[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
October 14th 2014
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) : 130 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 252 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
294/15:33:44
000 0
0 0
0 0
0
N/A 0
0 0
0 225
6
000/00:00:00
000 0
0 0
0 221
1
300/05:39:30
000 0
0 0
0 0
0
N/A 0
0 0
0 225
7
000/00:00:00
000 0
0 0
0 220
7
Coasting Arc #1 (Orbit 2968)
---------------------------------------
Vector Time (GMT): 2014/286/13:16:35
919
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5335988
16 A = 6796628
76 meter
Y = -3080170
33 meter E =
0002291
Z = -2868592
69 I = 51
36532
XDOT = 608
404369 Wp = 43
30620
YDOT = -5738
991207 meter/sec RA = 231
84299 deg
ZDOT = 5034
594403 TA = 283
98685
MA = 284
01232
Ha = 225
893 n
mi
Hp = 221
413
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17506522
84 X = -5287213
48
Y = -10105545
70 feet Y = -3139568
27 meter
Z = -9411393
34 Z = -2894395
90
XDOT = 1996
077326 XDOT = 648
077058
YDOT = -18828
711309 feet/sec YDOT = -5731
965494 meter/sec
ZDOT = 16517
698173 ZDOT = 5037
646718
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19840189
20 X = 6047289
67
Y = -3591445
47 feet Y = -1094672
58 meter
Z = -9520668
68 Z = -2901899
81
XDOT = 10484
105997 XDOT = 3195
555508
YDOT = 14127
871685 feet/sec YDOT = 4306
175290 meter/sec
ZDOT = 16531
579498 ZDOT = 5038
825431
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
55910675
00016717 00000-0 10270-3 0 9006
2 25544 51
6446 232
8409 0002607 263
3333 96
7521 15
50401707 29690
Satellite: ISS
Catalog Number: 25544
Epoch time: 14286
55910675 = yrday
fracday
Element set: 900
Inclination: 51
6446 deg
RA of node: 232
8409 deg
Eccentricity:
0002607
Arg of perigee: 263
3333 deg
Mean anomaly: 96
7521 deg
Mean motion: 15
50401707 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2969
Checksum: 310
Coasting Arc #2 (Orbit 2984)
---------------------------------------
Vector Time (GMT): 2014/287/13:16:35
919
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5545301
80 A = 6797503
05 meter
Y = 3072075
23 meter E =
0011301
Z = 2437558
67 I = 51
38897
XDOT = -689
005340 Wp = 109
60480
YDOT = 5475
948207 meter/sec RA = 226
86908 deg
ZDOT = -5317
474459 TA = 43
05362
MA = 42
96526
Ha = 225
814 n
mi
Hp = 221
379
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18193247
39 X = 5498695
98
Y = 10078986
97 feet Y = 3133825
96 meter
Z = 7997239
72 Z = 2464383
90
XDOT = -2260
516207 XDOT = -724
356538
YDOT = 17965
709342 feet/sec YDOT = 5468
045293 meter/sec
ZDOT = -17445
782346 ZDOT = -5320
907820
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20280225
29 X = -6181412
67
Y = 4411596
79 feet Y = 1344654
70 meter
Z = 8110878
36 Z = 2472195
73
XDOT = -9926
480159 XDOT = -3025
591153
YDOT = -13431
271090 feet/sec YDOT = -4093
851428 meter/sec
ZDOT = -17461
238961 ZDOT = -5322
185635
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
59039997
00016717 00000-0 10270-3 0 9011
2 25544 51
6450 227
7285 0002563 266
3482 93
7376 15
50437027 29856
Satellite: ISS
Catalog Number: 25544
Epoch time: 14287
59039997 = yrday
fracday
Element set: 901
Inclination: 51
6450 deg
RA of node: 227
7285 deg
Eccentricity:
0002563
Arg of perigee: 266
3482 deg
Mean anomaly: 93
7376 deg
Mean motion: 15
50437027 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2985
Checksum: 341
Coasting Arc #3 (Orbit 2999)
---------------------------------------
Vector Time (GMT): 2014/288/13:16:35
919
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5751598
46 A = 6798247
17 meter
Y = -3016560
30 meter E =
0005332
Z = -1999597
67 I = 51
41359
XDOT = 811
607396 Wp = 18
79769
YDOT = -5219
159266 meter/sec RA = 221
89670 deg
ZDOT = 5548
136167 TA = 319
08884
MA = 319
12884
Ha = 225
767 n
mi
Hp = 221
352
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18870073
68 X = -5707725
60
Y = -9896851
38 feet Y = -3080633
24 meter
Z = -6560359
81 Z = -2027431
64
XDOT = 2662
753924 XDOT = 842
957567
YDOT = -17123
225939 feet/sec YDOT = -5209
907645 meter/sec
ZDOT = 18202
546481 ZDOT = 5552
155420
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20585819
95 X = 6274557
92
Y = -5356287
01 feet Y = -1632596
28 meter
Z = -6678313
80 Z = -2035550
05
XDOT = 9251
447117 XDOT = 2819
841081
YDOT = 12875
024946 feet/sec YDOT = 3924
307603 meter/sec
ZDOT = 18220
451192 ZDOT = 5553
593523
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
55721858
00016717 00000-0 10270-3 0 9023
2 25544 51
6448 222
9353 0002621 270
4305 89
6546 15
50465025 30002
Satellite: ISS
Catalog Number: 25544
Epoch time: 14288
55721858 = yrday
fracday
Element set: 902
Inclination: 51
6448 deg
RA of node: 222
9353 deg
Eccentricity:
0002621
Arg of perigee: 270
4305 deg
Mean anomaly: 89
6546 deg
Mean motion: 15
50465025 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3000
Checksum: 299
Coasting Arc #4 (Orbit 3015)
---------------------------------------
Vector Time (GMT): 2014/289/13:16:35
919
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5929562
93 A = 6798930
77 meter
Y = 2949742
36 meter E =
0011588
Z = 1510900
07 I = 51
44022
XDOT = -1003
828509 Wp = 123
36109
YDOT = 4973
121567 meter/sec RA = 216
92670 deg
ZDOT = -5743
815499 TA = 40
11329
MA = 40
02779
Ha = 225
764 n
mi
Hp = 221
307
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19453946
62 X = 5888797
99
Y = 9677632
42 feet Y = 3015822
77 meter
Z = 4957021
24 Z = 1539606
07
XDOT = -3293
400619 XDOT = -1031
462610
YDOT = 16316
015639 feet/sec YDOT = 4961
741105 meter/sec
ZDOT = -18844
539038 ZDOT = -5748
759550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20772476
04 X = -6331450
70
Y = 6276591
46 feet Y = 1913105
08 meter
Z = 5078711
15 Z = 1547991
16
XDOT = -8420
553477 XDOT = -2566
584700
YDOT = -12535
639949 feet/sec YDOT = -3820
863057 meter/sec
ZDOT = -18866
336380 ZDOT = -5750
459329
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
58847254
00016717 00000-0 10270-3 0 9037
2 25544 51
6452 217
8224 0002574 272
7081 87
3775 15
50485257 30165
Satellite: ISS
Catalog Number: 25544
Epoch time: 14289
58847254 = yrday
fracday
Element set: 903
Inclination: 51
6452 deg
RA of node: 217
8224 deg
Eccentricity:
0002574
Arg of perigee: 272
7081 deg
Mean anomaly: 87
3775 deg
Mean motion: 15
50485257 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3016
Checksum: 326
Coasting Arc #5 (Orbit 3030)
---------------------------------------
Vector Time (GMT): 2014/290/13:16:35
919
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6088189
47 A = 6799339
34 meter
Y = -2837787
92 meter E =
0008516
Z = -1023193
52 I = 51
46777
XDOT = 1231
015819 Wp = 23
26269
YDOT = -4753
057423 meter/sec RA = 211
95838 deg
ZDOT = 5882
090739 TA = 325
63818
MA = 325
69323
Ha = 225
670 n
mi
Hp = 221
286
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19974374
91 X = -6051033
78
Y = -9310327
81 feet Y = -2905662
35 meter
Z = -3356934
12 Z = -1052678
86
XDOT = 4038
765812 XDOT = 1255
500516
YDOT = -15594
020418 feet/sec YDOT = -4739
153938 meter/sec
ZDOT = 19298
197963 ZDOT = 5888
130831
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20784650
18 X = 6335161
37
Y = -7266433
13 feet Y = -2214808
82 meter
Z = -3481972
21 Z = -1061305
13
XDOT = 7553
072295 XDOT = 2302
176435
YDOT = 12381
498126 feet/sec YDOT = 3773
880629 meter/sec
ZDOT = 19324
622048 ZDOT = 5890
144800
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
55525375
00016717 00000-0 10270-3 0 9044
2 25544 51
6454 213
0289 0002659 277
8643 82
2206 15
50527335 30314
Satellite: ISS
Catalog Number: 25544
Epoch time: 14290
55525375 = yrday
fracday
Element set: 904
Inclination: 51
6454 deg
RA of node: 213
0289 deg
Eccentricity:
0002659
Arg of perigee: 277
8643 deg
Mean anomaly: 82
2206 deg
Mean motion: 15
50527335 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3031
Checksum: 302
Coasting Arc #6 (Orbit 3046)
---------------------------------------
Vector Time (GMT): 2014/291/13:16:35
919
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6205161
89 A = 6799685
18 meter
Y = 2722527
76 meter E =
0010785
Z = 490762
35 I = 51
49632
XDOT = -1521
127449 Wp = 136
77907
YDOT = 4555
898878 meter/sec RA = 206
99261 deg
ZDOT = -5970
786695 TA = 37
92464
MA = 37
84873
Ha = 225
718 n
mi
Hp = 221
250
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20358142
70 X = 6171872
78
Y = 8932177
69 feet Y = 2791731
82 meter
Z = 1610112
69 Z = 520825
35
XDOT = -4990
575620 XDOT = -1542
955012
YDOT = 14947
174796 feet/sec YDOT = 4538
765964 meter/sec
ZDOT = -19589
195194 ZDOT = -5978
229706
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20665644
95 X = -6298888
58
Y = 8169575
26 feet Y = 2490086
54 meter
Z = 1737640
41 Z = 529632
80
XDOT = -6596
967731 XDOT = -2010
755764
YDOT = -12468
729399 feet/sec YDOT = -3800
468721 meter/sec
ZDOT = -19621
557278 ZDOT = -5980
650658
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
58646844
00016717 00000-0 10270-3 0 9054
2 25544 51
6458 207
9158 0002626 278
8934 81
1920 15
50532288 30474
Satellite: ISS
Catalog Number: 25544
Epoch time: 14291
58646844 = yrday
fracday
Element set: 905
Inclination: 51
6458 deg
RA of node: 207
9158 deg
Eccentricity:
0002626
Arg of perigee: 278
8934 deg
Mean anomaly: 81
1920 deg
Mean motion: 15
50532288 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3047
Checksum: 332
Coasting Arc #7 (Orbit 3061)
---------------------------------------
Vector Time (GMT): 2014/292/13:16:35
919
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6288083
36 A = 6799637
85 meter
Y = -2570846
12 meter E =
0010958
Z = 31113
54 I = 51
52533
XDOT = 1834
070302 Wp = 33
45005
YDOT = -4401
268543 meter/sec RA = 202
02837 deg
ZDOT = 5999
469301 TA = 326
88514
MA = 326
95369
Ha = 225
610 n
mi
Hp = 221
215
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20630194
74 X = -6259019
35
Y = -8434534
51 feet Y = -2641001
03 meter
Z = 102078
56 Z = 637
40
XDOT = 6017
291016 XDOT = 1854
006096
YDOT = -14439
857423 feet/sec YDOT = -4380
646621 meter/sec
ZDOT = 19683
298230 ZDOT = 6008
428007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20357999
44 X = 6205118
23
Y = -9072367
04 feet Y = -2765257
48 meter
Z = -27243
09 Z = -8303
69
XDOT = 5694
479807 XDOT = 1735
677445
YDOT = 12755
887488 feet/sec YDOT = 3887
994506 meter/sec
ZDOT = 19722
086885 ZDOT = 6011
292082
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
55321238
00016717 00000-0 10270-3 0 9060
2 25544 51
6462 203
1220 0002741 285
5732 74
5116 15
50588666 30627
Satellite: ISS
Catalog Number: 25544
Epoch time: 14292
55321238 = yrday
fracday
Element set: 906
Inclination: 51
6462 deg
RA of node: 203
1220 deg
Eccentricity:
0002741
Arg of perigee: 285
5732 deg
Mean anomaly: 74
5116 deg
Mean motion: 15
50588666 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3062
Checksum: 291
Coasting Arc #8 (Orbit 3077)
---------------------------------------
Vector Time (GMT): 2014/293/13:16:35
919
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6318821
26 A = 6799525
51 meter
Y = 2428171
54 meter E =
0008735
Z = -587947
33 I = 51
55450
XDOT = -2195
025854 Wp = 149
14819
YDOT = 4279
238150 meter/sec RA = 197
06673 deg
ZDOT = -5964
351323 TA = 37
19488
MA = 37
13440
Ha = 225
659 n
mi
Hp = 221
207
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20731040
88 X = 6294055
36
Y = 7966442
07 feet Y = 2498694
15 meter
Z = -1928961
07 Z = -557311
33
XDOT = -7201
528392 XDOT = -2213
740758
YDOT = 14039
495244 feet/sec YDOT = 4254
586589 meter/sec
ZDOT = -19568
081769 ZDOT = -5975
060599
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19931409
94 X = -6075093
75
Y = 9821604
18 feet Y = 2993624
95 meter
Z = -1798926
06 Z = -548312
66
XDOT = -4785
449087 XDOT = -1458
604882
YDOT = -13273
770132 feet/sec YDOT = -4045
845136 meter/sec
ZDOT = -19614
303976 ZDOT = -5978
439852
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
58438785
00016717 00000-0 10270-3 0 9071
2 25544 51
6465 198
0090 0002743 285
4386 74
6461 15
50583343 30781
Satellite: ISS
Catalog Number: 25544
Epoch time: 14293
58438785 = yrday
fracday
Element set: 907
Inclination: 51
6465 deg
RA of node: 198
0090 deg
Eccentricity:
0002743
Arg of perigee: 285
4386 deg
Mean anomaly: 74
6461 deg
Mean motion: 15
50583343 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3078
Checksum: 336
Coasting Arc #9 (Orbit 3093)
---------------------------------------
Vector Time (GMT): 2014/294/13:16:35
919
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6304526
18 A = 6798968
50 meter
Y = -2263413
22 meter E =
0012238
Z = 1123344
84 I = 51
58335
XDOT = 2563
084418 Wp = 46
01820
YDOT = -4210
696434 meter/sec RA = 192
10602 deg
ZDOT = 5869
126040 TA = 326
16798
MA = 326
24600
Ha = 225
590 n
mi
Hp = 221
133
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20684141
01 X = -6284204
56
Y = -7425896
40 feet Y = -2333800
76 meter
Z = 3685514
55 Z = 1092767
36
XDOT = 8409
069614 XDOT = 2581
468003
YDOT = -13814
620846 feet/sec YDOT = -4181
930871 meter/sec
ZDOT = 19255
662860 ZDOT = 5881
622549
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19332399
11 X = 5892515
25
Y = -10496477
18 feet Y = -3199326
24 meter
Z = 3555693
38 Z = 1083775
34
XDOT = 4015
331104 XDOT = 1223
872921
YDOT = 13972
879009 feet/sec YDOT = 4258
933522 meter/sec
ZDOT = 19309
485377 ZDOT = 5885
531143
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
61554165
00016717 00000-0 10270-3 0 9088
2 25544 51
6465 192
8953 0002867 293
3312 66
7537 15
50649472 30945
Satellite: ISS
Catalog Number: 25544
Epoch time: 14294
61554165 = yrday
fracday
Element set: 908
Inclination: 51
6465 deg
RA of node: 192
8953 deg
Eccentricity:
0002867
Arg of perigee: 293
3312 deg
Mean anomaly: 66
7537 deg
Mean motion: 15
50649472 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3094
Checksum: 337
Coasting Arc #10 (Orbit 3094)
---------------------------------------
Vector Time (GMT): 2014/294/15:33:44
000
Vector Time (MET): N/A
Weight (LBS) : 929923
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6572867
27 A = 6799444
34 meter
Y = 1675272
78 meter E =
0008824
Z = -398888
63 I = 51
58581
XDOT = -1514
925139 Wp = 146
18930
YDOT = 4535
197005 meter/sec RA = 191
62605 deg
ZDOT = -5986
737176 TA = 38
10753
MA = 38
04516
Ha = 225
584 n
mi
Hp = 221
143
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21564525
15 X = 6555583
18
Y = 5496301
77 feet Y = 1748678
15 meter
Z = -1308689
74 Z = -367000
11
XDOT = -4970
226834 XDOT = -1536
443928
YDOT = 14879
255267 feet/sec YDOT = 4518
135097 meter/sec
ZDOT = -19641
526168 ZDOT = -5994
149428
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8226976
94 X = -2507582
57
Y = 20685531
22 feet Y = 6304949
91 meter
Z = -1173198
99 Z = -357591
05
XDOT = -12621
651399 XDOT = -3847
079346
YDOT = -6120
911470 feet/sec YDOT = -1865
653816 meter/sec
ZDOT = -19673
755238 ZDOT = -5996
560597
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
67998749
00016717 00000-0 10270-3 0 9095
2 25544 51
6445 192
5753 0002907 291
2328 68
8512 15
50636185 30951
Satellite: ISS
Catalog Number: 25544
Epoch time: 14294
67998749 = yrday
fracday
Element set: 909
Inclination: 51
6445 deg
RA of node: 192
5753 deg
Eccentricity:
0002907
Arg of perigee: 291
2328 deg
Mean anomaly: 68
8512 deg
Mean motion: 15
50636185 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3095
Checksum: 350
Coasting Arc #11 (Orbit 3110)
---------------------------------------
Vector Time (GMT): 2014/295/15:33:44
000
Vector Time (MET): N/A
Weight (LBS) : 929923
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6551287
31 A = 6799020
27 meter
Y = -1521474
31 meter E =
0012192
Z = 947559
20 I = 51
61453
XDOT = 1903
522283 Wp = 43
22027
YDOT = -4492
174823 meter/sec RA = 186
66661 deg
ZDOT = 5911
282672 TA = 327
03185
MA = 327
10782
Ha = 225
526 n
mi
Hp = 221
101
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21493724
79 X = -6538389
97
Y = -4991713
62 feet Y = -1594662
84 meter
Z = 3108790
03 Z = 915764
72
XDOT = 6245
151847 XDOT = 1924
897554
YDOT = -14738
106375 feet/sec YDOT = -4470
768233 meter/sec
ZDOT = 19393
972021 ZDOT = 5920
582350
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7361714
86 X = 2243850
69
Y = -20821249
99 feet Y = -6346317
00 meter
Z = 2973665
87 Z = 906373
36
XDOT = 12442
532938 XDOT = 3792
484040
YDOT = 7192
684278 feet/sec YDOT = 2192
330168 meter/sec
ZDOT = 19434
233203 ZDOT = 5923
554280
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 14295
71112033
00016717 00000-0 10270-3 0 9107
2 25544 51
6435 187
4605 0002951 294
3827 65
7016 15
50682784 31116
Satellite: ISS
Catalog Number: 25544
Epoch time: 14295
71112033 = yrday
fracday
Element set: 910
Inclination: 51
6435 deg
RA of node: 187
4605 deg
Eccentricity:
0002951
Arg of perigee: 294
3827 deg
Mean anomaly: 65
7016 deg
Mean motion: 15
50682784 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3111
Checksum: 297
Coasting Arc #12 (Orbit 3125)
---------------------------------------
Vector Time (GMT): 2014/296/15:33:44
000
Vector Time (MET): N/A
Weight (LBS) : 929923
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6474550
95 A = 6798362
62 meter
Y = 1396298
01 meter E =
0005754
Z = -1519428
84 I = 51
64320
XDOT = -2316
512659 Wp = 154
69670
YDOT = 4489
759627 meter/sec RA = 181
71045 deg
ZDOT = -5758
295855 TA = 41
87046
MA = 41
82647
Ha = 225
565 n
mi
Hp = 221
016
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21241965
07 X = 6465837
11
Y = 4581030
21 feet Y = 1468651
77 meter
Z = -4985002
74 Z = -1487996
85
XDOT = -7600
107148 XDOT = -2338
573333
YDOT = 14730
182502 feet/sec YDOT = 4463
730984 meter/sec
ZDOT = -18892
046770 ZDOT = -5769
603455
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6570787
13 X = -2002775
92
Y = 20744780
62 feet Y = 6323009
13 meter
Z = -4851391
96 Z = -1478704
27
XDOT = -12442
787382 XDOT = -3792
561594
YDOT = -8360
336616 feet/sec YDOT = -2548
230601 meter/sec
ZDOT = -18940
862355 ZDOT = -5773
174846
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 14296
67778986
00016717 00000-0 10270-3 0 9119
2 25544 51
6430 182
6667 0002959 298
7384 61
3469 15
50708546 31265
Satellite: ISS
Catalog Number: 25544
Epoch time: 14296
67778986 = yrday
fracday
Element set: 911
Inclination: 51
6430 deg
RA of node: 182
6667 deg
Eccentricity:
0002959
Arg of perigee: 298
7384 deg
Mean anomaly: 61
3469 deg
Mean motion: 15
50708546 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3126
Checksum: 358
Coasting Arc #13 (Orbit 3141)
---------------------------------------
Vector Time (GMT): 2014/297/15:33:44
000
Vector Time (MET): N/A
Weight (LBS) : 929923
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6345013
43 A = 6797464
22 meter
Y = -1270586
02 meter E =
0012286
Z = 2059037
40 I = 51
67074
XDOT = 2714
950788 Wp = 58
35440
YDOT = -4544
098777 meter/sec RA = 176
75385 deg
ZDOT = 5544
107832 TA = 324
38422
MA = 324
46615
Ha = 225
561 n
mi
Hp = 220
949
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20816973
21 X = -6340336
29
Y = -4168589
32 feet Y = -1341513
77 meter
Z = 6755372
04 Z = 2028224
82
XDOT = 8907
318857 XDOT = 2738
629926
YDOT = -14908
460556 feet/sec YDOT = -4513
605619 meter/sec
ZDOT = 18189
330157 ZDOT = 5557
354908
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5769596
13 X = 1758572
90
Y = -20474083
07 feet Y = -6240500
52 meter
Z = 6624367
50 Z = 2019107
21
XDOT = 12688
819775 XDOT = 3867
552267
YDOT = 9498
878999 feet/sec YDOT = 2895
258319 meter/sec
ZDOT = 18246
420686 ZDOT = 5561
509025
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 14297
70888396
00016717 00000-0 10270-3 0 9122
2 25544 51
6419 177
5514 0002918 299
8232 60
2628 15
50744954 31421
Satellite: ISS
Catalog Number: 25544
Epoch time: 14297
70888396 = yrday
fracday
Element set: 912
Inclination: 51
6419 deg
RA of node: 177
5514 deg
Eccentricity:
0002918
Arg of perigee: 299
8232 deg
Mean anomaly: 60
2628 deg
Mean motion: 15
50744954 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3142
Checksum: 337
Coasting Arc #14 (Orbit 3156)
---------------------------------------
Vector Time (GMT): 2014/298/15:33:44
000
Vector Time (MET): N/A
Weight (LBS) : 929923
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6162678
90 A = 6796301
52 meter
Y = 1190939
40 meter E =
0002266
Z = -2605395
25 I = 51
69792
XDOT = -3110
919702 Wp = 132
15374
YDOT = 4633
523340 meter/sec RA = 171
79970 deg
ZDOT = -5244
828503 TA = 77
09014
MA = 77
06483
Ha = 225
586 n
mi
Hp = 220
844
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20218762
79 X = 6161560
03
Y = 3907281
50 feet Y = 1259848
07 meter
Z = -8547884
67 Z = -2575459
77
XDOT = -10206
429470 XDOT = -3137
023219
YDOT = 15201
848228 feet/sec YDOT = 4598
588769 meter/sec
ZDOT = -17207
442594 ZDOT = -5260
005002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5120226
86 X = -1560645
15
Y = 20000212
40 feet Y = 6096064
74 meter
Z = -8420589
68 Z = -2566595
74
XDOT = -13106
240775 XDOT = -3994
782188
YDOT = -10621
392684 feet/sec YDOT = -3237
400490 meter/sec
ZDOT = -17272
773978 ZDOT = -5264
741509
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 14298
67551717
00016717 00000-0 10270-3 0 9134
2 25544 51
6415 172
7570 0002904 306
4800 53
6083 15
50778620 31571
Satellite: ISS
Catalog Number: 25544
Epoch time: 14298
67551717 = yrday
fracday
Element set: 913
Inclination: 51
6415 deg
RA of node: 172
7570 deg
Eccentricity:
0002904
Arg of perigee: 306
4800 deg
Mean anomaly: 53
6083 deg
Mean motion: 15
50778620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3157
Checksum: 309
Coasting Arc #15 (Orbit 3172)
---------------------------------------
Vector Time (GMT): 2014/299/15:33:44
000
Vector Time (MET): N/A
Weight (LBS) : 929923
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5930597
49 A = 6795026
00 meter
Y = -1130335
45 meter E =
0011057
Z = 3105396
23 I = 51
72394
XDOT = 3475
551776 Wp = 74
73848
YDOT = -4773
498894 meter/sec RA = 166
84507 deg
ZDOT = 4888
323799 TA = 320
89886
MA = 320
97872
Ha = 225
619 n
mi
Hp = 220
758
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19457340
86 X = -5932602
46
Y = -3708449
65 feet Y = -1196666
32 meter
Z = 10188307
86 Z = 3076580
64
XDOT = 11402
728925 XDOT = 3504
925298
YDOT = -15661
085609 feet/sec YDOT = -4734
468590 meter/sec
ZDOT = 16037
807741 ZDOT = 4905
279527
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4544319
88 X = 1385108
70
Y = -19343525
81 feet Y = -5895906
67 meter
Z = 10065758
55 Z = 3068043
21
XDOT = 13748
201687 XDOT = 4190
451874
YDOT = 11633
529184 feet/sec YDOT = 3545
899695 meter/sec
ZDOT = 16110
751285 ZDOT = 4910
556992
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 14299
70657261
00016717 00000-0 10270-3 0 9141
2 25544 51
6407 167
6415 0002846 305
9576 54
1311 15
50807297 31733
Satellite: ISS
Catalog Number: 25544
Epoch time: 14299
70657261 = yrday
fracday
Element set: 914
Inclination: 51
6407 deg
RA of node: 167
6415 deg
Eccentricity:
0002846
Arg of perigee: 305
9576 deg
Mean anomaly: 54
1311 deg
Mean motion: 15
50807297 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3173
Checksum: 318
Coasting Arc #16 (Orbit 3181)
---------------------------------------
Vector Time (GMT): 2014/300/05:39:30
000
Vector Time (MET): N/A
Weight (LBS) : 915489
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2611940
16 A = 6787640
93 meter
Y = -3509146
95 meter E =
0001546
Z = 5188811
07 I = 51
71852
XDOT = 6875
173132 Wp = 109
78376
YDOT = -3100
609548 meter/sec RA = 163
92573 deg
ZDOT = 1363
063683 TA = 327
11649
MA = 327
12610
Ha = 225
672 n
mi
Hp = 220
660
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8569357
48 X = -2597712
15
Y = -11512949
32 feet Y = -3538275
64 meter
Z = 17023658
37 Z = 5176156
99
XDOT = 22556
342296 XDOT = 6902
712392
YDOT = -10172
603503 feet/sec YDOT = -3023
572884 meter/sec
ZDOT = 4471
993711 ZDOT = 1396
530133
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5734128
28 X = -1747762
30
Y = 13225561
31 feet Y = 4031151
09 meter
Z = 16970301
56 Z = 5172547
91
XDOT = -18995
874637 XDOT = -5789
942589
YDOT = -14161
207411 feet/sec YDOT = -4316
336019 meter/sec
ZDOT = 4615
011457 ZDOT = 1406
655492
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 14300
28653384
00016717 00000-0 10270-3 0 9150
2 25544 51
6419 164
7679 0003025 312
9785 47
1112 15
50823927 31825
Satellite: ISS
Catalog Number: 25544
Epoch time: 14300
28653384 = yrday
fracday
Element set: 915
Inclination: 51
6419 deg
RA of node: 164
7679 deg
Eccentricity:
0003025
Arg of perigee: 312
9785 deg
Mean anomaly: 47
1112 deg
Mean motion: 15
50823927 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3182
Checksum: 309
Coasting Arc #17 (Orbit 3196)
---------------------------------------
Vector Time (GMT): 2014/301/05:39:30
000
Vector Time (MET): N/A
Weight (LBS) : 915489
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2214344
83 A = 6787146
35 meter
Y = 3627780
81 meter E =
0012976
Z = -5302757
99 I = 51
74690
XDOT = -6907
472633 Wp = 74
10642
YDOT = 3226
405805 meter/sec RA = 158
96650 deg
ZDOT = -675
074798 TA = 189
43233
MA = 189
45672
Ha = 225
685 n
mi
Hp = 220
641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7264910
84 X = 2199373
21
Y = 11902168
02 feet Y = 3652459
22 meter
Z = -17397499
97 Z = -5292037
23
XDOT = -22662
311788 XDOT = -6939
758300
YDOT = 10585
320882 feet/sec YDOT = 3148
981436 meter/sec
ZDOT = -2214
812330 ZDOT = -708
709549
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6502593
38 X = 1981990
46
Y = -12398559
03 feet Y = -3779080
79 meter
Z = -17352393
26 Z = -5289009
47
XDOT = 19720
723110 XDOT = 6010
876404
YDOT = 13653
378306 feet/sec YDOT = 4161
549708 meter/sec
ZDOT = -2358
588992 ZDOT = -718
897925
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 14301
25312050
00016717 00000-0 10270-3 0 9161
2 25544 51
6421 159
9723 0003036 317
4101 42
6814 15
50831095 31978
Satellite: ISS
Catalog Number: 25544
Epoch time: 14301
25312050 = yrday
fracday
Element set: 916
Inclination: 51
6421 deg
RA of node: 159
9723 deg
Eccentricity:
0003036
Arg of perigee: 317
4101 deg
Mean anomaly: 42
6814 deg
Mean motion: 15
50831095 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3197
Checksum: 273
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