[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 23rd 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 23680 6 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 3071)
---------------------------------------
Vector Time (GMT): 2013/142/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 74247
49 A = 6793651
60 meter
Y = 5549807
09 meter E =
0011346
Z = -3929064
24 I = 51
35562
XDOT = -5892
588597 Wp = 16
63966
YDOT = -2771
961585 meter/sec RA = 234
76120 deg
ZDOT = -4018
987690 TA = 211
07157
MA = 211
13872
Ha = 228
359 n
mi
Hp = 220
536
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 243594
12 X = 31269
57
Y = 18208028
52 feet Y = 5550397
25 meter
Z = -12890630
71 Z = -3928807
69
XDOT = -19332
639755 XDOT = -5841
630398
YDOT = -9094
362155 feet/sec YDOT = -2837
571123 meter/sec
ZDOT = -13185
655152 ZDOT = -4047
490319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15846152
92 X = 4829907
41
Y = 8972207
88 feet Y = 2734728
96 meter
Z = -12890264
70 Z = -3928952
68
XDOT = -16960
604675 XDOT = -5169
592305
YDOT = 10804
200256 feet/sec YDOT = 3293
120238 meter/sec
ZDOT = -13304
187083 ZDOT = -4055
116223
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 13142
52373773
00016717 00000-0 10270-3 0 9005
2 25544 51
6495 235
5897 0009572 341
2095 18
8701 15
50413260 30722
Satellite: ISS
Catalog Number: 25544
Epoch time: 13142
52373773 = yrday
fracday
Element set: 900
Inclination: 51
6495 deg
RA of node: 235
5897 deg
Eccentricity:
0009572
Arg of perigee: 341
2095 deg
Mean anomaly: 18
8701 deg
Mean motion: 15
50413260 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3072
Checksum: 301
Coasting Arc #2 (Orbit 3087)
---------------------------------------
Vector Time (GMT): 2013/143/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 879644
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -45916
90 A = 6792387
20 meter
Y = -5299492
64 meter E =
0009713
Z = 4237992
43 I = 51
37061
XDOT = 6153
971661 Wp = 47
84834
YDOT = 2823
811888 meter/sec RA = 229
78344 deg
ZDOT = 3598
860684 TA = 5
23003
MA = 5
21989
Ha = 228
400 n
mi
Hp = 220
243
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -150646
00 X = -7240
91
Y = -17386786
89 feet Y = -5299790
17 meter
Z = 13904174
63 Z = 4237862
93
XDOT = 20190
195738 XDOT = 6104
455118
YDOT = 9264
474699 feet/sec YDOT = 2892
352361 meter/sec
ZDOT = 11807
285709 ZDOT = 3628
636733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15240905
94 X = -4645428
13
Y = -8368642
34 feet Y = -2550762
19 meter
Z = 13904306
39 Z = 4238032
59
XDOT = 17371
313576 XDOT = 5294
776378
YDOT = -11819
117952 feet/sec YDOT = -3602
467152 meter/sec
ZDOT = 11931
132971 ZDOT = 3636
609329
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 13143
55502354
00016717 00000-0 10270-3 0 9019
2 25544 51
6497 230
4771 0009651 345
2865 14
8004 15
50470002 30882
Satellite: ISS
Catalog Number: 25544
Epoch time: 13143
55502354 = yrday
fracday
Element set: 901
Inclination: 51
6497 deg
RA of node: 230
4771 deg
Eccentricity:
0009651
Arg of perigee: 345
2865 deg
Mean anomaly: 14
8004 deg
Mean motion: 15
50470002 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3088
Checksum: 285
Coasting Arc #3 (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 = -16551
69 A = 6791387
47 meter
Y = 5076636
72 meter E =
0014751
Z = -4524310
62 I = 51
38677
XDOT = -6386
655988 Wp = 29
29824
YDOT = -2818
875360 meter/sec RA = 224
80764 deg
ZDOT = -3131
383427 TA = 209
07473
MA = 209
15695
Ha = 228
608 n
mi
Hp = 219
989
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -54303
43 X = -51340
16
Y = 16655632
28 feet Y = 5076257
56 meter
Z = -14843538
78 Z = -4524475
02
XDOT = -20953
595761 XDOT = -6339
448304
YDOT = -9248
278739 feet/sec YDOT = -2890
030708 meter/sec
ZDOT = -10273
567673 ZDOT = -3162
295508
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14645162
56 X = 4463845
55
Y = 7930496
21 feet Y = 2417215
24 meter
Z = -14844868
55 Z = -4524715
93
XDOT = -17533
401889 XDOT = -5344
180896
YDOT = 12856
538135 feet/sec YDOT = 3918
672824 meter/sec
ZDOT = -10402
167991 ZDOT = -3170
580804
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
52183830
00016717 00000-0 10270-3 0 9022
2 25544 51
6488 225
6857 0009734 348
9186 11
1749 15
50464134 31034
Satellite: ISS
Catalog Number: 25544
Epoch time: 13144
52183830 = yrday
fracday
Element set: 902
Inclination: 51
6488 deg
RA of node: 225
6857 deg
Eccentricity:
0009734
Arg of perigee: 348
9186 deg
Mean anomaly: 11
1749 deg
Mean motion: 15
50464134 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3103
Checksum: 310
Coasting Arc #4 (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 = 150318
45 A = 6790214
87 meter
Y = -4827436
06 meter E =
0008208
Z = 4765531
24 I = 51
40590
XDOT = 6635
427091 Wp = 41
65583
YDOT = 2800
288338 meter/sec RA = 219
83062 deg
ZDOT = 2630
764814 TA = 22
32293
MA = 22
28722
Ha = 228
630 n
mi
Hp = 219
712
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 493170
77 X = 181138
65
Y = -15838044
82 feet Y = -4825583
36 meter
Z = 15634945
00 Z = 4766335
75
XDOT = 21769
773920 XDOT = 6590
840736
YDOT = 9187
297696 feet/sec YDOT = 2874
240246 meter/sec
ZDOT = 8631
118157 ZDOT = 2662
891729
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13853754
23 X = -4222624
29
Y = -7683505
44 feet Y = -2341932
46 meter
Z = 15638913
78 Z = 4766740
92
XDOT = 17637
612039 XDOT = 5375
944149
YDOT = -13984
441482 feet/sec YDOT = -4262
457764 meter/sec
ZDOT = 8764
806390 ZDOT = 2671
512988
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
55308656
00016717 00000-0 10270-3 0 9032
2 25544 51
6488 220
5729 0009818 352
8067 7
2941 15
50523360 31195
Satellite: ISS
Catalog Number: 25544
Epoch time: 13145
55308656 = yrday
fracday
Element set: 903
Inclination: 51
6488 deg
RA of node: 220
5729 deg
Eccentricity:
0009818
Arg of perigee: 352
8067 deg
Mean anomaly: 7
2941 deg
Mean motion: 15
50523360 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3119
Checksum: 311
Coasting Arc #5 (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 = -308141
50 A = 6789424
27 meter
Y = 4622829
04 meter E =
0017497
Z = -4977224
27 I = 51
42587
XDOT = -6835
212253 Wp = 41
06006
YDOT = -2722
504021 meter/sec RA = 214
85534 deg
ZDOT = -2096
779370 TA = 208
37020
MA = 208
46558
Ha = 228
843 n
mi
Hp = 219
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1010962
91 X = -335633
78
Y = 15166761
93 feet Y = 4619230
16 meter
Z = -16329475
94 Z = -4978787
36
XDOT = -22425
237049 XDOT = -6794
074912
YDOT = -8932
099806 feet/sec YDOT = -2798
709378 meter/sec
ZDOT = -6879
197408 ZDOT = -2129
885048
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13153692
17 X = 4009245
37
Y = 7602691
90 feet Y = 2317300
49 meter
Z = -16336583
37 Z = -4979390
61
XDOT = -17452
829827 XDOT = -5319
622531
YDOT = 15056
388457 feet/sec YDOT = 4589
187202 meter/sec
ZDOT = -7017
000193 ZDOT = -2138
781659
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
51986649
00016717 00000-0 10270-3 0 9044
2 25544 51
6474 215
7806 0009903 356
7039 3
4045 15
50514783 31348
Satellite: ISS
Catalog Number: 25544
Epoch time: 13146
51986649 = yrday
fracday
Element set: 904
Inclination: 51
6474 deg
RA of node: 215
7806 deg
Eccentricity:
0009903
Arg of perigee: 356
7039 deg
Mean anomaly: 3
4045 deg
Mean motion: 15
50514783 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3134
Checksum: 316
Coasting Arc #6 (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 = 541950
80 A = 6788518
12 meter
Y = -4404878
94 meter E =
0008245
Z = 5131674
69 I = 51
44925
XDOT = 7035
033027 Wp = 29
71469
YDOT = 2638
142444 meter/sec RA = 209
87962 deg
ZDOT = 1527
505501 TA = 45
56031
MA = 45
49288
Ha = 228
846 n
mi
Hp = 219
179
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1778053
82 X = 566238
40
Y = -14451702
55 feet Y = -4398683
38 meter
Z = 16836203
06 Z = 5134365
87
XDOT = 23080
817019 XDOT = 6997
589638
YDOT = 8655
322978 feet/sec YDOT = 2716
603057 meter/sec
ZDOT = 5011
500988 ZDOT = 1561
590664
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12307484
04 X = -3751321
13
Y = -7755128
03 feet Y = -2363763
02 meter
Z = 16847989
24 Z = 5135267
12
XDOT = 17202
173567 XDOT = 5243
222503
YDOT = -16146
743160 feet/sec YDOT = -4921
527315 meter/sec
ZDOT = 5153
424830 ZDOT = 1570
763888
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
55107786
00016717 00000-0 10270-3 0 9057
2 25544 51
6475 210
6676 0009979
5815 359
5345 15
50575385 31508
Satellite: ISS
Catalog Number: 25544
Epoch time: 13147
55107786 = yrday
fracday
Element set: 905
Inclination: 51
6475 deg
RA of node: 210
6676 deg
Eccentricity:
0009979
Arg of perigee:
5815 deg
Mean anomaly: 359
5345 deg
Mean motion: 15
50575385 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3150
Checksum: 329
Coasting Arc #7 (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 = -782878
11 A = 6788076
14 meter
Y = 4246830
92 meter E =
0019171
Z = -5252054
33 I = 51
47390
XDOT = -7168
289783 Wp = 51
87093
YDOT = -2499
868067 meter/sec RA = 204
90540 deg
ZDOT = -943
666249 TA = 209
00373
MA = 209
11038
Ha = 229
056 n
mi
Hp = 218
895
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2568497
72 X = -804795
80
Y = 13933172
32 feet Y = 4237954
36 meter
Z = -17231149
37 Z = -5255910
22
XDOT = -23518
011100 XDOT = -7135
218872
YDOT = -8201
666887 feet/sec YDOT = -2579
843380 meter/sec
ZDOT = -3096
017877 ZDOT = -978
409192
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11639352
14 X = 3547674
53
Y = 8042556
19 feet Y = 2451371
13 meter
Z = -17247775
27 Z = -5257121
90
XDOT = -16659
940593 XDOT = -5077
949893
YDOT = 17095
838503 feet/sec YDOT = 5210
811576 meter/sec
ZDOT = -3240
727517 ZDOT = -987
773747
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
51782355
00016717 00000-0 10270-3 0 9066
2 25544 51
6467 205
8742 0010070 4
5616 355
5625 15
50566954 31651
Satellite: ISS
Catalog Number: 25544
Epoch time: 13148
51782355 = yrday
fracday
Element set: 906
Inclination: 51
6467 deg
RA of node: 205
8742 deg
Eccentricity:
0010070
Arg of perigee: 4
5616 deg
Mean anomaly: 355
5625 deg
Mean motion: 15
50566954 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3165
Checksum: 311
Coasting Arc #8 (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 = 1099085
55 A = 6787594
56 meter
Y = -4087555
68 meter E =
0010111
Z = 5302216
75 I = 51
50124
XDOT = 7284
779956 Wp = 23
59444
YDOT = 2367
541302 meter/sec RA = 199
93203 deg
ZDOT = 323
987016 TA = 63
36203
MA = 63
25850
Ha = 229
043 n
mi
Hp = 218
647
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3605923
72 X = 1118955
06
Y = -13410615
75 feet Y = -4075154
45 meter
Z = 17395724
26 Z = 5307603
87
XDOT = 23900
196707 XDOT = 7256
190335
YDOT = 7767
523957 feet/sec YDOT = 2448
844419 meter/sec
ZDOT = 1062
949529 ZDOT = 359
306619
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10881721
86 X = -3316748
82
Y = -8581073
18 feet Y = -2615511
11 meter
Z = 17418720
84 Z = 5309226
11
XDOT = 16069
852614 XDOT = 4898
091077
YDOT = -17980
849014 feet/sec YDOT = -5480
562779 meter/sec
ZDOT = 1210
104316 ZDOT = 368
839796
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
54899880
00016717 00000-0 10270-3 0 9073
2 25544 51
6467 200
7609 0010135 8
6023 351
5299 15
50628792 31816
Satellite: ISS
Catalog Number: 25544
Epoch time: 13149
54899880 = yrday
fracday
Element set: 907
Inclination: 51
6467 deg
RA of node: 200
7609 deg
Eccentricity:
0010135
Arg of perigee: 8
6023 deg
Mean anomaly: 351
5299 deg
Mean motion: 15
50628792 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3181
Checksum: 323
Coasting Arc #9 (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 = -1399797
89 A = 6787607
61 meter
Y = 3999045
32 meter E =
0019469
Z = -5317217
51 I = 51
53070
XDOT = -7323
561482 Wp = 61
19162
YDOT = -2193
796815 meter/sec RA = 194
96045 deg
ZDOT = 288
012140 TA = 211
50600
MA = 211
62274
Ha = 229
237 n
mi
Hp = 218
371
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4592512
75 X = -1418582
43
Y = 13120227
42 feet Y = 3983287
30 meter
Z = -17444939
35 Z = -5324062
91
XDOT = -24027
432683 XDOT = -7299
884753
YDOT = -7197
496112 feet/sec YDOT = -2275
561138 meter/sec
ZDOT = 944
921719 ZDOT = 252
492252
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10379898
07 X = 3163792
93
Y = 9190976
20 feet Y = 2801409
55 meter
Z = -17474012
76 Z = -5326079
09
XDOT = -15227
542169 XDOT = -4641
354853
YDOT = 18650
316018 feet/sec YDOT = 5684
616322 meter/sec
ZDOT = 796
890335 ZDOT = 242
892174
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
51571075
00016717 00000-0 10270-3 0 9086
2 25544 51
6471 195
9671 0010225 12
3466 347
7933 15
50621081 31960
Satellite: ISS
Catalog Number: 25544
Epoch time: 13150
51571075 = yrday
fracday
Element set: 908
Inclination: 51
6471 deg
RA of node: 195
9671 deg
Eccentricity:
0010225
Arg of perigee: 12
3466 deg
Mean anomaly: 347
7933 deg
Mean motion: 15
50621081 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3196
Checksum: 300
Coasting Arc #10 (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 = 1769628
31 A = 6787655
06 meter
Y = -3918365
15 meter E =
0012984
Z = 5248779
45 I = 51
56098
XDOT = 7329
721874 Wp = 27
16673
YDOT = 2043
494135 meter/sec RA = 189
99062 deg
ZDOT = -933
470453 TA = 71
84709
MA = 71
70576
Ha = 229
214 n
mi
Hp = 218
131
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5805867
16 X = 1787815
58
Y = -12855528
71 feet Y = -3898474
71 meter
Z = 17220405
04 Z = 5257420
08
XDOT = 24047
643943 XDOT = 7310
860876
YDOT = 6704
377084 feet/sec YDOT = 2125
354314 meter/sec
ZDOT = -3062
567103 ZDOT = -897
908908
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9842019
18 X = -2999847
45
Y = -10042253
97 feet Y = -3060879
01 meter
Z = 17256965
41 Z = 5259923
06
XDOT = 14383
145506 XDOT = 4383
982750
YDOT = -19173
195837 feet/sec YDOT = -5843
990091 meter/sec
ZDOT = -2914
326987 ZDOT = -888
286866
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
54685043
00016717 00000-0 10270-3 0 9092
2 25544 51
6467 190
8537 0010289 16
6028 343
5458 15
50684729 32124
Satellite: ISS
Catalog Number: 25544
Epoch time: 13151
54685043 = yrday
fracday
Element set: 909
Inclination: 51
6467 deg
RA of node: 190
8537 deg
Eccentricity:
0010289
Arg of perigee: 16
6028 deg
Mean anomaly: 343
5458 deg
Mean motion: 15
50684729 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3212
Checksum: 320
Coasting Arc #11 (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 = -2098039
53 A = 6788166
83 meter
Y = 3912606
96 meter E =
0018347
Z = -5148198
14 I = 51
59401
XDOT = -7256
588622 Wp = 67
88158
YDOT = -1869
492399 meter/sec RA = 185
02339 deg
ZDOT = 1547
639820 TA = 217
01291
MA = 217
13962
Ha = 229
381 n
mi
Hp = 217
888
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6883331
79 X = -2116626
52
Y = 12836637
02 feet Y = 3889041
75 meter
Z = -16890413
83 Z = -5158435
19
XDOT = -23807
705453 XDOT = -7242
662283
YDOT = -6133
505247 feet/sec YDOT = -1950
562380 meter/sec
ZDOT = 5077
558463 ZDOT = 1512
421477
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9614436
69 X = 2930480
30
Y = 10874738
32 feet Y = 3314620
24 meter
Z = -16933642
83 Z = -5161374
34
XDOT = -13363
487475 XDOT = -4073
190982
YDOT = 19435
693240 feet/sec YDOT = 5923
999300 meter/sec
ZDOT = 4930
715914 ZDOT = 1502
882211
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
51352875
00016717 00000-0 10270-3 0 9106
2 25544 51
6478 186
0599 0010360 19
9417 340
2137 15
50676071 32274
Satellite: ISS
Catalog Number: 25544
Epoch time: 13152
51352875 = yrday
fracday
Element set: 910
Inclination: 51
6478 deg
RA of node: 186
0599 deg
Eccentricity:
0010360
Arg of perigee: 19
9417 deg
Mean anomaly: 340
2137 deg
Mean motion: 15
50676071 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3227
Checksum: 304
Coasting Arc #12 (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 = 2484706
64 A = 6788758
04 meter
Y = -3918488
96 meter E =
0016039
Z = 4951690
10 I = 51
62602
XDOT = 7137
802949 Wp = 36
92634
YDOT = 1740
118091 meter/sec RA = 180
05796 deg
ZDOT = -2188
412782 TA = 74
51672
MA = 74
33965
Ha = 229
352 n
mi
Hp = 217
653
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8151924
66 X = 2504285
17
Y = -12855934
92 feet Y = -3890594
25 meter
Z = 16245702
44 Z = 4963808
00
XDOT = 23417
988677 XDOT = 7128
444884
YDOT = 5709
048854 feet/sec YDOT = 1819
885323 meter/sec
ZDOT = -7179
831961 ZDOT = -2153
760283
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9389436
36 X = -2861900
20
Y = -11912381
72 feet Y = -3630893
95 meter
Z = 16296792
09 Z = 4967262
23
XDOT = 12412
615376 XDOT = 3783
365166
YDOT = -19481
055807 feet/sec YDOT = -5937
825810 meter/sec
ZDOT = -7035
323590 ZDOT = -2144
366630
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
54463283
00016717 00000-0 10270-3 0 9117
2 25544 51
6465 180
9462 0010424 24
2503 335
9137 15
50742394 32439
Satellite: ISS
Catalog Number: 25544
Epoch time: 13153
54463283 = yrday
fracday
Element set: 911
Inclination: 51
6465 deg
RA of node: 180
9462 deg
Eccentricity:
0010424
Arg of perigee: 24
2503 deg
Mean anomaly: 335
9137 deg
Mean motion: 15
50742394 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3243
Checksum: 290
Coasting Arc #13 (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 = -2803798
34 A = 6789721
37 meter
Y = 3995404
20 meter E =
0016243
Z = -4730384
47 I = 51
66071
XDOT = -6949
451074 Wp = 69
79200
YDOT = -1606
683395 meter/sec RA = 175
09621 deg
ZDOT = 2775
261068 TA = 227
67479
MA = 227
81252
Ha = 229
491 n
mi
Hp = 217
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9198813
45 X = -2825288
23
Y = 13108281
50 feet Y = 3963930
56 meter
Z = -15519634
08 Z = -4744057
13
XDOT = -22800
036332 XDOT = -6944
449916
YDOT = -5271
270982 feet/sec YDOT = -1684
368785 meter/sec
ZDOT = 9105
187231 ZDOT = 2741
512888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9494790
45 X = 2894012
13
Y = 12825871
52 feet Y = 3909325
64 meter
Z = -15577234
32 Z = -4747941
02
XDOT = -11387
982531 XDOT = -3471
057076
YDOT = 19265
301873 feet/sec YDOT = 5872
064011 meter/sec
ZDOT = 8964
426757 ZDOT = 2732
357275
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
51127724
00016717 00000-0 10270-3 0 9123
2 25544 51
6474 176
1526 0010466 27
3285 332
8414 15
50731242 32584
Satellite: ISS
Catalog Number: 25544
Epoch time: 13154
51127724 = yrday
fracday
Element set: 912
Inclination: 51
6474 deg
RA of node: 176
1526 deg
Eccentricity:
0010466
Arg of perigee: 27
3285 deg
Mean anomaly: 332
8414 deg
Mean motion: 15
50731242 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3258
Checksum: 291
Coasting Arc #14 (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 = 3167235
45 A = 6790757
92 meter
Y = -4080763
40 meter E =
0018700
Z = 4402707
08 I = 51
69358
XDOT = 6707
217760 Wp = 49
80601
YDOT = 1540
504594 meter/sec RA = 170
13586 deg
ZDOT = -3375
928772 TA = 74
43947
MA = 74
23312
Ha = 229
452 n
mi
Hp = 217
234
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10391192
44 X = 3191244
59
Y = -13388331
37 feet Y = -4045211
53 meter
Z = 14444577
05 Z = 4418151
39
XDOT = 22005
307612 XDOT = 6705
892573
YDOT = 5054
148930 feet/sec YDOT = 1615
501827 meter/sec
ZDOT = -11075
881799 ZDOT = -3343
348352
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9615846
58 X = -2930910
04
Y = -13888022
44 feet Y = -4233069
24 meter
Z = 14509597
87 Z = 4422525
43
XDOT = 10520
229597 XDOT = 3206
565981
YDOT = -18786
255121 feet/sec YDOT = -5726
050561 meter/sec
ZDOT = -10939
978007 ZDOT = -3334
505296
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
54234517
00016717 00000-0 10270-3 0 9137
2 25544 51
6457 171
0381 0010515 31
3661 328
8115 15
50800290 32747
Satellite: ISS
Catalog Number: 25544
Epoch time: 13155
54234517 = yrday
fracday
Element set: 913
Inclination: 51
6457 deg
RA of node: 171
0381 deg
Eccentricity:
0010515
Arg of perigee: 31
3661 deg
Mean anomaly: 328
8115 deg
Mean motion: 15
50800290 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3274
Checksum: 278
Coasting Arc #15 (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 = -3440166
63 A = 6792019
89 meter
Y = 4225101
08 meter E =
0014372
Z = -4061843
16 I = 51
72808
XDOT = -6416
278150 Wp = 64
17116
YDOT = -1487
926788 meter/sec RA = 165
18009 deg
ZDOT = 3903
378409 TA = 246
24930
MA = 246
40011
Ha = 229
569 n
mi
Hp = 217
067
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11286635
94 X = -3467425
34
Y = 13861880
18 feet Y = 4186478
99 meter
Z = -13326257
09 Z = -4078621
17
XDOT = -21050
781332 XDOT = -6418
124770
YDOT = -4881
649566 feet/sec YDOT = -1559
688398 meter/sec
ZDOT = 12806
359610 ZDOT = 3872
203632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10047021
64 X = 3062332
20
Y = 14721072
51 feet Y = 4486982
90 meter
Z = -13396879
53 Z = -4083368
88
XDOT = -9685
441017 XDOT = -2952
122422
YDOT = 18096
210652 feet/sec YDOT = 5515
725007 meter/sec
ZDOT = 12676
307951 ZDOT = 3863
738663
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
50895526
00016717 00000-0 10270-3 0 9148
2 25544 51
6460 166
2445 0010546 34
5982 325
5853 15
50787946 32894
Satellite: ISS
Catalog Number: 25544
Epoch time: 13156
50895526 = yrday
fracday
Element set: 914
Inclination: 51
6460 deg
RA of node: 166
2445 deg
Eccentricity:
0010546
Arg of perigee: 34
5982 deg
Mean anomaly: 325
5853 deg
Mean motion: 15
50787946 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3289
Checksum: 336
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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