[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 1st 2020
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ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19920 769 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 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
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
253/10:08:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
3
000/00:00:00
000 0
0 0
0 221
7
254/20:33:53
536 0
4 1
4 1
4
N/A -1
4 0
1 229
3
000/00:03:43
072 -0
1 -0
0 222
4
Coasting Arc #1 (Orbit 368)
---------------------------------------
Vector Time (GMT): 2020/244/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3893493
39 A = 6793156
19 meter
Y = 2540174
58 meter E =
0007390
Z = 4948477
26 I = 51
46741
XDOT = -5753
761167 Wp = 114
26626
YDOT = 4571
943721 meter/sec RA = 335
15942 deg
ZDOT = 2174
659024 TA = 314
43548
MA = 314
49592
Ha = 229
135 n
mi
Hp = 221
837
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12773928
43 X = 3840762
63
Y = 8333906
11 feet Y = 2583419
67 meter
Z = 16235161
62 Z = 4967261
83
XDOT = -18877
169183 XDOT = -5815
021424
YDOT = 14999
815359 feet/sec YDOT = 4507
258560 meter/sec
ZDOT = 7134
708085 ZDOT = 2146
561189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8882292
00 X = -2707322
60
Y = -12284755
83 feet Y = -3744393
58 meter
Z = 16321684
18 Z = 4974849
34
XDOT = 22120
134746 XDOT = 6742
217071
YDOT = -6662
866998 feet/sec YDOT = -2030
841861 meter/sec
ZDOT = 7004
815439 ZDOT = 2135
067746
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
55212941
00016717 00000-0 10270-3 0 9008
2 25544 51
6452 335
5071 0001496 79
4117 280
7201 15
49230409 3693
Satellite: ISS
Catalog Number: 25544
Epoch time: 20244
55212941 = yrday
fracday
Element set: 900
Inclination: 51
6452 deg
RA of node: 335
5071 deg
Eccentricity:
0001496
Arg of perigee: 79
4117 deg
Mean anomaly: 280
7201 deg
Mean motion: 15
49230409 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 369
Checksum: 285
Coasting Arc #2 (Orbit 383)
---------------------------------------
Vector Time (GMT): 2020/245/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4032137
31 A = 6793173
83 meter
Y = -2271496
77 meter E =
0014071
Z = -4985852
87 I = 51
43616
XDOT = 5395
666975 Wp = 75
14793
YDOT = -5005
376459 meter/sec RA = 330
19972 deg
ZDOT = -2084
587950 TA = 174
46260
MA = 174
44702
Ha = 229
297 n
mi
Hp = 221
793
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13228796
96 X = -3982219
11
Y = -7452417
23 feet Y = -2316308
11 meter
Z = -16357785
00 Z = -5005317
71
XDOT = 17702
319472 XDOT = 5461
363131
YDOT = -16421
838776 feet/sec YDOT = -4944
671003 meter/sec
ZDOT = -6839
199310 ZDOT = -2058
218635
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9817977
90 X = 2992519
66
Y = 11454479
67 feet Y = 3491325
40 meter
Z = -16447459
60 Z = -5013185
69
XDOT = -21425
729283 XDOT = -6530
562286
YDOT = 8725
962280 feet/sec YDOT = 2659
673303 meter/sec
ZDOT = -6717
276578 ZDOT = -2047
425901
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
51973125
00016717 00000-0 10270-3 0 9014
2 25544 51
6445 330
7204 0001423 82
0955 278
0356 15
49186074 3846
Satellite: ISS
Catalog Number: 25544
Epoch time: 20245
51973125 = yrday
fracday
Element set: 901
Inclination: 51
6445 deg
RA of node: 330
7204 deg
Eccentricity:
0001423
Arg of perigee: 82
0955 deg
Mean anomaly: 278
0356 deg
Mean motion: 15
49186074 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 384
Checksum: 294
Coasting Arc #3 (Orbit 399)
---------------------------------------
Vector Time (GMT): 2020/246/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4146305
51 A = 6792913
48 meter
Y = 1978637
95 meter E =
0006993
Z = 4999107
83 I = 51
40775
XDOT = -5018
871177 Wp = 115
27784
YDOT = 5433
185482 meter/sec RA = 325
23728 deg
ZDOT = 2007
118609 TA = 315
11739
MA = 315
17391
Ha = 229
103 n
mi
Hp = 221
832
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13603364
52 X = 4099589
20
Y = 6491594
32 feet Y = 2024744
00 meter
Z = 16401272
42 Z = 5019135
06
XDOT = -16466
112787 XDOT = -5089
002960
YDOT = 17825
411686 feet/sec YDOT = 5376
668856 meter/sec
ZDOT = 6585
034805 ZDOT = 1982
568629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10677592
24 X = -3254530
11
Y = -10495034
60 feet Y = -3198886
55 meter
Z = 16493554
28 Z = 5027235
35
XDOT = 20610
655302 XDOT = 6282
127736
YDOT = -10772
508014 feet/sec YDOT = -3283
460443 meter/sec
ZDOT = 6471
502956 ZDOT = 1972
514101
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 20246
55183382
00016717 00000-0 10270-3 0 9028
2 25544 51
6452 325
6137 0001467 82
0639 278
0678 15
49237634 4004
Satellite: ISS
Catalog Number: 25544
Epoch time: 20246
55183382 = yrday
fracday
Element set: 902
Inclination: 51
6452 deg
RA of node: 325
6137 deg
Eccentricity:
0001467
Arg of perigee: 82
0639 deg
Mean anomaly: 278
0678 deg
Mean motion: 15
49237634 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 400
Checksum: 306
Coasting Arc #4 (Orbit 414)
---------------------------------------
Vector Time (GMT): 2020/247/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4245112
76 A = 6792940
50 meter
Y = -1702881
11 meter E =
0014521
Z = -5035560
53 I = 51
37903
XDOT = 4596
810309 Wp = 76
23950
YDOT = -5806
860229 meter/sec RA = 320
27326 deg
ZDOT = -1912
805596 TA = 175
10042
MA = 175
08620
Ha = 229
329 n
mi
Hp = 221
730
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13927535
30 X = -4201295
54
Y = -5586880
29 feet Y = -1750108
36 meter
Z = -16520867
89 Z = -5056074
84
XDOT = 15081
398653 XDOT = 4670
693929
YDOT = -19051
378704 feet/sec YDOT = -5755
042428 meter/sec
ZDOT = -6275
608911 ZDOT = -1890
296501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11441262
28 X = 3487296
74
Y = 9547477
29 feet Y = 2910071
08 meter
Z = -16615406
76 Z = -5064375
98
XDOT = -19532
855727 XDOT = -5953
614426
YDOT = 12674
366199 feet/sec YDOT = 3863
146817 meter/sec
ZDOT = -6171
493076 ZDOT = -1881
071090
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
51942983
00016717 00000-0 10270-3 0 9036
2 25544 51
6439 320
8268 0001533 82
3887 277
7437 15
49192059 4159
Satellite: ISS
Catalog Number: 25544
Epoch time: 20247
51942983 = yrday
fracday
Element set: 903
Inclination: 51
6439 deg
RA of node: 320
8268 deg
Eccentricity:
0001533
Arg of perigee: 82
3887 deg
Mean anomaly: 277
7437 deg
Mean motion: 15
49192059 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 415
Checksum: 329
Coasting Arc #5 (Orbit 430)
---------------------------------------
Vector Time (GMT): 2020/248/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4317458
65 A = 6792710
72 meter
Y = 1406259
83 meter E =
0006713
Z = 5047568
83 I = 51
35314
XDOT = -4157
124430 Wp = 115
65080
YDOT = 6172
715682 meter/sec RA = 315
30721 deg
ZDOT = 1831
325221 TA = 316
50743
MA = 316
56036
Ha = 229
139 n
mi
Hp = 221
795
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14164890
58 X = 4276894
52
Y = 4613713
36 feet Y = 1454314
31 meter
Z = 16560265
18 Z = 5068442
57
XDOT = -13638
859680 XDOT = -4234
736094
YDOT = 20251
691869 feet/sec YDOT = 6125
793919 meter/sec
ZDOT = 6008
284846 ZDOT = 1810
942725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12112580
05 X = -3691914
40
Y = -8486472
21 feet Y = -2586676
73 meter
Z = 16656471
80 Z = 5076892
61
XDOT = 18340
089793 XDOT = 5590
059369
YDOT = -14538
562200 feet/sec YDOT = -4431
353759 meter/sec
ZDOT = 5913
979835 ZDOT = 1802
581054
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 20248
55152854
00016717 00000-0 10270-3 0 9042
2 25544 51
6435 315
7203 0001575 85
6192 274
5138 15
49234332 4310
Satellite: ISS
Catalog Number: 25544
Epoch time: 20248
55152854 = yrday
fracday
Element set: 904
Inclination: 51
6435 deg
RA of node: 315
7203 deg
Eccentricity:
0001575
Arg of perigee: 85
6192 deg
Mean anomaly: 274
5138 deg
Mean motion: 15
49234332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 431
Checksum: 296
Coasting Arc #6 (Orbit 445)
---------------------------------------
Vector Time (GMT): 2020/249/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4029655
67 A = 6792040
75 meter
Y = 1686167
55 meter E =
0005246
Z = 5197217
66 I = 51
32863
XDOT = -4164
963068 Wp = 114
05192
YDOT = 6325
452762 meter/sec RA = 310
48962 deg
ZDOT = 1174
050245 TA = 324
61518
MA = 324
64998
Ha = 229
107 n
mi
Hp = 221
802
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13220655
07 X = 3985255
90
Y = 5532045
78 feet Y = 1730982
17 meter
Z = 17051239
03 Z = 5216684
13
XDOT = -13664
576994 XDOT = -4241
089482
YDOT = 20752
797777 feet/sec YDOT = 6278
451596 meter/sec
ZDOT = 3851
870884 ZDOT = 1153
633194
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9138768
78 X = -2785496
72
Y = -10899777
38 feet Y = -3322252
14 meter
Z = 17140938
18 Z = 5224557
96
XDOT = 20853
297451 XDOT = 6356
085063
YDOT = -11559
662091 feet/sec YDOT = -3523
385005 meter/sec
ZDOT = 3757
417419 ZDOT = 1145
260829
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
51911981
00016717 00000-0 10270-3 0 9054
2 25544 51
6436 310
9325 0001519 90
3533 269
7791 15
49243410 4467
Satellite: ISS
Catalog Number: 25544
Epoch time: 20249
51911981 = yrday
fracday
Element set: 905
Inclination: 51
6436 deg
RA of node: 310
9325 deg
Eccentricity:
0001519
Arg of perigee: 90
3533 deg
Mean anomaly: 269
7791 deg
Mean motion: 15
49243410 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 446
Checksum: 305
Coasting Arc #7 (Orbit 460)
---------------------------------------
Vector Time (GMT): 2020/250/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4116462
65 A = 6792111
62 meter
Y = -1433495
55 meter E =
0015797
Z = -5222863
02 I = 51
30674
XDOT = 3670
001868 Wp = 82
40753
YDOT = -6623
877127 meter/sec RA = 305
51955 deg
ZDOT = -1075
295327 TA = 177
21989
MA = 177
21110
Ha = 229
328 n
mi
Hp = 221
696
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13505454
90 X = -4074757
23
Y = -4703069
38 feet Y = -1479295
93 meter
Z = -17135377
35 Z = -5242757
81
XDOT = 12040
688543 XDOT = 3749
022465
YDOT = -21731
880339 feet/sec YDOT = -6582
394774 meter/sec
ZDOT = -3527
871807 ZDOT = -1057
275527
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9945332
96 X = 3031337
48
Y = 10122058
75 feet Y = 3085203
51 meter
Z = -17227060
39 Z = -5250808
01
XDOT = -19668
252598 XDOT = -5994
883392
YDOT = 13466
833782 feet/sec YDOT = 4104
690937 meter/sec
ZDOT = -3444
477249 ZDOT = -1049
876666
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 20250
48670955
00016717 00000-0 10270-3 0 9066
2 25544 51
6430 306
1447 0001550 89
9248 270
2079 15
49200083 4617
Satellite: ISS
Catalog Number: 25544
Epoch time: 20250
48670955 = yrday
fracday
Element set: 906
Inclination: 51
6430 deg
RA of node: 306
1447 deg
Eccentricity:
0001550
Arg of perigee: 89
9248 deg
Mean anomaly: 270
2079 deg
Mean motion: 15
49200083 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 461
Checksum: 297
Coasting Arc #8 (Orbit 476)
---------------------------------------
Vector Time (GMT): 2020/251/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4174807
62 A = 6791908
08 meter
Y = 1165879
17 meter E =
0004998
Z = 5225154
18 I = 51
28807
XDOT = -3163
740278 Wp = 111
61293
YDOT = 6911
004320 meter/sec RA = 300
54828 deg
ZDOT = 983
164822 TA = 328
90982
MA = 328
93939
Ha = 229
136 n
mi
Hp = 221
761
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13696875
38 X = 4136079
22
Y = 3825062
88 feet Y = 1212348
58 meter
Z = 17142894
29 Z = 5245339
71
XDOT = -10379
725321 XDOT = -3245
561739
YDOT = 22673
898687 feet/sec YDOT = 6875
167668 meter/sec
ZDOT = 3225
606371 ZDOT = 967
597467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10664463
75 X = -3250528
55
Y = -9236142
93 feet Y = -2815176
37 meter
Z = 17235927
67 Z = 5253510
75
XDOT = 18380
993326 XDOT = 5602
526766
YDOT = -15322
959222 feet/sec YDOT = -4670
437971 meter/sec
ZDOT = 3153
523823 ZDOT = 961
194061
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 20251
51880076
00016717 00000-0 10270-3 0 9079
2 25544 51
6432 301
0378 0001627 90
6334 269
5002 15
49244768 4778
Satellite: ISS
Catalog Number: 25544
Epoch time: 20251
51880076 = yrday
fracday
Element set: 907
Inclination: 51
6432 deg
RA of node: 301
0378 deg
Eccentricity:
0001627
Arg of perigee: 90
6334 deg
Mean anomaly: 269
5002 deg
Mean motion: 15
49244768 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 477
Checksum: 301
Coasting Arc #9 (Orbit 491)
---------------------------------------
Vector Time (GMT): 2020/252/11:15:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4231163
12 A = 6791983
85 meter
Y = -909989
41 meter E =
0016133
Z = -5248715
64 I = 51
27073
XDOT = 2627
056991 Wp = 84
22459
YDOT = -7128
652077 meter/sec RA = 295
57585 deg
ZDOT = -882
598487 TA = 177
27323
MA = 177
26443
Ha = 229
382 n
mi
Hp = 221
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13881768
77 X = -4195177
49
Y = -2985529
57 feet Y = -957104
29 meter
Z = -17220195
68 Z = -5269181
64
XDOT = 8618
953381 XDOT = 2710
863652
YDOT = -23387
966131 feet/sec YDOT = -7098
805883 meter/sec
ZDOT = -2895
664328 ZDOT = -869
633402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11333750
28 X = 3454527
09
Y = 8360927
27 feet Y = 2548410
63 meter
Z = -17314532
34 Z = -5277469
46
XDOT = -16849
083160 XDOT = -5135
600547
YDOT = 16972
938091 feet/sec YDOT = 5173
351530 meter/sec
ZDOT = -2835
586432 ZDOT = -864
286745
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 20252
48638776
00016717 00000-0 10270-3 0 9085
2 25544 51
6421 296
2503 0001714 93
9497 266
1849 15
49203723 4929
Satellite: ISS
Catalog Number: 25544
Epoch time: 20252
48638776 = yrday
fracday
Element set: 908
Inclination: 51
6421 deg
RA of node: 296
2503 deg
Eccentricity:
0001714
Arg of perigee: 93
9497 deg
Mean anomaly: 266
1849 deg
Mean motion: 15
49203723 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 492
Checksum: 328
Coasting Arc #10 (Orbit 506)
---------------------------------------
Vector Time (GMT): 2020/253/10:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2613954
13 A = 6803565
18 meter
Y = 6269742
60 meter E =
0012877
Z = -266683
61 I = 51
29713
XDOT = -4337
224178 Wp = 131
79822
YDOT = -2053
915109 meter/sec RA = 290
82942 deg
ZDOT = -5970
923164 TA = 51
08316
MA = 50
96842
Ha = 229
317 n
mi
Hp = 221
748
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8575964
99 X = -2682574
60
Y = 20570021
65 feet Y = 6240127
81 meter
Z = -874946
21 Z = -279548
02
XDOT = -14229
738117 XDOT = -4284
930870
YDOT = -6738
566629 feet/sec YDOT = -2102
124786 meter/sec
ZDOT = -19589
642927 ZDOT = -5991
864743
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19784222
55 X = 6030231
03
Y = -10254253
76 feet Y = -3125496
55 meter
Z = -934513
30 Z = -284839
65
XDOT = 5721
771799 XDOT = 1743
996044
YDOT = 12778
755048 feet/sec YDOT = 3894
964539 meter/sec
ZDOT = -19686
128325 ZDOT = -6000
331914
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 20253
45397139
00016717 00000-0 10270-3 0 9099
2 25544 51
6425 291
4623 0001720 98
1838 261
9507 15
49231921 5078
Satellite: ISS
Catalog Number: 25544
Epoch time: 20253
45397139 = yrday
fracday
Element set: 909
Inclination: 51
6425 deg
RA of node: 291
4623 deg
Eccentricity:
0001720
Arg of perigee: 98
1838 deg
Mean anomaly: 261
9507 deg
Mean motion: 15
49231921 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 507
Checksum: 311
Coasting Arc #11 (Orbit 522)
---------------------------------------
Vector Time (GMT): 2020/254/10:08:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2111352
60 A = 6803654
32 meter
Y = -6452660
87 meter E =
0013992
Z = 334372
60 I = 51
28660
XDOT = 4465
433156 Wp = 53
65247
YDOT = 1778
894297 meter/sec RA = 285
85606 deg
ZDOT = 5965
502907 TA = 309
96193
MA = 310
08474
Ha = 229
394 n
mi
Hp = 221
783
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6927009
85 X = 2181727
08
Y = -21170147
20 feet Y = -6428656
72 meter
Z = 1097022
96 Z = 344799
72
XDOT = 14650
371246 XDOT = 4416
232071
YDOT = 5836
267377 feet/sec YDOT = 1828
554906 meter/sec
ZDOT = 19571
859930 ZDOT = 5987
074776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18699920
43 X = -5699735
75
Y = 12098066
63 feet Y = 3687490
71 meter
Z = 1145345
84 Z = 349101
41
XDOT = -6725
793024 XDOT = -2050
021714
YDOT = -12307
982500 feet/sec YDOT = -3751
473066 meter/sec
ZDOT = 19671
267243 ZDOT = 5995
802256
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 20254
48605920
00016717 00000-0 10270-3 0 9105
2 25544 51
6429 286
3551 0001728 92
5875 267
5473 15
49196489 5233
Satellite: ISS
Catalog Number: 25544
Epoch time: 20254
48605920 = yrday
fracday
Element set: 910
Inclination: 51
6429 deg
RA of node: 286
3551 deg
Eccentricity:
0001728
Arg of perigee: 92
5875 deg
Mean anomaly: 267
5473 deg
Mean motion: 15
49196489 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 523
Checksum: 332
Coasting Arc #12 (Orbit 528)
---------------------------------------
Vector Time (GMT): 2020/254/20:35:45
072
Vector Time (MET): N/A
Weight (LBS) : 922309
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3922518
31 A = 6792560
63 meter
Y = -1769108
35 meter E =
0015175
Z = -5269066
79 I = 51
24491
XDOT = 2338
001892 Wp = 95
04292
YDOT = -7249
573035 meter/sec RA = 283
68055 deg
ZDOT = 693
990567 TA = 181
63600
MA = 181
64097
Ha = 229
334 n
mi
Hp = 222
391
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12869154
57 X = -3876849
94
Y = -5804161
24 feet Y = -1812717
42 meter
Z = -17286964
54 Z = -5288009
95
XDOT = 7670
609882 XDOT = 2415
524018
YDOT = -23784
688435 feet/sec YDOT = -7222
994368 meter/sec
ZDOT = 2276
871938 ZDOT = 705
535982
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -950481
22 X = -289706
67
Y = -13977642
05 feet Y = -4260385
30 meter
Z = -17374253
31 Z = -5295672
41
XDOT = 23546
167129 XDOT = 7176
871741
YDOT = -4496
066693 feet/sec YDOT = -1370
401128 meter/sec
ZDOT = 2330
374868 ZDOT = 710
298260
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 20254
87309090
00016717 00000-0 10270-3 0 9118
2 25544 51
6442 284
4423 0000611 87
3245 272
7975 15
48978810 5294
Satellite: ISS
Catalog Number: 25544
Epoch time: 20254
87309090 = yrday
fracday
Element set: 911
Inclination: 51
6442 deg
RA of node: 284
4423 deg
Eccentricity:
0000611
Arg of perigee: 87
3245 deg
Mean anomaly: 272
7975 deg
Mean motion: 15
48978810 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 529
Checksum: 316
Coasting Arc #13 (Orbit 544)
---------------------------------------
Vector Time (GMT): 2020/255/20:35:45
072
Vector Time (MET): N/A
Weight (LBS) : 922309
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4053521
20 A = 6792466
36 meter
Y = 1423447
44 meter E =
0003540
Z = 5258526
79 I = 51
23744
XDOT = -1705
476347 Wp = 66
61876
YDOT = 7438
027080 meter/sec RA = 278
70838 deg
ZDOT = -697
006043 TA = 30
09036
MA = 30
07003
Ha = 229
102 n
mi
Hp = 222
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13298954
06 X = 4011759
66
Y = 4670103
15 feet Y = 1468543
31 meter
Z = 17252384
48 Z = 5278115
73
XDOT = -5595
394840 XDOT = -1785
138198
YDOT = 24402
975985 feet/sec YDOT = 7418
509805 meter/sec
ZDOT = -2286
765233 ZDOT = -705
484034
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2390027
50 X = 728480
38
Y = 13778111
86 feet Y = 4199568
49 meter
Z = 17342670
35 Z = 5286045
92
XDOT = -23000
167455 XDOT = -7010
451040
YDOT = 6924
853940 feet/sec YDOT = 2110
695481 meter/sec
ZDOT = -2326
113317 ZDOT = -708
999339
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 20255
90535463
00016717 00000-0 10270-3 0 9129
2 25544 51
6435 279
3369 0000511 89
2158 270
9051 15
49006501 5454
Satellite: ISS
Catalog Number: 25544
Epoch time: 20255
90535463 = yrday
fracday
Element set: 912
Inclination: 51
6435 deg
RA of node: 279
3369 deg
Eccentricity:
0000511
Arg of perigee: 89
2158 deg
Mean anomaly: 270
9051 deg
Mean motion: 15
49006501 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 545
Checksum: 297
Coasting Arc #14 (Orbit 559)
---------------------------------------
Vector Time (GMT): 2020/256/20:35:45
072
Vector Time (MET): N/A
Weight (LBS) : 922309
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4169820
07 A = 6792536
27 meter
Y = -1067254
44 meter E =
0015077
Z = -5267950
71 I = 51
23334
XDOT = 1052
462301 Wp = 95
25047
YDOT = -7544
126792 meter/sec RA = 273
73574 deg
ZDOT = 695
698892 TA = 181
44629
MA = 181
45066
Ha = 229
283 n
mi
Hp = 222
410
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13680512
05 X = -4131987
27
Y = -3501490
94 feet Y = -1113672
84 meter
Z = -17283302
86 Z = -5288114
05
XDOT = 3452
960304 XDOT = 1133
365486
YDOT = -24751
072152 feet/sec YDOT = -7531
905043 meter/sec
ZDOT = 2282
476681 ZDOT = 701
007845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3827862
58 X = -1166732
51
Y = -13473773
53 feet Y = -4106806
17 meter
Z = -17376256
83 Z = -5296283
08
XDOT = 22114
961640 XDOT = 6740
640308
YDOT = -9256
656284 feet/sec YDOT = -2821
428835 meter/sec
ZDOT = 2307
194381 ZDOT = 703
232847
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 20256
87310286
00016717 00000-0 10270-3 0 9131
2 25544 51
6433 274
5506 0000504 90
8916 269
2292 15
48986081 5608
Satellite: ISS
Catalog Number: 25544
Epoch time: 20256
87310286 = yrday
fracday
Element set: 913
Inclination: 51
6433 deg
RA of node: 274
5506 deg
Eccentricity:
0000504
Arg of perigee: 90
8916 deg
Mean anomaly: 269
2292 deg
Mean motion: 15
48986081 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 560
Checksum: 313
Coasting Arc #15 (Orbit 575)
---------------------------------------
Vector Time (GMT): 2020/257/20:35:45
072
Vector Time (MET): N/A
Weight (LBS) : 922309
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4238709
10 A = 6792457
02 meter
Y = 706335
75 meter E =
0003385
Z = 5257836
76 I = 51
23272
XDOT = -398
380382 Wp = 66
78568
YDOT = 7620
194112 meter/sec RA = 268
76259 deg
ZDOT = -700
859200 TA = 29
96069
MA = 29
94133
Ha = 229
041 n
mi
Hp = 222
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13906525
93 X = 4204956
29
Y = 2317374
50 feet Y = 753547
41 meter
Z = 17250120
60 Z = 5278344
57
XDOT = -1307
022251 XDOT = -480
157733
YDOT = 25000
636852 feet/sec YDOT = 7615
281877 meter/sec
ZDOT = -2299
406825 ZDOT = -702
993132
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5188190
81 X = 1581360
56
Y = 12983568
61 feet Y = 3957391
71 meter
Z = 17344681
35 Z = 5286658
87
XDOT = -21080
750688 XDOT = -6425
412810
YDOT = 11516
285265 feet/sec YDOT = 3510
163749 meter/sec
ZDOT = -2309
461187 ZDOT = -703
923770
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 20257
90536292
00016717 00000-0 10270-3 0 9144
2 25544 51
6437 269
4449 0000378 97
3959 262
7234 15
49008888 5761
Satellite: ISS
Catalog Number: 25544
Epoch time: 20257
90536292 = yrday
fracday
Element set: 914
Inclination: 51
6437 deg
RA of node: 269
4449 deg
Eccentricity:
0000378
Arg of perigee: 97
3959 deg
Mean anomaly: 262
7234 deg
Mean motion: 15
49008888 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 576
Checksum: 349
Coasting Arc #16 (Orbit 590)
---------------------------------------
Vector Time (GMT): 2020/258/20:35:45
072
Vector Time (MET): N/A
Weight (LBS) : 922309
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4291655
90 A = 6792506
83 meter
Y = -339151
10 meter E =
0015015
Z = -5267201
89 I = 51
23417
XDOT = -260
632491 Wp = 95
09569
YDOT = -7612
126798 meter/sec RA = 263
78879 deg
ZDOT = 702
932480 TA = 181
67059
MA = 181
67561
Ha = 229
247 n
mi
Hp = 222
411
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14080235
89 X = -4261959
67
Y = -1112700
46 feet Y = -386977
65 meter
Z = -17280846
10 Z = -5287976
71
XDOT = -855
093473 XDOT = -178
906436
YDOT = -24974
169286 feet/sec YDOT = -7614
584388 meter/sec
ZDOT = 2306
208923 ZDOT = 701
865265
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6521636
86 X = -1987794
91
Y = -12395116
92 feet Y = -3778031
64 meter
Z = -17376654
35 Z = -5296404
25
XDOT = 19737
754943 XDOT = 6016
067707
YDOT = -13609
377487 feet/sec YDOT = -4148
138258 meter/sec
ZDOT = 2301
473481 ZDOT = 701
489117
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 20258
87310559
00016717 00000-0 10270-3 0 9158
2 25544 51
6432 264
6577 0000450 82
6378 277
4823 15
48995854 5919
Satellite: ISS
Catalog Number: 25544
Epoch time: 20258
87310559 = yrday
fracday
Element set: 915
Inclination: 51
6432 deg
RA of node: 264
6577 deg
Eccentricity:
0000450
Arg of perigee: 82
6378 deg
Mean anomaly: 277
4823 deg
Mean motion: 15
48995854 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 591
Checksum: 341
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