[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
June 15th 2020
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16490 3108 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 0 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
There are no maneuvers
Coasting Arc #1 (Orbit 3174)
---------------------------------------
Vector Time (GMT): 2020/167/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6022416
23 A = 6800787
31 meter
Y = 2190768
42 meter E =
0014927
Z = 2258415
51 I = 51
63110
XDOT = -3534
123084 Wp = 100
93968
YDOT = -4080
691791 meter/sec RA = 356
21098 deg
ZDOT = -5438
019087 TA = 53
97739
MA = 53
83914
Ha = 228
972 n
mi
Hp = 221
443
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19758583
43 X = -6057436
57
Y = 7187560
43 feet Y = 2123225
37 meter
Z = 7409499
71 Z = 2229076
12
XDOT = -11594
892009 XDOT = -3461
814068
YDOT = -13388
096426 feet/sec YDOT = -4119
807885 meter/sec
ZDOT = -17841
269969 ZDOT = -5455
011402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4838280
46 X = 1474707
88
Y = 20509463
17 feet Y = 6251284
37 meter
Z = 7274358
60 Z = 2217224
50
XDOT = -13135
607202 XDOT = -4003
733075
YDOT = 9487
312791 feet/sec YDOT = 2891
732939 meter/sec
ZDOT = -17919
096846 ZDOT = -5461
740719
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20167
53669763
00016717 00000-0 10270-3 0 9008
2 25544 51
6418 356
6428 0002131 45
8857 314
2468 15
49486482 31750
Satellite: ISS
Catalog Number: 25544
Epoch time: 20167
53669763 = yrday
fracday
Element set: 900
Inclination: 51
6418 deg
RA of node: 356
6428 deg
Eccentricity:
0002131
Arg of perigee: 45
8857 deg
Mean anomaly: 314
2468 deg
Mean motion: 15
49486482 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3175
Checksum: 332
Coasting Arc #2 (Orbit 3189)
---------------------------------------
Vector Time (GMT): 2020/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5899591
48 A = 6801132
29 meter
Y = -2619550
32 meter E =
0008542
Z = -2135237
94 I = 51
59740
XDOT = 3690
341653 Wp = 44
93720
YDOT = 3843
636424 meter/sec RA = 351
25855 deg
ZDOT = 5500
227275 TA = 291
43791
MA = 291
52900
Ha = 229
130 n
mi
Hp = 221
405
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19355615
11 X = 5938817
42
Y = -8594325
18 feet Y = -2553357
26 meter
Z = -7005373
82 Z = -2106484
98
XDOT = 12107
420121 XDOT = 3620
369610
YDOT = 12610
355721 feet/sec YDOT = 3884
512457 meter/sec
ZDOT = 18045
365074 ZDOT = 5517
984179
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6630368
76 X = -2020936
40
Y = -20158841
92 feet Y = -6144415
02 meter
Z = -6872905
24 Z = -2094861
52
XDOT = 12266
476570 XDOT = 3738
822058
YDOT = -10192
502273 feet/sec YDOT = -3106
674693 meter/sec
ZDOT = 18126
721781 ZDOT = 5525
024799
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20168
50414951
00016717 00000-0 10270-3 0 9014
2 25544 51
6409 351
8532 0002159 58
0050 302
1310 15
49441877 31902
Satellite: ISS
Catalog Number: 25544
Epoch time: 20168
50414951 = yrday
fracday
Element set: 901
Inclination: 51
6409 deg
RA of node: 351
8532 deg
Eccentricity:
0002159
Arg of perigee: 58
0050 deg
Mean anomaly: 302
1310 deg
Mean motion: 15
49441877 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3190
Checksum: 280
Coasting Arc #3 (Orbit 3205)
---------------------------------------
Vector Time (GMT): 2020/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5764830
41 A = 6801301
91 meter
Y = 3011615
37 meter E =
0015204
Z = 1967177
88 I = 51
56494
XDOT = -3807
198260 Wp = 105
34734
YDOT = -3625
535200 meter/sec RA = 346
30478 deg
ZDOT = -5574
483862 TA = 52
96262
MA = 52
82364
Ha = 229
041 n
mi
Hp = 221
351
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18913485
60 X = -5807634
22
Y = 9880627
84 feet Y = 2946909
29 meter
Z = 6453995
67 Z = 1939070
91
XDOT = -12490
807938 XDOT = -3739
295668
YDOT = -11894
800524 feet/sec YDOT = -3667
729471 meter/sec
ZDOT = -18288
989048 ZDOT = -5592
813499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8294625
92 X = 2528201
98
Y = 19702817
14 feet Y = 6005418
67 meter
Z = 6324474
83 Z = 1927699
93
XDOT = -11432
196584 XDOT = -3484
533519
YDOT = 10744
904205 feet/sec YDOT = 3275
046802 meter/sec
ZDOT = -18372
992091 ZDOT = -5600
087989
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20169
53609307
00016717 00000-0 10270-3 0 9020
2 25544 51
6406 346
7449 0002169 55
8924 304
2432 15
49483541 32065
Satellite: ISS
Catalog Number: 25544
Epoch time: 20169
53609307 = yrday
fracday
Element set: 902
Inclination: 51
6406 deg
RA of node: 346
7449 deg
Eccentricity:
0002169
Arg of perigee: 55
8924 deg
Mean anomaly: 304
2432 deg
Mean motion: 15
49483541 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3206
Checksum: 309
Coasting Arc #4 (Orbit 3220)
---------------------------------------
Vector Time (GMT): 2020/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5577162
99 A = 6801608
87 meter
Y = -3425616
62 meter E =
0009354
Z = -1840201
23 I = 51
53242
XDOT = 3932
643929 Wp = 45
27946
YDOT = 3392
151436 meter/sec RA = 341
34844 deg
ZDOT = 5628
237635 TA = 294
49682
MA = 294
59433
Ha = 229
204 n
mi
Hp = 221
290
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18297778
84 X = 5623993
45
Y = -11238899
68 feet Y = -3362986
65 meter
Z = -6037405
61 Z = -1812996
23
XDOT = 12902
375095 XDOT = 3867
080676
YDOT = 11129
105760 feet/sec YDOT = 3435
761492 meter/sec
ZDOT = 18465
346573 ZDOT = 5647
182353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10027775
38 X = -3056465
94
Y = -19027972
76 feet Y = -5799726
10 meter
Z = -5912006
15 Z = -1801979
48
XDOT = 10546
777793 XDOT = 3214
657871
YDOT = -11297
289422 feet/sec YDOT = -3443
413816 meter/sec
ZDOT = 18552
193257 ZDOT = 5654
708505
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20170
50354346
00016717 00000-0 10270-3 0 9030
2 25544 51
6399 341
9559 0002255 69
5799 290
5593 15
49443347 32215
Satellite: ISS
Catalog Number: 25544
Epoch time: 20170
50354346 = yrday
fracday
Element set: 903
Inclination: 51
6399 deg
RA of node: 341
9559 deg
Eccentricity:
0002255
Arg of perigee: 69
5799 deg
Mean anomaly: 290
5593 deg
Mean motion: 15
49443347 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3221
Checksum: 329
Coasting Arc #5 (Orbit 3236)
---------------------------------------
Vector Time (GMT): 2020/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5381521
11 A = 6801780
32 meter
Y = 3799414
99 meter E =
0015376
Z = 1667191
22 I = 51
50190
XDOT = -4022
408302 Wp = 110
08106
YDOT = -3183
041975 meter/sec RA = 336
39022 deg
ZDOT = -5692
360283 TA = 51
64932
MA = 51
51125
Ha = 229
092 n
mi
Hp = 221
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17655909
14 X = -5431705
63
Y = 12465272
28 feet Y = 3738954
07 meter
Z = 5469787
47 Z = 1640928
61
XDOT = -13196
877630 XDOT = -3958
865275
YDOT = -10443
051098 feet/sec YDOT = -3227
667022 meter/sec
ZDOT = -18675
722713 ZDOT = -5711
745940
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11609285
94 X = 3538510
35
Y = 18266051
41 feet Y = 5567492
47 meter
Z = 5348697
19 Z = 1630282
90
XDOT = -9722
351999 XDOT = -2963
372889
YDOT = 11710
848160 feet/sec YDOT = 3569
466519 meter/sec
ZDOT = -18764
611978 ZDOT = -5719
453731
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20171
53548593
00016717 00000-0 10270-3 0 9044
2 25544 51
6401 336
8475 0002140 67
7107 292
4270 15
49472465 32378
Satellite: ISS
Catalog Number: 25544
Epoch time: 20171
53548593 = yrday
fracday
Element set: 904
Inclination: 51
6401 deg
RA of node: 336
8475 deg
Eccentricity:
0002140
Arg of perigee: 67
7107 deg
Mean anomaly: 292
4270 deg
Mean motion: 15
49472465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3237
Checksum: 306
Coasting Arc #6 (Orbit 3251)
---------------------------------------
Vector Time (GMT): 2020/172/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5131793
27 A = 6801992
90 meter
Y = -4186824
01 meter E =
0010177
Z = -1535771
23 I = 51
47371
XDOT = 4121
130916 Wp = 45
60096
YDOT = 2957
743606 meter/sec RA = 331
42945 deg
ZDOT = 5737
944678 TA = 297
61639
MA = 297
71968
Ha = 229
223 n
mi
Hp = 221
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16836592
11 X = 5185690
09
Y = -13736299
24 feet Y = -4129134
97 meter
Z = -5038619
52 Z = -1510712
90
XDOT = 13520
770723 XDOT = 4059
878570
YDOT = 9703
883223 feet/sec YDOT = 3003
485362 meter/sec
ZDOT = 18825
277816 ZDOT = 5757
815391
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13217188
79 X = -4028599
14
Y = -17280452
05 feet Y = -5267081
78 meter
Z = -4923041
21 Z = -1500542
96
XDOT = 8847
585679 XDOT = 2696
744115
YDOT = -12127
075788 feet/sec YDOT = -3696
332700 meter/sec
ZDOT = 18916
416011 ZDOT = 5765
723600
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20172
50293266
00016717 00000-0 10270-3 0 9057
2 25544 51
6417 332
0584 0002322 77
0130 283
1279 15
49455558 32523
Satellite: ISS
Catalog Number: 25544
Epoch time: 20172
50293266 = yrday
fracday
Element set: 905
Inclination: 51
6417 deg
RA of node: 332
0584 deg
Eccentricity:
0002322
Arg of perigee: 77
0130 deg
Mean anomaly: 283
1279 deg
Mean motion: 15
49455558 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3252
Checksum: 294
Coasting Arc #7 (Orbit 3267)
---------------------------------------
Vector Time (GMT): 2020/173/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4879119
82 A = 6802187
48 meter
Y = 4531152
38 meter E =
0015534
Z = 1357222
58 I = 51
44425
XDOT = -4188
671094 Wp = 114
19917
YDOT = -2761
738813 meter/sec RA = 326
46725 deg
ZDOT = -5791
508410 TA = 51
00357
MA = 50
86533
Ha = 229
183 n
mi
Hp = 221
209
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16007610
95 X = -4936018
48
Y = 14865985
49 feet Y = 4476272
16 meter
Z = 4452829
99 Z = 1333384
56
XDOT = -13742
359231 XDOT = -4129
345447
YDOT = -9060
822876 feet/sec YDOT = -2808
246572 meter/sec
ZDOT = -19001
011843 ZDOT = -5811
711781
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14653040
62 X = 4466246
78
Y = 16232589
26 feet Y = 4947693
21 meter
Z = 4342841
73 Z = 1323698
16
XDOT = -8057
238598 XDOT = -2455
846325
YDOT = 12423
153952 feet/sec YDOT = 3786
577325 meter/sec
ZDOT = -19093
697803 ZDOT = -5819
759090
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20173
53487230
00016717 00000-0 10270-3 0 9068
2 25544 51
6406 326
9501 0002303 78
0376 282
1032 15
49463718 32684
Satellite: ISS
Catalog Number: 25544
Epoch time: 20173
53487230 = yrday
fracday
Element set: 906
Inclination: 51
6406 deg
RA of node: 326
9501 deg
Eccentricity:
0002303
Arg of perigee: 78
0376 deg
Mean anomaly: 282
1032 deg
Mean motion: 15
49463718 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3268
Checksum: 296
Coasting Arc #8 (Orbit 3282)
---------------------------------------
Vector Time (GMT): 2020/174/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4571107
55 A = 6802345
34 meter
Y = -4881742
15 meter E =
0010935
Z = -1222600
57 I = 51
41860
XDOT = 4267
504014 Wp = 46
66570
YDOT = 2546
457705 meter/sec RA = 321
50372 deg
ZDOT = 5828
016460 TA = 300
03462
MA = 300
14306
Ha = 229
238 n
mi
Hp = 221
169
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14997072
00 X = 4631295
56
Y = -16016214
41 feet Y = -4830287
98 meter
Z = -4011156
71 Z = -1200250
93
XDOT = 14000
997421 XDOT = 4210
402644
YDOT = 8354
520029 feet/sec YDOT = 2593
859462 meter/sec
ZDOT = 19120
788911 ZDOT = 5848
608029
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16076246
45 X = -4900039
92
Y = -14960032
11 feet Y = -4559817
79 meter
Z = -3907993
12 Z = -1191156
30
XDOT = 7209
272665 XDOT = 2197
386308
YDOT = -12731
318410 feet/sec YDOT = -3880
505851 meter/sec
ZDOT = 19215
281148 ZDOT = 5856
817694
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20174
50231674
00016717 00000-0 10270-3 0 9076
2 25544 51
6419 322
1621 0002350 84
6836 275
4582 15
49455188 32839
Satellite: ISS
Catalog Number: 25544
Epoch time: 20174
50231674 = yrday
fracday
Element set: 907
Inclination: 51
6419 deg
RA of node: 322
1621 deg
Eccentricity:
0002350
Arg of perigee: 84
6836 deg
Mean anomaly: 275
4582 deg
Mean motion: 15
49455188 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3283
Checksum: 309
Coasting Arc #9 (Orbit 3298)
---------------------------------------
Vector Time (GMT): 2020/175/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4265410
51 A = 6802501
06 meter
Y = 5187127
61 meter E =
0015360
Z = 1040579
84 I = 51
39351
XDOT = -4320
457367 Wp = 118
56038
YDOT = -2363
288334 meter/sec RA = 316
53768 deg
ZDOT = -5870
294301 TA = 50
13969
MA = 50
00468
Ha = 229
166 n
mi
Hp = 221
212
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13994128
96 X = -4328151
98
Y = 17018135
21 feet Y = 5139077
73 meter
Z = 3413975
84 Z = 1019709
05
XDOT = -14174
728893 XDOT = -4265
195080
YDOT = -7753
570651 feet/sec YDOT = -2411
292581 meter/sec
ZDOT = -19259
495739 ZDOT = -5891
147410
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17311524
55 X = 5276552
68
Y = 13653294
46 feet Y = 4161524
15 meter
Z = 3317600
11 Z = 1011204
51
XDOT = -6459
701802 XDOT = -1968
917109
YDOT = 12941
957036 feet/sec YDOT = 3944
708505 meter/sec
ZDOT = -19355
210009 ZDOT = -5899
468011
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 20175
53425512
00016717 00000-0 10270-3 0 9087
2 25544 51
6418 317
0537 0002243 86
6474 273
4932 15
49461520 32999
Satellite: ISS
Catalog Number: 25544
Epoch time: 20175
53425512 = yrday
fracday
Element set: 908
Inclination: 51
6418 deg
RA of node: 317
0537 deg
Eccentricity:
0002243
Arg of perigee: 86
6474 deg
Mean anomaly: 273
4932 deg
Mean motion: 15
49461520 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3299
Checksum: 310
Coasting Arc #10 (Orbit 3313)
---------------------------------------
Vector Time (GMT): 2020/176/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3906217
92 A = 6802609
19 meter
Y = -5490446
50 meter E =
0011736
Z = -901937
87 I = 51
37176
XDOT = 4384
133904 Wp = 47
70525
YDOT = 2159
639116 meter/sec RA = 311
57046 deg
ZDOT = 5897
853745 TA = 302
51700
MA = 302
63035
Ha = 229
227 n
mi
Hp = 221
150
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12815675
58 X = 3971704
44
Y = -18013275
93 feet Y = -5446398
07 meter
Z = -2959113
73 Z = -882805
23
XDOT = 14383
641418 XDOT = 4331
010373
YDOT = 7085
430169 feet/sec YDOT = 2208
367496 meter/sec
ZDOT = 19349
913862 ZDOT = 5919
021216
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18492847
60 X = -5636619
95
Y = -12134642
35 feet Y = -3698638
99 meter
Z = -2870722
42 Z = -874996
19
XDOT = 5649
364727 XDOT = 1721
926369
YDOT = -13164
436454 feet/sec YDOT = -4012
520231 meter/sec
ZDOT = 19447
094365 ZDOT = 5927
474363
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 20176
50169588
00016717 00000-0 10270-3 0 9094
2 25544 51
6434 312
2656 0002353 88
4606 271
6814 15
49459340 33149
Satellite: ISS
Catalog Number: 25544
Epoch time: 20176
50169588 = yrday
fracday
Element set: 909
Inclination: 51
6434 deg
RA of node: 312
2656 deg
Eccentricity:
0002353
Arg of perigee: 88
4606 deg
Mean anomaly: 271
6814 deg
Mean motion: 15
49459340 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3314
Checksum: 317
Coasting Arc #11 (Orbit 3329)
---------------------------------------
Vector Time (GMT): 2020/177/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3555663
96 A = 6802719
04 meter
Y = 5747358
07 meter E =
0015134
Z = 715742
67 I = 51
34971
XDOT = -4427
427411 Wp = 122
09675
YDOT = -1990
280303 meter/sec RA = 306
60196 deg
ZDOT = -5928
312175 TA = 50
15313
MA = 50
02009
Ha = 229
188 n
mi
Hp = 221
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11665564
16 X = -3623144
97
Y = 18856161
66 feet Y = 5707218
68 meter
Z = 2348237
11 Z = 698307
95
XDOT = -14525
680481 XDOT = -4376
046562
YDOT = -6529
791019 feet/sec YDOT = -2039
502703 meter/sec
ZDOT = -19449
843093 ZDOT = -5949
694077
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19476254
36 X = 5936362
33
Y = 10615446
62 feet Y = 3235588
13 meter
Z = 2267652
16 Z = 691180
38
XDOT = -4946
902587 XDOT = -1507
815908
YDOT = 13313
229485 feet/sec YDOT = 4057
872347 meter/sec
ZDOT = -19548
026572 ZDOT = -5958
238499
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 20177
53363085
00016717 00000-0 10270-3 0 9108
2 25544 51
6424 307
1579 0002337 92
0316 268
1102 15
49465299 33305
Satellite: ISS
Catalog Number: 25544
Epoch time: 20177
53363085 = yrday
fracday
Element set: 910
Inclination: 51
6424 deg
RA of node: 307
1579 deg
Eccentricity:
0002337
Arg of perigee: 92
0316 deg
Mean anomaly: 268
1102 deg
Mean motion: 15
49465299 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3330
Checksum: 297
Coasting Arc #12 (Orbit 3344)
---------------------------------------
Vector Time (GMT): 2020/178/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3152847
57 A = 6802809
86 meter
Y = -5995257
28 meter E =
0012426
Z = -574610
25 I = 51
33122
XDOT = 4482
347142 Wp = 49
72629
YDOT = 1796
249663 meter/sec RA = 301
63197 deg
ZDOT = 5946
201687 TA = 304
05874
MA = 304
17665
Ha = 229
222 n
mi
Hp = 221
149
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10343988
10 X = 3222445
09
Y = -19669479
27 feet Y = -5959610
67 meter
Z = -1885204
25 Z = -559126
96
XDOT = 14705
863326 XDOT = 4433
044980
YDOT = 5893
207555 feet/sec YDOT = 1846
097982 meter/sec
ZDOT = 19508
535717 ZDOT = 5967
855368
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20370759
69 X = -6209007
55
Y = -8898512
52 feet Y = -2712266
62 meter
Z = -1813594
32 Z = -552783
55
XDOT = 4169
847093 XDOT = 1270
969394
YDOT = -13477
225733 feet/sec YDOT = -4107
858403 meter/sec
ZDOT = 19607
985880 ZDOT = 5976
514096
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 20178
50106955
00016717 00000-0 10270-3 0 9118
2 25544 51
6428 302
3699 0002353 94
6255 265
5164 15
49457278 33450
Satellite: ISS
Catalog Number: 25544
Epoch time: 20178
50106955 = yrday
fracday
Element set: 911
Inclination: 51
6428 deg
RA of node: 302
3699 deg
Eccentricity:
0002353
Arg of perigee: 94
6255 deg
Mean anomaly: 265
5164 deg
Mean motion: 15
49457278 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3345
Checksum: 322
Coasting Arc #13 (Orbit 3360)
---------------------------------------
Vector Time (GMT): 2020/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2765403
71 A = 6802850
84 meter
Y = 6196338
03 meter E =
0014702
Z = 385797
78 I = 51
31485
XDOT = -4522
004327 Wp = 126
01275
YDOT = -1637
361805 meter/sec RA = 296
66043 deg
ZDOT = -5964
488131 TA = 49
81699
MA = 49
68837
Ha = 229
148 n
mi
Hp = 221
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9072846
81 X = -2836361
44
Y = 20329193
02 feet Y = 6165016
52 meter
Z = 1265740
75 Z = 372193
07
XDOT = -14835
972202 XDOT = -4474
387022
YDOT = -5371
921933 feet/sec YDOT = -1687
663124 meter/sec
ZDOT = -19568
530612 ZDOT = -5986
338566
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21063196
33 X = 6420062
24
Y = 7217328
54 feet Y = 2199841
74 meter
Z = 1202774
54 Z = 366605
68
XDOT = -3503
516974 XDOT = -1067
871974
YDOT = 13589
722841 feet/sec YDOT = 4142
147522 meter/sec
ZDOT = -19668
898278 ZDOT = -5995
080195
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 20179
53300201
00016717 00000-0 10270-3 0 9123
2 25544 51
6428 297
2619 0002278 99
3207 260
8201 15
49469471 33615
Satellite: ISS
Catalog Number: 25544
Epoch time: 20179
53300201 = yrday
fracday
Element set: 912
Inclination: 51
6428 deg
RA of node: 297
2619 deg
Eccentricity:
0002278
Arg of perigee: 99
3207 deg
Mean anomaly: 260
8201 deg
Mean motion: 15
49469471 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3361
Checksum: 302
Coasting Arc #14 (Orbit 3375)
---------------------------------------
Vector Time (GMT): 2020/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2329713
06 A = 6802897
29 meter
Y = -6381453
15 meter E =
0013154
Z = -241475
86 I = 51
30181
XDOT = 4571
831200 Wp = 51
99851
YDOT = 1451
799802 meter/sec RA = 291
68765 deg
ZDOT = 5972
678791 TA = 305
39270
MA = 305
51551
Ha = 229
212 n
mi
Hp = 221
128
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7643415
54 X = 2402072
16
Y = -20936526
07 feet Y = -6354996
02 meter
Z = -792243
64 Z = -229984
08
XDOT = 14999
446195 XDOT = 4526
245283
YDOT = 4763
122709 feet/sec YDOT = 1502
669710 meter/sec
ZDOT = 19595
402858 ZDOT = 5994
776268
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21634761
49 X = -6594275
30
Y = -5364564
44 feet Y = -1635119
24 meter
Z = -738998
44 Z = -225246
72
XDOT = 2755
069094 XDOT = 839
745060
YDOT = -13712
330345 feet/sec YDOT = -4179
518289 meter/sec
ZDOT = 19696
919802 ZDOT = 6003
621156
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 20180
50043687
00016717 00000-0 10270-3 0 9135
2 25544 51
6437 292
4734 0002385 98
0730 262
0691 15
49464429 33767
Satellite: ISS
Catalog Number: 25544
Epoch time: 20180
50043687 = yrday
fracday
Element set: 913
Inclination: 51
6437 deg
RA of node: 292
4734 deg
Eccentricity:
0002385
Arg of perigee: 98
0730 deg
Mean anomaly: 262
0691 deg
Mean motion: 15
49464429 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3376
Checksum: 316
Coasting Arc #15 (Orbit 3391)
---------------------------------------
Vector Time (GMT): 2020/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1916282
08 A = 6802918
94 meter
Y = 6520805
58 meter E =
0014258
Z = 49990
98 I = 51
28959
XDOT = -4611
912065 Wp = 129
04297
YDOT = -1300
714075 meter/sec RA = 286
71434 deg
ZDOT = -5978
101909 TA = 50
41696
MA = 50
29113
Ha = 229
184 n
mi
Hp = 221
152
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6287014
70 X = -1989300
08
Y = 21393719
09 feet Y = 6498968
07 meter
Z = 164012
41 Z = 40505
91
XDOT = -15130
945094 XDOT = -4567
986190
YDOT = -4267
434629 feet/sec YDOT = -1352
041424 meter/sec
ZDOT = -19613
195241 ZDOT = -6000
398202
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22008629
00 X = 6708230
12
Y = 3584762
15 feet Y = 1092635
50 meter
Z = 120000
37 Z = 36576
11
XDOT = -2113
224015 XDOT = -644
110680
YDOT = 13805
774052 feet/sec YDOT = 4207
999931 meter/sec
ZDOT = -19715
637324 ZDOT = -6009
326256
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 20181
53236619
00016717 00000-0 10270-3 0 9149
2 25544 51
6428 287
3655 0002389 103
8430 256
2986 15
49465054 33923
Satellite: ISS
Catalog Number: 25544
Epoch time: 20181
53236619 = yrday
fracday
Element set: 914
Inclination: 51
6428 deg
RA of node: 287
3655 deg
Eccentricity:
0002389
Arg of perigee: 103
8430 deg
Mean anomaly: 256
2986 deg
Mean motion: 15
49465054 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3392
Checksum: 326
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