[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
November 17th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14531 28 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 114 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 940 ET - UTC (sec) : 67 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
329/19:52:48
707 4
7 5
2 5
2
N/A 0
7 -0
6 220
0
000/00:13:37
414 2
1 -0
1 215
5
Coasting Arc #1 (Orbit 1173)
---------------------------------------
Vector Time (GMT): 2015/320/11:27:21
181
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4188723
60 A = 6775454
51 meter
Y = 1538153
30 meter E =
0007992
Z = 5091390
61 I = 51
88329
XDOT = -4378
382256 Wp = 103
46474
YDOT = -6050
428818 meter/sec RA = 43
36988 deg
ZDOT = -1773
725126 TA = 3
61761
MA = 3
61184
Ha = 221
275 n
mi
Hp = 211
648
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13742531
51 X = -4230344
73
Y = 5046434
70 feet Y = 1491079
35 meter
Z = 16704037
44 Z = 5070941
25
XDOT = -14364
771182 XDOT = -4301
783249
YDOT = -19850
488248 feet/sec YDOT = -6098
962433 meter/sec
ZDOT = -5819
308156 ZDOT = -1794
808905
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5938377
72 X = 1810017
53
Y = -13491289
53 feet Y = -4112145
05 meter
Z = 16615333
86 Z = 5064353
76
XDOT = 23261
345570 XDOT = 7090
058130
YDOT = 2959
167365 feet/sec YDOT = 901
954213 meter/sec
ZDOT = -5909
209345 ZDOT = -1801
127008
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 15320
52244061
00016717 00000-0 10270-3 0 9002
2 25544 51
6446 43
7957 0005986 146
5526 213
6006 15
55145108 11746
Satellite: ISS
Catalog Number: 25544
Epoch time: 15320
52244061 = yrday
fracday
Element set: 900
Inclination: 51
6446 deg
RA of node: 43
7957 deg
Eccentricity:
0005986
Arg of perigee: 146
5526 deg
Mean anomaly: 213
6006 deg
Mean motion: 15
55145108 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1174
Checksum: 292
Coasting Arc #2 (Orbit 1188)
---------------------------------------
Vector Time (GMT): 2015/321/11:27:21
181
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5380762
99 A = 6779187
32 meter
Y = 120935
05 meter E =
0012601
Z = -4135932
05 I = 51
87173
XDOT = 2792
787737 Wp = 126
73427
YDOT = 6027
587375 meter/sec RA = 38
38410 deg
ZDOT = 3810
297786 TA = 182
49677
MA = 182
50307
Ha = 221
062 n
mi
Hp = 211
818
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17653421
89 X = 5399101
81
Y = 396768
54 feet Y = 181208
92 meter
Z = -13569330
87 Z = -4109748
48
XDOT = 9162
689427 XDOT = 2706
668993
YDOT = 19775
549132 feet/sec YDOT = 6058
336568 meter/sec
ZDOT = 12500
976989 ZDOT = 3823
655728
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12343057
77 X = -3762164
01
Y = 12747847
35 feet Y = 3885543
87 meter
Z = -13456180
10 Z = -4101443
70
XDOT = -19752
414372 XDOT = -6020
535901
YDOT = -5872
380243 feet/sec YDOT = -1789
901498 meter/sec
ZDOT = 12557
482016 ZDOT = 3827
520519
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 15321
48634777
00016717 00000-0 10270-3 0 9016
2 25544 51
6442 38
9839 0006027 149
6967 210
4535 15
55167294 11895
Satellite: ISS
Catalog Number: 25544
Epoch time: 15321
48634777 = yrday
fracday
Element set: 901
Inclination: 51
6442 deg
RA of node: 38
9839 deg
Eccentricity:
0006027
Arg of perigee: 149
6967 deg
Mean anomaly: 210
4535 deg
Mean motion: 15
55167294 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1189
Checksum: 335
Coasting Arc #3 (Orbit 1204)
---------------------------------------
Vector Time (GMT): 2015/322/11:27:21
181
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6069465
16 A = 6783650
14 meter
Y = -1623013
82 meter E =
0018293
Z = 2530796
03 I = 51
86078
XDOT = -754
148968 Wp = 118
14716
YDOT = -5492
677680 meter/sec RA = 33
41002 deg
ZDOT = -5310
410113 TA = 33
48936
MA = 33
37383
Ha = 221
069 n
mi
Hp = 211
781
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19912943
45 X = -6063158
92
Y = -5324848
50 feet Y = -1690851
35 meter
Z = 8303136
59 Z = 2501326
74
XDOT = -2474
242020 XDOT = -666
876199
YDOT = -18020
596064 feet/sec YDOT = -5500
623052 meter/sec
ZDOT = -17422
605358 ZDOT = -5313
861733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17279282
91 X = 5266725
43
Y = -11331339
91 feet Y = -3453792
40 meter
Z = 8176094
65 Z = 2492073
65
XDOT = 14181
379568 XDOT = 4322
484492
YDOT = 8994
375832 feet/sec YDOT = 2741
485754 meter/sec
ZDOT = -17436
396312 ZDOT = -5314
613596
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 15322
51449534
00016717 00000-0 10270-3 0 9027
2 25544 51
6439 33
8504 0005957 152
0220 208
1255 15
55176251 12050
Satellite: ISS
Catalog Number: 25544
Epoch time: 15322
51449534 = yrday
fracday
Element set: 902
Inclination: 51
6439 deg
RA of node: 33
8504 deg
Eccentricity:
0005957
Arg of perigee: 152
0220 deg
Mean anomaly: 208
1255 deg
Mean motion: 15
55176251 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1205
Checksum: 281
Coasting Arc #4 (Orbit 1219)
---------------------------------------
Vector Time (GMT): 2015/323/11:27:21
181
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6145980
12 A = 6786164
90 meter
Y = 2815949
55 meter E =
0010106
Z = -574687
24 I = 51
84231
XDOT = -1523
600975 Wp = 72
01425
YDOT = 4530
182378 meter/sec RA = 28
44601 deg
ZDOT = 5993
140657 TA = 281
80178
MA = 281
91511
Ha = 220
864 n
mi
Hp = 211
920
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20163976
76 X = 6116826
34
Y = 9238679
62 feet Y = 2884514
94 meter
Z = -1885456
84 Z = -544901
77
XDOT = -4998
690862 XDOT = -1603
258093
YDOT = 14862
803078 feet/sec YDOT = 4512
699109 meter/sec
ZDOT = 19662
534964 ZDOT = 5985
545713
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20181077
57 X = -6151192
44
Y = 9226598
19 feet Y = 2812267
13 meter
Z = -1757299
52 Z = -535624
89
XDOT = -7224
799000 XDOT = -2202
118735
YDOT = -12124
106934 feet/sec YDOT = -3695
427793 meter/sec
ZDOT = 19628
775324 ZDOT = 5982
850719
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 15323
47836403
00016717 00000-0 10270-3 0 9039
2 25544 51
6441 29
0376 0005712 155
0895 205
0535 15
55173447 12205
Satellite: ISS
Catalog Number: 25544
Epoch time: 15323
47836403 = yrday
fracday
Element set: 903
Inclination: 51
6441 deg
RA of node: 29
0376 deg
Eccentricity:
0005712
Arg of perigee: 155
0895 deg
Mean anomaly: 205
0535 deg
Mean motion: 15
55173447 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1220
Checksum: 288
Coasting Arc #5 (Orbit 1235)
---------------------------------------
Vector Time (GMT): 2015/324/11:27:21
181
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5483263
89 A = 6785099
76 meter
Y = -3685006
84 meter E =
0013820
Z = -1518889
07 I = 51
81028
XDOT = 3811
180037 Wp = 148
49783
YDOT = -3302
575224 meter/sec RA = 23
48342 deg
ZDOT = -5781
272285 TA = 48
06580
MA = 47
94807
Ha = 220
698 n
mi
Hp = 211
872
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17989710
93 X = -5434271
42
Y = -12089917
45 feet Y = -3746050
41 meter
Z = -4983231
86 Z = -1545406
99
XDOT = 12503
871511 XDOT = 3875
910604
YDOT = -10835
220550 feet/sec YDOT = -3259
594260 meter/sec
ZDOT = -18967
428758 ZDOT = -5762
600790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20787998
60 X = 6336181
97
Y = -6042127
12 feet Y = -1841640
35 meter
Z = -5097079
29 Z = -1553589
77
XDOT = -208
179763 XDOT = -63
453192
YDOT = 15120
679586 feet/sec YDOT = 4608
783138 meter/sec
ZDOT = -18886
049555 ZDOT = -5756
467904
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 15324
50647249
00016717 00000-0 10270-3 0 9043
2 25544 51
6435 23
9038 0005825 158
2610 201
8792 15
55230911 12367
Satellite: ISS
Catalog Number: 25544
Epoch time: 15324
50647249 = yrday
fracday
Element set: 904
Inclination: 51
6435 deg
RA of node: 23
9038 deg
Eccentricity:
0005825
Arg of perigee: 158
2610 deg
Mean anomaly: 201
8792 deg
Mean motion: 15
55230911 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1236
Checksum: 294
Coasting Arc #6 (Orbit 1251)
---------------------------------------
Vector Time (GMT): 2015/325/11:27:21
181
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4165497
26 A = 6781176
56 meter
Y = 4172323
64 meter E =
0015266
Z = 3343481
64 I = 51
76847
XDOT = -5747
511850 Wp = 109
92614
YDOT = 1966
905298 meter/sec RA = 18
51022 deg
ZDOT = 4683
639366 TA = 288
97610
MA = 289
14146
Ha = 220
536 n
mi
Hp = 211
913
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13666329
60 X = 4102290
08
Y = 13688725
85 feet Y = 4218551
64 meter
Z = 10969427
97 Z = 3363563
54
XDOT = -18856
666176 XDOT = -5791
830833
YDOT = 6453
101370 feet/sec YDOT = 1902
385120 meter/sec
ZDOT = 15366
270887 ZDOT = 4655
610926
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19190141
67 X = -5849155
18
Y = 1998954
68 feet Y = 609281
39 meter
Z = 11055350
41 Z = 3369670
81
XDOT = 7010
933537 XDOT = 2136
932542
YDOT = -17410
370460 feet/sec YDOT = -5306
680916 meter/sec
ZDOT = 15244
733563 ZDOT = 4646
594790
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 15325
53455950
00016717 00000-0 10270-3 0 9054
2 25544 51
6439 18
7700 0005753 161
9587 198
1772 15
55276400 12520
Satellite: ISS
Catalog Number: 25544
Epoch time: 15325
53455950 = yrday
fracday
Element set: 905
Inclination: 51
6439 deg
RA of node: 18
7700 deg
Eccentricity:
0005753
Arg of perigee: 161
9587 deg
Mean anomaly: 198
1772 deg
Mean motion: 15
55276400 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1252
Checksum: 318
Coasting Arc #7 (Orbit 1266)
---------------------------------------
Vector Time (GMT): 2015/326/11:27:21
181
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2244089
07 A = 6776588
24 meter
Y = -4350462
71 meter E =
0011910
Z = -4695440
49 I = 51
72219
XDOT = 7090
799515 Wp = 98
75723
YDOT = -600
446939 meter/sec RA = 13
51976 deg
ZDOT = -2840
492141 TA = 143
10383
MA = 143
02183
Ha = 220
479 n
mi
Hp = 211
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7362496
94 X = -2172465
20
Y = -14273171
61 feet Y = -4375157
19 meter
Z = -15404988
50 Z = -4706168
03
XDOT = 23263
777935 XDOT = 7110
785173
YDOT = -1969
970271 feet/sec YDOT = -521
041231 meter/sec
ZDOT = -9319
199937 ZDOT = -2805
997175
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15727478
16 X = 4793735
34
Y = 3028823
54 feet Y = 923185
42 meter
Z = -15450440
72 Z = -4709294
33
XDOT = -12540
795724 XDOT = -3822
434537
YDOT = 18474
107147 feet/sec YDOT = 5630
907858 meter/sec
ZDOT = -9170
008833 ZDOT = -2795
018692
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 15326
49837522
00016717 00000-0 10270-3 0 9060
2 25544 51
6435 13
9567 0005687 164
5803 195
5524 15
55277468 12677
Satellite: ISS
Catalog Number: 25544
Epoch time: 15326
49837522 = yrday
fracday
Element set: 906
Inclination: 51
6435 deg
RA of node: 13
9567 deg
Eccentricity:
0005687
Arg of perigee: 164
5803 deg
Mean anomaly: 195
5524 deg
Mean motion: 15
55277468 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1267
Checksum: 341
Coasting Arc #8 (Orbit 1282)
---------------------------------------
Vector Time (GMT): 2015/327/11:27:21
181
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 21592
58 A = 6773918
32 meter
Y = 4229180
28 meter E =
0007527
Z = 5288688
81 I = 51
68259
XDOT = -7621
416147 Wp = 149
44059
YDOT = -684
311737 meter/sec RA = 8
51511 deg
ZDOT = 571
640774 TA = 295
07193
MA = 295
15003
Ha = 220
295 n
mi
Hp = 212
065
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 70841
81 X = -51391
80
Y = 13875263
37 feet Y = 4229013
65 meter
Z = 17351341
23 Z = 5288616
43
XDOT = -25004
646151 XDOT = -7615
974440
YDOT = -2245
117246 feet/sec YDOT = -769
509017 meter/sec
ZDOT = 1875
461858 ZDOT = 534
629790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11075231
00 X = -3375730
41
Y = -8361146
31 feet Y = -2548477
40 meter
Z = 17350143
67 Z = 5288323
79
XDOT = 16200
809820 XDOT = 4938
006833
YDOT = -17853
927572 feet/sec YDOT = -5441
877124 meter/sec
ZDOT = 1715
675799 ZDOT = 522
937983
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 15327
52642434
00016717 00000-0 10270-3 0 9072
2 25544 51
6437 8
8231 0005593 167
8889 192
2400 15
55337268 12836
Satellite: ISS
Catalog Number: 25544
Epoch time: 15327
52642434 = yrday
fracday
Element set: 907
Inclination: 51
6437 deg
RA of node: 8
8231 deg
Eccentricity:
0005593
Arg of perigee: 167
8889 deg
Mean anomaly: 192
2400 deg
Mean motion: 15
55337268 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1283
Checksum: 322
Coasting Arc #9 (Orbit 1297)
---------------------------------------
Vector Time (GMT): 2015/328/11:27:21
181
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2287303
31 A = 6774992
70 meter
Y = -3881378
24 meter E =
0016090
Z = -5074159
70 I = 51
65423
XDOT = 7201
820342 Wp = 121
53289
YDOT = 1874
381293 meter/sec RA = 3
50392 deg
ZDOT = 1808
639580 TA = 166
01448
MA = 165
96987
Ha = 220
225 n
mi
Hp = 212
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7504275
97 X = 2355184
79
Y = -12734180
59 feet Y = -3855420
44 meter
Z = -16647505
59 Z = -5062883
37
XDOT = 23628
019494 XDOT = 7171
539390
YDOT = 6149
544925 feet/sec YDOT = 1954
747448 meter/sec
ZDOT = 5933
856890 ZDOT = 1843
551949
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5853999
23 X = 1784298
97
Y = 13632725
51 feet Y = 4155254
73 meter
Z = -16597965
04 Z = -5059059
75
XDOT = -17819
802319 XDOT = -5431
475747
YDOT = 15075
652057 feet/sec YDOT = 4595
058747 meter/sec
ZDOT = 6084
316335 ZDOT = 1854
499619
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 15328
49020463
00016717 00000-0 10270-3 0 9082
2 25544 51
6436 4
0093 0005466 170
1945 189
9316 15
55333931 12986
Satellite: ISS
Catalog Number: 25544
Epoch time: 15328
49020463 = yrday
fracday
Element set: 908
Inclination: 51
6436 deg
RA of node: 4
0093 deg
Eccentricity:
0005466
Arg of perigee: 170
1945 deg
Mean anomaly: 189
9316 deg
Mean motion: 15
55333931 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1298
Checksum: 312
Coasting Arc #10 (Orbit 1313)
---------------------------------------
Vector Time (GMT): 2015/329/11:27:21
181
Vector Time (MET): N/A
Weight (LBS) : 907028
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4320598
62 A = 6778795
16 meter
Y = 3305959
94 meter E =
0011743
Z = 4032044
16 I = 51
63512
XDOT = -5911
092989 Wp = 105
53429
YDOT = -2944
289613 meter/sec RA = 358
50013 deg
ZDOT = -3913
631617 TA = 25
05323
MA = 24
99629
Ha = 220
112 n
mi
Hp = 212
169
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14175192
33 X = -4376832
15
Y = 10846325
28 feet Y = 3257329
55 meter
Z = 13228491
32 Z = 4010918
62
XDOT = -19393
349703 XDOT = -5858
718513
YDOT = -9659
742825 feet/sec YDOT = -3010
098330 meter/sec
ZDOT = -12839
998742 ZDOT = -3942
220125
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -733856
29 X = -223679
40
Y = -17901544
51 feet Y = -5456390
77 meter
Z = 13136513
68 Z = 4004009
37
XDOT = 17669
102196 XDOT = 5385
542349
YDOT = -10252
291412 feet/sec YDOT = -3124
898422 meter/sec
ZDOT = -12962
901426 ZDOT = -3951
092355
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 15329
51821646
00016717 00000-0 10270-3 0 9099
2 25544 51
6430 358
8750 0005405 173
2983 186
8243 15
55406244 13141
Satellite: ISS
Catalog Number: 25544
Epoch time: 15329
51821646 = yrday
fracday
Element set: 909
Inclination: 51
6430 deg
RA of node: 358
8750 deg
Eccentricity:
0005405
Arg of perigee: 173
2983 deg
Mean anomaly: 186
8243 deg
Mean motion: 15
55406244 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1314
Checksum: 314
Coasting Arc #11 (Orbit 1318)
---------------------------------------
Vector Time (GMT): 2015/329/19:59:37
414
Vector Time (MET): N/A
Weight (LBS) : 906444
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5323639
29 A = 6784544
78 meter
Y = -2797621
24 meter E =
0002359
Z = -3143838
33 I = 51
63432
XDOT = 4740
027544 Wp = 152
10030
YDOT = 3572
067478 meter/sec RA = 356
72280 deg
ZDOT = 4847
300703 TA = 171
68152
MA = 171
67761
Ha = 220
049 n
mi
Hp = 215
521
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17466008
16 X = 5369799
22
Y = -9178547
36 feet Y = -2737830
52 meter
Z = -10314430
22 Z = -3117864
60
XDOT = 15551
271471 XDOT = 4676
184648
YDOT = 11719
381490 feet/sec YDOT = 3624
716366 meter/sec
ZDOT = 15903
217531 ZDOT = 4870
172452
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16937716
20 X = 5162615
90
Y = -10234037
64 feet Y = -3119334
67 meter
Z = -10201611
97 Z = -3109451
33
XDOT = 15390
527628 XDOT = 4691
032821
YDOT = 9519
447221 feet/sec YDOT = 2901
527513 meter/sec
ZDOT = 16001
284851 ZDOT = 4877
191623
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 15329
83946755
00016717 00000-0 10270-3 0 9105
2 25544 51
6445 357
2693 0004624 225
1516 134
9261 15
54364073 13198
Satellite: ISS
Catalog Number: 25544
Epoch time: 15329
83946755 = yrday
fracday
Element set: 910
Inclination: 51
6445 deg
RA of node: 357
2693 deg
Eccentricity:
0004624
Arg of perigee: 225
1516 deg
Mean anomaly: 134
9261 deg
Mean motion: 15
54364073 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1319
Checksum: 317
Coasting Arc #12 (Orbit 1334)
---------------------------------------
Vector Time (GMT): 2015/330/19:59:37
414
Vector Time (MET): N/A
Weight (LBS) : 906444
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6252274
16 A = 6787721
38 meter
Y = 2130488
15 meter E =
0013052
Z = 1528126
11 I = 51
61308
XDOT = -2842
555792 Wp = 137
30500
YDOT = -4197
482856 meter/sec RA = 351
74404 deg
ZDOT = -5758
714366 TA = 25
98339
MA = 25
91792
Ha = 219
991 n
mi
Hp = 215
556
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20512710
49 X = -6283056
30
Y = 6989790
51 feet Y = 2060398
87 meter
Z = 5013537
10 Z = 1497678
63
XDOT = -9325
970445 XDOT = -2767
433084
YDOT = -13771
269212 feet/sec YDOT = -4228
849749 meter/sec
ZDOT = -18893
419837 ZDOT = -5772
341019
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19934047
74 X = -6075897
75
Y = 8577203
41 feet Y = 2614331
60 meter
Z = 4881530
45 Z = 1487890
48
XDOT = -9629
467723 XDOT = -2935
061762
YDOT = -11556
519759 feet/sec YDOT = -3522
427222 meter/sec
ZDOT = -18951
405943 ZDOT = -5776
388532
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 15330
86814306
00016717 00000-0 10270-3 0 9117
2 25544 51
6444 352
1392 0004615 228
3767 131
6991 15
54359664 13352
Satellite: ISS
Catalog Number: 25544
Epoch time: 15330
86814306 = yrday
fracday
Element set: 911
Inclination: 51
6444 deg
RA of node: 352
1392 deg
Eccentricity:
0004615
Arg of perigee: 228
3767 deg
Mean anomaly: 131
6991 deg
Mean motion: 15
54359664 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1335
Checksum: 313
Coasting Arc #13 (Orbit 1350)
---------------------------------------
Vector Time (GMT): 2015/331/19:59:37
414
Vector Time (MET): N/A
Weight (LBS) : 906444
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6642545
35 A = 6788496
33 meter
Y = -1356974
80 meter E =
0008125
Z = 251480
04 I = 51
58504
XDOT = 732
036261 Wp = 44
72311
YDOT = 4716
310065 meter/sec RA = 346
76856 deg
ZDOT = 6000
715571 TA = 317
98846
MA = 318
05074
Ha = 219
716 n
mi
Hp = 215
544
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21793127
80 X = 6656004
07
Y = -4452017
05 feet Y = -1282618
24 meter
Z = 825065
74 Z = 283781
23
XDOT = 2401
693771 XDOT = 650
093326
YDOT = 15473
458217 feet/sec YDOT = 4724
037539 meter/sec
ZDOT = 19687
387045 ZDOT = 6004
073040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21263143
55 X = 6481006
15
Y = -6510704
29 feet Y = -1984462
67 meter
Z = 964917
00 Z = 294106
70
XDOT = 3267
271891 XDOT = 995
864472
YDOT = 13637
002268 feet/sec YDOT = 4156
558291 meter/sec
ZDOT = 19700
892443 ZDOT = 6004
832017
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 15331
89679930
00016717 00000-0 10270-3 0 9124
2 25544 51
6447 347
0084 0004547 234
1888 125
8843 15
54402347 13515
Satellite: ISS
Catalog Number: 25544
Epoch time: 15331
89679930 = yrday
fracday
Element set: 912
Inclination: 51
6447 deg
RA of node: 347
0084 deg
Eccentricity:
0004547
Arg of perigee: 234
1888 deg
Mean anomaly: 125
8843 deg
Mean motion: 15
54402347 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1351
Checksum: 323
Coasting Arc #14 (Orbit 1365)
---------------------------------------
Vector Time (GMT): 2015/332/19:59:37
414
Vector Time (MET): N/A
Weight (LBS) : 906444
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6457255
56 A = 6786702
35 meter
Y = 428036
89 meter E =
0007498
Z = -2029188
62 I = 51
54886
XDOT = 1403
605335 Wp = 177
00711
YDOT = -5101
843936 meter/sec RA = 341
79028 deg
ZDOT = -5550
970305 TA = 25
45356
MA = 25
41665
Ha = 219
517 n
mi
Hp = 215
629
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21185221
67 X = -6451704
94
Y = 1404320
50 feet Y = 355858
78 meter
Z = -6657442
97 Z = -2060543
46
XDOT = 4605
004379 XDOT = 1487
515839
YDOT = -16738
333124 feet/sec YDOT = -5085
678306 meter/sec
ZDOT = -18211
844833 ZDOT = -5543
948377
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20849921
74 X = -6355056
15
Y = 3774002
62 feet Y = 1150316
00 meter
Z = -6793007
27 Z = -2070508
62
XDOT = 3082
819553 XDOT = 939
643400
YDOT = -15644
640311 feet/sec YDOT = -4768
486367 meter/sec
ZDOT = -18180
424431 ZDOT = -5541
393366
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 15332
86114838
00016717 00000-0 10270-3 0 9134
2 25544 51
6452 342
1989 0004696 237
0830 122
9872 15
54406035 13669
Satellite: ISS
Catalog Number: 25544
Epoch time: 15332
86114838 = yrday
fracday
Element set: 913
Inclination: 51
6452 deg
RA of node: 342
1989 deg
Eccentricity:
0004696
Arg of perigee: 237
0830 deg
Mean anomaly: 122
9872 deg
Mean motion: 15
54406035 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1366
Checksum: 317
Coasting Arc #15 (Orbit 1381)
---------------------------------------
Vector Time (GMT): 2015/333/19:59:37
414
Vector Time (MET): N/A
Weight (LBS) : 906444
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5740095
94 A = 6782927
36 meter
Y = 616870
96 meter E =
0008541
Z = 3556343
08 I = 51
50672
XDOT = -3332
724391 Wp = 108
64983
YDOT = 5280
084735 meter/sec RA = 336
80103 deg
ZDOT = 4451
845693 TA = 293
42611
MA = 293
51589
Ha = 219
344 n
mi
Hp = 215
581
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18832335
76 X = 5715495
85
Y = 2023854
86 feet Y = 680922
73 meter
Z = 11667792
25 Z = 3584167
78
XDOT = -10934
135142 XDOT = -3413
145402
YDOT = 17323
112648 feet/sec YDOT = 5242
366067 meter/sec
ZDOT = 14605
792955 ZDOT = 4435
460882
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18861519
86 X = 5748991
25
Y = -423256
21 feet Y = -129008
49 meter
Z = 11787881
80 Z = 3592946
37
XDOT = -8719
794054 XDOT = -2657
793228
YDOT = 17232
212757 feet/sec YDOT = 5252
378448 meter/sec
ZDOT = 14533
885897 ZDOT = 4429
928421
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 15333
88977014
00016717 00000-0 10270-3 0 9141
2 25544 51
6453 337
0681 0004452 242
0020 118
0683 15
54447612 13829
Satellite: ISS
Catalog Number: 25544
Epoch time: 15333
88977014 = yrday
fracday
Element set: 914
Inclination: 51
6453 deg
RA of node: 337
0681 deg
Eccentricity:
0004452
Arg of perigee: 242
0020 deg
Mean anomaly: 118
0683 deg
Mean motion: 15
54447612 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1382
Checksum: 294
Coasting Arc #16 (Orbit 1396)
---------------------------------------
Vector Time (GMT): 2015/334/19:59:37
414
Vector Time (MET): N/A
Weight (LBS) : 906444
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4568734
28 A = 6778832
20 meter
Y = -1784340
94 meter E =
0006303
Z = -4685316
23 I = 51
46460
XDOT = 4904
411238 Wp = 73
28075
YDOT = -5172
778355 meter/sec RA = 331
79832 deg
ZDOT = -2813
760498 TA = 168
73165
MA = 168
71753
Ha = 219
104 n
mi
Hp = 215
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14989285
70 X = -4525682
20
Y = -5854136
95 feet Y = -1835190
60 meter
Z = -15371772
41 Z = -4707405
85
XDOT = 16090
588050 XDOT = 4975
558243
YDOT = -16971
057596 feet/sec YDOT = -5117
536050 meter/sec
ZDOT = -9231
497698 ZDOT = -2789
763178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15588323
91 X = -4751321
13
Y = -3608617
12 feet Y = -1099906
50 meter
Z = -15466836
53 Z = -4714291
77
XDOT = 13222
709458 XDOT = 4030
281843
YDOT = -18019
975053 feet/sec YDOT = -5492
488396 meter/sec
ZDOT = -9126
730140 ZDOT = -2781
827347
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 15334
85408505
00016717 00000-0 10270-3 0 9154
2 25544 51
6453 332
2583 0004586 246
9317 113
1352 15
54499228 13972
Satellite: ISS
Catalog Number: 25544
Epoch time: 15334
85408505 = yrday
fracday
Element set: 915
Inclination: 51
6453 deg
RA of node: 332
2583 deg
Eccentricity:
0004586
Arg of perigee: 246
9317 deg
Mean anomaly: 113
1352 deg
Mean motion: 15
54499228 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1397
Checksum: 320
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