[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 2nd 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) : 16490 3108 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
Coasting Arc #1 (Orbit 1267)
---------------------------------------
Vector Time (GMT): 2020/302/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3354833
90 A = 6791255
21 meter
Y = 2521482
29 meter E =
0004160
Z = 5335985
33 I = 51
91887
XDOT = -4921
718054 Wp = 71
25440
YDOT = -5866
202924 meter/sec RA = 48
12210 deg
ZDOT = -320
837404 TA = 21
80304
MA = 21
78534
Ha = 229
160 n
mi
Hp = 221
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11006672
91 X = -3408700
17
Y = 8272579
70 feet Y = 2483665
17 meter
Z = 17506513
56 Z = 5319557
63
XDOT = -16147
368943 XDOT = -4854
196134
YDOT = -19246
072586 feet/sec YDOT = -5920
863583 meter/sec
ZDOT = -1052
616155 ZDOT = -344
581353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4048886
18 X = 1234100
51
Y = -13260807
06 feet Y = -4041893
99 meter
Z = 17430374
56 Z = 5312778
17
XDOT = 23443
489252 XDOT = 7145
575524
YDOT = 5623
734964 feet/sec YDOT = 1714
114417 meter/sec
ZDOT = -1162
238670 ZDOT = -354
250347
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 20302
54779374
00016717 00000-0 10270-3 0 9000
2 25544 51
6452 48
5907 0001575 67
5552 292
5765 15
49377052 12682
Satellite: ISS
Catalog Number: 25544
Epoch time: 20302
54779374 = yrday
fracday
Element set: 900
Inclination: 51
6452 deg
RA of node: 48
5907 deg
Eccentricity:
0001575
Arg of perigee: 67
5552 deg
Mean anomaly: 292
5765 deg
Mean motion: 15
49377052 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1268
Checksum: 326
Coasting Arc #2 (Orbit 1282)
---------------------------------------
Vector Time (GMT): 2020/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3239534
72 A = 6791355
82 meter
Y = -2699950
91 meter E =
0016228
Z = -5337395
26 I = 51
89550
XDOT = 5316
040512 Wp = 91
23167
YDOT = 5480
421558 meter/sec RA = 43
19287 deg
ZDOT = 455
128778 TA = 183
10013
MA = 183
11019
Ha = 229
082 n
mi
Hp = 221
715
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10628394
74 X = 3295412
19
Y = -8858106
66 feet Y = -2663411
88 meter
Z = -17511139
29 Z = -5321522
70
XDOT = 17441
077795 XDOT = 5252
150877
YDOT = 17980
385688 feet/sec YDOT = 5539
512126 meter/sec
ZDOT = 1493
204653 ZDOT = 480
797199
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3164183
73 X = -964443
20
Y = 13564225
78 feet Y = 4134376
02 meter
Z = -17437561
41 Z = -5314968
72
XDOT = -23777
008641 XDOT = -7247
232234
YDOT = -3478
222190 feet/sec YDOT = -1060
162124 meter/sec
ZDOT = 1611
731217 ZDOT = 491
255675
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 20303
51530531
00016717 00000-0 10270-3 0 9019
2 25544 51
6452 43
8043 0001630 71
2596 288
8731 15
49360714 12838
Satellite: ISS
Catalog Number: 25544
Epoch time: 20303
51530531 = yrday
fracday
Element set: 901
Inclination: 51
6452 deg
RA of node: 43
8043 deg
Eccentricity:
0001630
Arg of perigee: 71
2596 deg
Mean anomaly: 288
8731 deg
Mean motion: 15
49360714 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1283
Checksum: 281
Coasting Arc #3 (Orbit 1298)
---------------------------------------
Vector Time (GMT): 2020/304/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3110618
24 A = 6791304
30 meter
Y = 2858830
92 meter E =
0004459
Z = 5313827
15 I = 51
87064
XDOT = -5698
950347 Wp = 67
32393
YDOT = -5089
794190 meter/sec RA = 38
26010 deg
ZDOT = -595
687744 TA = 28
35873
MA = 28
33446
Ha = 229
119 n
mi
Hp = 221
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10205440
41 X = -3168167
55
Y = 9379366
54 feet Y = 2823724
11 meter
Z = 17433816
11 Z = 5298576
74
XDOT = -18697
343658 XDOT = -5638
717585
YDOT = -16698
799836 feet/sec YDOT = -5153
187176 meter/sec
ZDOT = -1954
356114 ZDOT = -623
225292
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2274847
83 X = 693373
62
Y = -13762593
62 feet Y = -4194838
53 meter
Z = 17363109
14 Z = 5292275
67
XDOT = 24009
968396 XDOT = 7318
238367
YDOT = 1333
949966 feet/sec YDOT = 406
587950 meter/sec
ZDOT = -2081
530209 ZDOT = -634
450408
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 20304
54731313
00016717 00000-0 10270-3 0 9025
2 25544 51
6457 38
6966 0001518 73
3459 286
7857 15
49391671 12994
Satellite: ISS
Catalog Number: 25544
Epoch time: 20304
54731313 = yrday
fracday
Element set: 902
Inclination: 51
6457 deg
RA of node: 38
6966 deg
Eccentricity:
0001518
Arg of perigee: 73
3459 deg
Mean anomaly: 286
7857 deg
Mean motion: 15
49391671 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1299
Checksum: 333
Coasting Arc #4 (Orbit 1313)
---------------------------------------
Vector Time (GMT): 2020/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2983666
71 A = 6791456
03 meter
Y = -3030344
45 meter E =
0016019
Z = -5309068
61 I = 51
84369
XDOT = 6027
021669 Wp = 93
36064
YDOT = 4652
114363 meter/sec RA = 33
32686 deg
ZDOT = 732
784404 TA = 183
63167
MA = 183
64331
Ha = 229
069 n
mi
Hp = 221
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9788932
79 X = 3043120
34
Y = -9942074
96 feet Y = -2996646
57 meter
Z = -17418204
10 Z = -5294430
28
XDOT = 19773
693141 XDOT = 5970
992828
YDOT = 15262
842399 feet/sec YDOT = 4719
199575 meter/sec
ZDOT = 2404
148308 ZDOT = 761
926015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1358850
97 X = -414177
77
Y = 13970749
20 feet Y = 4258284
36 meter
Z = -17350319
43 Z = -5288377
36
XDOT = -23936
544127 XDOT = -7295
858650
YDOT = 820
639416 feet/sec YDOT = 250
130894 meter/sec
ZDOT = 2538
746318 ZDOT = 773
809878
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 20305
51481828
00016717 00000-0 10270-3 0 9037
2 25544 51
6459 33
9096 0001604 73
4767 286
6560 15
49366747 13141
Satellite: ISS
Catalog Number: 25544
Epoch time: 20305
51481828 = yrday
fracday
Element set: 903
Inclination: 51
6459 deg
RA of node: 33
9096 deg
Eccentricity:
0001604
Arg of perigee: 73
4767 deg
Mean anomaly: 286
6560 deg
Mean motion: 15
49366747 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1314
Checksum: 322
Coasting Arc #5 (Orbit 1329)
---------------------------------------
Vector Time (GMT): 2020/306/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2846963
37 A = 6791417
30 meter
Y = 3180508
86 meter E =
0005002
Z = 5278710
16 I = 51
81530
XDOT = -6341
612968 Wp = 63
26701
YDOT = -4213
248476 meter/sec RA = 28
39064 deg
ZDOT = -878
831001 TA = 35
13788
MA = 35
10491
Ha = 229
112 n
mi
Hp = 221
550
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9340431
01 X = -2907958
90
Y = 10434740
35 feet Y = 3148330
97 meter
Z = 17318602
90 Z = 5264732
20
XDOT = -20805
816823 XDOT = -6289
758839
YDOT = -13822
993689 feet/sec YDOT = -4283
875000 meter/sec
ZDOT = -2883
303808 ZDOT = -909
511084
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 457072
50 X = 139315
70
Y = -14076938
08 feet Y = -4290650
73 meter
Z = 17253763
73 Z = 5258947
19
XDOT = 23765
174407 XDOT = 7243
625159
YDOT = -2947
501541 feet/sec YDOT = -898
398470 meter/sec
ZDOT = -3025
024117 ZDOT = -922
027351
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 20306
54681781
00016717 00000-0 10270-3 0 9042
2 25544 51
6462 28
8023 0001582 74
1897 285
9427 15
49403810 13300
Satellite: ISS
Catalog Number: 25544
Epoch time: 20306
54681781 = yrday
fracday
Element set: 904
Inclination: 51
6462 deg
RA of node: 28
8023 deg
Eccentricity:
0001582
Arg of perigee: 74
1897 deg
Mean anomaly: 285
9427 deg
Mean motion: 15
49403810 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1330
Checksum: 306
Coasting Arc #6 (Orbit 1344)
---------------------------------------
Vector Time (GMT): 2020/307/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2706856
37 A = 6791632
30 meter
Y = -3346566
88 meter E =
0015829
Z = -5267392
94 I = 51
78389
XDOT = 6596
602126 Wp = 95
49259
YDOT = 3735
493362 meter/sec RA = 23
45363 deg
ZDOT = 1017
788366 TA = 184
25136
MA = 184
26482
Ha = 229
105 n
mi
Hp = 221
647
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8880762
36 X = 2769664
25
Y = -10979550
14 feet Y = -3315945
53 meter
Z = -17281472
90 Z = -5254091
25
XDOT = 21642
395427 XDOT = 6549
396454
YDOT = 12255
555649 feet/sec YDOT = 3808
997326 meter/sec
ZDOT = 3339
200675 ZDOT = 1049
718480
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 490254
05 X = 149429
44
Y = 14188290
73 feet Y = 4324591
01 meter
Z = -17219751
00 Z = -5248580
10
XDOT = -23294
439928 XDOT = -7100
145290
YDOT = 5031
945868 feet/sec YDOT = 1533
737101 meter/sec
ZDOT = 3486
713616 ZDOT = 1062
750310
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20307
51431737
00016717 00000-0 10270-3 0 9055
2 25544 51
6448 24
0153 0001683 76
8880 283
2458 15
49366591 13454
Satellite: ISS
Catalog Number: 25544
Epoch time: 20307
51431737 = yrday
fracday
Element set: 905
Inclination: 51
6448 deg
RA of node: 24
0153 deg
Eccentricity:
0001683
Arg of perigee: 76
8880 deg
Mean anomaly: 283
2458 deg
Mean motion: 15
49366591 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1345
Checksum: 313
Coasting Arc #7 (Orbit 1360)
---------------------------------------
Vector Time (GMT): 2020/308/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2559533
58 A = 6791613
77 meter
Y = 3490411
18 meter E =
0005507
Z = 5229945
11 I = 51
75310
XDOT = -6837
498233 Wp = 62
24486
YDOT = -3259
846163 meter/sec RA = 18
51330 deg
ZDOT = -1167
238800 TA = 38
95674
MA = 38
91708
Ha = 229
093 n
mi
Hp = 221
541
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8397419
88 X = -2623778
97
Y = 11451480
24 feet Y = 3461429
16 meter
Z = 17158612
56 Z = 5217355
67
XDOT = -22432
736986 XDOT = -6794
867531
YDOT = -10695
033343 feet/sec YDOT = -3336
069553 meter/sec
ZDOT = -3829
523623 ZDOT = -1200
350233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1409957
55 X = -429755
06
Y = -14200953
35 feet Y = -4328450
58 meter
Z = 17100175
11 Z = 5212133
37
XDOT = 22734
555780 XDOT = 6929
492602
YDOT = -7066
447404 feet/sec YDOT = -2153
853169 meter/sec
ZDOT = -3982
514479 ZDOT = -1213
870413
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20308
54631125
00016717 00000-0 10270-3 0 9063
2 25544 51
6452 18
9080 0001554 80
8008 279
3318 15
49407496 13613
Satellite: ISS
Catalog Number: 25544
Epoch time: 20308
54631125 = yrday
fracday
Element set: 906
Inclination: 51
6452 deg
RA of node: 18
9080 deg
Eccentricity:
0001554
Arg of perigee: 80
8008 deg
Mean anomaly: 279
3318 deg
Mean motion: 15
49407496 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1361
Checksum: 300
Coasting Arc #8 (Orbit 1375)
---------------------------------------
Vector Time (GMT): 2020/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2405155
28 A = 6791854
92 meter
Y = -3650448
67 meter E =
0015489
Z = -5211643
12 I = 51
72040
XDOT = 7014
456458 Wp = 97
62836
YDOT = 2755
459154 meter/sec RA = 13
57092 deg
ZDOT = 1308
447278 TA = 184
95047
MA = 184
96581
Ha = 229
112 n
mi
Hp = 221
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7890929
40 X = 2471112
75
Y = -11976537
65 feet Y = -3623183
38 meter
Z = -17098566
67 Z = -5199799
56
XDOT = 23013
308590 XDOT = 6976
766902
YDOT = 9040
220322 feet/sec YDOT = 2833
689020 meter/sec
ZDOT = 4292
806030 ZDOT = 1342
430246
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2383005
80 X = 726340
17
Y = 14209266
72 feet Y = 4330984
50 meter
Z = -17043568
45 Z = -5194879
66
XDOT = -21892
814768 XDOT = -6672
929941
YDOT = 9003
771717 feet/sec YDOT = 2744
349619 meter/sec
ZDOT = 4449
846595 ZDOT = 1356
313242
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20309
51380379
00016717 00000-0 10270-3 0 9074
2 25544 51
6446 14
1200 0001707 79
7242 280
4100 15
49370769 13765
Satellite: ISS
Catalog Number: 25544
Epoch time: 20309
51380379 = yrday
fracday
Element set: 907
Inclination: 51
6446 deg
RA of node: 14
1200 deg
Eccentricity:
0001707
Arg of perigee: 79
7242 deg
Mean anomaly: 280
4100 deg
Mean motion: 15
49370769 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1376
Checksum: 293
Coasting Arc #9 (Orbit 1391)
---------------------------------------
Vector Time (GMT): 2020/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 938443
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2247227
08 A = 6791868
86 meter
Y = 3787650
65 meter E =
0006280
Z = 5166282
43 I = 51
68787
XDOT = -7176
862046 Wp = 61
53815
YDOT = -2257
457643 meter/sec RA = 8
62618 deg
ZDOT = -1462
461189 TA = 42
56074
MA = 42
51208
Ha = 229
122 n
mi
Hp = 221
481
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7372792
25 X = -2314510
08
Y = 12426675
35 feet Y = 3762143
97 meter
Z = 16949745
49 Z = 5155202
89
XDOT = -23546
135321 XDOT = -7143
981121
YDOT = -7406
357095 feet/sec YDOT = -2337
530510 meter/sec
ZDOT = -4798
101013 ZDOT = -1497
244610
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3313013
12 X = -1009806
40
Y = -14126093
59 feet Y = -4305633
33 meter
Z = 16898272
76 Z = 5150593
54
XDOT = 20976
132948 XDOT = 6393
525323
YDOT = -10868
413754 feet/sec YDOT = -3312
692512 meter/sec
ZDOT = -4958
864705 ZDOT = -1511
461962
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20310
54578983
00016717 00000-0 10270-3 0 9080
2 25544 51
6448 9
0126 0001692 82
2411 277
8931 15
49412391 13925
Satellite: ISS
Catalog Number: 25544
Epoch time: 20310
54578983 = yrday
fracday
Element set: 908
Inclination: 51
6448 deg
RA of node: 9
0126 deg
Eccentricity:
0001692
Arg of perigee: 82
2411 deg
Mean anomaly: 277
8931 deg
Mean motion: 15
49412391 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1392
Checksum: 309
Coasting Arc #10 (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 = 2075389
30 A = 6792145
99 meter
Y = -3941710
77 meter E =
0015193
Z = -5140866
68 I = 51
65364
XDOT = 7273
846538 Wp = 99
78930
YDOT = 1739
471482 meter/sec RA = 3
67936 deg
ZDOT = 1604
292018 TA = 185
71327
MA = 185
73062
Ha = 229
170 n
mi
Hp = 221
531
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6809020
00 X = 2144284
26
Y = -12932121
95 feet Y = -3918116
70 meter
Z = -16866360
50 Z = -5130618
02
XDOT = 23864
325913 XDOT = 7246
061768
YDOT = 5706
927434 feet/sec YDOT = 1820
657385 meter/sec
ZDOT = 5263
425256 ZDOT = 1639
558758
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4311754
50 X = 1314222
77
Y = 14021982
01 feet Y = 4273900
12 meter
Z = -16818722
95 Z = -5126346
75
XDOT = -19804
043226 XDOT = -6036
272375
YDOT = 12592
460621 feet/sec YDOT = 3838
181997 meter/sec
ZDOT = 5426
447722 ZDOT = 1653
981266
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
51327715
00016717 00000-0 10270-3 0 9094
2 25544 51
6437 4
2247 0001860 84
3420 275
7943 15
49372683 14070
Satellite: ISS
Catalog Number: 25544
Epoch time: 20311
51327715 = yrday
fracday
Element set: 909
Inclination: 51
6437 deg
RA of node: 4
2247 deg
Eccentricity:
0001860
Arg of perigee: 84
3420 deg
Mean anomaly: 275
7943 deg
Mean motion: 15
49372683 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1407
Checksum: 298
Coasting Arc #11 (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 = 6791670
51 A = 6803093
61 meter
Y = 62524
12 meter E =
0013217
Z = -273452
76 I = 51
67967
XDOT = 190
006017 Wp = 48
33290
YDOT = 4755
946132 meter/sec RA = 2
35089 deg
ZDOT = 6002
754655 TA = 308
72793
MA = 308
84601
Ha = 229
184 n
mi
Hp = 221
398
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22282383
57 X = 6791794
87
Y = 205131
62 feet Y = 138474
16 meter
Z = -897154
74 Z = -240460
65
XDOT = 623
379321 XDOT = 107
651057
YDOT = 15603
497808 feet/sec YDOT = 4757
610027 meter/sec
ZDOT = 19694
076951 ZDOT = 6003
477944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17682347
38 X = 5389579
48
Y = 13569517
69 feet Y = 4135988
99 meter
Z = -744556
26 Z = -226940
75
XDOT = -8005
905680 XDOT = -2440
200051
YDOT = 11470
661850 feet/sec YDOT = 3496
257732 meter/sec
ZDOT = 19697
141576 ZDOT = 6003
688752
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
77127347
00016717 00000-0 10270-3 0 9103
2 25544 51
6420 2
9484 0001949 81
0894 279
0477 15
49397291 14113
Satellite: ISS
Catalog Number: 25544
Epoch time: 20311
77127347 = yrday
fracday
Element set: 910
Inclination: 51
6420 deg
RA of node: 2
9484 deg
Eccentricity:
0001949
Arg of perigee: 81
0894 deg
Mean anomaly: 279
0477 deg
Mean motion: 15
49397291 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1411
Checksum: 310
Coasting Arc #12 (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 = -6784999
46 A = 6803136
56 meter
Y = 396340
24 meter E =
0013432
Z = 111856
05 I = 51
64731
XDOT = -383
993522 Wp = 126
93393
YDOT = -4739
855509 meter/sec RA = 357
40305 deg
ZDOT = -6006
200570 TA = 51
86370
MA = 51
74271
Ha = 229
129 n
mi
Hp = 221
468
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22260496
90 X = -6789470
52
Y = 1300328
88 feet Y = 320440
50 meter
Z = 366981
80 Z = 78885
92
XDOT = -1259
821266 XDOT = -301
787424
YDOT = -15550
707052 feet/sec YDOT = -4743
689608 meter/sec
ZDOT = -19705
382448 ZDOT = -6007
866495
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18777158
31 X = -5723277
85
Y = -12030277
79 feet Y = -3666828
67 meter
Z = 214465
48 Z = 65369
08
XDOT = 7351
427889 XDOT = 2240
715220
YDOT = -11874
899496 feet/sec YDOT = -3619
469366 meter/sec
ZDOT = -19712
809424 ZDOT = -6008
464312
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
80325455
00016717 00000-0 10270-3 0 9119
2 25544 51
6435 357
8404 0001879 81
7112 278
4244 15
49389929 14276
Satellite: ISS
Catalog Number: 25544
Epoch time: 20312
80325455 = yrday
fracday
Element set: 911
Inclination: 51
6435 deg
RA of node: 357
8404 deg
Eccentricity:
0001879
Arg of perigee: 81
7112 deg
Mean anomaly: 278
4244 deg
Mean motion: 15
49389929 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1427
Checksum: 319
Coasting Arc #13 (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 = 6739007
08 A = 6803096
77 meter
Y = -887011
50 meter E =
0013737
Z = 7272
00 I = 51
61340
XDOT = 606
415392 Wp = 50
50846
YDOT = 4718
540655 meter/sec RA = 352
45307 deg
ZDOT = 6005
119066 TA = 309
56974
MA = 309
69100
Ha = 229
155 n
mi
Hp = 221
390
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22109603
27 X = 6748389
73
Y = -2910142
71 feet Y = -811598
62 meter
Z = 23858
26 Z = 40030
59
XDOT = 1989
551812 XDOT = 524
436405
YDOT = 15480
776426 feet/sec YDOT = 4724
863401 meter/sec
ZDOT = 19701
834205 ZDOT = 6007
865913
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19778970
03 X = 6028630
06
Y = 10298816
96 feet Y = 3139079
41 meter
Z = 175415
32 Z = 53466
59
XDOT = -6610
807948 XDOT = -2014
974262
YDOT = 12302
750184 feet/sec YDOT = 3749
878256 meter/sec
ZDOT = 19714
264813 ZDOT = 6008
907915
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
83523161
00016717 00000-0 10270-3 0 9128
2 25544 51
6433 352
7331 0001911 84
1356 276
0012 15
49404240 14430
Satellite: ISS
Catalog Number: 25544
Epoch time: 20313
83523161 = yrday
fracday
Element set: 912
Inclination: 51
6433 deg
RA of node: 352
7331 deg
Eccentricity:
0001911
Arg of perigee: 84
1356 deg
Mean anomaly: 276
0012 deg
Mean motion: 15
49404240 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1443
Checksum: 262
Coasting Arc #14 (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 = -6662807
80 A = 6803108
55 meter
Y = 1336837
10 meter E =
0012949
Z = -172507
35 I = 51
58015
XDOT = -795
210713 Wp = 128
96411
YDOT = -4697
242461 meter/sec RA = 347
50103 deg
ZDOT = -5998
854438 TA = 52
89204
MA = 52
77377
Ha = 229
150 n
mi
Hp = 221
421
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21859605
65 X = -6676423
57
Y = 4385948
48 feet Y = 1262252
67 meter
Z = -565969
01 Z = -204906
10
XDOT = -2608
959032 XDOT = -713
486269
YDOT = -15410
900464 feet/sec YDOT = -4705
677986 meter/sec
ZDOT = -19681
280964 ZDOT = -6002
518923
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20568558
80 X = -6269296
72
Y = -8591922
66 feet Y = -2618818
03 meter
Z = -715875
82 Z = -218198
95
XDOT = 5945
159785 XDOT = 1812
084702
YDOT = -12658
455444 feet/sec YDOT = -3858
297219 meter/sec
ZDOT = -19697
960524 ZDOT = -6003
938368
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
80270869
00016717 00000-0 10270-3 0 9131
2 25544 51
6435 347
9449 0001959 85
0478 275
0896 15
49392980 14587
Satellite: ISS
Catalog Number: 25544
Epoch time: 20314
80270869 = yrday
fracday
Element set: 913
Inclination: 51
6435 deg
RA of node: 347
9449 deg
Eccentricity:
0001959
Arg of perigee: 85
0478 deg
Mean anomaly: 275
0896 deg
Mean motion: 15
49392980 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1458
Checksum: 352
Coasting Arc #15 (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 = 6544034
48 A = 6803053
57 meter
Y = -1812935
07 meter E =
0014174
Z = 293710
31 I = 51
54664
XDOT = 1015
487807 Wp = 53
30571
YDOT = 4667
242389 meter/sec RA = 342
54698 deg
ZDOT = 5990
304062 TA = 309
85750
MA = 309
98210
Ha = 229
146 n
mi
Hp = 221
385
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21469929
38 X = 6562394
20
Y = -5947949
69 feet Y = -1739652
32 meter
Z = 963616
51 Z = 325543
72
XDOT = 3331
652909 XDOT = 934
123917
YDOT = 15312
475031 feet/sec YDOT = 4678
143322 meter/sec
ZDOT = 19653
228550 ZDOT = 5995
039394
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21235819
25 X = 6472677
71
Y = 6713446
49 feet Y = 2046258
49 meter
Z = 1110921
70 Z = 338608
93
XDOT = -5177
951349 XDOT = -1578
239571
YDOT = 13032
277990 feet/sec YDOT = 3972
238331 meter/sec
ZDOT = 19674
865524 ZDOT = 5996
899012
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
83468200
00016717 00000-0 10270-3 0 9144
2 25544 51
6429 342
8380 0001899 89
3140 270
8228 15
49403144 14749
Satellite: ISS
Catalog Number: 25544
Epoch time: 20315
83468200 = yrday
fracday
Element set: 914
Inclination: 51
6429 deg
RA of node: 342
8380 deg
Eccentricity:
0001899
Arg of perigee: 89
3140 deg
Mean anomaly: 270
8228 deg
Mean motion: 15
49403144 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1474
Checksum: 307
Coasting Arc #16 (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 = -6400703
30 A = 6802994
82 meter
Y = 2242923
41 meter E =
0012349
Z = -461138
00 I = 51
51570
XDOT = -1203
905654 Wp = 131
67619
YDOT = -4640
931425 meter/sec RA = 337
59013 deg
ZDOT = -5974
192133 TA = 53
29523
MA = 53
18185
Ha = 229
096 n
mi
Hp = 221
430
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20999682
75 X = -6423068
65
Y = 7358672
62 feet Y = 2171221
10 meter
Z = -1512919
96 Z = -492285
03
XDOT = -3949
821698 XDOT = -1122
900116
YDOT = -15226
152969 feet/sec YDOT = -4653
941432 meter/sec
ZDOT = -19600
367889 ZDOT = -5979
843595
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21694940
50 X = -6612617
87
Y = -4899936
13 feet Y = -1493500
53 meter
Z = -1657059
92 Z = -505071
86
XDOT = 4488
482748 XDOT = 1368
089541
YDOT = -13349
157159 feet/sec YDOT = -4068
823102 meter/sec
ZDOT = -19626
245105 ZDOT = -5982
079508
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
80215427
00016717 00000-0 10270-3 0 9154
2 25544 51
6441 338
0495 0001864 92
0741 268
0622 15
49401733 14892
Satellite: ISS
Catalog Number: 25544
Epoch time: 20316
80215427 = yrday
fracday
Element set: 915
Inclination: 51
6441 deg
RA of node: 338
0495 deg
Eccentricity:
0001864
Arg of perigee: 92
0741 deg
Mean anomaly: 268
0622 deg
Mean motion: 15
49401733 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1489
Checksum: 300
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