[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 26th 2020
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ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16490 3108 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 475 ET - UTC (sec) : 68 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
238/20:27:30
000 0
0 0
0 0
0
N/A 0
0 0
0 229
4
000/00:00:00
000 0
0 0
0 221
8
245/23:00:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
4
000/00:00:00
000 0
0 0
0 221
8
249/11:15:00
000 0
0 0
0 0
0
N/A 0
0 0
0 229
1
000/00:00:00
000 0
0 0
0 221
8
Coasting Arc #1 (Orbit 259)
---------------------------------------
Vector Time (GMT): 2020/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2363839
79 A = 6794119
29 meter
Y = -4233354
78 meter E =
0012546
Z = -4771387
74 I = 51
69947
XDOT = 7099
467029 Wp = 69
98379
YDOT = -930
251770 meter/sec RA = 9
81777 deg
ZDOT = -2693
444219 TA = 173
36766
MA = 173
35104
Ha = 229
241 n
mi
Hp = 221
950
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7755379
88 X = -2293148
86
Y = -13888959
25 feet Y = -4259393
72 meter
Z = -15654159
26 Z = -4782698
58
XDOT = 23292
214661 XDOT = 7122
424907
YDOT = -3052
007121 feet/sec YDOT = -850
732113 meter/sec
ZDOT = -8836
759250 ZDOT = -2658
902127
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 321324
30 X = 97939
65
Y = 15852973
94 feet Y = 4831986
46 meter
Z = -15706106
34 Z = -4787221
21
XDOT = -20941
782088 XDOT = -6383
055181
YDOT = -8167
291743 feet/sec YDOT = -2489
390523 meter/sec
ZDOT = -8677
276845 ZDOT = -2644
833982
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20237
52084312
00016717 00000-0 10270-3 0 9006
2 25544 51
6432 10
2947 0001355 62
5167 297
6121 15
49180070 2608
Satellite: ISS
Catalog Number: 25544
Epoch time: 20237
52084312 = yrday
fracday
Element set: 900
Inclination: 51
6432 deg
RA of node: 10
2947 deg
Eccentricity:
0001355
Arg of perigee: 62
5167 deg
Mean anomaly: 297
6121 deg
Mean motion: 15
49180070 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 260
Checksum: 268
Coasting Arc #2 (Orbit 275)
---------------------------------------
Vector Time (GMT): 2020/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2643917
77 A = 6793907
92 meter
Y = 4024483
23 meter E =
0008188
Z = 4787357
85 I = 51
66667
XDOT = -7042
375067 Wp = 110
94495
YDOT = 1488
128544 meter/sec RA = 4
87284 deg
ZDOT = 2631
806155 TA = 313
05850
MA = 313
12702
Ha = 229
114 n
mi
Hp = 221
971
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8674270
90 X = 2575464
12
Y = 13203685
14 feet Y = 4053666
61 meter
Z = 15706554
63 Z = 4800034
71
XDOT = -23104
905076 XDOT = -7071
276131
YDOT = 4882
311496 feet/sec YDOT = 1409
214043 meter/sec
ZDOT = 8634
534630 ZDOT = 2597
526988
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1722414
84 X = -524992
04
Y = -15645450
56 feet Y = -4768733
33 meter
Z = 15764812
06 Z = 4805114
71
XDOT = 21747
318132 XDOT = 6628
582567
YDOT = 6168
142250 feet/sec YDOT = 1880
049758 meter/sec
ZDOT = 8476
241625 ZDOT = 2583
558447
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20238
55296258
00016717 00000-0 10270-3 0 9015
2 25544 51
6443 5
1875 0001304 64
4486 295
6799 15
49213573 2763
Satellite: ISS
Catalog Number: 25544
Epoch time: 20238
55296258 = yrday
fracday
Element set: 901
Inclination: 51
6443 deg
RA of node: 5
1875 deg
Eccentricity:
0001304
Arg of perigee: 64
4486 deg
Mean anomaly: 295
6799 deg
Mean motion: 15
49213573 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 276
Checksum: 322
Coasting Arc #3 (Orbit 280)
---------------------------------------
Vector Time (GMT): 2020/238/20:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4100534
74 A = 6796443
91 meter
Y = -3506426
71 meter E =
0009444
Z = -4143172
57 I = 51
66112
XDOT = 6094
874899 Wp = 67
54618
YDOT = -2661
885447 meter/sec RA = 3
13872 deg
ZDOT = -3782
753303 TA = 163
39569
MA = 163
36475
Ha = 229
367 n
mi
Hp = 221
816
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13453197
98 X = -4040894
99
Y = -11504024
64 feet Y = -3551948
28 meter
Z = -13593085
86 Z = -4162946
49
XDOT = 19996
308723 XDOT = 6142
562297
YDOT = -8733
219970 feet/sec YDOT = -2593
461492 meter/sec
ZDOT = -12410
607948 ZDOT = -3753
031125
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8869355
48 X = 2703379
55
Y = -15237530
21 feet Y = -4644399
21 meter
Z = -13684126
15 Z = -4170921
65
XDOT = 11145
382633 XDOT = 3397
112627
YDOT = 17499
560412 feet/sec YDOT = 5333
866013 meter/sec
ZDOT = -12273
275987 ZDOT = -3740
894521
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20238
87550004
00016717 00000-0 10270-3 0 9023
2 25544 51
6425 3
5956 0001793 57
2989 302
8334 15
49176915 2815
Satellite: ISS
Catalog Number: 25544
Epoch time: 20238
87550004 = yrday
fracday
Element set: 902
Inclination: 51
6425 deg
RA of node: 3
5956 deg
Eccentricity:
0001793
Arg of perigee: 57
2989 deg
Mean anomaly: 302
8334 deg
Mean motion: 15
49176915 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 281
Checksum: 312
Coasting Arc #4 (Orbit 296)
---------------------------------------
Vector Time (GMT): 2020/239/20:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4322668
47 A = 6796265
36 meter
Y = 3167881
05 meter E =
0011356
Z = 4170840
49 I = 51
62593
XDOT = -5912
065633 Wp = 97
97498
YDOT = 3142
110449 meter/sec RA = 358
19187 deg
ZDOT = 3730
494350 TA = 313
59934
MA = 313
69352
Ha = 229
215 n
mi
Hp = 221
905
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14181983
16 X = 4266663
59
Y = 10393310
52 feet Y = 3215906
94 meter
Z = 13683859
88 Z = 4191702
25
XDOT = -19396
540790 XDOT = -5964
882741
YDOT = 10308
761314 feet/sec YDOT = 3075
702064 meter/sec
ZDOT = 12239
154690 ZDOT = 3701
647865
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7372222
86 X = -2247053
53
Y = 15879586
70 feet Y = 4840098
03 meter
Z = 13779935
68 Z = 4200124
40
XDOT = -12832
742482 XDOT = -3911
419909
YDOT = -16491
859899 feet/sec YDOT = -5026
718897 meter/sec
ZDOT = 12105
840402 ZDOT = 3689
860154
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20239
90761717
00016717 00000-0 10270-3 0 9034
2 25544 51
6415 358
4893 0001708 55
0542 305
0768 15
49194867 2972
Satellite: ISS
Catalog Number: 25544
Epoch time: 20239
90761717 = yrday
fracday
Element set: 903
Inclination: 51
6415 deg
RA of node: 358
4893 deg
Eccentricity:
0001708
Arg of perigee: 55
0542 deg
Mean anomaly: 305
0768 deg
Mean motion: 15
49194867 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 297
Checksum: 330
Coasting Arc #5 (Orbit 311)
---------------------------------------
Vector Time (GMT): 2020/240/20:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4509978
09 A = 6796141
13 meter
Y = -2840398
22 meter E =
0009920
Z = -4227085
08 I = 51
59122
XDOT = 5682
976603 Wp = 67
63660
YDOT = -3590
601311 meter/sec RA = 353
24170 deg
ZDOT = -3653
791313 TA = 164
82953
MA = 164
79977
Ha = 229
385 n
mi
Hp = 221
782
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14796516
05 X = -4457348
18
Y = -9318891
79 feet Y = -2890537
59 meter
Z = -13868389
36 Z = -4248864
82
XDOT = 18644
936362 XDOT = 5740
453247
YDOT = -11780
188028 feet/sec YDOT = -3526
728696 meter/sec
ZDOT = -11987
504307 ZDOT = -3626
046473
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5916299
13 X = 1803287
98
Y = -16370191
68 feet Y = -4989634
43 meter
Z = -13968718
04 Z = -4257665
26
XDOT = 14361
292763 XDOT = 4377
322034
YDOT = 15300
901185 feet/sec YDOT = 4663
714681 meter/sec
ZDOT = -11859
252622 ZDOT = -3614
700199
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20240
87522716
00016717 00000-0 10270-3 0 9047
2 25544 51
6411 353
7013 0001805 60
0450 300
0879 15
49175605 3127
Satellite: ISS
Catalog Number: 25544
Epoch time: 20240
87522716 = yrday
fracday
Element set: 904
Inclination: 51
6411 deg
RA of node: 353
7013 deg
Eccentricity:
0001805
Arg of perigee: 60
0450 deg
Mean anomaly: 300
0879 deg
Mean motion: 15
49175605 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 312
Checksum: 268
Coasting Arc #6 (Orbit 327)
---------------------------------------
Vector Time (GMT): 2020/241/20:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4675637
60 A = 6795887
78 meter
Y = 2480042
42 meter E =
0011037
Z = 4254732
33 I = 51
55786
XDOT = -5427
339400 Wp = 100
44246
YDOT = 4041
918630 meter/sec RA = 348
29040 deg
ZDOT = 3598
333677 TA = 312
68211
MA = 312
77503
Ha = 229
156 n
mi
Hp = 221
867
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15340018
38 X = 4626890
78
Y = 8136622
10 feet Y = 2532056
05 meter
Z = 13959095
58 Z = 4277326
09
XDOT = -17806
231627 XDOT = -5489
612359
YDOT = 13260
887895 feet/sec YDOT = 3980
877938 meter/sec
ZDOT = 11805
556683 ZDOT = 3571
819063
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4357562
14 X = -1328184
94
Y = 16721697
91 feet Y = 5096773
52 meter
Z = 14063200
34 Z = 4286463
46
XDOT = -15847
942085 XDOT = -4830
452748
YDOT = -13982
577098 feet/sec YDOT = -4261
889500 meter/sec
ZDOT = 11682
962694 ZDOT = 3560
967029
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
90734045
00016717 00000-0 10270-3 0 9053
2 25544 51
6416 348
5952 0001608 60
9506 299
1805 15
49218088 3285
Satellite: ISS
Catalog Number: 25544
Epoch time: 20241
90734045 = yrday
fracday
Element set: 905
Inclination: 51
6416 deg
RA of node: 348
5952 deg
Eccentricity:
0001608
Arg of perigee: 60
9506 deg
Mean anomaly: 299
1805 deg
Mean motion: 15
49218088 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 328
Checksum: 312
Coasting Arc #7 (Orbit 342)
---------------------------------------
Vector Time (GMT): 2020/242/20:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4808489
91 A = 6795780
16 meter
Y = -2137099
97 meter E =
0010442
Z = -4311325
92 I = 51
52522
XDOT = 5130
717856 Wp = 67
93240
YDOT = -4453
931797 meter/sec RA = 343
33511 deg
ZDOT = -3517
609284 TA = 166
11804
MA = 166
08931
Ha = 229
386 n
mi
Hp = 221
709
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15775885
54 X = -4763293
28
Y = -7011482
83 feet Y = -2190619
16 meter
Z = -14144770
07 Z = -4334573
51
XDOT = 16833
063832 XDOT = 5197
227955
YDOT = -14612
637128 feet/sec YDOT = -4396
184501 meter/sec
ZDOT = -11540
712873 ZDOT = -3492
525256
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2871242
78 X = 875154
80
Y = -16933782
48 feet Y = -5161416
90 meter
Z = -14251910
48 Z = -4343982
31
XDOT = 17141
119784 XDOT = 5224
613310
YDOT = 12513
430827 feet/sec YDOT = 3814
093716 meter/sec
ZDOT = -11424
706570 ZDOT = -3482
250563
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
87494598
00016717 00000-0 10270-3 0 9067
2 25544 51
6424 343
8068 0001852 63
0385 297
0954 15
49192555 3439
Satellite: ISS
Catalog Number: 25544
Epoch time: 20242
87494598 = yrday
fracday
Element set: 906
Inclination: 51
6424 deg
RA of node: 343
8068 deg
Eccentricity:
0001852
Arg of perigee: 63
0385 deg
Mean anomaly: 297
0954 deg
Mean motion: 15
49192555 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 343
Checksum: 330
Coasting Arc #8 (Orbit 358)
---------------------------------------
Vector Time (GMT): 2020/243/20:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4915699
77 A = 6795524
50 meter
Y = 1765630
99 meter E =
0010769
Z = 4339384
47 I = 51
49254
XDOT = -4808
134645 Wp = 102
15955
YDOT = 4864
978633 meter/sec RA = 338
37965 deg
ZDOT = 3457
715619 TA = 312
58880
MA = 312
67960
Ha = 229
151 n
mi
Hp = 221
805
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16127623
92 X = 4874512
78
Y = 5792752
58 feet Y = 1820371
59 meter
Z = 14236825
69 Z = 4363162
50
XDOT = -15774
719965 XDOT = -4878
974219
YDOT = 15961
215988 feet/sec YDOT = 4810
814557 meter/sec
ZDOT = 11344
211349 ZDOT = 3434
187974
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1311312
56 X = -399688
07
Y = 16994227
65 feet Y = 5179840
59 meter
Z = 14346432
57 Z = 4372792
65
XDOT = -18370
188414 XDOT = -5599
233428
YDOT = -10928
443022 feet/sec YDOT = -3330
989433 meter/sec
ZDOT = 11235
376643 ZDOT = 3424
542801
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
90705378
00016717 00000-0 10270-3 0 9074
2 25544 51
6422 338
7011 0001669 64
4855 295
6467 15
49234178 3599
Satellite: ISS
Catalog Number: 25544
Epoch time: 20243
90705378 = yrday
fracday
Element set: 907
Inclination: 51
6422 deg
RA of node: 338
7011 deg
Eccentricity:
0001669
Arg of perigee: 64
4855 deg
Mean anomaly: 295
6467 deg
Mean motion: 15
49234178 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 359
Checksum: 327
Coasting Arc #9 (Orbit 373)
---------------------------------------
Vector Time (GMT): 2020/244/20:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4995434
81 A = 6795439
42 meter
Y = -1415497
04 meter E =
0010904
Z = -4395256
58 I = 51
46075
XDOT = 4448
318745 Wp = 68
39471
YDOT = -5230
770136 meter/sec RA = 333
42034 deg
ZDOT = -3374
009397 TA = 167
29866
MA = 167
27116
Ha = 229
376 n
mi
Hp = 221
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16389221
82 X = -4957885
81
Y = -4644019
18 feet Y = -1471149
74 meter
Z = -14420133
14 Z = -4419430
73
XDOT = 14594
221604 XDOT = 4522
868866
YDOT = -17161
319343 feet/sec YDOT = -5180
609107 meter/sec
ZDOT = -11069
584637 ZDOT = -3352
220425
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -156642
49 X = -47744
63
Y = -16938780
81 feet Y = -5162940
39 meter
Z = -14531583
32 Z = -4429226
60
XDOT = 19377
267692 XDOT = 5906
191193
YDOT = 9222
849142 feet/sec YDOT = 2811
124418 meter/sec
ZDOT = -10968
768174 ZDOT = -3343
280539
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
87465680
00016717 00000-0 10270-3 0 9081
2 25544 51
6419 333
9132 0001834 65
7889 294
3452 15
49201807 3741
Satellite: ISS
Catalog Number: 25544
Epoch time: 20244
87465680 = yrday
fracday
Element set: 908
Inclination: 51
6419 deg
RA of node: 333
9132 deg
Eccentricity:
0001834
Arg of perigee: 65
7889 deg
Mean anomaly: 294
3452 deg
Mean motion: 15
49201807 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 374
Checksum: 326
Coasting Arc #10 (Orbit 389)
---------------------------------------
Vector Time (GMT): 2020/245/20:27:30
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5046002
96 A = 6795179
10 meter
Y = 1041265
99 meter E =
0010420
Z = 4423106
16 I = 51
43145
XDOT = -4063
820589 Wp = 104
58971
YDOT = 5591
599823 meter/sec RA = 328
46049 deg
ZDOT = 3310
643201 TA = 311
82898
MA = 311
91791
Ha = 229
119 n
mi
Hp = 221
790
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16555127
83 X = 5012499
65
Y = 3416227
02 feet Y = 1097506
90 meter
Z = 14511503
15 Z = 4447535
81
XDOT = -13332
744714 XDOT = -4142
126433
YDOT = 18345
143777 feet/sec YDOT = 5545
717595 meter/sec
ZDOT = 10861
690292 ZDOT = 3290
712648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1668913
67 X = 508684
89
Y = 16723505
95 feet Y = 5097324
61 meter
Z = 14624146
62 Z = 4457439
89
XDOT = -20299
556378 XDOT = -6187
304784
YDOT = -7417
728406 feet/sec YDOT = -2260
923618 meter/sec
ZDOT = 10769
446719 ZDOT = 3282
527360
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
90676121
00016717 00000-0 10270-3 0 9091
2 25544 51
6428 328
8075 0001603 70
2551 289
8772 15
49244273 3907
Satellite: ISS
Catalog Number: 25544
Epoch time: 20245
90676121 = yrday
fracday
Element set: 909
Inclination: 51
6428 deg
RA of node: 328
8075 deg
Eccentricity:
0001603
Arg of perigee: 70
2551 deg
Mean anomaly: 289
8772 deg
Mean motion: 15
49244273 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 390
Checksum: 312
Coasting Arc #11 (Orbit 390)
---------------------------------------
Vector Time (GMT): 2020/245/23:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -419841
42 A = 6792849
81 meter
Y = -4513177
82 meter E =
0014510
Z = -5072505
39 I = 51
42155
XDOT = 6941
926919 Wp = 99
03638
YDOT = -2663
023705 meter/sec RA = 327
89690 deg
ZDOT = 1796
999156 TA = 188
43958
MA = 188
46401
Ha = 229
357 n
mi
Hp = 221
785
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1377432
48 X = -344703
61
Y = -14807013
83 feet Y = -4517452
92 meter
Z = -16642078
06 Z = -5074362
06
XDOT = 22775
350784 XDOT = 6962
461073
YDOT = -8736
954412 feet/sec YDOT = -2585
279202 meter/sec
ZDOT = 5895
666523 ZDOT = 1830
769733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7309976
90 X = 2228080
96
Y = -12939554
69 feet Y = -3943976
27 meter
Z = -16650402
49 Z = -5075042
68
XDOT = 22756
698024 XDOT = 6936
241558
YDOT = 5078
137452 feet/sec YDOT = 1547
816295 meter/sec
ZDOT = 6051
598151 ZDOT = 1844
527116
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
97126965
00016717 00000-0 10270-3 0 9106
2 25544 51
6443 328
4885 0001778 65
7932 294
3404 15
49207194 3919
Satellite: ISS
Catalog Number: 25544
Epoch time: 20245
97126965 = yrday
fracday
Element set: 910
Inclination: 51
6443 deg
RA of node: 328
4885 deg
Eccentricity:
0001778
Arg of perigee: 65
7932 deg
Mean anomaly: 294
3404 deg
Mean motion: 15
49207194 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 391
Checksum: 329
Coasting Arc #12 (Orbit 406)
---------------------------------------
Vector Time (GMT): 2020/246/23:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 709693
03 A = 6792882
22 meter
Y = 4500860
92 meter E =
0007520
Z = 5033640
48 I = 51
39384
XDOT = -6712
469741 Wp = 58
07728
YDOT = 3178
957209 meter/sec RA = 322
93421 deg
ZDOT = -1890
110626 TA = 50
35277
MA = 50
28645
Ha = 229
301 n
mi
Hp = 221
770
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2328389
19 X = 634860
10
Y = 14766604
08 feet Y = 4508379
13 meter
Z = 16514568
51 Z = 5036905
80
XDOT = -22022
538519 XDOT = -6738
337965
YDOT = 10429
649637 feet/sec YDOT = 3103
748803 meter/sec
ZDOT = -6201
150347 ZDOT = -1922
779751
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6269075
71 X = -1910814
28
Y = 13552954
55 feet Y = 4130940
55 meter
Z = 16529400
41 Z = 5038161
25
XDOT = -23105
140308 XDOT = -7042
446766
YDOT = -2916
620808 feet/sec YDOT = -888
986022 meter/sec
ZDOT = -6352
009034 ZDOT = -1936
092354
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
00337181
00016717 00000-0 10270-3 0 9117
2 25544 51
6441 323
3826 0001798 66
3115 293
8224 15
49232560 4075
Satellite: ISS
Catalog Number: 25544
Epoch time: 20247
00337181 = yrday
fracday
Element set: 911
Inclination: 51
6441 deg
RA of node: 323
3826 deg
Eccentricity:
0001798
Arg of perigee: 66
3115 deg
Mean anomaly: 293
8224 deg
Mean motion: 15
49232560 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 407
Checksum: 286
Coasting Arc #13 (Orbit 421)
---------------------------------------
Vector Time (GMT): 2020/247/23:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1022178
78 A = 6793043
75 meter
Y = -4477798
39 meter E =
0014304
Z = -5018009
40 I = 51
36813
XDOT = 6417
787757 Wp = 100
28869
YDOT = -3667
676046 meter/sec RA = 317
96858 deg
ZDOT = 1967
822647 TA = 188
92596
MA = 188
95142
Ha = 229
390 n
mi
Hp = 221
707
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3353604
92 X = -947656
34
Y = -14690939
59 feet Y = -4488812
80 meter
Z = -16463285
44 Z = -5022793
37
XDOT = 21055
734111 XDOT = 6448
765366
YDOT = -12033
057894 feet/sec YDOT = -3595
734396 meter/sec
ZDOT = 6456
111045 ZDOT = 1999
072948
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5128325
71 X = 1563113
68
Y = -14143933
82 feet Y = -4311071
03 meter
Z = -16485131
20 Z = -5024667
99
XDOT = 23156
923313 XDOT = 7058
230226
YDOT = 712
091101 feet/sec YDOT = 217
045368 meter/sec
ZDOT = 6600
430428 ZDOT = 2011
811195
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
97096720
00016717 00000-0 10270-3 0 9125
2 25544 51
6443 318
5948 0001861 70
3154 289
8197 15
49213832 4229
Satellite: ISS
Catalog Number: 25544
Epoch time: 20247
97096720 = yrday
fracday
Element set: 912
Inclination: 51
6443 deg
RA of node: 318
5948 deg
Eccentricity:
0001861
Arg of perigee: 70
3154 deg
Mean anomaly: 289
8197 deg
Mean motion: 15
49213832 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 422
Checksum: 318
Coasting Arc #14 (Orbit 437)
---------------------------------------
Vector Time (GMT): 2020/248/23:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 922462
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1312964
14 A = 6793056
25 meter
Y = 4428514
05 meter E =
0007850
Z = 4976308
94 I = 51
34358
XDOT = -6113
268414 Wp = 59
93972
YDOT = 4136
711409 meter/sec RA = 313
00207 deg
ZDOT = -2062
088913 TA = 50
24927
MA = 50
18013
Ha = 229
248 n
mi
Hp = 221
741
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4307625
12 X = 1239173
64
Y = 14529245
57 feet Y = 4442784
33 meter
Z = 16326472
89 Z = 4982507
22
XDOT = -20056
654901 XDOT = -6149
055616
YDOT = 13571
887824 feet/sec YDOT = 4068
148211 meter/sec
ZDOT = -6765
383574 ZDOT = -2091
871850
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3984842
75 X = -1214580
07
Y = 14589318
37 feet Y = 4446824
24 meter
Z = 16354850
83 Z = 4984958
53
XDOT = -23086
235866 XDOT = -7036
684692
YDOT = 1455
819105 feet/sec YDOT = 443
733663 meter/sec
ZDOT = -6902
939073 ZDOT = -2104
015829
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
00306676
00016717 00000-0 10270-3 0 9136
2 25544 51
6436 313
4887 0001738 71
8864 288
2476 15
49250058 4385
Satellite: ISS
Catalog Number: 25544
Epoch time: 20249
00306676 = yrday
fracday
Element set: 913
Inclination: 51
6436 deg
RA of node: 313
4887 deg
Eccentricity:
0001738
Arg of perigee: 71
8864 deg
Mean anomaly: 288
2476 deg
Mean motion: 15
49250058 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 438
Checksum: 325
Coasting Arc #15 (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 = 4027837
75 A = 6792048
10 meter
Y = 1688934
38 meter E =
0005231
Z = 5197732
02 I = 51
32867
XDOT = -4167
215073 Wp = 113
72600
YDOT = 6324
499109 meter/sec RA = 310
49000 deg
ZDOT = 1171
200067 TA = 324
96915
MA = 325
00355
Ha = 229
113 n
mi
Hp = 221
806
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13214690
78 X = 3983404
68
Y = 5541123
31 feet Y = 1733728
48 meter
Z = 17052926
56 Z = 5217189
58
XDOT = -13671
965462 XDOT = -4243
316811
YDOT = 20749
668993 feet/sec YDOT = 6277
472897 meter/sec
ZDOT = 3842
519906 ZDOT = 1150
772136
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9129310
96 X = -2782613
98
Y = -10905131
02 feet Y = -3323883
93 meter
Z = 17142584
49 Z = 5225059
75
XDOT = 20857
998474 XDOT = 6357
517935
YDOT = -11554
226723 feet/sec YDOT = -3521
728305 meter/sec
ZDOT = 3748
016310 ZDOT = 1142
395371
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
51911496
00016717 00000-0 10270-3 0 9145
2 25544 51
6437 310
9327 0001522 89
2832 270
8493 15
49240148 4460
Satellite: ISS
Catalog Number: 25544
Epoch time: 20249
51911496 = yrday
fracday
Element set: 914
Inclination: 51
6437 deg
RA of node: 310
9327 deg
Eccentricity:
0001522
Arg of perigee: 89
2832 deg
Mean anomaly: 270
8493 deg
Mean motion: 15
49240148 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 446
Checksum: 309
Coasting Arc #16 (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 = -4115657
13 A = 6792122
52 meter
Y = -1434975
38 meter E =
0015806
Z = -5223115
48 I = 51
30679
XDOT = 3671
194755 Wp = 82
31978
YDOT = -6623
436239 meter/sec RA = 305
51997 deg
ZDOT = -1073
834216 TA = 177
32173
MA = 177
31325
Ha = 229
336 n
mi
Hp = 221
701
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13502812
10 X = -4073933
99
Y = -4707924
46 feet Y = -1480766
65 meter
Z = -17136205
65 Z = -5243006
32
XDOT = 12044
602216 XDOT = 3750
203237
YDOT = -21730
433856 feet/sec YDOT = -6581
940614 meter/sec
ZDOT = -3523
078136 ZDOT = -1055
808651
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9940816
12 X = 3029960
75
Y = 10125250
05 feet Y = 3086176
21 meter
Z = -17227870
38 Z = -5251054
89
XDOT = -19670
866106 XDOT = -5995
679989
YDOT = 13464
154377 feet/sec YDOT = 4103
874254 meter/sec
ZDOT = -3439
657010 ZDOT = -1048
407457
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
48670702
00016717 00000-0 10270-3 0 9156
2 25544 51
6430 306
1449 0001555 88
9030 271
2298 15
49196018 4618
Satellite: ISS
Catalog Number: 25544
Epoch time: 20250
48670702 = yrday
fracday
Element set: 915
Inclination: 51
6430 deg
RA of node: 306
1449 deg
Eccentricity:
0001555
Arg of perigee: 88
9030 deg
Mean anomaly: 271
2298 deg
Mean motion: 15
49196018 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 461
Checksum: 298
Coasting Arc #17 (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 = 4174868
04 A = 6791922
39 meter
Y = 1165760
51 meter E =
0004994
Z = 5225141
91 I = 51
28812
XDOT = -3163
668990 Wp = 111
30103
YDOT = 6911
013656 meter/sec RA = 300
54875 deg
ZDOT = 983
326909 TA = 329
22030
MA = 329
24957
Ha = 229
146 n
mi
Hp = 221
766
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13697073
64 X = 4136141
03
Y = 3824673
59 feet Y = 1212230
61 meter
Z = 17142854
02 Z = 5245327
73
XDOT = -10379
491438 XDOT = -3245
491349
YDOT = 22673
929317 feet/sec YDOT = 6875
177796 meter/sec
ZDOT = 3226
138153 ZDOT = 967
759898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10664808
95 X = -3250633
77
Y = -9235874
97 feet Y = -2815094
69 meter
Z = 17235888
78 Z = 5253498
90
XDOT = 18380
817501 XDOT = 5602
473174
YDOT = -15323
059684 feet/sec YDOT = -4670
468592 meter/sec
ZDOT = 3154
057190 ZDOT = 961
356632
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
51880123
00016717 00000-0 10270-3 0 9162
2 25544 51
6432 301
0380 0001633 89
6808 270
4529 15
49239908 4777
Satellite: ISS
Catalog Number: 25544
Epoch time: 20251
51880123 = yrday
fracday
Element set: 916
Inclination: 51
6432 deg
RA of node: 301
0380 deg
Eccentricity:
0001633
Arg of perigee: 89
6808 deg
Mean anomaly: 270
4529 deg
Mean motion: 15
49239908 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 477
Checksum: 303
Coasting Arc #18 (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 = -4232020
27 A = 6792001
66 meter
Y = -907708
45 meter E =
0016140
Z = -5248450
49 I = 51
27079
XDOT = 2625
387788 Wp = 84
11917
YDOT = -7128
983031 meter/sec RA = 295
57638 deg
ZDOT = -884
743798 TA = 177
35767
MA = 177
34913
Ha = 229
393 n
mi
Hp = 221
630
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13884580
94 X = -4196061
37
Y = -2978046
11 feet Y = -954833
07 meter
Z = -17219325
76 Z = -5268920
72
XDOT = 8613
476995 XDOT = 2709
208695
YDOT = -23389
051940 feet/sec YDOT = -7099
155424 meter/sec
ZDOT = -2902
702749 ZDOT = -871
786787
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11339385
80 X = 3456244
79
Y = 8355254
09 feet Y = 2546681
45 meter
Z = -17313682
02 Z = -5277210
28
XDOT = -16844
989529 XDOT = -5134
352809
YDOT = 16975
740948 feet/sec YDOT = 5174
205841 meter/sec
ZDOT = -2842
662068 ZDOT = -866
443398
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
48639155
00016717 00000-0 10270-3 0 9177
2 25544 51
6421 296
2506 0001720 93
0552 267
0795 15
49198067 4926
Satellite: ISS
Catalog Number: 25544
Epoch time: 20252
48639155 = yrday
fracday
Element set: 917
Inclination: 51
6421 deg
RA of node: 296
2506 deg
Eccentricity:
0001720
Arg of perigee: 93
0552 deg
Mean anomaly: 267
0795 deg
Mean motion: 15
49198067 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 492
Checksum: 317
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