricity:
0001849
Arg of perigee: 78
1086 deg
Mean anomaly: 282
0271 deg
Mean motion: 15
49041513 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1734
Checksum: 307
Coasting Arc #11 (Orbit 1748)
---------------------------------------
Vector Time (GMT): 2020/333/13:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 272066
10 A = 6802662
86 meter
Y = 6528676
63 meter E =
0008199
Z = -1885030
82 I = 51
28160
XDOT = -5047
101801 Wp = 130
19594
YDOT = -1396
366223 meter/sec RA = 254
24195 deg
ZDOT = -5586
026785 TA = 70
61290
MA = 70
52429
Ha = 229
669 n
mi
Hp = 222
012
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 892605
31 X = 208196
84
Y = 21419542
74 feet Y = 6531362
12 meter
Z = -6184484
33 Z = -1883863
73
XDOT = -16558
732942 XDOT = -5003
977774
YDOT = -4581
254013 feet/sec YDOT = -1452
564903 meter/sec
ZDOT = -18326
859530 ZDOT = -5610
439563
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21396427
89 X = -6521631
22
Y = -1360549
93 feet Y = -414695
62 meter
Z = -6179253
95 Z = -1883436
60
XDOT = 6213
664470 XDOT = 1893
924931
YDOT = -14288
352259 feet/sec YDOT = -4355
089769 meter/sec
ZDOT = -18439
702354 ZDOT = -5620
421278
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 20333
57546928
00016717 00000-0 10270-3 0 9105
2 25544 51
6454 255
0744 0001807 82
9920 277
1435 15
49039882 17499
Satellite: ISS
Catalog Number: 25544
Epoch time: 20333
57546928 = yrday
fracday
Element set: 910
Inclination: 51
6454 deg
RA of node: 255
0744 deg
Eccentricity:
0001807
Arg of perigee: 82
9920 deg
Mean anomaly: 277
1435 deg
Mean motion: 15
49039882 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1749
Checksum: 328
Coasting Arc #12 (Orbit 1764)
---------------------------------------
Vector Time (GMT): 2020/334/13:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -827527
97 A = 6802637
28 meter
Y = -6473600
89 meter E =
0015770
Z = 1893558
31 I = 51
29136
XDOT = 5155
970744 Wp = 68
78130
YDOT = 983
315384 meter/sec RA = 249
26980 deg
ZDOT = 5582
862924 TA = 312
14041
MA = 312
27430
Ha = 229
689 n
mi
Hp = 221
969
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2714986
79 X = -764274
72
Y = -21238848
07 feet Y = -6482501
45 meter
Z = 6212461
63 Z = 1889691
32
XDOT = 16915
914516 XDOT = 5117
472869
YDOT = 3226
100341 feet/sec YDOT = 1040
757268 meter/sec
ZDOT = 18316
479411 ZDOT = 5607
815764
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21400366
36 X = 6522831
67
Y = -839094
08 feet Y = -255755
88 meter
Z = 6194734
93 Z = 1888155
21
XDOT = -4782
920042 XDOT = -1457
834029
YDOT = 14871
800651 feet/sec YDOT = 4532
924838 meter/sec
ZDOT = 18431
840682 ZDOT = 5618
025040
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 20334
60767322
00016717 00000-0 10270-3 0 9114
2 25544 51
6448 249
9686 0001918 82
1920 277
9448 15
49048989 17652
Satellite: ISS
Catalog Number: 25544
Epoch time: 20334
60767322 = yrday
fracday
Element set: 911
Inclination: 51
6448 deg
RA of node: 249
9686 deg
Eccentricity:
0001918
Arg of perigee: 82
1920 deg
Mean anomaly: 277
9448 deg
Mean motion: 15
49048989 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1765
Checksum: 350
Coasting Arc #13 (Orbit 1779)
---------------------------------------
Vector Time (GMT): 2020/335/13:07:30
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1340842
36 A = 6802588
33 meter
Y = 6377373
64 meter E =
0008163
Z = -1944333
58 I = 51
30445
XDOT = -5228
800908 Wp = 131
59440
YDOT = -590
234633 meter/sec RA = 244
29952 deg
ZDOT = -5562
343556 TA = 69
89428
MA = 69
80645
Ha = 229
647 n
mi
Hp = 222
056
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4399089
11 X = 1278873
63
Y = 20923141
87 feet Y = 6392021
67 meter
Z = -6379047
18 Z = -1937969
84
XDOT = -17154
858623 XDOT = -5194
792898
YDOT = -1936
465333 feet/sec YDOT = -648
515961 meter/sec
ZDOT = -18249
158648 ZDOT = -5587
661004
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21190328
40 X = -6458812
10
Y = 2910776
74 feet Y = 887204
75 meter
Z = -6349760
21 Z = -1935406
91
XDOT = 3381
800382 XDOT = 1030
772756
YDOT = -15298
366881 feet/sec YDOT = -4662
942225 meter/sec
ZDOT = -18366
228102 ZDOT = -5598
026325
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 20335
57536183
00016717 00000-0 10270-3 0 9121
2 25544 51
6450 245
1828 0001707 91
8106 268
3240 15
49036816 17807
Satellite: ISS
Catalog Number: 25544
Epoch time: 20335
57536183 = yrday
fracday
Element set: 912
Inclination: 51
6450 deg
RA of node: 245
1828 deg
Eccentricity:
0001707
Arg of perigee: 91
8106 deg
Mean anomaly: 268
3240 deg
Mean motion: 15
49036816 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1780
Checksum: 302
Coasting Arc #14 (Orbit 1780)
---------------------------------------
Vector Time (GMT): 2020/335/15:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4530619
28 A = 6793097
94 meter
Y = 4952
24 meter E =
0014899
Z = -5075092
45 I = 51
27350
XDOT = -1963
140933 Wp = 101
30053
YDOT = -7183
140316 meter/sec RA = 243
87037 deg
ZDOT = 1747
042763 TA = 185
71533
MA = 185
73235
Ha = 229
570 n
mi
Hp = 221
829
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14864236
47 X = -4505685
56
Y = 16247
51 feet Y = -45572
31 meter
Z = -16650565
78 Z = -5097040
29
XDOT = -6440
751093 XDOT = -1891
157276
YDOT = -23566
733320 feet/sec YDOT = -7204
691311 meter/sec
ZDOT = 5731
767594 ZDOT = 1737
680297
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6168592
92 X = -1880187
12
Y = -13397904
92 feet Y = -4083681
42 meter
Z = -16752066
61 Z = -5106029
90
XDOT = 17736
001576 XDOT = 5405
933280
YDOT = -15272
480808 feet/sec YDOT = -4655
052150 meter/sec
ZDOT = 5688
629413 ZDOT = 1733
894245
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 20335
63987267
00016717 00000-0 10270-3 0 9132
2 25544 51
6441 244
8631 0001696 85
6739 274
4605 15
49078028 17810
Satellite: ISS
Catalog Number: 25544
Epoch time: 20335
63987267 = yrday
fracday
Element set: 913
Inclination: 51
6441 deg
RA of node: 244
8631 deg
Eccentricity:
0001696
Arg of perigee: 85
6739 deg
Mean anomaly: 274
4605 deg
Mean motion: 15
49078028 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1781
Checksum: 336
Coasting Arc #15 (Orbit 1796)
---------------------------------------
Vector Time (GMT): 2020/336/15:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4520237
19 A = 6793079
19 meter
Y = -349044
41 meter E =
0006706
Z = 5054464
00 I = 51
29014
XDOT = 2548
284283 Wp = 62
67009
YDOT = 7002
403342 meter/sec RA = 238
89983 deg
ZDOT = -1790
522579 TA = 44
77900
MA = 44
72489
Ha = 229
336 n
mi
Hp = 222
022
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14830174
52 X = 4499252
28
Y = -1145158
84 feet Y = -298613
95 meter
Z = 16582887
13 Z = 5076370
88
XDOT = 8360
512739 XDOT = 2478
489366
YDOT = 22973
764246 feet/sec YDOT = 7030
510098 meter/sec
ZDOT = -5874
417910 ZDOT = -1778
312315
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7401279
93 X = 2255910
12
Y = 12770886
40 feet Y = 3892566
18 meter
Z = 16684217
89 Z = 5085349
61
XDOT = -16142
611876 XDOT = -4920
268100
YDOT = 16976
947825 feet/sec YDOT = 5174
573697 meter/sec
ZDOT = -5818
087419 ZDOT = -1773
353045
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 20336
67206973
00016717 00000-0 10270-3 0 9146
2 25544 51
6445 239
7573 0001545 87
5930 272
5397 15
49096526 17976
Satellite: ISS
Catalog Number: 25544
Epoch time: 20336
67206973 = yrday
fracday
Element set: 914
Inclination: 51
6445 deg
RA of node: 239
7573 deg
Eccentricity:
0001545
Arg of perigee: 87
5930 deg
Mean anomaly: 272
5397 deg
Mean motion: 15
49096526 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1797
Checksum: 346
Coasting Arc #16 (Orbit 1811)
---------------------------------------
Vector Time (GMT): 2020/337/15:02:30
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4495514
12 A = 6793154
08 meter
Y = 707565
14 meter E =
0014755
Z = -5056907
07 I = 51
30743
XDOT = -3109
436479 Wp = 102
33008
YDOT = -6746
671256 meter/sec RA = 233
92884 deg
ZDOT = 1821
682708 TA = 185
42845
MA = 185
44447
Ha = 229
541 n
mi
Hp = 221
839
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14749062
06 X = -4478528
36
Y = 2321407
94 feet Y = 657388
82 meter
Z = -16590902
44 Z = -5078703
41
XDOT = -10201
563250 XDOT = -3042
610852
YDOT = -22134
748215 feet/sec YDOT = -6781
069837 meter/sec
ZDOT = 5976
649305 ZDOT = 1806
739385
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8634912
96 X = -2631921
47
Y = -12041837
29 feet Y = -3670352
01 meter
Z = -16691741
77 Z = -5087642
89
XDOT = 14316
343297 XDOT = 4363
621437
YDOT = -18448
270215 feet/sec YDOT = -5623
032762 meter/sec
ZDOT = 5907
651082 ZDOT = 1800
652050
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 20337
63975290
00016717 00000-0 10270-3 0 9159
2 25544 51
6432 234
9691 0001645 90
3615 269
7723 15
49085646 18123
Satellite: ISS
Catalog Number: 25544
Epoch time: 20337
63975290 = yrday
fracday
Element set: 915
Inclination: 51
6432 deg
RA of node: 234
9691 deg
Eccentricity:
0001645
Arg of perigee: 90
3615 deg
Mean anomaly: 269
7723 deg
Mean motion: 15
49085646 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1812
Checksum: 326
Coasting Arc #17 (Orbit 1813)
---------------------------------------
Vector Time (GMT): 2020/337/17:50:56
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 861054
46 A = 6798999
73 meter
Y = 5795401
19 meter E =
0006881
Z = -3455202
96 I = 51
32703
XDOT = -5884
578325 Wp = 91
47353
YDOT = -1827
390966 meter/sec RA = 233
38478 deg
ZDOT = -4539
592108 TA = 129
11648
MA = 129
05528
Ha = 229
651 n
mi
Hp = 221
882
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2824981
83 X = 812968
12
Y = 19013783
43 feet Y = 5804761
78 meter
Z = -11335967
72 Z = -3451136
16
XDOT = -19306
359333 XDOT = -5841
655544
YDOT = -5995
377186 feet/sec YDOT = -1892
955856 meter/sec
ZDOT = -14893
674896 ZDOT = -4568
073439
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4150797
95 X = -1265163
22
Y = 18780284
44 feet Y = 5724230
70 meter
Z = -11317262
89 Z = -3449501
73
XDOT = -14378
784384 XDOT = -4382
653480
YDOT = -12216
558621 feet/sec YDOT = -3723
607068 meter/sec
ZDOT = -15025
392518 ZDOT = -4579
739640
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 20337
76877822
00016717 00000-0 10270-3 0 9166
2 25544 51
6410 234
3280 0001969 97
4162 262
7212 15
49091621 18149
Satellite: ISS
Catalog Number: 25544
Epoch time: 20337
76877822 = yrday
fracday
Element set: 916
Inclination: 51
6410 deg
RA of node: 234
3280 deg
Eccentricity:
0001969
Arg of perigee: 97
4162 deg
Mean anomaly: 262
7212 deg
Mean motion: 15
49091621 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1814
Checksum: 309
Coasting Arc #18 (Orbit 1829)
---------------------------------------
Vector Time (GMT): 2020/338/17:50:56
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1340605
93 A = 6798982
13 meter
Y = -5686876
01 meter E =
0014121
Z = 3465395
26 I = 51
34656
XDOT = 6035
074048 Wp = 93
36538
YDOT = 1346
134968 meter/sec RA = 228
41648 deg
ZDOT = 4526
937321 TA = 307
42013
MA = 307
54855
Ha = 229
618 n
mi
Hp = 221
946
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4398313
40 X = -1293746
94
Y = -18657729
69 feet Y = -5701606
14 meter
Z = 11369407
02 Z = 3458996
03
XDOT = 19800
111707 XDOT = 5997
583203
YDOT = 4416
453306 feet/sec YDOT = 1413
413192 meter/sec
ZDOT = 14852
156564 ZDOT = 4556
162694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2227291
57 X = 678878
47
Y = -19056899
33 feet Y = -5808542
92 meter
Z = 11339894
81 Z = 3456399
94
XDOT = 15579
489617 XDOT = 4748
628435
YDOT = 10772
103085 feet/sec YDOT = 3283
337020 meter/sec
ZDOT = 14987
347367 ZDOT = 4568
143478
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 20338
80097072
00016717 00000-0 10270-3 0 9174
2 25544 51
6394 229
2214 0001897 108
5953 251
5404 15
49089496 18306
Satellite: ISS
Catalog Number: 25544
Epoch time: 20338
80097072 = yrday
fracday
Element set: 917
Inclination: 51
6394 deg
RA of node: 229
2214 deg
Eccentricity:
0001897
Arg of perigee: 108
5953 deg
Mean anomaly: 251
5404 deg
Mean motion: 15
49089496 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1830
Checksum: 324
Coasting Arc #19 (Orbit 1830)
---------------------------------------
Vector Time (GMT): 2020/338/19:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 966705
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -13967
18 A = 6796021
58 meter
Y = -5219210
90 meter E =
0011508
Z = 4345507
68 I = 51
34033
XDOT = 6237
182149 Wp = 109
30793
YDOT = 2844
850239 meter/sec RA = 228
08196 deg
ZDOT = 3425
697337 TA = 305
71744
MA = 305
82445
Ha = 229
563 n
mi
Hp = 221
946
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -45824
07 X = 23288
54
Y = -17123395
34 feet Y = -5219159
43 meter
Z = 14256914
95 Z = 4345529
53
XDOT = 20463
196026 XDOT = 6188
266428
YDOT = 9333
498161 feet/sec YDOT = 2914
324868 meter/sec
ZDOT = 11239
164492 ZDOT = 3455
876946
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1352631
34 X = -412282
03
Y = -17069792
83 feet Y = -5202872
86 meter
Z = 14257101
83 Z = 4345564
64
XDOT = 19749
277967 XDOT = 6019
579924
YDOT = 7969
489655 feet/sec YDOT = 2429
100447 meter/sec
ZDOT = 11378
747105 ZDOT = 3468
242118
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 20338
86548272
00016717 00000-0 10270-3 0 9184
2 25544 51
6415 228
9020 0001883 112
8765 247
2584 15
49099520 18316
Satellite: ISS
Catalog Number: 25544
Epoch time: 20338
86548272 = yrday
fracday
Element set: 918
Inclination: 51
6415 deg
RA of node: 228
9020 deg
Eccentricity:
0001883
Arg of perigee: 112
8765 deg
Mean anomaly: 247
2584 deg
Mean motion: 15
49099520 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1831
Checksum: 324
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