[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 16th 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) : 14262 1813 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
320/00:49:49
100 0
0 0
0 0
0
N/A 0
0 0
0 229
4
000/00:00:00
000 0
0 0
0 222
2
320/09:40:00
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
2
323/04:57:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
4
000/00:00:00
000 0
0 0
0 222
1
328/12:55:00
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
0
Coasting Arc #1 (Orbit 1515)
---------------------------------------
Vector Time (GMT): 2020/318/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -536789
14 A = 6794463
04 meter
Y = 4781635
73 meter E =
0009258
Z = 4792352
75 I = 51
43016
XDOT = -6988
162115 Wp = 57
94225
YDOT = 1804
962373 meter/sec RA = 328
98749 deg
ZDOT = -2575
186256 TA = 57
55812
MA = 57
46862
Ha = 229
547 n
mi
Hp = 222
174
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1761119
23 X = -613498
09
Y = 15687781
25 feet Y = 4775203
97 meter
Z = 15722942
08 Z = 4789558
93
XDOT = -22927
041060 XDOT = -6995
317246
YDOT = 5921
792563 feet/sec YDOT = 1726
775766 meter/sec
ZDOT = -8448
773806 ZDOT = -2609
150292
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11242610
87 X = -3426747
79
Y = -11100709
76 feet Y = -3383496
33 meter
Z = 15709769
98 Z = 4788337
89
XDOT = 8544
427315 XDOT = 2604
341445
YDOT = -20872
150346 feet/sec YDOT = -6361
831425 meter/sec
ZDOT = -8605
890066 ZDOT = -2623
075292
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
54377416
00016717 00000-0 10270-3 0 9008
2 25544 51
6432 329
4307 0001849 45
7369 314
3933 15
49048288 15165
Satellite: ISS
Catalog Number: 25544
Epoch time: 20318
54377416 = yrday
fracday
Element set: 900
Inclination: 51
6432 deg
RA of node: 329
4307 deg
Eccentricity:
0001849
Arg of perigee: 45
7369 deg
Mean anomaly: 314
3933 deg
Mean motion: 15
49048288 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1516
Checksum: 317
Coasting Arc #2 (Orbit 1530)
---------------------------------------
Vector Time (GMT): 2020/319/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 128455
73 A = 6794605
01 meter
Y = -4823205
47 meter E =
0012171
Z = -4795360
89 I = 51
40123
XDOT = 6794
871713 Wp = 100
65805
YDOT = -2383
947641 meter/sec RA = 324
02666 deg
ZDOT = 2583
212935 TA = 194
92184
MA = 194
95778
Ha = 229
580 n
mi
Hp = 222
244
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 421442
68 X = 205674
54
Y = -15824164
92 feet Y = -4821337
01 meter
Z = -15732811
31 Z = -4794549
55
XDOT = 22292
886198 XDOT = 6808
476576
YDOT = -7821
350527 feet/sec YDOT = -2307
886556 meter/sec
ZDOT = 8475
108056 ZDOT = 2616
253692
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12344537
69 X = 3762615
09
Y = 9915657
81 feet Y = 3022292
50 meter
Z = -15728804
16 Z = -4794139
51
XDOT = -6355
955327 XDOT = -1937
295184
YDOT = 21581
354457 feet/sec YDOT = 6577
996838 meter/sec
ZDOT = 8627
976799 ZDOT = 2629
807328
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
51148530
00016717 00000-0 10270-3 0 9010
2 25544 51
6426 324
6443 0001771 46
1290 314
0006 15
49004233 15315
Satellite: ISS
Catalog Number: 25544
Epoch time: 20319
51148530 = yrday
fracday
Element set: 901
Inclination: 51
6426 deg
RA of node: 324
6443 deg
Eccentricity:
0001771
Arg of perigee: 46
1290 deg
Mean anomaly: 314
0006 deg
Mean motion: 15
49004233 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1531
Checksum: 259
Coasting Arc #3 (Orbit 1539)
---------------------------------------
Vector Time (GMT): 2020/320/00:49:49
100
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5796589
42 A = 6799385
13 meter
Y = -1235326
53 meter E =
0013736
Z = 3319193
29 I = 51
40084
XDOT = -1424
670190 Wp = 84
80111
YDOT = 5906
655055 meter/sec RA = 321
41452 deg
ZDOT = 4670
832178 TA = 313
89711
MA = 314
01045
Ha = 229
360 n
mi
Hp = 222
197
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19017681
83 X = 5793849
17
Y = -4052908
58 feet Y = -1170520
44 meter
Z = 10889741
77 Z = 3347344
97
XDOT = -4674
114797 XDOT = -1513
303221
YDOT = 19378
789550 feet/sec YDOT = 5890
227495 meter/sec
ZDOT = 15324
252554 ZDOT = 4663
696575
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3961645
71 X = 1207509
61
Y = -18961828
50 feet Y = -5779565
33 meter
Z = 11019945
06 Z = 3358879
25
XDOT = 14404
012386 XDOT = 4390
342975
YDOT = 11925
178939 feet/sec YDOT = 3634
794540 meter/sec
ZDOT = 15290
953421 ZDOT = 4660
682603
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
09211049
00016717 00000-0 10270-3 0 9022
2 25544 51
6401 321
7681 0001510 52
1461 307
9826 15
49047282 15400
Satellite: ISS
Catalog Number: 25544
Epoch time: 20320
09211049 = yrday
fracday
Element set: 902
Inclination: 51
6401 deg
RA of node: 321
7681 deg
Eccentricity:
0001510
Arg of perigee: 52
1461 deg
Mean anomaly: 307
9826 deg
Mean motion: 15
49047282 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1540
Checksum: 266
Coasting Arc #4 (Orbit 1544)
---------------------------------------
Vector Time (GMT): 2020/320/09:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 965450
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -485043
73 A = 6794193
89 meter
Y = -4712400
52 meter E =
0012849
Z = -4882080
66 I = 51
37708
XDOT = 6571
745986 Wp = 100
22703
YDOT = -3121
950754 meter/sec RA = 319
54608 deg
ZDOT = 2363
627112 TA = 193
05203
MA = 193
08531
Ha = 229
574 n
mi
Hp = 222
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1591350
81 X = -408597
14
Y = -15460631
62 feet Y = -4717396
82 meter
Z = -16017324
98 Z = -4884251
55
XDOT = 21560
846411 XDOT = 6594
686667
YDOT = -10242
620585 feet/sec YDOT = -3048
332683 meter/sec
ZDOT = 7754
682127 ZDOT = 2395
606512
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6442552
92 X = 1963690
13
Y = 14133061
93 feet Y = 4307757
28 meter
Z = -16027111
39 Z = -4885063
55
XDOT = -15960
958662 XDOT = -4864
900200
YDOT = 16226
042867 feet/sec YDOT = 4945
697866 meter/sec
ZDOT = 7902
677874 ZDOT = 2408
736216
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
41468041
00016717 00000-0 10270-3 0 9035
2 25544 51
6439 320
1752 0001769 49
3545 310
7758 15
49018813 15459
Satellite: ISS
Catalog Number: 25544
Epoch time: 20320
41468041 = yrday
fracday
Element set: 903
Inclination: 51
6439 deg
RA of node: 320
1752 deg
Eccentricity:
0001769
Arg of perigee: 49
3545 deg
Mean anomaly: 310
7758 deg
Mean motion: 15
49018813 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1545
Checksum: 298
Coasting Arc #5 (Orbit 1560)
---------------------------------------
Vector Time (GMT): 2020/321/09:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 965450
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 855958
83 A = 6794118
57 meter
Y = 4666487
14 meter E =
0008854
Z = 4858517
34 I = 51
35213
XDOT = -6293
857992 Wp = 57
93004
YDOT = 3657
081762 meter/sec RA = 314
58107 deg
ZDOT = -2395
873700 TA = 55
70927
MA = 55
62548
Ha = 229
534 n
mi
Hp = 222
094
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2808263
88 X = 780112
64
Y = 15309997
17 feet Y = 4675634
49 meter
Z = 15940017
51 Z = 4862491
62
XDOT = -20649
140394 XDOT = -6322
646727
YDOT = 11998
299743 feet/sec YDOT = 3586
538606 meter/sec
ZDOT = -7860
478020 ZDOT = -2426
517136
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7777002
66 X = -2370430
41
Y = -13461884
59 feet Y = -4103182
42 meter
Z = 15958145
58 Z = 4864042
77
XDOT = 14261
918978 XDOT = 4347
032905
YDOT = -17755
816513 feet/sec YDOT = -5411
972873 meter/sec
ZDOT = -8002
322550 ZDOT = -2439
107913
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
44689839
00016717 00000-0 10270-3 0 9040
2 25544 51
6437 315
0691 0001866 52
9740 307
1581 15
49060160 15611
Satellite: ISS
Catalog Number: 25544
Epoch time: 20321
44689839 = yrday
fracday
Element set: 904
Inclination: 51
6437 deg
RA of node: 315
0691 deg
Eccentricity:
0001866
Arg of perigee: 52
9740 deg
Mean anomaly: 307
1581 deg
Mean motion: 15
49060160 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1561
Checksum: 305
Coasting Arc #6 (Orbit 1575)
---------------------------------------
Vector Time (GMT): 2020/322/09:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 965450
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1247380
23 A = 6794244
24 meter
Y = -4593295
94 meter E =
0012924
Z = -4860412
44 I = 51
33044
XDOT = 5948
727317 Wp = 100
46297
YDOT = -4162
265759 meter/sec RA = 309
61436 deg
ZDOT = 2410
023056 TA = 193
31749
MA = 193
35164
Ha = 229
625 n
mi
Hp = 222
079
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4092454
82 X = -1172314
32
Y = -15069868
58 feet Y = -4606824
74 meter
Z = -15946235
04 Z = -4866290
07
XDOT = 19516
821906 XDOT = 5983
122161
YDOT = -13655
727555 feet/sec YDOT = -4095
550797 meter/sec
ZDOT = 7906
899791 ZDOT = 2439
003269
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9120140
56 X = 2779818
84
Y = 12641692
45 feet Y = 3853187
86 meter
Z = -15973170
81 Z = -4868622
46
XDOT = -12352
872452 XDOT = -3765
155523
YDOT = 19058
720695 feet/sec YDOT = 5809
098068 meter/sec
ZDOT = 8041
078933 ZDOT = 2450
920859
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
41460168
00016717 00000-0 10270-3 0 9051
2 25544 51
6449 310
2822 0001888 53
8310 306
3015 15
49024683 15763
Satellite: ISS
Catalog Number: 25544
Epoch time: 20322
41460168 = yrday
fracday
Element set: 905
Inclination: 51
6449 deg
RA of node: 310
2822 deg
Eccentricity:
0001888
Arg of perigee: 53
8310 deg
Mean anomaly: 306
3015 deg
Mean motion: 15
49024683 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1576
Checksum: 288
Coasting Arc #7 (Orbit 1588)
---------------------------------------
Vector Time (GMT): 2020/323/04:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 965450
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2758678
17 A = 6792419
80 meter
Y = 3339516
96 meter E =
0005142
Z = 5228618
73 I = 51
30834
XDOT = -5038
507421 Wp = 58
43201
YDOT = 5691
615692 meter/sec RA = 305
62955 deg
ZDOT = -973
507222 TA = 40
95401
MA = 40
91541
Ha = 229
351 n
mi
Hp = 222
128
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9050781
41 X = 2695731
63
Y = 10956420
46 feet Y = 3370013
88 meter
Z = 17154260
94 Z = 5241867
04
XDOT = -16530
536159 XDOT = -5097
049504
YDOT = 18673
279830 feet/sec YDOT = 5634
944276 meter/sec
ZDOT = -3193
921333 ZDOT = -998
124189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2367439
67 X = 721595
61
Y = -13937568
36 feet Y = -4248170
84 meter
Z = 17215338
49 Z = 5247235
17
XDOT = 23907
345725 XDOT = 7286
958977
YDOT = -38
591407 feet/sec YDOT = -11
762661 meter/sec
ZDOT = -3308
003096 ZDOT = -1008
279344
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
25327528
00016717 00000-0 10270-3 0 9067
2 25544 51
6450 306
1314 0001516 60
9923 299
1379 15
49080479 15893
Satellite: ISS
Catalog Number: 25544
Epoch time: 20323
25327528 = yrday
fracday
Element set: 906
Inclination: 51
6450 deg
RA of node: 306
1314 deg
Eccentricity:
0001516
Arg of perigee: 60
9923 deg
Mean anomaly: 299
1379 deg
Mean motion: 15
49080479 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1589
Checksum: 314
Coasting Arc #8 (Orbit 1603)
---------------------------------------
Vector Time (GMT): 2020/324/04:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 965450
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3028954
74 A = 6792530
69 meter
Y = -3116561
85 meter E =
0015604
Z = -5233972
04 I = 51
28919
XDOT = 4533
341988 Wp = 94
46198
YDOT = -6078
953944 meter/sec RA = 300
66121 deg
ZDOT = 997
607721 TA = 185
15228
MA = 185
16836
Ha = 229
521 n
mi
Hp = 222
015
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9937515
56 X = -2968455
39
Y = -10224940
47 feet Y = -3150094
94 meter
Z = -17171824
27 Z = -5248539
07
XDOT = 14873
169251 XDOT = 4596
135906
YDOT = -19944
074619 feet/sec YDOT = -6027
907870 meter/sec
ZDOT = 3272
991212 ZDOT = 1019
780975
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -990051
47 X = -301767
69
Y = 14142533
45 feet Y = 4310644
20 meter
Z = -17239017
30 Z = -5254452
47
XDOT = -23720
388640 XDOT = -7229
974457
YDOT = 2448
797695 feet/sec YDOT = 746
393538 meter/sec
ZDOT = 3375
784890 ZDOT = 1028
939235
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
22097554
00016717 00000-0 10270-3 0 9079
2 25544 51
6446 301
3456 0001560 64
1334 295
9976 15
49051616 16049
Satellite: ISS
Catalog Number: 25544
Epoch time: 20324
22097554 = yrday
fracday
Element set: 907
Inclination: 51
6446 deg
RA of node: 301
3456 deg
Eccentricity:
0001560
Arg of perigee: 64
1334 deg
Mean anomaly: 295
9976 deg
Mean motion: 15
49051616 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1604
Checksum: 302
Coasting Arc #9 (Orbit 1619)
---------------------------------------
Vector Time (GMT): 2020/325/04:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 965450
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3260121
76 A = 6792427
10 meter
Y = 2873311
64 meter E =
0005229
Z = 5216922
33 I = 51
27381
XDOT = -4019
014986 Wp = 59
07751
YDOT = 6442
740029 meter/sec RA = 295
69028 deg
ZDOT = -1033
505252 TA = 40
89659
MA = 40
85738
Ha = 229
325 n
mi
Hp = 222
101
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10695937
52 X = 3202408
23
Y = 9426875
47 feet Y = 2909445
46 meter
Z = 17115886
92 Z = 5232618
94
XDOT = -13185
744705 XDOT = -4085
740743
YDOT = 21137
598520 feet/sec YDOT = 6397
423531 meter/sec
ZDOT = -3390
765263 ZDOT = -1053
189629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -354545
71 X = -108065
53
Y = -14165398
85 feet Y = -4317613
57 meter
Z = 17188322
16 Z = 5239000
59
XDOT = 23390
645923 XDOT = 7129
468877
YDOT = -4824
107162 feet/sec YDOT = -1470
387863 meter/sec
ZDOT = -3482
055759 ZDOT = -1061
330595
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
25318303
00016717 00000-0 10270-3 0 9082
2 25544 51
6453 296
2393 0001502 64
5696 295
5610 15
49090390 16201
Satellite: ISS
Catalog Number: 25544
Epoch time: 20325
25318303 = yrday
fracday
Element set: 908
Inclination: 51
6453 deg
RA of node: 296
2393 deg
Eccentricity:
0001502
Arg of perigee: 64
5696 deg
Mean anomaly: 295
5610 deg
Mean motion: 15
49090390 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1620
Checksum: 297
Coasting Arc #10 (Orbit 1634)
---------------------------------------
Vector Time (GMT): 2020/326/04:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 965450
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3490614
49 A = 6792574
39 meter
Y = -2613741
92 meter E =
0015666
Z = -5221787
88 I = 51
25903
XDOT = 3459
490222 Wp = 94
86515
YDOT = -6738
234249 meter/sec RA = 290
71936 deg
ZDOT = 1061
688168 TA = 185
37774
MA = 185
39458
Ha = 229
571 n
mi
Hp = 221
952
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11452147
29 X = -3435762
82
Y = -8575268
75 feet Y = -2652469
37 meter
Z = -17131850
01 Z = -5238610
99
XDOT = 11350
033537 XDOT = 3529
424980
YDOT = -22107
067745 feet/sec YDOT = -6699
156799 meter/sec
ZDOT = 3483
228896 ZDOT = 1078
662436
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1735858
43 X = 529089
65
Y = 14106971
73 feet Y = 4299804
98 meter
Z = -17209513
08 Z = -5245459
59
XDOT = -22725
203133 XDOT = -6926
641915
YDOT = 7135
863045 feet/sec YDOT = 2175
011056 meter/sec
ZDOT = 3561
986097 ZDOT = 1085
693362
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
22087693
00016717 00000-0 10270-3 0 9096
2 25544 51
6440 291
4532 0001681 66
0233 294
1092 15
49050323 16358
Satellite: ISS
Catalog Number: 25544
Epoch time: 20326
22087693 = yrday
fracday
Element set: 909
Inclination: 51
6440 deg
RA of node: 291
4532 deg
Eccentricity:
0001681
Arg of perigee: 66
0233 deg
Mean anomaly: 294
1092 deg
Mean motion: 15
49050323 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1635
Checksum: 288
Coasting Arc #11 (Orbit 1650)
---------------------------------------
Vector Time (GMT): 2020/327/04:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 965450
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3680132
60 A = 6792473
41 meter
Y = 2339642
39 meter E =
0005419
Z = 5204039
67 I = 51
24807
XDOT = -2894
777672 Wp = 60
73464
YDOT = 7009
965402 meter/sec RA = 285
74704 deg
ZDOT = -1100
984502 TA = 39
90069
MA = 39
86087
Ha = 229
362 n
mi
Hp = 222
047
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12073925
86 X = 3628418
11
Y = 7675992
09 feet Y = 2380506
79 meter
Z = 17073620
96 Z = 5221790
96
XDOT = -9497
302073 XDOT = -2967
602098
YDOT = 22998
574154 feet/sec YDOT = 6977
186801 meter/sec
ZDOT = -3612
153879 ZDOT = -1115
222718
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3053691
93 X = -930765
30
Y = -13876946
23 feet Y = -4229693
21 meter
Z = 17155593
90 Z = 5229025
02
XDOT = 21929
421435 XDOT = 6684
087654
YDOT = -9387
002991 feet/sec YDOT = -2861
158512 meter/sec
ZDOT = -3678
254044 ZDOT = -1121
131833
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
25307942
00016717 00000-0 10270-3 0 9104
2 25544 51
6438 286
3475 0001595 71
2458 288
8865 15
49089483 16510
Satellite: ISS
Catalog Number: 25544
Epoch time: 20327
25307942 = yrday
fracday
Element set: 910
Inclination: 51
6438 deg
RA of node: 286
3475 deg
Eccentricity:
0001595
Arg of perigee: 71
2458 deg
Mean anomaly: 288
8865 deg
Mean motion: 15
49089483 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1651
Checksum: 338
Coasting Arc #12 (Orbit 1665)
---------------------------------------
Vector Time (GMT): 2020/328/04:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 965450
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3867109
43 A = 6792625
94 meter
Y = -2049217
62 meter E =
0015680
Z = -5208667
44 I = 51
23923
XDOT = 2296
471547 Wp = 96
04703
YDOT = -7207
182872 meter/sec RA = 280
77377 deg
ZDOT = 1131
832320 TA = 184
88513
MA = 184
90045
Ha = 229
594 n
mi
Hp = 221
917
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12687366
88 X = -3818606
12
Y = -6723154
92 feet Y = -2092190
95 meter
Z = -17088803
94 Z = -5227334
79
XDOT = 7534
355470 XDOT = 2371
395933
YDOT = -23645
613097 feet/sec YDOT = -7181
083207 meter/sec
ZDOT = 3713
360630 ZDOT = 1143
169375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4394575
39 X = 1339466
58
Y = 13561098
18 feet Y = 4133422
73 meter
Z = -17175029
37 Z = -5234948
95
XDOT = -20817
585876 XDOT = -6345
200175
YDOT = 11510
227996 feet/sec YDOT = 3508
317493 meter/sec
ZDOT = 3766
036358 ZDOT = 1147
887882
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
22076872
00016717 00000-0 10270-3 0 9118
2 25544 51
6429 281
5606 0001681 73
2093 286
9242 15
49048591 16665
Satellite: ISS
Catalog Number: 25544
Epoch time: 20328
22076872 = yrday
fracday
Element set: 911
Inclination: 51
6429 deg
RA of node: 281
5606 deg
Eccentricity:
0001681
Arg of perigee: 73
2093 deg
Mean anomaly: 286
9242 deg
Mean motion: 15
49048591 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1666
Checksum: 317
Coasting Arc #13 (Orbit 1670)
---------------------------------------
Vector Time (GMT): 2020/328/12:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 965450
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1073818
80 A = 6801364
18 meter
Y = -6213086
04 meter E =
0007016
Z = -2548661
23 I = 51
26582
XDOT = 4731
801301 Wp = 54
82019
YDOT = -2961
378316 meter/sec RA = 279
11352 deg
ZDOT = 5239
809063 TA = 276
46675
MA = 276
54664
Ha = 229
619 n
mi
Hp = 222
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3523027
55 X = -991882
33
Y = -20384140
56 feet Y = -6224636
00 meter
Z = -8361749
44 Z = -2553678
76
XDOT = 15524
282484 XDOT = 4739
112437
YDOT = -9715
808125 feet/sec YDOT = -2908
423292 meter/sec
ZDOT = 17190
974616 ZDOT = 5262
812116
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20611860
88 X = 6282495
20
Y = 1640535
81 feet Y = 500035
31 meter
Z = -8384724
00 Z = -2555663
87
XDOT = 5758
705621 XDOT = 1755
253473
YDOT = 15815
440662 feet/sec YDOT = 4820
546314 meter/sec
ZDOT = 17297
425000 ZDOT = 5272
255140
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
54333154
00016717 00000-0 10270-3 0 9123
2 25544 51
6423 279
9659 0001870 65
9559 294
1787 15
49054186 16711
Satellite: ISS
Catalog Number: 25544
Epoch time: 20328
54333154 = yrday
fracday
Element set: 912
Inclination: 51
6423 deg
RA of node: 279
9659 deg
Eccentricity:
0001870
Arg of perigee: 65
9559 deg
Mean anomaly: 294
1787 deg
Mean motion: 15
49054186 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1671
Checksum: 338
Coasting Arc #14 (Orbit 1686)
---------------------------------------
Vector Time (GMT): 2020/329/12:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 965450
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1565620
22 A = 6801413
22 meter
Y = 6122356
05 meter E =
0015282
Z = 2497440
82 I = 51
26283
XDOT = -4476
741293 Wp = 100
12771
YDOT = 3304
167047 meter/sec RA = 274
13960 deg
ZDOT = -5268
583095 TA = 51
76050
MA = 51
62305
Ha = 229
617 n
mi
Hp = 221
939
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5136549
27 X = 1484910
53
Y = 20086470
00 feet Y = 6139412
56 meter
Z = 8193703
46 Z = 2504850
32
XDOT = -14687
471433 XDOT = -4487
764699
YDOT = 10840
443068 feet/sec YDOT = 3254
043510 meter/sec
ZDOT = -17285
377609 ZDOT = -5290
356240
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20716316
86 X = -6314333
38
Y = 354188
20 feet Y = 107956
56 meter
Z = 8227755
35 Z = 2507819
83
XDOT = -7196
597306 XDOT = -2193
522859
YDOT = -15150
068284 feet/sec YDOT = -4617
740813 meter/sec
ZDOT = -17386
146435 ZDOT = -5299
297433
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
57552673
00016717 00000-0 10270-3 0 9137
2 25544 51
6431 274
8592 0001966 68
0213 292
1146 15
49074535 16871
Satellite: ISS
Catalog Number: 25544
Epoch time: 20329
57552673 = yrday
fracday
Element set: 913
Inclination: 51
6431 deg
RA of node: 274
8592 deg
Eccentricity:
0001966
Arg of perigee: 68
0213 deg
Mean anomaly: 292
1146 deg
Mean motion: 15
49074535 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1687
Checksum: 322
Coasting Arc #15 (Orbit 1701)
---------------------------------------
Vector Time (GMT): 2020/330/12:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 965450
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2080563
38 A = 6801441
58 meter
Y = -5979089
40 meter E =
0007193
Z = -2484594
74 I = 51
26096
XDOT = 4181
997711 Wp = 55
08390
YDOT = -3642
361626 meter/sec RA = 269
16603 deg
ZDOT = 5278
231798 TA = 276
98708
MA = 277
06889
Ha = 229
639 n
mi
Hp = 221
916
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6825995
33 X = -2001479
83
Y = -19616435
03 feet Y = -6001913
45 meter
Z = -8151557
56 Z = -2494509
67
XDOT = 13720
464930 XDOT = 4196
777857
YDOT = -11950
005334 feet/sec YDOT = -3595
513133 meter/sec
ZDOT = 17317
033457 ZDOT = 5298
582348
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20605675
70 X = 6280609
95
Y = -2461398
42 feet Y = -750234
24 meter
Z = -8197211
31 Z = -2498510
01
XDOT = 8617
701354 XDOT = 2626
675373
YDOT = 14321
189255 feet/sec YDOT = 4365
098485 meter/sec
ZDOT = 17411
229574 ZDOT = 5306
942774
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
54320652
00016717 00000-0 10270-3 0 9147
2 25544 51
6424 270
0726 0001967 71
0212 289
1151 15
49069266 17029
Satellite: ISS
Catalog Number: 25544
Epoch time: 20330
54320652 = yrday
fracday
Element set: 914
Inclination: 51
6424 deg
RA of node: 270
0726 deg
Eccentricity:
0001967
Arg of perigee: 71
0212 deg
Mean anomaly: 289
1151 deg
Mean motion: 15
49069266 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1702
Checksum: 280
Coasting Arc #16 (Orbit 1717)
---------------------------------------
Vector Time (GMT): 2020/331/12:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 965450
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2550802
28 A = 6801524
62 meter
Y = 5809990
36 meter E =
0015402
Z = 2430631
35 I = 51
26384
XDOT = -3880
112936 Wp = 101
92265
YDOT = 3935
002082 meter/sec RA = 264
19255 deg
ZDOT = -5308
437096 TA = 50
78136
MA = 50
64472
Ha = 229
607 n
mi
Hp = 221
912
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8368773
87 X = 2473836
78
Y = 19061648
15 feet Y = 5838084
78 meter
Z = 7974512
31 Z = 2442835
78
XDOT = -12730
029319 XDOT = -3898
041109
YDOT = 12910
111818 feet/sec YDOT = 3891
511933 meter/sec
ZDOT = -17416
132205 ZDOT = -5327
328841
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20317155
67 X = -6192669
05
Y = 4437970
75 feet Y = 1352693
48 meter
Z = 8030769
22 Z = 2447778
46
XDOT = -9879
359873 XDOT = -3011
228889
YDOT = -13403
673491 feet/sec YDOT = -4085
439680 meter/sec
ZDOT = -17503
587258 ZDOT = -5335
093396
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
57539598
00016717 00000-0 10270-3 0 9153
2 25544 51
6432 264
9665 0001925 75
6228 284
5135 15
49079339 17183
Satellite: ISS
Catalog Number: 25544
Epoch time: 20331
57539598 = yrday
fracday
Element set: 915
Inclination: 51
6432 deg
RA of node: 264
9665 deg
Eccentricity:
0001925
Arg of perigee: 75
6228 deg
Mean anomaly: 284
5135 deg
Mean motion: 15
49079339 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1718
Checksum: 340
Coasting Arc #17 (Orbit 1732)
---------------------------------------
Vector Time (GMT): 2020/332/12:55:00
000
Vector Time (MET): N/A
Weight (LBS) : 965450
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3035455
14 A = 6801511
61 meter
Y = -5586185
37 meter E =
0007144
Z = -2415012
59 I = 51
26911
XDOT = 3540
286763 Wp = 55
29380
YDOT = -4216
961010 meter/sec RA = 259
21880 deg
ZDOT = 5319
727206 TA = 277
62795
MA = 277
70908
Ha = 229
578 n
mi
Hp = 221
895
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9958842
33 X = -2961032
13
Y = -18327379
82 feet Y = -5619713
71 meter
Z = -7923269
66 Z = -2429577
60
XDOT = 11615
114052 XDOT = 3561
338239
YDOT = -13835
173918 feet/sec YDOT = -4177
253662 meter/sec
ZDOT = 17453
173247 ZDOT = 5336
975722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19798465
70 X = 6034572
34
Y = -6482507
86 feet Y = -1975868
40 meter
Z = -7990459
41 Z = -2435492
03
XDOT = 11093
647675 XDOT = 3381
343811
YDOT = 12331
184163 feet/sec YDOT = 3758
544933 meter/sec
ZDOT = 17533
035055 ZDOT = 5344
069085
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
54306957
00016717 00000-0 10270-3 0 9163
2 25544 51
6437 260
1795 0001853 78
3244 281
8114 15
49090067 17333
Satellite: ISS
Catalog Number: 25544
Epoch time: 20332
54306957 = yrday
fracday
Element set: 916
Inclination: 51
6437 deg
RA of node: 260
1795 deg
Eccentricity:
0001853
Arg of perigee: 78
3244 deg
Mean anomaly: 281
8114 deg
Mean motion: 15
49090067 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1733
Checksum: 310
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