[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 8th 2020
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ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14262 1813 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
254/20:33:56
036 0
2 1
5 1
5
N/A -1
5 -0
1 229
4
000/00:03:48
073 0
0 -0
0 222
5
263/19:52:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
3
000/00:00:00
000 0
0 0
0 222
5
Coasting Arc #1 (Orbit 476)
---------------------------------------
Vector Time (GMT): 2020/251/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4442006
84 A = 6792547
47 meter
Y = -543784
27 meter E =
0015329
Z = -5123744
25 I = 51
28875
XDOT = 2656
332761 Wp = 79
04315
YDOT = -7000
708688 meter/sec RA = 300
39743 deg
ZDOT = -1561
050271 TA = 175
80097
MA = 175
78809
Ha = 229
407 n
mi
Hp = 221
624
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14573513
25 X = -4410707
63
Y = -1784069
12 feet Y = -593283
23 meter
Z = -16810184
55 Z = -5145245
81
XDOT = 8715
002496 XDOT = 2742
002083
YDOT = -22968
204357 feet/sec YDOT = -6970
524745 meter/sec
ZDOT = -5121
556008 ZDOT = -1547
938364
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13608001
43 X = 4147718
83
Y = 5200953
84 feet Y = 1585250
73 meter
Z = -16909313
17 Z = -5153958
65
XDOT = -13624
669149 XDOT = -4152
799157
YDOT = 19206
658410 feet/sec YDOT = 5854
189483 meter/sec
ZDOT = -5060
793062 ZDOT = -1542
529725
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
51882512
00016717 00000-0 10270-3 0 9009
2 25544 51
6429 301
0379 0001750 87
1061 273
0289 15
49195530 4779
Satellite: ISS
Catalog Number: 25544
Epoch time: 20251
51882512 = yrday
fracday
Element set: 900
Inclination: 51
6429 deg
RA of node: 301
0379 deg
Eccentricity:
0001750
Arg of perigee: 87
1061 deg
Mean anomaly: 273
0289 deg
Mean motion: 15
49195530 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 477
Checksum: 292
Coasting Arc #2 (Orbit 492)
---------------------------------------
Vector Time (GMT): 2020/252/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4437977
74 A = 6792387
20 meter
Y = 249934
41 meter E =
0006159
Z = 5131706
46 I = 51
27164
XDOT = -2118
777196 Wp = 114
94825
YDOT = 7215
872919 meter/sec RA = 295
42540 deg
ZDOT = 1476
957985 TA = 320
72787
MA = 320
77253
Ha = 229
233 n
mi
Hp = 221
739
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14560294
43 X = 4409926
04
Y = 819994
77 feet Y = 299406
39 meter
Z = 16836307
29 Z = 5153196
38
XDOT = -6951
368753 XDOT = -2206
484036
YDOT = 23674
123749 feet/sec YDOT = 7191
688887 meter/sec
ZDOT = 4845
662681 ZDOT = 1466
452464
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13897514
15 X = -4235962
31
Y = -4023355
25 feet Y = -1226318
68 meter
Z = 16935392
57 Z = 5161907
66
XDOT = 11797
574860 XDOT = 3595
900817
YDOT = -20505
505236 feet/sec YDOT = -6250
077996 meter/sec
ZDOT = 4796
923293 ZDOT = 1462
102220
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
55092531
00016717 00000-0 10270-3 0 9019
2 25544 51
6421 295
9313 0001794 89
4023 270
7332 15
49218908 4937
Satellite: ISS
Catalog Number: 25544
Epoch time: 20252
55092531 = yrday
fracday
Element set: 901
Inclination: 51
6421 deg
RA of node: 295
9313 deg
Eccentricity:
0001794
Arg of perigee: 89
4023 deg
Mean anomaly: 270
7332 deg
Mean motion: 15
49218908 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 493
Checksum: 300
Coasting Arc #3 (Orbit 507)
---------------------------------------
Vector Time (GMT): 2020/253/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4430652
24 A = 6792367
16 meter
Y = 27421
38 meter E =
0015602
Z = -5162218
15 I = 51
25890
XDOT = 1561
909297 Wp = 80
90344
YDOT = -7359
010741 meter/sec RA = 290
45146 deg
ZDOT = -1380
828694 TA = 175
72030
MA = 175
70694
Ha = 229
413 n
mi
Hp = 221
599
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14536260
62 X = -4405554
36
Y = 89965
15 feet Y = -21985
12 meter
Z = -16936411
25 Z = -5183679
66
XDOT = 5124
374334 XDOT = 1650
791188
YDOT = -24143
736026 feet/sec YDOT = -7341
047408 meter/sec
ZDOT = -4530
277869 ZDOT = -1373
025499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14128236
59 X = 4306286
51
Y = 2888231
71 feet Y = 880333
03 meter
Z = -17035376
16 Z = -5192382
65
XDOT = -9815
559738 XDOT = -2991
782608
YDOT = 21530
390408 feet/sec YDOT = 6562
462996 meter/sec
ZDOT = -4494
007442 ZDOT = -1369
773468
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
51852011
00016717 00000-0 10270-3 0 9024
2 25544 51
6430 291
1433 0001787 93
0779 267
0575 15
49200242 5086
Satellite: ISS
Catalog Number: 25544
Epoch time: 20253
51852011 = yrday
fracday
Element set: 902
Inclination: 51
6430 deg
RA of node: 291
1433 deg
Eccentricity:
0001787
Arg of perigee: 93
0779 deg
Mean anomaly: 267
0575 deg
Mean motion: 15
49200242 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 508
Checksum: 284
Coasting Arc #4 (Orbit 523)
---------------------------------------
Vector Time (GMT): 2020/254/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4390959
52 A = 6792212
72 meter
Y = -312216
27 meter E =
0005921
Z = 5168401
85 I = 51
24776
XDOT = -995
387612 Wp = 114
22229
YDOT = 7488
275160 meter/sec RA = 285
47719 deg
ZDOT = 1294
451359 TA = 323
24973
MA = 323
29031
Ha = 229
268 n
mi
Hp = 221
687
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14406035
16 X = 4369019
27
Y = -1024331
61 feet Y = -263236
07 meter
Z = 16956698
97 Z = 5189678
17
XDOT = -3265
707388 XDOT = -1085
337495
YDOT = 24567
831891 feet/sec YDOT = 7476
641089 meter/sec
ZDOT = 4246
887660 ZDOT = 1289
397631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14224866
18 X = -4335739
21
Y = -1702639
98 feet Y = -518964
67 meter
Z = 17054821
71 Z = 5198309
66
XDOT = 7765
958589 XDOT = 2367
064178
YDOT = -22461
408612 feet/sec YDOT = -6846
237345 meter/sec
ZDOT = 4223
305524 ZDOT = 1287
263524
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
55061864
00016717 00000-0 10270-3 0 9038
2 25544 51
6428 286
0364 0001916 91
8463 268
2906 15
49223889 5240
Satellite: ISS
Catalog Number: 25544
Epoch time: 20254
55061864 = yrday
fracday
Element set: 903
Inclination: 51
6428 deg
RA of node: 286
0364 deg
Eccentricity:
0001916
Arg of perigee: 91
8463 deg
Mean anomaly: 268
2906 deg
Mean motion: 15
49223889 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 524
Checksum: 322
Coasting Arc #5 (Orbit 528)
---------------------------------------
Vector Time (GMT): 2020/254/20:35:50
073
Vector Time (MET): N/A
Weight (LBS) : 922305
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3922948
21 A = 6792639
32 meter
Y = -1767889
95 meter E =
0015121
Z = -5269208
87 I = 51
24489
XDOT = 2337
115899 Wp = 94
79825
YDOT = -7249
955945 meter/sec RA = 283
67965 deg
ZDOT = 692
952506 TA = 181
87030
MA = 181
87596
Ha = 229
359 n
mi
Hp = 222
451
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12870564
99 X = -3877292
74
Y = -5800163
89 feet Y = -1811503
90 meter
Z = -17287430
68 Z = -5288154
15
XDOT = 7667
703082 XDOT = 2414
647415
YDOT = -23785
944702 feet/sec YDOT = -7223
387133 meter/sec
ZDOT = 2273
466226 ZDOT = 704
493640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -959764
19 X = -292536
13
Y = -13976631
90 feet Y = -4260077
40 meter
Z = -17374729
27 Z = -5295817
48
XDOT = 23544
308617 XDOT = 7176
305266
YDOT = -4507
482050 feet/sec YDOT = -1373
880529 meter/sec
ZDOT = 2326
949425 ZDOT = 709
254185
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
87315068
00016717 00000-0 10270-3 0 9042
2 25544 51
6443 284
4416 0000570 80
3263 279
7951 15
48951731 5298
Satellite: ISS
Catalog Number: 25544
Epoch time: 20254
87315068 = yrday
fracday
Element set: 904
Inclination: 51
6443 deg
RA of node: 284
4416 deg
Eccentricity:
0000570
Arg of perigee: 80
3263 deg
Mean anomaly: 279
7951 deg
Mean motion: 15
48951731 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 529
Checksum: 314
Coasting Arc #6 (Orbit 544)
---------------------------------------
Vector Time (GMT): 2020/255/20:35:50
073
Vector Time (MET): N/A
Weight (LBS) : 922305
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4056537
04 A = 6792547
63 meter
Y = 1410638
49 meter E =
0003509
Z = 5259807
77 I = 51
23741
XDOT = -1696
482126 Wp = 65
52174
YDOT = 7441
063977 meter/sec RA = 278
70778 deg
ZDOT = -685
459810 TA = 31
07620
MA = 31
05545
Ha = 229
132 n
mi
Hp = 222
611
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13308848
56 X = 4014912
29
Y = 4628079
04 feet Y = 1455768
85 meter
Z = 17256587
18 Z = 5279411
70
XDOT = -5565
886240 XDOT = -1776
234690
YDOT = 24412
939557 feet/sec YDOT = 7421
646775 meter/sec
ZDOT = -2248
883891 ZDOT = -693
894331
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2436512
05 X = 742648
87
Y = 13765222
80 feet Y = 4195639
91 meter
Z = 17346942
58 Z = 5287348
10
XDOT = -22992
853681 XDOT = -7008
221802
YDOT = 6960
594482 feet/sec YDOT = 2121
589198 meter/sec
ZDOT = -2288
031615 ZDOT = -697
392036
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
90543334
00016717 00000-0 10270-3 0 9057
2 25544 51
6436 279
3364 0000473 80
4722 279
6481 15
48976904 5452
Satellite: ISS
Catalog Number: 25544
Epoch time: 20255
90543334 = yrday
fracday
Element set: 905
Inclination: 51
6436 deg
RA of node: 279
3364 deg
Eccentricity:
0000473
Arg of perigee: 80
4722 deg
Mean anomaly: 279
6481 deg
Mean motion: 15
48976904 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 545
Checksum: 323
Coasting Arc #7 (Orbit 559)
---------------------------------------
Vector Time (GMT): 2020/256/20:35:50
073
Vector Time (MET): N/A
Weight (LBS) : 922305
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4173476
84 A = 6792618
92 meter
Y = -1041132
27 meter E =
0015046
Z = -5270360
19 I = 51
23328
XDOT = 1034
202885 Wp = 94
80524
YDOT = -7548
716162 meter/sec RA = 273
73547 deg
ZDOT = 672
681418 TA = 181
66862
MA = 181
67364
Ha = 229
319 n
mi
Hp = 222
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13692509
31 X = -4135924
16
Y = -3415788
28 feet Y = -1087593
13 meter
Z = -17291207
96 Z = -5290541
97
XDOT = 3393
054084 XDOT = 1115
270552
YDOT = -24766
129142 feet/sec YDOT = -7536
697684 meter/sec
ZDOT = 2206
960034 ZDOT = 677
902074
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3912761
64 X = -1192609
75
Y = -13439364
51 feet Y = -4096318
30 meter
Z = -17384247
80 Z = -5298718
73
XDOT = 22096
969620 XDOT = 6735
156340
YDOT = -9317
744262 feet/sec YDOT = -2840
048451 meter/sec
ZDOT = 2231
270676 ZDOT = 680
091302
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
87320083
00016717 00000-0 10270-3 0 9069
2 25544 51
6434 274
5503 0000468 81
6257 278
4945 15
48954203 5609
Satellite: ISS
Catalog Number: 25544
Epoch time: 20256
87320083 = yrday
fracday
Element set: 906
Inclination: 51
6434 deg
RA of node: 274
5503 deg
Eccentricity:
0000468
Arg of perigee: 81
6257 deg
Mean anomaly: 278
4945 deg
Mean motion: 15
48954203 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 560
Checksum: 312
Coasting Arc #8 (Orbit 575)
---------------------------------------
Vector Time (GMT): 2020/257/20:35:50
073
Vector Time (MET): N/A
Weight (LBS) : 922305
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4240829
72 A = 6792543
16 meter
Y = 666035
52 meter E =
0003327
Z = 5261547
66 I = 51
23265
XDOT = -369
835633 Wp = 66
14009
YDOT = 7624
713613 meter/sec RA = 268
76267 deg
ZDOT = -665
430948 TA = 30
26429
MA = 30
24507
Ha = 229
083 n
mi
Hp = 222
662
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13913483
32 X = 4207509
37
Y = 2185155
91 feet Y = 713273
32 meter
Z = 17262295
48 Z = 5282066
82
XDOT = -1213
371498 XDOT = -451
837732
YDOT = 25015
464610 feet/sec YDOT = 7620
119330 meter/sec
ZDOT = -2183
172402 ZDOT = -667
426768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5309420
73 X = 1618311
44
Y = 12918765
68 feet Y = 3937639
78 meter
Z = 17356909
71 Z = 5290386
08
XDOT = -21045
501944 XDOT = -6414
668993
YDOT = 11602
494596 feet/sec YDOT = 3536
440353 meter/sec
ZDOT = -2192
589928 ZDOT = -668
301410
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
90548310
00016717 00000-0 10270-3 0 9070
2 25544 51
6438 269
4446 0000340 84
9384 275
1805 15
48973938 5760
Satellite: ISS
Catalog Number: 25544
Epoch time: 20257
90548310 = yrday
fracday
Element set: 907
Inclination: 51
6438 deg
RA of node: 269
4446 deg
Eccentricity:
0000340
Arg of perigee: 84
9384 deg
Mean anomaly: 275
1805 deg
Mean motion: 15
48973938 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 576
Checksum: 334
Coasting Arc #9 (Orbit 590)
---------------------------------------
Vector Time (GMT): 2020/258/20:35:50
073
Vector Time (MET): N/A
Weight (LBS) : 922305
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4289660
10 A = 6792592
79 meter
Y = -283509
29 meter E =
0015009
Z = -5272218
47 I = 51
23408
XDOT = -300
213601 Wp = 94
42109
YDOT = -7614
966375 meter/sec RA = 263
78925 deg
ZDOT = 654
238045 TA = 181
87406
MA = 181
87969
Ha = 229
293 n
mi
Hp = 222
482
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14073687
99 X = -4260561
85
Y = -930148
60 feet Y = -331316
87 meter
Z = -17297304
68 Z = -5292985
04
XDOT = -984
952758 XDOT = -218
216324
YDOT = -24983
485482 feet/sec YDOT = -7617
865074 meter/sec
ZDOT = 2146
450280 ZDOT = 652
979222
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6676844
04 X = -2035102
06
Y = -12289478
02 feet Y = -3745832
90 meter
Z = -17393076
29 Z = -5301409
65
XDOT = 19679
332954 XDOT = 5998
260684
YDOT = -13719
373926 feet/sec YDOT = -4181
665173 meter/sec
ZDOT = 2140
831181 ZDOT = 652
525344
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
87324815
00016717 00000-0 10270-3 0 9080
2 25544 51
6433 264
6576 0000436 70
9510 289
1687 15
48958979 5916
Satellite: ISS
Catalog Number: 25544
Epoch time: 20258
87324815 = yrday
fracday
Element set: 908
Inclination: 51
6433 deg
RA of node: 264
6576 deg
Eccentricity:
0000436
Arg of perigee: 70
9510 deg
Mean anomaly: 289
1687 deg
Mean motion: 15
48958979 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 591
Checksum: 350
Coasting Arc #10 (Orbit 606)
---------------------------------------
Vector Time (GMT): 2020/259/20:35:50
073
Vector Time (MET): N/A
Weight (LBS) : 922305
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4289118
22 A = 6792568
41 meter
Y = -96229
57 meter E =
0003371
Z = 5263666
61 I = 51
23811
XDOT = 967
082048 Wp = 66
46823
YDOT = 7573
717237 meter/sec RA = 258
81643 deg
ZDOT = -647
914682 TA = 29
76663
MA = 29
74745
Ha = 229
126 n
mi
Hp = 222
657
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14071910
17 X = 4264307
89
Y = -315713
81 feet Y = -48403
94 meter
Z = 17269247
40 Z = 5284441
00
XDOT = 3172
841366 XDOT = 885
465756
YDOT = 24848
153666 feet/sec YDOT = 7584
075452 meter/sec
ZDOT = -2125
704336 ZDOT = -643
415771
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7927477
89 X = 2416295
26
Y = 11487155
53 feet Y = 3501285
01 meter
Z = 17365068
06 Z = 5292872
74
XDOT = -18175
692968 XDOT = -5539
951217
YDOT = 15733
795771 feet/sec YDOT = 4795
660951 meter/sec
ZDOT = -2105
113289 ZDOT = -641
638530
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 20259
90552948
00016717 00000-0 10270-3 0 9096
2 25544 51
6424 259
5517 0000416 78
2037 281
9159 15
48961498 6079
Satellite: ISS
Catalog Number: 25544
Epoch time: 20259
90552948 = yrday
fracday
Element set: 909
Inclination: 51
6424 deg
RA of node: 259
5517 deg
Eccentricity:
0000416
Arg of perigee: 78
2037 deg
Mean anomaly: 281
9159 deg
Mean motion: 15
48961498 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 607
Checksum: 339
Coasting Arc #11 (Orbit 621)
---------------------------------------
Vector Time (GMT): 2020/260/20:35:50
073
Vector Time (MET): N/A
Weight (LBS) : 922305
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4268833
39 A = 6792589
08 meter
Y = 481393
69 meter E =
0015003
Z = -5274758
82 I = 51
24505
XDOT = -1625
588943 Wp = 94
43122
YDOT = -7447
042349 meter/sec RA = 253
84356 deg
ZDOT = 636
373331 TA = 181
69061
MA = 181
69569
Ha = 229
287 n
mi
Hp = 222
496
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14005358
88 X = -4248277
61
Y = 1579375
62 feet Y = 433770
99 meter
Z = -17305639
19 Z = -5295445
12
XDOT = -5333
297058 XDOT = -1545
284176
YDOT = -24432
553638 feet/sec YDOT = -7464
771779 meter/sec
ZDOT = 2087
839013 ZDOT = 628
672629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9130127
37 X = -2782862
82
Y = -10581749
44 feet Y = -3225317
23 meter
Z = -17401063
34 Z = -5303844
10
XDOT = 16397
614216 XDOT = 4997
992813
YDOT = -17520
951647 feet/sec YDOT = -5340
386062 meter/sec
ZDOT = 2052
451745 ZDOT = 625
587292
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 20260
87329457
00016717 00000-0 10270-3 0 9103
2 25544 51
6416 254
7645 0000402 73
9586 286
1608 15
48956547 6227
Satellite: ISS
Catalog Number: 25544
Epoch time: 20260
87329457 = yrday
fracday
Element set: 910
Inclination: 51
6416 deg
RA of node: 254
7645 deg
Eccentricity:
0000402
Arg of perigee: 73
9586 deg
Mean anomaly: 286
1608 deg
Mean motion: 15
48956547 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 622
Checksum: 324
Coasting Arc #12 (Orbit 637)
---------------------------------------
Vector Time (GMT): 2020/261/20:35:50
073
Vector Time (MET): N/A
Weight (LBS) : 922305
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4200398
07 A = 6792588
99 meter
Y = -854646
50 meter E =
0003238
Z = 5266834
99 I = 51
25654
XDOT = 2275
134525 Wp = 66
34425
YDOT = 7289
830414 meter/sec RA = 248
87175 deg
ZDOT = -629
959557 TA = 29
71555
MA = 29
69716
Ha = 229
109 n
mi
Hp = 222
712
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13780833
56 X = 4184059
55
Y = -2803958
33 feet Y = -807765
45 meter
Z = 17279642
34 Z = 5287199
26
XDOT = 7464
352117 XDOT = 2196
508336
YDOT = 23916
766450 feet/sec YDOT = 7314
832907 meter/sec
ZDOT = -2066
796446 ZDOT = -619
099574
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10180767
62 X = 3103097
97
Y = 9532575
69 feet Y = 2905529
07 meter
Z = 17373588
20 Z = 5295469
68
XDOT = -14506
746173 XDOT = -4421
656233
YDOT = 19178
336078 feet/sec YDOT = 5845
556837 meter/sec
ZDOT = -2016
811606 ZDOT = -614
724177
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 20261
90557580
00016717 00000-0 10270-3 0 9119
2 25544 51
6425 249
6585 0000317 72
7659 287
3526 15
48950655 6389
Satellite: ISS
Catalog Number: 25544
Epoch time: 20261
90557580 = yrday
fracday
Element set: 911
Inclination: 51
6425 deg
RA of node: 249
6585 deg
Eccentricity:
0000317
Arg of perigee: 72
7659 deg
Mean anomaly: 287
3526 deg
Mean motion: 15
48950655 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 638
Checksum: 332
Coasting Arc #13 (Orbit 652)
---------------------------------------
Vector Time (GMT): 2020/262/20:35:50
073
Vector Time (MET): N/A
Weight (LBS) : 922305
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4112160
23 A = 6792574
07 meter
Y = 1228372
22 meter E =
0014977
Z = -5278119
23 I = 51
26919
XDOT = -2900
734365 Wp = 94
16607
YDOT = -7050
408760 meter/sec RA = 243
89917 deg
ZDOT = 619
576374 TA = 181
79133
MA = 181
79670
Ha = 229
270 n
mi
Hp = 222
515
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13491339
33 X = -4099952
41
Y = 4030092
57 feet Y = 1182454
82 meter
Z = -17316664
13 Z = -5298065
07
XDOT = -9516
845028 XDOT = -2824
688547
YDOT = -23131
262336 feet/sec YDOT = -7082
421590 meter/sec
ZDOT = 2032
730887 ZDOT = 605
671083
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11160311
75 X = -3401663
02
Y = -8397013
41 feet Y = -2559409
69 meter
Z = -17408685
97 Z = -5306167
48
XDOT = 12397
181606 XDOT = 3778
660953
YDOT = -20555
192494 feet/sec YDOT = -6265
222672 meter/sec
ZDOT = 1968
676813 ZDOT = 600
052693
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 20262
87333844
00016717 00000-0 10270-3 0 9122
2 25544 51
6419 244
8701 0000379 65
8997 294
2193 15
48958095 6535
Satellite: ISS
Catalog Number: 25544
Epoch time: 20262
87333844 = yrday
fracday
Element set: 912
Inclination: 51
6419 deg
RA of node: 244
8701 deg
Eccentricity:
0000379
Arg of perigee: 65
8997 deg
Mean anomaly: 294
2193 deg
Mean motion: 15
48958095 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 653
Checksum: 341
Coasting Arc #14 (Orbit 667)
---------------------------------------
Vector Time (GMT): 2020/263/19:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 922305
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4472095
62 A = 6793340
80 meter
Y = 492944
57 meter E =
0013795
Z = -5102341
12 I = 51
28728
XDOT = -2647
023519 Wp = 101
59614
YDOT = -6985
491480 meter/sec RA = 239
07283 deg
ZDOT = 1646
265345 TA = 184
40818
MA = 184
42034
Ha = 229
284 n
mi
Hp = 222
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14672229
73 X = -4452491
00
Y = 1617272
23 feet Y = 443043
57 meter
Z = -16739964
32 Z = -5124017
45
XDOT = -8684
460364 XDOT = -2576
709613
YDOT = -22918
279133 feet/sec YDOT = -7014
699103 meter/sec
ZDOT = 5401
133023 ZDOT = 1633
578395
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7892937
75 X = -2405767
43
Y = -12338292
45 feet Y = -3760711
54 meter
Z = -16839963
57 Z = -5132820
90
XDOT = 15790
923154 XDOT = 4813
073377
YDOT = -17388
782948 feet/sec YDOT = -5300
101043 meter/sec
ZDOT = 5342
683103 ZDOT = 1628
449810
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 20263
84110149
00016717 00000-0 10270-3 0 9132
2 25544 51
6419 240
0840 0000410 68
1889 291
9304 15
48955024 6682
Satellite: ISS
Catalog Number: 25544
Epoch time: 20263
84110149 = yrday
fracday
Element set: 913
Inclination: 51
6419 deg
RA of node: 240
0840 deg
Eccentricity:
0000410
Arg of perigee: 68
1889 deg
Mean anomaly: 291
9304 deg
Mean motion: 15
48955024 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 668
Checksum: 298
Coasting Arc #15 (Orbit 683)
---------------------------------------
Vector Time (GMT): 2020/264/19:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 922305
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4402236
00 A = 6793313
48 meter
Y = -878848
05 meter E =
0005272
Z = 5095652
19 I = 51
30614
XDOT = 3253
014118 Wp = 56
12133
YDOT = 6740
281811 meter/sec RA = 234
10505 deg
ZDOT = -1643
732595 TA = 49
85438
MA = 49
80821
Ha = 229
091 n
mi
Hp = 222
706
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14443031
50 X = 4386984
30
Y = -2883359
75 feet Y = -829704
06 meter
Z = 16718019
01 Z = 5116999
80
XDOT = 10672
618499 XDOT = 3185
384898
YDOT = 22113
785470 feet/sec YDOT = 6776
281106 meter/sec
ZDOT = -5392
823476 ZDOT = -1628
095214
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9124610
65 X = 2781181
33
Y = 11417244
74 feet Y = 3479976
20 meter
Z = 16816512
27 Z = 5125672
94
XDOT = -13920
954309 XDOT = -4243
106873
YDOT = 18982
278178 feet/sec YDOT = 5785
798389 meter/sec
ZDOT = -5320
745793 ZDOT = -1621
763318
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 20264
87338180
00016717 00000-0 10270-3 0 9144
2 25544 51
6424 234
9790 0000295 69
2239 290
8942 15
48958652 6840
Satellite: ISS
Catalog Number: 25544
Epoch time: 20264
87338180 = yrday
fracday
Element set: 914
Inclination: 51
6424 deg
RA of node: 234
9790 deg
Eccentricity:
0000295
Arg of perigee: 69
2239 deg
Mean anomaly: 290
8942 deg
Mean motion: 15
48958652 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 684
Checksum: 338
Coasting Arc #16 (Orbit 698)
---------------------------------------
Vector Time (GMT): 2020/265/19:52:00
000
Vector Time (MET): N/A
Weight (LBS) : 922305
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4307243
77 A = 6793308
51 meter
Y = 1271821
73 meter E =
0013743
Z = -5109382
31 I = 51
32624
XDOT = -3827
944474 Wp = 101
86872
YDOT = -6419
060725 meter/sec RA = 229
13662 deg
ZDOT = 1630
127042 TA = 183
96616
MA = 183
97706
Ha = 229
241 n
mi
Hp = 222
550
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14131377
19 X = -4296326
79
Y = 4172643
46 feet Y = 1223715
89 meter
Z = -16763065
32 Z = -5130278
99
XDOT = -12558
872945 XDOT = -3763
798421
YDOT = -21059
910515 feet/sec YDOT = -6461
508818 meter/sec
ZDOT = 5348
185832 ZDOT = 1611
688214
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10307827
24 X = -3141825
74
Y = -10373688
79 feet Y = -3161900
34 meter
Z = -16859490
27 Z = -5138772
63
XDOT = 11836
073708 XDOT = 3607
635266
YDOT = -20309
570436 feet/sec YDOT = -6190
357069 meter/sec
ZDOT = 5263
164797 ZDOT = 1604
212630
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 20265
84114449
00016717 00000-0 10270-3 0 9153
2 25544 51
6418 230
1912 0000285 72
7070 287
4111 15
48957230 6995
Satellite: ISS
Catalog Number: 25544
Epoch time: 20265
84114449 = yrday
fracday
Element set: 915
Inclination: 51
6418 deg
RA of node: 230
1912 deg
Eccentricity:
0000285
Arg of perigee: 72
7070 deg
Mean anomaly: 287
4111 deg
Mean motion: 15
48957230 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 699
Checksum: 302
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