[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 11th 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) : 71 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 940 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
There are no maneuvers
Coasting Arc #1 (Orbit 3065)
---------------------------------------
Vector Time (GMT): 2020/160/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5963526
14 A = 6798803
65 meter
Y = 624869
64 meter E =
0006147
Z = -3205843
22 I = 51
85234
XDOT = 1999
452087 Wp = 61
09293
YDOT = 5601
541990 meter/sec RA = 30
81230 deg
ZDOT = 4821
107263 TA = 262
07016
MA = 262
13992
Ha = 228
934 n
mi
Hp = 221
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19565374
49 X = 5971667
51
Y = 2050097
23 feet Y = 691604
18 meter
Z = -10517858
34 Z = -3176855
00
XDOT = 6559
882176 XDOT = 1913
247324
YDOT = 18377
762434 feet/sec YDOT = 5623
418334 meter/sec
ZDOT = 15817
281046 ZDOT = 4830
611501
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6599680
13 X = 2011582
50
Y = -18607482
61 feet Y = -5671560
70 meter
Z = -10384504
55 Z = -3165196
99
XDOT = 18022
564043 XDOT = 5493
277520
YDOT = -2440
939818 feet/sec YDOT = -743
998457 meter/sec
ZDOT = 15860
561511 ZDOT = 4834
299148
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 20160
50652981
00016717 00000-0 10270-3 0 9002
2 25544 51
6446 31
4434 0002187 26
4102 333
7159 15
49427741 30660
Satellite: ISS
Catalog Number: 25544
Epoch time: 20160
50652981 = yrday
fracday
Element set: 900
Inclination: 51
6446 deg
RA of node: 31
4434 deg
Eccentricity:
0002187
Arg of perigee: 26
4102 deg
Mean anomaly: 333
7159 deg
Mean motion: 15
49427741 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3066
Checksum: 286
Coasting Arc #2 (Orbit 3081)
---------------------------------------
Vector Time (GMT): 2020/161/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6058212
79 A = 6799072
31 meter
Y = -261241
82 meter E =
0014204
Z = 3063747
81 I = 51
82405
XDOT = -2270
157722 Wp = 87
48434
YDOT = -5409
091287 meter/sec RA = 25
87543 deg
ZDOT = -4929
862936 TA = 57
51037
MA = 57
37316
Ha = 228
978 n
mi
Hp = 221
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19876026
20 X = -6069723
05
Y = -857092
59 feet Y = -329053
98 meter
Z = 10051666
05 Z = 3034291
63
XDOT = -7448
024023 XDOT = -2185
556687
YDOT = -17746
362491 feet/sec YDOT = -5434
003886 meter/sec
ZDOT = -16174
090998 ZDOT = -4940
685878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5181304
40 X = -1579261
58
Y = 19278262
92 feet Y = 5876014
54 meter
Z = 9916132
26 Z = 3022437
11
XDOT = -17513
829532 XDOT = -5338
215241
YDOT = 3672
542831 feet/sec YDOT = 1119
391055 meter/sec
ZDOT = -16223
451758 ZDOT = -4944
908096
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 20161
53848338
00016717 00000-0 10270-3 0 9010
2 25544 51
6447 26
3349 0002354 30
7207 329
4080 15
49464320 30826
Satellite: ISS
Catalog Number: 25544
Epoch time: 20161
53848338 = yrday
fracday
Element set: 901
Inclination: 51
6447 deg
RA of node: 26
3349 deg
Eccentricity:
0002354
Arg of perigee: 30
7207 deg
Mean anomaly: 329
4080 deg
Mean motion: 15
49464320 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3082
Checksum: 290
Coasting Arc #3 (Orbit 3096)
---------------------------------------
Vector Time (GMT): 2020/162/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6121518
96 A = 6799434
17 meter
Y = -148780
78 meter E =
0006584
Z = -2955537
37 I = 51
79254
XDOT = 2541
672509 Wp = 54
59372
YDOT = 5198
317966 meter/sec RA = 20
93673 deg
ZDOT = 5014
231072 TA = 271
82017
MA = 271
89558
Ha = 229
005 n
mi
Hp = 221
663
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20083723
61 X = 6137083
87
Y = -488125
91 feet Y = -80238
09 meter
Z = -9696644
92 Z = -2925763
93
XDOT = 8338
820567 XDOT = 2458
998445
YDOT = 17054
848971 feet/sec YDOT = 5226
277699 meter/sec
ZDOT = 16450
889345 ZDOT = 5026
377436
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3572471
05 X = 1088889
18
Y = -19836083
34 feet Y = -6046038
20 meter
Z = -9559623
00 Z = -2913773
09
XDOT = 16915
015664 XDOT = 5155
696775
YDOT = -4889
944240 feet/sec YDOT = -1490
455004 meter/sec
ZDOT = 16506
354277 ZDOT = 5031
136784
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 20162
50594026
00016717 00000-0 10270-3 0 9021
2 25544 51
6430 21
5460 0002212 33
9806 326
1486 15
49432009 30971
Satellite: ISS
Catalog Number: 25544
Epoch time: 20162
50594026 = yrday
fracday
Element set: 902
Inclination: 51
6430 deg
RA of node: 21
5460 deg
Eccentricity:
0002212
Arg of perigee: 33
9806 deg
Mean anomaly: 326
1486 deg
Mean motion: 15
49432009 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3097
Checksum: 276
Coasting Arc #4 (Orbit 3112)
---------------------------------------
Vector Time (GMT): 2020/163/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6164148
13 A = 6799674
06 meter
Y = 533830
77 meter E =
0014469
Z = 2807037
18 I = 51
76258
XDOT = -2771
288673 Wp = 92
00187
YDOT = -4987
271098 meter/sec RA = 15
99673 deg
ZDOT = -5114
889627 TA = 56
26222
MA = 56
12442
Ha = 228
961 n
mi
Hp = 221
552
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20223583
09 X = -6183294
30
Y = 1751413
28 feet Y = 464791
43 meter
Z = 9209439
56 Z = 2777048
00
XDOT = -9092
154440 XDOT = -2690
468582
YDOT = -16362
437984 feet/sec YDOT = -5017
809006 meter/sec
ZDOT = -16781
133948 ZDOT = -5128
155750
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2014234
79 X = -613938
76
Y = 20261467
83 feet Y = 6175695
39 meter
Z = 9071401
11 Z = 2764963
06
XDOT = -16259
424229 XDOT = -4955
872505
YDOT = 5957
210172 feet/sec YDOT = 1815
757661 meter/sec
ZDOT = -16841
765400 ZDOT = -5133
370094
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 20163
53789227
00016717 00000-0 10270-3 0 9035
2 25544 51
6438 16
4383 0002258 34
3756 325
7540 15
49473544 31139
Satellite: ISS
Catalog Number: 25544
Epoch time: 20163
53789227 = yrday
fracday
Element set: 903
Inclination: 51
6438 deg
RA of node: 16
4383 deg
Eccentricity:
0002258
Arg of perigee: 34
3756 deg
Mean anomaly: 325
7540 deg
Mean motion: 15
49473544 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3113
Checksum: 308
Coasting Arc #5 (Orbit 3127)
---------------------------------------
Vector Time (GMT): 2020/164/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6168762
64 A = 6800023
44 meter
Y = -959811
22 meter E =
0007070
Z = -2693207
46 I = 51
73012
XDOT = 3001
792042 Wp = 49
08920
YDOT = 4760
199599 meter/sec RA = 11
05306 deg
ZDOT = 5192
552626 TA = 280
61041
MA = 280
69003
Ha = 229
008 n
mi
Hp = 221
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20238722
57 X = 6192119
03
Y = -3148986
95 feet Y = -890696
79 meter
Z = -8835982
49 Z = -2663185
63
XDOT = 9848
399088 XDOT = 2923
116709
YDOT = 15617
452752 feet/sec YDOT = 4793
327212 meter/sec
ZDOT = 17035
933812 ZDOT = 5206
943576
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 289651
07 X = 88285
65
Y = -20539267
74 feet Y = -6260368
81 meter
Z = -8697768
66 Z = -2651079
89
XDOT = 15528
298083 XDOT = 4733
025256
YDOT = -7004
143175 feet/sec YDOT = -2134
862840 meter/sec
ZDOT = 17101
755285 ZDOT = 5212
615011
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 20164
50534689
00016717 00000-0 10270-3 0 9044
2 25544 51
6432 11
6487 0002136 38
9313 321
1990 15
49440900 31284
Satellite: ISS
Catalog Number: 25544
Epoch time: 20164
50534689 = yrday
fracday
Element set: 904
Inclination: 51
6432 deg
RA of node: 11
6487 deg
Eccentricity:
0002136
Arg of perigee: 38
9313 deg
Mean anomaly: 321
1990 deg
Mean motion: 15
49440900 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3128
Checksum: 292
Coasting Arc #6 (Orbit 3143)
---------------------------------------
Vector Time (GMT): 2020/165/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6155278
23 A = 6800244
84 meter
Y = 1356671
21 meter E =
0014808
Z = 2537240
89 I = 51
69779
XDOT = -3189
477548 Wp = 96
11456
YDOT = -4539
548184 meter/sec RA = 6
10841 deg
ZDOT = -5285
264328 TA = 55
47075
MA = 55
33105
Ha = 229
002 n
mi
Hp = 221
458
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20194482
37 X = -6182315
87
Y = 4451021
02 feet Y = 1287687
02 meter
Z = 8324281
14 Z = 2507275
58
XDOT = -10464
165184 XDOT = -3112
805243
YDOT = -14893
530788 feet/sec YDOT = -4574
785856 meter/sec
ZDOT = -17340
106063 ZDOT = -5300
571823
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1358088
40 X = 413945
34
Y = 20689667
79 feet Y = 6306210
74 meter
Z = 8186305
96 Z = 2495186
06
XDOT = -14771
216398 XDOT = -4502
266758
YDOT = 7891
308683 feet/sec YDOT = 2405
270886 meter/sec
ZDOT = -17410
157315 ZDOT = -5306
615950
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 20165
53729498
00016717 00000-0 10270-3 0 9053
2 25544 51
6430 6
5406 0002319 40
0340 320
0981 15
49483080 31445
Satellite: ISS
Catalog Number: 25544
Epoch time: 20165
53729498 = yrday
fracday
Element set: 905
Inclination: 51
6430 deg
RA of node: 6
5406 deg
Eccentricity:
0002319
Arg of perigee: 40
0340 deg
Mean anomaly: 320
0981 deg
Mean motion: 15
49483080 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3144
Checksum: 282
Coasting Arc #7 (Orbit 3158)
---------------------------------------
Vector Time (GMT): 2020/166/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6097170
98 A = 6800609
66 meter
Y = -1789499
85 meter E =
0007784
Z = -2418676
48 I = 51
66312
XDOT = 3381
280686 Wp = 46
53396
YDOT = 4304
300788 meter/sec RA = 1
16111 deg
ZDOT = 5355
221858 TA = 286
49597
MA = 286
58148
Ha = 229
085 n
mi
Hp = 221
494
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20003841
79 X = 6128477
08
Y = -5871062
49 feet Y = -1721141
61 meter
Z = -7935290
29 Z = -2388983
01
XDOT = 11093
440570 XDOT = 3306
884832
YDOT = 14121
721747 feet/sec YDOT = 4341
696064 meter/sec
ZDOT = 17569
625518 ZDOT = 5371
466605
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3146889
22 X = -959171
83
Y = -20660874
26 feet Y = -6297434
47 meter
Z = -7798541
94 Z = -2376995
58
XDOT = 13952
174309 XDOT = 4252
622729
YDOT = -8764
647275 feet/sec YDOT = -2671
464489 meter/sec
ZDOT = 17644
001788 ZDOT = 5377
891745
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 20166
50474826
00016717 00000-0 10270-3 0 9064
2 25544 51
6411 1
7518 0002144 49
2678 310
8658 15
49438857 31592
Satellite: ISS
Catalog Number: 25544
Epoch time: 20166
50474826 = yrday
fracday
Element set: 906
Inclination: 51
6411 deg
RA of node: 1
7518 deg
Eccentricity:
0002144
Arg of perigee: 49
2678 deg
Mean anomaly: 310
8658 deg
Mean motion: 15
49438857 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3159
Checksum: 320
Coasting Arc #8 (Orbit 3174)
---------------------------------------
Vector Time (GMT): 2020/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6023365
19 A = 6800786
06 meter
Y = 2189624
01 meter E =
0014921
Z = 2257006
81 I = 51
63112
XDOT = -3532
075983 Wp = 100
93709
YDOT = -4081
462340 meter/sec RA = 356
21181 deg
ZDOT = -5438
763108 TA = 53
99673
MA = 53
85850
Ha = 228
969 n
mi
Hp = 221
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19761696
83 X = -6058365
82
Y = 7183805
82 feet Y = 2122070
47 meter
Z = 7404878
00 Z = 2227662
86
XDOT = -11588
175797 XDOT = -3459
754889
YDOT = -13390
624475 feet/sec YDOT = -4120
555475 meter/sec
ZDOT = -17843
710984 ZDOT = -5455
745450
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4834193
02 X = 1473462
03
Y = 20512087
97 feet Y = 6252084
41 meter
Z = 7269715
99 Z = 2215809
43
XDOT = -13137
144777 XDOT = -4004
201728
YDOT = 9480
630069 feet/sec YDOT = 2889
696045 meter/sec
ZDOT = -17921
491922 ZDOT = -5462
470738
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 20167
53669462
00016717 00000-0 10270-3 0 9071
2 25544 51
6418 356
6435 0002132 45
6543 314
4782 15
49487798 31751
Satellite: ISS
Catalog Number: 25544
Epoch time: 20167
53669462 = yrday
fracday
Element set: 907
Inclination: 51
6418 deg
RA of node: 356
6435 deg
Eccentricity:
0002132
Arg of perigee: 45
6543 deg
Mean anomaly: 314
4782 deg
Mean motion: 15
49487798 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3175
Checksum: 336
Coasting Arc #9 (Orbit 3189)
---------------------------------------
Vector Time (GMT): 2020/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5900856
44 A = 6801131
52 meter
Y = -2618173
86 meter E =
0008549
Z = -2133392
38 I = 51
59742
XDOT = 3687
783316 Wp = 44
85945
YDOT = 3844
806141 meter/sec RA = 351
25937 deg
ZDOT = 5501
143457 TA = 291
53728
MA = 291
62838
Ha = 229
127 n
mi
Hp = 221
404
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19359765
23 X = 5940057
93
Y = -8589809
26 feet Y = -2551966
80 meter
Z = -6999318
82 Z = -2104633
33
XDOT = 12099
026627 XDOT = 3617
793933
YDOT = 12614
193377 feet/sec YDOT = 3885
653468 meter/sec
ZDOT = 18048
370923 ZDOT = 5518
887893
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6625467
71 X = -2019442
56
Y = -20162483
11 feet Y = -6145524
85 meter
Z = -6866822
35 Z = -2093007
45
XDOT = 12269
196518 XDOT = 3739
651099
YDOT = -10184
107099 feet/sec YDOT = -3104
115844 meter/sec
ZDOT = 18129
670181 ZDOT = 5525
923471
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 20168
50414567
00016717 00000-0 10270-3 0 9084
2 25544 51
6409 351
8539 0002158 57
7744 302
3615 15
49443248 31908
Satellite: ISS
Catalog Number: 25544
Epoch time: 20168
50414567 = yrday
fracday
Element set: 908
Inclination: 51
6409 deg
RA of node: 351
8539 deg
Eccentricity:
0002158
Arg of perigee: 57
7744 deg
Mean anomaly: 302
3615 deg
Mean motion: 15
49443248 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3190
Checksum: 316
Coasting Arc #10 (Orbit 3205)
---------------------------------------
Vector Time (GMT): 2020/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5766449
86 A = 6801301
23 meter
Y = 3010032
62 meter E =
0015197
Z = 1964870
89 I = 51
56496
XDOT = -3804
108851 Wp = 105
35301
YDOT = -3627
172191 meter/sec RA = 346
30559 deg
ZDOT = -5575
519202 TA = 52
98369
MA = 52
84474
Ha = 229
037 n
mi
Hp = 221
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18918798
75 X = -5809224
64
Y = 9875435
11 feet Y = 2945308
60 meter
Z = 6446426
80 Z = 1936756
13
XDOT = -12480
672083 XDOT = -3736
183155
YDOT = -11900
171230 feet/sec YDOT = -3669
331785 meter/sec
ZDOT = -18292
385834 ZDOT = -5593
833776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8289019
16 X = 2526493
04
Y = 19707635
45 feet Y = 6006887
29 meter
Z = 6316870
23 Z = 1925382
04
XDOT = -11436
365762 XDOT = -3485
804284
YDOT = 10734
748419 feet/sec YDOT = 3271
951318 meter/sec
ZDOT = -18376
319463 ZDOT = -5601
102172
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 20169
53608827
00016717 00000-0 10270-3 0 9093
2 25544 51
6406 346
7456 0002169 55
6586 304
4769 15
49485049 32065
Satellite: ISS
Catalog Number: 25544
Epoch time: 20169
53608827 = yrday
fracday
Element set: 909
Inclination: 51
6406 deg
RA of node: 346
7456 deg
Eccentricity:
0002169
Arg of perigee: 55
6586 deg
Mean anomaly: 304
4769 deg
Mean motion: 15
49485049 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3206
Checksum: 342
Coasting Arc #11 (Orbit 3220)
---------------------------------------
Vector Time (GMT): 2020/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5579163
16 A = 6801608
65 meter
Y = -3423840
21 meter E =
0009365
Z = -1837391
69 I = 51
53243
XDOT = 3929
070332 Wp = 45
20874
YDOT = 3394
378036 meter/sec RA = 341
34925 deg
ZDOT = 5629
411658 TA = 294
59972
MA = 294
69726
Ha = 229
201 n
mi
Hp = 221
289
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18304341
08 X = 5625959
96
Y = -11233071
55 feet Y = -3361188
05 meter
Z = -6028187
96 Z = -1810177
06
XDOT = 12890
650697 XDOT = 3863
476744
YDOT = 11136
410879 feet/sec YDOT = 3437
947959 meter/sec
ZDOT = 18469
198352 ZDOT = 5648
338943
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10021538
00 X = -3054564
78
Y = -19034080
86 feet Y = -5801587
85 meter
Z = -5902744
35 Z = -1799156
48
XDOT = 10552
861256 XDOT = 3216
512111
YDOT = -11285
545380 feet/sec YDOT = -3439
834232 meter/sec
ZDOT = 18555
964681 ZDOT = 5655
858035
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 20170
50353772
00016717 00000-0 10270-3 0 9100
2 25544 51
6398 341
9566 0002253 69
3585 290
7806 15
49444881 32214
Satellite: ISS
Catalog Number: 25544
Epoch time: 20170
50353772 = yrday
fracday
Element set: 910
Inclination: 51
6398 deg
RA of node: 341
9566 deg
Eccentricity:
0002253
Arg of perigee: 69
3585 deg
Mean anomaly: 290
7806 deg
Mean motion: 15
49444881 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3221
Checksum: 318
Coasting Arc #12 (Orbit 3236)
---------------------------------------
Vector Time (GMT): 2020/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5383935
30 A = 6801779
95 meter
Y = 3797470
69 meter E =
0015367
Z = 1663849
94 I = 51
50192
XDOT = -4018
342789 Wp = 110
09534
YDOT = -3185
931947 meter/sec RA = 336
39101 deg
ZDOT = -5693
604531 TA = 51
67298
MA = 51
53493
Ha = 229
088 n
mi
Hp = 221
299
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17663829
72 X = -5434081
67
Y = 12458893
33 feet Y = 3736982
98 meter
Z = 5458825
27 Z = 1637575
70
XDOT = -13183
539333 XDOT = -3954
761704
YDOT = -10452
532633 feet/sec YDOT = -3230
511317 meter/sec
ZDOT = -18679
804892 ZDOT = -5712
970347
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11602540
16 X = 3536454
24
Y = 18273584
58 feet Y = 5569788
58 meter
Z = 5337681
64 Z = 1626925
36
XDOT = -9730
637485 XDOT = -2965
898306
YDOT = 11697
538104 feet/sec YDOT = 3565
409614 meter/sec
ZDOT = -18768
602676 ZDOT = -5720
670096
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 20171
53547913
00016717 00000-0 10270-3 0 9117
2 25544 51
6400 336
8482 0002140 67
4671 292
6705 15
49474161 32378
Satellite: ISS
Catalog Number: 25544
Epoch time: 20171
53547913 = yrday
fracday
Element set: 911
Inclination: 51
6400 deg
RA of node: 336
8482 deg
Eccentricity:
0002140
Arg of perigee: 67
4671 deg
Mean anomaly: 292
6705 deg
Mean motion: 15
49474161 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3237
Checksum: 299
Coasting Arc #13 (Orbit 3251)
---------------------------------------
Vector Time (GMT): 2020/172/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5134647
40 A = 6801992
87 meter
Y = -4184730
87 meter E =
0010192
Z = -1531862
08 I = 51
47373
XDOT = 4116
657927 Wp = 45
54305
YDOT = 2961
422124 meter/sec RA = 331
43024 deg
ZDOT = 5739
281561 TA = 297
71824
MA = 297
82159
Ha = 229
220 n
mi
Hp = 221
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16845956
02 X = 5188501
60
Y = -13729431
99 feet Y = -4127010
15 meter
Z = -5025794
23 Z = -1506789
99
XDOT = 13506
095560 XDOT = 4055
358284
YDOT = 9715
951849 feet/sec YDOT = 3007
113594 meter/sec
ZDOT = 18829
663914 ZDOT = 5759
130432
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13210041
92 X = -4026420
78
Y = -17289515
22 feet Y = -5269844
24 meter
Z = -4910152
81 Z = -1496614
58
XDOT = 8858
540895 XDOT = 2700
083265
YDOT = -12112
532031 feet/sec YDOT = -3691
899763 meter/sec
ZDOT = 18920
701363 ZDOT = 5767
029775
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 20172
50292481
00016717 00000-0 10270-3 0 9123
2 25544 51
6416 332
0591 0002321 76
7969 283
3440 15
49457260 32529
Satellite: ISS
Catalog Number: 25544
Epoch time: 20172
50292481 = yrday
fracday
Element set: 912
Inclination: 51
6416 deg
RA of node: 332
0591 deg
Eccentricity:
0002321
Arg of perigee: 76
7969 deg
Mean anomaly: 283
3440 deg
Mean motion: 15
49457260 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3252
Checksum: 296
Coasting Arc #14 (Orbit 3267)
---------------------------------------
Vector Time (GMT): 2020/173/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4882441
68 A = 6802186
99 meter
Y = 4528933
80 meter E =
0015524
Z = 1352713
88 I = 51
44427
XDOT = -4183
798645 Wp = 114
22154
YDOT = -2766
279596 meter/sec RA = 326
46803 deg
ZDOT = -5792
850891 TA = 51
03150
MA = 50
89330
Ha = 229
179 n
mi
Hp = 221
207
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16018509
45 X = -4939293
38
Y = 14858706
71 feet Y = 4474016
70 meter
Z = 4438037
65 Z = 1328859
83
XDOT = -13726
373507 XDOT = -4124
416063
YDOT = -9075
720458 feet/sec YDOT = -2812
732549 meter/sec
ZDOT = -19005
416308 ZDOT = -5813
030457
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14645619
00 X = 4463984
67
Y = 16243289
60 feet Y = 4950954
67 meter
Z = 4327975
89 Z = 1319167
05
XDOT = -8071
143242 XDOT = -2460
084460
YDOT = 12407
484353 feet/sec YDOT = 3781
801231 meter/sec
ZDOT = -19097
992428 ZDOT = -5821
068092
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 20173
53486328
00016717 00000-0 10270-3 0 9133
2 25544 51
6405 326
9507 0002302 77
8087 282
3321 15
49465601 32680
Satellite: ISS
Catalog Number: 25544
Epoch time: 20173
53486328 = yrday
fracday
Element set: 913
Inclination: 51
6405 deg
RA of node: 326
9507 deg
Eccentricity:
0002302
Arg of perigee: 77
8087 deg
Mean anomaly: 282
3321 deg
Mean motion: 15
49465601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3268
Checksum: 307
Coasting Arc #15 (Orbit 3282)
---------------------------------------
Vector Time (GMT): 2020/174/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4574924
88 A = 6802345
04 meter
Y = -4879424
91 meter E =
0010954
Z = -1217462
18 I = 51
41862
XDOT = 4262
356782 Wp = 46
62382
YDOT = 2551
980824 meter/sec RA = 321
50450 deg
ZDOT = 5829
393457 TA = 300
13340
MA = 300
24191
Ha = 229
235 n
mi
Hp = 221
166
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15009596
05 X = 4635061
73
Y = -16008611
92 feet Y = -4827928
34 meter
Z = -3994298
49 Z = -1195094
12
XDOT = 13984
110178 XDOT = 4205
187345
YDOT = 8372
640499 feet/sec YDOT = 2599
324640 meter/sec
ZDOT = 19125
306618 ZDOT = 5849
959859
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16068692
59 X = -4897737
50
Y = -14972471
24 feet Y = -4563609
23 meter
Z = -3891050
38 Z = -1185992
15
XDOT = 7226
553657 XDOT = 2202
653555
YDOT = -12715
024047 feet/sec YDOT = -3875
539329 meter/sec
ZDOT = 19219
682684 ZDOT = 5858
159282
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 20174
50230656
00016717 00000-0 10270-3 0 9143
2 25544 51
6418 322
1628 0002349 84
4695 275
6723 15
49457060 32834
Satellite: ISS
Catalog Number: 25544
Epoch time: 20174
50230656 = yrday
fracday
Element set: 914
Inclination: 51
6418 deg
RA of node: 322
1628 deg
Eccentricity:
0002349
Arg of perigee: 84
4695 deg
Mean anomaly: 275
6723 deg
Mean motion: 15
49457060 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3283
Checksum: 311
Coasting Arc #16 (Orbit 3297)
---------------------------------------
Vector Time (GMT): 2020/175/11:57:30
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3564628
41 A = 6801475
87 meter
Y = 5464514
44 meter E =
0015968
Z = 1896500
42 I = 51
39003
XDOT = -5064
141255 Wp = 109
48690
YDOT = -1351
643718 meter/sec RA = 316
53978 deg
ZDOT = -5590
544932 TA = 49
58432
MA = 49
44512
Ha = 229
196 n
mi
Hp = 221
218
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11694975
08 X = -3634681
31
Y = 17928196
97 feet Y = 5424260
15 meter
Z = 6222114
24 Z = 1879016
02
XDOT = -16614
636663 XDOT = -5021
495053
YDOT = -4434
526635 feet/sec YDOT = -1408
034966 meter/sec
ZDOT = -18341
682847 ZDOT = -5615
040961
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18047941
42 X = 5501012
54
Y = 11552651
77 feet Y = 3521248
26 meter
Z = 6141289
95 Z = 1871865
18
XDOT = -3423
802691 XDOT = -1043
575060
YDOT = 15217
804834 feet/sec YDOT = 4638
386913 meter/sec
ZDOT = -18454
227316 ZDOT = -5624
848486
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 20175
53424390
00016717 00000-0 10270-3 0 9158
2 25544 51
6417 317
0543 0002255 87
2881 272
8527 15
49454732 32986
Satellite: ISS
Catalog Number: 25544
Epoch time: 20175
53424390 = yrday
fracday
Element set: 915
Inclination: 51
6417 deg
RA of node: 317
0543 deg
Eccentricity:
0002255
Arg of perigee: 87
2881 deg
Mean anomaly: 272
8527 deg
Mean motion: 15
49454732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3298
Checksum: 318
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