[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 13th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 37673 69 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
257/02:09:53
050 1
6 1
7 1
7
N/A 0
4 -0
2 227
8
000/00:03:42
101 0
2 -0
0 220
1
263/11:28:05
000 0
0 0
0 0
0
N/A 0
0 0
0 227
2
000/00:00:00
000 0
0 0
0 219
6
Coasting Arc #1 (Orbit 2487)
---------------------------------------
Vector Time (GMT): 2014/255/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912103
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4360480
53 A = 6796794
80 meter
Y = 4478390
65 meter E =
0016699
Z = 2651819
04 I = 51
81995
XDOT = -5242
189505 Wp = 82
07311
YDOT = 1994
577951 meter/sec RA = 26
27601 deg
ZDOT = 5225
575999 TA = 307
71846
MA = 307
86971
Ha = 227
868 n
mi
Hp = 219
088
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14306038
48 X = 4297196
30
Y = 14692882
72 feet Y = 4526798
82 meter
Z = 8700193
72 Z = 2672847
54
XDOT = -17198
784464 XDOT = -5289
488020
YDOT = 6543
890916 feet/sec YDOT = 1935
692514 meter/sec
ZDOT = 17144
278211 ZDOT = 5199
994952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11655841
51 X = -3552700
49
Y = -16826590
72 feet Y = -5128744
85 meter
Z = 8788863
06 Z = 2678845
46
XDOT = 16916
875439 XDOT = 5156
263634
YDOT = -2776
688189 feet/sec YDOT = -846
334560 meter/sec
ZDOT = 17035
071916 ZDOT = 5192
289920
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 14255
55904840
00016717 00000-0 10270-3 0 9009
2 25544 51
6467 26
5361 0003391 100
8321 259
3212 15
50526260 24883
Satellite: ISS
Catalog Number: 25544
Epoch time: 14255
55904840 = yrday
fracday
Element set: 900
Inclination: 51
6467 deg
RA of node: 26
5361 deg
Eccentricity:
0003391
Arg of perigee: 100
8321 deg
Mean anomaly: 259
3212 deg
Mean motion: 15
50526260 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2488
Checksum: 286
Coasting Arc #2 (Orbit 2502)
---------------------------------------
Vector Time (GMT): 2014/256/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912103
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4259141
77 A = 6795610
86 meter
Y = -4290295
99 meter E =
0007878
Z = -3108404
59 I = 51
78781
XDOT = 5547
986456 Wp = 102
25086
YDOT = -1970
247324 meter/sec RA = 21
33057 deg
ZDOT = -4894
592394 TA = 113
33859
MA = 113
25569
Ha = 227
829 n
mi
Hp = 219
046
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13973562
25 X = -4195750
43
Y = -14075774
24 feet Y = -4337570
32 meter
Z = -10198177
79 Z = -3128940
62
XDOT = 18202
055301 XDOT = 5593
382356
YDOT = -6464
066024 feet/sec YDOT = -1907
952790 meter/sec
ZDOT = -16058
373995 ZDOT = -4867
530472
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11695769
34 X = 3564870
50
Y = 15963177
92 feet Y = 4865576
63 meter
Z = -10284776
26 Z = -3134799
81
XDOT = -17888
711753 XDOT = -5452
479342
YDOT = 2860
250621 feet/sec YDOT = 871
804389 meter/sec
ZDOT = -15942
873903 ZDOT = -4859
387966
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 14256
52582343
00016717 00000-0 10270-3 0 9018
2 25544 51
6466 21
7430 0003357 101
1325 259
0204 15
50547335 25038
Satellite: ISS
Catalog Number: 25544
Epoch time: 14256
52582343 = yrday
fracday
Element set: 901
Inclination: 51
6466 deg
RA of node: 21
7430 deg
Eccentricity:
0003357
Arg of perigee: 101
1325 deg
Mean anomaly: 259
0204 deg
Mean motion: 15
50547335 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2503
Checksum: 270
Coasting Arc #3 (Orbit 2511)
---------------------------------------
Vector Time (GMT): 2014/257/02:11:44
101
Vector Time (MET): N/A
Weight (LBS) : 911938
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2355362
76 A = 6788944
12 meter
Y = -3595329
45 meter E =
0016269
Z = -5269302
45 I = 51
74655
XDOT = 6921
876494 Wp = 96
57987
YDOT = 3108
328598 meter/sec RA = 18
37439 deg
ZDOT = 973
966863 TA = 182
74609
MA = 182
75503
Ha = 227
789 n
mi
Hp = 220
072
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7727568
11 X = 2420988
20
Y = -11795700
30 feet Y = -3568623
78 meter
Z = -17287737
70 Z = -5257700
67
XDOT = 22709
568550 XDOT = 6881
872755
YDOT = 10197
928471 feet/sec YDOT = 3185
509908 meter/sec
ZDOT = 3195
429341 ZDOT = 1007
495076
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2094631
49 X = 638443
68
Y = -14006898
48 feet Y = -4269302
66 meter
Z = -17237721
51 Z = -5254057
52
XDOT = 23851
196343 XDOT = 7269
844645
YDOT = -537
448503 feet/sec YDOT = -163
814304 meter/sec
ZDOT = 3337
515812 ZDOT = 1017
274820
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 14257
10587211
00016717 00000-0 10270-3 0 9023
2 25544 51
6477 18
8708 0001972 91
1658 268
9719 15
50274647 25126
Satellite: ISS
Catalog Number: 25544
Epoch time: 14257
10587211 = yrday
fracday
Element set: 902
Inclination: 51
6477 deg
RA of node: 18
8708 deg
Eccentricity:
0001972
Arg of perigee: 91
1658 deg
Mean anomaly: 268
9719 deg
Mean motion: 15
50274647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2512
Checksum: 323
Coasting Arc #4 (Orbit 2527)
---------------------------------------
Vector Time (GMT): 2014/258/02:11:44
101
Vector Time (MET): N/A
Weight (LBS) : 911938
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2557690
06 A = 6789093
99 meter
Y = 3580971
57 meter E =
0006310
Z = 5165464
55 I = 51
71769
XDOT = -6963
113870 Wp = 64
24738
YDOT = -2851
759357 meter/sec RA = 13
42167 deg
ZDOT = -1466
737596 TA = 39
88318
MA = 39
83684
Ha = 227
689 n
mi
Hp = 219
926
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8391371
60 X = -2622635
45
Y = 11748594
38 feet Y = 3552007
09 meter
Z = 16947062
16 Z = 5152881
59
XDOT = -22844
861777 XDOT = -6923
582363
YDOT = -9356
165871 feet/sec YDOT = -2929
404481 meter/sec
ZDOT = -4812
131220 ZDOT = -1500
467266
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2468409
38 X = -752371
18
Y = 14289342
31 feet Y = 4355391
54 meter
Z = 16892872
90 Z = 5148947
66
XDOT = -23562
748612 XDOT = -7181
925777
YDOT = 1803
445135 feet/sec YDOT = 549
690077 meter/sec
ZDOT = -4955
114234 ZDOT = -1510
318819
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 14258
13724731
00016717 00000-0 10270-3 0 9038
2 25544 51
6474 13
7593 0001838 90
6405 269
4956 15
50360189 25287
Satellite: ISS
Catalog Number: 25544
Epoch time: 14258
13724731 = yrday
fracday
Element set: 903
Inclination: 51
6474 deg
RA of node: 13
7593 deg
Eccentricity:
0001838
Arg of perigee: 90
6405 deg
Mean anomaly: 269
4956 deg
Mean motion: 15
50360189 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2528
Checksum: 319
Coasting Arc #5 (Orbit 2542)
---------------------------------------
Vector Time (GMT): 2014/259/02:11:44
101
Vector Time (MET): N/A
Weight (LBS) : 911938
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2778429
65 A = 6789598
44 meter
Y = -3615353
20 meter E =
0014609
Z = -5044021
49 I = 51
68962
XDOT = 6926
386608 Wp = 102
64817
YDOT = 2594
439964 meter/sec RA = 8
46617 deg
ZDOT = 1957
388045 TA = 186
37139
MA = 186
38999
Ha = 227
584 n
mi
Hp = 219
934
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9115582
84 X = 2843153
10
Y = -11861395
01 feet Y = -3583921
50 meter
Z = -16548626
92 Z = -5030366
78
XDOT = 22724
365513 XDOT = 6887
351832
YDOT = 8511
942138 feet/sec YDOT = 2671
677191 meter/sec
ZDOT = 6421
876787 ZDOT = 1990
940448
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2813635
19 X = 857596
01
Y = -14758427
52 feet Y = -4498368
71 meter
Z = -16489871
71 Z = -5026112
90
XDOT = 22996
645816 XDOT = 7009
377645
YDOT = -2943
867418 feet/sec YDOT = -897
290789 meter/sec
ZDOT = 6564
146924 ZDOT = 2000
751982
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 14259
10412889
00016717 00000-0 10270-3 0 9045
2 25544 51
6480 8
9665 0001887 91
3465 268
7902 15
50386387 25436
Satellite: ISS
Catalog Number: 25544
Epoch time: 14259
10412889 = yrday
fracday
Element set: 904
Inclination: 51
6480 deg
RA of node: 8
9665 deg
Eccentricity:
0001887
Arg of perigee: 91
3465 deg
Mean anomaly: 268
7902 deg
Mean motion: 15
50386387 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2543
Checksum: 335
Coasting Arc #6 (Orbit 2558)
---------------------------------------
Vector Time (GMT): 2014/260/02:11:44
101
Vector Time (MET): N/A
Weight (LBS) : 911938
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3018891
51 A = 6790100
34 meter
Y = 3659620
95 meter E =
0008797
Z = 4852346
88 I = 51
66100
XDOT = -6858
281062 Wp = 65
66395
YDOT = -2375
937391 meter/sec RA = 3
50873 deg
ZDOT = -2467
891485 TA = 48
60515
MA = 48
52956
Ha = 227
499 n
mi
Hp = 219
764
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9904499
72 X = -3083160
96
Y = 12006630
42 feet Y = 3625502
79 meter
Z = 15919773
22 Z = 4837525
16
XDOT = -22500
922121 XDOT = -6819
214861
YDOT = -7795
070181 feet/sec YDOT = -2452
412893 meter/sec
ZDOT = -8096
756839 ZDOT = -2501
112888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3183863
42 X = -970441
57
Y = 15301838
68 feet Y = 4664000
43 meter
Z = 15856046
63 Z = 4832923
01
XDOT = -22362
845540 XDOT = -6816
195321
YDOT = 3907
092344 feet/sec YDOT = 1190
881746 meter/sec
ZDOT = -8237
653965 ZDOT = -2510
836929
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 14260
13543060
00016717 00000-0 10270-3 0 9057
2 25544 51
6479 3
8542 0001804 89
8626 270
2732 15
50472851 25590
Satellite: ISS
Catalog Number: 25544
Epoch time: 14260
13543060 = yrday
fracday
Element set: 905
Inclination: 51
6479 deg
RA of node: 3
8542 deg
Eccentricity:
0001804
Arg of perigee: 89
8626 deg
Mean anomaly: 270
2732 deg
Mean motion: 15
50472851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2559
Checksum: 301
Coasting Arc #7 (Orbit 2573)
---------------------------------------
Vector Time (GMT): 2014/261/02:11:44
101
Vector Time (MET): N/A
Weight (LBS) : 911938
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3256503
76 A = 6790924
54 meter
Y = -3755609
79 meter E =
0011895
Z = -4638349
54 I = 51
63311
XDOT = 6714
829820 Wp = 106
74468
YDOT = 2172
555097 meter/sec RA = 358
54908 deg
ZDOT = 2958
230410 TA = 192
78112
MA = 192
81130
Ha = 227
375 n
mi
Hp = 219
797
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10684067
44 X = 3320789
34
Y = -12321554
43 feet Y = -3718834
43 meter
Z = -15217682
23 Z = -4622373
49
XDOT = 22030
281561 XDOT = 6675
666670
YDOT = 7127
805435 feet/sec YDOT = 2247
425959 meter/sec
ZDOT = 9705
480347 ZDOT = 2990
754650
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3445121
67 X = 1050073
09
Y = -16005807
15 feet Y = -4878570
02 meter
Z = -15149030
57 Z = -4617424
52
XDOT = 21500
713833 XDOT = 6553
417576
YDOT = -4679
458975 feet/sec YDOT = -1426
299096 meter/sec
ZDOT = 9843
444237 ZDOT = 3000
281803
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 14261
10224272
00016717 00000-0 10270-3 0 9067
2 25544 51
6483 359
0610 0001786 91
2881 268
8474 15
50497989 25748
Satellite: ISS
Catalog Number: 25544
Epoch time: 14261
10224272 = yrday
fracday
Element set: 906
Inclination: 51
6483 deg
RA of node: 359
0610 deg
Eccentricity:
0001786
Arg of perigee: 91
2881 deg
Mean anomaly: 268
8474 deg
Mean motion: 15
50497989 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2574
Checksum: 329
Coasting Arc #8 (Orbit 2589)
---------------------------------------
Vector Time (GMT): 2014/262/02:11:44
101
Vector Time (MET): N/A
Weight (LBS) : 911938
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3505192
63 A = 6791750
43 meter
Y = 3859050
67 meter E =
0011420
Z = 4345432
47 I = 51
60565
XDOT = -6533
902681 Wp = 74
28406
YDOT = -2025
584817 meter/sec RA = 353
58784 deg
ZDOT = -3461
024483 TA = 50
93742
MA = 50
83587
Ha = 227
303 n
mi
Hp = 219
607
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11499975
82 X = -3569193
52
Y = 12660927
40 feet Y = 3819495
93 meter
Z = 14256668
21 Z = 4328248
98
XDOT = -21436
688586 XDOT = -6493
954046
YDOT = -6645
619477 feet/sec YDOT = -2098
428131 meter/sec
ZDOT = -11355
067203 ZDOT = -3492
667863
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3700781
72 X = -1127998
27
Y = 16761611
95 feet Y = 5108939
32 meter
Z = 14182866
22 Z = 4322937
62
XDOT = -20601
959676 XDOT = -6279
477309
YDOT = 5202
614267 feet/sec YDOT = 1585
756828 meter/sec
ZDOT = -11489
305875 ZDOT = -3501
940431
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 14262
13347069
00016717 00000-0 10270-3 0 9072
2 25544 51
6484 353
9482 0001769 89
1849 270
9504 15
50584825 25902
Satellite: ISS
Catalog Number: 25544
Epoch time: 14262
13347069 = yrday
fracday
Element set: 907
Inclination: 51
6484 deg
RA of node: 353
9482 deg
Eccentricity:
0001769
Arg of perigee: 89
1849 deg
Mean anomaly: 270
9504 deg
Mean motion: 15
50584825 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2590
Checksum: 338
Coasting Arc #9 (Orbit 2604)
---------------------------------------
Vector Time (GMT): 2014/263/02:11:44
101
Vector Time (MET): N/A
Weight (LBS) : 911938
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3728551
21 A = 6792821
66 meter
Y = -4009877
26 meter E =
0008551
Z = -4028844
65 I = 51
57835
XDOT = 6288
496830 Wp = 103
92109
YDOT = 1909
752581 meter/sec RA = 348
62462 deg
ZDOT = 3924
021783 TA = 206
92622
MA = 206
97062
Ha = 227
176 n
mi
Hp = 219
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12232779
55 X = 3792684
21
Y = -13155765
29 feet Y = -3967824
06 meter
Z = -13217994
25 Z = -4010575
72
XDOT = 20631
551280 XDOT = 6247
612610
YDOT = 6265
592456 feet/sec YDOT = 1979
846477 meter/sec
ZDOT = 12874
087216 ZDOT = 3954
470743
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3779577
66 X = 1152015
27
Y = -17620934
48 feet Y = -5370860
83 meter
Z = -13139554
35 Z = -4004936
17
XDOT = 19557
232522 XDOT = 5961
044473
YDOT = -5489
034428 feet/sec YDOT = -1673
057694 meter/sec
ZDOT = 13003
260734 ZDOT = 3963
393872
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 14263
10021333
00016717 00000-0 10270-3 0 9084
2 25544 51
6482 349
1545 0001697 91
5513 268
5832 15
50607547 26053
Satellite: ISS
Catalog Number: 25544
Epoch time: 14263
10021333 = yrday
fracday
Element set: 908
Inclination: 51
6482 deg
RA of node: 349
1545 deg
Eccentricity:
0001697
Arg of perigee: 91
5513 deg
Mean anomaly: 268
5832 deg
Mean motion: 15
50607547 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2605
Checksum: 301
Coasting Arc #10 (Orbit 2610)
---------------------------------------
Vector Time (GMT): 2014/263/11:28:05
000
Vector Time (MET): N/A
Weight (LBS) : 929394
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3407090
51 A = 6792344
15 meter
Y = -4180330
14 meter E =
0009317
Z = -4139215
75 I = 51
56517
XDOT = 6476
918836 Wp = 108
57467
YDOT = 1546
566641 meter/sec RA = 346
70526 deg
ZDOT = 3773
471318 TA = 200
41230
MA = 200
44956
Ha = 227
158 n
mi
Hp = 219
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11178118
47 X = 3473689
60
Y = -13714993
89 feet Y = -4141857
97 meter
Z = -13580104
16 Z = -4122502
39
XDOT = 21249
733713 XDOT = 6440
813156
YDOT = 5074
037536 feet/sec YDOT = 1618
794315 meter/sec
ZDOT = 12380
155242 ZDOT = 3804
847253
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13378780
51 X = -4077852
30
Y = 11662158
82 feet Y = 3554626
01 meter
Z = -13508253
12 Z = -4117315
55
XDOT = -19188
552777 XDOT = -5848
670886
YDOT = -7534
478446 feet/sec YDOT = -2296
509030 meter/sec
ZDOT = 12513
335422 ZDOT = 3814
064637
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 14263
48690120
00016717 00000-0 10270-3 0 9092
2 25544 51
6481 347
2351 0001874 109
3004 250
8350 15
50639920 26112
Satellite: ISS
Catalog Number: 25544
Epoch time: 14263
48690120 = yrday
fracday
Element set: 909
Inclination: 51
6481 deg
RA of node: 347
2351 deg
Eccentricity:
0001874
Arg of perigee: 109
3004 deg
Mean anomaly: 250
8350 deg
Mean motion: 15
50639920 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2611
Checksum: 288
Coasting Arc #11 (Orbit 2626)
---------------------------------------
Vector Time (GMT): 2014/264/11:28:05
000
Vector Time (MET): N/A
Weight (LBS) : 929394
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3640465
49 A = 6793509
64 meter
Y = 4334217
30 meter E =
0013474
Z = 3745688
24 I = 51
53913
XDOT = -6195
366007 Wp = 87
11867
YDOT = -1514
687366 meter/sec RA = 341
73977 deg
ZDOT = -4254
735844 TA = 48
07016
MA = 47
95537
Ha = 227
167 n
mi
Hp = 219
425
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11943784
41 X = -3706856
45
Y = 14219873
02 feet Y = 4293136
54 meter
Z = 12289003
40 Z = 3727841
58
XDOT = -20326
003960 XDOT = -6157
299879
YDOT = -4969
446740 feet/sec YDOT = -1583
755688 meter/sec
ZDOT = -13959
107099 ZDOT = -4284
739316
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14000299
92 X = 4267291
42
Y = -12277190
42 feet Y = -3742087
64 meter
Z = 12212312
50 Z = 3722312
85
XDOT = 18379
345032 XDOT = 5602
024366
YDOT = 6901
191256 feet/sec YDOT = 2103
483095 meter/sec
ZDOT = -14086
448462 ZDOT = -4293
549491
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 14264
51804246
00016717 00000-0 10270-3 0 9105
2 25544 51
6480 342
1219 0001929 107
2338 252
9025 15
50682669 26273
Satellite: ISS
Catalog Number: 25544
Epoch time: 14264
51804246 = yrday
fracday
Element set: 910
Inclination: 51
6480 deg
RA of node: 342
1219 deg
Eccentricity:
0001929
Arg of perigee: 107
2338 deg
Mean anomaly: 252
9025 deg
Mean motion: 15
50682669 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2627
Checksum: 302
Coasting Arc #12 (Orbit 2641)
---------------------------------------
Vector Time (GMT): 2014/265/11:28:05
000
Vector Time (MET): N/A
Weight (LBS) : 929394
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3829158
91 A = 6794603
28 meter
Y = -4523314
65 meter E =
0006367
Z = -3328874
33 I = 51
51367
XDOT = 5865
549475 Wp = 91
05138
YDOT = 1529
118991 meter/sec RA = 336
77339 deg
ZDOT = 4676
929472 TA = 230
21889
MA = 230
27498
Ha = 226
994 n
mi
Hp = 219
423
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12562857
30 X = 3895625
67
Y = -14840271
16 feet Y = -4480123
36 meter
Z = -10921503
71 Z = -3310110
72
XDOT = 19243
928724 XDOT = 5825
295544
YDOT = 5016
794591 feet/sec YDOT = 1594
486967 meter/sec
ZDOT = 15344
256797 ZDOT = 4705
325489
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14473775
15 X = -4411606
67
Y = 13050795
02 feet Y = 3977882
32 meter
Z = -10840888
22 Z = -3304302
73
XDOT = -17368
805884 XDOT = -5294
012034
YDOT = -6437
520998 feet/sec YDOT = -1962
156400 meter/sec
ZDOT = 15464
751573 ZDOT = 4713
656279
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 14265
48470267
00016717 00000-0 10270-3 0 9115
2 25544 51
6477 337
3287 0001816 109
2696 250
8651 15
50734931 26423
Satellite: ISS
Catalog Number: 25544
Epoch time: 14265
48470267 = yrday
fracday
Element set: 911
Inclination: 51
6477 deg
RA of node: 337
3287 deg
Eccentricity:
0001816
Arg of perigee: 109
2696 deg
Mean anomaly: 250
8651 deg
Mean motion: 15
50734931 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2642
Checksum: 322
Coasting Arc #13 (Orbit 2657)
---------------------------------------
Vector Time (GMT): 2014/266/11:28:05
000
Vector Time (MET): N/A
Weight (LBS) : 929394
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4007698
60 A = 6795717
84 meter
Y = 4696660
11 meter E =
0015258
Z = 2822394
60 I = 51
48936
XDOT = -5505
837298 Wp = 100
58660
YDOT = -1633
811304 meter/sec RA = 331
80546 deg
ZDOT = -5078
652345 TA = 47
31905
MA = 47
19061
Ha = 226
940 n
mi
Hp = 219
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13148617
46 X = -4073630
21
Y = 15408989
86 feet Y = 4651475
21 meter
Z = 9259824
80 Z = 2802764
84
XDOT = -18063
770662 XDOT = -5462
487882
YDOT = -5360
273307 feet/sec YDOT = -1695
139531 meter/sec
ZDOT = -16662
245228 ZDOT = -5105
293477
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14883723
25 X = 4536558
85
Y = -13796824
41 feet Y = -4205272
08 meter
Z = 9175504
53 Z = 2796693
78
XDOT = 16220
628469 XDOT = 4944
047557
YDOT = 6296
681813 feet/sec YDOT = 1919
228617 meter/sec
ZDOT = -16775
250838 ZDOT = -5113
096456
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 14266
51577129
00016717 00000-0 10270-3 0 9126
2 25544 51
6474 332
2150 0001880 106
9264 253
2093 15
50800963 26582
Satellite: ISS
Catalog Number: 25544
Epoch time: 14266
51577129 = yrday
fracday
Element set: 912
Inclination: 51
6474 deg
RA of node: 332
2150 deg
Eccentricity:
0001880
Arg of perigee: 106
9264 deg
Mean anomaly: 253
2093 deg
Mean motion: 15
50800963 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2658
Checksum: 302
Coasting Arc #14 (Orbit 2672)
---------------------------------------
Vector Time (GMT): 2014/267/11:28:05
000
Vector Time (MET): N/A
Weight (LBS) : 929394
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4126120
36 A = 6796762
92 meter
Y = -4885512
30 meter E =
0006908
Z = -2301042
68 I = 51
46533
XDOT = 5124
705698 Wp = 57
10994
YDOT = 1790
945154 meter/sec RA = 326
83643 deg
ZDOT = 5402
391714 TA = 277
24226
MA = 277
32078
Ha = 226
852 n
mi
Hp = 219
262
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13537140
29 X = 4191622
43
Y = -16028583
68 feet Y = -4839005
46 meter
Z = -7549352
64 Z = -2280838
58
XDOT = 16813
338905 XDOT = 5078
054777
YDOT = 5875
804312 feet/sec YDOT = 1847
992916 meter/sec
ZDOT = 17724
382265 ZDOT = 5427
173403
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15080450
69 X = -4596521
37
Y = 14630533
24 feet Y = 4459386
53 meter
Z = -7462566
00 Z = -2274590
12
XDOT = -14982
940047 XDOT = -4566
800126
YDOT = -6375
705899 feet/sec YDOT = -1943
315158 meter/sec
ZDOT = 17829
445951 ZDOT = 5434
415126
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 14267
48236398
00016717 00000-0 10270-3 0 9134
2 25544 51
6466 327
4209 0001791 107
7767 252
3579 15
50823962 26732
Satellite: ISS
Catalog Number: 25544
Epoch time: 14267
48236398 = yrday
fracday
Element set: 913
Inclination: 51
6466 deg
RA of node: 327
4209 deg
Eccentricity:
0001791
Arg of perigee: 107
7767 deg
Mean anomaly: 252
3579 deg
Mean motion: 15
50823962 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2673
Checksum: 340
Coasting Arc #15 (Orbit 2688)
---------------------------------------
Vector Time (GMT): 2014/268/11:28:05
000
Vector Time (MET): N/A
Weight (LBS) : 929394
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4229481
58 A = 6797513
65 meter
Y = 5035268
35 meter E =
0015779
Z = 1692313
09 I = 51
44295
XDOT = -4723
877223 Wp = 114
58354
YDOT = -2047
093170 meter/sec RA = 321
86611 deg
ZDOT = -5679
829970 TA = 46
83133
MA = 46
69956
Ha = 226
736 n
mi
Hp = 219
070
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13876251
90 X = -4293693
57
Y = 16519909
29 feet Y = 4987612
77 meter
Z = 5552208
32 Z = 1671609
94
XDOT = -15498
284851 XDOT = -4673
043973
YDOT = -6716
184941 feet/sec YDOT = -2099
635235 meter/sec
ZDOT = -18634
612761 ZDOT = -5702
654369
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15191428
50 X = 4630347
41
Y = -15351151
01 feet Y = -4679030
83 meter
Z = 5463281
96 Z = 1665208
34
XDOT = 13672
674578 XDOT = 4167
431211
YDOT = 6822
223549 feet/sec YDOT = 2079
413738 meter/sec
ZDOT = -18731
302607 ZDOT = -5709
301035
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 14268
51335995
00016717 00000-0 10270-3 0 9143
2 25544 51
6465 322
3064 0001896 106
5111 253
6249 15
50916876 26892
Satellite: ISS
Catalog Number: 25544
Epoch time: 14268
51335995 = yrday
fracday
Element set: 914
Inclination: 51
6465 deg
RA of node: 322
3064 deg
Eccentricity:
0001896
Arg of perigee: 106
5111 deg
Mean anomaly: 253
6249 deg
Mean motion: 15
50916876 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2689
Checksum: 329
Coasting Arc #16 (Orbit 2703)
---------------------------------------
Vector Time (GMT): 2014/269/11:28:05
000
Vector Time (MET): N/A
Weight (LBS) : 929394
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4266155
64 A = 6798211
79 meter
Y = -5176244
20 meter E =
0010443
Z = -1082982
19 I = 51
42056
XDOT = 4332
289203 Wp = 47
60318
YDOT = 2352
642706 meter/sec RA = 316
89441 deg
ZDOT = 5864
471771 TA = 300
63236
MA = 300
73529
Ha = 226
735 n
mi
Hp = 219
060
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13996573
62 X = 4328981
38
Y = -16982428
49 feet Y = -5128186
16 meter
Z = -3553091
18 Z = -1062104
22
XDOT = 14213
547254 XDOT = 4277
171311
YDOT = 7718
644048 feet/sec YDOT = 2400
781784 meter/sec
ZDOT = 19240
392951 ZDOT = 5885
383505
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15061790
53 X = -4590833
75
Y = 16064828
16 feet Y = 4896559
62 meter
Z = -3463404
34 Z = -1055645
64
XDOT = -12405
662734 XDOT = -3781
246001
YDOT = -7495
315476 feet/sec YDOT = -2284
572157 meter/sec
ZDOT = 19328
892103 ZDOT = 5891
446313
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 14269
47988476
00016717 00000-0 10270-3 0 9158
2 25544 51
6457 317
5115 0001863 105
5654 254
5703 15
50914851 27045
Satellite: ISS
Catalog Number: 25544
Epoch time: 14269
47988476 = yrday
fracday
Element set: 915
Inclination: 51
6457 deg
RA of node: 317
5115 deg
Eccentricity:
0001863
Arg of perigee: 105
5654 deg
Mean anomaly: 254
5703 deg
Mean motion: 15
50914851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2704
Checksum: 327
Coasting Arc #17 (Orbit 2718)
---------------------------------------
Vector Time (GMT): 2014/270/11:28:05
000
Vector Time (MET): N/A
Weight (LBS) : 929394
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4289552
65 A = 6798309
96 meter
Y = 5250690
30 meter E =
0014594
Z = 396281
18 I = 51
40012
XDOT = -3935
601180 Wp = 127
51225
YDOT = -2753
627929 meter/sec RA = 311
92138 deg
ZDOT = -5972
871526 TA = 48
20609
MA = 48
08150
Ha = 226
574 n
mi
Hp = 218
856
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14073335
46 X = -4349873
31
Y = 17226674
22 feet Y = 5202384
52 meter
Z = 1300135
10 Z = 375295
67
XDOT = -12912
077361 XDOT = -3875
502229
YDOT = -9034
212367 feet/sec YDOT = -2797
303060 meter/sec
ZDOT = -19596
035190 ZDOT = -5991
844102
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14856927
07 X = 4528391
37
Y = -16562460
05 feet Y = -5048237
82 meter
Z = 1209984
28 Z = 368803
21
XDOT = 11152
503800 XDOT = 3399
283158
YDOT = 8529
829064 feet/sec YDOT = 2599
891899 meter/sec
ZDOT = -19676
216501 ZDOT = -5997
310789
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 14270
51080799
00016717 00000-0 10270-3 0 9167
2 25544 51
6461 312
3960 0002001 107
9743 252
1636 15
51024911 27196
Satellite: ISS
Catalog Number: 25544
Epoch time: 14270
51080799 = yrday
fracday
Element set: 916
Inclination: 51
6461 deg
RA of node: 312
3960 deg
Eccentricity:
0002001
Arg of perigee: 107
9743 deg
Mean anomaly: 252
1636 deg
Mean motion: 15
51024911 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2719
Checksum: 287
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