[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 10th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 22066 02 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
253/23:02:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
1
000/00:00:00
000 0
0 0
0 219
3
257/02:09:27
923 1
3 1
3 1
3
N/A 0
3 -0
2 227
9
000/00:02:55
846 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 2425)
---------------------------------------
Vector Time (GMT): 2014/251/13:06:03
794
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2639662
85 A = 6788423
54 meter
Y = -3289067
12 meter E =
0018252
Z = -5335282
75 I = 51
88651
XDOT = 5574
746777 Wp = 86
92735
YDOT = 5216
888510 meter/sec RA = 45
79999 deg
ZDOT = -458
343241 TA = 178
70700
MA = 178
70228
Ha = 228
221 n
mi
Hp = 219
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8660311
19 X = 2702162
60
Y = -10790902
61 feet Y = -3259199
92 meter
Z = -17504208
50 Z = -5322307
55
XDOT = 18289
851632 XDOT = 5518
222461
YDOT = 17115
775953 feet/sec YDOT = 5278
912831 meter/sec
ZDOT = -1503
750791 ZDOT = -431
400141
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8153214
36 X = -2485099
74
Y = 11265880
11 feet Y = 3433840
26 meter
Z = -17448407
53 Z = -5318274
61
XDOT = -18405
799772 XDOT = -5610
087771
YDOT = -15471
190965 feet/sec YDOT = -4715
619006 meter/sec
ZDOT = -1389
998157 ZDOT = -423
671438
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 14251
56274613
00016717 00000-0 10270-3 0 9004
2 25544 51
6446 46
3457 0003505 89
5533 270
6019 15
50356774 24265
Satellite: ISS
Catalog Number: 25544
Epoch time: 14251
56274613 = yrday
fracday
Element set: 900
Inclination: 51
6446 deg
RA of node: 46
3457 deg
Eccentricity:
0003505
Arg of perigee: 89
5533 deg
Mean anomaly: 270
6019 deg
Mean motion: 15
50356774 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2426
Checksum: 303
Coasting Arc #2 (Orbit 2441)
---------------------------------------
Vector Time (GMT): 2014/252/13:06:03
794
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2791810
49 A = 6788309
85 meter
Y = 3124208
03 meter E =
0005822
Z = 5335978
19 I = 51
86436
XDOT = -5768
057393 Wp = 88
45021
YDOT = -5051
032766 meter/sec RA = 40
85457 deg
ZDOT = -60
293406 TA = 2
12387
MA = 2
12140
Ha = 228
270 n
mi
Hp = 219
333
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9159483
24 X = -2852458
94
Y = 10250026
34 feet Y = 3092649
82 meter
Z = 17506490
11 Z = 5322268
30
XDOT = -18924
072811 XDOT = -5710
853999
YDOT = -16571
629811 feet/sec YDOT = -5115
215081 meter/sec
ZDOT = -197
813013 ZDOT = -88
174019
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8495589
13 X = 2589455
57
Y = -10901506
99 feet Y = -3322779
33 meter
Z = 17447592
38 Z = 5318026
16
XDOT = 19287
948501 XDOT = 5878
966703
YDOT = 14525
001070 feet/sec YDOT = 4427
220326 meter/sec
ZDOT = -315
574244 ZDOT = -96
187030
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 14252
59408436
00016717 00000-0 10270-3 0 9011
2 25544 51
6450 41
2321 0003407 91
3629 268
7912 15
50370161 24426
Satellite: ISS
Catalog Number: 25544
Epoch time: 14252
59408436 = yrday
fracday
Element set: 901
Inclination: 51
6450 deg
RA of node: 41
2321 deg
Eccentricity:
0003407
Arg of perigee: 91
3629 deg
Mean anomaly: 268
7912 deg
Mean motion: 15
50370161 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2442
Checksum: 281
Coasting Arc #3 (Orbit 2456)
---------------------------------------
Vector Time (GMT): 2014/253/13:06:03
794
Vector Time (MET): N/A
Weight (LBS) : 928977
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2992483
76 A = 6788299
15 meter
Y = -2995651
08 meter E =
0018085
Z = -5321550
92 I = 51
84140
XDOT = 5893
486402 Wp = 94
35928
YDOT = 4840
004630 meter/sec RA = 35
90977 deg
ZDOT = 589
918552 TA = 181
26728
MA = 181
27187
Ha = 228
092 n
mi
Hp = 219
324
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9817860
12 X = 3051609
79
Y = -9828251
57 feet Y = -2961857
32 meter
Z = -17459156
56 Z = -5306869
85
XDOT = 19335
585308 XDOT = 5836
060702
YDOT = 15879
280281 feet/sec YDOT = 4905
588402 meter/sec
ZDOT = 1935
428320 ZDOT = 618
408111
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9000248
24 X = -2743275
66
Y = 10685343
72 feet Y = 3256892
77 meter
Z = -17396149
43 Z = -5302346
35
XDOT = -19897
720987 XDOT = -6064
825357
YDOT = -13414
988582 feet/sec YDOT = -4088
888520 meter/sec
ZDOT = 2055
805498 ZDOT = 626
609516
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 14253
56094373
00016717 00000-0 10270-3 0 9021
2 25544 51
6459 36
4405 0003444 94
2561 265
8983 15
50423259 24571
Satellite: ISS
Catalog Number: 25544
Epoch time: 14253
56094373 = yrday
fracday
Element set: 902
Inclination: 51
6459 deg
RA of node: 36
4405 deg
Eccentricity:
0003444
Arg of perigee: 94
2561 deg
Mean anomaly: 265
8983 deg
Mean motion: 15
50423259 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2457
Checksum: 316
Coasting Arc #4 (Orbit 2463)
---------------------------------------
Vector Time (GMT): 2014/253/23:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 912081
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 52640
79 A = 6789922
00 meter
Y = 4683452
98 meter E =
0009618
Z = 4909227
23 I = 51
83442
XDOT = -6890
982556 Wp = 109
82321
YDOT = -2398
761591 meter/sec RA = 33
89043 deg
ZDOT = 2355
405481 TA = 317
13956
MA = 317
21449
Ha = 228
066 n
mi
Hp = 219
276
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 172706
00 X = -23582
05
Y = 15365659
37 feet Y = 4683616
11 meter
Z = 16106388
56 Z = 4909297
19
XDOT = -22608
210486 XDOT = -6875
088712
YDOT = -7869
952727 feet/sec YDOT = -2475
731836 meter/sec
ZDOT = 7727
708270 ZDOT = 2321
968952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6534706
22 X = -1991778
46
Y = 13908566
05 feet Y = 4239330
93 meter
Z = 16105852
13 Z = 4909063
73
XDOT = -16067
461810 XDOT = -4897
362360
YDOT = -16359
619392 feet/sec YDOT = -4986
411991 meter/sec
ZDOT = 7585
850707 ZDOT = 2312
167295
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
01213781
00016717 00000-0 10270-3 0 9039
2 25544 51
6438 34
2067 0003331 87
4675 272
6857 15
50425309 24645
Satellite: ISS
Catalog Number: 25544
Epoch time: 14254
01213781 = yrday
fracday
Element set: 903
Inclination: 51
6438 deg
RA of node: 34
2067 deg
Eccentricity:
0003331
Arg of perigee: 87
4675 deg
Mean anomaly: 272
6857 deg
Mean motion: 15
50425309 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2464
Checksum: 298
Coasting Arc #5 (Orbit 2478)
---------------------------------------
Vector Time (GMT): 2014/254/23:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 912081
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 127536
98 A = 6789185
65 meter
Y = -4506541
25 meter E =
0016547
Z = -5091121
86 I = 51
80611
XDOT = 7073
444974 Wp = 78
85718
YDOT = 2265
885370 meter/sec RA = 28
94197 deg
ZDOT = -1830
450840 TA = 173
42794
MA = 173
40621
Ha = 228
067 n
mi
Hp = 219
222
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 418428
42 X = 202651
82
Y = -14785240
32 feet Y = -4504695
66 meter
Z = -16703155
71 Z = -5090319
31
XDOT = 23206
840466 XDOT = 7056
473384
YDOT = 7434
007121 feet/sec YDOT = 2344
890096 meter/sec
ZDOT = -6005
416143 ZDOT = -1796
130399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6595871
17 X = 2010421
53
Y = -13244393
75 feet Y = -4036891
21 meter
Z = -16698932
36 Z = -5089834
58
XDOT = 17118
399353 XDOT = 5217
688123
YDOT = 15905
348315 feet/sec YDOT = 4847
950166 meter/sec
ZDOT = -5859
785372 ZDOT = -1786
062581
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
97896998
00016717 00000-0 10270-3 0 9042
2 25544 51
6443 29
4132 0003429 89
6054 270
5490 15
50436438 24794
Satellite: ISS
Catalog Number: 25544
Epoch time: 14254
97896998 = yrday
fracday
Element set: 904
Inclination: 51
6443 deg
RA of node: 29
4132 deg
Eccentricity:
0003429
Arg of perigee: 89
6054 deg
Mean anomaly: 270
5490 deg
Mean motion: 15
50436438 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2479
Checksum: 340
Coasting Arc #6 (Orbit 2494)
---------------------------------------
Vector Time (GMT): 2014/255/23:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 912081
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -332170
27 A = 6788473
63 meter
Y = 4339020
19 meter E =
0007105
Z = 5204818
26 I = 51
77689
XDOT = -7255
793361 Wp = 109
09832
YDOT = -2113
123816 meter/sec RA = 23
99252 deg
ZDOT = 1294
840916 TA = 328
46701
MA = 328
50957
Ha = 227
953 n
mi
Hp = 219
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1089797
48 X = -405948
98
Y = 14235630
55 feet Y = 4334893
66 meter
Z = 17076175
38 Z = 5203024
96
XDOT = -23805
096328 XDOT = -7237
914608
YDOT = -6932
820919 feet/sec YDOT = -2194
162691 meter/sec
ZDOT = 4248
165734 ZDOT = 1259
636758
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6766297
44 X = -2062367
46
Y = 12583534
93 feet Y = 3835461
45 meter
Z = 17067761
10 Z = 5202253
58
XDOT = -18183
890196 XDOT = -5542
449732
YDOT = -15353
567096 feet/sec YDOT = -4679
767251 meter/sec
ZDOT = 4098
757750 ZDOT = 1249
301362
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
01023481
00016717 00000-0 10270-3 0 9059
2 25544 51
6446 24
3014 0003282 90
9533 269
1994 15
50490601 24957
Satellite: ISS
Catalog Number: 25544
Epoch time: 14256
01023481 = yrday
fracday
Element set: 905
Inclination: 51
6446 deg
RA of node: 24
3014 deg
Eccentricity:
0003282
Arg of perigee: 90
9533 deg
Mean anomaly: 269
1994 deg
Mean motion: 15
50490601 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2495
Checksum: 290
Coasting Arc #7 (Orbit 2509)
---------------------------------------
Vector Time (GMT): 2014/256/23:02:00
000
Vector Time (MET): N/A
Weight (LBS) : 912081
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 589695
85 A = 6788085
08 meter
Y = -4218009
04 meter E =
0017892
Z = -5301282
54 I = 51
74704
XDOT = 7364
262426 Wp = 85
83884
YDOT = 1937
849692 meter/sec RA = 19
03889 deg
ZDOT = -723
536056 TA = 177
24791
MA = 177
23805
Ha = 227
917 n
mi
Hp = 219
167
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1934697
68 X = 662570
82
Y = -13838612
34 feet Y = -4211007
68 meter
Z = -17392659
25 Z = -5298240
49
XDOT = 24160
965965 XDOT = 7345
560335
YDOT = 6357
774581 feet/sec YDOT = 2020
097004 meter/sec
ZDOT = -2373
805957 ZDOT = -687
806940
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7179642
78 X = 2188355
12
Y = -12007484
97 feet Y = -3659881
42 meter
Z = -17378949
23 Z = -5297103
73
XDOT = 19033
351035 XDOT = 5801
365396
YDOT = 14592
810873 feet/sec YDOT = 4447
888754 meter/sec
ZDOT = -2222
141306 ZDOT = -677
308670
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
97702558
00016717 00000-0 10270-3 0 9064
2 25544 51
6449 19
5076 0003312 93
0367 267
1163 15
50503993 25100
Satellite: ISS
Catalog Number: 25544
Epoch time: 14256
97702558 = yrday
fracday
Element set: 906
Inclination: 51
6449 deg
RA of node: 19
5076 deg
Eccentricity:
0003312
Arg of perigee: 93
0367 deg
Mean anomaly: 267
1163 deg
Mean motion: 15
50503993 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2510
Checksum: 308
Coasting Arc #8 (Orbit 2511)
---------------------------------------
Vector Time (GMT): 2014/257/02:10:55
846
Vector Time (MET): N/A
Weight (LBS) : 911952
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1983222
39 A = 6788731
15 meter
Y = -3754308
59 meter E =
0016896
Z = -5311749
56 I = 51
74553
XDOT = 7067
623396 Wp = 94
46586
YDOT = 2860
921821 meter/sec RA = 18
37878 deg
ZDOT = 617
137580 TA = 181
42846
MA = 181
43330
Ha = 227
891 n
mi
Hp = 219
941
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6506635
13 X = 2050859
42
Y = -12317285
40 feet Y = -3731753
19 meter
Z = -17426999
86 Z = -5301950
69
XDOT = 23187
740802 XDOT = 7032
108755
YDOT = 9386
226446 feet/sec YDOT = 2939
758036 meter/sec
ZDOT = 2024
729593 ZDOT = 651
384739
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 817663
41 X = 249223
81
Y = -13959167
76 feet Y = -4254754
33 meter
Z = -17384625
58 Z = -5298833
88
XDOT = 23954
688072 XDOT = 7301
388924
YDOT = -1297
552361 feet/sec YDOT = -395
493959 meter/sec
ZDOT = 2169
919985 ZDOT = 661
391611
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
10592985
00016717 00000-0 10270-3 0 9072
2 25544 51
6474 18
8692 0002278 93
5552 266
5859 15
50280080 25121
Satellite: ISS
Catalog Number: 25544
Epoch time: 14257
10592985 = yrday
fracday
Element set: 907
Inclination: 51
6474 deg
RA of node: 18
8692 deg
Eccentricity:
0002278
Arg of perigee: 93
5552 deg
Mean anomaly: 266
5859 deg
Mean motion: 15
50280080 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2512
Checksum: 327
Coasting Arc #9 (Orbit 2527)
---------------------------------------
Vector Time (GMT): 2014/258/02:10:55
846
Vector Time (MET): N/A
Weight (LBS) : 911952
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2179837
38 A = 6788826
62 meter
Y = 3727211
35 meter E =
0005749
Z = 5234424
95 I = 51
71630
XDOT = -7124
940449 Wp = 69
12505
YDOT = -2602
408576 meter/sec RA = 13
42591 deg
ZDOT = -1111
077470 TA = 31
53208
MA = 31
49764
Ha = 227
807 n
mi
Hp = 219
848
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7151697
43 X = -2246781
13
Y = 12228383
68 feet Y = 3702461
10 meter
Z = 17173310
21 Z = 5223672
69
XDOT = -23375
788876 XDOT = -7089
912901
YDOT = -8538
085878 feet/sec YDOT = -2681
888504 meter/sec
ZDOT = -3645
267291 ZDOT = -1145
604233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1195188
01 X = -364293
30
Y = 14171948
77 feet Y = 4319609
99 meter
Z = 17126882
98 Z = 5220273
93
XDOT = -23704
145436 XDOT = -7225
023529
YDOT = 2595
066194 feet/sec YDOT = 790
976176 meter/sec
ZDOT = -3791
687152 ZDOT = -1155
706244
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
13731009
00016717 00000-0 10270-3 0 9089
2 25544 51
6471 13
7576 0002124 94
8209 265
3184 15
50344178 25280
Satellite: ISS
Catalog Number: 25544
Epoch time: 14258
13731009 = yrday
fracday
Element set: 908
Inclination: 51
6471 deg
RA of node: 13
7576 deg
Eccentricity:
0002124
Arg of perigee: 94
8209 deg
Mean anomaly: 265
3184 deg
Mean motion: 15
50344178 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2528
Checksum: 303
Coasting Arc #10 (Orbit 2542)
---------------------------------------
Vector Time (GMT): 2014/259/02:10:55
846
Vector Time (MET): N/A
Weight (LBS) : 911952
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2390993
23 A = 6789284
31 meter
Y = -3751798
32 meter E =
0015615
Z = -5142488
63 I = 51
68785
XDOT = 7106
688844 Wp = 101
10453
YDOT = 2336
873938 meter/sec RA = 8
47041 deg
ZDOT = 1600
536304 TA = 184
35259
MA = 184
36619
Ha = 227
750 n
mi
Hp = 219
880
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7844465
99 X = 2457749
57
Y = -12309049
62 feet Y = -3724687
82 meter
Z = -16871681
86 Z = -5130711
09
XDOT = 23315
908280 XDOT = 7072
254301
YDOT = 7666
909246 feet/sec YDOT = 2416
153116 meter/sec
ZDOT = 5251
103360 ZDOT = 1634
975783
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1531134
70 X = 466689
86
Y = -14574476
17 feet Y = -4442300
34 meter
Z = -16820887
88 Z = -5127006
62
XDOT = 23172
022116 XDOT = 7062
832341
YDOT = -3790
164177 feet/sec YDOT = -1155
242041 meter/sec
ZDOT = 5397
194689 ZDOT = 1645
064941
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
10421046
00016717 00000-0 10270-3 0 9095
2 25544 51
6477 8
9649 0002186 96
3143 263
8257 15
50347372 25435
Satellite: ISS
Catalog Number: 25544
Epoch time: 14259
10421046 = yrday
fracday
Element set: 909
Inclination: 51
6477 deg
RA of node: 8
9649 deg
Eccentricity:
0002186
Arg of perigee: 96
3143 deg
Mean anomaly: 263
8257 deg
Mean motion: 15
50347372 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2543
Checksum: 314
Coasting Arc #11 (Orbit 2558)
---------------------------------------
Vector Time (GMT): 2014/260/02:10:55
846
Vector Time (MET): N/A
Weight (LBS) : 911952
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2614011
63 A = 6789712
69 meter
Y = 3789808
27 meter E =
0007971
Z = 4985157
17 I = 51
65880
XDOT = -7066
796485 Wp = 66
30382
YDOT = -2100
314082 meter/sec RA = 3
51307 deg
ZDOT = -2103
044317 TA = 44
20002
MA = 44
13637
Ha = 227
679 n
mi
Hp = 219
765
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8576153
65 X = -2680412
10
Y = 12433754
17 feet Y = 3760205
84 meter
Z = 16355502
51 Z = 4972297
11
XDOT = -23185
027839 XDOT = -7032
569176
YDOT = -6890
794232 feet/sec YDOT = -2179
148364 meter/sec
ZDOT = -6899
751696 ZDOT = -2137
290432
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1866072
74 X = -568778
97
Y = 15049109
99 feet Y = 4586968
73 meter
Z = 16300097
47 Z = 4968269
71
XDOT = -22583
208364 XDOT = -6883
361909
YDOT = 4851
067517 feet/sec YDOT = 1478
605379 meter/sec
ZDOT = -7045
058768 ZDOT = -2147
333913
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
13554669
00016717 00000-0 10270-3 0 9100
2 25544 51
6475 3
8527 0002066 96
7437 263
3949 15
50413048 25593
Satellite: ISS
Catalog Number: 25544
Epoch time: 14260
13554669 = yrday
fracday
Element set: 910
Inclination: 51
6475 deg
RA of node: 3
8527 deg
Eccentricity:
0002066
Arg of perigee: 96
7437 deg
Mean anomaly: 263
3949 deg
Mean motion: 15
50413048 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2559
Checksum: 317
Coasting Arc #12 (Orbit 2573)
---------------------------------------
Vector Time (GMT): 2014/261/02:10:55
846
Vector Time (MET): N/A
Weight (LBS) : 911952
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2831425
34 A = 6790477
48 meter
Y = -3881774
46 meter E =
0013303
Z = -4811101
90 I = 51
63048
XDOT = 6954
238841 Wp = 106
55660
YDOT = 1871
576922 meter/sec RA = 358
55359 deg
ZDOT = 2584
887294 TA = 188
95543
MA = 188
97919
Ha = 227
599 n
mi
Hp = 219
828
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9289453
20 X = 2897992
49
Y = -12735480
50 feet Y = -3849739
86 meter
Z = -15784455
04 Z = -4797185
25
XDOT = 22815
744229 XDOT = 6920
237079
YDOT = 6140
344231 feet/sec YDOT = 1949
153836 meter/sec
ZDOT = 8480
601357 ZDOT = 2618
587108
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2083190
78 X = 634956
55
Y = -15685488
34 feet Y = -4780936
85 meter
Z = -15724541
23 Z = -4792840
17
XDOT = 21758
153888 XDOT = 6631
885305
YDOT = -5747
987313 feet/sec YDOT = -1751
986533 meter/sec
ZDOT = 8623
621398 ZDOT = 2628
479802
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
10240542
00016717 00000-0 10270-3 0 9111
2 25544 51
6479 359
0598 0002063 99
0558 261
0826 15
50414466 25749
Satellite: ISS
Catalog Number: 25544
Epoch time: 14261
10240542 = yrday
fracday
Element set: 911
Inclination: 51
6479 deg
RA of node: 359
0598 deg
Eccentricity:
0002063
Arg of perigee: 99
0558 deg
Mean anomaly: 261
0826 deg
Mean motion: 15
50414466 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2574
Checksum: 304
Coasting Arc #13 (Orbit 2589)
---------------------------------------
Vector Time (GMT): 2014/262/02:10:55
846
Vector Time (MET): N/A
Weight (LBS) : 911952
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3053647
16 A = 6791211
25 meter
Y = 3984750
53 meter E =
0010485
Z = 4566559
04 I = 51
60255
XDOT = -6816
353407 Wp = 72
31845
YDOT = -1687
877948 meter/sec RA = 353
59257 deg
ZDOT = -3076
303444 TA = 48
52370
MA = 48
43373
Ha = 227
538 n
mi
Hp = 219
692
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10018527
43 X = -3120161
38
Y = 13073328
50 feet Y = 3950231
23 meter
Z = 14982149
09 Z = 4551562
97
XDOT = -22363
364196 XDOT = -6782
028938
YDOT = -5537
657309 feet/sec YDOT = -1763
911216 meter/sec
ZDOT = -10092
859067 ZDOT = -3109
332617
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2273298
74 X = -692901
46
Y = 16372050
93 feet Y = 4990201
12 meter
Z = 14917629
25 Z = 4546893
40
XDOT = -20907
543191 XDOT = -6372
619165
YDOT = 6447
785128 feet/sec YDOT = 1965
284907 meter/sec
ZDOT = -10233
054483 ZDOT = -3119
035007
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
13369762
00016717 00000-0 10270-3 0 9122
2 25544 51
6480 353
9474 0001990 98
6687 261
4690 15
50481367 25908
Satellite: ISS
Catalog Number: 25544
Epoch time: 14262
13369762 = yrday
fracday
Element set: 912
Inclination: 51
6480 deg
RA of node: 353
9474 deg
Eccentricity:
0001990
Arg of perigee: 98
6687 deg
Mean anomaly: 261
4690 deg
Mean motion: 15
50481367 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2590
Checksum: 334
Coasting Arc #14 (Orbit 2604)
---------------------------------------
Vector Time (GMT): 2014/263/02:10:55
846
Vector Time (MET): N/A
Weight (LBS) : 911952
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3249925
64 A = 6792220
26 meter
Y = -4137820
36 meter E =
0010229
Z = -4305876
91 I = 51
57480
XDOT = 6616
278780 Wp = 108
24258
YDOT = 1526
443937 meter/sec RA = 348
62958 deg
ZDOT = 3530
654752 TA = 197
81641
MA = 197
85230
Ha = 227
451 n
mi
Hp = 219
773
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10662485
71 X = 3316870
64
Y = -13575526
13 feet Y = -4101103
78 meter
Z = -14126892
73 Z = -4289926
22
XDOT = 21706
951379 XDOT = 6581
567286
YDOT = 5008
018166 feet/sec YDOT = 1600
237772 meter/sec
ZDOT = 11583
512967 ZDOT = 3562
711060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2282716
71 X = 695772
05
Y = -17167011
31 feet Y = -5232505
05 meter
Z = -14058290
67 Z = -4284967
00
XDOT = 19895
220725 XDOT = 6064
063277
YDOT = -6941
617727 feet/sec YDOT = -2115
805083 meter/sec
ZDOT = 11719
593397 ZDOT = 3572
132067
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
10051492
00016717 00000-0 10270-3 0 9139
2 25544 51
6478 349
1542 0001944 102
1948 257
9421 15
50480072 26059
Satellite: ISS
Catalog Number: 25544
Epoch time: 14263
10051492 = yrday
fracday
Element set: 913
Inclination: 51
6478 deg
RA of node: 349
1542 deg
Eccentricity:
0001944
Arg of perigee: 102
1948 deg
Mean anomaly: 257
9421 deg
Mean motion: 15
50480072 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2605
Checksum: 292
Coasting Arc #15 (Orbit 2610)
---------------------------------------
Vector Time (GMT): 2014/263/11:28:05
000
Vector Time (MET): N/A
Weight (LBS) : 929408
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3218974
09 A = 6792363
21 meter
Y = -4223126
70 meter E =
0010178
Z = -4246154
56 I = 51
56358
XDOT = 6597
519925 Wp = 110
92215
YDOT = 1392
977951 meter/sec RA = 346
70731 deg
ZDOT = 3619
585041 TA = 196
20453
MA = 196
23710
Ha = 227
458 n
mi
Hp = 219
700
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10560938
61 X = 3286585
19
Y = -13855402
55 feet Y = -4186752
52 meter
Z = -13930953
30 Z = -4230352
58
XDOT = 21645
406579 XDOT = 6563
870273
YDOT = 4570
137635 feet/sec YDOT = 1466
567979 meter/sec
ZDOT = 11875
279005 ZDOT = 3651
552821
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12795559
26 X = -3900086
46
Y = 11902468
60 feet Y = 3627872
43 meter
Z = -13862971
13 Z = -4225433
60
XDOT = -19647
800570 XDOT = -5988
649614
YDOT = -7146
049593 feet/sec YDOT = -2178
115916 meter/sec
ZDOT = 12011
004551 ZDOT = 3660
954187
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
48723636
00016717 00000-0 10270-3 0 9147
2 25544 51
6478 347
2350 0002204 116
7845 243
3531 15
50504214 26115
Satellite: ISS
Catalog Number: 25544
Epoch time: 14263
48723636 = yrday
fracday
Element set: 914
Inclination: 51
6478 deg
RA of node: 347
2350 deg
Eccentricity:
0002204
Arg of perigee: 116
7845 deg
Mean anomaly: 243
3531 deg
Mean motion: 15
50504214 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2611
Checksum: 286
Coasting Arc #16 (Orbit 2626)
---------------------------------------
Vector Time (GMT): 2014/264/11:28:05
000
Vector Time (MET): N/A
Weight (LBS) : 929408
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3406746
36 A = 6793468
86 meter
Y = 4386899
37 meter E =
0013123
Z = 3900874
18 I = 51
53719
XDOT = -6362
473647 Wp = 86
38519
YDOT = -1307
988642 meter/sec RA = 341
74253 deg
ZDOT = -4072
911752 TA = 46
39209
MA = 46
28327
Ha = 227
487 n
mi
Hp = 219
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11176989
37 X = -3474497
63
Y = 14392714
48 feet Y = 4348424
63 meter
Z = 12798143
65 Z = 3884159
59
XDOT = -20874
257373 XDOT = -6327
589693
YDOT = -4291
301320 feet/sec YDOT = -1378
943438 meter/sec
ZDOT = -13362
571365 ZDOT = -4103
734764
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13270885
92 X = 4044966
03
Y = -12561597
82 feet Y = -3828775
01 meter
Z = 12726258
27 Z = 3878963
52
XDOT = 19005
236985 XDOT = 5792
796233
YDOT = 6365
719809 feet/sec YDOT = 1940
271398 meter/sec
ZDOT = -13493
435861 ZDOT = -4112
799250
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
51847756
00016717 00000-0 10270-3 0 9153
2 25544 51
6477 342
1224 0002209 115
8272 244
3107 15
50524081 26278
Satellite: ISS
Catalog Number: 25544
Epoch time: 14264
51847756 = yrday
fracday
Element set: 915
Inclination: 51
6477 deg
RA of node: 342
1224 deg
Eccentricity:
0002209
Arg of perigee: 115
8272 deg
Mean anomaly: 244
3107 deg
Mean motion: 15
50524081 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2627
Checksum: 295
Coasting Arc #17 (Orbit 2641)
---------------------------------------
Vector Time (GMT): 2014/265/11:28:05
000
Vector Time (MET): N/A
Weight (LBS) : 929408
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3550201
01 A = 6794499
24 meter
Y = -4588994
56 meter E =
0007090
Z = -3543254
96 I = 51
51128
XDOT = 6084
041696 Wp = 101
18193
YDOT = 1258
739441 meter/sec RA = 336
77694 deg
ZDOT = 4472
011644 TA = 217
06925
MA = 217
11825
Ha = 227
338 n
mi
Hp = 219
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11647641
10 X = 3618464
35
Y = -15055756
44 feet Y = -4548912
75 meter
Z = -11624852
24 Z = -3525842
12
XDOT = 19960
766718 XDOT = 6047
790397
YDOT = 4129
722575 feet/sec YDOT = 1326
573088 meter/sec
ZDOT = 14671
954211 ZDOT = 4501
478826
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13599272
22 X = -4145058
17
Y = 13384264
17 feet Y = 4079523
72 meter
Z = -11549969
80 Z = -3520430
80
XDOT = -18175
970157 XDOT = -5540
035704
YDOT = -5716
713013 feet/sec YDOT = -1742
454126 meter/sec
ZDOT = 14797
053312 ZDOT = 4510
141849
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
48524544
00016717 00000-0 10270-3 0 9168
2 25544 51
6473 337
3299 0002126 119
4128 240
7235 15
50558457 26423
Satellite: ISS
Catalog Number: 25544
Epoch time: 14265
48524544 = yrday
fracday
Element set: 916
Inclination: 51
6473 deg
RA of node: 337
3299 deg
Eccentricity:
0002126
Arg of perigee: 119
4128 deg
Mean anomaly: 240
7235 deg
Mean motion: 15
50558457 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2642
Checksum: 315
Coasting Arc #18 (Orbit 2657)
---------------------------------------
Vector Time (GMT): 2014/266/11:28:05
000
Vector Time (MET): N/A
Weight (LBS) : 929408
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3682315
06 A = 6795591
06 meter
Y = 4780958
71 meter E =
0014968
Z = 3109161
62 I = 51
48675
XDOT = -5788
285865 Wp = 98
21619
YDOT = -1285
841090 meter/sec RA = 331
80956 deg
ZDOT = -4860
088733 TA = 45
95717
MA = 45
83397
Ha = 227
306 n
mi
Hp = 219
547
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12081086
14 X = -3750606
53
Y = 15685560
07 feet Y = 4739399
31 meter
Z = 10200661
47 Z = 3091106
79
XDOT = -18990
439191 XDOT = -5749
868256
YDOT = -4218
638746 feet/sec YDOT = -1350
355382 meter/sec
ZDOT = -15945
173008 ZDOT = -4888
113996
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13860782
99 X = 4224766
66
Y = -14193167
86 feet Y = -4326077
56 meter
Z = 10123023
89 Z = 3085497
68
XDOT = 17247
454746 XDOT = 5257
024207
YDOT = 5343
667901 feet/sec YDOT = 1628
749976 meter/sec
ZDOT = -16064
127220 ZDOT = -4896
345977
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
51644343
00016717 00000-0 10270-3 0 9174
2 25544 51
6471 332
2170 0002109 117
8774 242
2591 15
50598297 26588
Satellite: ISS
Catalog Number: 25544
Epoch time: 14266
51644343 = yrday
fracday
Element set: 917
Inclination: 51
6471 deg
RA of node: 332
2170 deg
Eccentricity:
0002109
Arg of perigee: 117
8774 deg
Mean anomaly: 242
2591 deg
Mean motion: 15
50598297 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2658
Checksum: 316
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