[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 30th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16684 06 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
281/17:02:31
522 -0
7 3
1 3
2
N/A -3
0 -0
5 226
3
000/00:07:03
044 0
8 0
1 221
1
Coasting Arc #1 (Orbit 2750)
---------------------------------------
Vector Time (GMT): 2014/272/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -972272
76 A = 6791109
73 meter
Y = -5095914
13 meter E =
0010759
Z = -4393485
99 I = 51
33412
XDOT = 5622
801933 Wp = 112
37966
YDOT = -3962
647236 meter/sec RA = 301
85860 deg
ZDOT = 3354
473312 TA = 191
75771
MA = 191
78285
Ha = 226
969 n
mi
Hp = 219
407
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3189871
25 X = -893874
35
Y = -16718878
37 feet Y = -5106348
75 meter
Z = -14414324
11 Z = -4398018
34
XDOT = 18447
512903 XDOT = 5650
400075
YDOT = -13000
811142 feet/sec YDOT = -3899
614816 meter/sec
ZDOT = 11005
489870 ZDOT = 3381
855878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5210304
57 X = 1588100
83
Y = 16186992
70 feet Y = 4933795
37 meter
Z = -14432702
65 Z = -4399087
77
XDOT = -15385
463002 XDOT = -4689
489123
YDOT = 14861
887838 feet/sec YDOT = 4529
903413 meter/sec
ZDOT = 11122
603595 ZDOT = 3390
169576
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
50997117
00016717 00000-0 10270-3 0 9002
2 25544 51
6457 302
5077 0001867 122
7816 237
3515 15
50717336 27512
Satellite: ISS
Catalog Number: 25544
Epoch time: 14272
50997117 = yrday
fracday
Element set: 900
Inclination: 51
6457 deg
RA of node: 302
5077 deg
Eccentricity:
0001867
Arg of perigee: 122
7816 deg
Mean anomaly: 237
3515 deg
Mean motion: 15
50717336 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2751
Checksum: 308
Coasting Arc #2 (Orbit 2766)
---------------------------------------
Vector Time (GMT): 2014/273/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 873008
40 A = 6792253
34 meter
Y = 5397216
38 meter E =
0012161
Z = 4020530
76 I = 51
32163
XDOT = -5412
724601 Wp = 84
61002
YDOT = 3784
644992 meter/sec RA = 296
87570 deg
ZDOT = -3893
937591 TA = 46
02471
MA = 45
92449
Ha = 226
844 n
mi
Hp = 219
370
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2864200
79 X = 793059
91
Y = 17707402
81 feet Y = 5406532
22 meter
Z = 13190717
71 Z = 4024577
15
XDOT = -17758
282811 XDOT = -5435
727362
YDOT = 12416
814277 feet/sec YDOT = 3723
987480 meter/sec
ZDOT = -12775
385796 ZDOT = -3920
288328
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5316522
45 X = -1620476
04
Y = -17119024
02 feet Y = -5217878
52 meter
Z = 13206983
00 Z = 4025488
42
XDOT = 14444
486796 XDOT = 4402
679575
YDOT = -14457
413703 feet/sec YDOT = -4406
619697 meter/sec
ZDOT = -12888
078781 ZDOT = -3928
286412
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
54105683
00016717 00000-0 10270-3 0 9017
2 25544 51
6446 297
3936 0001873 124
7296 235
4032 15
50771928 27673
Satellite: ISS
Catalog Number: 25544
Epoch time: 14273
54105683 = yrday
fracday
Element set: 901
Inclination: 51
6446 deg
RA of node: 297
3936 deg
Eccentricity:
0001873
Arg of perigee: 124
7296 deg
Mean anomaly: 235
4032 deg
Mean motion: 15
50771928 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2767
Checksum: 324
Coasting Arc #3 (Orbit 2781)
---------------------------------------
Vector Time (GMT): 2014/274/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -838659
80 A = 6793539
72 meter
Y = -5690983
30 meter E =
0007152
Z = -3621848
42 I = 51
31376
XDOT = 5193
430260 Wp = 105
37984
YDOT = -3542
107056 meter/sec RA = 291
89323 deg
ZDOT = 4368
501305 TA = 211
57478
MA = 211
61771
Ha = 226
866 n
mi
Hp = 219
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2751508
52 X = -757365
65
Y = -18671205
06 feet Y = -5699907
47 meter
Z = -11882704
77 Z = -3625724
65
XDOT = 17038
813188 XDOT = 5211
431972
YDOT = -11621
086142 feet/sec YDOT = -3483
929774 meter/sec
ZDOT = 14332
353363 ZDOT = 4393
774464
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5663086
74 X = 1726108
84
Y = 17992931
22 feet Y = 5484245
44 meter
Z = -11898203
45 Z = -3626572
41
XDOT = -13532
223767 XDOT = -4124
621804
YDOT = 13796
492145 feet/sec YDOT = 4205
170806 meter/sec
ZDOT = 14440
420277 ZDOT = 4401
440101
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
50768561
00016717 00000-0 10270-3 0 9025
2 25544 51
6456 292
5995 0001908 126
7421 233
3905 15
50777460 27827
Satellite: ISS
Catalog Number: 25544
Epoch time: 14274
50768561 = yrday
fracday
Element set: 902
Inclination: 51
6456 deg
RA of node: 292
5995 deg
Eccentricity:
0001908
Arg of perigee: 126
7421 deg
Mean anomaly: 233
3905 deg
Mean motion: 15
50777460 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2782
Checksum: 326
Coasting Arc #4 (Orbit 2797)
---------------------------------------
Vector Time (GMT): 2014/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 814831
80 A = 6794796
50 meter
Y = 5963110
28 meter E =
0014478
Z = 3138825
13 I = 51
30605
XDOT = -5014
678762 Wp = 98
56003
YDOT = 3229
765963 meter/sec RA = 286
91045 deg
ZDOT = -4817
091456 TA = 45
10769
MA = 44
99025
Ha = 226
749 n
mi
Hp = 219
326
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2673332
67 X = 732842
87
Y = 19564010
10 feet Y = 5971764
09 meter
Z = 10297982
72 Z = 3142583
86
XDOT = -16452
358144 XDOT = -5027
022041
YDOT = 10596
345024 feet/sec YDOT = 3173
619169 meter/sec
ZDOT = -15804
105826 ZDOT = -4841
482431
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6064251
69 X = -1848383
92
Y = -18783334
65 feet Y = -5725160
40 meter
Z = 10312945
16 Z = 3143385
68
XDOT = 12825
075033 XDOT = 3909
082870
YDOT = -12905
618374 feet/sec YDOT = -3933
632480 meter/sec
ZDOT = -15908
365402 ZDOT = -4848
869774
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
53873898
00016717 00000-0 10270-3 0 9030
2 25544 51
6441 287
4849 0001853 128
5268 231
6049 15
50817910 27982
Satellite: ISS
Catalog Number: 25544
Epoch time: 14275
53873898 = yrday
fracday
Element set: 903
Inclination: 51
6441 deg
RA of node: 287
4849 deg
Eccentricity:
0001853
Arg of perigee: 128
5268 deg
Mean anomaly: 231
6049 deg
Mean motion: 15
50817910 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2798
Checksum: 346
Coasting Arc #5 (Orbit 2812)
---------------------------------------
Vector Time (GMT): 2014/276/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -852090
36 A = 6795947
59 meter
Y = -6204268
35 meter E =
0005712
Z = -2641550
01 I = 51
30227
XDOT = 4850
816269 Wp = 73
18565
YDOT = -2868
826777 meter/sec RA = 281
92901 deg
ZDOT = 5184
304860 TA = 256
94843
MA = 257
01220
Ha = 226
742 n
mi
Hp = 219
281
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2795572
05 X = -769817
62
Y = -20355211
11 feet Y = -6213337
21 meter
Z = -8666502
64 Z = -2645488
92
XDOT = 15914
751538 XDOT = 4857
351860
YDOT = -9412
161342 feet/sec YDOT = -2814
544763 meter/sec
ZDOT = 17008
874214 ZDOT = 5207
885666
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6671201
20 X = 2033382
13
Y = 19426078
97 feet Y = 5921068
87 meter
Z = -8682202
54 Z = -2646335
33
XDOT = -12243
595534 XDOT = -3731
847919
YDOT = 11835
479337 feet/sec YDOT = 3607
454102 meter/sec
ZDOT = 17109
624327 ZDOT = 5215
013495
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
50533648
00016717 00000-0 10270-3 0 9045
2 25544 51
6444 282
6909 0001932 132
1786 227
9529 15
50839205 28133
Satellite: ISS
Catalog Number: 25544
Epoch time: 14276
50533648 = yrday
fracday
Element set: 904
Inclination: 51
6444 deg
RA of node: 282
6909 deg
Eccentricity:
0001932
Arg of perigee: 132
1786 deg
Mean anomaly: 227
9529 deg
Mean motion: 15
50839205 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2813
Checksum: 322
Coasting Arc #6 (Orbit 2828)
---------------------------------------
Vector Time (GMT): 2014/277/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 886276
44 A = 6797028
73 meter
Y = 6406645
97 meter E =
0015551
Z = 2065263
82 I = 51
29910
XDOT = -4742
327000 Wp = 113
21685
YDOT = 2440
153967 meter/sec RA = 276
94682 deg
ZDOT = -5507
375492 TA = 43
84256
MA = 43
71923
Ha = 226
626 n
mi
Hp = 219
309
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2907731
11 X = 804537
56
Y = 21019179
68 feet Y = 6416100
10 meter
Z = 6775799
93 Z = 2069369
95
XDOT = -15558
815617 XDOT = -4742
507766
YDOT = 8005
754484 feet/sec YDOT = 2387
120543 meter/sec
ZDOT = -18068
817230 ZDOT = -5530
413833
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7266676
39 X = -2214882
96
Y = -19930726
08 feet Y = -6074885
31 meter
Z = 6792190
49 Z = 2070259
66
XDOT = 11937
403117 XDOT = 3638
520470
YDOT = -10573
778182 feet/sec YDOT = -3222
887590 meter/sec
ZDOT = -18167
185104 ZDOT = -5537
358020
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
53635642
00016717 00000-0 10270-3 0 9057
2 25544 51
6430 277
5756 0001774 133
5477 226
5821 15
50863973 28293
Satellite: ISS
Catalog Number: 25544
Epoch time: 14277
53635642 = yrday
fracday
Element set: 905
Inclination: 51
6430 deg
RA of node: 277
5756 deg
Eccentricity:
0001774
Arg of perigee: 133
5477 deg
Mean anomaly: 226
5821 deg
Mean motion: 15
50863973 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2829
Checksum: 334
Coasting Arc #7 (Orbit 2843)
---------------------------------------
Vector Time (GMT): 2014/278/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -969070
44 A = 6797771
49 meter
Y = -6559151
92 meter E =
0008144
Z = -1489727
14 I = 51
29881
XDOT = 4668
505360 Wp = 51
19663
YDOT = -1987
102858 meter/sec RA = 271
96623 deg
ZDOT = 5738
470995 TA = 292
48955
MA = 292
57576
Ha = 226
597 n
mi
Hp = 219
240
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3179364
96 X = -888415
81
Y = -21519527
30 feet Y = -6569537
93 meter
Z = -4887556
25 Z = -1494237
99
XDOT = 15316
618636 XDOT = 4662
502847
YDOT = -6519
366333 feet/sec YDOT = -1934
929399 meter/sec
ZDOT = 18827
004576 ZDOT = 5761
135725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7999100
18 X = 2438125
73
Y = 20224627
51 feet Y = 6164466
47 meter
Z = -4905656
03 Z = -1495243
96
XDOT = -11823
441046 XDOT = -3603
784831
YDOT = 9245
589060 feet/sec YDOT = 2818
055546 meter/sec
ZDOT = 18923
705140 ZDOT = 5767
945327
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
50292171
00016717 00000-0 10270-3 0 9062
2 25544 51
6427 272
7812 0001940 138
8214 221
3083 15
50903187 28443
Satellite: ISS
Catalog Number: 25544
Epoch time: 14278
50292171 = yrday
fracday
Element set: 906
Inclination: 51
6427 deg
RA of node: 272
7812 deg
Eccentricity:
0001940
Arg of perigee: 138
8214 deg
Mean anomaly: 221
3083 deg
Mean motion: 15
50903187 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2844
Checksum: 299
Coasting Arc #8 (Orbit 2859)
---------------------------------------
Vector Time (GMT): 2014/279/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1029130
71 A = 6798397
10 meter
Y = 6659080
78 meter E =
0015016
Z = 845564
13 I = 51
30016
XDOT = -4659
293492 Wp = 127
33637
YDOT = 1477
924274 meter/sec RA = 266
98470 deg
ZDOT = -5904
770484 TA = 43
48324
MA = 43
36492
Ha = 226
495 n
mi
Hp = 219
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3376413
07 X = 950483
32
Y = 21847377
87 feet Y = 6670149
56 meter
Z = 2774160
54 Z = 850371
55
XDOT = -15286
395970 XDOT = -4646
789969
YDOT = 4848
832920 feet/sec YDOT = 1425
890089 meter/sec
ZDOT = -19372
606576 ZDOT = -5927
374706
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8630313
20 X = -2630519
46
Y = -20349889
59 feet Y = -6202646
35 meter
Z = 2793517
39 Z = 851464
10
XDOT = 12021
617223 XDOT = 3664
188929
YDOT = -7799
334078 feet/sec YDOT = -2377
237027 meter/sec
ZDOT = -19468
963625 ZDOT = -5934
140113
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
53390701
00016717 00000-0 10270-3 0 9075
2 25544 51
6420 267
6652 0001684 139
3752 220
7525 15
50910287 28600
Satellite: ISS
Catalog Number: 25544
Epoch time: 14279
53390701 = yrday
fracday
Element set: 907
Inclination: 51
6420 deg
RA of node: 267
6652 deg
Eccentricity:
0001684
Arg of perigee: 139
3752 deg
Mean anomaly: 220
7525 deg
Mean motion: 15
50910287 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2860
Checksum: 309
Coasting Arc #9 (Orbit 2874)
---------------------------------------
Vector Time (GMT): 2014/280/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1118663
49 A = 6798514
32 meter
Y = -6697800
90 meter E =
0011351
Z = -219941
98 I = 51
30333
XDOT = 4696
582950 Wp = 53
13298
YDOT = -973
361315 meter/sec RA = 262
00475 deg
ZDOT = 5975
010325 TA = 304
48982
MA = 304
59697
Ha = 226
427 n
mi
Hp = 219
231
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3670155
80 X = -1042615
56
Y = -21974412
41 feet Y = -6709885
35 meter
Z = -721594
43 Z = -225190
67
XDOT = 15408
736712 XDOT = 4678
093172
YDOT = -3193
442635 feet/sec YDOT = -920
943590 meter/sec
ZDOT = 19603
052246 ZDOT = 5997
781190
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9308305
24 X = 2837171
44
Y = 20240286
51 feet Y = 6169239
33 meter
Z = -742831
54 Z = -226415
05
XDOT = -12434
052130 XDOT = -3789
899089
YDOT = 6415
416465 feet/sec YDOT = 1955
418939 meter/sec
ZDOT = 19700
034655 ZDOT = 6004
570563
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
50043905
00016717 00000-0 10270-3 0 9086
2 25544 51
6417 262
8703 0001903 146
7283 213
3988 15
50965523 28755
Satellite: ISS
Catalog Number: 25544
Epoch time: 14280
50043905 = yrday
fracday
Element set: 908
Inclination: 51
6417 deg
RA of node: 262
8703 deg
Eccentricity:
0001903
Arg of perigee: 146
7283 deg
Mean anomaly: 213
3988 deg
Mean motion: 15
50965523 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2875
Checksum: 315
Coasting Arc #10 (Orbit 2890)
---------------------------------------
Vector Time (GMT): 2014/281/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1161880
70 A = 6798473
24 meter
Y = 6676619
50 meter E =
0012714
Z = -458206
55 I = 51
30886
XDOT = -4798
590810 Wp = 139
22103
YDOT = 433
131801 meter/sec RA = 257
02400 deg
ZDOT = -5959
956092 TA = 45
73704
MA = 45
63277
Ha = 226
355 n
mi
Hp = 219
305
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3811944
55 X = 1089360
70
Y = 21904919
63 feet Y = 6689206
86 meter
Z = -1503302
32 Z = -452739
27
XDOT = -15743
408169 XDOT = -4774
125479
YDOT = 1421
036092 feet/sec YDOT = 379
606823 meter/sec
ZDOT = -19553
661719 ZDOT = -5983
208011
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9785242
53 X = -2982541
92
Y = -19966763
44 feet Y = -6085869
50 meter
Z = -1481124
39 Z = -451446
72
XDOT = 13146
424027 XDOT = 4007
030043
YDOT = -5010
463776 feet/sec YDOT = -1527
189359 meter/sec
ZDOT = -19652
603255 ZDOT = -5990
113472
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
53138858
00016717 00000-0 10270-3 0 9093
2 25544 51
6422 257
7540 0001603 146
5850 213
5403 15
50958466 28918
Satellite: ISS
Catalog Number: 25544
Epoch time: 14281
53138858 = yrday
fracday
Element set: 909
Inclination: 51
6422 deg
RA of node: 257
7540 deg
Eccentricity:
0001603
Arg of perigee: 146
5850 deg
Mean anomaly: 213
5403 deg
Mean motion: 15
50958466 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2891
Checksum: 315
Coasting Arc #11 (Orbit 2893)
---------------------------------------
Vector Time (GMT): 2014/281/17:06:03
044
Vector Time (MET): N/A
Weight (LBS) : 946249
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4442570
30 A = 6790006
17 meter
Y = -1546921
05 meter E =
0010853
Z = -4906617
36 I = 51
27997
XDOT = 42
357060 Wp = 113
62823
YDOT = -7310
249393 meter/sec RA = 255
94189 deg
ZDOT = 2266
102512 TA = 178
67553
MA = 178
67265
Ha = 226
310 n
mi
Hp = 221
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14575361
87 X = -4401106
87
Y = -5075200
30 feet Y = -1596369
58 meter
Z = -16097825
98 Z = -4928098
21
XDOT = 138
966732 XDOT = 113
090612
YDOT = -23983
757852 feet/sec YDOT = -7309
379930 meter/sec
ZDOT = 7434
719526 ZDOT = 2266
481075
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4328895
43 X = 1319447
33
Y = -14714563
04 feet Y = -4484998
81 meter
Z = -16188920
04 Z = -4934382
83
XDOT = 22883
380593 XDOT = 6974
854405
YDOT = -1451
581417 feet/sec YDOT = -442
442016 meter/sec
ZDOT = 7437
499484 ZDOT = 2266
949843
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
72468999
00016717 00000-0 10270-3 0 9108
2 25544 51
6457 256
7948 0001932 243
1739 116
9214 15
50375526 28941
Satellite: ISS
Catalog Number: 25544
Epoch time: 14281
72468999 = yrday
fracday
Element set: 910
Inclination: 51
6457 deg
RA of node: 256
7948 deg
Eccentricity:
0001932
Arg of perigee: 243
1739 deg
Mean anomaly: 116
9214 deg
Mean motion: 15
50375526 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2894
Checksum: 343
Coasting Arc #12 (Orbit 2909)
---------------------------------------
Vector Time (GMT): 2014/282/17:06:03
044
Vector Time (MET): N/A
Weight (LBS) : 946249
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4582156
42 A = 6790654
90 meter
Y = 1731439
45 meter E =
0005866
Z = 4699906
37 I = 51
29128
XDOT = 131
006099 Wp = 60
91688
YDOT = 7149
952999 meter/sec RA = 250
95784 deg
ZDOT = -2756
340631 TA = 56
55576
MA = 56
49968
Ha = 226
036 n
mi
Hp = 221
147
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15033321
59 X = 4539623
39
Y = 5680575
61 feet Y = 1782442
82 meter
Z = 15419640
32 Z = 4722062
79
XDOT = 429
810036 XDOT = 64
433632
YDOT = 23457
851048 feet/sec YDOT = 7151
045442 meter/sec
ZDOT = -9043
112305 ZDOT = -2755
866752
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4647447
20 X = -1416541
91
Y = 15289375
84 feet Y = 4660201
75 meter
Z = 15513581
99 Z = 4728539
79
XDOT = -22253
986306 XDOT = -6783
015026
YDOT = 2428
305539 feet/sec YDOT = 740
147528 meter/sec
ZDOT = -9042
236188 ZDOT = -2756
073590
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 14282
75600769
00016717 00000-0 10270-3 0 9116
2 25544 51
6458 251
6825 0001955 249
3044 110
7898 15
50429996 29102
Satellite: ISS
Catalog Number: 25544
Epoch time: 14282
75600769 = yrday
fracday
Element set: 911
Inclination: 51
6458 deg
RA of node: 251
6825 deg
Eccentricity:
0001955
Arg of perigee: 249
3044 deg
Mean anomaly: 110
7898 deg
Mean motion: 15
50429996 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2910
Checksum: 332
Coasting Arc #13 (Orbit 2924)
---------------------------------------
Vector Time (GMT): 2014/283/17:06:03
044
Vector Time (MET): N/A
Weight (LBS) : 946249
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4760715
83 A = 6791574
13 meter
Y = -1890339
48 meter E =
0008014
Z = -4467832
59 I = 51
30603
XDOT = -267
788117 Wp = 119
49224
YDOT = -6938
731917 meter/sec RA = 245
97462 deg
ZDOT = 3221
630308 TA = 183
13602
MA = 183
14105
Ha = 226
131 n
mi
Hp = 221
052
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15619146
44 X = -4717520
02
Y = -6201901
17 feet Y = -1943335
80 meter
Z = -14658243
41 Z = -4490854
87
XDOT = -878
569937 XDOT = -205
827691
YDOT = -22764
868495 feet/sec YDOT = -6941
379742 meter/sec
ZDOT = 10569
653240 ZDOT = 3220
480581
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4852607
00 X = 1479074
61
Y = -16000080
12 feet Y = -4876824
42 meter
Z = -14755848
16 Z = -4497582
52
XDOT = 21432
985889 XDOT = 6532
774099
YDOT = -3242
350425 feet/sec YDOT = -988
268410 meter/sec
ZDOT = 10565
864802 ZDOT = 3220
475592
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 14283
72285202
00016717 00000-0 10270-3 0 9126
2 25544 51
6464 246
8892 0002000 252
3309 107
7623 15
50431136 29256
Satellite: ISS
Catalog Number: 25544
Epoch time: 14283
72285202 = yrday
fracday
Element set: 912
Inclination: 51
6464 deg
RA of node: 246
8892 deg
Eccentricity:
0002000
Arg of perigee: 252
3309 deg
Mean anomaly: 107
7623 deg
Mean motion: 15
50431136 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2925
Checksum: 286
Coasting Arc #14 (Orbit 2940)
---------------------------------------
Vector Time (GMT): 2014/284/17:06:03
044
Vector Time (MET): N/A
Weight (LBS) : 946249
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4950919
09 A = 6792462
42 meter
Y = 2036604
12 meter E =
0008189
Z = 4175360
13 I = 51
32318
XDOT = 351
281621 Wp = 74
12525
YDOT = 6712
392925 meter/sec RA = 240
99337 deg
ZDOT = -3682
374992 TA = 53
89678
MA = 53
82098
Ha = 225
906 n
mi
Hp = 221
092
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16243172
86 X = 4907494
37
Y = 6681772
05 feet Y = 2091726
04 meter
Z = 13698688
09 Z = 4199305
84
XDOT = 1152
498756 XDOT = 294
084139
YDOT = 22022
286499 feet/sec YDOT = 6716
001081 meter/sec
ZDOT = -12081
282781 ZDOT = -3680
807946
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4989250
56 X = -1520723
57
Y = 16757162
91 feet Y = 5107583
25 meter
Z = 13800205
35 Z = 4206302
59
XDOT = -20556
862023 XDOT = -6265
731545
YDOT = 3846
350582 feet/sec YDOT = 1172
367657 meter/sec
ZDOT = -12075
678869 ZDOT = -3680
666919
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 14284
75413322
00016717 00000-0 10270-3 0 9137
2 25544 51
6465 241
7769 0001984 258
2346 101
8583 15
50486764 29415
Satellite: ISS
Catalog Number: 25544
Epoch time: 14284
75413322 = yrday
fracday
Element set: 913
Inclination: 51
6465 deg
RA of node: 241
7769 deg
Eccentricity:
0001984
Arg of perigee: 258
2346 deg
Mean anomaly: 101
8583 deg
Mean motion: 15
50486764 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2941
Checksum: 326
Coasting Arc #15 (Orbit 2955)
---------------------------------------
Vector Time (GMT): 2014/285/17:06:03
044
Vector Time (MET): N/A
Weight (LBS) : 946249
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5167856
87 A = 6793551
25 meter
Y = -2142537
55 meter E =
0004582
Z = -3859489
54 I = 51
34254
XDOT = -389
448646 Wp = 116
70135
YDOT = -6451
490786 meter/sec RA = 236
01322 deg
ZDOT = 4104
690602 TA = 196
64701
MA = 196
66206
Ha = 225
959 n
mi
Hp = 221
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16954910
99 X = -5124765
93
Y = -7029322
68 feet Y = -2200087
20 meter
Z = -12662367
25 Z = -3884489
90
XDOT = -1277
718655 XDOT = -337
217263
YDOT = -21166
308354 feet/sec YDOT = -6455
553535 meter/sec
ZDOT = 13466
832684 ZDOT = 4102
925984
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4959226
04 X = 1511572
10
Y = -17595194
97 feet Y = -5363015
43 meter
Z = -12768364
02 Z = -3891797
35
XDOT = 19566
645240 XDOT = 5963
913469
YDOT = -4248
748705 feet/sec YDOT = -1295
018605 meter/sec
ZDOT = 13460
341651 ZDOT = 4102
712135
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 14285
72094247
00016717 00000-0 10270-3 0 9147
2 25544 51
6463 236
9834 0002099 261
0036 99
0877 15
50485791 29567
Satellite: ISS
Catalog Number: 25544
Epoch time: 14285
72094247 = yrday
fracday
Element set: 914
Inclination: 51
6463 deg
RA of node: 236
9834 deg
Eccentricity:
0002099
Arg of perigee: 261
0036 deg
Mean anomaly: 99
0877 deg
Mean motion: 15
50485791 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2956
Checksum: 338
Coasting Arc #16 (Orbit 2971)
---------------------------------------
Vector Time (GMT): 2014/286/17:06:03
044
Vector Time (MET): N/A
Weight (LBS) : 946249
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5384965
53 A = 6794553
60 meter
Y = 2232459
60 meter E =
0010130
Z = 3481985
60 I = 51
36460
XDOT = 361
979702 Wp = 88
84422
YDOT = 6184
034371 meter/sec RA = 231
03561 deg
ZDOT = -4513
063587 TA = 50
12370
MA = 50
03466
Ha = 225
798 n
mi
Hp = 221
032
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17667209
76 X = 5342686
81
Y = 7324342
53 feet Y = 2292441
60 meter
Z = 11423837
26 Z = 3508042
56
XDOT = 1187
597446 XDOT = 314
724837
YDOT = 20288
826678 feet/sec YDOT = 6187
817761 meter/sec
ZDOT = -14806
639064 ZDOT = -4511
420285
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4849464
29 X = -1478116
71
Y = 18431558
67 feet Y = 5617939
08 meter
Z = 11534326
72 Z = 3515662
79
XDOT = -18577
532610 XDOT = -5662
431939
YDOT = 4397
852061 feet/sec YDOT = 1340
465308 meter/sec
ZDOT = -14800
615498 ZDOT = -4511
227604
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 14286
75218610
00016717 00000-0 10270-3 0 9154
2 25544 51
6462 231
8709 0002048 266
6651 93
4266 15
50542842 29728
Satellite: ISS
Catalog Number: 25544
Epoch time: 14286
75218610 = yrday
fracday
Element set: 915
Inclination: 51
6462 deg
RA of node: 231
8709 deg
Eccentricity:
0002048
Arg of perigee: 266
6651 deg
Mean anomaly: 93
4266 deg
Mean motion: 15
50542842 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2972
Checksum: 316
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