[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 7th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21527 82 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 127 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 423 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
281/09:17:17
621 -1
1 3
8 3
9
N/A -3
7 -0
6 226
4
000/00:08:35
242 0
6 -0
0 221
4
Coasting Arc #1 (Orbit 2859)
---------------------------------------
Vector Time (GMT): 2014/279/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 989883
49 A = 6798313
29 meter
Y = 6670996
99 meter E =
0015020
Z = 796535
43 I = 51
30002
XDOT = -4670
151749 Wp = 127
72145
YDOT = 1407
154218 meter/sec RA = 266
98934 deg
ZDOT = -5913
511762 TA = 43
63457
MA = 43
51590
Ha = 226
454 n
mi
Hp = 219
217
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3247649
23 X = 911343
94
Y = 21886473
05 feet Y = 6681627
48 meter
Z = 2613305
22 Z = 801152
45
XDOT = -15322
020174 XDOT = -4656
813590
YDOT = 4616
647697 feet/sec YDOT = 1355
003275 meter/sec
ZDOT = -19401
285310 ZDOT = -5936
166695
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8516105
80 X = -2595709
05
Y = -20419196
78 feet Y = -6223771
18 meter
Z = 2631850
52 Z = 802188
04
XDOT = 12108
036680 XDOT = 3690
529580
YDOT = -7591
329304 feet/sec YDOT = -2313
837172 meter/sec
ZDOT = -19497
846460 ZDOT = -5942
943601
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 14279
53381035
00016717 00000-0 10270-3 0 9008
2 25544 51
6419 267
6700 0001733 138
1373 221
9910 15
50950788 28604
Satellite: ISS
Catalog Number: 25544
Epoch time: 14279
53381035 = yrday
fracday
Element set: 900
Inclination: 51
6419 deg
RA of node: 267
6700 deg
Eccentricity:
0001733
Arg of perigee: 138
1373 deg
Mean anomaly: 221
9910 deg
Mean motion: 15
50950788 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2860
Checksum: 306
Coasting Arc #2 (Orbit 2874)
---------------------------------------
Vector Time (GMT): 2014/280/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1067424
57 A = 6798379
98 meter
Y = -6707753
90 meter E =
0011532
Z = -155528
01 I = 51
30311
XDOT = 4711
719596 Wp = 53
83189
YDOT = -881
016589 meter/sec RA = 262
00920 deg
ZDOT = 5977
620425 TA = 304
48730
MA = 304
59618
Ha = 226
371 n
mi
Hp = 219
132
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3502049
11 X = -991582
06
Y = -22007066
62 feet Y = -6719266
50 meter
Z = -510262
50 Z = -160528
28
XDOT = 15458
397624 XDOT = 4692
183394
YDOT = -2890
474372 feet/sec YDOT = -828
435446 meter/sec
ZDOT = 19611
615569 ZDOT = 6000
462269
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9155960
13 X = 2790736
65
Y = 20315578
32 feet Y = 6192188
27 meter
Z = -530441
68 Z = -161678
63
XDOT = -12555
999085 XDOT = -3827
068521
YDOT = 6147
221676 feet/sec YDOT = 1873
673167 meter/sec
ZDOT = 19708
884881 ZDOT = 6007
268112
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 14280
50031428
00016717 00000-0 10270-3 0 9016
2 25544 51
6415 262
8749 0001955 145
7842 214
3435 15
51015274 28758
Satellite: ISS
Catalog Number: 25544
Epoch time: 14280
50031428 = yrday
fracday
Element set: 901
Inclination: 51
6415 deg
RA of node: 262
8749 deg
Eccentricity:
0001955
Arg of perigee: 145
7842 deg
Mean anomaly: 214
3435 deg
Mean motion: 15
51015274 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2875
Checksum: 298
Coasting Arc #3 (Orbit 2888)
---------------------------------------
Vector Time (GMT): 2014/281/09:21:35
242
Vector Time (MET): N/A
Weight (LBS) : 946181
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4401469
50 A = 6790168
13 meter
Y = -1531139
62 meter E =
0010892
Z = -4948662
31 I = 51
27598
XDOT = 141
165252 Wp = 115
44668
YDOT = -7345
022048 meter/sec RA = 257
55377 deg
ZDOT = 2146
153876 TA = 175
62334
MA = 175
61381
Ha = 226
391 n
mi
Hp = 221
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14440516
73 X = -4359981
38
Y = -5023423
96 feet Y = -1580128
42 meter
Z = -16235768
74 Z = -4969943
41
XDOT = 463
140590 XDOT = 212
862991
YDOT = -24097
841364 feet/sec YDOT = -7343
042263 meter/sec
ZDOT = 7041
187256 ZDOT = 2147
014821
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11145273
11 X = 3397079
25
Y = 10325096
87 feet Y = 3147089
52 meter
Z = -16326014
83 Z = -4976169
32
XDOT = -9239
475576 XDOT = -2816
192156
YDOT = 21119
085491 feet/sec YDOT = 6437
097258 meter/sec
ZDOT = 7046
026211 ZDOT = 2147
628789
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 14281
40236598
00016717 00000-0 10270-3 0 9022
2 25544 51
6446 258
3972 0002491 239
1009 120
9897 15
50260770 28890
Satellite: ISS
Catalog Number: 25544
Epoch time: 14281
40236598 = yrday
fracday
Element set: 902
Inclination: 51
6446 deg
RA of node: 258
3972 deg
Eccentricity:
0002491
Arg of perigee: 239
1009 deg
Mean anomaly: 120
9897 deg
Mean motion: 15
50260770 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2889
Checksum: 326
Coasting Arc #4 (Orbit 2904)
---------------------------------------
Vector Time (GMT): 2014/282/09:21:35
242
Vector Time (MET): N/A
Weight (LBS) : 946181
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4532385
33 A = 6790693
84 meter
Y = 1685430
81 meter E =
0005018
Z = 4764816
95 I = 51
28494
XDOT = 69
282003 Wp = 61
34772
YDOT = 7205
198088 meter/sec RA = 252
56952 deg
ZDOT = -2610
092639 TA = 54
55587
MA = 54
50904
Ha = 226
129 n
mi
Hp = 221
417
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14870030
61 X = 4490055
17
Y = 5529628
65 feet Y = 1735878
79 meter
Z = 15632601
53 Z = 4786732
06
XDOT = 227
303159 XDOT = 1
385911
YDOT = 23639
101340 feet/sec YDOT = 7205
592893 meter/sec
ZDOT = -8563
296059 ZDOT = -2609
921879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11527705
76 X = -3513644
72
Y = -10765350
28 feet Y = -3281278
76 meter
Z = 15725522
80 Z = 4793139
35
XDOT = 8006
261834 XDOT = 2440
308607
YDOT = -21103
972582 feet/sec YDOT = -6432
490843 meter/sec
ZDOT = -8563
719385 ZDOT = -2610
221669
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 14282
43374312
00016717 00000-0 10270-3 0 9034
2 25544 51
6435 253
2844 0002415 241
7621 118
3286 15
50327961 29053
Satellite: ISS
Catalog Number: 25544
Epoch time: 14282
43374312 = yrday
fracday
Element set: 903
Inclination: 51
6435 deg
RA of node: 253
2844 deg
Eccentricity:
0002415
Arg of perigee: 241
7621 deg
Mean anomaly: 118
3286 deg
Mean motion: 15
50327961 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2905
Checksum: 291
Coasting Arc #5 (Orbit 2919)
---------------------------------------
Vector Time (GMT): 2014/283/09:21:35
242
Vector Time (MET): N/A
Weight (LBS) : 946181
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4701807
75 A = 6791534
56 meter
Y = -1823519
82 meter E =
0008389
Z = -4557425
52 I = 51
29863
XDOT = -243
222053 Wp = 121
78289
YDOT = -7013
427974 meter/sec RA = 247
58710 deg
ZDOT = 3056
976770 TA = 178
99745
MA = 178
99577
Ha = 226
199 n
mi
Hp = 221
339
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15425878
45 X = -4658928
29
Y = -5982676
59 feet Y = -1875859
20 meter
Z = -14952183
48 Z = -4580162
39
XDOT = -797
972614 XDOT = -179
628333
YDOT = -23009
934299 feet/sec YDOT = -7015
791950 meter/sec
ZDOT = 10029
451346 ZDOT = 3055
950405
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12065999
92 X = 3677716
78
Y = 11192396
35 feet Y = 3411442
41 meter
Z = -15048582
85 Z = -4586808
05
XDOT = -6825
978475 XDOT = -2080
558239
YDOT = 20840
094474 feet/sec YDOT = 6352
060796 meter/sec
ZDOT = 10026
200878 ZDOT = 3055
986027
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 14283
40063801
00016717 00000-0 10270-3 0 9041
2 25544 51
6441 248
4921 0002451 247
1341 112
9551 15
50328293 29202
Satellite: ISS
Catalog Number: 25544
Epoch time: 14283
40063801 = yrday
fracday
Element set: 904
Inclination: 51
6441 deg
RA of node: 248
4921 deg
Eccentricity:
0002451
Arg of perigee: 247
1341 deg
Mean anomaly: 112
9551 deg
Mean motion: 15
50328293 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2920
Checksum: 277
Coasting Arc #6 (Orbit 2935)
---------------------------------------
Vector Time (GMT): 2014/284/09:21:35
242
Vector Time (MET): N/A
Weight (LBS) : 946181
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4883821
05 A = 6792295
30 meter
Y = 1952147
79 meter E =
0007260
Z = 4293301
73 I = 51
31368
XDOT = 366
439644 Wp = 72
79820
YDOT = 6805
894580 meter/sec RA = 242
60500 deg
ZDOT = -3504
423104 TA = 53
09455
MA = 53
02805
Ha = 225
923 n
mi
Hp = 221
373
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16023034
95 X = 4840772
79
Y = 6404684
33 feet Y = 2006521
50 meter
Z = 14085635
61 Z = 4316922
41
XDOT = 1202
229802 XDOT = 307
331037
YDOT = 22329
050458 feet/sec YDOT = 6809
661552 meter/sec
ZDOT = -11497
451127 ZDOT = -3502
787106
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12672968
23 X = -3862720
72
Y = -11589747
94 feet Y = -3532555
17 meter
Z = 14185780
91 Z = 4323826
02
XDOT = 5796
085669 XDOT = 1766
646912
YDOT = -20431
461847 feet/sec YDOT = -6227
509571 meter/sec
ZDOT = -11491
570431 ZDOT = -3502
630667
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 14284
43196836
00016717 00000-0 10270-3 0 9051
2 25544 51
6431 243
3792 0002459 251
1345 108
9539 15
50399051 29366
Satellite: ISS
Catalog Number: 25544
Epoch time: 14284
43196836 = yrday
fracday
Element set: 905
Inclination: 51
6431 deg
RA of node: 243
3792 deg
Eccentricity:
0002459
Arg of perigee: 251
1345 deg
Mean anomaly: 108
9539 deg
Mean motion: 15
50399051 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2936
Checksum: 321
Coasting Arc #7 (Orbit 2950)
---------------------------------------
Vector Time (GMT): 2014/285/09:21:35
242
Vector Time (MET): N/A
Weight (LBS) : 946181
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5094444
51 A = 6793320
18 meter
Y = -2049397
49 meter E =
0005190
Z = -4005400
19 I = 51
33223
XDOT = -443
466929 Wp = 122
77258
YDOT = -6560
396473 meter/sec RA = 237
62536 deg
ZDOT = 3921
691185 TA = 188
22269
MA = 188
23120
Ha = 226
020 n
mi
Hp = 221
279
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16714056
78 X = -5051691
72
Y = -6723745
04 feet Y = -2106128
10 meter
Z = -13141076
75 Z = -4030044
76
XDOT = -1454
943992 XDOT = -389
124770
YDOT = -21523
610477 feet/sec YDOT = -6565
051487 meter/sec
ZDOT = 12866
440895 ZDOT = 3919
669302
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13420428
02 X = 4090546
46
Y = 11903919
25 feet Y = 3628314
59 meter
Z = -13245571
25 Z = -4037250
12
XDOT = -4888
934339 XDOT = -1490
147186
YDOT = 19816
425740 feet/sec YDOT = 6040
046566 meter/sec
ZDOT = 12858
874785 ZDOT = 3919
385035
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 14285
39881894
00016717 00000-0 10270-3 0 9063
2 25544 51
6431 238
5867 0002417 255
3571 104
7312 15
50398983 29519
Satellite: ISS
Catalog Number: 25544
Epoch time: 14285
39881894 = yrday
fracday
Element set: 906
Inclination: 51
6431 deg
RA of node: 238
5867 deg
Eccentricity:
0002417
Arg of perigee: 255
3571 deg
Mean anomaly: 104
7312 deg
Mean motion: 15
50398983 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2951
Checksum: 336
Coasting Arc #8 (Orbit 2966)
---------------------------------------
Vector Time (GMT): 2014/286/09:21:35
242
Vector Time (MET): N/A
Weight (LBS) : 946181
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5308027
00 A = 6794230
04 meter
Y = 2133523
10 meter E =
0009252
Z = 3657781
45 I = 51
35272
XDOT = 456
660749 Wp = 86
55616
YDOT = 6306
422974 meter/sec RA = 232
64649 deg
ZDOT = -4331
066231 TA = 49
83462
MA = 49
75363
Ha = 225
751 n
mi
Hp = 221
307
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17414786
73 X = 5266006
33
Y = 6999747
70 feet Y = 2192646
17 meter
Z = 12000595
30 Z = 3683465
30
XDOT = 1498
230803 XDOT = 407
146191
YDOT = 20690
364087 feet/sec YDOT = 6311
252523 meter/sec
ZDOT = -14209
534878 ZDOT = -4328
968472
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14206375
32 X = -4330103
20
Y = -12158299
43 feet Y = -3705849
66 meter
Z = 12109508
98 Z = 3690978
34
XDOT = 4197
361874 XDOT = 1279
355899
YDOT = -19081
576240 feet/sec YDOT = -5816
064438 meter/sec
ZDOT = -14201
599645 ZDOT = -4328
647572
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 14286
43010113
00016717 00000-0 10270-3 0 9078
2 25544 51
6423 233
4735 0002515 260
4683 99
6184 15
50470825 29670
Satellite: ISS
Catalog Number: 25544
Epoch time: 14286
43010113 = yrday
fracday
Element set: 907
Inclination: 51
6423 deg
RA of node: 233
4735 deg
Eccentricity:
0002515
Arg of perigee: 260
4683 deg
Mean anomaly: 99
6184 deg
Mean motion: 15
50470825 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2967
Checksum: 302
Coasting Arc #9 (Orbit 2981)
---------------------------------------
Vector Time (GMT): 2014/287/09:21:35
242
Vector Time (MET): N/A
Weight (LBS) : 946181
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5535531
24 A = 6795307
45 meter
Y = -2175021
66 meter E =
0002296
Z = -3288759
31 I = 51
37575
XDOT = -418
603916 Wp = 88
06030
YDOT = -6033
222640 meter/sec RA = 227
67023 deg
ZDOT = 4697
580633 TA = 233
66745
MA = 233
68865
Ha = 225
850 n
mi
Hp = 221
205
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18161191
74 X = -5494822
28
Y = -7135897
82 feet Y = -2236696
15 meter
Z = -10789892
75 Z = -3315551
47
XDOT = -1373
372428 XDOT = -373
927551
YDOT = -19794
037533 feet/sec YDOT = -6037
653635 meter/sec
ZDOT = 15412
009951 ZDOT = 4695
655997
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15091090
01 X = 4599764
23
Y = 12269628
82 feet Y = 3739782
86 meter
Z = -10903527
86 Z = -3323395
29
XDOT = -3683
400572 XDOT = -1122
700494
YDOT = 18211
565364 feet/sec YDOT = 5550
885123 meter/sec
ZDOT = 15404
761195 ZDOT = 4695
371212
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 14287
39690615
00016717 00000-0 10270-3 0 9086
2 25544 51
6420 228
6806 0002406 263
5727 96
5150 15
50475580 29823
Satellite: ISS
Catalog Number: 25544
Epoch time: 14287
39690615 = yrday
fracday
Element set: 908
Inclination: 51
6420 deg
RA of node: 228
6806 deg
Eccentricity:
0002406
Arg of perigee: 263
5727 deg
Mean anomaly: 96
5150 deg
Mean motion: 15
50475580 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2982
Checksum: 323
Coasting Arc #10 (Orbit 2997)
---------------------------------------
Vector Time (GMT): 2014/288/09:21:35
242
Vector Time (MET): N/A
Weight (LBS) : 946181
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5752834
96 A = 6796239
97 meter
Y = 2202516
43 meter E =
0010756
Z = 2858981
37 I = 51
40094
XDOT = 307
617185 Wp = 101
29437
YDOT = 5762
111777 meter/sec RA = 222
69538 deg
ZDOT = -5043
928634 TA = 46
11265
MA = 46
02387
Ha = 225
634 n
mi
Hp = 221
215
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18874130
45 X = 5713890
18
Y = 7226103
77 feet Y = 2266630
81 meter
Z = 9379860
15 Z = 2886833
39
XDOT = 1009
242732 XDOT = 267
663110
YDOT = 18904
566196 feet/sec YDOT = 5765
327988 meter/sec
ZDOT = -16548
322289 ZDOT = -5042
531722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15965902
60 X = -4866407
11
Y = -12300765
59 feet Y = -3749273
35 meter
Z = 9498014
13 Z = 2894994
71
XDOT = 3436
204119 XDOT = 1047
355016
YDOT = -17269
192592 feet/sec YDOT = -5263
649902 meter/sec
ZDOT = -16543
268976 ZDOT = -5042
388384
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 14288
42813934
00016717 00000-0 10270-3 0 9093
2 25544 51
6418 223
5670 0002556 269
0905 90
9953 15
50541243 29984
Satellite: ISS
Catalog Number: 25544
Epoch time: 14288
42813934 = yrday
fracday
Element set: 909
Inclination: 51
6418 deg
RA of node: 223
5670 deg
Eccentricity:
0002556
Arg of perigee: 269
0905 deg
Mean anomaly: 90
9953 deg
Mean motion: 15
50541243 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2998
Checksum: 331
Coasting Arc #11 (Orbit 3012)
---------------------------------------
Vector Time (GMT): 2014/289/09:21:35
242
Vector Time (MET): N/A
Weight (LBS) : 946181
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5966076
34 A = 6797190
07 meter
Y = -2181988
65 meter E =
0004039
Z = -2413093
10 I = 51
42776
XDOT = -146
450974 Wp = 23
71290
YDOT = -5493
349124 meter/sec RA = 217
72325 deg
ZDOT = 5336
070569 TA = 309
27360
MA = 309
30942
Ha = 225
683 n
mi
Hp = 221
126
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19573741
28 X = -5929511
28
Y = -7158755
40 feet Y = -2248500
93 meter
Z = -7916972
13 Z = -2441986
75
XDOT = -480
482198 XDOT = -110
933364
YDOT = -18022
798962 feet/sec YDOT = -5494
787798 meter/sec
ZDOT = 17506
793206 ZDOT = 5335
445853
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16875949
16 X = 5143789
30
Y = 12150108
57 feet Y = 3703353
09 meter
Z = -8039575
62 Z = -2450462
65
XDOT = -3395
528271 XDOT = -1034
957017
YDOT = 16284
644298 feet/sec YDOT = 4963
559582 meter/sec
ZDOT = 17504
976709 ZDOT = 5335
516901
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 14289
39489787
00016717 00000-0 10270-3 0 9107
2 25544 51
6417 218
7736 0002446 271
4669 88
6202 15
50558130 30137
Satellite: ISS
Catalog Number: 25544
Epoch time: 14289
39489787 = yrday
fracday
Element set: 910
Inclination: 51
6417 deg
RA of node: 218
7736 deg
Eccentricity:
0002446
Arg of perigee: 271
4669 deg
Mean anomaly: 88
6202 deg
Mean motion: 15
50558130 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3013
Checksum: 328
Coasting Arc #12 (Orbit 3028)
---------------------------------------
Vector Time (GMT): 2014/290/09:21:35
242
Vector Time (MET): N/A
Weight (LBS) : 946181
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6153592
85 A = 6797982
17 meter
Y = 2150661
18 meter E =
0011451
Z = 1908544
21 I = 51
45660
XDOT = -90
173939 Wp = 116
37796
YDOT = 5239
481386 meter/sec RA = 212
75307 deg
ZDOT = -5592
307344 TA = 42
56741
MA = 42
47869
Ha = 225
564 n
mi
Hp = 221
110
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20188952
93 X = 6119815
12
Y = 7055975
00 feet Y = 2219285
96 meter
Z = 6261627
97 Z = 1938355
54
XDOT = -295
846257 XDOT = -121
590424
YDOT = 17189
899559 feet/sec YDOT = 5238
296813 meter/sec
ZDOT = -18347
465041 ZDOT = -5592
822206
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17713795
54 X = -5399164
88
Y = -11916438
53 feet Y = -3632130
46 meter
Z = 6388155
36 Z = 1947109
75
XDOT = 3646
298477 XDOT = 1111
391776
YDOT = -15293
915307 feet/sec YDOT = -4661
585386 meter/sec
ZDOT = -18350
452403 ZDOT = -5593
217892
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 14290
42608182
00016717 00000-0 10270-3 0 9116
2 25544 51
6422 213
6597 0002588 276
6289 83
4567 15
50608497 30290
Satellite: ISS
Catalog Number: 25544
Epoch time: 14290
42608182 = yrday
fracday
Element set: 911
Inclination: 51
6422 deg
RA of node: 213
6597 deg
Eccentricity:
0002588
Arg of perigee: 276
6289 deg
Mean anomaly: 83
4567 deg
Mean motion: 15
50608497 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3029
Checksum: 330
Coasting Arc #13 (Orbit 3043)
---------------------------------------
Vector Time (GMT): 2014/291/09:21:35
242
Vector Time (MET): N/A
Weight (LBS) : 946181
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6318017
26 A = 6798610
57 meter
Y = -2073133
59 meter E =
0007579
Z = -1396185
23 I = 51
48585
XDOT = 369
068387 Wp = 20
96244
YDOT = -5009
667391 meter/sec RA = 207
78562 deg
ZDOT = 5785
199768 TA = 323
81191
MA = 323
86316
Ha = 225
530 n
mi
Hp = 221
052
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20728403
07 X = -6287583
13
Y = -6801619
40 feet Y = -2143615
74 meter
Z = -4580660
19 Z = -1426803
46
XDOT = 1210
854289 XDOT = 396
957259
YDOT = -16435
916637 feet/sec YDOT = -5005
383686 meter/sec
ZDOT = 18980
314201 ZDOT = 5787
060938
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18510697
76 X = 5642060
68
Y = 11492390
72 feet Y = 3502880
69 meter
Z = -4710646
67 Z = -1435805
10
XDOT = -4098
697489 XDOT = -1249
282995
YDOT = 14363
380536 feet/sec YDOT = 4377
958387 meter/sec
ZDOT = 18988
990894 ZDOT = 5787
844425
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 14291
39279351
00016717 00000-0 10270-3 0 9126
2 25544 51
6422 208
8660 0002546 278
9059 81
1804 15
50641621 30443
Satellite: ISS
Catalog Number: 25544
Epoch time: 14291
39279351 = yrday
fracday
Element set: 912
Inclination: 51
6422 deg
RA of node: 208
8660 deg
Eccentricity:
0002546
Arg of perigee: 278
9059 deg
Mean anomaly: 81
1804 deg
Mean motion: 15
50641621 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3044
Checksum: 303
Coasting Arc #14 (Orbit 3059)
---------------------------------------
Vector Time (GMT): 2014/292/09:21:35
242
Vector Time (MET): N/A
Weight (LBS) : 946181
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6440911
51 A = 6799065
65 meter
Y = 1993101
48 meter E =
0010993
Z = 831458
35 I = 51
51676
XDOT = -717
267611 Wp = 131
27372
YDOT = 4807
673816 meter/sec RA = 202
82039 deg
ZDOT = -5924
260771 TA = 39
73086
MA = 39
65039
Ha = 225
507 n
mi
Hp = 221
010
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21131599
46 X = 6414106
47
Y = 6539046
85 feet Y = 2064978
15 meter
Z = 2727881
74 Z = 862682
47
XDOT = -2353
240195 XDOT = -742
196284
YDOT = 15773
208059 feet/sec YDOT = 4799
512806 meter/sec
ZDOT = -19436
551086 ZDOT = -5927
806301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19167998
46 X = -5842405
93
Y = -11006839
06 feet Y = -3354884
55 meter
Z = 2860471
48 Z = 871871
71
XDOT = 4829
659815 XDOT = 1472
080312
YDOT = -13501
718666 feet/sec YDOT = -4115
323849 meter/sec
ZDOT = -19452
362435 ZDOT = -5929
080070
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 14292
42392824
00016717 00000-0 10270-3 0 9133
2 25544 51
6433 203
7521 0002643 283
3596 76
7260 15
50675350 30609
Satellite: ISS
Catalog Number: 25544
Epoch time: 14292
42392824 = yrday
fracday
Element set: 913
Inclination: 51
6433 deg
RA of node: 203
7521 deg
Eccentricity:
0002643
Arg of perigee: 283
3596 deg
Mean anomaly: 76
7260 deg
Mean motion: 15
50675350 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3060
Checksum: 296
Coasting Arc #15 (Orbit 3074)
---------------------------------------
Vector Time (GMT): 2014/293/09:21:35
242
Vector Time (MET): N/A
Weight (LBS) : 946181
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6523387
83 A = 6799217
37 meter
Y = -1876282
75 meter E =
0010515
Z = -270141
03 I = 51
54674
XDOT = 1093
356924 Wp = 30
27943
YDOT = -4648
347217 meter/sec RA = 197
85755 deg
ZDOT = 5993
766057 TA = 326
80987
MA = 326
87579
Ha = 225
425 n
mi
Hp = 220
979
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21402191
05 X = -6500609
69
Y = -6155783
31 feet Y = -1949104
17 meter
Z = -886289
48 Z = -301775
69
XDOT = 3587
129015 XDOT = 1116
138296
YDOT = -15250
482994 feet/sec YDOT = -4635
992494 meter/sec
ZDOT = 19664
586801 ZDOT = 5999
133409
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19708422
38 X = 6007127
14
Y = 10357089
74 feet Y = 3156840
95 meter
Z = -1020655
81 Z = -311095
89
XDOT = -5721
106332 XDOT = -1743
793210
YDOT = 12795
728934 feet/sec YDOT = 3900
138179 meter/sec
ZDOT = 19688
127015 ZDOT = 6000
941114
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 14293
39059343
00016717 00000-0 10270-3 0 9147
2 25544 51
6432 198
9582 0002678 286
3097 73
7759 15
50718606 30755
Satellite: ISS
Catalog Number: 25544
Epoch time: 14293
39059343 = yrday
fracday
Element set: 914
Inclination: 51
6432 deg
RA of node: 198
9582 deg
Eccentricity:
0002678
Arg of perigee: 286
3097 deg
Mean anomaly: 73
7759 deg
Mean motion: 15
50718606 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3075
Checksum: 346
Coasting Arc #16 (Orbit 3090)
---------------------------------------
Vector Time (GMT): 2014/294/09:21:35
242
Vector Time (MET): N/A
Weight (LBS) : 946181
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6551107
00 A = 6799137
93 meter
Y = 1770522
28 meter E =
0009134
Z = -332407
75 I = 51
57781
XDOT = -1522
922576 Wp = 145
00247
YDOT = 4526
831123 meter/sec RA = 192
89686 deg
ZDOT = -5991
452790 TA = 38
57784
MA = 38
51260
Ha = 225
449 n
mi
Hp = 220
909
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21493133
21 X = 6532436
47
Y = 5808800
13 feet Y = 1843676
57 meter
Z = -1090576
61 Z = -300628
34
XDOT = -4996
465143 XDOT = -1544
324340
YDOT = 14851
808146 feet/sec YDOT = 4509
680430 meter/sec
ZDOT = -19656
997342 ZDOT = -5998
903606
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20049642
96 X = -6111131
17
Y = -9694586
10 feet Y = -2954909
84 meter
Z = -955567
31 Z = -291256
92
XDOT = 6834
622900 XDOT = 2083
193060
YDOT = -12227
047875 feet/sec YDOT = -3726
804192 meter/sec
ZDOT = -19689
388678 ZDOT = -6001
325669
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 14294
42167909
00016717 00000-0 10270-3 0 9151
2 25544 51
6443 193
8444 0002724 290
2389 69
8469 15
50747498 30911
Satellite: ISS
Catalog Number: 25544
Epoch time: 14294
42167909 = yrday
fracday
Element set: 915
Inclination: 51
6443 deg
RA of node: 193
8444 deg
Eccentricity:
0002724
Arg of perigee: 290
2389 deg
Mean anomaly: 69
8469 deg
Mean motion: 15
50747498 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3091
Checksum: 346
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