[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 22nd 2020
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) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 475 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
238/20:27:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
4
000/00:00:00
000 0
0 0
0 221
8
245/23:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
4
000/00:00:00
000 0
0 0
0 221
8
249/11:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
1
000/00:00:00
000 0
0 0
0 221
8
Coasting Arc #1 (Orbit 213)
---------------------------------------
Vector Time (GMT): 2020/234/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1448012
37 A = 6794446
49 meter
Y = 4709718
59 meter E =
0008676
Z = 4672447
78 I = 51
79596
XDOT = -7055
235918 Wp = 108
22739
YDOT = -720
078642 meter/sec RA = 24
63634 deg
ZDOT = 2905
196035 TA = 312
89393
MA = 312
96674
Ha = 229
116 n
mi
Hp = 222
070
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4750696
74 X = 1372543
53
Y = 15451832
64 feet Y = 4725489
51 meter
Z = 15329553
09 Z = 4679298
07
XDOT = -23147
099468 XDOT = -7060
770988
YDOT = -2362
462737 feet/sec YDOT = -799
006177 meter/sec
ZDOT = 9531
483055 ZDOT = 2870
911578
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3876588
85 X = 1181584
28
Y = -15663273
92 feet Y = -4774165
89 meter
Z = 15360903
57 Z = 4682003
41
XDOT = 17626
337182 XDOT = 5372
507573
YDOT = 13577
456146 feet/sec YDOT = 4138
408633 meter/sec
ZDOT = 9373
244126 ZDOT = 2856
964809
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 20234
55348663
00016717 00000-0 10270-3 0 9008
2 25544 51
6420 24
9750 0001230 52
3978 307
7283 15
49198389 2141
Satellite: ISS
Catalog Number: 25544
Epoch time: 20234
55348663 = yrday
fracday
Element set: 900
Inclination: 51
6420 deg
RA of node: 24
9750 deg
Eccentricity:
0001230
Arg of perigee: 52
3978 deg
Mean anomaly: 307
7283 deg
Mean motion: 15
49198389 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 214
Checksum: 303
Coasting Arc #2 (Orbit 228)
---------------------------------------
Vector Time (GMT): 2020/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1763055
63 A = 6794349
09 meter
Y = -4576455
43 meter E =
0012249
Z = -4714151
62 I = 51
76515
XDOT = 7105
344878 Wp = 68
75480
YDOT = 175
865620 meter/sec RA = 19
69936 deg
ZDOT = -2829
684199 TA = 173
16034
MA = 173
14361
Ha = 229
251 n
mi
Hp = 221
952
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5784303
24 X = -1688850
87
Y = -15014617
57 feet Y = -4595756
47 meter
Z = -15466376
70 Z = -4722535
35
XDOT = 23311
498942 XDOT = 7116
595065
YDOT = 576
986943 feet/sec YDOT = 255
385461 meter/sec
ZDOT = -9283
740810 ZDOT = -2795
142242
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2492860
29 X = -759823
82
Y = 15858508
48 feet Y = 4833673
38 meter
Z = -15504807
93 Z = -4725865
46
XDOT = -18872
381097 XDOT = -5752
301758
YDOT = -11882
256821 feet/sec YDOT = -3621
711879 meter/sec
ZDOT = -9124
297253 ZDOT = -2781
085803
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 20235
52110466
00016717 00000-0 10270-3 0 9015
2 25544 51
6429 20
1884 0001461 57
3158 302
8133 15
49185219 2291
Satellite: ISS
Catalog Number: 25544
Epoch time: 20235
52110466 = yrday
fracday
Element set: 901
Inclination: 51
6429 deg
RA of node: 20
1884 deg
Eccentricity:
0001461
Arg of perigee: 57
3158 deg
Mean anomaly: 302
8133 deg
Mean motion: 15
49185219 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 229
Checksum: 280
Coasting Arc #3 (Orbit 244)
---------------------------------------
Vector Time (GMT): 2020/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2077650
89 A = 6794179
56 meter
Y = 4406183
07 meter E =
0008493
Z = 4730372
44 I = 51
73229
XDOT = -7134
974765 Wp = 109
66095
YDOT = 381
335361 meter/sec RA = 14
75934 deg
ZDOT = 2771
744134 TA = 312
87494
MA = 312
94623
Ha = 229
134 n
mi
Hp = 222
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6816439
94 X = 2005247
90
Y = 14455981
19 feet Y = 4429012
16 meter
Z = 15519594
61 Z = 4740288
81
XDOT = -23408
709860 XDOT = -7152
172161
YDOT = 1251
100265 feet/sec YDOT = 301
450893 meter/sec
ZDOT = 9093
648732 ZDOT = 2737
043631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1046438
37 X = 318954
42
Y = -15903760
51 feet Y = -4847466
20 meter
Z = 15565102
98 Z = 4744243
39
XDOT = 20034
655240 XDOT = 6106
562917
YDOT = 10083
377864 feet/sec YDOT = 3073
413573 meter/sec
ZDOT = 8933
455418 ZDOT = 2722
917211
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 20236
55322812
00016717 00000-0 10270-3 0 9020
2 25544 51
6426 15
0815 0001291 60
7115 299
4164 15
49204779 2453
Satellite: ISS
Catalog Number: 25544
Epoch time: 20236
55322812 = yrday
fracday
Element set: 902
Inclination: 51
6426 deg
RA of node: 15
0815 deg
Eccentricity:
0001291
Arg of perigee: 60
7115 deg
Mean anomaly: 299
4164 deg
Mean motion: 15
49204779 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 245
Checksum: 287
Coasting Arc #4 (Orbit 259)
---------------------------------------
Vector Time (GMT): 2020/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2364837
57 A = 6794123
83 meter
Y = -4233244
50 meter E =
0012544
Z = -4770993
44 I = 51
69926
XDOT = 7099
039552 Wp = 70
10008
YDOT = -931
023116 meter/sec RA = 9
81785 deg
ZDOT = -2694
306424 TA = 173
24223
MA = 173
22530
Ha = 229
246 n
mi
Hp = 221
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7758653
45 X = -2294149
72
Y = -13888597
43 feet Y = -4259294
61 meter
Z = -15652865
62 Z = -4782309
13
XDOT = 23290
812179 XDOT = 7122
010276
YDOT = -3054
537781 feet/sec YDOT = -851
508166 meter/sec
ZDOT = -8839
588006 ZDOT = -2659
766377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 324399
14 X = 98876
86
Y = 15854178
10 feet Y = 4832353
49 meter
Z = -15704835
11 Z = -4786833
74
XDOT = -20941
644975 XDOT = -6383
013388
YDOT = -8164
632297 feet/sec YDOT = -2488
579924 meter/sec
ZDOT = -8680
114995 ZDOT = -2645
699050
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 20237
52084486
00016717 00000-0 10270-3 0 9031
2 25544 51
6430 10
2947 0001353 63
6269 296
5020 15
49179055 2606
Satellite: ISS
Catalog Number: 25544
Epoch time: 20237
52084486 = yrday
fracday
Element set: 903
Inclination: 51
6430 deg
RA of node: 10
2947 deg
Eccentricity:
0001353
Arg of perigee: 63
6269 deg
Mean anomaly: 296
5020 deg
Mean motion: 15
49179055 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 260
Checksum: 291
Coasting Arc #5 (Orbit 275)
---------------------------------------
Vector Time (GMT): 2020/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2645475
44 A = 6793914
88 meter
Y = 4024177
59 meter E =
0008209
Z = 4786765
27 I = 51
66647
XDOT = -7041
636211 Wp = 111
08065
YDOT = 1489
251588 meter/sec RA = 4
87291 deg
ZDOT = 2633
133416 TA = 312
90845
MA = 312
97732
Ha = 229
119 n
mi
Hp = 221
971
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8679381
35 X = 2577027
97
Y = 13202682
38 feet Y = 4053378
42 meter
Z = 15704610
45 Z = 4799449
71
XDOT = -23102
481006 XDOT = -7070
556334
YDOT = 4885
996024 feet/sec YDOT = 1410
345243 meter/sec
ZDOT = 8638
889161 ZDOT = 2598
857791
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1727442
93 X = -526524
60
Y = -15646856
10 feet Y = -4769161
74 meter
Z = 15762902
89 Z = 4804532
80
XDOT = 21746
731702 XDOT = 6628
403823
YDOT = 6164
141341 feet/sec YDOT = 1878
830281 meter/sec
ZDOT = 8480
612438 ZDOT = 2584
890671
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 20238
55296518
00016717 00000-0 10270-3 0 9047
2 25544 51
6440 5
1874 0001301 65
6362 294
4924 15
49212021 2766
Satellite: ISS
Catalog Number: 25544
Epoch time: 20238
55296518 = yrday
fracday
Element set: 904
Inclination: 51
6440 deg
RA of node: 5
1874 deg
Eccentricity:
0001301
Arg of perigee: 65
6362 deg
Mean anomaly: 294
4924 deg
Mean motion: 15
49212021 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 276
Checksum: 287
Coasting Arc #6 (Orbit 280)
---------------------------------------
Vector Time (GMT): 2020/238/20:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4102019
18 A = 6796452
32 meter
Y = -3505793
96 meter E =
0009437
Z = -4142234
84 I = 51
66092
XDOT = 6093
602460 Wp = 67
71826
YDOT = -2662
989965 meter/sec RA = 3
13878 deg
ZDOT = -3784
040311 TA = 163
20785
MA = 163
17659
Ha = 229
371 n
mi
Hp = 221
816
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13458068
18 X = -4042390
94
Y = -11501948
68 feet Y = -3551332
19 meter
Z = -13590009
33 Z = -4162016
00
XDOT = 19992
134056 XDOT = 6141
308556
YDOT = -8736
843716 feet/sec YDOT = -2594
580134 meter/sec
ZDOT = -12414
830417 ZDOT = -3754
324269
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8866420
46 X = 2702484
96
Y = -15241959
53 feet Y = -4645749
26 meter
Z = -13681083
07 Z = -4169994
12
XDOT = 11147
864920 XDOT = 3397
869228
YDOT = 17495
036246 feet/sec YDOT = 5332
487048 meter/sec
ZDOT = -12277
526704 ZDOT = -3742
190139
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 20238
87550298
00016717 00000-0 10270-3 0 9051
2 25544 51
6422 3
5956 0001786 58
1496 301
9828 15
49175154 2819
Satellite: ISS
Catalog Number: 25544
Epoch time: 20238
87550298 = yrday
fracday
Element set: 905
Inclination: 51
6422 deg
RA of node: 3
5956 deg
Eccentricity:
0001786
Arg of perigee: 58
1496 deg
Mean anomaly: 301
9828 deg
Mean motion: 15
49175154 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 281
Checksum: 324
Coasting Arc #7 (Orbit 296)
---------------------------------------
Vector Time (GMT): 2020/239/20:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4324854
79 A = 6796277
16 meter
Y = 3166747
95 meter E =
0011372
Z = 4169462
56 I = 51
62574
XDOT = -5910
044419 Wp = 98
08578
YDOT = 3143
589868 meter/sec RA = 358
19193 deg
ZDOT = 3732
423508 TA = 313
46469
MA = 313
55922
Ha = 229
220 n
mi
Hp = 221
906
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14189156
14 X = 4268869
11
Y = 10389593
00 feet Y = 3214798
40 meter
Z = 13679339
10 Z = 4190334
99
XDOT = -19389
909510 XDOT = -5962
887591
YDOT = 10313
615053 feet/sec YDOT = 3077
203940 meter/sec
ZDOT = 12245
483950 ZDOT = 3703
586778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7367141
83 X = -2245504
83
Y = 15885903
19 feet Y = 4842023
29 meter
Z = 13775464
20 Z = 4198761
49
XDOT = -12835
723025 XDOT = -3912
328378
YDOT = -16484
806099 feet/sec YDOT = -5024
568899 meter/sec
ZDOT = 12112
214587 ZDOT = 3691
803006
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 20239
90762149
00016717 00000-0 10270-3 0 9067
2 25544 51
6412 358
4892 0001698 55
9494 304
1817 15
49192508 2976
Satellite: ISS
Catalog Number: 25544
Epoch time: 20239
90762149 = yrday
fracday
Element set: 906
Inclination: 51
6412 deg
RA of node: 358
4892 deg
Eccentricity:
0001698
Arg of perigee: 55
9494 deg
Mean anomaly: 304
1817 deg
Mean motion: 15
49192508 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 297
Checksum: 337
Coasting Arc #8 (Orbit 311)
---------------------------------------
Vector Time (GMT): 2020/240/20:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4512883
10 A = 6796156
77 meter
Y = -2838579
31 meter E =
0009904
Z = -4225203
95 I = 51
59102
XDOT = 5680
050727 Wp = 67
81101
YDOT = -3592
459265 meter/sec RA = 353
24175 deg
ZDOT = -3656
535195 TA = 164
62216
MA = 164
59205
Ha = 229
390 n
mi
Hp = 221
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14806046
92 X = -4460282
45
Y = -9312924
24 feet Y = -2888751
33 meter
Z = -13862217
67 Z = -4246997
87
XDOT = 18635
337031 XDOT = 5737
561693
YDOT = -11786
283677 feet/sec YDOT = -3528
619177 meter/sec
ZDOT = -11996
506546 ZDOT = -3628
804485
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5908400
62 X = 1800880
51
Y = -16378245
72 feet Y = -4992089
29 meter
Z = -13962611
91 Z = -4255804
11
XDOT = 14364
592473 XDOT = 4378
327786
YDOT = 15290
846110 feet/sec YDOT = 4660
649894 meter/sec
ZDOT = -11868
319947 ZDOT = -3617
463920
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 20240
87523319
00016717 00000-0 10270-3 0 9070
2 25544 51
6409 353
7013 0001794 60
9314 299
2015 15
49172534 3128
Satellite: ISS
Catalog Number: 25544
Epoch time: 20240
87523319 = yrday
fracday
Element set: 907
Inclination: 51
6409 deg
RA of node: 353
7013 deg
Eccentricity:
0001794
Arg of perigee: 60
9314 deg
Mean anomaly: 299
2015 deg
Mean motion: 15
49172534 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 312
Checksum: 292
Coasting Arc #9 (Orbit 327)
---------------------------------------
Vector Time (GMT): 2020/241/20:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4679504
96 A = 6795907
80 meter
Y = 2477197
68 meter E =
0011056
Z = 4252178
45 I = 51
55768
XDOT = -5423
119620 Wp = 100
55179
YDOT = 4044
149282 meter/sec RA = 348
29046 deg
ZDOT = 3602
149274 TA = 312
52686
MA = 312
62017
Ha = 229
161 n
mi
Hp = 221
872
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15352706
57 X = 4630802
07
Y = 8127288
96 feet Y = 2529254
80 meter
Z = 13950716
69 Z = 4274791
09
XDOT = -17792
387206 XDOT = -5485
436370
YDOT = 13268
206306 feet/sec YDOT = 3983
155534 meter/sec
ZDOT = 11818
075047 ZDOT = 3575
655052
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4345513
51 X = -1324512
52
Y = 16731914
77 feet Y = 5099887
62 meter
Z = 14054908
79 Z = 4283936
20
XDOT = -15851
105412 XDOT = -4831
416930
YDOT = -13968
369589 feet/sec YDOT = -4257
559051 meter/sec
ZDOT = 11695
575016 ZDOT = 3564
811265
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 20241
90734876
00016717 00000-0 10270-3 0 9088
2 25544 51
6413 348
5951 0001596 61
9657 298
1654 15
49214404 3284
Satellite: ISS
Catalog Number: 25544
Epoch time: 20241
90734876 = yrday
fracday
Element set: 908
Inclination: 51
6413 deg
RA of node: 348
5951 deg
Eccentricity:
0001596
Arg of perigee: 61
9657 deg
Mean anomaly: 298
1654 deg
Mean motion: 15
49214404 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 328
Checksum: 326
Coasting Arc #10 (Orbit 342)
---------------------------------------
Vector Time (GMT): 2020/242/20:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4813245
36 A = 6795804
72 meter
Y = -2132988
82 meter E =
0010414
Z = -4308052
86 I = 51
52505
XDOT = 5125
069601 Wp = 68
10103
YDOT = -4456
454407 meter/sec RA = 343
33518 deg
ZDOT = -3522
676653 TA = 165
88967
MA = 165
86056
Ha = 229
392 n
mi
Hp = 221
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15791487
41 X = -4768110
24
Y = -6997994
83 feet Y = -2186561
54 meter
Z = -14134031
68 Z = -4331323
70
XDOT = 16814
532813 XDOT = 5191
632943
YDOT = -14620
913408 feet/sec YDOT = -4398
769976 meter/sec
ZDOT = -11557
338099 ZDOT = -3497
619932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2854264
88 X = 869979
93
Y = -16945588
96 feet Y = -5165015
51 meter
Z = -14241279
61 Z = -4340742
02
XDOT = 17143
670561 XDOT = 5225
390787
YDOT = 12494
767738 feet/sec YDOT = 3808
405206 meter/sec
ZDOT = -11441
457646 ZDOT = -3487
356290
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 20242
87495683
00016717 00000-0 10270-3 0 9096
2 25544 51
6421 343
8068 0001839 63
9276 296
2063 15
49188199 3430
Satellite: ISS
Catalog Number: 25544
Epoch time: 20242
87495683 = yrday
fracday
Element set: 909
Inclination: 51
6421 deg
RA of node: 343
8068 deg
Eccentricity:
0001839
Arg of perigee: 63
9276 deg
Mean anomaly: 296
2063 deg
Mean motion: 15
49188199 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 343
Checksum: 340
Coasting Arc #11 (Orbit 358)
---------------------------------------
Vector Time (GMT): 2020/243/20:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4921483
91 A = 6795554
51 meter
Y = 1759820
96 meter E =
0010794
Z = 4335241
48 I = 51
49238
XDOT = -4800
637568 Wp = 102
25947
YDOT = 4867
655626 meter/sec RA = 338
37974 deg
ZDOT = 3464
308248 TA = 312
41131
MA = 312
50258
Ha = 229
158 n
mi
Hp = 221
814
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16146600
75 X = 4880381
59
Y = 5773690
80 feet Y = 1814626
72 meter
Z = 14223233
20 Z = 4359047
81
XDOT = -15750
123254 XDOT = -4871
539656
YDOT = 15969
998772 feet/sec YDOT = 4813
575038 meter/sec
ZDOT = 11365
840710 ZDOT = 3440
816868
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1287857
08 X = -392538
84
Y = 17007526
29 feet Y = 5183894
01 meter
Z = 14332971
00 Z = 4368689
56
XDOT = -18371
168392 XDOT = -5599
532126
YDOT = -10904
248316 feet/sec YDOT = -3323
614887 meter/sec
ZDOT = 11257
173173 ZDOT = 3431
186383
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 20243
90706778
00016717 00000-0 10270-3 0 9103
2 25544 51
6419 338
7011 0001655 65
4979 294
6343 15
49229140 3593
Satellite: ISS
Catalog Number: 25544
Epoch time: 20243
90706778 = yrday
fracday
Element set: 910
Inclination: 51
6419 deg
RA of node: 338
7011 deg
Eccentricity:
0001655
Arg of perigee: 65
4979 deg
Mean anomaly: 294
6343 deg
Mean motion: 15
49229140 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 359
Checksum: 320
Coasting Arc #12 (Orbit 373)
---------------------------------------
Vector Time (GMT): 2020/244/20:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5002059
72 A = 6795474
54 meter
Y = -1407722
27 meter E =
0010861
Z = -4390215
52 I = 51
46061
XDOT = 4438
894030 Wp = 68
54926
YDOT = -5233
446820 meter/sec RA = 333
42046 deg
ZDOT = -3382
306836 TA = 167
04809
MA = 167
02017
Ha = 229
382 n
mi
Hp = 221
685
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16410957
10 X = -4964621
65
Y = -4618511
40 feet Y = -1463449
68 meter
Z = -14403594
22 Z = -4414422
12
XDOT = 14563
300623 XDOT = 4513
515086
YDOT = -17170
101116 feet/sec YDOT = -5183
390789 meter/sec
ZDOT = -11096
807206 ZDOT = -3360
563473
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -187292
26 X = -57086
68
Y = -16952514
14 feet Y = -5167126
31 meter
Z = -14515194
54 Z = -4424231
30
XDOT = 19375
989984 XDOT = 5905
801747
YDOT = 9193
120772 feet/sec YDOT = 2802
063211 meter/sec
ZDOT = -10996
201010 ZDOT = -3351
642068
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 20244
87467417
00016717 00000-0 10270-3 0 9115
2 25544 51
6417 333
9131 0001818 66
6939 293
4402 15
49196145 3749
Satellite: ISS
Catalog Number: 25544
Epoch time: 20244
87467417 = yrday
fracday
Element set: 911
Inclination: 51
6417 deg
RA of node: 333
9131 deg
Eccentricity:
0001818
Arg of perigee: 66
6939 deg
Mean anomaly: 293
4402 deg
Mean motion: 15
49196145 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 374
Checksum: 318
Coasting Arc #13 (Orbit 389)
---------------------------------------
Vector Time (GMT): 2020/245/20:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5053479
30 A = 6795220
76 meter
Y = 1031028
18 meter E =
0010453
Z = 4417034
11 I = 51
43132
XDOT = -4052
043689 Wp = 104
67127
YDOT = 5594
001822 meter/sec RA = 328
46064 deg
ZDOT = 3320
940961 TA = 311
62873
MA = 311
71822
Ha = 229
127 n
mi
Hp = 221
802
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16579656
51 X = 5020119
41
Y = 3382638
38 feet Y = 1087353
49 meter
Z = 14491581
71 Z = 4441500
42
XDOT = -13294
106590 XDOT = -4130
427288
YDOT = 18353
024349 feet/sec YDOT = 5548
250857 meter/sec
ZDOT = 10895
475594 ZDOT = 3301
067425
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1708348
74 X = 520704
70
Y = 16736976
66 feet Y = 5101430
49 meter
Z = 14604394
88 Z = 4451419
56
XDOT = -20294
590483 XDOT = -6185
791179
YDOT = -7381
600144 feet/sec YDOT = -2249
911724 meter/sec
ZDOT = 10803
494927 ZDOT = 3292
905254
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 20245
90678261
00016717 00000-0 10270-3 0 9122
2 25544 51
6425 328
8074 0001587 71
3532 288
7791 15
49237825 3909
Satellite: ISS
Catalog Number: 25544
Epoch time: 20245
90678261 = yrday
fracday
Element set: 912
Inclination: 51
6425 deg
RA of node: 328
8074 deg
Eccentricity:
0001587
Arg of perigee: 71
3532 deg
Mean anomaly: 288
7791 deg
Mean motion: 15
49237825 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 390
Checksum: 325
Coasting Arc #14 (Orbit 390)
---------------------------------------
Vector Time (GMT): 2020/245/23:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -432772
44 A = 6792854
36 meter
Y = -4508241
92 meter E =
0014533
Z = -5075840
45 I = 51
42129
XDOT = 6940
913803 Wp = 99
10498
YDOT = -2673
633651 meter/sec RA = 327
89710 deg
ZDOT = 1785
008683 TA = 188
25094
MA = 188
27486
Ha = 229
364 n
mi
Hp = 221
797
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1419857
09 X = -357672
66
Y = -14790819
95 feet Y = -4512661
84 meter
Z = -16653019
84 Z = -5077760
02
XDOT = 22772
026914 XDOT = 6961
624918
YDOT = -8771
763946 feet/sec YDOT = -2595
899489 meter/sec
ZDOT = 5856
327701 ZDOT = 1818
774769
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7265874
76 X = 2214638
63
Y = -12950073
77 feet Y = -3947182
48 meter
Z = -16661634
73 Z = -5078466
27
XDOT = 22773
046319 XDOT = 6941
224518
YDOT = 5050
886555 feet/sec YDOT = 1539
510222 meter/sec
ZDOT = 6012
239178 ZDOT = 1832
530502
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 20245
97129131
00016717 00000-0 10270-3 0 9137
2 25544 51
6440 328
4884 0001758 66
7134 293
4201 15
49200699 3916
Satellite: ISS
Catalog Number: 25544
Epoch time: 20245
97129131 = yrday
fracday
Element set: 913
Inclination: 51
6440 deg
RA of node: 328
4884 deg
Eccentricity:
0001758
Arg of perigee: 66
7134 deg
Mean anomaly: 293
4201 deg
Mean motion: 15
49200699 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 391
Checksum: 307
Coasting Arc #15 (Orbit 406)
---------------------------------------
Vector Time (GMT): 2020/246/23:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 724783
07 A = 6792883
27 meter
Y = 4493731
88 meter E =
0007458
Z = 5037869
28 I = 51
39356
XDOT = -6710
421651 Wp = 58
21616
YDOT = 3191
763337 meter/sec RA = 322
93445 deg
ZDOT = -1875
710351 TA = 50
06845
MA = 50
00294
Ha = 229
306 n
mi
Hp = 221
784
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2377897
22 X = 650008
20
Y = 14743214
84 feet Y = 4501419
16 meter
Z = 16528442
51 Z = 5041208
04
XDOT = -22015
819065 XDOT = -6736
503177
YDOT = 10471
664493 feet/sec YDOT = 3116
576643 meter/sec
ZDOT = -6153
905350 ZDOT = -1908
370046
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6214943
28 X = -1894314
71
Y = 13560587
06 feet Y = 4133266
94 meter
Z = 16543613
55 Z = 5042493
41
XDOT = -23122
343375 XDOT = -7047
690261
YDOT = -2881
955457 feet/sec YDOT = -878
420023 meter/sec
ZDOT = -6304
721196 ZDOT = -1921
679021
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 20247
00339791
00016717 00000-0 10270-3 0 9149
2 25544 51
6439 323
3825 0001776 67
1807 292
9530 15
49225908 4072
Satellite: ISS
Catalog Number: 25544
Epoch time: 20247
00339791 = yrday
fracday
Element set: 914
Inclination: 51
6439 deg
RA of node: 323
3825 deg
Eccentricity:
0001776
Arg of perigee: 67
1807 deg
Mean anomaly: 292
9530 deg
Mean motion: 15
49225908 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 407
Checksum: 315
Coasting Arc #16 (Orbit 421)
---------------------------------------
Vector Time (GMT): 2020/247/23:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1039110
99 A = 6793043
43 meter
Y = -4468136
91 meter E =
0014336
Z = -5023178
06 I = 51
36784
XDOT = 6414
345530 Wp = 100
34255
YDOT = -3682
577182 meter/sec RA = 317
96886 deg
ZDOT = 1951
024788 TA = 188
70205
MA = 188
72694
Ha = 229
397 n
mi
Hp = 221
722
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3409156
81 X = -964670
22
Y = -14659241
83 feet Y = -4479341
13 meter
Z = -16480242
98 Z = -5028044
48
XDOT = 21044
440716 XDOT = 6445
571618
YDOT = -12081
946136 feet/sec YDOT = -3610
672637 meter/sec
ZDOT = 6400
999959 ZDOT = 1982
258972
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5064535
04 X = 1543670
28
Y = -14146841
16 feet Y = -4311957
19 meter
Z = -16502469
51 Z = -5029952
71
XDOT = 23173
666531 XDOT = 7063
333559
YDOT = 669
604659 feet/sec YDOT = 204
095500 meter/sec
ZDOT = 6545
245741 ZDOT = 1994
990902
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 20247
97099783
00016717 00000-0 10270-3 0 9150
2 25544 51
6441 318
5947 0001840 71
2003 288
9346 15
49206377 4228
Satellite: ISS
Catalog Number: 25544
Epoch time: 20247
97099783 = yrday
fracday
Element set: 915
Inclination: 51
6441 deg
RA of node: 318
5947 deg
Eccentricity:
0001840
Arg of perigee: 71
2003 deg
Mean anomaly: 288
9346 deg
Mean motion: 15
49206377 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 422
Checksum: 322
Coasting Arc #17 (Orbit 437)
---------------------------------------
Vector Time (GMT): 2020/248/23:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1331811
64 A = 6793051
91 meter
Y = 4415767
76 meter E =
0007772
Z = 4982636
35 I = 51
34328
XDOT = -6108
092559 Wp = 60
02480
YDOT = 4153
990603 meter/sec RA = 313
00240 deg
ZDOT = -2042
549125 TA = 49
96468
MA = 49
89652
Ha = 229
254 n
mi
Hp = 221
759
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4369460
75 X = 1258131
53
Y = 14487427
03 feet Y = 4430249
43 meter
Z = 16347232
12 Z = 4988926
46
XDOT = -20039
673750 XDOT = -6144
168280
YDOT = 13628
578095 feet/sec YDOT = 4085
483673 meter/sec
ZDOT = -6701
276657 ZDOT = -2072
307621
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3910398
86 X = -1191889
57
Y = 14585746
93 feet Y = 4445735
66 meter
Z = 16376034
15 Z = 4991415
21
XDOT = -23101
898511 XDOT = -7041
458666
YDOT = 1507
404238 feet/sec YDOT = 459
456812 meter/sec
ZDOT = -6838
720253 ZDOT = -2084
441933
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 20249
00310255
00016717 00000-0 10270-3 0 9167
2 25544 51
6433 313
4887 0001714 72
8123 287
3215 15
49242260 4382
Satellite: ISS
Catalog Number: 25544
Epoch time: 20249
00310255 = yrday
fracday
Element set: 916
Inclination: 51
6433 deg
RA of node: 313
4887 deg
Eccentricity:
0001714
Arg of perigee: 72
8123 deg
Mean anomaly: 287
3215 deg
Mean motion: 15
49242260 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 438
Checksum: 283
Coasting Arc #18 (Orbit 444)
---------------------------------------
Vector Time (GMT): 2020/249/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4041651
80 A = 6792089
44 meter
Y = 1667994
04 meter E =
0005277
Z = 5193829
14 I = 51
32852
XDOT = -4150
233943 Wp = 114
33027
YDOT = 6331
533266 meter/sec RA = 310
49039 deg
ZDOT = 1193
101854 TA = 324
15037
MA = 324
18577
Ha = 229
121 n
mi
Hp = 221
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13260012
47 X = 3997470
83
Y = 5472421
39 feet Y = 1712944
03 meter
Z = 17040121
85 Z = 5213354
42
XDOT = -13616
253095 XDOT = -4226
521988
YDOT = 20772
746937 feet/sec YDOT = 6284
695909 meter/sec
ZDOT = 3914
376163 ZDOT = 1172
755958
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9201053
04 X = -2804480
97
Y = -10864695
78 feet Y = -3311559
27 meter
Z = 17130093
05 Z = 5221252
36
XDOT = 20822
329077 XDOT = 6346
645903
YDOT = -11594
718765 feet/sec YDOT = -3534
070280 meter/sec
ZDOT = 3820
250574 ZDOT = 1164
412375
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 20249
51915349
00016717 00000-0 10270-3 0 9179
2 25544 51
6434 310
9326 0001508 90
5419 269
5904 15
49231831 4456
Satellite: ISS
Catalog Number: 25544
Epoch time: 20249
51915349 = yrday
fracday
Element set: 917
Inclination: 51
6434 deg
RA of node: 310
9326 deg
Eccentricity:
0001508
Arg of perigee: 90
5419 deg
Mean anomaly: 269
5904 deg
Mean motion: 15
49231831 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 445
Checksum: 309
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