[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 22nd 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 127 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 568 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 2371)
---------------------------------------
Vector Time (GMT): 2015/140/10:37:02
026
Vector Time (MET): N/A
Weight (LBS) : 910639
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5446556
39 A = 6786277
21 meter
Y = -3954368
24 meter E =
0011332
Z = -812246
37 I = 51
41745
XDOT = 2255
860766 Wp = 19
56686
YDOT = -4317
391462 meter/sec RA = 221
50558 deg
ZDOT = 5926
615040 TA = 331
61694
MA = 331
67862
Ha = 218
897 n
mi
Hp = 214
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17869279
50 X = -5397987
27
Y = -12973649
07 feet Y = -4015003
55 meter
Z = -2664850
31 Z = -838587
40
XDOT = 7401
118000 XDOT = 2275
181581
YDOT = -14164
670150 feet/sec YDOT = -4292
057459 meter/sec
ZDOT = 19444
275067 ZDOT = 5937
620248
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22068318
27 X = -6726423
41
Y = 70745
26 feet Y = 21563
16 meter
Z = -2777133
63 Z = -846470
33
XDOT = -2484
558296 XDOT = -757
293369
YDOT = -14118
081182 feet/sec YDOT = -4303
191144 meter/sec
ZDOT = 19492
221840 ZDOT = 5941
229217
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 15140
44402236
00016717 00000-0 10270-3 0 9003
2 25544 51
6442 222
5566 0003929 316
2947 43
7894 15
55074071 23721
Satellite: ISS
Catalog Number: 25544
Epoch time: 15140
44402236 = yrday
fracday
Element set: 900
Inclination: 51
6442 deg
RA of node: 222
5566 deg
Eccentricity:
0003929
Arg of perigee: 316
2947 deg
Mean anomaly: 43
7894 deg
Mean motion: 15
55074071 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2372
Checksum: 298
Coasting Arc #2 (Orbit 2387)
---------------------------------------
Vector Time (GMT): 2015/141/10:37:02
026
Vector Time (MET): N/A
Weight (LBS) : 910639
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4717268
35 A = 6785823
99 meter
Y = 4716071
71 meter E =
0005321
Z = -1233348
71 I = 51
43981
XDOT = -4196
460606 Wp = 144
67651
YDOT = 2676
904457 meter/sec RA = 216
51686 deg
ZDOT = -5831
408899 TA = 48
76879
MA = 48
72295
Ha = 218
959 n
mi
Hp = 213
987
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15476602
20 X = 4670172
71
Y = 15472676
22 feet Y = 4768560
08 meter
Z = -4046419
65 Z = -1210546
90
XDOT = -13767
915373 XDOT = -4197
755459
YDOT = 8782
494939 feet/sec YDOT = 2629
970178 meter/sec
ZDOT = -19131
918961 ZDOT = -5851
797571
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21701167
43 X = 6614515
83
Y = 2960367
06 feet Y = 902319
88 meter
Z = -3949429
85 Z = -1203786
22
XDOT = -5350
931585 XDOT = -1630
963947
YDOT = 13659
793567 feet/sec YDOT = 4163
505079 meter/sec
ZDOT = -19219
833313 ZDOT = -5858
205194
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 15141
47220626
00016717 00000-0 10270-3 0 9019
2 25544 51
6434 217
4239 0003860 319
1282 40
9581 15
55122046 23885
Satellite: ISS
Catalog Number: 25544
Epoch time: 15141
47220626 = yrday
fracday
Element set: 901
Inclination: 51
6434 deg
RA of node: 217
4239 deg
Eccentricity:
0003860
Arg of perigee: 319
1282 deg
Mean anomaly: 40
9581 deg
Mean motion: 15
55122046 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2388
Checksum: 288
Coasting Arc #3 (Orbit 2403)
---------------------------------------
Vector Time (GMT): 2015/142/10:37:02
026
Vector Time (MET): N/A
Weight (LBS) : 910639
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3412297
68 A = 6782320
75 meter
Y = -4975363
40 meter E =
0011600
Z = 3084046
19 I = 51
45465
XDOT = 5842
318652 Wp = 67
56881
YDOT = -976
441115 meter/sec RA = 211
52210 deg
ZDOT = 4878
548126 TA = 328
02031
MA = 328
09067
Ha = 219
042 n
mi
Hp = 213
818
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11195202
35 X = -3371389
59
Y = -16323370
74 feet Y = -5013293
46 meter
Z = 10118261
79 Z = 3067568
77
XDOT = 19167
712113 XDOT = 5829
104942
YDOT = -3203
546964 feet/sec YDOT = -911
182768 meter/sec
ZDOT = 16005
735323 ZDOT = 4906
896967
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18938282
76 X = -5772388
58
Y = -5876625
08 feet Y = -1791195
32 meter
Z = 10048429
40 Z = 3062761
28
XDOT = 12583
467363 XDOT = 3835
440852
YDOT = -12917
203226 feet/sec YDOT = -3937
163543 meter/sec
ZDOT = 16127
514581 ZDOT = 4915
666444
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 15142
50036813
00016717 00000-0 10270-3 0 9028
2 25544 51
6435 212
2900 0003910 324
3095 35
7796 15
55169617 24044
Satellite: ISS
Catalog Number: 25544
Epoch time: 15142
50036813 = yrday
fracday
Element set: 902
Inclination: 51
6435 deg
RA of node: 212
2900 deg
Eccentricity:
0003910
Arg of perigee: 324
3095 deg
Mean anomaly: 35
7796 deg
Mean motion: 15
55169617 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2404
Checksum: 286
Coasting Arc #4 (Orbit 2418)
---------------------------------------
Vector Time (GMT): 2015/143/10:37:02
026
Vector Time (MET): N/A
Weight (LBS) : 910639
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1617830
89 A = 6777753
68 meter
Y = 4812188
14 meter E =
0009527
Z = -4499886
11 I = 51
46625
XDOT = -6943
212861 Wp = 45
71425
YDOT = -637
652681 meter/sec RA = 206
51625 deg
ZDOT = -3175
838476 TA = 192
27529
MA = 192
29851
Ha = 219
105 n
mi
Hp = 213
753
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5307844
12 X = 1585758
46
Y = 15788018
83 feet Y = 4830100
76 meter
Z = -14763405
87 Z = -4492104
54
XDOT = -22779
569755 XDOT = -6920
139345
YDOT = -2092
036355 feet/sec YDOT = -715
166999 meter/sec
ZDOT = -10419
417571 ZDOT = -3209
511397
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14155562
10 X = 4314615
33
Y = 8832627
81 feet Y = 2692184
96 meter
Z = -14730840
03 Z = -4489960
04
XDOT = -18291
489344 XDOT = -5575
245952
YDOT = 11683
902423 feet/sec YDOT = 3561
253458 meter/sec
ZDOT = -10563
778256 ZDOT = -3219
839613
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 15143
46425234
00016717 00000-0 10270-3 0 9034
2 25544 51
6428 207
4781 0003995 327
6248 32
4659 15
55172323 24194
Satellite: ISS
Catalog Number: 25544
Epoch time: 15143
46425234 = yrday
fracday
Element set: 903
Inclination: 51
6428 deg
RA of node: 207
4781 deg
Eccentricity:
0003995
Arg of perigee: 327
6248 deg
Mean anomaly: 32
4659 deg
Mean motion: 15
55172323 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2419
Checksum: 312
Coasting Arc #5 (Orbit 2434)
---------------------------------------
Vector Time (GMT): 2015/144/10:37:02
026
Vector Time (MET): N/A
Weight (LBS) : 910639
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 481848
89 A = 6774465
55 meter
Y = -4281091
08 meter E =
0001986
Z = 5226877
12 I = 51
48520
XDOT = 7329
389596 Wp = 36
97567
YDOT = 2036
664342 meter/sec RA = 201
49742 deg
ZDOT = 993
822643 TA = 43
50229
MA = 43
48663
Ha = 219
071 n
mi
Hp = 213
528
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1580869
08 X = 504294
96
Y = -14045574
40 feet Y = -4275577
51 meter
Z = 17148546
97 Z = 5229272
14
XDOT = 24046
553794 XDOT = 7301
242756
YDOT = 6681
969625 feet/sec YDOT = 2118
468937 meter/sec
ZDOT = 3260
572975 ZDOT = 1029
359280
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7927116
17 X = -2416185
01
Y = -11685917
87 feet Y = -3561867
77 meter
Z = 17159549
04 Z = 5230230
55
XDOT = 21823
441971 XDOT = 6651
785113
YDOT = -9799
214354 feet/sec YDOT = -2986
800535 meter/sec
ZDOT = 3412
711258 ZDOT = 1040
194391
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 15144
49237372
00016717 00000-0 10270-3 0 9043
2 25544 51
6432 202
3439 0004068 332
0131 28
0803 15
55240811 24354
Satellite: ISS
Catalog Number: 25544
Epoch time: 15144
49237372 = yrday
fracday
Element set: 904
Inclination: 51
6432 deg
RA of node: 202
3439 deg
Eccentricity:
0004068
Arg of perigee: 332
0131 deg
Mean anomaly: 28
0803 deg
Mean motion: 15
55240811 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2435
Checksum: 271
Coasting Arc #6 (Orbit 2449)
---------------------------------------
Vector Time (GMT): 2015/145/10:37:02
026
Vector Time (MET): N/A
Weight (LBS) : 910639
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2625723
05 A = 6774681
90 meter
Y = 3512787
05 meter E =
0012289
Z = -5173847
28 I = 51
51500
XDOT = -6855
160995 Wp = 83
61585
YDOT = -3144
948832 meter/sec RA = 196
47653 deg
ZDOT = 1347
817088 TA = 199
34822
MA = 199
39492
Ha = 219
265 n
mi
Hp = 213
282
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8614576
92 X = -2639675
99
Y = 11524891
91 feet Y = 3483346
71 meter
Z = -16974564
58 Z = -5186636
33
XDOT = -22490
685678 XDOT = -6826
031157
YDOT = -10318
073595 feet/sec YDOT = -3221
444910 meter/sec
ZDOT = 4421
972075 ZDOT = 1314
586497
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1169788
73 X = 356551
61
Y = 14275127
64 feet Y = 4351058
91 meter
Z = -17030039
25 Z = -5190755
96
XDOT = -22708
231242 XDOT = -6921
468883
YDOT = 6950
738305 feet/sec YDOT = 2118
585035 meter/sec
ZDOT = 4279
898245 ZDOT = 1304
512985
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 15145
45622113
00016717 00000-0 10270-3 0 9052
2 25544 51
6424 197
5316 0004197 337
7264 22
3706 15
55239605 24501
Satellite: ISS
Catalog Number: 25544
Epoch time: 15145
45622113 = yrday
fracday
Element set: 905
Inclination: 51
6424 deg
RA of node: 197
5316 deg
Eccentricity:
0004197
Arg of perigee: 337
7264 deg
Mean anomaly: 22
3706 deg
Mean motion: 15
55239605 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2450
Checksum: 297
Coasting Arc #7 (Orbit 2465)
---------------------------------------
Vector Time (GMT): 2015/146/10:37:02
026
Vector Time (MET): N/A
Weight (LBS) : 910639
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4562655
24 A = 6777921
11 meter
Y = -2562033
36 meter E =
0010522
Z = 4305538
23 I = 51
55787
XDOT = 5549
354431 Wp = 48
10231
YDOT = 3966
581346 meter/sec RA = 191
46295 deg
ZDOT = -3508
007157 TA = 77
68288
MA = 77
56510
Ha = 219
198 n
mi
Hp = 213
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14969341
32 X = 4570050
56
Y = -8405621
26 feet Y = -2510969
58 meter
Z = 14125781
60 Z = 4327720
74
XDOT = 18206
543409 XDOT = 5521
627431
YDOT = 13013
718326 feet/sec YDOT = 4028
482960 meter/sec
ZDOT = -11509
209833 ZDOT = -3481
116479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5404145
62 X = 1647183
58
Y = -16211721
54 feet Y = -4941332
72 meter
Z = 14221415
16 Z = 4334687
34
XDOT = 21104
445345 XDOT = 6432
634941
YDOT = -2995
915153 feet/sec YDOT = -913
154939 meter/sec
ZDOT = -11394
467116 ZDOT = -3473
033577
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 15146
48430357
00016717 00000-0 10270-3 0 9064
2 25544 51
6430 192
3972 0004295 341
1070 18
9924 15
55308311 24663
Satellite: ISS
Catalog Number: 25544
Epoch time: 15146
48430357 = yrday
fracday
Element set: 906
Inclination: 51
6430 deg
RA of node: 192
3972 deg
Eccentricity:
0004295
Arg of perigee: 341
1070 deg
Mean anomaly: 18
9924 deg
Mean motion: 15
55308311 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2466
Checksum: 301
Coasting Arc #8 (Orbit 2480)
---------------------------------------
Vector Time (GMT): 2015/147/10:37:02
026
Vector Time (MET): N/A
Weight (LBS) : 910639
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5984828
91 A = 6782506
81 meter
Y = 1544170
64 meter E =
0007094
Z = -2786621
27 I = 51
60362
XDOT = -3535
377826 Wp = 26
48544
YDOT = -4483
830979 meter/sec RA = 186
46641 deg
ZDOT = 5119
510618 TA = 301
88508
MA = 301
95408
Ha = 219
323 n
mi
Hp = 212
971
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19635265
46 X = -5988114
90
Y = 5066176
66 feet Y = 1477226
10 meter
Z = -9142458
25 Z = -2815702
61
XDOT = -11599
008614 XDOT = -3509
844696
YDOT = -14710
731559 feet/sec YDOT = -4523
223311 meter/sec
ZDOT = 16796
294679 ZDOT = 5102
398130
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10835987
93 X = -3302809
12
Y = 17073030
80 feet Y = 5203859
79 meter
Z = -9267541
38 Z = -2824746
61
XDOT = -17351
903387 XDOT = -5288
860152
YDOT = -1954
858982 feet/sec YDOT = -595
841018 meter/sec
ZDOT = 16723
596492 ZDOT = 5097
352211
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 15147
44811472
00016717 00000-0 10270-3 0 9073
2 25544 51
6421 187
5844 0004237 346
4533 13
6506 15
55309172 24816
Satellite: ISS
Catalog Number: 25544
Epoch time: 15147
44811472 = yrday
fracday
Element set: 907
Inclination: 51
6421 deg
RA of node: 187
5844 deg
Eccentricity:
0004237
Arg of perigee: 346
4533 deg
Mean anomaly: 13
6506 deg
Mean motion: 15
55309172 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2481
Checksum: 303
Coasting Arc #9 (Orbit 2496)
---------------------------------------
Vector Time (GMT): 2015/148/10:37:02
026
Vector Time (MET): N/A
Weight (LBS) : 910639
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6720375
42 A = 6785465
91 meter
Y = -452689
66 meter E =
0010795
Z = 792031
28 I = 51
64588
XDOT = 1026
882063 Wp = 109
51562
YDOT = 4732
813593 meter/sec RA = 181
48523 deg
ZDOT = -5945
512450 TA = 61
91985
MA = 61
81076
Ha = 219
490 n
mi
Hp = 212
768
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22048475
77 X = 6721090
59
Y = -1485202
28 feet Y = -377534
05 meter
Z = 2598527
81 Z = 824679
67
XDOT = 3369
035640 XDOT = 1002
763713
YDOT = 15527
603650 feet/sec YDOT = 4744
162242 meter/sec
ZDOT = -19506
274442 ZDOT = -5940
582389
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14794796
74 X = 4509454
05
Y = -16392275
02 feet Y = -4996365
43 meter
Z = 2738752
55 Z = 834771
78
XDOT = 12114
028510 XDOT = 3692
355890
YDOT = 7645
347703 feet/sec YDOT = 2330
301980 meter/sec
ZDOT = -19485
906320 ZDOT = -5939
304246
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 15148
47615914
00016717 00000-0 10270-3 0 9081
2 25544 51
6425 182
4499 0004400 351
9397 8
1685 15
55356266 24971
Satellite: ISS
Catalog Number: 25544
Epoch time: 15148
47615914 = yrday
fracday
Element set: 908
Inclination: 51
6425 deg
RA of node: 182
4499 deg
Eccentricity:
0004400
Arg of perigee: 351
9397 deg
Mean anomaly: 8
1685 deg
Mean motion: 15
55356266 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2497
Checksum: 336
Coasting Arc #10 (Orbit 2512)
---------------------------------------
Vector Time (GMT): 2015/149/10:37:02
026
Vector Time (MET): N/A
Weight (LBS) : 910639
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6618543
12 A = 6785184
86 meter
Y = -630882
44 meter E =
0016415
Z = 1306258
16 I = 51
67543
XDOT = 1608
224297 Wp = 45
39694
YDOT = -4719
288053 meter/sec RA = 176
51071 deg
ZDOT = 5835
494667 TA = 328
82874
MA = 328
92600
Ha = 219
723 n
mi
Hp = 212
709
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21714380
32 X = -6617341
94
Y = -2069824
29 feet Y = -704888
67 meter
Z = 4285623
89 Z = 1274108
98
XDOT = 5276
326433 XDOT = 1632
529913
YDOT = -15483
228520 feet/sec YDOT = -4701
168219 meter/sec
ZDOT = 19145
323710 ZDOT = 5843
366032
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16821610
67 X = -5127226
93
Y = 13928207
81 feet Y = 4245317
74 meter
Z = 4147710
12 Z = 1264222
04
XDOT = -6302
336429 XDOT = -1920
952144
YDOT = -13357
289338 feet/sec YDOT = -4071
301790 meter/sec
ZDOT = 19179
911318 ZDOT = 5846
036970
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 15149
50418567
00016717 00000-0 10270-3 0 9092
2 25544 51
6417 177
3155 0004516 357
6631 2
4501 15
55323668 25139
Satellite: ISS
Catalog Number: 25544
Epoch time: 15149
50418567 = yrday
fracday
Element set: 909
Inclination: 51
6417 deg
RA of node: 177
3155 deg
Eccentricity:
0004516
Arg of perigee: 357
6631 deg
Mean anomaly: 2
4501 deg
Mean motion: 15
55323668 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2513
Checksum: 305
Coasting Arc #11 (Orbit 2527)
---------------------------------------
Vector Time (GMT): 2015/150/10:37:02
026
Vector Time (MET): N/A
Weight (LBS) : 910639
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5705712
49 A = 6781279
87 meter
Y = 1734799
53 meter E =
0005821
Z = -3236174
01 I = 51
69531
XDOT = -4050
002525 Wp = 52
33806
YDOT = 4416
639670 meter/sec RA = 171
53080 deg
ZDOT = -4775
378610 TA = 165
09228
MA = 165
07511
Ha = 219
633 n
mi
Hp = 212
549
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18719529
18 X = 5701609
87
Y = 5691599
50 feet Y = 1798581
80 meter
Z = -10617368
79 Z = -3208466
16
XDOT = -13287
409860 XDOT = -4075
892055
YDOT = 14490
287630 feet/sec YDOT = 4371
205437 meter/sec
ZDOT = -15667
252659 ZDOT = -4795
115669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17135850
72 X = 5223007
30
Y = -9575154
84 feet Y = -2918507
19 meter
Z = -10498696
46 Z = -3200002
68
XDOT = 579
526247 XDOT = 176
639600
YDOT = 18300
496177 feet/sec YDOT = 5577
991235 meter/sec
ZDOT = -15752
742875 ZDOT = -4801
436028
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 15150
46793881
00016717 00000-0 10270-3 0 9106
2 25544 51
6423 172
5017 0004411 1
2772 358
8392 15
55403646 25289
Satellite: ISS
Catalog Number: 25544
Epoch time: 15150
46793881 = yrday
fracday
Element set: 910
Inclination: 51
6423 deg
RA of node: 172
5017 deg
Eccentricity:
0004411
Arg of perigee: 1
2772 deg
Mean anomaly: 358
8392 deg
Mean motion: 15
55403646 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2528
Checksum: 299
Coasting Arc #12 (Orbit 2543)
---------------------------------------
Vector Time (GMT): 2015/151/10:37:02
026
Vector Time (MET): N/A
Weight (LBS) : 910639
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4087355
66 A = 6776541
94 meter
Y = -2778950
37 meter E =
0008164
Z = 4628575
17 I = 51
70966
XDOT = 5957
883861 Wp = 84
00969
YDOT = -3828
360749 meter/sec RA = 166
53756 deg
ZDOT = 2959
073708 TA = 336
55198
MA = 336
58918
Ha = 219
800 n
mi
Hp = 212
299
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13409959
50 X = -4078461
26
Y = -9117291
25 feet Y = -2824608
50 meter
Z = 15185614
06 Z = 4608740
62
XDOT = 19546
863062 XDOT = 5985
876382
YDOT = -12560
238679 feet/sec YDOT = -3761
579523 meter/sec
ZDOT = 9708
247075 ZDOT = 2988
084132
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15876032
94 X = -4839014
84
Y = 3669986
72 feet Y = 1118611
95 meter
Z = 15100915
98 Z = 4602759
19
XDOT = 4357
689018 XDOT = 1328
223613
YDOT = -21660
357032 feet/sec YDOT = -6602
076823 meter/sec
ZDOT = 9833
472538 ZDOT = 2997
242430
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 15151
49592383
00016717 00000-0 10270-3 0 9115
2 25544 51
6410 167
3668 0004434 5
9075 354
2129 15
55426640 25446
Satellite: ISS
Catalog Number: 25544
Epoch time: 15151
49592383 = yrday
fracday
Element set: 911
Inclination: 51
6410 deg
RA of node: 167
3668 deg
Eccentricity:
0004434
Arg of perigee: 5
9075 deg
Mean anomaly: 354
2129 deg
Mean motion: 15
55426640 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2544
Checksum: 305
Coasting Arc #13 (Orbit 2558)
---------------------------------------
Vector Time (GMT): 2015/152/10:37:02
026
Vector Time (MET): N/A
Weight (LBS) : 910639
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2015094
47 A = 6773704
45 meter
Y = 3731331
83 meter E =
0016250
Z = -5295688
97 I = 51
73192
XDOT = -7061
847691 Wp = 69
67679
YDOT = 2894
066631 meter/sec RA = 161
53260 deg
ZDOT = -644
088241 TA = 194
15156
MA = 194
19714
Ha = 219
733 n
mi
Hp = 212
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6611202
33 X = 1998944
95
Y = 12241902
32 feet Y = 3753776
17 meter
Z = -17374307
65 Z = -5285938
72
XDOT = -23168
791638 XDOT = -7090
556190
YDOT = 9494
969262 feet/sec YDOT = 2814
935979 meter/sec
ZDOT = -2113
150397 ZDOT = -678
463333
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13594919
11 X = 4143731
34
Y = 3190840
15 feet Y = 972568
08 meter
Z = -17333073
83 Z = -5283120
90
XDOT = -8197
275245 XDOT = -2498
529495
YDOT = 22572
073048 feet/sec YDOT = 6879
967865 meter/sec
ZDOT = -2261
275717 ZDOT = -689
236839
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 15152
45964160
00016717 00000-0 10270-3 0 9129
2 25544 51
6419 162
5528 0004440 8
0723 352
0501 15
55438637 25593
Satellite: ISS
Catalog Number: 25544
Epoch time: 15152
45964160 = yrday
fracday
Element set: 912
Inclination: 51
6419 deg
RA of node: 162
5528 deg
Eccentricity:
0004440
Arg of perigee: 8
0723 deg
Mean anomaly: 352
0501 deg
Mean motion: 15
55438637 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2559
Checksum: 296
Coasting Arc #14 (Orbit 2574)
---------------------------------------
Vector Time (GMT): 2015/153/10:37:02
026
Vector Time (MET): N/A
Weight (LBS) : 910639
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 259167
92 A = 6774373
13 meter
Y = -4474234
16 meter E =
0009161
Z = 5077288
28 I = 51
76332
XDOT = 7282
066682 Wp = 36
27780
YDOT = -1622
503794 meter/sec RA = 156
52550 deg
ZDOT = -1792
634056 TA = 71
07591
MA = 70
97662
Ha = 219
739 n
mi
Hp = 211
973
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 850288
45 X = 284516
70
Y = -14679245
93 feet Y = -4471194
83 meter
Z = 16657769
93 Z = 5078608
33
XDOT = 23891
294890 XDOT = 7308
376752
YDOT = -5323
175178 feet/sec YDOT = -1540
923646 meter/sec
ZDOT = -5881
345329 ZDOT = -1757
194967
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10589812
80 X = -3227774
94
Y = -10190408
15 feet Y = -3106036
41 meter
Z = 16664213
06 Z = 5079252
14
XDOT = 10935
719179 XDOT = 3333
207206
YDOT = -20780
179628 feet/sec YDOT = -6333
798751 meter/sec
ZDOT = -5728
845417 ZDOT = -1746
152083
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 15153
48758640
00016717 00000-0 10270-3 0 9138
2 25544 51
6405 157
4173 0004523 13
2138 346
9133 15
55499230 25754
Satellite: ISS
Catalog Number: 25544
Epoch time: 15153
48758640 = yrday
fracday
Element set: 913
Inclination: 51
6405 deg
RA of node: 157
4173 deg
Eccentricity:
0004523
Arg of perigee: 13
2138 deg
Mean anomaly: 346
9133 deg
Mean motion: 15
55499230 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2575
Checksum: 306
Coasting Arc #15 (Orbit 2589)
---------------------------------------
Vector Time (GMT): 2015/154/10:37:02
026
Vector Time (MET): N/A
Weight (LBS) : 910639
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2368974
26 A = 6778332
81 meter
Y = 4902618
68 meter E =
0008398
Z = -4042563
42 I = 51
80658
XDOT = -6580
967599 Wp = 75
67095
YDOT = 52
444813 meter/sec RA = 151
52986 deg
ZDOT = 3928
951352 TA = 234
99895
MA = 235
07781
Ha = 219
801 n
mi
Hp = 211
820
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7772225
27 X = -2403982
98
Y = 16084706
97 feet Y = 4875932
03 meter
Z = -13263003
34 Z = -4054155
97
XDOT = -21591
101046 XDOT = -6600
150512
YDOT = 172
063035 feet/sec YDOT = -21
255624 meter/sec
ZDOT = 12890
260342 ZDOT = 3896
935353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7376216
50 X = 2248270
79
Y = 16228694
36 feet Y = 4946506
04 meter
Z = -13313656
56 Z = -4058002
52
XDOT = -12617
674777 XDOT = -3845
867272
YDOT = 16173
259315 feet/sec YDOT = 4929
609439 meter/sec
ZDOT = 12752
714604 ZDOT = 3887
027411
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 15154
45126659
00016717 00000-0 10270-3 0 9146
2 25544 51
6417 152
6033 0004598 16
1470 343
9829 15
55507363 25905
Satellite: ISS
Catalog Number: 25544
Epoch time: 15154
45126659 = yrday
fracday
Element set: 914
Inclination: 51
6417 deg
RA of node: 152
6033 deg
Eccentricity:
0004598
Arg of perigee: 16
1470 deg
Mean anomaly: 343
9829 deg
Mean motion: 15
55507363 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2590
Checksum: 315
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