[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 29th 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
8
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 321)
---------------------------------------
Vector Time (GMT): 2020/241/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3356679
76 A = 6793645
51 meter
Y = -3343249
16 meter E =
0013307
Z = -4881723
70 I = 51
56482
XDOT = 6571
569162 Wp = 72
46705
YDOT = -3091
711701 meter/sec RA = 350
02628 deg
ZDOT = -2402
769735 TA = 173
90092
MA = 173
88471
Ha = 229
271 n
mi
Hp = 221
876
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11012728
86 X = -3295332
77
Y = -10968665
21 feet Y = -3380442
77 meter
Z = -16016153
88 Z = -4897880
03
XDOT = 21560
266280 XDOT = 6617
324320
YDOT = -10143
411094 feet/sec YDOT = -3017
967800 meter/sec
ZDOT = -7883
102805 ZDOT = -2370
737039
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5565443
91 X = 1696347
30
Y = 14430197
33 feet Y = 4398324
15 meter
Z = -16090501
47 Z = -4904384
85
XDOT = -22816
164454 XDOT = -6954
366926
YDOT = 180
159168 feet/sec YDOT = 54
912514 meter/sec
ZDOT = -7735
100900 ZDOT = -2357
658754
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
52030229
00016717 00000-0 10270-3 0 9009
2 25544 51
6448 350
5068 0001358 72
9939 287
1360 15
49179357 3228
Satellite: ISS
Catalog Number: 25544
Epoch time: 20241
52030229 = yrday
fracday
Element set: 900
Inclination: 51
6448 deg
RA of node: 350
5068 deg
Eccentricity:
0001358
Arg of perigee: 72
9939 deg
Mean anomaly: 287
1360 deg
Mean motion: 15
49179357 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 322
Checksum: 301
Coasting Arc #2 (Orbit 337)
---------------------------------------
Vector Time (GMT): 2020/242/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3557914
00 A = 6793409
93 meter
Y = 3077412
10 meter E =
0007656
Z = 4896138
80 I = 51
53220
XDOT = -6344
084479 Wp = 113
16142
YDOT = 3610
985461 meter/sec RA = 345
07229 deg
ZDOT = 2334
600805 TA = 313
91087
MA = 313
97405
Ha = 229
130 n
mi
Hp = 221
886
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11672946
19 X = 3499454
80
Y = 10096496
39 feet Y = 3116872
27 meter
Z = 16063447
49 Z = 4913279
53
XDOT = -20813
925457 XDOT = -6395
332058
YDOT = 11847
065162 feet/sec YDOT = 3539
754775 meter/sec
ZDOT = 7659
451459 ZDOT = 2303
659872
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6758649
36 X = -2060036
32
Y = -13783190
10 feet Y = -4201116
34 meter
Z = 16142353
83 Z = 4920189
45
XDOT = 22818
876117 XDOT = 6955
193440
YDOT = -2363
932991 feet/sec YDOT = -720
526776 meter/sec
ZDOT = 7516
466370 ZDOT = 2291
018950
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
55241598
00016717 00000-0 10270-3 0 9017
2 25544 51
6456 345
3997 0001426 74
0707 286
0600 15
49221925 3383
Satellite: ISS
Catalog Number: 25544
Epoch time: 20242
55241598 = yrday
fracday
Element set: 901
Inclination: 51
6456 deg
RA of node: 345
3997 deg
Eccentricity:
0001426
Arg of perigee: 74
0707 deg
Mean anomaly: 286
0600 deg
Mean motion: 15
49221925 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 338
Checksum: 304
Coasting Arc #3 (Orbit 352)
---------------------------------------
Vector Time (GMT): 2020/243/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3736287
05 A = 6793404
90 meter
Y = -2822716
06 meter E =
0013741
Z = -4934483
93 I = 51
49932
XDOT = 6058
958703 Wp = 73
37900
YDOT = -4092
716041 meter/sec RA = 340
11708 deg
ZDOT = -2247
895665 TA = 174
57351
MA = 174
55861
Ha = 229
293 n
mi
Hp = 221
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12258159
61 X = -3680476
47
Y = -9260879
46 feet Y = -2864185
82 meter
Z = -16189251
72 Z = -4952497
45
XDOT = 19878
473436 XDOT = 6115
193149
YDOT = -13427
546065 feet/sec YDOT = -4024
645995 meter/sec
ZDOT = -7374
985776 ZDOT = -2218
327624
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7847255
80 X = 2391843
57
Y = 13105506
35 feet Y = 3994558
34 meter
Z = -16272200
73 Z = -4959766
78
XDOT = -22531
090113 XDOT = -6867
476266
YDOT = 4509
303820 feet/sec YDOT = 1374
435804 meter/sec
ZDOT = -7238
320510 ZDOT = -2206
240091
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
52002196
00016717 00000-0 10270-3 0 9025
2 25544 51
6455 340
6132 0001434 73
8175 286
3133 15
49183430 3535
Satellite: ISS
Catalog Number: 25544
Epoch time: 20243
52002196 = yrday
fracday
Element set: 902
Inclination: 51
6455 deg
RA of node: 340
6132 deg
Eccentricity:
0001434
Arg of perigee: 73
8175 deg
Mean anomaly: 286
3133 deg
Mean motion: 15
49183430 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 353
Checksum: 274
Coasting Arc #4 (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 = 3894690
27 A = 6793164
20 meter
Y = 2539230
90 meter E =
0007343
Z = 4948048
02 I = 51
46748
XDOT = -5752
701182 Wp = 114
09172
YDOT = 4572
616214 meter/sec RA = 335
15938 deg
ZDOT = 2175
982837 TA = 314
59668
MA = 314
65658
Ha = 229
125 n
mi
Hp = 221
854
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12777855
20 X = 3841972
06
Y = 8330810
04 feet Y = 2582489
44 meter
Z = 16233753
33 Z = 4966838
43
XDOT = -18873
691542 XDOT = -5813
975468
YDOT = 15002
021701 feet/sec YDOT = 4507
942828 meter/sec
ZDOT = 7139
051304 ZDOT = 2147
890117
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8887070
66 X = -2708779
14
Y = -12283257
50 feet Y = -3743936
89 meter
Z = 16320302
91 Z = 4974428
33
XDOT = 22117
803172 XDOT = 6741
506407
YDOT = -6665
804725 feet/sec YDOT = -2031
737280 meter/sec
ZDOT = 7009
182218 ZDOT = 2136
398740
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
55213190
00016717 00000-0 10270-3 0 9038
2 25544 51
6453 335
5069 0001468 77
5622 282
5693 15
49228300 3692
Satellite: ISS
Catalog Number: 25544
Epoch time: 20244
55213190 = yrday
fracday
Element set: 903
Inclination: 51
6453 deg
RA of node: 335
5069 deg
Eccentricity:
0001468
Arg of perigee: 77
5622 deg
Mean anomaly: 282
5693 deg
Mean motion: 15
49228300 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 369
Checksum: 304
Coasting Arc #5 (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 = -4034153
45 A = 6793186
54 meter
Y = -2269614
56 meter E =
0014043
Z = -4985074
70 I = 51
43623
XDOT = 5393
787027 Wp = 74
93367
YDOT = -5006
444529 meter/sec RA = 330
19971 deg
ZDOT = -2086
926492 TA = 174
65272
MA = 174
63771
Ha = 229
290 n
mi
Hp = 221
811
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13235411
58 X = -3984259
92
Y = -7446242
00 feet Y = -2314448
59 meter
Z = -16355231
97 Z = -5004549
40
XDOT = 17696
151663 XDOT = 5459
506625
YDOT = -16425
342944 feet/sec YDOT = -4945
759965 meter/sec
ZDOT = -6846
871692 ZDOT = -2060
566252
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9826309
13 X = 2995059
02
Y = 11450914
86 feet Y = 3490238
85 meter
Z = -16444952
12 Z = -5012421
41
XDOT = -21421
421988 XDOT = -6529
249422
YDOT = 8730
723002 feet/sec YDOT = 2661
124371 meter/sec
ZDOT = -6724
990767 ZDOT = -2049
777186
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
51973545
00016717 00000-0 10270-3 0 9043
2 25544 51
6446 330
7203 0001396 80
1934 279
9374 15
49182827 3843
Satellite: ISS
Catalog Number: 25544
Epoch time: 20245
51973545 = yrday
fracday
Element set: 904
Inclination: 51
6446 deg
RA of node: 330
7203 deg
Eccentricity:
0001396
Arg of perigee: 80
1934 deg
Mean anomaly: 279
9374 deg
Mean motion: 15
49182827 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 384
Checksum: 320
Coasting Arc #6 (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 = 4149165
28 A = 6792930
76 meter
Y = 1975554
36 meter E =
0006954
Z = 4997989
41 I = 51
40783
XDOT = -5015
842696 Wp = 115
06714
YDOT = 5434
608906 meter/sec RA = 325
23732 deg
ZDOT = 2010
758621 TA = 315
29135
MA = 315
34739
Ha = 229
098 n
mi
Hp = 221
851
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13612746
99 X = 4102488
68
Y = 6481477
55 feet Y = 2021692
60 meter
Z = 16397603
04 Z = 5018030
63
XDOT = -16456
176823 XDOT = -5086
008301
YDOT = 17830
081714 feet/sec YDOT = 5378
125959 meter/sec
ZDOT = 6596
977102 ZDOT = 1986
223270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10689758
86 X = -3258238
50
Y = -10488490
61 feet Y = -3196891
94 meter
Z = 16489949
60 Z = 5026136
64
XDOT = 20603
310251 XDOT = 6279
888965
YDOT = -10779
218867 feet/sec YDOT = -3285
505911 meter/sec
ZDOT = 6483
512660 ZDOT = 1976
174659
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
55184057
00016717 00000-0 10270-3 0 9051
2 25544 51
6452 325
6136 0001442 80
1900 279
9413 15
49233355 4009
Satellite: ISS
Catalog Number: 25544
Epoch time: 20246
55184057 = yrday
fracday
Element set: 905
Inclination: 51
6452 deg
RA of node: 325
6136 deg
Eccentricity:
0001442
Arg of perigee: 80
1900 deg
Mean anomaly: 279
9413 deg
Mean motion: 15
49233355 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 400
Checksum: 284
Coasting Arc #7 (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 = -4249019
87 A = 6792962
43 meter
Y = -1697939
19 meter E =
0014492
Z = -5033940
09 I = 51
37912
XDOT = 4592
276171 Wp = 76
01109
YDOT = -5808
676660 meter/sec RA = 320
27335 deg
ZDOT = -1918
202171 TA = 175
27400
MA = 175
26030
Ha = 229
327 n
mi
Hp = 221
749
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13940353
90 X = -4205265
49
Y = -5570666
65 feet Y = -1745210
48 meter
Z = -16515551
49 Z = -5054473
54
XDOT = 15066
522871 XDOT = 4666
206653
YDOT = -19057
338124 feet/sec YDOT = -5756
909301 meter/sec
ZDOT = -6293
314210 ZDOT = -1895
714987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11458462
42 X = 3492539
35
Y = 9535975
69 feet Y = 2906565
39 meter
Z = -16610178
85 Z = -5062782
51
XDOT = -19521
472194 XDOT = -5950
144725
YDOT = 12683
301870 feet/sec YDOT = 3865
870410 meter/sec
ZDOT = -6189
299349 ZDOT = -1886
498442
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
51943958
00016717 00000-0 10270-3 0 9062
2 25544 51
6440 320
8267 0001511 80
5855 279
5466 15
49186884 4152
Satellite: ISS
Catalog Number: 25544
Epoch time: 20247
51943958 = yrday
fracday
Element set: 906
Inclination: 51
6440 deg
RA of node: 320
8267 deg
Eccentricity:
0001511
Arg of perigee: 80
5855 deg
Mean anomaly: 279
5466 deg
Mean motion: 15
49186884 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 415
Checksum: 328
Coasting Arc #8 (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 = 4322241
26 A = 6792737
63 meter
Y = 1399173
37 meter E =
0006687
Z = 5045485
45 I = 51
35323
XDOT = -4150
791203 Wp = 115
40421
YDOT = 6174
750741 meter/sec RA = 315
30736 deg
ZDOT = 1838
735375 TA = 316
67967
MA = 316
73223
Ha = 229
139 n
mi
Hp = 221
815
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14180581
57 X = 4281766
14
Y = 4590463
82 feet Y = 1447281
83 meter
Z = 16553429
94 Z = 5066382
64
XDOT = -13618
081374 XDOT = -4228
462088
YDOT = 20258
368572 feet/sec YDOT = 6127
899471 meter/sec
ZDOT = 6032
596375 ZDOT = 1818
383499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12134376
81 X = -3698558
05
Y = -8468776
98 feet Y = -2581283
22 meter
Z = 16649745
06 Z = 5074842
29
XDOT = 18323
586095 XDOT = 5585
029042
YDOT = -14549
334228 feet/sec YDOT = -4434
637073 meter/sec
ZDOT = 5938
432492 ZDOT = 1810
034224
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
55154209
00016717 00000-0 10270-3 0 9071
2 25544 51
6436 315
7203 0001552 83
8703 276
2624 15
49228175 4311
Satellite: ISS
Catalog Number: 25544
Epoch time: 20248
55154209 = yrday
fracday
Element set: 907
Inclination: 51
6436 deg
RA of node: 315
7203 deg
Eccentricity:
0001552
Arg of perigee: 83
8703 deg
Mean anomaly: 276
2624 deg
Mean motion: 15
49228175 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 431
Checksum: 296
Coasting Arc #9 (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 = 4035927
24 A = 6792068
96 meter
Y = 1676658
35 meter E =
0005225
Z = 5195472
44 I = 51
32872
XDOT = -4157
230132 Wp = 113
79972
YDOT = 6328
649948 meter/sec RA = 310
48985 deg
ZDOT = 1184
034707 TA = 324
76998
MA = 324
80451
Ha = 229
109 n
mi
Hp = 221
822
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13241231
09 X = 3991641
82
Y = 5500847
62 feet Y = 1721543
74 meter
Z = 17045513
27 Z = 5214969
66
XDOT = -13639
206470 XDOT = -4233
441371
YDOT = 20763
287232 feet/sec YDOT = 6281
734784 meter/sec
ZDOT = 3884
628305 ZDOT = 1163
655013
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9171342
53 X = -2795425
20
Y = -10881412
83 feet Y = -3316654
63 meter
Z = 17135354
65 Z = 5222856
10
XDOT = 20837
041754 XDOT = 6351
130327
YDOT = -11578
090760 feet/sec YDOT = -3529
002064 meter/sec
ZDOT = 3790
346979 ZDOT = 1155
297759
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
51913750
00016717 00000-0 10270-3 0 9083
2 25544 51
6437 310
9325 0001495 88
5855 271
5466 15
49236383 4468
Satellite: ISS
Catalog Number: 25544
Epoch time: 20249
51913750 = yrday
fracday
Element set: 908
Inclination: 51
6437 deg
RA of node: 310
9325 deg
Eccentricity:
0001495
Arg of perigee: 88
5855 deg
Mean anomaly: 271
5466 deg
Mean motion: 15
49236383 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 446
Checksum: 325
Coasting Arc #10 (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 = -4123560
61 A = 6792143
47 meter
Y = -1420672
31 meter E =
0015766
Z = -5220783
60 I = 51
30684
XDOT = 3659
964222 Wp = 82
14224
YDOT = -6627
348355 meter/sec RA = 305
51987 deg
ZDOT = -1088
070025 TA = 177
36030
MA = 177
35197
Ha = 229
333 n
mi
Hp = 221
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13528742
16 X = -4082008
15
Y = -4660998
40 feet Y = -1466552
92 meter
Z = -17128555
10 Z = -5240713
24
XDOT = 12007
756633 XDOT = 3739
086434
YDOT = -21743
268882 feet/sec YDOT = -6585
977683 meter/sec
ZDOT = -3569
783545 ZDOT = -1070
098736
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9984817
67 X = 3043372
43
Y = 10094574
28 feet Y = 3076826
24 meter
Z = -17220399
43 Z = -5248777
75
XDOT = -19645
971706 XDOT = -5988
092176
YDOT = 13488
564554 feet/sec YDOT = 4111
314476 meter/sec
ZDOT = -3486
612549 ZDOT = -1062
719505
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
48673191
00016717 00000-0 10270-3 0 9094
2 25544 51
6430 306
1447 0001528 88
1696 271
9629 15
49192269 4615
Satellite: ISS
Catalog Number: 25544
Epoch time: 20250
48673191 = yrday
fracday
Element set: 909
Inclination: 51
6430 deg
RA of node: 306
1447 deg
Eccentricity:
0001528
Arg of perigee: 88
1696 deg
Mean anomaly: 271
9629 deg
Mean motion: 15
49192269 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 461
Checksum: 323
Coasting Arc #11 (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 = 4182325
01 A = 6791943
77 meter
Y = 1149460
72 meter E =
0004991
Z = 5222828
55 I = 51
28817
XDOT = -3151
108809 Wp = 111
38938
YDOT = 6914
477060 meter/sec RA = 300
54869 deg
ZDOT = 999
011192 TA = 328
97946
MA = 329
00892
Ha = 229
143 n
mi
Hp = 221
782
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13721538
76 X = 4143790
95
Y = 3771196
58 feet Y = 1196015
28 meter
Z = 17135264
29 Z = 5243051
07
XDOT = -10338
283495 XDOT = -3233
047016
YDOT = 22685
292192 feet/sec YDOT = 6878
781010 meter/sec
ZDOT = 3277
595774 ZDOT = 983
504912
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10709735
15 X = -3264327
27
Y = -9197894
46 feet Y = -2803518
23 meter
Z = 17228468
94 Z = 5251237
33
XDOT = 18351
439938 XDOT = 5593
518893
YDOT = -15347
440177 feet/sec YDOT = -4677
899766 meter/sec
ZDOT = 3205
794718 ZDOT = 977
126230
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
51882862
00016717 00000-0 10270-3 0 9108
2 25544 51
6432 301
0379 0001608 88
9115 271
2220 15
49236070 4774
Satellite: ISS
Catalog Number: 25544
Epoch time: 20251
51882862 = yrday
fracday
Element set: 910
Inclination: 51
6432 deg
RA of node: 301
0379 deg
Eccentricity:
0001608
Arg of perigee: 88
9115 deg
Mean anomaly: 271
2220 deg
Mean motion: 15
49236070 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 477
Checksum: 286
Coasting Arc #12 (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 = -4238759
81 A = 6792022
30 meter
Y = -889337
02 meter E =
0016103
Z = -5246150
88 I = 51
27084
XDOT = 2611
607197 Wp = 83
91514
YDOT = -7131
921540 meter/sec RA = 295
57637 deg
ZDOT = -901
824408 TA = 177
39576
MA = 177
38737
Ha = 229
391 n
mi
Hp = 221
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13906692
28 X = -4203017
01
Y = -2917772
38 feet Y = -936538
21 meter
Z = -17211781
11 Z = -5266654
37
XDOT = 8568
265081 XDOT = 2695
544955
YDOT = -23398
692717 feet/sec YDOT = -7102
247384 meter/sec
ZDOT = -2958
741495 ZDOT = -888
934054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11384287
83 X = 3469930
93
Y = 8309341
73 feet Y = 2532687
36 meter
Z = -17306291
50 Z = -5274957
65
XDOT = -16811
390081 XDOT = -5124
111697
YDOT = 16999
622094 feet/sec YDOT = 5181
484814 meter/sec
ZDOT = -2899
008067 ZDOT = -883
617659
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
48642128
00016717 00000-0 10270-3 0 9115
2 25544 51
6422 296
2504 0001695 92
3356 267
7988 15
49194405 4923
Satellite: ISS
Catalog Number: 25544
Epoch time: 20252
48642128 = yrday
fracday
Element set: 911
Inclination: 51
6422 deg
RA of node: 296
2504 deg
Eccentricity:
0001695
Arg of perigee: 92
3356 deg
Mean anomaly: 267
7988 deg
Mean motion: 15
49194405 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 492
Checksum: 322
Coasting Arc #13 (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 = -2599177
53 A = 6803599
70 meter
Y = 6276756
40 meter E =
0012880
Z = -246298
39 I = 51
29721
XDOT = -4348
480118 Wp = 131
54315
YDOT = -2026
714987 meter/sec RA = 290
82967 deg
ZDOT = -5972
001561 TA = 51
11780
MA = 51
00298
Ha = 229
328 n
mi
Hp = 221
769
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8527485
32 X = -2667976
54
Y = 20593032
82 feet Y = 6247305
85 meter
Z = -808065
59 Z = -259091
46
XDOT = -14266
667055 XDOT = -4296
484895
YDOT = -6649
327384 feet/sec YDOT = -2075
052203 meter/sec
ZDOT = -19593
180974 ZDOT = -5992
998542
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19762216
39 X = 6023523
56
Y = -10302745
45 feet Y = -3140276
81 meter
Z = -867303
96 Z = -264354
25
XDOT = 5803
855583 XDOT = 1769
015182
YDOT = 12735
697152 feet/sec YDOT = 3881
840492 meter/sec
ZDOT = -19689
922910 ZDOT = -6001
488503
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
45401106
00016717 00000-0 10270-3 0 9123
2 25544 51
6426 291
4625 0001700 96
5616 263
5728 15
49221741 5077
Satellite: ISS
Catalog Number: 25544
Epoch time: 20253
45401106 = yrday
fracday
Element set: 912
Inclination: 51
6426 deg
RA of node: 291
4625 deg
Eccentricity:
0001700
Arg of perigee: 96
5616 deg
Mean anomaly: 263
5728 deg
Mean motion: 15
49221741 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 507
Checksum: 284
Coasting Arc #14 (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 = 2093502
82 A = 6803694
07 meter
Y = -6459697
60 meter E =
0013970
Z = 310508
74 I = 51
28668
XDOT = 4476
120561 Wp = 53
24710
YDOT = 1746
090967 meter/sec RA = 285
85636 deg
ZDOT = 5967
169250 TA = 310
10902
MA = 310
23137
Ha = 229
407 n
mi
Hp = 221
806
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6868447
57 X = 2164073
23
Y = -21193233
59 feet Y = -6435891
97 meter
Z = 1018729
45 Z = 320849
62
XDOT = 14685
434912 XDOT = 4427
277405
YDOT = 5728
644905 feet/sec YDOT = 1795
873092 meter/sec
ZDOT = 19577
326935 ZDOT = 5988
793904
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18669356
15 X = -5690419
76
Y = 12152527
31 feet Y = 3704090
32 meter
Z = 1066654
96 Z = 325116
43
XDOT = -6816
769449 XDOT = -2077
751328
YDOT = -12248
613837 feet/sec YDOT = -3733
377497 meter/sec
ZDOT = 19676
978877 ZDOT = 5997
543162
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
48610597
00016717 00000-0 10270-3 0 9134
2 25544 51
6429 286
3553 0001714 90
8432 269
2915 15
49185211 5231
Satellite: ISS
Catalog Number: 25544
Epoch time: 20254
48610597 = yrday
fracday
Element set: 913
Inclination: 51
6429 deg
RA of node: 286
3553 deg
Eccentricity:
0001714
Arg of perigee: 90
8432 deg
Mean anomaly: 269
2915 deg
Mean motion: 15
49185211 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 523
Checksum: 309
Coasting Arc #15 (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 = -3932482
61 A = 6792580
07 meter
Y = -1738067
35 meter E =
0015182
Z = -5272000
26 I = 51
24493
XDOT = 2316
825325 Wp = 94
66158
YDOT = -7259
025436 meter/sec RA = 283
68135 deg
ZDOT = 665
440739 TA = 181
74115
MA = 181
74645
Ha = 229
348 n
mi
Hp = 222
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12901845
82 X = -3887146
35
Y = -5702320
69 feet Y = -1781789
70 meter
Z = -17296588
77 Z = -5290992
63
XDOT = 7601
132956 XDOT = 2394
593403
YDOT = -23815
700250 feet/sec YDOT = -7232
682206 meter/sec
ZDOT = 2183
204523 ZDOT = 676
883883
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1055592
67 X = -321744
65
Y = -13957960
70 feet Y = -4254386
42 meter
Z = -17384105
59 Z = -5298675
38
XDOT = 23542
187659 XDOT = 7175
658798
YDOT = -4563
707574 feet/sec YDOT = -1391
018069 meter/sec
ZDOT = 2236
236198 ZDOT = 681
604793
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
87314047
00016717 00000-0 10270-3 0 9149
2 25544 51
6443 284
4425 0000605 82
9024 277
2195 15
48967645 5294
Satellite: ISS
Catalog Number: 25544
Epoch time: 20254
87314047 = yrday
fracday
Element set: 914
Inclination: 51
6443 deg
RA of node: 284
4425 deg
Eccentricity:
0000605
Arg of perigee: 82
9024 deg
Mean anomaly: 277
2195 deg
Mean motion: 15
48967645 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 529
Checksum: 317
Coasting Arc #16 (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 = 4061862
59 A = 6792487
23 meter
Y = 1386857
03 meter E =
0003499
Z = 5261915
32 I = 51
23747
XDOT = -1680
149080 Wp = 66
62791
YDOT = 7446
772007 meter/sec RA = 278
70931 deg
ZDOT = -664
023857 TA = 29
76267
MA = 29
74277
Ha = 229
118 n
mi
Hp = 222
569
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13326320
85 X = 4020493
14
Y = 4550055
86 feet Y = 1432048
37 meter
Z = 17263501
72 Z = 5281545
74
XDOT = -5512
300130 XDOT = -1760
070810
YDOT = 24431
666691 feet/sec YDOT = 7427
536507 meter/sec
ZDOT = -2178
555960 ZDOT = -672
379449
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2508038
91 X = 764450
26
Y = 13743050
74 feet Y = 4188881
86 meter
Z = 17353980
08 Z = 5289493
13
XDOT = -22987
365848 XDOT = -7006
549110
YDOT = 7002
094796 feet/sec YDOT = 2134
238494 meter/sec
ZDOT = -2217
339905 ZDOT = -675
845203
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
90541204
00016717 00000-0 10270-3 0 9152
2 25544 51
6436 279
3372 0000507 84
0225 276
0983 15
48994169 5458
Satellite: ISS
Catalog Number: 25544
Epoch time: 20255
90541204 = yrday
fracday
Element set: 915
Inclination: 51
6436 deg
RA of node: 279
3372 deg
Eccentricity:
0000507
Arg of perigee: 84
0225 deg
Mean anomaly: 276
0983 deg
Mean motion: 15
48994169 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 545
Checksum: 314
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