[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 9th 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
317/19:38:04
567 1
8 2
1 2
1
N/A -1
1 -0
2 229
1
000/00:06:09
133 0
2 0
1 222
6
320/00:49:49
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
320/09:20:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
1
000/00:00:00
000 0
0 0
0 222
5
323/04:57:30
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
7
Coasting Arc #1 (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 = 2077777
23 A = 6792154
35 meter
Y = -3941136
06 meter E =
0015176
Z = -5140340
01 I = 51
65376
XDOT = 7272
996314 Wp = 99
86201
YDOT = 1741
068179 meter/sec RA = 3
67896 deg
ZDOT = 1606
446658 TA = 185
66197
MA = 185
67915
Ha = 229
168 n
mi
Hp = 221
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6816854
44 X = 2146663
04
Y = -12930236
41 feet Y = -3917515
33 meter
Z = -16864632
57 Z = -5130079
77
XDOT = 23861
536463 XDOT = 7245
183286
YDOT = 5712
165943 feet/sec YDOT = 1822
244416 meter/sec
ZDOT = 5270
494286 ZDOT = 1641
709199
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4304908
80 X = 1312136
20
Y = 14026210
77 feet Y = 4275189
04 meter
Z = -16816941
50 Z = -5125803
77
XDOT = -19805
458309 XDOT = -6036
703692
YDOT = 12587
256460 feet/sec YDOT = 3836
595769 meter/sec
ZDOT = 5433
497235 ZDOT = 1656
129957
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
51327331
00016717 00000-0 10270-3 0 9009
2 25544 51
6438 4
2246 0001844 84
7055 275
4306 15
49370628 14077
Satellite: ISS
Catalog Number: 25544
Epoch time: 20311
51327331 = yrday
fracday
Element set: 900
Inclination: 51
6438 deg
RA of node: 4
2246 deg
Eccentricity:
0001844
Arg of perigee: 84
7055 deg
Mean anomaly: 275
4306 deg
Mean motion: 15
49370628 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1407
Checksum: 280
Coasting Arc #2 (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 = 6791742
65 A = 6803101
00 meter
Y = 63897
70 meter E =
0013200
Z = -271667
21 I = 51
67978
XDOT = 187
479833 Wp = 48
34089
YDOT = 4755
901751 meter/sec RA = 2
35053 deg
ZDOT = 6002
855504 TA = 308
73915
MA = 308
85707
Ha = 229
181 n
mi
Hp = 221
408
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22282620
23 X = 6791842
97
Y = 209638
11 feet Y = 139848
41 meter
Z = -891296
61 Z = -238674
80
XDOT = 615
091315 XDOT = 105
125066
YDOT = 15603
352200 feet/sec YDOT = 4757
537397 meter/sec
ZDOT = 19694
407820 ZDOT = 6003
566522
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17679793
68 X = 5388801
11
Y = 13573236
33 feet Y = 4137122
43 meter
Z = -738696
87 Z = -225154
81
XDOT = -8012
169817 XDOT = -2442
109360
YDOT = 11465
745482 feet/sec YDOT = 3494
759223 meter/sec
ZDOT = 19697
415689 ZDOT = 6003
772302
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
77127000
00016717 00000-0 10270-3 0 9019
2 25544 51
6422 2
9483 0001930 81
4028 278
7340 15
49394878 14110
Satellite: ISS
Catalog Number: 25544
Epoch time: 20311
77127000 = yrday
fracday
Element set: 901
Inclination: 51
6422 deg
RA of node: 2
9483 deg
Eccentricity:
0001930
Arg of perigee: 81
4028 deg
Mean anomaly: 278
7340 deg
Mean motion: 15
49394878 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1411
Checksum: 283
Coasting Arc #3 (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 = -6785047
50 A = 6803146
74 meter
Y = 395781
15 meter E =
0013424
Z = 111097
70 I = 51
64742
XDOT = -382
917957 Wp = 127
02797
YDOT = -4739
908825 meter/sec RA = 357
40271 deg
ZDOT = -6006
230234 TA = 51
77782
MA = 51
65705
Ha = 229
128 n
mi
Hp = 221
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22260654
52 X = -6789508
62
Y = 1298494
59 feet Y = 319880
93 meter
Z = 364493
76 Z = 78127
35
XDOT = -1256
292509 XDOT = -300
711198
YDOT = -15550
881973 feet/sec YDOT = -4743
730892 meter/sec
ZDOT = -19705
479770 ZDOT = -6007
890932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18776194
08 X = -5722983
95
Y = -12031844
65 feet Y = -3667306
25 meter
Z = 211976
51 Z = 64610
44
XDOT = 7354
272084 XDOT = 2241
582131
YDOT = -11873
037349 feet/sec YDOT = -3618
901784 meter/sec
ZDOT = -19712
882570 ZDOT = -6008
486607
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
80325309
00016717 00000-0 10270-3 0 9027
2 25544 51
6436 357
8403 0001860 82
0080 278
1276 15
49386462 14275
Satellite: ISS
Catalog Number: 25544
Epoch time: 20312
80325309 = yrday
fracday
Element set: 902
Inclination: 51
6436 deg
RA of node: 357
8403 deg
Eccentricity:
0001860
Arg of perigee: 82
0080 deg
Mean anomaly: 278
1276 deg
Mean motion: 15
49386462 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1427
Checksum: 296
Coasting Arc #4 (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 = 6738968
51 A = 6803109
94 meter
Y = -887475
37 meter E =
0013713
Z = 6731
01 I = 51
61351
XDOT = 607
224511 Wp = 50
48934
YDOT = 4718
412835 meter/sec RA = 352
45277 deg
ZDOT = 6005
115920 TA = 309
58304
MA = 309
70407
Ha = 229
155 n
mi
Hp = 221
404
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22109476
75 X = 6748358
98
Y = -2911664
59 feet Y = -812062
88 meter
Z = 22083
38 Z = 39489
43
XDOT = 1992
206402 XDOT = 525
246909
YDOT = 15480
357071 feet/sec YDOT = 4724
744637 meter/sec
ZDOT = 19701
823884 ZDOT = 6007
866701
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19779749
41 X = 6028867
62
Y = 10297504
70 feet Y = 3138679
43 meter
Z = 173639
69 Z = 52925
38
XDOT = -6608
488677 XDOT = -2014
267349
YDOT = 12303
872634 feet/sec YDOT = 3750
220379 meter/sec
ZDOT = 19714
272692 ZDOT = 6008
910317
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
83523281
00016717 00000-0 10270-3 0 9031
2 25544 51
6435 352
7330 0001890 84
4134 275
7232 15
49399736 14437
Satellite: ISS
Catalog Number: 25544
Epoch time: 20313
83523281 = yrday
fracday
Element set: 903
Inclination: 51
6435 deg
RA of node: 352
7330 deg
Eccentricity:
0001890
Arg of perigee: 84
4134 deg
Mean anomaly: 275
7232 deg
Mean motion: 15
49399736 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1443
Checksum: 302
Coasting Arc #5 (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 = -6662508
89 A = 6803125
17 meter
Y = 1338646
17 meter E =
0012944
Z = -170240
45 I = 51
58026
XDOT = -798
414947 Wp = 129
04388
YDOT = -4696
587894 meter/sec RA = 347
50075 deg
ZDOT = -5998
944798 TA = 52
78786
MA = 52
66980
Ha = 229
151 n
mi
Hp = 221
438
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21858624
96 X = -6676155
92
Y = 4391883
76 feet Y = 1264064
91 meter
Z = -558531
64 Z = -202637
81
XDOT = -2619
471612 XDOT = -716
697146
YDOT = -15408
752934 feet/sec YDOT = -4705
059288 meter/sec
ZDOT = -19681
577421 ZDOT = -6002
624865
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20571108
96 X = -6270074
01
Y = -8586482
74 feet Y = -2617159
94 meter
Z = -708432
19 Z = -215930
13
XDOT = 5935
643501 XDOT = 1809
184139
YDOT = -12662
369645 feet/sec YDOT = -3859
490268 meter/sec
ZDOT = -19698
329074 ZDOT = -6004
050702
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
80271306
00016717 00000-0 10270-3 0 9048
2 25544 51
6437 347
9448 0001937 85
2875 274
8496 15
49387438 14582
Satellite: ISS
Catalog Number: 25544
Epoch time: 20314
80271306 = yrday
fracday
Element set: 904
Inclination: 51
6437 deg
RA of node: 347
9448 deg
Eccentricity:
0001937
Arg of perigee: 85
2875 deg
Mean anomaly: 274
8496 deg
Mean motion: 15
49387438 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1458
Checksum: 344
Coasting Arc #6 (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 = 6543330
33 A = 6803073
98 meter
Y = -1816274
81 meter E =
0014143
Z = 289468
59 I = 51
54675
XDOT = 1021
410034 Wp = 53
24307
YDOT = 4665
577942 meter/sec RA = 342
54674 deg
ZDOT = 5990
562716 TA = 309
87439
MA = 309
99868
Ha = 229
148 n
mi
Hp = 221
404
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21467619
20 X = 6561748
06
Y = -5958906
86 feet Y = -1742999
61 meter
Z = 949700
09 Z = 321298
71
XDOT = 3351
082789 XDOT = 940
063060
YDOT = 15307
014247 feet/sec YDOT = 4676
545196 meter/sec
ZDOT = 19654
077151 ZDOT = 5995
326857
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21239935
82 X = 6473932
44
Y = 6703052
60 feet Y = 2043090
43 meter
Z = 1096990
30 Z = 334362
64
XDOT = -5159
448613 XDOT = -1572
599937
YDOT = 13037
988041 feet/sec YDOT = 3973
978755 meter/sec
ZDOT = 19675
847438 ZDOT = 5997
198299
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
83469044
00016717 00000-0 10270-3 0 9051
2 25544 51
6431 342
8380 0001876 89
5548 270
5817 15
49396565 14740
Satellite: ISS
Catalog Number: 25544
Epoch time: 20315
83469044 = yrday
fracday
Element set: 905
Inclination: 51
6431 deg
RA of node: 342
8380 deg
Eccentricity:
0001876
Arg of perigee: 89
5548 deg
Mean anomaly: 270
5817 deg
Mean motion: 15
49396565 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1474
Checksum: 335
Coasting Arc #7 (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 = -6399367
54 A = 6803019
71 meter
Y = 2248107
27 meter E =
0012352
Z = -454499
70 I = 51
51582
XDOT = -1212
936880 Wp = 131
74035
YDOT = -4637
748545 meter/sec RA = 337
58994 deg
ZDOT = -5974
843849 TA = 53
15931
MA = 53
04610
Ha = 229
100 n
mi
Hp = 221
451
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20995300
33 X = -6421823
20
Y = 7375680
01 feet Y = 2176419
39 meter
Z = -1491140
73 Z = -485640
45
XDOT = -3979
451706 XDOT = -1131
963097
YDOT = -15215
710450 feet/sec YDOT = -4650
859724 meter/sec
ZDOT = -19602
506067 ZDOT = -5980
539260
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21700377
50 X = -6614275
06
Y = -4883273
46 feet Y = -1488421
75 meter
Z = -1635251
98 Z = -498424
80
XDOT = 4459
055193 XDOT = 1359
120023
YDOT = -13355
623821 feet/sec YDOT = -4070
794141 meter/sec
ZDOT = -19628
586663 ZDOT = -5982
793215
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
80216717
00016717 00000-0 10270-3 0 9067
2 25544 51
6442 338
0496 0001840 92
3055 267
8306 15
49394185 14897
Satellite: ISS
Catalog Number: 25544
Epoch time: 20316
80216717 = yrday
fracday
Element set: 906
Inclination: 51
6442 deg
RA of node: 338
0496 deg
Eccentricity:
0001840
Arg of perigee: 92
3055 deg
Mean anomaly: 267
8306 deg
Mean motion: 15
49394185 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1489
Checksum: 318
Coasting Arc #8 (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 = 6211118
29 A = 6802962
64 meter
Y = -2698667
33 meter E =
0014574
Z = 576477
95 I = 51
48424
XDOT = 1435
131659 Wp = 56
00609
YDOT = 4597
375464 meter/sec RA = 332
63076 deg
ZDOT = 5958
798174 TA = 310
21722
MA = 310
34466
Ha = 229
143 n
mi
Hp = 221
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20377684
68 X = 6238033
71
Y = -8853895
44 feet Y = -2629059
66 meter
Z = 1891331
87 Z = 606715
22
XDOT = 4708
437202 XDOT = 1354
670621
YDOT = 15083
252834 feet/sec YDOT = 4612
974221 meter/sec
ZDOT = 19549
862777 ZDOT = 5965
574244
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22012470
12 X = 6709400
89
Y = 2922962
80 feet Y = 890919
06 meter
Z = 2031275
80 Z = 619132
86
XDOT = -3651
243918 XDOT = -1112
899146
YDOT = 13676
323665 feet/sec YDOT = 4168
543453 meter/sec
ZDOT = 19580
943089 ZDOT = 5968
271454
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
83413970
00016717 00000-0 10270-3 0 9072
2 25544 51
6437 332
9420 0001886 91
9533 268
1833 15
49395753 15057
Satellite: ISS
Catalog Number: 25544
Epoch time: 20317
83413970 = yrday
fracday
Element set: 907
Inclination: 51
6437 deg
RA of node: 332
9420 deg
Eccentricity:
0001886
Arg of perigee: 91
9533 deg
Mean anomaly: 268
1833 deg
Mean motion: 15
49395753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1505
Checksum: 323
Coasting Arc #9 (Orbit 1504)
---------------------------------------
Vector Time (GMT): 2020/317/19:41:09
133
Vector Time (MET): N/A
Weight (LBS) : 938215
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -656992
22 A = 6792841
09 meter
Y = -4334706
78 meter E =
0014116
Z = -5201115
74 I = 51
44680
XDOT = 7090
281269 Wp = 99
63549
YDOT = -2581
408116 meter/sec RA = 332
36913 deg
ZDOT = 1256
379735 TA = 182
48470
MA = 182
49172
Ha = 229
107 n
mi
Hp = 222
615
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2155486
28 X = -583206
73
Y = -14221478
92 feet Y = -4341641
14 meter
Z = -17064028
01 Z = -5204128
03
XDOT = 23262
077654 XDOT = 7112
517464
YDOT = -8469
186731 feet/sec YDOT = -2501
995176 meter/sec
ZDOT = 4121
980759 ZDOT = 1290
876381
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1269253
84 X = 386868
57
Y = -14311466
13 feet Y = -4362134
88 meter
Z = -17077721
38 Z = -5205289
48
XDOT = 23511
030001 XDOT = 7166
161944
YDOT = -3021
658200 feet/sec YDOT = -921
001419 meter/sec
ZDOT = 4281
610307 ZDOT = 1305
034822
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
83413941
00016717 00000-0 10270-3 0 9081
2 25544 51
6453 332
9420 0000169 109
4136 250
7032 15
49018165 15059
Satellite: ISS
Catalog Number: 25544
Epoch time: 20317
83413941 = yrday
fracday
Element set: 908
Inclination: 51
6453 deg
RA of node: 332
9420 deg
Eccentricity:
0000169
Arg of perigee: 109
4136 deg
Mean anomaly: 250
7032 deg
Mean motion: 15
49018165 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1505
Checksum: 284
Coasting Arc #10 (Orbit 1520)
---------------------------------------
Vector Time (GMT): 2020/318/19:41:09
133
Vector Time (MET): N/A
Weight (LBS) : 938215
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1009805
85 A = 6792748
93 meter
Y = 4265564
11 meter E =
0004333
Z = 5186447
83 I = 51
41658
XDOT = -6855
863215 Wp = 55
65177
YDOT = 3176
251417 meter/sec RA = 327
40958 deg
ZDOT = -1274
287253 TA = 46
64931
MA = 46
61321
Ha = 228
978 n
mi
Hp = 222
642
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3313011
32 X = 936838
45
Y = 13994632
92 feet Y = 4276448
37 meter
Z = 17015904
94 Z = 5191176
09
XDOT = -22492
989551 XDOT = -6884
681538
YDOT = 10420
772364 feet/sec YDOT = 3099
423131 meter/sec
ZDOT = -4180
732458 ZDOT = -1307
661221
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 156708
39 X = 47764
72
Y = 14354951
26 feet Y = 4375389
14 meter
Z = 17037535
98 Z = 5193040
97
XDOT = -23115
592662 XDOT = -7045
632643
YDOT = 5409
964659 feet/sec YDOT = 1648
957228 meter/sec
ZDOT = -4335
190423 ZDOT = -1321
366041
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
86637460
00016717 00000-0 10270-3 0 9090
2 25544 51
6444 327
8363 0000064 108
5448 251
5708 15
49050972 15217
Satellite: ISS
Catalog Number: 25544
Epoch time: 20318
86637460 = yrday
fracday
Element set: 909
Inclination: 51
6444 deg
RA of node: 327
8363 deg
Eccentricity:
0000064
Arg of perigee: 108
5448 deg
Mean anomaly: 251
5708 deg
Mean motion: 15
49050972 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1521
Checksum: 311
Coasting Arc #11 (Orbit 1535)
---------------------------------------
Vector Time (GMT): 2020/319/19:41:09
133
Vector Time (MET): N/A
Weight (LBS) : 938215
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1368315
82 A = 6792840
59 meter
Y = -4177364
57 meter E =
0013957
Z = -5191222
07 I = 51
38873
XDOT = 6548
072561 Wp = 99
89661
YDOT = -3740
212160 meter/sec RA = 322
44763 deg
ZDOT = 1284
395264 TA = 182
50817
MA = 182
51517
Ha = 229
049 n
mi
Hp = 222
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4489225
14 X = -1296284
82
Y = -13705264
33 feet Y = -4192263
01 meter
Z = -17031568
48 Z = -5197694
30
XDOT = 21483
177695 XDOT = 6583
171029
YDOT = -12271
037271 feet/sec YDOT = -3666
790737 meter/sec
ZDOT = 4213
895222 ZDOT = 1316
289239
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1613541
67 X = -491807
50
Y = -14295852
83 feet Y = -4357375
94 meter
Z = -17061266
44 Z = -5200274
01
XDOT = 22393
569011 XDOT = 6825
559834
YDOT = -7730
351281 feet/sec YDOT = -2356
211070 meter/sec
ZDOT = 4361
532294 ZDOT = 1329
395043
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
83409633
00016717 00000-0 10270-3 0 9109
2 25544 51
6444 323
0494 0000055 141
5168 218
5986 15
49025648 15365
Satellite: ISS
Catalog Number: 25544
Epoch time: 20319
83409633 = yrday
fracday
Element set: 910
Inclination: 51
6444 deg
RA of node: 323
0494 deg
Eccentricity:
0000055
Arg of perigee: 141
5168 deg
Mean anomaly: 218
5986 deg
Mean motion: 15
49025648 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1536
Checksum: 308
Coasting Arc #12 (Orbit 1539)
---------------------------------------
Vector Time (GMT): 2020/320/00:49:49
000
Vector Time (MET): N/A
Weight (LBS) : 938215
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5803322
62 A = 6799492
54 meter
Y = -1259154
75 meter E =
0012584
Z = 3301078
05 I = 51
40075
XDOT = -1394
902884 Wp = 90
27918
YDOT = 5899
247974 meter/sec RA = 321
41480 deg
ZDOT = 4686
852132 TA = 308
16034
MA = 308
27366
Ha = 228
964 n
mi
Hp = 222
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19039772
36 X = 5800936
32
Y = -4131085
13 feet Y = -1194271
38 meter
Z = 10830308
58 Z = 3329263
30
XDOT = -4576
453032 XDOT = -1483
533117
YDOT = 19354
488103 feet/sec YDOT = 5883
153308 meter/sec
ZDOT = 15376
811458 ZDOT = 4679
861138
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3899401
29 X = 1188537
51
Y = -19014015
87 feet Y = -5795472
04 meter
Z = 10960668
30 Z = 3340811
70
XDOT = 14417
282013 XDOT = 4394
387558
YDOT = 11831
025018 feet/sec YDOT = 3606
096425 meter/sec
ZDOT = 15344
181205 ZDOT = 4676
906431
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
09215407
00016717 00000-0 10270-3 0 9114
2 25544 51
6398 321
7681 0000441 173
8924 186
2231 15
49028544 15400
Satellite: ISS
Catalog Number: 25544
Epoch time: 20320
09215407 = yrday
fracday
Element set: 911
Inclination: 51
6398 deg
RA of node: 321
7681 deg
Eccentricity:
0000441
Arg of perigee: 173
8924 deg
Mean anomaly: 186
2231 deg
Mean motion: 15
49028544 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1540
Checksum: 288
Coasting Arc #13 (Orbit 1544)
---------------------------------------
Vector Time (GMT): 2020/320/09:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 965221
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5813742
65 A = 6800076
36 meter
Y = 1695237
06 meter E =
0004830
Z = -3095563
79 I = 51
39706
XDOT = 881
879613 Wp = 106
09776
YDOT = -5844
406572 meter/sec RA = 319
65803 deg
ZDOT = -4864
502898 TA = 109
52290
MA = 109
47073
Ha = 229
097 n
mi
Hp = 222
534
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19073958
84 X = -5817230
29
Y = 5561801
38 feet Y = 1630204
35 meter
Z = -10156049
17 Z = -3123813
85
XDOT = 2893
305816 XDOT = 970
797660
YDOT = -19174
562244 feet/sec YDOT = -5834
047224 meter/sec
ZDOT = -15959
655178 ZDOT = -4860
003412
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17090818
31 X = 5209281
42
Y = -9999099
36 feet Y = -3047725
49 meter
Z = -10286730
11 Z = -3135395
34
XDOT = 1002
650565 XDOT = 305
607892
YDOT = 18085
279282 feet/sec YDOT = 5512
393125 meter/sec
ZDOT = -15938
546452 ZDOT = -4858
068958
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
41472805
00016717 00000-0 10270-3 0 9128
2 25544 51
6435 320
1750 0000371 139
3029 220
8149 15
49020577 15453
Satellite: ISS
Catalog Number: 25544
Epoch time: 20320
41472805 = yrday
fracday
Element set: 912
Inclination: 51
6435 deg
RA of node: 320
1750 deg
Eccentricity:
0000371
Arg of perigee: 139
3029 deg
Mean anomaly: 220
8149 deg
Mean motion: 15
49020577 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1545
Checksum: 275
Coasting Arc #14 (Orbit 1560)
---------------------------------------
Vector Time (GMT): 2020/321/09:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 965221
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5640452
72 A = 6800147
82 meter
Y = -2188379
62 meter E =
0013278
Z = 3091757
20 I = 51
37187
XDOT = -381
549100 Wp = 85
41829
YDOT = 5910
143017 meter/sec RA = 314
69308 deg
ZDOT = 4862
282607 TA = 310
20770
MA = 310
32383
Ha = 229
128 n
mi
Hp = 222
570
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18505422
32 X = 5649486
26
Y = -7179723
17 feet Y = -2125253
84 meter
Z = 10143560
38 Z = 3119178
74
XDOT = -1251
801508 XDOT = -471
228545
YDOT = 19390
232994 feet/sec YDOT = 5905
374328 meter/sec
ZDOT = 15952
370759 ZDOT = 4860
211935
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15948369
24 X = -4861062
94
Y = 11707202
40 feet Y = 3568355
29 meter
Z = 10270434
65 Z = 3130428
48
XDOT = -2851
747067 XDOT = -869
212506
YDOT = -17919
293985 feet/sec YDOT = -5461
800807 meter/sec
ZDOT = 15942
489993 ZDOT = 4859
270950
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
44696034
00016717 00000-0 10270-3 0 9135
2 25544 51
6433 315
0687 0000393 107
9728 252
1465 15
49000905 15614
Satellite: ISS
Catalog Number: 25544
Epoch time: 20321
44696034 = yrday
fracday
Element set: 913
Inclination: 51
6433 deg
RA of node: 315
0687 deg
Eccentricity:
0000393
Arg of perigee: 107
9728 deg
Mean anomaly: 252
1465 deg
Mean motion: 15
49000905 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1561
Checksum: 293
Coasting Arc #15 (Orbit 1575)
---------------------------------------
Vector Time (GMT): 2020/322/09:20:00
000
Vector Time (MET): N/A
Weight (LBS) : 965221
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5436947
43 A = 6799982
91 meter
Y = 2638382
03 meter E =
0004830
Z = -3120179
64 I = 51
34996
XDOT = -104
481788 Wp = 103
28700
YDOT = -5929
876494 meter/sec RA = 309
72707 deg
ZDOT = -4839
599704 TA = 112
68761
MA = 112
63654
Ha = 229
092 n
mi
Hp = 222
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17837754
02 X = -5450890
17
Y = 8656109
03 feet Y = 2577504
60 meter
Z = -10236809
83 Z = -3146624
28
XDOT = -342
788020 XDOT = -14
655874
YDOT = -19454
975373 feet/sec YDOT = -5930
542056 meter/sec
ZDOT = -15877
951784 ZDOT = -4839
889781
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14695498
49 X = 4479187
94
Y = -13214971
55 feet Y = -4027923
33 meter
Z = -10359190
07 Z = -3157481
13
XDOT = 4620
668074 XDOT = 1408
379629
YDOT = 17566
949464 feet/sec YDOT = 5354
406197 meter/sec
ZDOT = -15878
989449 ZDOT = -4839
915984
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
41467526
00016717 00000-0 10270-3 0 9146
2 25544 51
6446 310
2822 0000306 115
6592 244
4589 15
49032589 15765
Satellite: ISS
Catalog Number: 25544
Epoch time: 20322
41467526 = yrday
fracday
Element set: 914
Inclination: 51
6446 deg
RA of node: 310
2822 deg
Eccentricity:
0000306
Arg of perigee: 115
6592 deg
Mean anomaly: 244
4589 deg
Mean motion: 15
49032589 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1576
Checksum: 305
Coasting Arc #16 (Orbit 1588)
---------------------------------------
Vector Time (GMT): 2020/323/04:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 965221
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2798259
75 A = 6792453
84 meter
Y = 3295424
13 meter E =
0003282
Z = 5236677
91 I = 51
30798
XDOT = -5010
795191 Wp = 63
06248
YDOT = 5723
256048 meter/sec RA = 305
63075 deg
ZDOT = -922
160748 TA = 35
81827
MA = 35
79627
Ha = 228
856 n
mi
Hp = 222
680
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9180642
23 X = 2735764
18
Y = 10811758
94 feet Y = 3326366
20 meter
Z = 17180701
80 Z = 5250119
58
XDOT = -16439
616770 XDOT = -5069
942561
YDOT = 18777
086772 feet/sec YDOT = 5666
891139 meter/sec
ZDOT = -3025
461771 ZDOT = -946
644564
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2173179
75 X = 662385
19
Y = -13939952
34 feet Y = -4248897
47 meter
Z = 17242675
43 Z = 5255567
47
XDOT = 23926
227534 XDOT = 7292
714152
YDOT = -160
337014 feet/sec YDOT = -48
870722 meter/sec
ZDOT = -3138
929588 ZDOT = -956
745739
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
25336077
00016717 00000-0 10270-3 0 9156
2 25544 51
6447 306
1316 0000375 191
3872 168
7269 15
49057504 15897
Satellite: ISS
Catalog Number: 25544
Epoch time: 20323
25336077 = yrday
fracday
Element set: 915
Inclination: 51
6447 deg
RA of node: 306
1316 deg
Eccentricity:
0000375
Arg of perigee: 191
3872 deg
Mean anomaly: 168
7269 deg
Mean motion: 15
49057504 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1589
Checksum: 317
Coasting Arc #17 (Orbit 1603)
---------------------------------------
Vector Time (GMT): 2020/324/04:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 965221
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3067746
70 A = 6792564
41 meter
Y = -3063391
93 meter E =
0014327
Z = -5241735
55 I = 51
28881
XDOT = 4500
152941 Wp = 98
55408
YDOT = -6113
914861 meter/sec RA = 300
66256 deg
ZDOT = 939
505847 TA = 180
50118
MA = 180
50262
Ha = 229
016 n
mi
Hp = 222
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10064785
74 X = -3007801
31
Y = -10050498
47 feet Y = -3097361
91 meter
Z = -17197295
12 Z = -5256492
36
XDOT = 14764
281304 XDOT = 4563
622499
YDOT = -20058
775790 feet/sec YDOT = -6063
236146 meter/sec
ZDOT = 3082
368264 ZDOT = 961
519517
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -775436
70 X = -236353
11
Y = 14119672
68 feet Y = 4303676
23 meter
Z = -17265368
00 Z = -5262484
17
XDOT = -23734
890103 XDOT = -7234
394504
YDOT = 2589
886558 feet/sec YDOT = 789
397423 meter/sec
ZDOT = 3184
425877 ZDOT = 970
613007
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
22107566
00016717 00000-0 10270-3 0 9164
2 25544 51
6442 301
3458 0000335 191
0091 169
1052 15
49026836 16049
Satellite: ISS
Catalog Number: 25544
Epoch time: 20324
22107566 = yrday
fracday
Element set: 916
Inclination: 51
6442 deg
RA of node: 301
3458 deg
Eccentricity:
0000335
Arg of perigee: 191
0091 deg
Mean anomaly: 169
1052 deg
Mean motion: 15
49026836 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1604
Checksum: 277
Coasting Arc #18 (Orbit 1619)
---------------------------------------
Vector Time (GMT): 2020/325/04:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 965221
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3302553
23 A = 6792458
41 meter
Y = 2805947
54 meter E =
0003311
Z = 5228152
73 I = 51
27341
XDOT = -3975
215371 Wp = 60
19810
YDOT = 6479
264973 meter/sec RA = 295
69194 deg
ZDOT = -964
251855 TA = 39
09658
MA = 39
07266
Ha = 228
790 n
mi
Hp = 222
706
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10835148
40 X = 3245535
28
Y = 9205864
64 feet Y = 2842559
75 meter
Z = 17152732
06 Z = 5244057
14
XDOT = -13042
045182 XDOT = -4042
689212
YDOT = 21257
431014 feet/sec YDOT = 6434
434084 meter/sec
ZDOT = -3163
555956 ZDOT = -983
725283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -610826
27 X = -186179
85
Y = -14115661
67 feet Y = -4302453
68 meter
Z = 17226130
98 Z = 5250524
72
XDOT = 23384
522286 XDOT = 7127
602393
YDOT = -4991
082445 feet/sec YDOT = -1521
281929 meter/sec
ZDOT = -3253
872894 ZDOT = -991
780458
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
25329982
00016717 00000-0 10270-3 0 9177
2 25544 51
6449 296
2396 0000316 212
8006 147
3124 15
49063700 16203
Satellite: ISS
Catalog Number: 25544
Epoch time: 20325
25329982 = yrday
fracday
Element set: 917
Inclination: 51
6449 deg
RA of node: 296
2396 deg
Eccentricity:
0000316
Arg of perigee: 212
8006 deg
Mean anomaly: 147
3124 deg
Mean motion: 15
49063700 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1620
Checksum: 294
Coasting Arc #19 (Orbit 1634)
---------------------------------------
Vector Time (GMT): 2020/326/04:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 965221
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3529946
15 A = 6792602
37 meter
Y = -2535143
36 meter E =
0014272
Z = -5232946
51 I = 51
25860
XDOT = 3408
243016 Wp = 98
10905
YDOT = -6777
095581 meter/sec RA = 290
72121 deg
ZDOT = 984
492013 TA = 181
38652
MA = 181
39048
Ha = 229
023 n
mi
Hp = 222
580
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11581188
15 X = -3475916
26
Y = -8317399
48 feet Y = -2574315
24 meter
Z = -17168459
67 Z = -5249962
67
XDOT = 11181
899660 XDOT = 3478
991119
YDOT = -22234
565554 feet/sec YDOT = -6738
586660 meter/sec
ZDOT = 3229
960674 ZDOT = 1001
219314
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2010622
58 X = 612837
76
Y = 14019871
93 feet Y = 4273256
97 meter
Z = -17247018
53 Z = -5256891
25
XDOT = -22707
226982 XDOT = -6921
162784
YDOT = 7324
043319 feet/sec YDOT = 2232
368404 meter/sec
ZDOT = 3307
577788 ZDOT = 1008
149710
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
22101028
00016717 00000-0 10270-3 0 9185
2 25544 51
6437 291
4536 0000137 202
1596 157
9548 15
49022282 16353
Satellite: ISS
Catalog Number: 25544
Epoch time: 20326
22101028 = yrday
fracday
Element set: 918
Inclination: 51
6437 deg
RA of node: 291
4536 deg
Eccentricity:
0000137
Arg of perigee: 202
1596 deg
Mean anomaly: 157
9548 deg
Mean motion: 15
49022282 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1635
Checksum: 292
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