[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
September 12th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 20989 63 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
257/02:09:27
924 1
3 1
3 1
3
N/A 0
3 -0
2 227
9
000/00:02:55
847 0
1 0
0 219
9
263/11:28:05
000 0
0 0
0 0
0
N/A 0
0 0
0 227
5
000/00:00:00
000 0
0 0
0 219
7
Coasting Arc #1 (Orbit 2464)
---------------------------------------
Vector Time (GMT): 2014/254/00:29:18
518
Vector Time (MET): N/A
Weight (LBS) : 912103
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2308305
44 A = 6793853
40 meter
Y = 5123650
41 meter E =
0014701
Z = 3806351
82 I = 51
84740
XDOT = -6394
486758 Wp = 95
07447
YDOT = -266
764974 meter/sec RA = 33
59991 deg
ZDOT = 4221
640543 TA = 310
41740
MA = 310
54557
Ha = 227
970 n
mi
Hp = 219
217
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7573180
57 X = 2232349
98
Y = 16809876
69 feet Y = 5149039
19 meter
Z = 12488030
91 Z = 3817380
09
XDOT = -20979
287265 XDOT = -6411
535879
YDOT = -875
213169 feet/sec YDOT = -338
367031 meter/sec
ZDOT = 13850
526715 ZDOT = 4190
535616
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6440729
81 X = 1963134
45
Y = 17242116
91 feet Y = 5255397
24 meter
Z = 12534047
15 Z = 3820377
57
XDOT = -19714
442763 XDOT = -6008
962154
YDOT = -2644
435387 feet/sec YDOT = -806
023906 meter/sec
ZDOT = 13718
211753 ZDOT = 4181
310942
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 14254
07660321
00016717 00000-0 10270-3 0 9008
2 25544 51
6448 33
8892 0003326 88
7027 271
4505 15
50458188 24655
Satellite: ISS
Catalog Number: 25544
Epoch time: 14254
07660321 = yrday
fracday
Element set: 900
Inclination: 51
6448 deg
RA of node: 33
8892 deg
Eccentricity:
0003326
Arg of perigee: 88
7027 deg
Mean anomaly: 271
4505 deg
Mean motion: 15
50458188 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2465
Checksum: 307
Coasting Arc #2 (Orbit 2479)
---------------------------------------
Vector Time (GMT): 2014/255/00:29:18
518
Vector Time (MET): N/A
Weight (LBS) : 912103
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2194224
32 A = 6792683
67 meter
Y = -4918550
96 meter E =
0010958
Z = -4150402
20 I = 51
81758
XDOT = 6643
023268 Wp = 75
43991
YDOT = 231
593163 meter/sec RA = 28
65436 deg
ZDOT = -3792
174851 TA = 155
50559
MA = 155
45348
Ha = 227
996 n
mi
Hp = 219
145
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7198898
70 X = -2118899
46
Y = -16136978
21 feet Y = -4942667
52 meter
Z = -13616805
12 Z = -4160877
93
XDOT = 21794
695760 XDOT = 6658
361060
YDOT = 759
820087 feet/sec YDOT = 305
965055 meter/sec
ZDOT = -12441
518540 ZDOT = -3759
866621
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6385399
17 X = -1946269
67
Y = -16439618
97 feet Y = -5010795
86 meter
Z = -13660497
62 Z = -4163719
68
XDOT = 20618
130372 XDOT = 6284
406137
YDOT = 2200
185515 feet/sec YDOT = 670
616545 meter/sec
ZDOT = -12304
085458 ZDOT = -3750
285248
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
04342796
00016717 00000-0 10270-3 0 9010
2 25544 51
6453 29
0957 0003395 87
8674 272
2866 15
50469304 24802
Satellite: ISS
Catalog Number: 25544
Epoch time: 14255
04342796 = yrday
fracday
Element set: 901
Inclination: 51
6453 deg
RA of node: 29
0957 deg
Eccentricity:
0003395
Arg of perigee: 87
8674 deg
Mean anomaly: 272
2866 deg
Mean motion: 15
50469304 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2480
Checksum: 326
Coasting Arc #3 (Orbit 2495)
---------------------------------------
Vector Time (GMT): 2014/256/00:29:18
518
Vector Time (MET): N/A
Weight (LBS) : 912103
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2056617
45 A = 6791498
68 meter
Y = 4711765
72 meter E =
0012365
Z = 4429386
15 I = 51
78675
XDOT = -6895
633790 Wp = 105
37515
YDOT = -148
564030 meter/sec RA = 23
70747 deg
ZDOT = 3348
775289 TA = 310
79964
MA = 310
90684
Ha = 227
844 n
mi
Hp = 219
144
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6747432
59 X = 1982259
90
Y = 15458548
95 feet Y = 4734348
84 meter
Z = 14532106
78 Z = 4439195
87
XDOT = -22623
470440 XDOT = -6909
727373
YDOT = -487
414798 feet/sec YDOT = -225
753928 meter/sec
ZDOT = 10986
795566 ZDOT = 3315
242882
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6228811
60 X = 1898541
78
Y = 15636702
19 feet Y = 4766066
83 meter
Z = 14572994
21 Z = 4441848
64
XDOT = -21530
054148 XDOT = -6562
360504
YDOT = -1563
552711 feet/sec YDOT = -476
570866 meter/sec
ZDOT = 10844
146091 ZDOT = 3305
295728
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
07468472
00016717 00000-0 10270-3 0 9025
2 25544 51
6458 23
9839 0003270 92
6283 267
5242 15
50519493 24968
Satellite: ISS
Catalog Number: 25544
Epoch time: 14256
07468472 = yrday
fracday
Element set: 902
Inclination: 51
6458 deg
RA of node: 23
9839 deg
Eccentricity:
0003270
Arg of perigee: 92
6283 deg
Mean anomaly: 267
5242 deg
Mean motion: 15
50519493 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2496
Checksum: 327
Coasting Arc #4 (Orbit 2510)
---------------------------------------
Vector Time (GMT): 2014/257/00:29:18
518
Vector Time (MET): N/A
Weight (LBS) : 912103
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1847198
35 A = 6790427
12 meter
Y = -4545733
70 meter E =
0013973
Z = -4707379
61 I = 51
75451
XDOT = 7104
790771 Wp = 75
34506
YDOT = 49
247670 meter/sec RA = 18
75593 deg
ZDOT = -2839
126104 TA = 166
47837
MA = 166
44090
Ha = 227
880 n
mi
Hp = 219
050
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6060362
04 X = -1773362
57
Y = -14913824
48 feet Y = -4565977
84 meter
Z = -15444158
82 Z = -4716173
34
XDOT = 23309
681008 XDOT = 7117
503653
YDOT = 161
573719 feet/sec YDOT = 128
768869 meter/sec
ZDOT = -9314
718189 ZDOT = -2804
581002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5809681
22 X = -1770790
83
Y = -14975522
60 feet Y = -4564539
29 meter
Z = -15480746
66 Z = -4718531
58
XDOT = 22272
969963 XDOT = 6788
801245
YDOT = 824
113531 feet/sec YDOT = 251
189804 meter/sec
ZDOT = -9167
748054 ZDOT = -2794
329607
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
04147030
00016717 00000-0 10270-3 0 9038
2 25544 51
6459 19
1902 0003350 92
2182 267
9353 15
50533599 25118
Satellite: ISS
Catalog Number: 25544
Epoch time: 14257
04147030 = yrday
fracday
Element set: 903
Inclination: 51
6459 deg
RA of node: 19
1902 deg
Eccentricity:
0003350
Arg of perigee: 92
2182 deg
Mean anomaly: 267
9353 deg
Mean motion: 15
50533599 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2511
Checksum: 290
Coasting Arc #5 (Orbit 2511)
---------------------------------------
Vector Time (GMT): 2014/257/02:10:55
847
Vector Time (MET): N/A
Weight (LBS) : 911974
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1987956
58 A = 6788714
45 meter
Y = -3752396
81 meter E =
0016912
Z = -5311323
03 I = 51
74532
XDOT = 7065
899933 Wp = 94
49546
YDOT = 2864
214948 meter/sec RA = 18
38018 deg
ZDOT = 621
549004 TA = 181
44116
MA = 181
44604
Ha = 227
888 n
mi
Hp = 219
925
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6522167
27 X = 2055569
82
Y = -12311013
16 feet Y = -3729788
61 meter
Z = -17425600
49 Z = -5301501
22
XDOT = 23182
086394 XDOT = 7030
327166
YDOT = 9397
030668 feet/sec YDOT = 2943
031565 meter/sec
ZDOT = 2039
202770 ZDOT = 655
787650
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 834383
53 X = 254320
10
Y = -13960010
58 feet Y = -4255011
22 meter
Z = -17383128
95 Z = -5298377
70
XDOT = 23953
961948 XDOT = 7301
167602
YDOT = -1286
553528 feet/sec YDOT = -392
141515 meter/sec
ZDOT = 2184
356342 ZDOT = 665
791813
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
10592224
00016717 00000-0 10270-3 0 9045
2 25544 51
6471 18
8707 0002297 93
5701 266
5712 15
50286483 25123
Satellite: ISS
Catalog Number: 25544
Epoch time: 14257
10592224 = yrday
fracday
Element set: 904
Inclination: 51
6471 deg
RA of node: 18
8707 deg
Eccentricity:
0002297
Arg of perigee: 93
5701 deg
Mean anomaly: 266
5712 deg
Mean motion: 15
50286483 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2512
Checksum: 302
Coasting Arc #6 (Orbit 2527)
---------------------------------------
Vector Time (GMT): 2014/258/02:10:55
847
Vector Time (MET): N/A
Weight (LBS) : 911974
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2186845
93 A = 6788817
51 meter
Y = 3724630
79 meter E =
0005778
Z = 5233305
50 I = 51
71610
XDOT = -7122
197528 Wp = 69
17220
YDOT = -2607
203668 meter/sec RA = 13
42724 deg
ZDOT = -1117
564903 TA = 31
54788
MA = 31
51325
Ha = 227
807 n
mi
Hp = 219
833
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7174691
37 X = -2253754
86
Y = 12219917
30 feet Y = 3699802
37 meter
Z = 17169637
47 Z = 5222519
28
XDOT = -23366
789791 XDOT = -7087
085050
YDOT = -8553
817807 feet/sec YDOT = -2686
652448 meter/sec
ZDOT = -3666
551520 ZDOT = -1152
078134
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1219549
53 X = -371718
70
Y = 14174354
59 feet Y = 4320343
28 meter
Z = 17123066
23 Z = 5219110
59
XDOT = -23702
618179 XDOT = -7224
558021
YDOT = 2578
702412 feet/sec YDOT = 785
988495 meter/sec
ZDOT = -3812
912938 ZDOT = -1162
175864
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
13729874
00016717 00000-0 10270-3 0 9053
2 25544 51
6468 13
7590 0002143 94
9087 265
2308 15
50349018 25283
Satellite: ISS
Catalog Number: 25544
Epoch time: 14258
13729874 = yrday
fracday
Element set: 905
Inclination: 51
6468 deg
RA of node: 13
7590 deg
Eccentricity:
0002143
Arg of perigee: 94
9087 deg
Mean anomaly: 265
2308 deg
Mean motion: 15
50349018 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2528
Checksum: 320
Coasting Arc #7 (Orbit 2542)
---------------------------------------
Vector Time (GMT): 2014/259/02:10:55
847
Vector Time (MET): N/A
Weight (LBS) : 911974
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2399608
10 A = 6789283
56 meter
Y = -3748956
27 meter E =
0015621
Z = -5140552
60 I = 51
68766
XDOT = 7102
991058 Wp = 101
16824
YDOT = 2342
734109 meter/sec RA = 8
47167 deg
ZDOT = 1608
345279 TA = 184
36626
MA = 184
37990
Ha = 227
752 n
mi
Hp = 219
868
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7872729
98 X = 2466322
61
Y = -12299725
28 feet Y = -3721749
66 meter
Z = -16865330
05 Z = -5128733
31
XDOT = 23303
776437 XDOT = 7068
453327
YDOT = 7686
135528 feet/sec YDOT = 2421
971359 meter/sec
ZDOT = 5276
723356 ZDOT = 1642
766544
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1560525
32 X = 475648
12
Y = -14578908
40 feet Y = -4443651
28 meter
Z = -16814358
97 Z = -5125016
61
XDOT = 23169
419036 XDOT = 7062
038922
YDOT = -3769
601131 feet/sec YDOT = -1148
974425 meter/sec
ZDOT = 5422
736123 ZDOT = 1652
849970
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
10419660
00016717 00000-0 10270-3 0 9061
2 25544 51
6474 8
9663 0002205 96
4851 263
6551 15
50350570 25436
Satellite: ISS
Catalog Number: 25544
Epoch time: 14259
10419660 = yrday
fracday
Element set: 906
Inclination: 51
6474 deg
RA of node: 8
9663 deg
Eccentricity:
0002205
Arg of perigee: 96
4851 deg
Mean anomaly: 263
6551 deg
Mean motion: 15
50350570 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2543
Checksum: 301
Coasting Arc #8 (Orbit 2558)
---------------------------------------
Vector Time (GMT): 2014/260/02:10:55
847
Vector Time (MET): N/A
Weight (LBS) : 911974
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2623527
33 A = 6789720
15 meter
Y = 3786945
85 meter E =
0008006
Z = 4982314
59 I = 51
65862
XDOT = -7062
313077 Wp = 66
45392
YDOT = -2106
933060 meter/sec RA = 3
51429 deg
ZDOT = -2111
537676 TA = 44
13644
MA = 44
07258
Ha = 227
683 n
mi
Hp = 219
755
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8607373
14 X = -2689881
28
Y = 12424363
02 feet Y = 3757237
26 meter
Z = 16346176
46 Z = 4969408
42
XDOT = -23170
318495 XDOT = -7027
970829
YDOT = -6912
510040 feet/sec YDOT = -2185
716564 meter/sec
ZDOT = -6927
617048 ZDOT = -2145
761732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1898010
76 X = -578513
68
Y = 15055359
51 feet Y = 4588873
58 meter
Z = 16290575
77 Z = 4965367
50
XDOT = -22579
734960 XDOT = -6882
303216
YDOT = 4827
242421 feet/sec YDOT = 1471
343490 meter/sec
ZDOT = -7072
829063 ZDOT = -2155
798298
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
13553122
00016717 00000-0 10270-3 0 9079
2 25544 51
6473 3
8542 0002086 97
0029 263
1359 15
50414655 25599
Satellite: ISS
Catalog Number: 25544
Epoch time: 14260
13553122 = yrday
fracday
Element set: 907
Inclination: 51
6473 deg
RA of node: 3
8542 deg
Eccentricity:
0002086
Arg of perigee: 97
0029 deg
Mean anomaly: 263
1359 deg
Mean motion: 15
50414655 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2559
Checksum: 292
Coasting Arc #9 (Orbit 2573)
---------------------------------------
Vector Time (GMT): 2014/261/02:10:55
847
Vector Time (MET): N/A
Weight (LBS) : 911974
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2841148
27 A = 6790492
27 meter
Y = -3879138
59 meter E =
0013300
Z = -4807512
34 I = 51
63031
XDOT = 6949
212649 Wp = 106
62980
YDOT = 1878
540842 meter/sec RA = 358
55479 deg
ZDOT = 2593
322079 TA = 188
97161
MA = 188
99540
Ha = 227
605 n
mi
Hp = 219
822
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9321352
59 X = 2907667
79
Y = -12726832
66 feet Y = -3846995
54 meter
Z = -15772678
29 Z = -4793548
58
XDOT = 22799
254097 XDOT = 6915
092415
YDOT = 6163
191739 feet/sec YDOT = 1956
060889 meter/sec
ZDOT = 8508
274538 ZDOT = 2626
997189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2115240
30 X = 644725
24
Y = -15693257
74 feet Y = -4783304
96 meter
Z = -15712564
53 Z = -4789189
67
XDOT = 21754
006672 XDOT = 6630
621234
YDOT = -5722
272725 feet/sec YDOT = -1744
148727 meter/sec
ZDOT = 8651
188210 ZDOT = 2636
882166
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
10238944
00016717 00000-0 10270-3 0 9080
2 25544 51
6477 359
0612 0002082 99
3959 260
7428 15
50414449 25748
Satellite: ISS
Catalog Number: 25544
Epoch time: 14261
10238944 = yrday
fracday
Element set: 908
Inclination: 51
6477 deg
RA of node: 359
0612 deg
Eccentricity:
0002082
Arg of perigee: 99
3959 deg
Mean anomaly: 260
7428 deg
Mean motion: 15
50414449 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2574
Checksum: 322
Coasting Arc #10 (Orbit 2589)
---------------------------------------
Vector Time (GMT): 2014/262/02:10:55
847
Vector Time (MET): N/A
Weight (LBS) : 911974
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3062864
56 A = 6791232
18 meter
Y = 3982424
40 meter E =
0010517
Z = 4562409
31 I = 51
60239
XDOT = -6811
108594 Wp = 72
50758
YDOT = -1694
848880 meter/sec RA = 353
59376 deg
ZDOT = -3084
114764 TA = 48
42140
MA = 48
33130
Ha = 227
547 n
mi
Hp = 219
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10048768
23 X = -3129331
92
Y = 13065696
85 feet Y = 3947802
29 meter
Z = 14968534
48 Z = 4547368
57
XDOT = -22346
156803 XDOT = -6776
668619
YDOT = -5560
527820 feet/sec YDOT = -1770
822852 meter/sec
ZDOT = -10118
486760 ZDOT = -3117
118178
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2303255
58 X = -702032
30
Y = 16380421
65 feet Y = 4992752
52 meter
Z = 14903825
08 Z = 4542685
88
XDOT = -20903
235379 XDOT = -6371
306143
YDOT = 6421
490425 feet/sec YDOT = 1957
270282 meter/sec
ZDOT = -10258
571326 ZDOT = -3126
812540
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
13368217
00016717 00000-0 10270-3 0 9092
2 25544 51
6478 353
9488 0002008 99
1068 261
0310 15
50479738 25904
Satellite: ISS
Catalog Number: 25544
Epoch time: 14262
13368217 = yrday
fracday
Element set: 909
Inclination: 51
6478 deg
RA of node: 353
9488 deg
Eccentricity:
0002008
Arg of perigee: 99
1068 deg
Mean anomaly: 261
0310 deg
Mean motion: 15
50479738 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2590
Checksum: 320
Coasting Arc #11 (Orbit 2604)
---------------------------------------
Vector Time (GMT): 2014/263/02:10:55
847
Vector Time (MET): N/A
Weight (LBS) : 911974
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3258040
45 A = 6792245
35 meter
Y = -4135924
96 meter E =
0010226
Z = -4301598
71 I = 51
57463
XDOT = 6611
237267 Wp = 108
30922
YDOT = 1532
945251 meter/sec RA = 348
63078 deg
ZDOT = 3537
251835 TA = 197
82797
MA = 197
86387
Ha = 227
462 n
mi
Hp = 219
773
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10689109
07 X = 3324942
86
Y = -13569307
60 feet Y = -4099117
86 meter
Z = -14112856
66 Z = -4285608
71
XDOT = 21690
410981 XDOT = 6576
421402
YDOT = 5029
347936 feet/sec YDOT = 1606
682125 meter/sec
ZDOT = 11605
156939 ZDOT = 3569
283398
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2308692
07 X = 703689
34
Y = -17175256
22 feet Y = -5235018
10 meter
Z = -14044087
70 Z = -4280637
93
XDOT = 19891
217834 XDOT = 6062
843196
YDOT = -6916
651337 feet/sec YDOT = -2108
195328 meter/sec
ZDOT = 11741
130931 ZDOT = 3578
696708
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
10050096
00016717 00000-0 10270-3 0 9105
2 25544 51
6476 349
1555 0001961 102
7080 257
4290 15
50476837 26056
Satellite: ISS
Catalog Number: 25544
Epoch time: 14263
10050096 = yrday
fracday
Element set: 910
Inclination: 51
6476 deg
RA of node: 349
1555 deg
Eccentricity:
0001961
Arg of perigee: 102
7080 deg
Mean anomaly: 257
4290 deg
Mean motion: 15
50476837 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2605
Checksum: 295
Coasting Arc #12 (Orbit 2610)
---------------------------------------
Vector Time (GMT): 2014/263/11:28:05
000
Vector Time (MET): N/A
Weight (LBS) : 929430
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3226569
24 A = 6792389
53 meter
Y = -4221500
92 meter E =
0010176
Z = -4242044
22 I = 51
56341
XDOT = 6592
838316 Wp = 110
99257
YDOT = 1399
204618 meter/sec RA = 346
70852 deg
ZDOT = 3625
681008 TA = 196
20741
MA = 196
23998
Ha = 227
470 n
mi
Hp = 219
702
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10585857
09 X = 3294141
63
Y = -13850068
62 feet Y = -4185042
02 meter
Z = -13917467
93 Z = -4226205
44
XDOT = 21630
046970 XDOT = 6559
089772
YDOT = 4590
566331 feet/sec YDOT = 1472
741740 meter/sec
ZDOT = 11895
278897 ZDOT = 3657
625805
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12819166
36 X = -3907281
91
Y = 11893095
92 feet Y = 3625015
64 meter
Z = -13849329
51 Z = -4221275
64
XDOT = -19629
830095 XDOT = -5983
172213
YDOT = -7161
912944 feet/sec YDOT = -2182
951065 meter/sec
ZDOT = 12030
905553 ZDOT = 3667
020012
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
48722327
00016717 00000-0 10270-3 0 9110
2 25544 51
6475 347
2363 0002225 117
1443 242
9935 15
50500280 26110
Satellite: ISS
Catalog Number: 25544
Epoch time: 14263
48722327 = yrday
fracday
Element set: 911
Inclination: 51
6475 deg
RA of node: 347
2363 deg
Eccentricity:
0002225
Arg of perigee: 117
1443 deg
Mean anomaly: 242
9935 deg
Mean motion: 15
50500280 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2611
Checksum: 284
Coasting Arc #13 (Orbit 2626)
---------------------------------------
Vector Time (GMT): 2014/264/11:28:05
000
Vector Time (MET): N/A
Weight (LBS) : 929430
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3412416
79 A = 6793496
64 meter
Y = 4385687
11 meter E =
0013145
Z = 3897288
85 I = 51
53701
XDOT = -6358
645824 Wp = 86
55024
YDOT = -1313
051237 meter/sec RA = 341
74376 deg
ZDOT = -4077
276146 TA = 46
28382
MA = 46
17503
Ha = 227
501 n
mi
Hp = 219
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11195593
13 X = -3480136
67
Y = 14388737
25 feet Y = 4347149
14 meter
Z = 12786380
74 Z = 3880546
78
XDOT = -20861
698898 XDOT = -6323
684342
YDOT = -4307
910883 feet/sec YDOT = -1383
962795 meter/sec
ZDOT = -13376
890242 ZDOT = -4108
080374
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13288618
56 X = 4050370
94
Y = -12554910
90 feet Y = -3826736
84 meter
Z = 12714378
74 Z = 3875342
64
XDOT = 18990
748749 XDOT = 5788
380219
YDOT = 6378
974036 feet/sec YDOT = 1944
311286 meter/sec
ZDOT = -13507
673931 ZDOT = -4117
139014
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
51846755
00016717 00000-0 10270-3 0 9128
2 25544 51
6474 342
1238 0002230 116
2689 243
8692 15
50518643 26271
Satellite: ISS
Catalog Number: 25544
Epoch time: 14264
51846755 = yrday
fracday
Element set: 912
Inclination: 51
6474 deg
RA of node: 342
1238 deg
Eccentricity:
0002230
Arg of perigee: 116
2689 deg
Mean anomaly: 243
8692 deg
Mean motion: 15
50518643 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2627
Checksum: 313
Coasting Arc #14 (Orbit 2641)
---------------------------------------
Vector Time (GMT): 2014/265/11:28:05
000
Vector Time (MET): N/A
Weight (LBS) : 929430
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3553586
00 A = 6794527
01 meter
Y = -4588275
27 meter E =
0007096
Z = -3540861
10 I = 51
51109
XDOT = 6081
580793 Wp = 101
31231
YDOT = 1262
006152 meter/sec RA = 336
77820 deg
ZDOT = 4474
395421 TA = 216
97355
MA = 217
02248
Ha = 227
354 n
mi
Hp = 219
653
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11658746
71 X = 3621829
41
Y = -15053396
54 feet Y = -4548155
71 meter
Z = -11616998
38 Z = -3523431
86
XDOT = 19952
692891 XDOT = 6045
281569
YDOT = 4140
440130 feet/sec YDOT = 1329
812012 meter/sec
ZDOT = 14679
775004 ZDOT = 4503
850532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13609921
58 X = -4148304
10
Y = 13380469
89 feet Y = 4078367
22 meter
Z = -11542046
34 Z = -3518015
72
XDOT = -18166
784678 XDOT = -5537
235970
YDOT = -5725
493104 feet/sec YDOT = -1745
130298 meter/sec
ZDOT = 14804
822179 ZDOT = 4512
509800
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
48523929
00016717 00000-0 10270-3 0 9131
2 25544 51
6471 337
3312 0002146 119
9132 240
2232 15
50551418 26421
Satellite: ISS
Catalog Number: 25544
Epoch time: 14265
48523929 = yrday
fracday
Element set: 913
Inclination: 51
6471 deg
RA of node: 337
3312 deg
Eccentricity:
0002146
Arg of perigee: 119
9132 deg
Mean anomaly: 240
2232 deg
Mean motion: 15
50551418 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2642
Checksum: 286
Coasting Arc #15 (Orbit 2657)
---------------------------------------
Vector Time (GMT): 2014/266/11:28:05
000
Vector Time (MET): N/A
Weight (LBS) : 929430
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3683011
36 A = 6795617
35 meter
Y = 4780759
62 meter E =
0014979
Z = 3108660
43 I = 51
48654
XDOT = -5787
787135 Wp = 98
32528
YDOT = -1286
615860 meter/sec RA = 331
81086 deg
ZDOT = -4860
486735 TA = 45
85468
MA = 45
73161
Ha = 227
323 n
mi
Hp = 219
557
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12083370
61 X = -3751298
12
Y = 15684906
88 feet Y = 4739192
46 meter
Z = 10199017
16 Z = 3090602
23
XDOT = -18988
802937 XDOT = -5749
358966
YDOT = -4221
180643 feet/sec YDOT = -1351
124516 meter/sec
ZDOT = -15946
478791 ZDOT = -4888
509550
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13862967
33 X = 4225432
44
Y = -14192258
53 feet Y = -4325800
40 meter
Z = 10121365
27 Z = 3084992
14
XDOT = 17245
596453 XDOT = 5256
457799
YDOT = 5345
845690 feet/sec YDOT = 1629
413766 meter/sec
ZDOT = -16065
422453 ZDOT = -4896
740764
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
51644244
00016717 00000-0 10270-3 0 9141
2 25544 51
6469 332
2183 0002128 118
4659 241
6706 15
50589753 26587
Satellite: ISS
Catalog Number: 25544
Epoch time: 14266
51644244 = yrday
fracday
Element set: 914
Inclination: 51
6469 deg
RA of node: 332
2183 deg
Eccentricity:
0002128
Arg of perigee: 118
4659 deg
Mean anomaly: 241
6706 deg
Mean motion: 15
50589753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2658
Checksum: 322
Coasting Arc #16 (Orbit 2672)
---------------------------------------
Vector Time (GMT): 2014/267/11:28:05
000
Vector Time (MET): N/A
Weight (LBS) : 929430
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3755449
00 A = 6796650
91 meter
Y = -4996117
34 meter E =
0006090
Z = -2672381
75 I = 51
46222
XDOT = 5475
116727 Wp = 71
91038
YDOT = 1351
127765 meter/sec RA = 326
84251 deg
ZDOT = 5179
697508 TA = 257
91674
MA = 257
98498
Ha = 227
251 n
mi
Hp = 219
598
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12321026
90 X = 3824019
29
Y = -16391461
09 feet Y = -4953738
49 meter
Z = -8767656
65 Z = -2653970
86
XDOT = 17962
981387 XDOT = 5434
439686
YDOT = 4432
833874 feet/sec YDOT = 1412
127417 meter/sec
ZDOT = 16993
758228 ZDOT = 5206
196033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13913115
32 X = -4240717
55
Y = 15109437
89 feet Y = 4605356
67 meter
Z = -8688475
83 Z = -2648247
43
XDOT = -16237
245953 XDOT = -4949
112567
YDOT = -5137
024058 feet/sec YDOT = -1565
764933 meter/sec
ZDOT = 17106
200990 ZDOT = 5213
970062
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
48317633
00016717 00000-0 10270-3 0 9158
2 25544 51
6461 327
4252 0002067 121
5280 238
6073 15
50596934 26738
Satellite: ISS
Catalog Number: 25544
Epoch time: 14267
48317633 = yrday
fracday
Element set: 915
Inclination: 51
6461 deg
RA of node: 327
4252 deg
Eccentricity:
0002067
Arg of perigee: 121
5280 deg
Mean anomaly: 238
6073 deg
Mean motion: 15
50596934 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2673
Checksum: 310
Coasting Arc #17 (Orbit 2688)
---------------------------------------
Vector Time (GMT): 2014/268/11:28:05
000
Vector Time (MET): N/A
Weight (LBS) : 929430
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3814663
85 A = 6797509
13 meter
Y = 5184444
70 meter E =
0015918
Z = 2161555
01 I = 51
44000
XDOT = -5154
815125 Wp = 110
76128
YDOT = -1499
834687 meter/sec RA = 321
87266 deg
ZDOT = -5472
604669 TA = 45
21469
MA = 45
08534
Ha = 227
162 n
mi
Hp = 219
478
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12515301
35 X = -3882854
25
Y = 17009333
01 feet Y = 5141405
70 meter
Z = 7091715
93 Z = 2142857
33
XDOT = -16912
123114 XDOT = -5111
076063
YDOT = -4920
717477 feet/sec YDOT = -1557
235414 meter/sec
ZDOT = -17954
739728 ZDOT = -5497
539838
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13883831
57 X = 4231791
86
Y = -15947527
61 feet Y = -4860806
41 meter
Z = 7011290
64 Z = 2137041
39
XDOT = 15186
750684 XDOT = 4628
921608
YDOT = 5241
601116 feet/sec YDOT = 1597
640020 meter/sec
ZDOT = -18060
502003 ZDOT = -5504
841010
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
51433847
00016717 00000-0 10270-3 0 9160
2 25544 51
6460 322
3117 0002067 119
9273 240
2083 15
50658808 26890
Satellite: ISS
Catalog Number: 25544
Epoch time: 14268
51433847 = yrday
fracday
Element set: 916
Inclination: 51
6460 deg
RA of node: 322
3117 deg
Eccentricity:
0002067
Arg of perigee: 119
9273 deg
Mean anomaly: 240
2083 deg
Mean motion: 15
50658808 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2689
Checksum: 314
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