[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
June 25th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10225 71 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 128 5 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
176/10:41:31
942 2
5 3
3 3
3
N/A 1
9 -0
3 227
6
000/00:01:03
884 -0
9 0
0 220
5
Coasting Arc #1 (Orbit 1230)
---------------------------------------
Vector Time (GMT): 2014/174/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888612
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2914122
38 A = 6798877
03 meter
Y = -6116787
27 meter E =
0016681
Z = 457322
21 I = 52
00258
XDOT = 4091
553571 Wp = 129
71817
YDOT = -2409
322101 meter/sec RA = 67
54879 deg
ZDOT = -6018
263331 TA = 45
37952
MA = 45
24358
Ha = 227
445 n
mi
Hp = 218
740
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9560768
98 X = -2847728
03
Y = -20068199
70 feet Y = -6149003
68 meter
Z = 1500400
97 Z = 443326
25
XDOT = 13423
732188 XDOT = 4147
426000
YDOT = -7904
600068 feet/sec YDOT = -2363
254571 meter/sec
ZDOT = -19744
958436 ZDOT = -5998
251624
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19940728
02 X = -6077933
90
Y = 9832586
88 feet Y = 2996972
48 meter
Z = 1442132
81 Z = 439562
08
XDOT = -7366
483071 XDOT = -2245
304040
YDOT = -11988
376217 feet/sec YDOT = -3654
057071 meter/sec
ZDOT = -19659
596283 ZDOT = -5992
244947
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 14174
53311729
00016717 00000-0 10270-3 0 9005
2 25544 51
6485 68
1102 0003843 129
0069 231
1425 15
50822815 12316
Satellite: ISS
Catalog Number: 25544
Epoch time: 14174
53311729 = yrday
fracday
Element set: 900
Inclination: 51
6485 deg
RA of node: 68
1102 deg
Eccentricity:
0003843
Arg of perigee: 129
0069 deg
Mean anomaly: 231
1425 deg
Mean motion: 15
50822815 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1231
Checksum: 275
Coasting Arc #2 (Orbit 1246)
---------------------------------------
Vector Time (GMT): 2014/175/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888612
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3020711
64 A = 6798788
99 meter
Y = 6084192
66 meter E =
0013281
Z = 148607
55 I = 51
99045
XDOT = -4289
593536 Wp = 62
74136
YDOT = 1972
384210 meter/sec RA = 62
61658 deg
ZDOT = 6034
286866 TA = 298
84935
MA = 298
98258
Ha = 227
270 n
mi
Hp = 218
738
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9910471
25 X = 2951730
41
Y = 19961261
99 feet Y = 6117586
48 meter
Z = 487557
58 Z = 163115
07
XDOT = -14073
469605 XDOT = -4340
643085
YDOT = 6471
076803 feet/sec YDOT = 1924
128955 meter/sec
ZDOT = 19797
529087 ZDOT = 6013
324831
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19651706
65 X = 5989840
19
Y = -10507961
93 feet Y = -3202826
80 meter
Z = 547991
87 Z = 167027
92
XDOT = 6134
122167 XDOT = 1869
680437
YDOT = 12561
648901 feet/sec YDOT = 3828
790585 meter/sec
ZDOT = 19708
208108 ZDOT = 6007
061831
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 14175
56411827
00016717 00000-0 10270-3 0 9010
2 25544 51
6488 62
9961 0003635 131
3029 228
8435 15
50875705 12472
Satellite: ISS
Catalog Number: 25544
Epoch time: 14175
56411827 = yrday
fracday
Element set: 901
Inclination: 51
6488 deg
RA of node: 62
9961 deg
Eccentricity:
0003635
Arg of perigee: 131
3029 deg
Mean anomaly: 228
8435 deg
Mean motion: 15
50875705 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1247
Checksum: 316
Coasting Arc #3 (Orbit 1260)
---------------------------------------
Vector Time (GMT): 2014/176/10:42:03
884
Vector Time (MET): N/A
Weight (LBS) : 888293
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1797559
62 A = 6790428
67 meter
Y = -4356824
51 meter E =
0011642
Z = -4898460
34 I = 51
94237
XDOT = 5328
597034 Wp = 90
20196
YDOT = 4926
474663 meter/sec RA = 57
96121 deg
ZDOT = -2431
365242 TA = 156
03046
MA = 155
97622
Ha = 227
570 n
mi
Hp = 220
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5897505
31 X = 1869940
18
Y = -14294043
68 feet Y = -4336317
63 meter
Z = -16071064
09 Z = -4889552
86
XDOT = 17482
273734 XDOT = 5284
922832
YDOT = 16162
974615 feet/sec YDOT = 4985
818616 meter/sec
ZDOT = -7976
920084 ZDOT = -2405
585018
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11949248
46 X = -3642130
93
Y = -9877017
05 feet Y = -3010514
80 meter
Z = -16032446
79 Z = -4886689
78
XDOT = 19822
453932 XDOT = 6041
883958
YDOT = -11236
006183 feet/sec YDOT = -3424
734685 meter/sec
ZDOT = -7868
439236 ZDOT = -2398
300279
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 14176
46624058
00016717 00000-0 10270-3 0 9023
2 25544 51
6485 58
5205 0003624 175
1972 184
9214 15
50298210 12615
Satellite: ISS
Catalog Number: 25544
Epoch time: 14176
46624058 = yrday
fracday
Element set: 902
Inclination: 51
6485 deg
RA of node: 58
5205 deg
Eccentricity:
0003624
Arg of perigee: 175
1972 deg
Mean anomaly: 184
9214 deg
Mean motion: 15
50298210 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1261
Checksum: 302
Coasting Arc #4 (Orbit 1276)
---------------------------------------
Vector Time (GMT): 2014/177/10:42:03
884
Vector Time (MET): N/A
Weight (LBS) : 888293
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1812906
28 A = 6789783
04 meter
Y = 4163831
79 meter E =
0008387
Z = 5045344
62 I = 51
92273
XDOT = -5594
548543 Wp = 144
64842
YDOT = -4848
102371 meter/sec RA = 53
02266 deg
ZDOT = 1982
498191 TA = 286
12029
MA = 286
21259
Ha = 227
517 n
mi
Hp = 220
584
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5947855
24 X = -1883841
04
Y = 13660865
44 feet Y = 4143161
34 meter
Z = 16552967
91 Z = 5036366
12
XDOT = -18354
818054 XDOT = -5549
550468
YDOT = -15905
847673 feet/sec YDOT = -4910
412904 meter/sec
ZDOT = 6504
259157 ZDOT = 1955
429312
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11493689
91 X = 3503276
68
Y = 9548680
09 feet Y = 2910437
69 meter
Z = 16514078
05 Z = 5033490
99
XDOT = -19623
307797 XDOT = -5981
184217
YDOT = 12521
444353 feet/sec YDOT = 3816
536239 meter/sec
ZDOT = 6390
299051 ZDOT = 1947
763151
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 14177
49762570
00016717 00000-0 10270-3 0 9030
2 25544 51
6482 53
4090 0003643 179
8030 180
3122 15
50298145 12777
Satellite: ISS
Catalog Number: 25544
Epoch time: 14177
49762570 = yrday
fracday
Element set: 903
Inclination: 51
6482 deg
RA of node: 53
4090 deg
Eccentricity:
0003643
Arg of perigee: 179
8030 deg
Mean anomaly: 180
3122 deg
Mean motion: 15
50298145 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1277
Checksum: 301
Coasting Arc #5 (Orbit 1291)
---------------------------------------
Vector Time (GMT): 2014/178/10:42:03
884
Vector Time (MET): N/A
Weight (LBS) : 888293
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1897422
51 A = 6789144
05 meter
Y = -3968770
67 meter E =
0013229
Z = -5182400
43 I = 51
90163
XDOT = 5824
939930 Wp = 93
48063
YDOT = 4732
535527 meter/sec RA = 48
08180 deg
ZDOT = -1495
655044 TA = 162
16259
MA = 162
11610
Ha = 227
314 n
mi
Hp = 220
709
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6225139
47 X = 1966835
47
Y = -13020901
15 feet Y = -3947163
61 meter
Z = -17002626
10 Z = -5173015
05
XDOT = 19110
695307 XDOT = 5778
852083
YDOT = 15526
691362 feet/sec YDOT = 4797
416275 meter/sec
ZDOT = -4907
004738 ZDOT = -1467
469727
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10965912
84 X = -3342410
24
Y = -9456397
31 feet Y = -2882309
90 meter
Z = -16962040
80 Z = -5170030
03
XDOT = 19221
918232 XDOT = 5858
840677
YDOT = -13725
517274 feet/sec YDOT = -4183
537665 meter/sec
ZDOT = -4788
287770 ZDOT = -1459
470112
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 14178
46454006
00016717 00000-0 10270-3 0 9041
2 25544 51
6484 48
6166 0003528 184
7479 175
3639 15
50328441 12920
Satellite: ISS
Catalog Number: 25544
Epoch time: 14178
46454006 = yrday
fracday
Element set: 904
Inclination: 51
6484 deg
RA of node: 48
6166 deg
Eccentricity:
0003528
Arg of perigee: 184
7479 deg
Mean anomaly: 175
3639 deg
Mean motion: 15
50328441 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1292
Checksum: 325
Coasting Arc #6 (Orbit 1307)
---------------------------------------
Vector Time (GMT): 2014/179/10:42:03
884
Vector Time (MET): N/A
Weight (LBS) : 888293
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1991425
33 A = 6788744
85 meter
Y = 3794549
67 meter E =
0005924
Z = 5263853
59 I = 51
87876
XDOT = -6055
292609 Wp = 154
92874
YDOT = -4587
555577 meter/sec RA = 43
13949 deg
ZDOT = 1010
540608 TA = 285
38969
MA = 285
45513
Ha = 227
270 n
mi
Hp = 220
751
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6533547
66 X = -2059278
72
Y = 12449309
95 feet Y = 3771900
17 meter
Z = 17269860
86 Z = 5254015
32
XDOT = -19866
445567 XDOT = -6008
452312
YDOT = -15051
035359 feet/sec YDOT = -4655
007991 meter/sec
ZDOT = 3315
421942 ZDOT = 981
238244
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10497753
09 X = 3199715
14
Y = 9430541
85 feet Y = 2874429
16 meter
Z = 17227382
80 Z = 5250906
28
XDOT = -18687
936235 XDOT = -5696
082964
YDOT = 14937
935205 feet/sec YDOT = 4553
082650 meter/sec
ZDOT = 3191
939149 ZDOT = 972
903053
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 14179
49590654
00016717 00000-0 10270-3 0 9056
2 25544 51
6483 43
5048 0003549 189
0472 171
0616 15
50329302 13089
Satellite: ISS
Catalog Number: 25544
Epoch time: 14179
49590654 = yrday
fracday
Element set: 905
Inclination: 51
6483 deg
RA of node: 43
5048 deg
Eccentricity:
0003549
Arg of perigee: 189
0472 deg
Mean anomaly: 171
0616 deg
Mean motion: 15
50329302 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1308
Checksum: 309
Coasting Arc #7 (Orbit 1322)
---------------------------------------
Vector Time (GMT): 2014/180/10:42:03
884
Vector Time (MET): N/A
Weight (LBS) : 888293
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2146258
30 A = 6788431
52 meter
Y = -3635554
37 meter E =
0014048
Z = -5327723
30 I = 51
85424
XDOT = 6235
686178 Wp = 99
60602
YDOT = 4407
417091 meter/sec RA = 38
19436 deg
ZDOT = -498
925439 TA = 165
65844
MA = 165
61852
Ha = 227
052 n
mi
Hp = 220
901
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7041529
85 X = 2212632
47
Y = -11927671
83 feet Y = -3611181
75 meter
Z = -17479407
16 Z = -5317136
43
XDOT = 20458
287985 XDOT = 6188
361579
YDOT = 14460
029826 feet/sec YDOT = 4476
883998 meter/sec
ZDOT = -1636
894485 ZDOT = -468
748069
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10036450
77 X = -3059110
20
Y = -9628870
04 feet Y = -2934879
59 meter
Z = -17433780
15 Z = -5313816
19
XDOT = 17953
968575 XDOT = 5472
369622
YDOT = -16000
842259 feet/sec YDOT = -4877
056721 meter/sec
ZDOT = -1509
666360 ZDOT = -460
146306
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 14180
46280356
00016717 00000-0 10270-3 0 9061
2 25544 51
6480 38
7118 0003458 194
7075 165
3975 15
50355789 13230
Satellite: ISS
Catalog Number: 25544
Epoch time: 14180
46280356 = yrday
fracday
Element set: 906
Inclination: 51
6480 deg
RA of node: 38
7118 deg
Eccentricity:
0003458
Arg of perigee: 194
7075 deg
Mean anomaly: 165
3975 deg
Mean motion: 15
50355789 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1323
Checksum: 325
Coasting Arc #8 (Orbit 1338)
---------------------------------------
Vector Time (GMT): 2014/181/10:42:03
884
Vector Time (MET): N/A
Weight (LBS) : 888293
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2307719
21 A = 6788341
47 meter
Y = 3502858
65 meter E =
0003449
Z = 5336089
14 I = 51
82912
XDOT = -6404
807374 Wp = 157
62910
YDOT = -4208
589961 meter/sec RA = 33
24831 deg
ZDOT = -10
303059 TA = 292
45062
MA = 292
48714
Ha = 227
012 n
mi
Hp = 220
927
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7571257
26 X = -2372638
17
Y = 11492318
39 feet Y = 3476688
68 meter
Z = 17506854
12 Z = 5324721
39
XDOT = -21013
147551 XDOT = -6357
219893
YDOT = -13807
709847 feet/sec YDOT = -4279
946558 meter/sec
ZDOT = -33
802688 ZDOT = -41
301239
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9665437
46 X = 2946025
34
Y = 9883672
89 feet Y = 3012543
50 meter
Z = 17457937
70 Z = 5321179
41
XDOT = -17118
730693 XDOT = -5217
789115
YDOT = 17013
338917 feet/sec YDOT = 5185
665702 meter/sec
ZDOT = -164
549013 ZDOT = -50
154539
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 14181
49415155
00016717 00000-0 10270-3 0 9073
2 25544 51
6481 33
5999 0003480 198
9344 161
1678 15
50359430 13399
Satellite: ISS
Catalog Number: 25544
Epoch time: 14181
49415155 = yrday
fracday
Element set: 907
Inclination: 51
6481 deg
RA of node: 33
5999 deg
Eccentricity:
0003480
Arg of perigee: 198
9344 deg
Mean anomaly: 161
1678 deg
Mean motion: 15
50359430 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1339
Checksum: 326
Coasting Arc #9 (Orbit 1353)
---------------------------------------
Vector Time (GMT): 2014/182/10:42:03
884
Vector Time (MET): N/A
Weight (LBS) : 888293
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2516476
89 A = 6788401
59 meter
Y = -3400272
39 meter E =
0013885
Z = -5320992
70 I = 51
80216
XDOT = 6512
775510 Wp = 107
46521
YDOT = 3982
361468 meter/sec RA = 28
29896 deg
ZDOT = 532
352208 TA = 167
63039
MA = 167
59627
Ha = 226
796 n
mi
Hp = 221
088
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8256157
78 X = 2580159
87
Y = -11155749
32 feet Y = -3371774
95 meter
Z = -17457325
13 Z = -5308613
79
XDOT = 21367
373722 XDOT = 6465
173825
YDOT = 13065
490381 feet/sec YDOT = 4054
925306 meter/sec
ZDOT = 1746
562363 ZDOT = 563
874769
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9374062
71 X = -2857214
31
Y = -10324535
42 feet Y = -3146918
40 meter
Z = -17404137
48 Z = -5304781
10
XDOT = 16115
436138 XDOT = 4911
984935
YDOT = -17816
416227 feet/sec YDOT = -5430
443666 meter/sec
ZDOT = 1879
572908 ZDOT = 572
893822
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 14182
46103159
00016717 00000-0 10270-3 0 9080
2 25544 51
6473 28
8062 0003428 204
4607 155
6382 15
50379864 13545
Satellite: ISS
Catalog Number: 25544
Epoch time: 14182
46103159 = yrday
fracday
Element set: 908
Inclination: 51
6473 deg
RA of node: 28
8062 deg
Eccentricity:
0003428
Arg of perigee: 204
4607 deg
Mean anomaly: 155
6382 deg
Mean motion: 15
50379864 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1354
Checksum: 309
Coasting Arc #10 (Orbit 1369)
---------------------------------------
Vector Time (GMT): 2014/183/10:42:03
884
Vector Time (MET): N/A
Weight (LBS) : 888293
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2726471
55 A = 6788652
54 meter
Y = 3327166
22 meter E =
0001784
Z = 5250414
51 I = 51
77561
XDOT = -6600
097466 Wp = 121
85482
YDOT = -3750
882710 meter/sec RA = 23
34936 deg
ZDOT = -1051
081726 TA = 338
19548
MA = 338
20308
Ha = 226
751 n
mi
Hp = 221
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8945116
64 X = -2788978
63
Y = 10915899
67 feet Y = 3296327
13 meter
Z = 17225769
40 Z = 5237018
28
XDOT = -21653
863079 XDOT = -6552
557939
YDOT = -12306
045638 feet/sec YDOT = -3824
423351 meter/sec
ZDOT = -3448
430860 ZDOT = -1083
028604
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9195608
72 X = 2802821
54
Y = 10797687
56 feet Y = 3291135
17 meter
Z = 17168279
84 Z = 5232891
69
XDOT = -15059
744757 XDOT = -4590
210202
YDOT = 18519
259702 feet/sec YDOT = 5644
670357 meter/sec
ZDOT = -3583
280548 ZDOT = -1092
183911
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 14183
49236126
00016717 00000-0 10270-3 0 9096
2 25544 51
6477 23
6945 0003456 209
0714 151
0245 15
50387649 13709
Satellite: ISS
Catalog Number: 25544
Epoch time: 14183
49236126 = yrday
fracday
Element set: 909
Inclination: 51
6477 deg
RA of node: 23
6945 deg
Eccentricity:
0003456
Arg of perigee: 209
0714 deg
Mean anomaly: 151
0245 deg
Mean motion: 15
50387649 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1370
Checksum: 309
Coasting Arc #11 (Orbit 1384)
---------------------------------------
Vector Time (GMT): 2014/184/10:42:03
884
Vector Time (MET): N/A
Weight (LBS) : 888293
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2966277
13 A = 6789087
36 meter
Y = -3294838
57 meter E =
0012665
Z = -5152817
70 I = 51
74710
XDOT = 6620
253837 Wp = 116
35349
YDOT = 3504
381690 meter/sec RA = 18
39618 deg
ZDOT = 1567
744749 TA = 168
78233
MA = 168
75407
Ha = 226
555 n
mi
Hp = 221
255
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9731880
33 X = 3027930
85
Y = -10809837
83 feet Y = -3261322
65 meter
Z = -16905569
87 Z = -5138258
54
XDOT = 21719
992902 XDOT = 6572
959466
YDOT = 11497
315257 feet/sec YDOT = 3578
149075 meter/sec
ZDOT = 5143
519518 ZDOT = 1599
790157
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9153377
24 X = -2789949
38
Y = -11396676
88 feet Y = -3473707
11 meter
Z = -16843153
58 Z = -5133793
21
XDOT = 13893
459902 XDOT = 4234
726578
YDOT = -18972
399764 feet/sec YDOT = -5782
787448 meter/sec
ZDOT = 5278
827387 ZDOT = 1608
986587
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 14184
45922459
00016717 00000-0 10270-3 0 9106
2 25544 51
6466 18
9005 0003430 213
4879 146
6056 15
50401668 13858
Satellite: ISS
Catalog Number: 25544
Epoch time: 14184
45922459 = yrday
fracday
Element set: 910
Inclination: 51
6466 deg
RA of node: 18
9005 deg
Eccentricity:
0003430
Arg of perigee: 213
4879 deg
Mean anomaly: 146
6056 deg
Mean motion: 15
50401668 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1385
Checksum: 308
Coasting Arc #12 (Orbit 1400)
---------------------------------------
Vector Time (GMT): 2014/185/10:42:03
884
Vector Time (MET): N/A
Weight (LBS) : 888293
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3200061
75 A = 6789672
51 meter
Y = 3292024
77 meter E =
0003106
Z = 4999773
10 I = 51
71978
XDOT = -6613
230744 Wp = 77
52403
YDOT = -3267
936845 meter/sec RA = 13
44321 deg
ZDOT = -2079
272052 TA = 32
70475
MA = 32
68552
Ha = 226
499 n
mi
Hp = 221
265
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10498890
26 X = -3260923
26
Y = 10800606
21 feet Y = 3255898
98 meter
Z = 16403455
05 Z = 4984080
12
XDOT = -21696
951259 XDOT = -6566
096030
YDOT = -10721
577576 feet/sec YDOT = -3341
626558 meter/sec
ZDOT = -6821
758701 ZDOT = -2111
283787
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9233314
61 X = 2814314
29
Y = 11992772
96 feet Y = 3655397
20 meter
Z = 16336230
49 Z = 4979283
05
XDOT = -12737
192418 XDOT = -3882
296249
YDOT = 19290
866599 feet/sec YDOT = 5879
856139 meter/sec
ZDOT = -6956
960970 ZDOT = -2120
481704
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 14185
49053600
00016717 00000-0 10270-3 0 9115
2 25544 51
6470 13
7888 0003472 218
7276 141
3626 15
50413410 14012
Satellite: ISS
Catalog Number: 25544
Epoch time: 14185
49053600 = yrday
fracday
Element set: 911
Inclination: 51
6470 deg
RA of node: 13
7888 deg
Eccentricity:
0003472
Arg of perigee: 218
7276 deg
Mean anomaly: 141
3626 deg
Mean motion: 15
50413410 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1401
Checksum: 281
Coasting Arc #13 (Orbit 1415)
---------------------------------------
Vector Time (GMT): 2014/186/10:42:03
884
Vector Time (MET): N/A
Weight (LBS) : 888293
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3444004
13 A = 6790430
47 meter
Y = -3335165
39 meter E =
0010442
Z = -4818740
89 I = 51
69052
XDOT = 6539
552332 Wp = 125
61127
YDOT = 3031
548306 meter/sec RA = 8
48661 deg
ZDOT = 2573
675696 TA = 169
77426
MA = 169
75300
Ha = 226
334 n
mi
Hp = 221
384
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11299226
16 X = 3504450
60
Y = -10942143
68 feet Y = -3296314
01 meter
Z = -15809517
35 Z = -4801863
85
XDOT = 21455
224187 XDOT = 6492
664766
YDOT = 9946
024626 feet/sec YDOT = 3104
415444 meter/sec
ZDOT = 8443
817901 ZDOT = 2605
330193
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9482186
41 X = -2890170
42
Y = -12640038
03 feet Y = -3852683
59 meter
Z = -15737262
74 Z = -4796717
68
XDOT = 11544
353774 XDOT = 3518
719030
YDOT = -19347
778215 feet/sec YDOT = -5897
202800 meter/sec
ZDOT = 8577
541475 ZDOT = 2614
434641
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 14186
45738266
00016717 00000-0 10270-3 0 9121
2 25544 51
6456 8
9946 0003441 221
4836 138
6054 15
50423204 14168
Satellite: ISS
Catalog Number: 25544
Epoch time: 14186
45738266 = yrday
fracday
Element set: 912
Inclination: 51
6456 deg
RA of node: 8
9946 deg
Eccentricity:
0003441
Arg of perigee: 221
4836 deg
Mean anomaly: 138
6054 deg
Mean motion: 15
50423204 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1416
Checksum: 303
Coasting Arc #14 (Orbit 1431)
---------------------------------------
Vector Time (GMT): 2014/187/10:42:03
884
Vector Time (MET): N/A
Weight (LBS) : 888293
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3673823
18 A = 6791299
38 meter
Y = 3404072
16 meter E =
0005519
Z = 4582479
92 I = 51
66299
XDOT = -6435
814167 Wp = 78
79287
YDOT = -2821
276339 meter/sec RA = 3
53031 deg
ZDOT = -3059
713528 TA = 41
82292
MA = 41
78076
Ha = 226
267 n
mi
Hp = 221
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12053225
66 X = -3733875
47
Y = 11168215
74 feet Y = 3362652
97 meter
Z = 15034382
94 Z = 4564487
40
XDOT = -21114
875876 XDOT = -6388
924575
YDOT = -9256
155968 feet/sec YDOT = -2892
983338 meter/sec
ZDOT = -10038
430210 ZDOT = -3090
864156
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9845045
07 X = 3000769
74
Y = 13243628
96 feet Y = 4036658
11 meter
Z = 14957384
18 Z = 4559010
70
XDOT = -10431
356744 XDOT = -3179
477536
YDOT = 19256
090291 feet/sec YDOT = 5869
256321 meter/sec
ZDOT = -10170
048656 ZDOT = -3099
830830
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 14187
48867572
00016717 00000-0 10270-3 0 9139
2 25544 51
6460 3
8827 0003501 227
2180 132
8677 15
50436873 14329
Satellite: ISS
Catalog Number: 25544
Epoch time: 14187
48867572 = yrday
fracday
Element set: 913
Inclination: 51
6460 deg
RA of node: 3
8827 deg
Eccentricity:
0003501
Arg of perigee: 227
2180 deg
Mean anomaly: 132
8677 deg
Mean motion: 15
50436873 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1432
Checksum: 312
Coasting Arc #15 (Orbit 1446)
---------------------------------------
Vector Time (GMT): 2014/188/10:42:03
884
Vector Time (MET): N/A
Weight (LBS) : 888293
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3894059
19 A = 6792279
58 meter
Y = -3518042
61 meter E =
0007386
Z = -4319979
68 I = 51
63393
XDOT = 6272
948475 Wp = 134
00580
YDOT = 2626
402067 meter/sec RA = 358
57061 deg
ZDOT = 3514
363796 TA = 171
84102
MA = 171
82901
Ha = 226
136 n
mi
Hp = 221
465
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12775784
74 X = 3954094
43
Y = -11542134
55 feet Y = -3474160
65 meter
Z = -14173161
68 Z = -4300917
37
XDOT = 20580
539615 XDOT = 6226
041551
YDOT = 8616
804681 feet/sec YDOT = 2696
287611 meter/sec
ZDOT = 11530
064949 ZDOT = 3544
723261
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10381491
07 X = -3164278
48
Y = -13819240
78 feet Y = -4212104
59 meter
Z = -14091603
36 Z = -4295120
70
XDOT = 9360
059107 XDOT = 2852
946016
YDOT = -18923
982942 feet/sec YDOT = -5768
030001 meter/sec
ZDOT = 11658
357990 ZDOT = 3553
467515
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 14188
45550549
00016717 00000-0 10270-3 0 9141
2 25544 51
6447 359
0884 0003436 228
4988 131
5868 15
50446332 14474
Satellite: ISS
Catalog Number: 25544
Epoch time: 14188
45550549 = yrday
fracday
Element set: 914
Inclination: 51
6447 deg
RA of node: 359
0884 deg
Eccentricity:
0003436
Arg of perigee: 228
4988 deg
Mean anomaly: 131
5868 deg
Mean motion: 15
50446332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1447
Checksum: 339
Coasting Arc #16 (Orbit 1462)
---------------------------------------
Vector Time (GMT): 2014/189/10:42:03
884
Vector Time (MET): N/A
Weight (LBS) : 888293
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4092488
27 A = 6793334
74 meter
Y = 3650006
99 meter E =
0007917
Z = 4002939
31 I = 51
60664
XDOT = -6081
327466 Wp = 89
86322
YDOT = -2473
046910 meter/sec RA = 353
61103 deg
ZDOT = -3955
573860 TA = 41
35021
MA = 41
29031
Ha = 226
060 n
mi
Hp = 221
485
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13426798
80 X = -4152444
34
Y = 11975088
54 feet Y = 3603906
47 meter
Z = 13133002
97 Z = 3982913
33
XDOT = -19951
861765 XDOT = -6034
006386
YDOT = -8113
670963 feet/sec YDOT = -2540
787194 meter/sec
ZDOT = -12977
604529 ZDOT = -3985
001468
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11004506
74 X = 3354173
66
Y = 14311723
12 feet Y = 4362213
21 meter
Z = 13047331
19 Z = 3976826
55
XDOT = -8437
797044 XDOT = -2571
840539
YDOT = 18452
866537 feet/sec YDOT = 5624
433721 meter/sec
ZDOT = -13101
969520 ZDOT = -3993
480310
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 14189
48678002
00016717 00000-0 10270-3 0 9151
2 25544 51
6448 353
9760 0003504 234
4325 125
6499 15
50459539 14634
Satellite: ISS
Catalog Number: 25544
Epoch time: 14189
48678002 = yrday
fracday
Element set: 915
Inclination: 51
6448 deg
RA of node: 353
9760 deg
Eccentricity:
0003504
Arg of perigee: 234
4325 deg
Mean anomaly: 125
6499 deg
Mean motion: 15
50459539 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1463
Checksum: 329
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