[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 4th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15607 67 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
There are no maneuvers
Coasting Arc #1 (Orbit 1422)
---------------------------------------
Vector Time (GMT): 2015/336/11:25:26
438
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3448552
49 A = 6776968
53 meter
Y = 2626225
41 meter E =
0007782
Z = 5213360
13 I = 51
40780
XDOT = -5562
131643 Wp = 205
08488
YDOT = 5165
243308 meter/sec RA = 323
58397 deg
ZDOT = 1070
947536 TA = 234
58231
MA = 234
65500
Ha = 220
276 n
mi
Hp = 216
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11314148
58 X = 3393604
44
Y = 8616225
10 feet Y = 2664482
04 meter
Z = 17104199
91 Z = 5229979
20
XDOT = -18248
463397 XDOT = -5624
679549
YDOT = 16946
336311 feet/sec YDOT = 5102
694126 meter/sec
ZDOT = 3513
607403 ZDOT = 1043
775886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12919178
46 X = -3937765
59
Y = 5735989
19 feet Y = 1748329
50 meter
Z = 17175453
52 Z = 5235078
23
XDOT = -5759
407517 XDOT = -1755
467411
YDOT = -23199
985888 feet/sec YDOT = -7071
355699 meter/sec
ZDOT = 3395
142966 ZDOT = 1034
839576
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 15336
52599216
00016717 00000-0 10270-3 0 9004
2 25544 51
6406 323
9335 0008187 232
2016 127
8396 15
54382723 14238
Satellite: ISS
Catalog Number: 25544
Epoch time: 15336
52599216 = yrday
fracday
Element set: 900
Inclination: 51
6406 deg
RA of node: 323
9335 deg
Eccentricity:
0008187
Arg of perigee: 232
2016 deg
Mean anomaly: 127
8396 deg
Mean motion: 15
54382723 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1423
Checksum: 306
Coasting Arc #2 (Orbit 1437)
---------------------------------------
Vector Time (GMT): 2015/337/11:25:26
438
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1934189
75 A = 6776905
88 meter
Y = -3863460
70 meter E =
0009889
Z = -5228423
90 I = 51
38238
XDOT = 6183
062095 Wp = 130
98093
YDOT = -4420
387966 meter/sec RA = 318
56382 deg
ZDOT = 973
875437 TA = 148
41013
MA = 148
35073
Ha = 220
113 n
mi
Hp = 216
422
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6345766
88 X = -1865445
96
Y = -12675395
99 feet Y = -3884705
62 meter
Z = -17153621
71 Z = -5237652
97
XDOT = 20285
636794 XDOT = 6227
301667
YDOT = -14502
585191 feet/sec YDOT = -4350
997543 meter/sec
ZDOT = 3195
129388 ZDOT = 1004
019093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14123994
61 X = 4304993
56
Y = 324336
38 feet Y = 98857
73 meter
Z = -17192694
40 Z = -5240333
25
XDOT = 3526
593969 XDOT = 1074
905842
YDOT = 23642
034348 feet/sec YDOT = 7206
092069 meter/sec
ZDOT = 3326
268562 ZDOT = 1013
846658
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 15337
49034855
00016717 00000-0 10270-3 0 9015
2 25544 51
6405 319
1241 0008187 236
0206 124
0169 15
54399752 14386
Satellite: ISS
Catalog Number: 25544
Epoch time: 15337
49034855 = yrday
fracday
Element set: 901
Inclination: 51
6405 deg
RA of node: 319
1241 deg
Eccentricity:
0008187
Arg of perigee: 236
0206 deg
Mean anomaly: 124
0169 deg
Mean motion: 15
54399752 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1438
Checksum: 305
Coasting Arc #3 (Orbit 1453)
---------------------------------------
Vector Time (GMT): 2015/338/11:25:26
438
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 416030
18 A = 6779278
64 meter
Y = 4933760
77 meter E =
0000679
Z = 4630103
52 I = 51
36687
XDOT = -6303
227349 Wp = 143
36077
YDOT = 3259
284429 meter/sec RA = 313
54517 deg
ZDOT = -2906
986898 TA = 335
66895
MA = 335
67215
Ha = 219
809 n
mi
Hp = 216
677
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1364928
41 X = 338337
25
Y = 16186879
18 feet Y = 4937978
61 meter
Z = 15190628
33 Z = 4631935
90
XDOT = -20679
879754 XDOT = -6325
083829
YDOT = 10693
190385 feet/sec YDOT = 3188
675421 meter/sec
ZDOT = -9537
358589 ZDOT = -2937
660028
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15050711
28 X = -4587456
80
Y = -6094622
80 feet Y = -1857641
03 meter
Z = 15197530
69 Z = 4632207
35
XDOT = -804
300788 XDOT = -245
150880
YDOT = -22125
623552 feet/sec YDOT = -6743
890059 meter/sec
ZDOT = -9670
536362 ZDOT = -2947
579483
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 15338
51897641
00016717 00000-0 10270-3 0 9020
2 25544 51
6399 313
9933 0008197 240
4420 119
5917 15
54453017 14549
Satellite: ISS
Catalog Number: 25544
Epoch time: 15338
51897641 = yrday
fracday
Element set: 902
Inclination: 51
6399 deg
RA of node: 313
9933 deg
Eccentricity:
0008197
Arg of perigee: 240
4420 deg
Mean anomaly: 119
5917 deg
Mean motion: 15
54453017 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1454
Checksum: 323
Coasting Arc #4 (Orbit 1468)
---------------------------------------
Vector Time (GMT): 2015/339/11:25:26
438
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1006397
80 A = 6783242
87 meter
Y = -5733932
92 meter E =
0004404
Z = -3483467
13 I = 51
35867
XDOT = 5960
648295 Wp = 210
19094
YDOT = -1697
227026 meter/sec RA = 308
53462 deg
ZDOT = 4509
552570 TA = 108
70795
MA = 108
66015
Ha = 219
643 n
mi
Hp = 216
832
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3301830
06 X = 1087362
80
Y = -18812115
87 feet Y = -5722225
94 meter
Z = -11428697
94 Z = -3478381
65
XDOT = 19555
932727 XDOT = 5957
278150
YDOT = -5568
330138 feet/sec YDOT = -1630
590053 meter/sec
ZDOT = 14795
119979 ZDOT = 4538
500323
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15520387
25 X = 4730614
04
Y = 11155435
88 feet Y = 3400176
86 meter
Z = -11405557
93 Z = -3476414
06
XDOT = -2552
867226 XDOT = -778
113931
YDOT = 18827
753037 feet/sec YDOT = 5738
699126 meter/sec
ZDOT = 14920
517155 ZDOT = 4547
773629
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 15339
48329760
00016717 00000-0 10270-3 0 9030
2 25544 51
6397 309
1832 0008066 243
9128 116
1195 15
54459741 14697
Satellite: ISS
Catalog Number: 25544
Epoch time: 15339
48329760 = yrday
fracday
Element set: 903
Inclination: 51
6397 deg
RA of node: 309
1832 deg
Eccentricity:
0008066
Arg of perigee: 243
9128 deg
Mean anomaly: 116
1195 deg
Mean motion: 15
54459741 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1469
Checksum: 331
Coasting Arc #5 (Orbit 1484)
---------------------------------------
Vector Time (GMT): 2015/340/11:25:26
438
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2216098
60 A = 6786662
92 meter
Y = 6114986
66 meter E =
0009956
Z = 1914337
40 I = 51
35156
XDOT = -5256
021853 Wp = 147
67790
YDOT = -154
585596 meter/sec RA = 303
53383 deg
ZDOT = -5585
529988 TA = 11
12815
MA = 11
10615
Ha = 219
311 n
mi
Hp = 217
007
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7270664
71 X = -2293612
42
Y = 20062292
18 feet Y = 6089771
32 meter
Z = 6280634
51 Z = 1903383
78
XDOT = -17244
166186 XDOT = -5226
769848
YDOT = -507
170589 feet/sec YDOT = -213
198195 meter/sec
ZDOT = -18325
229620 ZDOT = -5610
991995
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15211328
41 X = -4636412
90
Y = -14986034
71 feet Y = -4567743
38 meter
Z = 6232074
62 Z = 1899536
34
XDOT = 6486
295573 XDOT = 1977
022891
YDOT = -14257
414945 feet/sec YDOT = -4345
660075 meter/sec
ZDOT = -18435
187939 ZDOT = -5619
045284
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 15340
51188727
00016717 00000-0 10270-3 0 9043
2 25544 51
6397 304
0519 0008118 248
6417 111
3870 15
54519533 14855
Satellite: ISS
Catalog Number: 25544
Epoch time: 15340
51188727 = yrday
fracday
Element set: 904
Inclination: 51
6397 deg
RA of node: 304
0519 deg
Eccentricity:
0008118
Arg of perigee: 248
6417 deg
Mean anomaly: 111
3870 deg
Mean motion: 15
54519533 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1485
Checksum: 312
Coasting Arc #6 (Orbit 1499)
---------------------------------------
Vector Time (GMT): 2015/341/11:25:26
438
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3164137
57 A = 6788067
11 meter
Y = -6000094
34 meter E =
0005831
Z = -108792
78 I = 51
33966
XDOT = 4281
813534 Wp = 7
41333
YDOT = 2150
224682 meter/sec RA = 298
54001 deg
ZDOT = 5985
912448 TA = 351
40992
MA = 351
41990
Ha = 219
149 n
mi
Hp = 217
004
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10381028
77 X = 3231525
41
Y = -19685348
87 feet Y = -5964334
07 meter
Z = -356931
68 Z = -93258
35
XDOT = 14047
944665 XDOT = 4228
373233
YDOT = 7054
542921 feet/sec YDOT = 2197
807715 meter/sec
ZDOT = 19638
820367 ZDOT = 6006
583239
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13892498
49 X = 4234433
54
Y = 17387389
30 feet Y = 5299676
26 meter
Z = -288613
82 Z = -87969
49
XDOT = -10766
002843 XDOT = -3281
477667
YDOT = 8926
677710 feet/sec YDOT = 2720
851366 meter/sec
ZDOT = 19727
677099 ZDOT = 6012
995980
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 15341
47617262
00016717 00000-0 10270-3 0 9051
2 25544 51
6395 299
2417 0008095 250
5583 109
4695 15
54560512 15009
Satellite: ISS
Catalog Number: 25544
Epoch time: 15341
47617262 = yrday
fracday
Element set: 905
Inclination: 51
6395 deg
RA of node: 299
2417 deg
Eccentricity:
0008095
Arg of perigee: 250
5583 deg
Mean anomaly: 109
4695 deg
Mean motion: 15
54560512 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1500
Checksum: 314
Coasting Arc #7 (Orbit 1515)
---------------------------------------
Vector Time (GMT): 2015/342/11:25:26
438
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3825158
15 A = 6786754
77 meter
Y = 5327763
90 meter E =
0008505
Z = -1721898
38 I = 51
32195
XDOT = -3158
574708 Wp = 202
00016
YDOT = -4098
171284 meter/sec RA = 293
54505 deg
ZDOT = -5662
189064 TA = 356
98191
MA = 356
98703
Ha = 218
753 n
mi
Hp = 217
276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12549731
48 X = -3876085
76
Y = 17479540
34 feet Y = 5284703
79 meter
Z = -5649272
92 Z = -1740603
94
XDOT = -10362
777914 XDOT = -3085
008009
YDOT = -13445
443846 feet/sec YDOT = -4133
080906 meter/sec
ZDOT = -18576
735774 ZDOT = -5677
354566
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11334338
61 X = -3454706
41
Y = -18265570
97 feet Y = -5567346
03 meter
Z = -5731148
28 Z = -1746854
00
XDOT = 15017
744324 XDOT = 4577
408470
YDOT = -3468
514749 feet/sec YDOT = -1057
203295 meter/sec
ZDOT = -18641
421239 ZDOT = -5681
905194
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 15342
50472432
00016717 00000-0 10270-3 0 9065
2 25544 51
6405 294
1101 0008111 256
0807 103
9444 15
54568863 15169
Satellite: ISS
Catalog Number: 25544
Epoch time: 15342
50472432 = yrday
fracday
Element set: 906
Inclination: 51
6405 deg
RA of node: 294
1101 deg
Eccentricity:
0008111
Arg of perigee: 256
0807 deg
Mean anomaly: 103
9444 deg
Mean motion: 15
54568863 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1516
Checksum: 288
Coasting Arc #8 (Orbit 1531)
---------------------------------------
Vector Time (GMT): 2015/343/11:25:26
438
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4212031
65 A = 6783068
36 meter
Y = -4131243
52 meter E =
0004673
Z = 3344568
79 I = 51
29868
XDOT = 1979
788578 Wp = 108
09732
YDOT = 5777
015339 meter/sec RA = 288
54225 deg
ZDOT = 4635
772156 TA = 291
09447
MA = 291
14442
Ha = 218
650 n
mi
Hp = 217
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13819001
47 X = 4241668
29
Y = -13553948
54 feet Y = -4083976
33 meter
Z = 10972994
71 Z = 3365101
99
XDOT = 6495
369349 XDOT = 1892
522284
YDOT = 18953
462397 feet/sec YDOT = 5798
666371 meter/sec
ZDOT = 15209
226232 ZDOT = 4645
178171
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7541738
47 X = 2298721
88
Y = 17771430
11 feet Y = 5416731
90 meter
Z = 11062521
78 Z = 3371856
64
XDOT = -18683
226336 XDOT = -5694
647387
YDOT = -1577
197448 feet/sec YDOT = -480
729782 meter/sec
ZDOT = 15248
700772 ZDOT = 4647
803995
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 15343
53325524
00016717 00000-0 10270-3 0 9079
2 25544 51
6409 288
9793 0008225 258
9066 101
1162 15
54623793 15324
Satellite: ISS
Catalog Number: 25544
Epoch time: 15343
53325524 = yrday
fracday
Element set: 907
Inclination: 51
6409 deg
RA of node: 288
9793 deg
Eccentricity:
0008225
Arg of perigee: 258
9066 deg
Mean anomaly: 101
1162 deg
Mean motion: 15
54623793 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1532
Checksum: 317
Coasting Arc #9 (Orbit 1546)
---------------------------------------
Vector Time (GMT): 2015/344/11:25:26
438
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4359281
07 A = 6778935
10 meter
Y = 2483224
61 meter E =
0002932
Z = -4561519
37 I = 51
27605
XDOT = -814
542545 Wp = 29
13204
YDOT = -6995
507423 meter/sec RA = 283
52568 deg
ZDOT = -3028
129677 TA = 210
44180
MA = 210
45883
Ha = 217
947 n
mi
Hp = 217
152
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14302103
25 X = -4364566
70
Y = 8147062
37 feet Y = 2434447
10 meter
Z = -14965614
74 Z = -4582708
78
XDOT = -2672
383677 XDOT = -721
546841
YDOT = -22951
139839 feet/sec YDOT = -7004
095939 meter/sec
ZDOT = -9934
808651 ZDOT = -3031
861347
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2624041
58 X = -799807
87
Y = -16164036
63 feet Y = -4926798
36 meter
Z = -15057646
98 Z = -4589570
80
XDOT = 21222
805474 XDOT = 6468
711109
YDOT = 5828
383701 feet/sec YDOT = 1776
491352 meter/sec
ZDOT = -9949
535293 ZDOT = -3032
618357
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 15344
49748736
00016717 00000-0 10270-3 0 9080
2 25544 51
6413 284
1684 0008123 263
6167 96
4061 15
54630390 15479
Satellite: ISS
Catalog Number: 25544
Epoch time: 15344
49748736 = yrday
fracday
Element set: 908
Inclination: 51
6413 deg
RA of node: 284
1684 deg
Eccentricity:
0008123
Arg of perigee: 263
6167 deg
Mean anomaly: 96
4061 deg
Mean motion: 15
54630390 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1547
Checksum: 323
Coasting Arc #10 (Orbit 1562)
---------------------------------------
Vector Time (GMT): 2015/345/11:25:26
438
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4306214
68 A = 6776105
20 meter
Y = -544847
68 meter E =
0005692
Z = 5208238
45 I = 51
26102
XDOT = -294
041161 Wp = 244
97418
YDOT = 7589
524730 meter/sec RA = 278
49877 deg
ZDOT = 1035
601072 TA = 195
04326
MA = 195
06020
Ha = 218
003 n
mi
Hp = 217
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14128000
91 X = 4286687
37
Y = -1787557
99 feet Y = -496802
43 meter
Z = 17087396
47 Z = 5229109
89
XDOT = -964
701972 XDOT = -383
917835
YDOT = 24900
015520 feet/sec YDOT = 7585
733937 meter/sec
ZDOT = 3397
641312 ZDOT = 1033
955103
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3025615
77 X = -922207
69
Y = 13803915
79 feet Y = 4207433
53 meter
Z = 17177673
00 Z = 5235754
73
XDOT = -22116
284601 XDOT = -6741
043546
YDOT = -9070
881179 feet/sec YDOT = -2764
804583 meter/sec
ZDOT = 3389
027876 ZDOT = 1032
975697
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 15345
52598079
00016717 00000-0 10270-3 0 9099
2 25544 51
6419 279
0378 0008272 267
2765 92
7441 15
54678136 15636
Satellite: ISS
Catalog Number: 25544
Epoch time: 15345
52598079 = yrday
fracday
Element set: 909
Inclination: 51
6419 deg
RA of node: 279
0378 deg
Eccentricity:
0008272
Arg of perigee: 267
2765 deg
Mean anomaly: 92
7441 deg
Mean motion: 15
54678136 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1563
Checksum: 349
Coasting Arc #11 (Orbit 1577)
---------------------------------------
Vector Time (GMT): 2015/346/11:25:26
438
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4088104
53 A = 6776159
48 meter
Y = -1495715
88 meter E =
0006206
Z = -5198372
46 I = 51
25733
XDOT = 1334
864489 Wp = 108
24514
YDOT = -7467
538418 meter/sec RA = 273
46551 deg
ZDOT = 1098
026318 TA = 172
34295
MA = 172
33346
Ha = 217
163 n
mi
Hp = 216
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13412416
43 X = -4045823
38
Y = -4907204
32 feet Y = -1541194
83 meter
Z = -17055027
75 Z = -5218129
22
XDOT = 4379
476670 XDOT = 1412
935300
YDOT = -24499
797959 feet/sec YDOT = -7452
174673 meter/sec
ZDOT = 3602
448549 ZDOT = 1104
699737
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8902781
80 X = 2713567
89
Y = -11036541
15 feet Y = -3363937
74 meter
Z = -17140092
65 Z = -5224300
24
XDOT = 21017
675105 XDOT = 6406
187372
YDOT = 11308
239877 feet/sec YDOT = 3446
751515 meter/sec
ZDOT = 3632
747636 ZDOT = 1107
261480
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 15346
49017752
00016717 00000-0 10270-3 0 9102
2 25544 51
6418 274
2266 0008199 271
1607 88
8607 15
54677162 15789
Satellite: ISS
Catalog Number: 25544
Epoch time: 15346
49017752 = yrday
fracday
Element set: 910
Inclination: 51
6418 deg
RA of node: 274
2266 deg
Eccentricity:
0008199
Arg of perigee: 271
1607 deg
Mean anomaly: 88
8607 deg
Mean motion: 15
54677162 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1578
Checksum: 335
Coasting Arc #12 (Orbit 1593)
---------------------------------------
Vector Time (GMT): 2015/347/11:25:26
438
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3720933
83 A = 6778898
66 meter
Y = 3418986
65 meter E =
0004068
Z = 4520918
08 I = 51
26595
XDOT = -2308
708230 Wp = 358
81580
YDOT = 6619
759657 meter/sec RA = 268
43795 deg
ZDOT = -3102
129274 TA = 122
45069
MA = 122
41135
Ha = 218
039 n
mi
Hp = 217
416
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12207788
16 X = 3660464
40
Y = 11217147
82 feet Y = 3460258
05 meter
Z = 14832408
39 Z = 4538847
12
XDOT = -7574
502068 XDOT = -2367
491431
YDOT = 21718
371577 feet/sec YDOT = 6593
613781 meter/sec
ZDOT = -10177
589480 ZDOT = -3113
486674
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14363299
63 X = -4377933
73
Y = 8140386
24 feet Y = 2481189
73 meter
Z = 14909210
95 Z = 4544327
50
XDOT = -17824
202864 XDOT = -5432
817033
YDOT = -12693
696207 feet/sec YDOT = -3869
038604 meter/sec
ZDOT = -10227
950557 ZDOT = -3117
479330
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 15347
51863501
00016717 00000-0 10270-3 0 9118
2 25544 51
6420 269
0960 0008164 274
7476 85
2744 15
54703392 15946
Satellite: ISS
Catalog Number: 25544
Epoch time: 15347
51863501 = yrday
fracday
Element set: 911
Inclination: 51
6420 deg
RA of node: 269
0960 deg
Eccentricity:
0008164
Arg of perigee: 274
7476 deg
Mean anomaly: 85
2744 deg
Mean motion: 15
54703392 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1594
Checksum: 318
Coasting Arc #13 (Orbit 1608)
---------------------------------------
Vector Time (GMT): 2015/348/11:25:26
438
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3205945
61 A = 6783012
32 meter
Y = -5009257
67 meter E =
0003920
Z = -3256689
29 I = 51
28146
XDOT = 3213
648135 Wp = 296
22965
YDOT = -5123
614552 meter/sec RA = 263
42017 deg
ZDOT = 4714
561895 TA = 25
77617
MA = 25
75664
Ha = 218
134 n
mi
Hp = 217
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10518194
25 X = -3133872
86
Y = -16434572
40 feet Y = -5044705
40 meter
Z = -10684676
16 Z = -3272088
49
XDOT = 10543
465010 XDOT = 3247
801303
YDOT = -16809
759030 feet/sec YDOT = -5087
486868 meter/sec
ZDOT = 15467
722752 ZDOT = 4730
255632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18742067
27 X = 5712582
10
Y = -5296870
78 feet Y = -1614486
21 meter
Z = -10750253
92 Z = -3276677
39
XDOT = 12720
546995 XDOT = 3877
222724
YDOT = 13459
341467 feet/sec YDOT = 4102
407279 meter/sec
ZDOT = 15536
523688 ZDOT = 4735
532420
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 15348
48279613
00016717 00000-0 10270-3 0 9121
2 25544 51
6417 264
2847 0008226 278
5309 81
4912 15
54733812 16091
Satellite: ISS
Catalog Number: 25544
Epoch time: 15348
48279613 = yrday
fracday
Element set: 912
Inclination: 51
6417 deg
RA of node: 264
2847 deg
Eccentricity:
0008226
Arg of perigee: 278
5309 deg
Mean anomaly: 81
4912 deg
Mean motion: 15
54733812 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1609
Checksum: 326
Coasting Arc #14 (Orbit 1624)
---------------------------------------
Vector Time (GMT): 2015/349/11:25:26
438
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2524216
30 A = 6786449
80 meter
Y = 6099614
08 meter E =
0006396
Z = 1557556
24 I = 51
29801
XDOT = -4035
190040 Wp = 136
91318
YDOT = 3132
628158 meter/sec RA = 258
41560 deg
ZDOT = -5718
938711 TA = 25
97374
MA = 25
94166
Ha = 218
463 n
mi
Hp = 217
060
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8281549
56 X = 2448255
34
Y = 20011857
23 feet Y = 6127416
70 meter
Z = 5110092
64 Z = 1569634
27
XDOT = -13238
812467 XDOT = -4042
139648
YDOT = 10277
651438 feet/sec YDOT = 3087
465562 meter/sec
ZDOT = -18762
922280 ZDOT = -5738
557422
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21496962
11 X = -6552274
05
Y = 2532770
81 feet Y = 771988
54 meter
Z = 5161126
96 Z = 1573111
50
XDOT = -6163
125961 XDOT = -1878
520793
YDOT = -13839
893151 feet/sec YDOT = -4218
399432 meter/sec
ZDOT = -18848
299622 ZDOT = -5744
961725
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 15349
51121721
00016717 00000-0 10270-3 0 9133
2 25544 51
6420 259
1531 0008170 282
2466 77
7772 15
54757890 16254
Satellite: ISS
Catalog Number: 25544
Epoch time: 15349
51121721 = yrday
fracday
Element set: 913
Inclination: 51
6420 deg
RA of node: 259
1531 deg
Eccentricity:
0008170
Arg of perigee: 282
2466 deg
Mean anomaly: 77
7772 deg
Mean motion: 15
54757890 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1625
Checksum: 311
Coasting Arc #15 (Orbit 1640)
---------------------------------------
Vector Time (GMT): 2015/350/11:25:26
438
Vector Time (MET): N/A
Weight (LBS) : 906038
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1660332
03 A = 6787393
47 meter
Y = -6564196
07 meter E =
0010829
Z = 352165
68 I = 51
30820
XDOT = 4732
000839 Wp = 8
99622
YDOT = -875
596962 meter/sec RA = 253
41800 deg
ZDOT = 5974
522824 TA = 354
81947
MA = 354
83066
Ha = 218
634 n
mi
Hp = 216
892
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5447283
55 X = -1588516
85
Y = -21536076
36 feet Y = -6582361
48 meter
Z = 1155399
21 Z = 344274
21
XDOT = 15524
937137 XDOT = 4712
418479
YDOT = -2872
693444 feet/sec YDOT = -822
790437 meter/sec
ZDOT = 19601
452836 ZDOT = 5997
462208
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22215206
17 X = 6771194
84
Y = 187018
69 feet Y = 57003
30 meter
Z = 1122528
05 Z = 342146
55
XDOT = -1115
825059 XDOT = -340
103478
YDOT = 14003
662344 feet/sec YDOT = 4268
316282 meter/sec
ZDOT = 19700
755887 ZDOT = 6004
790394
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 15350
53961997
00016717 00000-0 10270-3 0 9145
2 25544 51
6415 254
0207 0008231 286
6033 73
4216 15
54778714 16410
Satellite: ISS
Catalog Number: 25544
Epoch time: 15350
53961997 = yrday
fracday
Element set: 914
Inclination: 51
6415 deg
RA of node: 254
0207 deg
Eccentricity:
0008231
Arg of perigee: 286
6033 deg
Mean anomaly: 73
4216 deg
Mean motion: 15
54778714 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1641
Checksum: 309
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