[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 26th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 22604 21 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 127 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 423 ET - UTC (sec) : 67 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
281/17:02:28
402 -0
6 3
1 3
2
N/A -3
0 -0
5 226
1
000/00:06:56
803 0
9 0
1 220
8
Coasting Arc #1 (Orbit 2672)
---------------------------------------
Vector Time (GMT): 2014/267/10:50:55
526
Vector Time (MET): N/A
Weight (LBS) : 932484
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5904123
15 A = 6799484
56 meter
Y = 3317152
25 meter E =
0012577
Z = -543745
48 I = 51
47297
XDOT = -1934
406565 Wp = 136
09881
YDOT = -4405
530483 meter/sec RA = 327
00580 deg
ZDOT = -5963
805565 TA = 49
77303
MA = 49
66306
Ha = 227
129 n
mi
Hp = 219
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19370482
77 X = -5938136
14
Y = 10883045
43 feet Y = 3250938
26 meter
Z = -1783941
87 Z = -572510
20
XDOT = -6346
478232 XDOT = -1856
028672
YDOT = -14453
840166 feet/sec YDOT = -4426
724944 meter/sec
ZDOT = -19566
291225 ZDOT = -5973
011657
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21506469
46 X = 6555171
89
Y = -5538448
47 feet Y = -1688119
09 meter
Z = -1906853
12 Z = -581208
83
XDOT = 1892
481436 XDOT = 576
828342
YDOT = 14001
415353 feet/sec YDOT = 4267
631399 meter/sec
ZDOT = -19604
655028 ZDOT = -5975
498853
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
48317942
00016717 00000-0 10270-3 0 9005
2 25544 51
6466 327
4331 0001833 121
8398 238
2932 15
50592139 26737
Satellite: ISS
Catalog Number: 25544
Epoch time: 14267
48317942 = yrday
fracday
Element set: 900
Inclination: 51
6466 deg
RA of node: 327
4331 deg
Eccentricity:
0001833
Arg of perigee: 121
8398 deg
Mean anomaly: 238
2932 deg
Mean motion: 15
50592139 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2673
Checksum: 316
Coasting Arc #2 (Orbit 2688)
---------------------------------------
Vector Time (GMT): 2014/268/10:50:55
526
Vector Time (MET): N/A
Weight (LBS) : 932484
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5769243
51 A = 6799049
15 meter
Y = -3423850
63 meter E =
0014514
Z = 1065877
44 I = 51
44625
XDOT = 1658
687941 Wp = 62
83748
YDOT = 4639
492152 meter/sec RA = 322
03787 deg
ZDOT = 5869
969844 TA = 308
73736
MA = 308
86701
Ha = 227
101 n
mi
Hp = 219
590
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18927964
29 X = 5801923
27
Y = -11233105
73 feet Y = -3359152
33 meter
Z = 3496973
24 Z = 1093983
79
XDOT = 5441
889571 XDOT = 1578
170054
YDOT = 15221
430944 feet/sec YDOT = 4657
591338 meter/sec
ZDOT = 19258
431247 ZDOT = 5877
831343
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21052179
08 X = -6416704
18
Y = 6356233
77 feet Y = 1937380
05 meter
Z = 3617093
65 Z = 1102490
14
XDOT = -1039
587035 XDOT = -316
866128
YDOT = -14520
688563 feet/sec YDOT = -4425
905874 meter/sec
ZDOT = 19291
036508 ZDOT = 5879
907928
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
51434380
00016717 00000-0 10270-3 0 9017
2 25544 51
6468 322
3198 0001763 119
5714 240
5613 15
50615905 26898
Satellite: ISS
Catalog Number: 25544
Epoch time: 14268
51434380 = yrday
fracday
Element set: 901
Inclination: 51
6468 deg
RA of node: 322
3198 deg
Eccentricity:
0001763
Arg of perigee: 119
5714 deg
Mean anomaly: 240
5613 deg
Mean motion: 15
50615905 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2689
Checksum: 309
Coasting Arc #3 (Orbit 2703)
---------------------------------------
Vector Time (GMT): 2014/269/10:50:55
526
Vector Time (MET): N/A
Weight (LBS) : 932484
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5620414
46 A = 6798248
92 meter
Y = 3454042
56 meter E =
0009489
Z = -1628744
11 I = 51
41908
XDOT = -1382
680835 Wp = 137
85935
YDOT = -4926
155039 meter/sec RA = 317
06791 deg
ZDOT = -5701
734802 TA = 59
99655
MA = 59
90242
Ha = 226
999 n
mi
Hp = 219
520
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18439679
99 X = -5650708
62
Y = 11332160
62 feet Y = 3391021
84 meter
Z = -5343648
67 Z = -1656121
72
XDOT = -4536
354447 XDOT = -1299
795093
YDOT = -16161
925981 feet/sec YDOT = -4941
154408 meter/sec
ZDOT = -18706
479008 ZDOT = -5708
249762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20474628
18 X = 6240666
67
Y = -6925673
82 feet Y = -2110945
38 meter
Z = -5460667
24 Z = -1664411
38
XDOT = 184
409254 XDOT = 56
207941
YDOT = 15249
323864 feet/sec YDOT = 4647
993914 meter/sec
ZDOT = -18733
309030 ZDOT = -5709
912592
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
48103988
00016717 00000-0 10270-3 0 9022
2 25544 51
6458 317
5260 0001807 121
8427 238
2900 15
50662810 27047
Satellite: ISS
Catalog Number: 25544
Epoch time: 14269
48103988 = yrday
fracday
Element set: 902
Inclination: 51
6458 deg
RA of node: 317
5260 deg
Eccentricity:
0001807
Arg of perigee: 121
8427 deg
Mean anomaly: 238
2900 deg
Mean motion: 15
50662810 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2704
Checksum: 303
Coasting Arc #4 (Orbit 2719)
---------------------------------------
Vector Time (GMT): 2014/270/10:50:55
526
Vector Time (MET): N/A
Weight (LBS) : 932484
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5434284
97 A = 6797357
76 meter
Y = -3463729
46 meter E =
0015073
Z = 2142215
44 I = 51
39406
XDOT = 1165
443201 Wp = 75
66656
YDOT = 5233
753162 meter/sec RA = 312
09502 deg
ZDOT = 5477
183427 TA = 308
14109
MA = 308
27684
Ha = 226
964 n
mi
Hp = 219
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17829018
93 X = 5462206
95
Y = -11363941
79 feet Y = -3402803
38 meter
Z = 7028265
89 Z = 2168683
08
XDOT = 3823
632549 XDOT = 1080
224734
YDOT = 17171
106176 feet/sec YDOT = 5246
310084 meter/sec
ZDOT = 17969
761900 ZDOT = 5482
637444
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19751206
71 X = -6020167
80
Y = 7436376
72 feet Y = 2266607
62 meter
Z = 7141410
58 Z = 2176701
95
XDOT = 466
540720 XDOT = 142
201611
YDOT = -16128
457893 feet/sec YDOT = -4915
953966 meter/sec
ZDOT = 17992
028349 ZDOT = 5483
970241
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
51216097
00016717 00000-0 10270-3 0 9035
2 25544 51
6458 312
4122 0001796 121
3741 238
7586 15
50686134 27207
Satellite: ISS
Catalog Number: 25544
Epoch time: 14270
51216097 = yrday
fracday
Element set: 903
Inclination: 51
6458 deg
RA of node: 312
4122 deg
Eccentricity:
0001796
Arg of perigee: 121
3741 deg
Mean anomaly: 238
7586 deg
Mean motion: 15
50686134 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2720
Checksum: 296
Coasting Arc #5 (Orbit 2734)
---------------------------------------
Vector Time (GMT): 2014/271/10:50:55
526
Vector Time (MET): N/A
Weight (LBS) : 932484
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5247967
97 A = 6796105
18 meter
Y = 3385572
61 meter E =
0006693
Z = -2679730
82 I = 51
37011
XDOT = -962
145071 Wp = 122
89005
YDOT = -5570
748510 meter/sec RA = 307
11953 deg
ZDOT = -5166
812562 TA = 87
42537
MA = 87
34875
Ha = 226
893 n
mi
Hp = 219
372
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17217742
70 X = -5272418
71
Y = 11107521
69 feet Y = 3326749
44 meter
Z = -8791767
77 Z = -2705284
85
XDOT = -3156
643933 XDOT = -874
681047
YDOT = -18276
733958 feet/sec YDOT = -5581
019343 meter/sec
ZDOT = -16951
484785 ZDOT = -5171
273569
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18960566
93 X = 5779180
80
Y = -7641453
42 feet Y = -2329115
00 meter
Z = -8901009
68 Z = -2713027
75
XDOT = -1037
996316 XDOT = -316
381277
YDOT = 17142
008532 feet/sec YDOT = 5224
884200 meter/sec
ZDOT = -16969
472612 ZDOT = -5172
295252
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 14271
47881667
00016717 00000-0 10270-3 0 9043
2 25544 51
6457 307
6177 0001828 122
2426 237
8902 15
50733658 27350
Satellite: ISS
Catalog Number: 25544
Epoch time: 14271
47881667 = yrday
fracday
Element set: 904
Inclination: 51
6457 deg
RA of node: 307
6177 deg
Eccentricity:
0001828
Arg of perigee: 122
2426 deg
Mean anomaly: 237
8902 deg
Mean motion: 15
50733658 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2735
Checksum: 327
Coasting Arc #6 (Orbit 2750)
---------------------------------------
Vector Time (GMT): 2014/272/10:50:55
526
Vector Time (MET): N/A
Weight (LBS) : 932484
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5039491
92 A = 6794859
43 meter
Y = -3276678
26 meter E =
0014371
Z = 3155700
76 I = 51
34768
XDOT = 823
843575 Wp = 90
27077
YDOT = 5914
476464 meter/sec RA = 302
14157 deg
ZDOT = 4806
484281 TA = 306
25600
MA = 306
38870
Ha = 226
840 n
mi
Hp = 219
355
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16533766
13 X = 5060428
33
Y = -10750256
75 feet Y = -3220206
05 meter
Z = 10353348
96 Z = 3180233
41
XDOT = 2702
898868 XDOT = 734
296598
YDOT = 19404
450342 feet/sec YDOT = 5923
188962 meter/sec
ZDOT = 15769
305385 ZDOT = 4810
268418
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18081099
89 X = -5511119
25
Y = 7734637
11 feet Y = 2357517
39 meter
Z = 10458226
08 Z = 3187667
31
XDOT = 1360
920976 XDOT = 414
808714
YDOT = -18244
948237 feet/sec YDOT = -5561
060223 meter/sec
ZDOT = 15784
359277 ZDOT = 4811
072708
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 14272
50989417
00016717 00000-0 10270-3 0 9051
2 25544 51
6454 302
5036 0001863 122
6879 237
4452 15
50756541 27510
Satellite: ISS
Catalog Number: 25544
Epoch time: 14272
50989417 = yrday
fracday
Element set: 905
Inclination: 51
6454 deg
RA of node: 302
5036 deg
Eccentricity:
0001863
Arg of perigee: 122
6879 deg
Mean anomaly: 237
4452 deg
Mean motion: 15
50756541 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2751
Checksum: 315
Coasting Arc #7 (Orbit 2765)
---------------------------------------
Vector Time (GMT): 2014/273/10:50:55
526
Vector Time (MET): N/A
Weight (LBS) : 932484
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4848878
69 A = 6793342
32 meter
Y = 3075746
91 meter E =
0007018
Z = -3636113
63 I = 51
32816
XDOT = -708
028265 Wp = 90
85212
YDOT = -6256
694322 meter/sec RA = 297
16078 deg
ZDOT = -4355
706833 TA = 132
40246
MA = 132
34305
Ha = 226
796 n
mi
Hp = 219
231
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15908394
67 X = -4865248
74
Y = 10091033
18 feet Y = 3021431
80 meter
Z = -11929506
66 Z = -3659709
09
XDOT = -2322
927380 XDOT = -616
852957
YDOT = -20527
212343 feet/sec YDOT = -6264
102505 meter/sec
ZDOT = -14290
376750 ZDOT = -4358
924422
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17214874
80 X = 5247093
84
Y = -7492501
42 feet Y = -2283714
43 meter
Z = -12030361
96 Z = -3666854
33
XDOT = -1548
119620 XDOT = -471
866860
YDOT = 19369
871726 feet/sec YDOT = 5903
936902 meter/sec
ZDOT = -14302
968332 ZDOT = -4359
544748
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 14273
47650877
00016717 00000-0 10270-3 0 9064
2 25544 51
6463 297
7089 0001873 124
4939 235
6389 15
50802113 27663
Satellite: ISS
Catalog Number: 25544
Epoch time: 14273
47650877 = yrday
fracday
Element set: 906
Inclination: 51
6463 deg
RA of node: 297
7089 deg
Eccentricity:
0001873
Arg of perigee: 124
4939 deg
Mean anomaly: 235
6389 deg
Mean motion: 15
50802113 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2766
Checksum: 341
Coasting Arc #8 (Orbit 2781)
---------------------------------------
Vector Time (GMT): 2014/274/10:50:55
526
Vector Time (MET): N/A
Weight (LBS) : 932484
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4653939
00 A = 6791935
21 meter
Y = -2839677
18 meter E =
0012448
Z = 4042654
80 I = 51
30929
XDOT = 654
226780 Wp = 105
66874
YDOT = 6589
658157 meter/sec RA = 292
17777 deg
ZDOT = 3862
352571 TA = 304
07021
MA = 304
18831
Ha = 226
713 n
mi
Hp = 219
247
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15268828
73 X = 4665708
94
Y = -9316526
17 feet Y = -2787567
71 meter
Z = 13263303
16 Z = 4065291
98
XDOT = 2146
413320 XDOT = 561
728841
YDOT = 21619
613375 feet/sec YDOT = 6596
457249 meter/sec
ZDOT = 12671
760402 ZDOT = 3865
305570
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16333954
60 X = -4978589
36
Y = 7110641
43 feet Y = 2167323
51 meter
Z = 13360041
43 Z = 4072140
63
XDOT = 1482
104974 XDOT = 451
745596
YDOT = -20506
761103 feet/sec YDOT = -6250
460784 meter/sec
ZDOT = 12683
178019 ZDOT = 3865
832660
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 14274
50754198
00016717 00000-0 10270-3 0 9071
2 25544 51
6453 292
5947 0001931 124
8337 235
2996 15
50827075 27821
Satellite: ISS
Catalog Number: 25544
Epoch time: 14274
50754198 = yrday
fracday
Element set: 907
Inclination: 51
6453 deg
RA of node: 292
5947 deg
Eccentricity:
0001931
Arg of perigee: 124
8337 deg
Mean anomaly: 235
2996 deg
Mean motion: 15
50827075 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2782
Checksum: 336
Coasting Arc #9 (Orbit 2796)
---------------------------------------
Vector Time (GMT): 2014/275/10:50:55
526
Vector Time (MET): N/A
Weight (LBS) : 932484
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4496487
48 A = 6790440
10 meter
Y = 2516909
66 meter E =
0010375
Z = -4432354
82 I = 51
29489
XDOT = -622
978199 Wp = 78
37630
YDOT = -6886
334124 meter/sec RA = 287
19219 deg
ZDOT = -3282
913731 TA = 158
30541
MA = 158
26144
Ha = 226
688 n
mi
Hp = 219
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14752255
51 X = -4502766
88
Y = 8257577
64 feet Y = 2466591
56 meter
Z = -14541846
51 Z = -4454213
69
XDOT = -2043
891730 XDOT = -529
979889
YDOT = -22592
959724 feet/sec YDOT = -6892
780953 meter/sec
ZDOT = -10770
714342 ZDOT = -3285
713640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15559153
25 X = 4742429
91
Y = -6403519
99 feet Y = -1951792
89 meter
Z = -14635218
24 Z = -4460814
52
XDOT = -1265
921168 XDOT = -385
852772
YDOT = 21531
457619 feet/sec YDOT = 6562
788282 meter/sec
ZDOT = -10781
441529 ZDOT = -3286
183378
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 14275
47411434
00016717 00000-0 10270-3 0 9082
2 25544 51
6464 287
8001 0001894 128
9619 231
1701 15
50866634 27976
Satellite: ISS
Catalog Number: 25544
Epoch time: 14275
47411434 = yrday
fracday
Element set: 908
Inclination: 51
6464 deg
RA of node: 287
8001 deg
Eccentricity:
0001894
Arg of perigee: 128
9619 deg
Mean anomaly: 231
1701 deg
Mean motion: 15
50866634 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2797
Checksum: 322
Coasting Arc #10 (Orbit 2812)
---------------------------------------
Vector Time (GMT): 2014/276/10:50:55
526
Vector Time (MET): N/A
Weight (LBS) : 932484
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4352214
88 A = 6789138
71 meter
Y = -2161274
98 meter E =
0009518
Z = 4736160
08 I = 51
28092
XDOT = 640
890339 Wp = 120
08488
YDOT = 7158
178618 meter/sec RA = 282
20423 deg
ZDOT = 2668
864716 TA = 303
37015
MA = 303
46121
Ha = 226
562 n
mi
Hp = 219
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14278920
22 X = 4353052
47
Y = -7090797
17 feet Y = -2112600
55 meter
Z = 15538582
95 Z = 4757304
84
XDOT = 2102
658593 XDOT = 547
833767
YDOT = 23484
837986 feet/sec YDOT = 7164
825416 meter/sec
ZDOT = 8756
117835 ZDOT = 2671
751364
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14847140
31 X = -4525408
37
Y = 5560199
92 feet Y = 1694748
94 meter
Z = 15628855
64 Z = 4763675
20
XDOT = 837
053687 XDOT = 255
133964
YDOT = -22488
045138 feet/sec YDOT = -6854
356158 meter/sec
ZDOT = 8767
181570 ZDOT = 2672
236943
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 14276
50510199
00016717 00000-0 10270-3 0 9096
2 25544 51
6448 282
6854 0001949 128
8490 231
2835 15
50898022 28138
Satellite: ISS
Catalog Number: 25544
Epoch time: 14276
50510199 = yrday
fracday
Element set: 909
Inclination: 51
6448 deg
RA of node: 282
6854 deg
Eccentricity:
0001949
Arg of perigee: 128
8490 deg
Mean anomaly: 231
2835 deg
Mean motion: 15
50898022 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2813
Checksum: 328
Coasting Arc #11 (Orbit 2827)
---------------------------------------
Vector Time (GMT): 2014/277/10:50:55
526
Vector Time (MET): N/A
Weight (LBS) : 932484
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4262909
17 A = 6787995
60 meter
Y = 1735058
21 meter E =
0013847
Z = -5001927
85 I = 51
27235
XDOT = -671
671304 Wp = 81
87912
YDOT = -7360
466511 meter/sec RA = 277
21447 deg
ZDOT = -1983
566869 TA = 168
73067
MA = 168
69963
Ha = 226
559 n
mi
Hp = 219
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13985922
48 X = -4257696
34
Y = 5692448
18 feet Y = 1687416
16 meter
Z = -16410524
45 Z = -5022624
06
XDOT = -2203
646011 XDOT = -579
679385
YDOT = -24148
512176 feet/sec YDOT = -7367
463447 meter/sec
ZDOT = -6507
765318 ZDOT = -1986
605470
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14328974
58 X = 4367471
45
Y = -4448018
28 feet Y = -1355755
97 meter
Z = -16498815
95 Z = -5028839
10
XDOT = -294
089684 XDOT = -89
638536
YDOT = 23200
804475 feet/sec YDOT = 7071
605204 meter/sec
ZDOT = -6519
456697 ZDOT = -1987
130401
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 14277
47163074
00016717 00000-0 10270-3 0 9101
2 25544 51
6455 277
8907 0001873 134
7921 225
3383 15
50928344 28281
Satellite: ISS
Catalog Number: 25544
Epoch time: 14277
47163074 = yrday
fracday
Element set: 910
Inclination: 51
6455 deg
RA of node: 277
8907 deg
Eccentricity:
0001873
Arg of perigee: 134
7921 deg
Mean anomaly: 225
3383 deg
Mean motion: 15
50928344 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2828
Checksum: 326
Coasting Arc #12 (Orbit 2843)
---------------------------------------
Vector Time (GMT): 2014/278/10:50:55
526
Vector Time (MET): N/A
Weight (LBS) : 932484
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4200487
07 A = 6787098
53 meter
Y = -1284754
42 meter E =
0006077
Z = 5170491
08 I = 51
26515
XDOT = 729
473862 Wp = 127
63253
YDOT = 7524
880997 meter/sec RA = 272
22227 deg
ZDOT = 1272
469851 TA = 310
05558
MA = 310
10887
Ha = 226
379 n
mi
Hp = 219
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13781125
55 X = 4189424
60
Y = -4215073
56 feet Y = -1237843
02 meter
Z = 16963553
41 Z = 5190869
84
XDOT = 2393
286949 XDOT = 639
093406
YDOT = 24687
929781 feet/sec YDOT = 7532
533270 meter/sec
ZDOT = 4174
769852 ZDOT = 1275
793014
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13937978
58 X = -4248295
87
Y = 3234872
78 feet Y = 985989
22 meter
Z = 17050418
23 Z = 5196967
48
XDOT = -377
074131 XDOT = -114
932195
YDOT = -23777
540804 feet/sec YDOT = -7247
394437 meter/sec
ZDOT = 4187
659596 ZDOT = 1276
398645
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 14278
50257118
00016717 00000-0 10270-3 0 9110
2 25544 51
6439 272
7751 0001902 134
9348 225
1957 15
50969809 28446
Satellite: ISS
Catalog Number: 25544
Epoch time: 14278
50257118 = yrday
fracday
Element set: 911
Inclination: 51
6439 deg
RA of node: 272
7751 deg
Eccentricity:
0001902
Arg of perigee: 134
9348 deg
Mean anomaly: 225
1957 deg
Mean motion: 15
50969809 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2844
Checksum: 330
Coasting Arc #13 (Orbit 2858)
---------------------------------------
Vector Time (GMT): 2014/279/10:50:55
526
Vector Time (MET): N/A
Weight (LBS) : 932484
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4204201
22 A = 6786597
57 meter
Y = 790177
04 meter E =
0015832
Z = -5282355
14 I = 51
26358
XDOT = -781
623775 Wp = 91
39575
YDOT = -7594
217619 meter/sec RA = 267
22952 deg
ZDOT = -515
637942 TA = 173
65822
MA = 173
63816
Ha = 226
413 n
mi
Hp = 219
001
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13793311
08 X = -4187064
50
Y = 2592444
36 feet Y = 743257
99 meter
Z = -17330561
50 Z = -5302737
22
XDOT = -2564
382463 XDOT = -694
140558
YDOT = -24915
412136 feet/sec YDOT = -7602
469170 meter/sec
ZDOT = -1691
725532 ZDOT = -519
221398
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13803098
03 X = 4207184
28
Y = -1853292
65 feet Y = -564883
60 meter
Z = -17417357
76 Z = -5308810
65
XDOT = 1078
498610 XDOT = 328
726376
YDOT = 24010
123207 feet/sec YDOT = 7318
285554 meter/sec
ZDOT = -1705
724950 ZDOT = -519
904965
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 14279
46905496
00016717 00000-0 10270-3 0 9126
2 25544 51
6441 267
9799 0001826 140
8687 219
2596 15
50991065 28592
Satellite: ISS
Catalog Number: 25544
Epoch time: 14279
46905496 = yrday
fracday
Element set: 912
Inclination: 51
6441 deg
RA of node: 267
9799 deg
Eccentricity:
0001826
Arg of perigee: 140
8687 deg
Mean anomaly: 219
2596 deg
Mean motion: 15
50991065 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2859
Checksum: 362
Coasting Arc #14 (Orbit 2874)
---------------------------------------
Vector Time (GMT): 2014/280/10:50:55
526
Vector Time (MET): N/A
Weight (LBS) : 932484
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4241269
95 A = 6786361
36 meter
Y = -285617
60 meter E =
0003675
Z = 5286935
80 I = 51
26479
XDOT = 831
288342 Wp = 104
81992
YDOT = 7617
157229 meter/sec RA = 262
23517 deg
ZDOT = -256
144117 TA = 347
63036
MA = 347
63938
Ha = 226
171 n
mi
Hp = 219
100
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13914927
65 X = 4218466
00
Y = -937065
62 feet Y = -238315
70 meter
Z = 17345589
89 Z = 5307484
20
XDOT = 2727
323958 XDOT = 747
294025
YDOT = 24990
673322 feet/sec YDOT = 7625
983556 meter/sec
ZDOT = -840
367837 ZDOT = -252
310919
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13830275
31 X = -4215467
91
Y = 431740
14 feet Y = 131594
40 meter
Z = 17433011
14 Z = 5313581
79
XDOT = -1788
340195 XDOT = -545
086091
YDOT = -24065
079925 feet/sec YDOT = -7335
036361 meter/sec
ZDOT = -825
298467 ZDOT = -251
550973
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 14280
49994654
00016717 00000-0 10270-3 0 9136
2 25544 51
6431 262
8637 0001814 142
7076 217
4201 15
51043777 28756
Satellite: ISS
Catalog Number: 25544
Epoch time: 14280
49994654 = yrday
fracday
Element set: 913
Inclination: 51
6431 deg
RA of node: 262
8637 deg
Eccentricity:
0001814
Arg of perigee: 142
7076 deg
Mean anomaly: 217
4201 deg
Mean motion: 15
51043777 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2875
Checksum: 316
Coasting Arc #15 (Orbit 2889)
---------------------------------------
Vector Time (GMT): 2014/281/10:50:55
526
Vector Time (MET): N/A
Weight (LBS) : 932484
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4345585
17 A = 6786665
74 meter
Y = -229659
03 meter E =
0015516
Z = -5221574
00 I = 51
27123
XDOT = -851
325971 Wp = 102
96344
YDOT = -7533
048224 meter/sec RA = 257
24170 deg
ZDOT = 1039
036062 TA = 177
06518
MA = 177
05607
Ha = 226
250 n
mi
Hp = 218
959
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14257169
19 X = -4317328
92
Y = -753474
52 feet Y = -278096
91 meter
Z = -17131148
28 Z = -5242615
94
XDOT = -2793
064209 XDOT = -772
073800
YDOT = -24714
725143 feet/sec YDOT = -7542
125034 meter/sec
ZDOT = 3408
910963 ZDOT = 1035
093911
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14131772
75 X = 4307364
33
Y = 1027251
25 feet Y = 313106
18 meter
Z = -17220586
30 Z = -5248834
70
XDOT = 2412
988951 XDOT = 735
479032
YDOT = 23733
542102 feet/sec YDOT = 7233
983633 meter/sec
ZDOT = 3393
355825 ZDOT = 1034
294856
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 14281
46638408
00016717 00000-0 10270-3 0 9147
2 25544 51
6432 258
0680 0001767 146
7157 213
4105 15
51058735 28909
Satellite: ISS
Catalog Number: 25544
Epoch time: 14281
46638408 = yrday
fracday
Element set: 914
Inclination: 51
6432 deg
RA of node: 258
0680 deg
Eccentricity:
0001767
Arg of perigee: 146
7157 deg
Mean anomaly: 213
4105 deg
Mean motion: 15
51058735 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2890
Checksum: 310
Coasting Arc #16 (Orbit 2893)
---------------------------------------
Vector Time (GMT): 2014/281/17:05:56
803
Vector Time (MET): N/A
Weight (LBS) : 932179
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4434939
99 A = 6790061
39 meter
Y = -1872092
52 meter E =
0010277
Z = -4798575
29 I = 51
28223
XDOT = 293
745981 Wp = 114
93201
YDOT = -7213
272941 meter/sec RA = 255
93113 deg
ZDOT = 2542
716940 TA = 180
26780
MA = 180
26835
Ha = 226
137 n
mi
Hp = 220
805
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14550328
07 X = -4390365
84
Y = -6142035
83 feet Y = -1921438
31 meter
Z = -15743357
24 Z = -4820011
47
XDOT = 963
733534 XDOT = 362
032707
YDOT = -23665
593639 feet/sec YDOT = -7209
605927 meter/sec
ZDOT = 8342
247180 ZDOT = 2544
310782
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5402179
34 X = 1646584
26
Y = -14743955
44 feet Y = -4493957
62 meter
Z = -15834209
31 Z = -4826267
00
XDOT = 22605
480580 XDOT = 6890
150481
YDOT = -684
818468 feet/sec YDOT = -208
732669 meter/sec
ZDOT = 8350
179236 ZDOT = 2545
134631
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 14281
72409761
00016717 00000-0 10270-3 0 9155
2 25544 51
6464 256
7882 0001762 244
6718 115
4250 15
50508028 28949
Satellite: ISS
Catalog Number: 25544
Epoch time: 14281
72409761 = yrday
fracday
Element set: 915
Inclination: 51
6464 deg
RA of node: 256
7882 deg
Eccentricity:
0001762
Arg of perigee: 244
6718 deg
Mean anomaly: 115
4250 deg
Mean motion: 15
50508028 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2894
Checksum: 318
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