[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 25th 2020
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 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
190/18:21:00
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
3
Coasting Arc #1 (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 = 3900118
42 A = 6802616
95 meter
Y = -5493454
56 meter E =
0011738
Z = -910069
15 I = 51
37154
XDOT = 4391
002106 Wp = 47
65708
YDOT = 2150
006452 meter/sec RA = 311
56999 deg
ZDOT = 5896
251974 TA = 302
47614
MA = 302
58955
Ha = 229
240 n
mi
Hp = 221
152
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12795664
10 X = 3965678
53
Y = -18023144
90 feet Y = -5449473
92 meter
Z = -2985791
19 Z = -890965
97
XDOT = 14406
174890 XDOT = 4337
993560
YDOT = 7053
826942 feet/sec YDOT = 2198
812281 meter/sec
ZDOT = 19344
658707 ZDOT = 5917
453084
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18501949
62 X = -5639394
24
Y = -12114448
87 feet Y = -3692484
02 meter
Z = -2897535
08 Z = -883168
69
XDOT = 5618
390745 XDOT = 1712
485499
YDOT = -13185
111759 feet/sec YDOT = -4018
822064 meter/sec
ZDOT = 19441
994624 ZDOT = 5925
919961
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
50171182
00016717 00000-0 10270-3 0 9008
2 25544 51
6433 312
2653 0002368 87
9597 272
1824 15
49454608 33143
Satellite: ISS
Catalog Number: 25544
Epoch time: 20176
50171182 = yrday
fracday
Element set: 900
Inclination: 51
6433 deg
RA of node: 312
2653 deg
Eccentricity:
0002368
Arg of perigee: 87
9597 deg
Mean anomaly: 272
1824 deg
Mean motion: 15
49454608 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3314
Checksum: 305
Coasting Arc #2 (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 = -3548479
04 A = 6802725
03 meter
Y = 5750610
94 meter E =
0015149
Z = 725303
81 I = 51
34949
XDOT = -4434
740998 Wp = 121
91322
YDOT = -1978
447288 meter/sec RA = 306
60148 deg
ZDOT = -5926
796012 TA = 50
23247
MA = 50
09913
Ha = 229
200 n
mi
Hp = 221
163
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11641991
59 X = -3616043
41
Y = 18866833
80 feet Y = 5710551
43 meter
Z = 2379605
67 Z = 707903
79
XDOT = -14549
675189 XDOT = -4383
499290
YDOT = -6490
968794 feet/sec YDOT = -2027
752253 meter/sec
ZDOT = -19444
868805 ZDOT = -5948
213776
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19485613
76 X = 5939215
08
Y = 10591531
34 feet Y = 3228298
75 meter
Z = 2299180
05 Z = 700790
08
XDOT = -4908
548828 XDOT = -1496
125683
YDOT = 13334
380633 feet/sec YDOT = 4064
319217 meter/sec
ZDOT = -19543
218043 ZDOT = -5956
772860
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
53364966
00016717 00000-0 10270-3 0 9017
2 25544 51
6423 307
1577 0002352 91
5062 268
6358 15
49461327 33307
Satellite: ISS
Catalog Number: 25544
Epoch time: 20177
53364966 = yrday
fracday
Element set: 901
Inclination: 51
6423 deg
RA of node: 307
1577 deg
Eccentricity:
0002352
Arg of perigee: 91
5062 deg
Mean anomaly: 268
6358 deg
Mean motion: 15
49461327 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3330
Checksum: 308
Coasting Arc #3 (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 = 3144654
16 A = 6802813
82 meter
Y = -5998527
63 meter E =
0012425
Z = -585394
13 I = 51
33100
XDOT = 4489
637223 Wp = 49
65295
YDOT = 1782
414850 meter/sec RA = 301
63148 deg
ZDOT = 5944
853308 TA = 304
01497
MA = 304
13292
Ha = 229
233 n
mi
Hp = 221
148
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10317106
82 X = 3214341
23
Y = -19680208
76 feet Y = -5962972
14 meter
Z = -1920584
41 Z = -569950
42
XDOT = 14729
780914 XDOT = 4440
495774
YDOT = 5847
817749 feet/sec YDOT = 1832
345590 meter/sec
ZDOT = 19504
111903 ZDOT = 5966
542790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20379525
08 X = -6211679
24
Y = -8871163
00 feet Y = -2703930
48 meter
Z = -1849156
28 Z = -563622
83
XDOT = 4124
829855 XDOT = 1257
248140
YDOT = -13497
168893 feet/sec YDOT = -4113
937079 meter/sec
ZDOT = 19603
727640 ZDOT = 5975
216185
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
50109053
00016717 00000-0 10270-3 0 9020
2 25544 51
6427 302
3697 0002368 94
0740 266
0681 15
49454169 33452
Satellite: ISS
Catalog Number: 25544
Epoch time: 20178
50109053 = yrday
fracday
Element set: 902
Inclination: 51
6427 deg
RA of node: 302
3697 deg
Eccentricity:
0002368
Arg of perigee: 94
0740 deg
Mean anomaly: 266
0681 deg
Mean motion: 15
49454169 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3345
Checksum: 306
Coasting Arc #4 (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 = -2756497
46 A = 6802854
40 meter
Y = 6199571
65 meter E =
0014724
Z = 397472
79 I = 51
31463
XDOT = -4528
904239 Wp = 125
81350
YDOT = -1621
887659 meter/sec RA = 296
65993 deg
ZDOT = -5963
478073 TA = 49
88979
MA = 49
76084
Ha = 229
158 n
mi
Hp = 221
177
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9043626
85 X = -2827548
73
Y = 20339802
02 feet Y = 6168349
21 meter
Z = 1304044
58 Z = 383911
12
XDOT = -14858
609707 XDOT = -4481
464363
YDOT = -5321
153738 feet/sec YDOT = -1672
267130 meter/sec
ZDOT = -19565
216776 ZDOT = -5985
362455
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21071161
73 X = 6422490
09
Y = 7187533
80 feet Y = 2190760
30 meter
Z = 1241276
06 Z = 378340
94
XDOT = -3453
090126 XDOT = -1052
501870
YDOT = 13607
146825 feet/sec YDOT = 4147
458352 meter/sec
ZDOT = -19665
741554 ZDOT = -5994
118026
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
53302478
00016717 00000-0 10270-3 0 9031
2 25544 51
6427 297
2616 0002292 98
7398 261
4012 15
49467001 33615
Satellite: ISS
Catalog Number: 25544
Epoch time: 20179
53302478 = yrday
fracday
Element set: 903
Inclination: 51
6427 deg
RA of node: 297
2616 deg
Eccentricity:
0002292
Arg of perigee: 98
7398 deg
Mean anomaly: 261
4012 deg
Mean motion: 15
49467001 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3361
Checksum: 310
Coasting Arc #5 (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 = 2320181
30 A = 6802899
41 meter
Y = -6384453
21 meter E =
0013152
Z = -253837
54 I = 51
30160
XDOT = 4577
982596 Wp = 51
90091
YDOT = 1434
992164 meter/sec RA = 291
68714 deg
ZDOT = 5972
019730 TA = 305
35665
MA = 305
47949
Ha = 229
221 n
mi
Hp = 221
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7612143
37 X = 2392634
71
Y = -20946368
79 feet Y = -6358102
14 meter
Z = -832800
31 Z = -242391
83
XDOT = 15019
627941 XDOT = 4532
587372
YDOT = 4707
979542 feet/sec YDOT = 1485
931928 meter/sec
ZDOT = 19593
240585 ZDOT = 5994
147550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21641233
50 X = -6596247
97
Y = -5332693
96 feet Y = -1625405
12 meter
Z = -779766
77 Z = -237672
91
XDOT = 2700
405486 XDOT = 823
083592
YDOT = -13726
038269 feet/sec YDOT = -4183
696465 meter/sec
ZDOT = 19694
898112 ZDOT = 6003
004945
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
50046082
00016717 00000-0 10270-3 0 9047
2 25544 51
6436 292
4732 0002400 97
4997 262
6426 15
49462867 33766
Satellite: ISS
Catalog Number: 25544
Epoch time: 20180
50046082 = yrday
fracday
Element set: 904
Inclination: 51
6436 deg
RA of node: 292
4732 deg
Eccentricity:
0002400
Arg of perigee: 97
4997 deg
Mean anomaly: 262
6426 deg
Mean motion: 15
49462867 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3376
Checksum: 317
Coasting Arc #6 (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 = -1906419
85 A = 6802920
97 meter
Y = 6523584
65 meter E =
0014286
Z = 62694
19 I = 51
28938
XDOT = -4617
101766 Wp = 128
83821
YDOT = -1283
039418 meter/sec RA = 286
71381 deg
ZDOT = -5977
918826 TA = 50
48448
MA = 50
35828
Ha = 229
192 n
mi
Hp = 221
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6254658
30 X = -1979531
36
Y = 21402836
76 feet Y = 6501856
90 meter
Z = 205689
60 Z = 53256
79
XDOT = -15147
971672 XDOT = -4573
374038
YDOT = -4209
446910 feet/sec YDOT = -1334
425910 meter/sec
ZDOT = -19612
594573 ZDOT = -6000
240807
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22013698
88 X = 6709775
42
Y = 3551806
78 feet Y = 1082590
71 meter
Z = 161896
63 Z = 49346
09
XDOT = -2055
974370 XDOT = -626
660988
YDOT = 13815
107634 feet/sec YDOT = 4210
844807 meter/sec
ZDOT = -19715
155856 ZDOT = -6009
179505
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
53239088
00016717 00000-0 10270-3 0 9052
2 25544 51
6427 287
3653 0002403 103
2454 256
8964 15
49464210 33922
Satellite: ISS
Catalog Number: 25544
Epoch time: 20181
53239088 = yrday
fracday
Element set: 905
Inclination: 51
6427 deg
RA of node: 287
3653 deg
Eccentricity:
0002403
Arg of perigee: 103
2454 deg
Mean anomaly: 256
8964 deg
Mean motion: 15
49464210 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3392
Checksum: 308
Coasting Arc #7 (Orbit 3407)
---------------------------------------
Vector Time (GMT): 2020/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1447716
75 A = 6802913
87 meter
Y = -6640942
62 meter E =
0013683
Z = 82612
31 I = 51
28157
XDOT = 4664
878939 Wp = 54
73366
YDOT = 1099
937786 meter/sec RA = 281
73970 deg
ZDOT = 5976
328568 TA = 306
15886
MA = 306
28538
Ha = 229
190 n
mi
Hp = 221
146
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4749726
87 X = 1521468
87
Y = -21787869
49 feet Y = -6624340
86 meter
Z = 271037
77 Z = 89822
94
XDOT = 15304
720929 XDOT = 4623
202807
YDOT = 3608
719769 feet/sec YDOT = 1151
869910 meter/sec
ZDOT = 19607
377191 ZDOT = 5998
887673
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22239839
99 X = -6778703
23
Y = -1625228
62 feet Y = -495369
68 meter
Z = 304586
59 Z = 92837
99
XDOT = 1314
030287 XDOT = 400
516432
YDOT = -13906
580631 feet/sec YDOT = -4238
725776 meter/sec
ZDOT = 19711
042594 ZDOT = 6007
925783
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 20182
56431984
00016717 00000-0 10270-3 0 9066
2 25544 51
6434 282
2578 0002371 103
8092 256
3322 15
49465867 34088
Satellite: ISS
Catalog Number: 25544
Epoch time: 20182
56431984 = yrday
fracday
Element set: 906
Inclination: 51
6434 deg
RA of node: 282
2578 deg
Eccentricity:
0002371
Arg of perigee: 103
8092 deg
Mean anomaly: 256
3322 deg
Mean motion: 15
49465867 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3408
Checksum: 318
Coasting Arc #8 (Orbit 3422)
---------------------------------------
Vector Time (GMT): 2020/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1018680
52 A = 6802875
39 meter
Y = 6714609
94 meter E =
0013622
Z = -275128
98 I = 51
27567
XDOT = -4707
254919 Wp = 132
15148
YDOT = -950
549192 meter/sec RA = 276
76511 deg
ZDOT = -5969
274317 TA = 50
82257
MA = 50
70164
Ha = 229
147 n
mi
Hp = 221
180
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3342127
71 X = -1092353
16
Y = 22029560
18 feet Y = 6702806
45 meter
Z = -902654
15 Z = -280255
16
XDOT = -15443
749733 XDOT = -4667
280404
YDOT = -3118
599712 feet/sec YDOT = -1002
964567 meter/sec
ZDOT = -19584
233322 ZDOT = -5992
043409
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22279844
19 X = 6790896
51
Y = -189888
19 feet Y = -57877
92 meter
Z = -926611
63 Z = -282431
23
XDOT = -673
110099 XDOT = -205
163958
YDOT = 13985
924598 feet/sec YDOT = 4262
909818 meter/sec
ZDOT = -19688
877925 ZDOT = -6001
169992
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 20183
53175104
00016717 00000-0 10270-3 0 9074
2 25544 51
6433 277
4692 0002345 109
5044 250
6360 15
49468341 34237
Satellite: ISS
Catalog Number: 25544
Epoch time: 20183
53175104 = yrday
fracday
Element set: 907
Inclination: 51
6433 deg
RA of node: 277
4692 deg
Eccentricity:
0002345
Arg of perigee: 109
5044 deg
Mean anomaly: 250
6360 deg
Mean motion: 15
49468341 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3423
Checksum: 295
Coasting Arc #9 (Orbit 3438)
---------------------------------------
Vector Time (GMT): 2020/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 550503
78 A = 6802833
83 meter
Y = -6761456
96 meter E =
0014215
Z = 422788
70 I = 51
27356
XDOT = 4755
493854 Wp = 57
47566
YDOT = 768
409202 meter/sec RA = 271
78995 deg
ZDOT = 5957
252826 TA = 307
09750
MA = 307
22734
Ha = 229
155 n
mi
Hp = 221
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1806114
77 X = 624017
83
Y = -22183257
76 feet Y = -6754889
87 meter
Z = 1387102
02 Z = 425640
10
XDOT = 15602
013956 XDOT = 4717
610956
YDOT = 2521
027565 feet/sec YDOT = 821
375585 meter/sec
ZDOT = 19544
792736 ZDOT = 5980
261261
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22155044
40 X = -6752857
53
Y = 2115509
58 feet Y = 644807
32 meter
Z = 1400590
66 Z = 426900
03
XDOT = -71
188517 XDOT = -21
698260
YDOT = -14055
490333 feet/sec YDOT = -4284
113454 meter/sec
ZDOT = 19650
555688 ZDOT = 5989
489374
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 20184
56367540
00016717 00000-0 10270-3 0 9086
2 25544 51
6441 272
3614 0002312 106
4759 253
6646 15
49468547 34392
Satellite: ISS
Catalog Number: 25544
Epoch time: 20184
56367540 = yrday
fracday
Element set: 908
Inclination: 51
6441 deg
RA of node: 272
3614 deg
Eccentricity:
0002312
Arg of perigee: 106
4759 deg
Mean anomaly: 253
6646 deg
Mean motion: 15
49468547 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3439
Checksum: 322
Coasting Arc #10 (Orbit 3453)
---------------------------------------
Vector Time (GMT): 2020/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -118241
25 A = 6802738
85 meter
Y = 6768380
83 meter E =
0012851
Z = -616033
77 I = 51
27208
XDOT = -4802
481585 Wp = 134
36949
YDOT = -616
404687 meter/sec RA = 266
81569 deg
ZDOT = -5936
551159 TA = 52
30169
MA = 52
18524
Ha = 229
139 n
mi
Hp = 221
183
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -387930
62 X = -190926
19
Y = 22205973
85 feet Y = 6766652
29 meter
Z = -2021108
17 Z = -616783
30
XDOT = -15756
173178 XDOT = -4766
395632
YDOT = -2022
325088 feet/sec YDOT = -669
906484 meter/sec
ZDOT = -19476
873882 ZDOT = -5959
792090
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21864501
94 X = 6664300
19
Y = -3896653
03 feet Y = -1187699
84 meter
Z = -2024918
06 Z = -617195
02
XDOT = 729
946930 XDOT = 222
487824
YDOT = 14126
453993 feet/sec YDOT = 4305
743177 meter/sec
ZDOT = -19583
724133 ZDOT = -5969
119116
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 20185
53110371
00016717 00000-0 10270-3 0 9093
2 25544 51
6428 267
5735 0002349 111
8175 248
3226 15
49471273 34541
Satellite: ISS
Catalog Number: 25544
Epoch time: 20185
53110371 = yrday
fracday
Element set: 909
Inclination: 51
6428 deg
RA of node: 267
5735 deg
Eccentricity:
0002349
Arg of perigee: 111
8175 deg
Mean anomaly: 248
3226 deg
Mean motion: 15
49471273 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3454
Checksum: 308
Coasting Arc #11 (Orbit 3469)
---------------------------------------
Vector Time (GMT): 2020/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -348491
33 A = 6802685
17 meter
Y = -6744646
43 meter E =
0014580
Z = 763557
19 I = 51
27478
XDOT = 4851
984743 Wp = 61
00924
YDOT = 427
753966 meter/sec RA = 261
84069 deg
ZDOT = 5913
847386 TA = 307
27017
MA = 307
40303
Ha = 229
139 n
mi
Hp = 221
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1143344
27 X = -276753
67
Y = -22128105
07 feet Y = -6748142
55 meter
Z = 2505108
89 Z = 762037
21
XDOT = 15918
585115 XDOT = 4818
115091
YDOT = 1403
392277 feet/sec YDOT = 481
821712 meter/sec
ZDOT = 19402
386436 ZDOT = 5937
334007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21397548
40 X = -6521972
75
Y = 5756600
00 feet Y = 1754611
68 meter
Z = 2498463
42 Z = 761531
65
XDOT = -1503
898058 XDOT = -458
388128
YDOT = -14170
772037 feet/sec YDOT = -4319
251317 meter/sec
ZDOT = 19510
387981 ZDOT = 5946
766257
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 20186
56302686
00016717 00000-0 10270-3 0 9101
2 25544 51
6427 262
4659 0002295 112
2697 247
8697 15
49462324 34704
Satellite: ISS
Catalog Number: 25544
Epoch time: 20186
56302686 = yrday
fracday
Element set: 910
Inclination: 51
6427 deg
RA of node: 262
4659 deg
Eccentricity:
0002295
Arg of perigee: 112
2697 deg
Mean anomaly: 247
8697 deg
Mean motion: 15
49462324 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3470
Checksum: 329
Coasting Arc #12 (Orbit 3484)
---------------------------------------
Vector Time (GMT): 2020/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 772677
17 A = 6802486
32 meter
Y = 6685575
26 meter E =
0011973
Z = -956255
44 I = 51
27961
XDOT = -4902
814026 Wp = 136
54937
YDOT = -266
823983 meter/sec RA = 256
86625 deg
ZDOT = -5879
668515 TA = 53
83805
MA = 53
72733
Ha = 229
089 n
mi
Hp = 221
211
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2535030
08 X = 702504
52
Y = 21934302
02 feet Y = 6693823
71 meter
Z = -3137320
99 Z = -952671
22
XDOT = -16085
347854 XDOT = -4870
906327
YDOT = -875
406768 feet/sec YDOT = -321
471154 meter/sec
ZDOT = -19290
251034 ZDOT = -5903
406653
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20791513
93 X = 6337253
45
Y = -7440032
62 feet Y = -2267721
94 meter
Z = -3121158
23 Z = -951329
03
XDOT = 2203
627193 XDOT = 671
665569
YDOT = 14223
593890 feet/sec YDOT = 4335
351418 meter/sec
ZDOT = -19399
429578 ZDOT = -5912
946135
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 20187
53045224
00016717 00000-0 10270-3 0 9112
2 25544 51
6420 257
6776 0002292 116
3077 243
8309 15
49481791 34858
Satellite: ISS
Catalog Number: 25544
Epoch time: 20187
53045224 = yrday
fracday
Element set: 911
Inclination: 51
6420 deg
RA of node: 257
6776 deg
Eccentricity:
0002292
Arg of perigee: 116
3077 deg
Mean anomaly: 243
8309 deg
Mean motion: 15
49481791 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3485
Checksum: 314
Coasting Arc #13 (Orbit 3500)
---------------------------------------
Vector Time (GMT): 2020/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1224727
33 A = 6802429
19 meter
Y = -6593073
82 meter E =
0014975
Z = 1104404
17 I = 51
28794
XDOT = 4952
174281 Wp = 64
36469
YDOT = 68
699874 meter/sec RA = 251
89150 deg
ZDOT = 5845
984414 TA = 307
65558
MA = 307
79134
Ha = 229
130 n
mi
Hp = 221
244
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4018134
27 X = -1156275
04
Y = -21630819
62 feet Y = -6606387
06 meter
Z = 3623373
26 Z = 1098620
08
XDOT = 16247
290947 XDOT = 4922
642123
YDOT = 225
393286 feet/sec YDOT = 123
912411 meter/sec
ZDOT = 19179
738890 ZDOT = 5869
967954
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20005728
86 X = -6097746
16
Y = 9165071
56 feet Y = 2793513
81 meter
Z = 3597064
12 Z = 1096385
14
XDOT = -3018
245214 XDOT = -919
961141
YDOT = -14231
606270 feet/sec YDOT = -4337
793591 meter/sec
ZDOT = 19290
067431 ZDOT = 5879
612553
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 20188
56237170
00016717 00000-0 10270-3 0 9120
2 25544 51
6420 252
5694 0002272 113
5354 246
6036 15
49460447 35018
Satellite: ISS
Catalog Number: 25544
Epoch time: 20188
56237170 = yrday
fracday
Element set: 912
Inclination: 51
6420 deg
RA of node: 252
5694 deg
Eccentricity:
0002272
Arg of perigee: 113
5354 deg
Mean anomaly: 246
6036 deg
Mean motion: 15
49460447 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3501
Checksum: 292
Coasting Arc #14 (Orbit 3515)
---------------------------------------
Vector Time (GMT): 2020/189/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1629243
68 A = 6802142
34 meter
Y = 6471427
56 meter E =
0011084
Z = -1295878
44 I = 51
29781
XDOT = -5004
303464 Wp = 137
20692
YDOT = 106
338268 meter/sec RA = 246
91818 deg
ZDOT = -5797
925849 TA = 56
93146
MA = 56
82507
Ha = 229
096 n
mi
Hp = 221
187
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5345287
66 X = 1563051
65
Y = 21231717
71 feet Y = 6489277
03 meter
Z = -4251569
69 Z = -1288124
10
XDOT = -16418
318451 XDOT = -4976
958257
YDOT = 348
878831 feet/sec YDOT = 50
530416 meter/sec
ZDOT = -19022
066433 ZDOT = -5822
167836
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19114725
66 X = 5826168
38
Y = -10690415
33 feet Y = -3258438
59 meter
Z = -4216167
09 Z = -1285087
73
XDOT = 3775
628043 XDOT = 1150
811428
YDOT = 14248
301109 feet/sec YDOT = 4342
882178 meter/sec
ZDOT = -19133
602532 ZDOT = -5831
922052
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 20189
52979455
00016717 00000-0 10270-3 0 9137
2 25544 51
6409 247
7810 0002347 117
2766 242
8624 15
49491549 35166
Satellite: ISS
Catalog Number: 25544
Epoch time: 20189
52979455 = yrday
fracday
Element set: 913
Inclination: 51
6409 deg
RA of node: 247
7810 deg
Eccentricity:
0002347
Arg of perigee: 117
2766 deg
Mean anomaly: 242
8624 deg
Mean motion: 15
49491549 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3516
Checksum: 337
Coasting Arc #15 (Orbit 3531)
---------------------------------------
Vector Time (GMT): 2020/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2056660
38 A = 6802090
28 meter
Y = -6314572
92 meter E =
0015188
Z = 1442064
26 I = 51
31093
XDOT = 5050
027218 Wp = 68
50874
YDOT = -320
922166 meter/sec RA = 241
94507 deg
ZDOT = 5753
435335 TA = 307
26611
MA = 307
40452
Ha = 229
135 n
mi
Hp = 221
274
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6747573
42 X = -1992900
65
Y = -20717102
76 feet Y = -6337215
66 meter
Z = 4731181
94 Z = 1432228
00
XDOT = 16568
330769 XDOT = 5025
294264
YDOT = -1052
894246 feet/sec YDOT = -264
588250 meter/sec
ZDOT = 18876
100182 ZDOT = 5777
905739
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18045923
93 X = -5500397
61
Y = 12226880
85 feet Y = 3726753
28 meter
Z = 4686170
14 Z = 1428344
66
XDOT = -4650
357019 XDOT = -1417
428820
YDOT = -14196
682064 feet/sec YDOT = -4327
148693 meter/sec
ZDOT = 18988
705636 ZDOT = 5787
757478
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 20190
56171338
00016717 00000-0 10270-3 0 9148
2 25544 51
6402 242
6730 0002313 118
4354 241
7029 15
49455699 35324
Satellite: ISS
Catalog Number: 25544
Epoch time: 20190
56171338 = yrday
fracday
Element set: 914
Inclination: 51
6402 deg
RA of node: 242
6730 deg
Eccentricity:
0002313
Arg of perigee: 118
4354 deg
Mean anomaly: 241
7029 deg
Mean motion: 15
49455699 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3532
Checksum: 296
Coasting Arc #16 (Orbit 3535)
---------------------------------------
Vector Time (GMT): 2020/190/18:21:00
000
Vector Time (MET): N/A
Weight (LBS) : 964251
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 924579
45 A = 6795456
71 meter
Y = -5244072
66 meter E =
0012393
Z = 4213875
18 I = 51
29230
XDOT = 5519
853464 Wp = 107
29610
YDOT = 3893
257406 meter/sec RA = 240
64121 deg
ZDOT = 3621
471724 TA = 305
38003
MA = 305
49576
Ha = 229
135 n
mi
Hp = 221
256
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3033397
15 X = 962683
37
Y = -17204962
81 feet Y = -5233520
86 meter
Z = 13825049
80 Z = 4218458
18
XDOT = 18109
755459 XDOT = 5458
317003
YDOT = 12773
154218 feet/sec YDOT = 3954
639790 meter/sec
ZDOT = 11881
468911 ZDOT = 3648
135492
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3573563
45 X = 1089222
14
Y = 17083700
10 feet Y = 5207111
79 meter
Z = 13846338
17 Z = 4220363
87
XDOT = -20210
548764 XDOT = -6160
175263
YDOT = -5534
722438 feet/sec YDOT = -1686
983399 meter/sec
ZDOT = 12004
007940 ZDOT = 3658
821620
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 20190
81969371
00016717 00000-0 10270-3 0 9159
2 25544 51
6396 241
3967 0002298 113
9027 246
2364 15
49446772 35361
Satellite: ISS
Catalog Number: 25544
Epoch time: 20190
81969371 = yrday
fracday
Element set: 915
Inclination: 51
6396 deg
RA of node: 241
3967 deg
Eccentricity:
0002298
Arg of perigee: 113
9027 deg
Mean anomaly: 246
2364 deg
Mean motion: 15
49446772 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3536
Checksum: 334
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