[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 22nd 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 3282)
---------------------------------------
Vector Time (GMT): 2020/174/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 980069
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4566890
86 A = 6802352
84 meter
Y = -4884291
78 meter E =
0010912
Z = -1228282
10 I = 51
41834
XDOT = 4273
207153 Wp = 46
65742
YDOT = 2540
371327 meter/sec RA = 321
50304 deg
ZDOT = 5826
467290 TA = 299
97996
MA = 300
08822
Ha = 229
243 n
mi
Hp = 221
178
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14983237
72 X = 4627135
29
Y = -16024579
32 feet Y = -4832884
44 meter
Z = -4029796
92 Z = -1205952
81
XDOT = 14019
708507 XDOT = 4216
180944
YDOT = 8334
551597 feet/sec YDOT = 2587
837281 meter/sec
ZDOT = 19115
706332 ZDOT = 5847
086744
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16084557
64 X = -4902573
17
Y = -14946291
88 feet Y = -4555629
77 meter
Z = -3926726
70 Z = -1196866
30
XDOT = 7190
231281 XDOT = 2191
582494
YDOT = -12749
377811 feet/sec YDOT = -3886
010357 meter/sec
ZDOT = 19210
327282 ZDOT = 5855
307756
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
50232802
00016717 00000-0 10270-3 0 9003
2 25544 51
6417 322
1616 0002344 84
7470 275
3947 15
49450652 32834
Satellite: ISS
Catalog Number: 25544
Epoch time: 20174
50232802 = yrday
fracday
Element set: 900
Inclination: 51
6417 deg
RA of node: 322
1616 deg
Eccentricity:
0002344
Arg of perigee: 84
7470 deg
Mean anomaly: 275
3947 deg
Mean motion: 15
49450652 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3283
Checksum: 291
Coasting Arc #2 (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 = -4260144
50 A = 6802505
84 meter
Y = 5190031
54 meter E =
0015363
Z = 1047645
91 I = 51
39325
XDOT = -4327
023963 Wp = 118
51024
YDOT = -2355
310940 meter/sec RA = 316
53699 deg
ZDOT = -5868
667742 TA = 50
11204
MA = 49
97705
Ha = 229
170 n
mi
Hp = 221
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13976852
05 X = -4322953
16
Y = 17027662
52 feet Y = 5142040
17 meter
Z = 3437158
51 Z = 1026800
55
XDOT = -14196
272846 XDOT = -4271
858295
YDOT = -7727
398097 feet/sec YDOT = -2403
389159 meter/sec
ZDOT = -19254
159257 ZDOT = -5889
552981
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17320688
25 X = 5279345
78
Y = 13635977
86 feet Y = 4156246
05 meter
Z = 3340899
44 Z = 1018306
15
XDOT = -6434
340300 XDOT = -1961
186924
YDOT = 12962
309165 feet/sec YDOT = 3950
911834 meter/sec
ZDOT = -19350
021898 ZDOT = -5897
886674
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
53426911
00016717 00000-0 10270-3 0 9014
2 25544 51
6417 317
0532 0002236 86
6859 273
4547 15
49457809 32999
Satellite: ISS
Catalog Number: 25544
Epoch time: 20175
53426911 = yrday
fracday
Element set: 901
Inclination: 51
6417 deg
RA of node: 317
0532 deg
Eccentricity:
0002236
Arg of perigee: 86
6859 deg
Mean anomaly: 273
4547 deg
Mean motion: 15
49457809 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3299
Checksum: 327
Coasting Arc #3 (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 = 3900131
95 A = 6802610
51 meter
Y = -5493458
16 meter E =
0011708
Z = -910025
01 I = 51
37150
XDOT = 4390
982404 Wp = 47
65839
YDOT = 2150
025834 meter/sec RA = 311
56976 deg
ZDOT = 5896
247919 TA = 302
47531
MA = 302
58843
Ha = 229
228 n
mi
Hp = 221
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12795708
50 X = 3965691
89
Y = -18023156
68 feet Y = -5449477
37 meter
Z = -2985646
35 Z = -890921
76
XDOT = 14406
110249 XDOT = 4337
973662
YDOT = 7053
890532 feet/sec YDOT = 2198
831442 meter/sec
ZDOT = 19344
645405 ZDOT = 5917
448934
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18501963
06 X = -5639398
34
Y = -12114491
80 feet Y = -3692497
10 meter
Z = -2897389
94 Z = -883124
45
XDOT = 5618
453635 XDOT = 1712
504668
YDOT = -13185
048719 feet/sec YDOT = -4018
802850 meter/sec
ZDOT = 19441
980878 ZDOT = 5925
915772
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
50171175
00016717 00000-0 10270-3 0 9022
2 25544 51
6432 312
2651 0002345 88
4417 271
7002 15
49456818 33140
Satellite: ISS
Catalog Number: 25544
Epoch time: 20176
50171175 = yrday
fracday
Element set: 902
Inclination: 51
6432 deg
RA of node: 312
2651 deg
Eccentricity:
0002345
Arg of perigee: 88
4417 deg
Mean anomaly: 271
7002 deg
Mean motion: 15
49456818 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3314
Checksum: 286
Coasting Arc #4 (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 = -3549018
14 A = 6802718
25 meter
Y = 5750355
59 meter E =
0015138
Z = 724535
87 I = 51
34945
XDOT = -4434
168295 Wp = 122
02796
YDOT = -1979
396686 meter/sec RA = 306
60124 deg
ZDOT = -5926
926576 TA = 50
12608
MA = 49
99305
Ha = 229
188 n
mi
Hp = 221
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11643760
30 X = -3616575
88
Y = 18865996
02 feet Y = 5710290
08 meter
Z = 2377086
19 Z = 707133
25
XDOT = -14547
796245 XDOT = -4382
915380
YDOT = -6494
083617 feet/sec YDOT = -2028
695184 meter/sec
ZDOT = -19445
297166 ZDOT = -5948
341532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19484874
47 X = 5938989
74
Y = 10593326
69 feet Y = 3228845
98 meter
Z = 2296648
62 Z = 700018
50
XDOT = -4911
632510 XDOT = -1497
065589
YDOT = 13332
728716 feet/sec YDOT = 4063
815713 meter/sec
ZDOT = -19543
633419 ZDOT = -5956
899466
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
53364802
00016717 00000-0 10270-3 0 9038
2 25544 51
6422 307
1574 0002328 91
9784 268
1633 15
49463802 33302
Satellite: ISS
Catalog Number: 25544
Epoch time: 20177
53364802 = yrday
fracday
Element set: 903
Inclination: 51
6422 deg
RA of node: 307
1574 deg
Eccentricity:
0002328
Arg of perigee: 91
9784 deg
Mean anomaly: 268
1633 deg
Mean motion: 15
49463802 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3330
Checksum: 304
Coasting Arc #5 (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 = 3145905
09 A = 6802806
59 meter
Y = -5998035
67 meter E =
0012399
Z = -583702
18 I = 51
33097
XDOT = 4488
517338 Wp = 49
64407
YDOT = 1784
546053 meter/sec RA = 301
63122 deg
ZDOT = 5945
055490 TA = 304
04221
MA = 304
15989
Ha = 229
219 n
mi
Hp = 221
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10321210
93 X = 3215578
36
Y = -19678594
72 feet Y = -5962466
27 meter
Z = -1915033
40 Z = -568252
42
XDOT = 14726
106752 XDOT = 4439
351159
YDOT = 5854
809884 feet/sec YDOT = 1834
464131 meter/sec
ZDOT = 19504
775231 ZDOT = 5966
739472
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20378210
77 X = -6211278
64
Y = -8875335
83 feet Y = -2705202
36 meter
Z = -1843577
51 Z = -561922
43
XDOT = 4131
766777 XDOT = 1259
362514
YDOT = -13494
104450 feet/sec YDOT = -4113
003036 meter/sec
ZDOT = 19604
365532 ZDOT = 5975
410614
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
50108725
00016717 00000-0 10270-3 0 9047
2 25544 51
6426 302
3694 0002344 94
5237 265
6181 15
49456920 33455
Satellite: ISS
Catalog Number: 25544
Epoch time: 20178
50108725 = yrday
fracday
Element set: 904
Inclination: 51
6426 deg
RA of node: 302
3694 deg
Eccentricity:
0002344
Arg of perigee: 94
5237 deg
Mean anomaly: 265
6181 deg
Mean motion: 15
49456920 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3345
Checksum: 306
Coasting Arc #6 (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 = -2758434
80 A = 6802846
32 meter
Y = 6198861
19 meter E =
0014707
Z = 394871
60 I = 51
31460
XDOT = -4527
387171 Wp = 125
94046
YDOT = -1625
326485 meter/sec RA = 296
65965 deg
ZDOT = -5963
707665 TA = 49
79099
MA = 49
66238
Ha = 229
144 n
mi
Hp = 221
182
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9049982
92 X = -2829465
34
Y = 20337471
08 feet Y = 6167617
20 meter
Z = 1295510
51 Z = 381300
57
XDOT = -14853
632452 XDOT = -4479
907840
YDOT = -5332
435973 feet/sec YDOT = -1675
688770 meter/sec
ZDOT = -19565
970031 ZDOT = -5985
584582
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21069405
80 X = 6421954
89
Y = 7194015
63 feet Y = 2192735
96 meter
Z = 1232698
99 Z = 375726
65
XDOT = -3464
301878 XDOT = -1055
919212
YDOT = 13603
326803 feet/sec YDOT = 4146
294010 meter/sec
ZDOT = -19666
460258 ZDOT = -5994
337087
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
53301957
00016717 00000-0 10270-3 0 9054
2 25544 51
6427 297
2613 0002268 99
1998 260
9409 15
49470047 33614
Satellite: ISS
Catalog Number: 25544
Epoch time: 20179
53301957 = yrday
fracday
Element set: 905
Inclination: 51
6427 deg
RA of node: 297
2613 deg
Eccentricity:
0002268
Arg of perigee: 99
1998 deg
Mean anomaly: 260
9409 deg
Mean motion: 15
49470047 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3361
Checksum: 332
Coasting Arc #7 (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 = 2322992
93 A = 6802890
53 meter
Y = -6383569
82 meter E =
0013132
Z = -250125
42 I = 51
30156
XDOT = 4576
165303 Wp = 51
89243
YDOT = 1439
992208 meter/sec RA = 291
68685 deg
ZDOT = 5972
212697 TA = 305
40526
MA = 305
52784
Ha = 229
206 n
mi
Hp = 221
129
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7621367
89 X = 2395418
22
Y = -20943470
54 feet Y = -6357187
47 meter
Z = -820621
47 Z = -238666
13
XDOT = 15013
665691 XDOT = 4530
713364
YDOT = 4724
383886 feet/sec YDOT = 1490
911333 meter/sec
ZDOT = 19593
873678 ZDOT = 5994
331552
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21639329
32 X = -6595667
58
Y = -5342092
96 feet Y = -1628269
93 meter
Z = -767525
50 Z = -233941
77
XDOT = 2716
668697 XDOT = 828
040619
YDOT = -13722
000180 feet/sec YDOT = -4182
465655 meter/sec
ZDOT = 19695
489667 ZDOT = 6003
185251
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
50045364
00016717 00000-0 10270-3 0 9061
2 25544 51
6436 292
4729 0002375 97
8854 262
2566 15
49466158 33767
Satellite: ISS
Catalog Number: 25544
Epoch time: 20180
50045364 = yrday
fracday
Element set: 906
Inclination: 51
6436 deg
RA of node: 292
4729 deg
Eccentricity:
0002375
Arg of perigee: 97
8854 deg
Mean anomaly: 262
2566 deg
Mean motion: 15
49466158 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3376
Checksum: 332
Coasting Arc #8 (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 = -1910081
61 A = 6802910
71 meter
Y = 6522546
88 meter E =
0014261
Z = 57900
11 I = 51
28934
XDOT = -4615
169161 Wp = 128
97543
YDOT = -1289
689148 meter/sec RA = 286
71350 deg
ZDOT = -5977
987918 TA = 50
39905
MA = 50
27322
Ha = 229
176 n
mi
Hp = 221
151
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6266671
94 X = -1983157
95
Y = 21399432
03 feet Y = 6500778
38 meter
Z = 189960
98 Z = 48445
01
XDOT = -15141
631106 XDOT = -4571
366883
YDOT = -4231
263608 feet/sec YDOT = -1341
053611 meter/sec
ZDOT = -19612
821254 ZDOT = -6000
300332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22011796
98 X = 6709195
72
Y = 3564043
50 feet Y = 1086320
46 meter
Z = 146086
68 Z = 44527
22
XDOT = -2077
517094 XDOT = -633
227210
YDOT = 13811
660486 feet/sec YDOT = 4209
794116 meter/sec
ZDOT = -19715
338136 ZDOT = -6009
235064
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
53238141
00016717 00000-0 10270-3 0 9073
2 25544 51
6426 287
3649 0002378 103
6393 256
5022 15
49467785 33925
Satellite: ISS
Catalog Number: 25544
Epoch time: 20181
53238141 = yrday
fracday
Element set: 907
Inclination: 51
6426 deg
RA of node: 287
3649 deg
Eccentricity:
0002378
Arg of perigee: 103
6393 deg
Mean anomaly: 256
5022 deg
Mean motion: 15
49467785 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3392
Checksum: 322
Coasting Arc #9 (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 = 1452419
51 A = 6802902
18 meter
Y = -6639823
27 meter E =
0013668
Z = 88688
47 I = 51
28153
XDOT = 4663
019773 Wp = 54
73604
YDOT = 1108
471161 meter/sec RA = 281
73938 deg
ZDOT = 5976
214182 TA = 306
22214
MA = 306
34841
Ha = 229
174 n
mi
Hp = 221
151
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4765155
87 X = 1526129
25
Y = -21784197
08 feet Y = -6623169
15 meter
Z = 290972
66 Z = 95921
84
XDOT = 15298
621304 XDOT = 4621
248913
YDOT = 3636
716408 feet/sec YDOT = 1160
381966 meter/sec
ZDOT = 19607
001911 ZDOT = 5998
764028
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22238361
59 X = -6778252
61
Y = -1640886
76 feet Y = -500142
28 meter
Z = 324625
99 Z = 98946
00
XDOT = 1341
465346 XDOT = 408
878638
YDOT = -13904
603828 feet/sec YDOT = -4238
123247 meter/sec
ZDOT = 19710
624230 ZDOT = 6007
798265
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
56430792
00016717 00000-0 10270-3 0 9084
2 25544 51
6434 282
2574 0002345 104
1735 255
9676 15
49469703 34083
Satellite: ISS
Catalog Number: 25544
Epoch time: 20182
56430792 = yrday
fracday
Element set: 908
Inclination: 51
6434 deg
RA of node: 282
2574 deg
Eccentricity:
0002345
Arg of perigee: 104
1735 deg
Mean anomaly: 255
9676 deg
Mean motion: 15
49469703 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3408
Checksum: 321
Coasting Arc #10 (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 = -1024403
68 A = 6802861
74 meter
Y = 6713428
44 meter E =
0013588
Z = -282441
69 I = 51
27562
XDOT = -4705
677939 Wp = 132
29693
YDOT = -961
001311 meter/sec RA = 276
76476 deg
ZDOT = -5968
844374 TA = 50
75625
MA = 50
63574
Ha = 229
130 n
mi
Hp = 221
184
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3360904
47 X = -1098027
16
Y = 22025683
86 feet Y = 6701561
22 meter
Z = -926645
98 Z = -287595
55
XDOT = -15438
575916 XDOT = -4665
588751
YDOT = -3152
891439 feet/sec YDOT = -1013
398409 meter/sec
ZDOT = -19582
822750 ZDOT = -5991
605529
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22278958
84 X = 6790626
65
Y = -170896
40 feet Y = -52089
22 meter
Z = -950730
68 Z = -289782
71
XDOT = -706
401989 XDOT = -215
311326
YDOT = 13986
313037 feet/sec YDOT = 4263
028214 meter/sec
ZDOT = -19687
430256 ZDOT = -6000
728742
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
53173666
00016717 00000-0 10270-3 0 9097
2 25544 51
6433 277
4688 0002320 109
8815 250
2585 15
49472401 34231
Satellite: ISS
Catalog Number: 25544
Epoch time: 20183
53173666 = yrday
fracday
Element set: 909
Inclination: 51
6433 deg
RA of node: 277
4688 deg
Eccentricity:
0002320
Arg of perigee: 109
8815 deg
Mean anomaly: 250
2585 deg
Mean motion: 15
49472401 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3423
Checksum: 312
Coasting Arc #11 (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 = 557430
85 A = 6802818
02 meter
Y = -6760316
74 meter E =
0014203
Z = 431521
41 I = 51
27351
XDOT = 4754
473510 Wp = 57
49828
YDOT = 780
956548 meter/sec RA = 271
78958 deg
ZDOT = 5956
454220 TA = 307
16957
MA = 307
29918
Ha = 229
137 n
mi
Hp = 221
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1828841
38 X = 630889
22
Y = -22179516
88 feet Y = -6753672
50 meter
Z = 1415752
65 Z = 434406
33
XDOT = 15598
666370 XDOT = 4716
454259
YDOT = 2562
193399 feet/sec YDOT = 833
910758 meter/sec
ZDOT = 19542
172637 ZDOT = 5979
457369
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22155305
00 X = -6752936
97
Y = 2092671
59 feet Y = 637846
30 meter
Z = 1429395
34 Z = 435679
70
XDOT = -31
741178 XDOT = -9
674711
YDOT = -14059
401412 feet/sec YDOT = -4285
305550 meter/sec
ZDOT = 19647
910587 ZDOT = 5988
683147
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
56365825
00016717 00000-0 10270-3 0 9103
2 25544 51
6441 272
3610 0002285 106
7861 253
3541 15
49472870 34399
Satellite: ISS
Catalog Number: 25544
Epoch time: 20184
56365825 = yrday
fracday
Element set: 910
Inclination: 51
6441 deg
RA of node: 272
3610 deg
Eccentricity:
0002285
Arg of perigee: 106
7861 deg
Mean anomaly: 253
3541 deg
Mean motion: 15
49472870 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3439
Checksum: 306
Coasting Arc #12 (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 = -126346
16 A = 6802720
49 meter
Y = 6767306
59 meter E =
0012805
Z = -626107
31 I = 51
27202
XDOT = -4802
232796 Wp = 134
51423
YDOT = -630
994249 meter/sec RA = 266
81529 deg
ZDOT = -5935
211015 TA = 52
26655
MA = 52
15057
Ha = 229
122 n
mi
Hp = 221
187
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -414521
51 X = -198969
55
Y = 22202449
43 feet Y = 6765487
76 meter
Z = -2054157
83 Z = -626896
06
XDOT = -15755
356942 XDOT = -4765
990227
YDOT = -2070
191107 feet/sec YDOT = -684
492389 meter/sec
ZDOT = -19472
477084 ZDOT = -5958
450360
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21866103
76 X = 6664788
43
Y = -3870101
57 feet Y = -1179606
96 meter
Z = -2058148
04 Z = -627323
52
XDOT = 684
757022 XDOT = 208
713940
YDOT = 14134
756468 feet/sec YDOT = 4308
273772 meter/sec
ZDOT = -19579
319260 ZDOT = -5967
776510
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
53108385
00016717 00000-0 10270-3 0 9118
2 25544 51
6427 267
5731 0002322 112
1304 248
0093 15
49475730 34546
Satellite: ISS
Catalog Number: 25544
Epoch time: 20185
53108385 = yrday
fracday
Element set: 911
Inclination: 51
6427 deg
RA of node: 267
5731 deg
Eccentricity:
0002322
Arg of perigee: 112
1304 deg
Mean anomaly: 248
0093 deg
Mean motion: 15
49475730 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3454
Checksum: 288
Coasting Arc #13 (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 = -339026
14 A = 6802663
67 meter
Y = -6743778
28 meter E =
0014571
Z = 775148
12 I = 51
27472
XDOT = 4852
850027 Wp = 61
06108
YDOT = 444
504975 meter/sec RA = 261
84027 deg
ZDOT = 5911
927144 TA = 307
34496
MA = 307
47761
Ha = 229
120 n
mi
Hp = 221
224
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1112290
49 X = -267355
19
Y = -22125256
83 feet Y = -6747168
94 meter
Z = 2543136
86 Z = 773673
95
XDOT = 15921
423972 XDOT = 4818
802323
YDOT = 1458
349656 feet/sec YDOT = 498
581402 meter/sec
ZDOT = 19396
086430 ZDOT = 5935
417539
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21401192
74 X = -6523083
55
Y = 5725890
05 feet Y = 1745251
29 meter
Z = 2536702
08 Z = 773186
79
XDOT = -1452
994454 XDOT = -442
872709
YDOT = -14184
803168 feet/sec YDOT = -4323
528006 meter/sec
ZDOT = 19504
104476 ZDOT = 5944
851044
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
56300398
00016717 00000-0 10270-3 0 9121
2 25544 51
6426 262
4655 0002268 112
5628 247
5762 15
49467109 34702
Satellite: ISS
Catalog Number: 25544
Epoch time: 20186
56300398 = yrday
fracday
Element set: 912
Inclination: 51
6426 deg
RA of node: 262
4655 deg
Eccentricity:
0002268
Arg of perigee: 112
5628 deg
Mean anomaly: 247
5762 deg
Mean motion: 15
49467109 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3470
Checksum: 317
Coasting Arc #14 (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 = 761874
91 A = 6802461
80 meter
Y = 6684942
55 meter E =
0011915
Z = -969260
39 I = 51
27954
XDOT = -4904
986406 Wp = 136
68036
YDOT = -285
604677 meter/sec RA = 256
86580 deg
ZDOT = -5876
955256 TA = 53
84994
MA = 53
73975
Ha = 229
071 n
mi
Hp = 221
215
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2499589
62 X = 691773
31
Y = 21932226
20 feet Y = 6693070
61 meter
Z = -3179988
15 Z = -965728
47
XDOT = -16092
475084 XDOT = -4872
881714
YDOT = -937
023219 feet/sec YDOT = -340
275040 meter/sec
ZDOT = -19281
349265 ZDOT = -5900
703471
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20797420
96 X = 6339053
91
Y = -7405321
54 feet Y = -2257142
01 meter
Z = -3164065
93 Z = -964407
29
XDOT = 2147
753653 XDOT = 654
635313
YDOT = 14244
069628 feet/sec YDOT = 4341
592423 meter/sec
ZDOT = -19390
573255 ZDOT = -5910
246728
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
53042641
00016717 00000-0 10270-3 0 9134
2 25544 51
6420 257
6771 0002264 116
5872 243
5511 15
49486558 34855
Satellite: ISS
Catalog Number: 25544
Epoch time: 20187
53042641 = yrday
fracday
Element set: 913
Inclination: 51
6420 deg
RA of node: 257
6771 deg
Eccentricity:
0002264
Arg of perigee: 116
5872 deg
Mean anomaly: 243
5511 deg
Mean motion: 15
49486558 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3485
Checksum: 313
Coasting Arc #15 (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 = -1212416
68 A = 6802400
44 meter
Y = -6592853
87 meter E =
0014967
Z = 1118983
80 I = 51
28785
XDOT = 4956
044392 Wp = 64
45211
YDOT = 89
551915 meter/sec RA = 251
89102 deg
ZDOT = 5842
453124 TA = 307
72934
MA = 307
86490
Ha = 229
111 n
mi
Hp = 221
247
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3977745
03 X = -1144038
59
Y = -21630098
01 feet Y = -6606029
86 meter
Z = 3671206
68 Z = 1113259
32
XDOT = 16259
988162 XDOT = 4926
295926
YDOT = 293
805495 feet/sec YDOT = 144
806522 meter/sec
ZDOT = 19168
153294 ZDOT = 5866
454942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20014736
58 X = -6100491
71
Y = 9126028
50 feet Y = 2781613
49 meter
Z = 3645171
79 Z = 1111048
36
XDOT = -2957
817321 XDOT = -901
542719
YDOT = -14259
926109 feet/sec YDOT = -4346
425478 meter/sec
ZDOT = 19278
564971 ZDOT = 5876
106603
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
56234261
00016717 00000-0 10270-3 0 9140
2 25544 51
6419 252
5689 0002244 113
7536 246
3849 15
49465626 35016
Satellite: ISS
Catalog Number: 25544
Epoch time: 20188
56234261 = yrday
fracday
Element set: 914
Inclination: 51
6419 deg
RA of node: 252
5689 deg
Eccentricity:
0002244
Arg of perigee: 113
7536 deg
Mean anomaly: 246
3849 deg
Mean motion: 15
49465626 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3501
Checksum: 320
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