[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 25th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 20451 43 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 135 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
There are no maneuvers
Coasting Arc #1 (Orbit 3102)
---------------------------------------
Vector Time (GMT): 2013/144/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -13556
42 A = 6791418
69 meter
Y = 5078097
85 meter E =
0014836
Z = -4522812
87 I = 51
38641
XDOT = -6386
554842 Wp = 29
34060
YDOT = -2815
837911 meter/sec RA = 224
80884 deg
ZDOT = -3134
122185 TA = 209
00086
MA = 209
08336
Ha = 228
655 n
mi
Hp = 219
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -44476
45 X = -48368
73
Y = 16660426
02 feet Y = 5077752
06 meter
Z = -14838624
89 Z = -4522962
78
XDOT = -20953
263918 XDOT = -6339
367826
YDOT = -9238
313357 feet/sec YDOT = -2886
992244 meter/sec
ZDOT = -10282
553099 ZDOT = -3165
033825
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14654057
31 X = 4466556
67
Y = 7924184
55 feet Y = 2415291
45 meter
Z = -14839894
39 Z = -4523199
81
XDOT = -17524
925158 XDOT = -5341
597188
YDOT = 12860
313937 feet/sec YDOT = 3919
823688 meter/sec
ZDOT = -10411
151959 ZDOT = -3173
319117
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 13144
52184415
00016717 00000-0 10270-3 0 9000
2 25544 51
6484 225
6869 0009793 349
3428 10
7514 15
50455516 31031
Satellite: ISS
Catalog Number: 25544
Epoch time: 13144
52184415 = yrday
fracday
Element set: 900
Inclination: 51
6484 deg
RA of node: 225
6869 deg
Eccentricity:
0009793
Arg of perigee: 349
3428 deg
Mean anomaly: 10
7514 deg
Mean motion: 15
50455516 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3103
Checksum: 305
Coasting Arc #2 (Orbit 3118)
---------------------------------------
Vector Time (GMT): 2013/145/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 143384
38 A = 6790262
64 meter
Y = -4830414
46 meter E =
0008312
Z = 4762690
65 I = 51
40556
XDOT = 6635
620522 Wp = 41
78108
YDOT = 2793
874064 meter/sec RA = 219
83188 deg
ZDOT = 2637
249036 TA = 22
12881
MA = 22
09295
Ha = 228
682 n
mi
Hp = 219
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 470421
19 X = 174252
20
Y = -15847816
48 feet Y = -4828639
04 meter
Z = 15625625
48 Z = 4763461
59
XDOT = 21770
408536 XDOT = 6591
074379
YDOT = 9166
253491 feet/sec YDOT = 2867
828360 meter/sec
ZDOT = 8652
391849 ZDOT = 2669
376986
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13872921
79 X = -4228466
56
Y = -7667916
65 feet Y = -2337180
99 meter
Z = 15629454
57 Z = 4763857
75
XDOT = 17620
330175 XDOT = 5370
676637
YDOT = -13993
231858 feet/sec YDOT = -4265
137070 meter/sec
ZDOT = 8786
085218 ZDOT = 2677
998774
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 13145
55309948
00016717 00000-0 10270-3 0 9015
2 25544 51
6484 220
5742 0009876 353
2213 6
8803 15
50510949 31199
Satellite: ISS
Catalog Number: 25544
Epoch time: 13145
55309948 = yrday
fracday
Element set: 901
Inclination: 51
6484 deg
RA of node: 220
5742 deg
Eccentricity:
0009876
Arg of perigee: 353
2213 deg
Mean anomaly: 6
8803 deg
Mean motion: 15
50510949 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3119
Checksum: 308
Coasting Arc #3 (Orbit 3133)
---------------------------------------
Vector Time (GMT): 2013/146/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -295478
23 A = 6789488
51 meter
Y = 4628002
15 meter E =
0017573
Z = -4973342
11 I = 51
42555
XDOT = -6835
795868 Wp = 41
00801
YDOT = -2711
678996 meter/sec RA = 214
85671 deg
ZDOT = -2108
525542 TA = 208
30159
MA = 208
39717
Ha = 228
900 n
mi
Hp = 219
432
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -969416
78 X = -323048
16
Y = 15183734
10 feet Y = 4624544
44 meter
Z = -16316739
21 Z = -4974843
88
XDOT = -22427
151797 XDOT = -6794
722471
YDOT = -8896
584634 feet/sec YDOT = -2787
891236 meter/sec
ZDOT = -6917
734718 ZDOT = -2141
634210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13187432
53 X = 4019529
43
Y = 7573210
45 feet Y = 2308314
54 meter
Z = -16323591
37 Z = -4975430
65
XDOT = -17423
974971 XDOT = -5310
827571
YDOT = 15071
324530 feet/sec YDOT = 4593
739717 meter/sec
ZDOT = -7055
551343 ZDOT = -2150
532049
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 13146
51988842
00016717 00000-0 10270-3 0 9029
2 25544 51
6470 215
7819 0009959 357
1108 2
9984 15
50498613 31340
Satellite: ISS
Catalog Number: 25544
Epoch time: 13146
51988842 = yrday
fracday
Element set: 902
Inclination: 51
6470 deg
RA of node: 215
7819 deg
Eccentricity:
0009959
Arg of perigee: 357
1108 deg
Mean anomaly: 2
9984 deg
Mean motion: 15
50498613 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3134
Checksum: 333
Coasting Arc #4 (Orbit 3149)
---------------------------------------
Vector Time (GMT): 2013/147/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 521916
30 A = 6788596
03 meter
Y = -4412429
68 meter E =
0008324
Z = 5127248
72 I = 51
44893
XDOT = 7036
950991 Wp = 30
25373
YDOT = 2622
208281 meter/sec RA = 209
88115 deg
ZDOT = 1546
272478 TA = 44
83569
MA = 44
76846
Ha = 228
909 n
mi
Hp = 219
177
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1712323
80 X = 546311
31
Y = -14476475
33 feet Y = -4406457
56 meter
Z = 16821682
14 Z = 5129842
83
XDOT = 23087
109550 XDOT = 6999
594472
YDOT = 8603
045541 feet/sec YDOT = 2700
690825 meter/sec
ZDOT = 5073
072436 ZDOT = 1580
367168
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12358194
36 X = -3766777
64
Y = -7706644
14 feet Y = -2348985
13 meter
Z = 16833064
16 Z = 5130717
96
XDOT = 17161
126124 XDOT = 5230
711243
YDOT = -16170
969186 feet/sec YDOT = -4928
911408 meter/sec
ZDOT = 5215
038038 ZDOT = 1589
543594
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 13147
55111188
00016717 00000-0 10270-3 0 9036
2 25544 51
6471 210
6689 0010035
9805 359
1364 15
50555447 31500
Satellite: ISS
Catalog Number: 25544
Epoch time: 13147
55111188 = yrday
fracday
Element set: 903
Inclination: 51
6471 deg
RA of node: 210
6689 deg
Eccentricity:
0010035
Arg of perigee:
9805 deg
Mean anomaly: 359
1364 deg
Mean motion: 15
50555447 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3150
Checksum: 290
Coasting Arc #5 (Orbit 3164)
---------------------------------------
Vector Time (GMT): 2013/148/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -753687
84 A = 6788163
43 meter
Y = 4257097
98 meter E =
0019260
Z = -5248208
43 I = 51
47358
XDOT = -7172
111933 Wp = 51
71787
YDOT = -2478
028227 meter/sec RA = 204
90713 deg
ZDOT = -970
842880 TA = 208
89297
MA = 208
99975
Ha = 229
123 n
mi
Hp = 218
900
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2472729
14 X = -775741
19
Y = 13966856
88 feet Y = 4248547
08 meter
Z = -17218531
60 Z = -5251922
85
XDOT = -23530
550962 XDOT = -7139
152938
YDOT = -8130
013868 feet/sec YDOT = -2558
046904 meter/sec
ZDOT = -3185
180053 ZDOT = -1005
604660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11709842
10 X = 3569159
87
Y = 7969602
64 feet Y = 2429134
88 meter
Z = -17234568
25 Z = -5253096
40
XDOT = -16605
123600 XDOT = -5061
241673
YDOT = 17131
446896 feet/sec YDOT = 5221
665014 meter/sec
ZDOT = -3329
971048 ZDOT = -1014
975175
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 13148
51787122
00016717 00000-0 10270-3 0 9041
2 25544 51
6463 205
8756 0010125 4
9534 355
1715 15
50543386 31656
Satellite: ISS
Catalog Number: 25544
Epoch time: 13148
51787122 = yrday
fracday
Element set: 904
Inclination: 51
6463 deg
RA of node: 205
8756 deg
Eccentricity:
0010125
Arg of perigee: 4
9534 deg
Mean anomaly: 355
1715 deg
Mean motion: 15
50543386 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3165
Checksum: 301
Coasting Arc #6 (Orbit 3180)
---------------------------------------
Vector Time (GMT): 2013/149/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1059162
23 A = 6787684
19 meter
Y = -4100506
05 meter E =
0010123
Z = 5300327
86 I = 51
50089
XDOT = 7292
289165 Wp = 24
15048
YDOT = 2339
076923 meter/sec RA = 199
93401 deg
ZDOT = 361
174484 TA = 62
44996
MA = 62
34715
Ha = 229
117 n
mi
Hp = 218
658
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3474941
70 X = 1079188
70
Y = -13453103
85 feet Y = -4088550
39 meter
Z = 17389527
12 Z = 5305521
41
XDOT = 23924
833218 XDOT = 7263
836634
YDOT = 7674
136885 feet/sec YDOT = 2420
464775 meter/sec
ZDOT = 1184
955657 ZDOT = 396
530896
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10973145
02 X = -3344614
60
Y = -8478152
39 feet Y = -2584140
85 meter
Z = 17411717
23 Z = 5307091
41
XDOT = 16001
388913 XDOT = 4877
223341
YDOT = -18033
498956 feet/sec YDOT = -5496
610482 meter/sec
ZDOT = 1332
267638 ZDOT = 406
075176
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 13149
54906349
00016717 00000-0 10270-3 0 9050
2 25544 51
6464 200
7624 0010191 8
9882 351
1450 15
50601342 31815
Satellite: ISS
Catalog Number: 25544
Epoch time: 13149
54906349 = yrday
fracday
Element set: 905
Inclination: 51
6464 deg
RA of node: 200
7624 deg
Eccentricity:
0010191
Arg of perigee: 8
9882 deg
Mean anomaly: 351
1450 deg
Mean motion: 15
50601342 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3181
Checksum: 289
Coasting Arc #7 (Orbit 3195)
---------------------------------------
Vector Time (GMT): 2013/150/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1347665
69 A = 6787691
44 meter
Y = 4014644
70 meter E =
0019615
Z = -5319183
41 I = 51
53030
XDOT = -7335
784511 Wp = 60
97585
YDOT = -2157
837103 meter/sec RA = 194
96269 deg
ZDOT = 239
937298 TA = 211
26151
MA = 211
37830
Ha = 229
315 n
mi
Hp = 218
389
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4421475
36 X = -1366618
99
Y = 13171406
49 feet Y = 3999468
71 meter
Z = -17451389
13 Z = -5325775
96
XDOT = -24067
534485 XDOT = -7312
275448
YDOT = -7079
518054 feet/sec YDOT = -2239
739045 meter/sec
ZDOT = 787
195861 ZDOT = 204
357628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10493012
94 X = 3198270
34
Y = 9052807
48 feet Y = 2759295
72 meter
Z = -17479408
80 Z = -5327723
80
XDOT = -15143
818810 XDOT = -4615
835973
YDOT = 18723
606297 feet/sec YDOT = 5706
955199 meter/sec
ZDOT = 638
910449 ZDOT = 194
739905
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 13150
51579368
00016717 00000-0 10270-3 0 9067
2 25544 51
6468 195
9686 0010280 12
7239 347
4169 15
50590188 31966
Satellite: ISS
Catalog Number: 25544
Epoch time: 13150
51579368 = yrday
fracday
Element set: 906
Inclination: 51
6468 deg
RA of node: 195
9686 deg
Eccentricity:
0010280
Arg of perigee: 12
7239 deg
Mean anomaly: 347
4169 deg
Mean motion: 15
50590188 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3196
Checksum: 337
Coasting Arc #8 (Orbit 3211)
---------------------------------------
Vector Time (GMT): 2013/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1704109
95 A = 6787722
85 meter
Y = -3936459
44 meter E =
0012926
Z = 5256872
14 I = 51
56048
XDOT = 7349
444074 Wp = 27
36659
YDOT = 1998
977597 meter/sec RA = 189
99316 deg
ZDOT = -873
484782 TA = 71
06761
MA = 70
92755
Ha = 229
300 n
mi
Hp = 218
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5590911
92 X = 1722465
11
Y = -12914893
19 feet Y = -3917300
74 meter
Z = 17246955
84 Z = 5265194
89
XDOT = 24112
349324 XDOT = 7330
788009
YDOT = 6558
325450 feet/sec YDOT = 2081
059464 meter/sec
ZDOT = -2865
763719 ZDOT = -837
826933
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9976605
83 X = -3040869
46
Y = -9864251
34 feet Y = -3006623
81 meter
Z = 17282191
10 Z = 5267611
85
XDOT = 14283
844588 XDOT = 4353
715831
YDOT = -19276
298559 feet/sec YDOT = -5875
415801 meter/sec
ZDOT = -2717
116023 ZDOT = -828
176964
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 13151
54695528
00016717 00000-0 10270-3 0 9079
2 25544 51
6463 190
8553 0010347 16
9769 343
1726 15
50649705 32127
Satellite: ISS
Catalog Number: 25544
Epoch time: 13151
54695528 = yrday
fracday
Element set: 907
Inclination: 51
6463 deg
RA of node: 190
8553 deg
Eccentricity:
0010347
Arg of perigee: 16
9769 deg
Mean anomaly: 343
1726 deg
Mean motion: 15
50649705 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3212
Checksum: 320
Coasting Arc #9 (Orbit 3226)
---------------------------------------
Vector Time (GMT): 2013/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2018262
59 A = 6788209
46 meter
Y = 3932929
12 meter E =
0018593
Z = -5164913
37 I = 51
59340
XDOT = -7285
044731 Wp = 67
75615
YDOT = -1815
134601 meter/sec RA = 185
02621 deg
ZDOT = 1475
698351 TA = 216
42859
MA = 216
55525
Ha = 229
471 n
mi
Hp = 217
917
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6621596
43 X = -2037001
56
Y = 12903310
75 feet Y = 3910255
17 meter
Z = -16945253
85 Z = -5174763
24
XDOT = -23901
065390 XDOT = -7271
374644
YDOT = -5955
166014 feet/sec YDOT = -1896
524224 meter/sec
ZDOT = 4841
530022 ZDOT = 1440
341152
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9769359
52 X = 2977700
78
Y = 10653098
61 feet Y = 3247064
46 meter
Z = -16986868
46 Z = -5177597
51
XDOT = -13245
271895 XDOT = -4037
158874
YDOT = 19573
346930 feet/sec YDOT = 5965
956144 meter/sec
ZDOT = 4694
100956 ZDOT = 1430
761972
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 13152
51365641
00016717 00000-0 10270-3 0 9088
2 25544 51
6474 186
0617 0010416 20
3013 339
8551 15
50637756 32272
Satellite: ISS
Catalog Number: 25544
Epoch time: 13152
51365641 = yrday
fracday
Element set: 908
Inclination: 51
6474 deg
RA of node: 186
0617 deg
Eccentricity:
0010416
Arg of perigee: 20
3013 deg
Mean anomaly: 339
8551 deg
Mean motion: 15
50637756 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3227
Checksum: 294
Coasting Arc #10 (Orbit 3242)
---------------------------------------
Vector Time (GMT): 2013/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2390260
26 A = 6788764
98 meter
Y = -3941050
36 meter E =
0015938
Z = 4980087
09 I = 51
62526
XDOT = 7178
741895 Wp = 36
64422
YDOT = 1674
238881 meter/sec RA = 180
06106 deg
ZDOT = -2104
614937 TA = 73
94268
MA = 73
76723
Ha = 229
450 n
mi
Hp = 217
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7842061
22 X = 2409960
15
Y = -12929955
26 feet Y = -3914211
14 meter
Z = 16338868
41 Z = 4991746
46
XDOT = 23552
302804 XDOT = 7169
710392
YDOT = 5492
909713 feet/sec YDOT = 1754
465739 meter/sec
ZDOT = -6904
904648 ZDOT = -2069
762769
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9563736
65 X = -2915026
93
Y = -11645049
68 feet Y = -3549411
14 meter
Z = 16388045
87 Z = 4995076
38
XDOT = 12273
323812 XDOT = 3740
909098
YDOT = -19666
031843 feet/sec YDOT = -5994
206506 meter/sec
ZDOT = -6759
554311 ZDOT = -2060
312154
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 13153
54478731
00016717 00000-0 10270-3 0 9098
2 25544 51
6461 180
9480 0010484 24
6111 335
5538 15
50699744 32431
Satellite: ISS
Catalog Number: 25544
Epoch time: 13153
54478731 = yrday
fracday
Element set: 909
Inclination: 51
6461 deg
RA of node: 180
9480 deg
Eccentricity:
0010484
Arg of perigee: 24
6111 deg
Mean anomaly: 335
5538 deg
Mean motion: 15
50699744 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3243
Checksum: 313
Coasting Arc #11 (Orbit 3257)
---------------------------------------
Vector Time (GMT): 2013/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2694591
32 A = 6789687
97 meter
Y = 4020020
70 meter E =
0016584
Z = -4773263
97 I = 51
65977
XDOT = -7003
877050 Wp = 70
15733
YDOT = -1527
333389 meter/sec RA = 175
09957 deg
ZDOT = 2680
580434 TA = 226
29690
MA = 226
43440
Ha = 229
593 n
mi
Hp = 217
496
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8840522
71 X = -2716156
30
Y = 13189044
30 feet Y = 3989767
86 meter
Z = -15660314
85 Z = -4786406
29
XDOT = -22978
599245 XDOT = -6999
299218
YDOT = -5010
936317 feet/sec YDOT = -1605
629764 meter/sec
ZDOT = 8794
555230 ZDOT = 2646
566832
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9686476
50 X = 2952438
04
Y = 12511596
42 feet Y = 3813534
59 meter
Z = -15715703
00 Z = -4790146
27
XDOT = -11221
001452 XDOT = -3420
161243
YDOT = 19502
125409 feet/sec YDOT = 5944
247825 meter/sec
ZDOT = 8652
676373 ZDOT = 2637
335758
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 13154
51145914
00016717 00000-0 10270-3 0 9102
2 25544 51
6470 176
1546 0010525 27
6614 332
5095 15
50685152 32587
Satellite: ISS
Catalog Number: 25544
Epoch time: 13154
51145914 = yrday
fracday
Element set: 910
Inclination: 51
6470 deg
RA of node: 176
1546 deg
Eccentricity:
0010525
Arg of perigee: 27
6614 deg
Mean anomaly: 332
5095 deg
Mean motion: 15
50685152 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3258
Checksum: 293
Coasting Arc #12 (Orbit 3273)
---------------------------------------
Vector Time (GMT): 2013/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3043923
13 A = 6790677
73 meter
Y = -4108083
85 meter E =
0018605
Z = 4463633
69 I = 51
69245
XDOT = 6779
551154 Wp = 49
01750
YDOT = 1445
292930 meter/sec RA = 170
13941 deg
ZDOT = -3272
228917 TA = 74
04198
MA = 73
83708
Ha = 229
561 n
mi
Hp = 217
282
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9986624
43 X = 3067950
96
Y = -13477965
39 feet Y = -4073910
84 meter
Z = 14644467
50 Z = 4478478
99
XDOT = 22242
621897 XDOT = 6778
781516
YDOT = 4741
774705 feet/sec YDOT = 1521
102138 meter/sec
ZDOT = -10735
659178 ZDOT = -3239
295762
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9824742
89 X = -2994581
63
Y = -13528766
85 feet Y = -4123568
14 meter
Z = 14706989
55 Z = 4482690
41
XDOT = 10320
503872 XDOT = 3145
689580
YDOT = -19090
148553 feet/sec YDOT = -5818
677279 meter/sec
ZDOT = -10598
270124 ZDOT = -3230
352734
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 13155
54255884
00016717 00000-0 10270-3 0 9115
2 25544 51
6453 171
0403 0010578 31
7092 328
4694 15
50750006 32746
Satellite: ISS
Catalog Number: 25544
Epoch time: 13155
54255884 = yrday
fracday
Element set: 911
Inclination: 51
6453 deg
RA of node: 171
0403 deg
Eccentricity:
0010578
Arg of perigee: 31
7092 deg
Mean anomaly: 328
4694 deg
Mean motion: 15
50750006 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3274
Checksum: 295
Coasting Arc #13 (Orbit 3288)
---------------------------------------
Vector Time (GMT): 2013/156/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3303397
83 A = 6791899
25 meter
Y = 4255459
82 meter E =
0014661
Z = -4143540
64 I = 51
72677
XDOT = -6506
785422 Wp = 65
64210
YDOT = -1374
166997 meter/sec RA = 165
18380 deg
ZDOT = 3792
661985 TA = 243
40877
MA = 243
55908
Ha = 229
685 n
mi
Hp = 217
122
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10837919
39 X = -3330609
31
Y = 13961482
35 feet Y = 4218367
44 meter
Z = -13594293
43 Z = -4159654
11
XDOT = -21347
721201 XDOT = -6509
359564
YDOT = -4508
421907 feet/sec YDOT = -1446
944773 meter/sec
ZDOT = 12443
116749 ZDOT = 3761
045771
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10272083
43 X = 3130931
03
Y = 14318464
95 feet Y = 4364268
12 meter
Z = -13662143
45 Z = -4164221
32
XDOT = -9442
277043 XDOT = -2878
006043
YDOT = 18469
478295 feet/sec YDOT = 5629
496984 meter/sec
ZDOT = 12311
206664 ZDOT = 3752
455791
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 13156
50920104
00016717 00000-0 10270-3 0 9127
2 25544 51
6457 166
2469 0010610 34
8902 325
2943 15
50733481 32895
Satellite: ISS
Catalog Number: 25544
Epoch time: 13156
50920104 = yrday
fracday
Element set: 912
Inclination: 51
6457 deg
RA of node: 166
2469 deg
Eccentricity:
0010610
Arg of perigee: 34
8902 deg
Mean anomaly: 325
2943 deg
Mean motion: 15
50733481 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3289
Checksum: 296
Coasting Arc #14 (Orbit 3304)
---------------------------------------
Vector Time (GMT): 2013/157/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3594600
27 A = 6793130
81 meter
Y = -4402074
36 meter E =
0020514
Z = 3713747
89 I = 51
75945
XDOT = 6183
039482 Wp = 62
72861
YDOT = 1388
240517 meter/sec RA = 160
22928 deg
ZDOT = -4311
635012 TA = 73
12706
MA = 72
90220
Ha = 229
641 n
mi
Hp = 216
930
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11793307
96 X = 3625517
44
Y = -14442501
18 feet Y = -4361704
86 meter
Z = 12184212
24 Z = 3731284
92
XDOT = 20285
562606 XDOT = 6188
001356
YDOT = 4554
594871 feet/sec YDOT = 1457
411435 meter/sec
ZDOT = -14145
784159 ZDOT = -4281
585754
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10718196
05 X = -3266906
16
Y = -15198146
64 feet Y = -4632395
10 meter
Z = 12258041
98 Z = 3736251
20
XDOT = 8804
822218 XDOT = 2683
709812
YDOT = -17589
873361 feet/sec YDOT = -5361
393400 meter/sec
ZDOT = -14020
408448 ZDOT = -4273
420495
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 13157
54026888
00016717 00000-0 10270-3 0 9139
2 25544 51
6442 161
1318 0010632 38
3972 321
7933 15
50799682 33050
Satellite: ISS
Catalog Number: 25544
Epoch time: 13157
54026888 = yrday
fracday
Element set: 913
Inclination: 51
6442 deg
RA of node: 161
1318 deg
Eccentricity:
0010632
Arg of perigee: 38
3972 deg
Mean anomaly: 321
7933 deg
Mean motion: 15
50799682 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3305
Checksum: 313
Coasting Arc #15 (Orbit 3319)
---------------------------------------
Vector Time (GMT): 2013/158/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3780100
01 A = 6794425
81 meter
Y = 4589989
88 meter E =
0014461
Z = -3288547
04 I = 51
79216
XDOT = -5839
333151 Wp = 55
27697
YDOT = -1424
737781 meter/sec RA = 155
27962 deg
ZDOT = 4746
433840 TA = 266
70473
MA = 266
87018
Ha = 229
751 n
mi
Hp = 216
782
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12401902
91 X = -3815170
28
Y = 15059021
93 feet Y = 4547522
78 meter
Z = -10789196
33 Z = -3306995
19
XDOT = -19157
917162 XDOT = -5846
024566
YDOT = -4674
336551 feet/sec YDOT = -1490
074940 meter/sec
ZDOT = 15572
289500 ZDOT = 4718
050130
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11416989
97 X = 3479898
54
Y = 15765516
92 feet Y = 4805329
56 meter
Z = -10866872
18 Z = -3312222
64
XDOT = -8276
491520 XDOT = -2522
674615
YDOT = 16594
380461 feet/sec YDOT = 5057
967165 meter/sec
ZDOT = 15453
863756 ZDOT = 4710
337673
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 13158
50688105
00016717 00000-0 10270-3 0 9143
2 25544 51
6442 156
3382 0010677 42
1184 318
0786 15
50786018 33205
Satellite: ISS
Catalog Number: 25544
Epoch time: 13158
50688105 = yrday
fracday
Element set: 914
Inclination: 51
6442 deg
RA of node: 156
3382 deg
Eccentricity:
0010677
Arg of perigee: 42
1184 deg
Mean anomaly: 318
0786 deg
Mean motion: 15
50786018 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3320
Checksum: 302
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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