[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 6th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6996 54 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 129 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 331 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 928)
---------------------------------------
Vector Time (GMT): 2013/004/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2478551
42 A = 6784226
89 meter
Y = -3517125
30 meter E =
0017474
Z = 5230225
35 I = 51
49756
XDOT = 6830
384398 Wp = 111
52706
YDOT = 3369
026425 meter/sec RA = 200
40942 deg
ZDOT = -974
978373 TA = 347
78975
MA = 347
83205
Ha = 230
053 n
mi
Hp = 212
942
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8131730
38 X = 2492289
41
Y = -11539124
99 feet Y = -3489331
93 meter
Z = 17159531
99 Z = 5242299
20
XDOT = 22409
397631 XDOT = 6796
939766
YDOT = 11053
236302 feet/sec YDOT = 3445
221092 meter/sec
ZDOT = -3198
747943 ZDOT = -941
878094
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13088228
88 X = 3989292
16
Y = 5122366
45 feet Y = 1561297
30 meter
Z = 17210043
85 Z = 5245621
37
XDOT = -5159
719484 XDOT = -1572
682499
YDOT = 23429
938688 feet/sec YDOT = 7141
445312 meter/sec
ZDOT = -3061
680508 ZDOT = -933
200219
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 13004
54674472
00016717 00000-0 10270-3 0 9004
2 25544 51
6442 201
2530 0015600 121
4050 238
8629 15
51861730 9297
Satellite: ISS
Catalog Number: 25544
Epoch time: 13004
54674472 = yrday
fracday
Element set: 900
Inclination: 51
6442 deg
RA of node: 201
2530 deg
Eccentricity:
0015600
Arg of perigee: 121
4050 deg
Mean anomaly: 238
8629 deg
Mean motion: 15
51861730 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 929
Checksum: 275
Coasting Arc #2 (Orbit 943)
---------------------------------------
Vector Time (GMT): 2013/005/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3288874
38 A = 6785216
69 meter
Y = 3222105
94 meter E =
0028034
Z = -5009727
50 I = 51
52912
XDOT = -6500
160215 Wp = 116
28505
YDOT = -3469
052499 meter/sec RA = 195
42384 deg
ZDOT = 2032
893075 TA = 173
59256
MA = 173
55664
Ha = 230
054 n
mi
Hp = 212
862
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10790270
29 X = -3300324
24
Y = 10571213
73 feet Y = 3185263
87 meter
Z = -16436113
86 Z = -5025732
29
XDOT = -21325
984956 XDOT = -6470
760705
YDOT = -11381
405836 feet/sec YDOT = -3541
577062 meter/sec
ZDOT = 6669
596702 ZDOT = 2001
387048
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12900922
68 X = -3932201
23
Y = -7716613
29 feet Y = -2352023
73 meter
Z = -16502921
09 Z = -5030090
35
XDOT = 5132
599158 XDOT = 1564
416223
YDOT = -22588
394198 feet/sec YDOT = -6884
942551 meter/sec
ZDOT = 6539
146613 ZDOT = 1993
131888
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 13005
51267136
00016717 00000-0 10270-3 0 9018
2 25544 51
6432 196
4526 0015685 124
8683 235
3945 15
51889078 9443
Satellite: ISS
Catalog Number: 25544
Epoch time: 13005
51267136 = yrday
fracday
Element set: 901
Inclination: 51
6432 deg
RA of node: 196
4526 deg
Eccentricity:
0015685
Arg of perigee: 124
8683 deg
Mean anomaly: 235
3945 deg
Mean motion: 15
51889078 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 944
Checksum: 325
Coasting Arc #3 (Orbit 959)
---------------------------------------
Vector Time (GMT): 2013/006/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4030432
44 A = 6786853
69 meter
Y = -2949135
78 meter E =
0020820
Z = 4575204
87 I = 51
56435
XDOT = 6076
562679 Wp = 107
94023
YDOT = 3575
743215 meter/sec RA = 190
44416 deg
ZDOT = -3043
028176 TA = 12
47596
MA = 12
42450
Ha = 229
882 n
mi
Hp = 213
124
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13223203
55 X = 4040885
54
Y = -9675642
31 feet Y = -2904006
77 meter
Z = 15010514
68 Z = 4594809
66
XDOT = 19936
229262 XDOT = 6050
908612
YDOT = 11731
440994 feet/sec YDOT = 3643
551881 meter/sec
ZDOT = -9983
688241 ZDOT = -3013
570751
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12817762
37 X = 3906853
97
Y = 10085417
97 feet Y = 3074035
40 meter
Z = 15092250
64 Z = 4600117
99
XDOT = -5255
604972 XDOT = -1601
908395
YDOT = 21461
906593 feet/sec YDOT = 6541
589130 meter/sec
ZDOT = -9861
743920 ZDOT = -3005
859547
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 13006
54298580
00016717 00000-0 10270-3 0 9020
2 25544 51
6432 191
3339 0015593 128
8153 231
4394 15
51888838 9609
Satellite: ISS
Catalog Number: 25544
Epoch time: 13006
54298580 = yrday
fracday
Element set: 902
Inclination: 51
6432 deg
RA of node: 191
3339 deg
Eccentricity:
0015593
Arg of perigee: 128
8153 deg
Mean anomaly: 231
4394 deg
Mean motion: 15
51888838 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 960
Checksum: 323
Coasting Arc #4 (Orbit 974)
---------------------------------------
Vector Time (GMT): 2013/007/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4738790
23 A = 6788847
71 meter
Y = 2755499
32 meter E =
0022483
Z = -4030630
81 I = 51
60098
XDOT = -5455
253228 Wp = 125
18619
YDOT = -3646
318186 meter/sec RA = 185
46810 deg
ZDOT = 3923
837049 TA = 185
71125
MA = 185
73694
Ha = 229
947 n
mi
Hp = 213
056
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15547212
04 X = -4749670
82
Y = 9040352
08 feet Y = 2702446
68 meter
Z = -13223854
35 Z = -4053677
72
XDOT = -17897
812429 XDOT = -5433
134891
YDOT = -11962
986175 feet/sec YDOT = -3707
198885 meter/sec
ZDOT = 12873
481133 ZDOT = 3897
389250
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13039546
65 X = -3974453
82
Y = -12282718
78 feet Y = -3743772
68 meter
Z = -13319877
42 Z = -4059898
64
XDOT = 5501
865669 XDOT = 1676
968656
YDOT = -19672
484793 feet/sec YDOT = -5996
173365 meter/sec
ZDOT = 12764
030818 ZDOT = 3890
476593
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 13007
50889913
00016717 00000-0 10270-3 0 9034
2 25544 51
6427 186
5339 0015761 132
1625 228
0869 15
51910264 9752
Satellite: ISS
Catalog Number: 25544
Epoch time: 13007
50889913 = yrday
fracday
Element set: 903
Inclination: 51
6427 deg
RA of node: 186
5339 deg
Eccentricity:
0015761
Arg of perigee: 132
1625 deg
Mean anomaly: 228
0869 deg
Mean motion: 15
51910264 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 975
Checksum: 320
Coasting Arc #5 (Orbit 990)
---------------------------------------
Vector Time (GMT): 2013/008/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5335831
89 A = 6791077
63 meter
Y = -2562431
66 meter E =
0026126
Z = 3295943
91 I = 51
63849
XDOT = 4738
531806 Wp = 116
69583
YDOT = 3775
886187 meter/sec RA = 180
49819 deg
ZDOT = -4718
327357 TA = 24
95647
MA = 24
83038
Ha = 229
754 n
mi
Hp = 213
320
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17506010
12 X = 5348078
15
Y = -8406928
03 feet Y = -2502694
91 meter
Z = 10813464
28 Z = 3321894
42
XDOT = 15546
364194 XDOT = 4718
877244
YDOT = 12388
078040 feet/sec YDOT = 3828
765992 meter/sec
ZDOT = -15480
076630 ZDOT = -4695
355339
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13234512
02 X = 4033879
26
Y = 14129240
17 feet Y = 4306592
40 meter
Z = 10921543
07 Z = 3328886
33
XDOT = -6115
050365 XDOT = -1863
867351
YDOT = 17663
669393 feet/sec YDOT = 5383
886431 meter/sec
ZDOT = -15385
064702 ZDOT = -4689
367721
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 13008
53919829
00016717 00000-0 10270-3 0 9049
2 25544 51
6423 181
4145 0015648 136
1152 224
1245 15
51913417 9916
Satellite: ISS
Catalog Number: 25544
Epoch time: 13008
53919829 = yrday
fracday
Element set: 904
Inclination: 51
6423 deg
RA of node: 181
4145 deg
Eccentricity:
0015648
Arg of perigee: 136
1152 deg
Mean anomaly: 224
1245 deg
Mean motion: 15
51913417 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 991
Checksum: 299
Coasting Arc #6 (Orbit 1005)
---------------------------------------
Vector Time (GMT): 2013/009/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5838089
07 A = 6792992
95 meter
Y = 2438155
14 meter E =
0016751
Z = -2500016
10 I = 51
67614
XDOT = -3893
036566 Wp = 121
55198
YDOT = -3901
213777 meter/sec RA = 175
53333 deg
ZDOT = 5304
147022 TA = 210
51503
MA = 210
61260
Ha = 229
808 n
mi
Hp = 213
326
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19153835
53 X = -5852774
79
Y = 7999196
66 feet Y = 2372788
14 meter
Z = -8202152
55 Z = -2528412
28
XDOT = -12772
429680 XDOT = -3874
889025
YDOT = -12799
257798 feet/sec YDOT = -3944
647274 meter/sec
ZDOT = 17402
057158 ZDOT = 5285
278725
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13613412
28 X = -4149368
06
Y = -15606981
45 feet Y = -4757007
95 meter
Z = -8320396
95 Z = -2536056
99
XDOT = 6946
682311 XDOT = 2117
348768
YDOT = -15264
598356 feet/sec YDOT = -4652
649579 meter/sec
ZDOT = 17324
094549 ZDOT = 5280
384018
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 13009
50509759
00016717 00000-0 10270-3 0 9055
2 25544 51
6427 176
6148 0015825 139
3602 220
8734 15
51934151 10063
Satellite: ISS
Catalog Number: 25544
Epoch time: 13009
50509759 = yrday
fracday
Element set: 905
Inclination: 51
6427 deg
RA of node: 176
6148 deg
Eccentricity:
0015825
Arg of perigee: 139
3602 deg
Mean anomaly: 220
8734 deg
Mean motion: 15
51934151 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1006
Checksum: 302
Coasting Arc #7 (Orbit 1021)
---------------------------------------
Vector Time (GMT): 2013/010/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6194148
49 A = 6794599
59 meter
Y = -2271529
24 meter E =
0028782
Z = 1553482
49 I = 51
71152
XDOT = 2967
596802 Wp = 131
28659
YDOT = 4117
593078 meter/sec RA = 170
57346 deg
ZDOT = -5761
189910 TA = 31
73527
MA = 31
56210
Ha = 229
605 n
mi
Hp = 213
545
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20322009
49 X = 6211542
53
Y = -7452523
75 feet Y = -2202165
31 meter
Z = 5096727
32 Z = 1583614
78
XDOT = 9736
209980 XDOT = 2949
318447
YDOT = 13509
163643 feet/sec YDOT = 4150
677047 meter/sec
ZDOT = -18901
541699 ZDOT = -5746
817681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13757959
74 X = 4193426
13
Y = 16671775
89 feet Y = 5081557
29 meter
Z = 5222187
45 Z = 1591722
74
XDOT = -8261
432523 XDOT = -2518
084633
YDOT = 12770
344509 feet/sec YDOT = 3892
401006 meter/sec
ZDOT = -18842
272855 ZDOT = -5743
124766
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 13010
53538101
00016717 00000-0 10270-3 0 9064
2 25544 51
6423 171
4949 0015641 143
2239 216
9989 15
51953061 10224
Satellite: ISS
Catalog Number: 25544
Epoch time: 13010
53538101 = yrday
fracday
Element set: 906
Inclination: 51
6423 deg
RA of node: 171
4949 deg
Eccentricity:
0015641
Arg of perigee: 143
2239 deg
Mean anomaly: 216
9989 deg
Mean motion: 15
51953061 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1022
Checksum: 292
Coasting Arc #8 (Orbit 1036)
---------------------------------------
Vector Time (GMT): 2013/011/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6423105
51 A = 6795435
71 meter
Y = 2146886
90 meter E =
0016480
Z = -614106
99 I = 51
74593
XDOT = -2010
982765 Wp = 108
58305
YDOT = -4344
650329 meter/sec RA = 165
61795 deg
ZDOT = 5971
190632 TA = 244
81325
MA = 244
98423
Ha = 229
630 n
mi
Hp = 213
652
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21073180
82 X = -6443651
96
Y = 7043592
21 feet Y = 2074944
90 meter
Z = -2014786
71 Z = -645359
04
XDOT = -6597
712484 XDOT = -1991
256457
YDOT = -14254
102128 feet/sec YDOT = -4367
028690 meter/sec
ZDOT = 19590
520445 ZDOT = 5961
469103
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13927295
06 X = -4245039
53
Y = -17296830
17 feet Y = -5272073
84 meter
Z = -2144906
69 Z = -653767
56
XDOT = 9765
794646 XDOT = 2976
614208
YDOT = -10239
407327 feet/sec YDOT = -3120
971353 meter/sec
ZDOT = 19550
594454 ZDOT = 5959
021190
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 13011
50126626
00016717 00000-0 10270-3 0 9078
2 25544 51
6438 166
6958 0015847 146
5487 213
6668 15
51963315 10372
Satellite: ISS
Catalog Number: 25544
Epoch time: 13011
50126626 = yrday
fracday
Element set: 907
Inclination: 51
6438 deg
RA of node: 166
6958 deg
Eccentricity:
0015847
Arg of perigee: 146
5487 deg
Mean anomaly: 213
6668 deg
Mean motion: 15
51963315 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1037
Checksum: 324
Coasting Arc #9 (Orbit 1052)
---------------------------------------
Vector Time (GMT): 2013/012/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6488553
97 A = 6795514
69 meter
Y = -1926046
23 meter E =
0026785
Z = -420102
08 I = 51
77553
XDOT = 1008
697515 Wp = 145
23921
YDOT = 4663
551365 meter/sec RA = 160
66506 deg
ZDOT = -6011
182220 TA = 39
28363
MA = 39
08959
Ha = 229
477 n
mi
Hp = 213
822
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21287906
72 X = 6511649
88
Y = -6319049
31 feet Y = -1853357
99 meter
Z = -1378287
67 Z = -388525
95
XDOT = 3309
375050 XDOT = 985
673840
YDOT = 15300
365370 feet/sec YDOT = 4674
702977 meter/sec
ZDOT = -19721
726444 ZDOT = -6006
337724
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13633812
90 X = 4155586
17
Y = 17537662
41 feet Y = 5345479
50 meter
Z = -1246826
65 Z = -380032
76
XDOT = -11723
572267 XDOT = -3573
344827
YDOT = 7767
283981 feet/sec YDOT = 2367
468157 meter/sec
ZDOT = -19702
099837 ZDOT = -6005
200030
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 13012
53153454
00016717 00000-0 10270-3 0 9082
2 25544 51
6437 161
5758 0015641 150
1715 210
0332 15
51985025 10539
Satellite: ISS
Catalog Number: 25544
Epoch time: 13012
53153454 = yrday
fracday
Element set: 908
Inclination: 51
6437 deg
RA of node: 161
5758 deg
Eccentricity:
0015641
Arg of perigee: 150
1715 deg
Mean anomaly: 210
0332 deg
Mean motion: 15
51985025 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1053
Checksum: 275
Coasting Arc #10 (Orbit 1068)
---------------------------------------
Vector Time (GMT): 2013/013/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6431016
84 A = 6794758
20 meter
Y = 1716621
27 meter E =
0020213
Z = 1372958
51 I = 51
80340
XDOT = -73
306065 Wp = 111
48295
YDOT = -4984
441890 meter/sec RA = 155
71432 deg
ZDOT = 5812
589723 TA = 263
41226
MA = 263
64239
Ha = 229
406 n
mi
Hp = 214
002
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21099136
63 X = -6456403
82
Y = 5631959
55 feet Y = 1644563
60 meter
Z = 4504457
06 Z = 1341656
29
XDOT = -240
505463 XDOT = -45
798932
YDOT = -16353
155806 feet/sec YDOT = -4985
108134 meter/sec
ZDOT = 19070
176258 ZDOT = 5812
300180
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13233680
20 X = -4033625
73
Y = -17404575
80 feet Y = -5304914
71 meter
Z = 4374141
93 Z = 1333238
46
XDOT = 13721
594242 XDOT = 4182
341925
YDOT = -5576
082815 feet/sec YDOT = -1699
590042 meter/sec
ZDOT = 19069
516067 ZDOT = 5812
388497
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 13013
56179519
00016717 00000-0 10270-3 0 9097
2 25544 51
6455 156
4572 0015820 154
1655 206
0290 15
52004383 10697
Satellite: ISS
Catalog Number: 25544
Epoch time: 13013
56179519 = yrday
fracday
Element set: 909
Inclination: 51
6455 deg
RA of node: 156
4572 deg
Eccentricity:
0015820
Arg of perigee: 154
1655 deg
Mean anomaly: 206
0290 deg
Mean motion: 15
52004383 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1069
Checksum: 298
Coasting Arc #11 (Orbit 1083)
---------------------------------------
Vector Time (GMT): 2013/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6217099
74 A = 6793278
08 meter
Y = -1361289
33 meter E =
0021155
Z = -2351427
12 I = 51
82582
XDOT = -860
247262 Wp = 151
80072
YDOT = 5361
406513 meter/sec RA = 150
76328 deg
ZDOT = -5416
292711 TA = 54
35747
MA = 54
16065
Ha = 229
349 n
mi
Hp = 214
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20397308
87 X = 6243282
28
Y = -4466172
36 feet Y = -1291619
37 meter
Z = -7714655
91 Z = -2321162
04
XDOT = -2822
333537 XDOT = -893
825332
YDOT = 17589
916381 feet/sec YDOT = 5351
599086 meter/sec
ZDOT = -17769
989209 ZDOT = -5420
553051
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12190800
72 X = 3715756
06
Y = 17009090
51 feet Y = 5184370
79 meter
Z = -7588678
29 Z = -2313029
14
XDOT = -15986
547447 XDOT = -4872
699662
YDOT = 3578
144389 feet/sec YDOT = 1090
618410 meter/sec
ZDOT = -17788
285702 ZDOT = -5421
869482
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 13014
52765845
00016717 00000-0 10270-3 0 9109
2 25544 51
6455 151
6576 0015660 157
4804 202
7038 15
51992019 10843
Satellite: ISS
Catalog Number: 25544
Epoch time: 13014
52765845 = yrday
fracday
Element set: 910
Inclination: 51
6455 deg
RA of node: 151
6576 deg
Eccentricity:
0015660
Arg of perigee: 157
4804 deg
Mean anomaly: 202
7038 deg
Mean motion: 15
51992019 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1084
Checksum: 306
Coasting Arc #12 (Orbit 1099)
---------------------------------------
Vector Time (GMT): 2013/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5916517
37 A = 6791241
48 meter
Y = 996763
65 meter E =
0022612
Z = 3182326
08 I = 51
84670
XDOT = 1655
441120 Wp = 128
06504
YDOT = -5711
417039 meter/sec RA = 145
81182 deg
ZDOT = 4829
727262 TA = 268
50953
MA = 268
76856
Ha = 229
149 n
mi
Hp = 214
393
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19411146
22 X = -5942682
29
Y = 3270221
95 feet Y = 930455
12 meter
Z = 10440702
37 Z = 3153521
10
XDOT = 5431
237270 XDOT = 1695
723233
YDOT = -18738
244880 feet/sec YDOT = -5692
679676 meter/sec
ZDOT = 15845
561884 ZDOT = 4837
866900
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10992911
85 X = -3350639
53
Y = -16405233
59 feet Y = -5000315
20 meter
Z = 10320824
33 Z = 3145787
26
XDOT = 18076
069876 XDOT = 5509
586098
YDOT = -2044
938094 feet/sec YDOT = -623
297131 meter/sec
ZDOT = 15880
029080 ZDOT = 4840
232864
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 13015
55790247
00016717 00000-0 10270-3 0 9118
2 25544 51
6466 146
5390 0015686 161
5466 198
6258 15
52037004 11001
Satellite: ISS
Catalog Number: 25544
Epoch time: 13015
55790247 = yrday
fracday
Element set: 911
Inclination: 51
6466 deg
RA of node: 146
5390 deg
Eccentricity:
0015686
Arg of perigee: 161
5466 deg
Mean anomaly: 198
6258 deg
Mean motion: 15
52037004 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1100
Checksum: 303
Coasting Arc #13 (Orbit 1114)
---------------------------------------
Vector Time (GMT): 2013/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5491674
65 A = 6788977
07 meter
Y = -457125
10 meter E =
0016779
Z = -3963752
74 I = 51
86356
XDOT = -2400
711940 Wp = 142
07436
YDOT = 6049
461954 meter/sec RA = 140
85798 deg
ZDOT = -4045
745734 TA = 85
86130
MA = 85
66955
Ha = 229
106 n
mi
Hp = 214
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18017305
29 X = 5515632
75
Y = -1499754
28 feet Y = -395579
79 meter
Z = -13004438
12 Z = -3937016
84
XDOT = -7876
351510 XDOT = -2448
526995
YDOT = 19847
316122 feet/sec YDOT = 6022
348350 meter/sec
ZDOT = -13273
444010 ZDOT = -4057
524147
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9084277
66 X = 2768887
83
Y = 15723514
78 feet Y = 4792527
31 meter
Z = -12893213
17 Z = -3929851
37
XDOT = -20127
799186 XDOT = -6134
953192
YDOT = 763
575533 feet/sec YDOT = 232
737822 meter/sec
ZDOT = -13323
085366 ZDOT = -4060
876420
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 13016
52375137
00016717 00000-0 10270-3 0 9124
2 25544 51
6466 141
7397 0015570 164
9701 195
1916 15
52002522 11152
Satellite: ISS
Catalog Number: 25544
Epoch time: 13016
52375137 = yrday
fracday
Element set: 912
Inclination: 51
6466 deg
RA of node: 141
7397 deg
Eccentricity:
0015570
Arg of perigee: 164
9701 deg
Mean anomaly: 195
1916 deg
Mean motion: 15
52002522 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1115
Checksum: 290
Coasting Arc #14 (Orbit 1130)
---------------------------------------
Vector Time (GMT): 2013/017/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5035129
57 A = 6786724
21 meter
Y = -92090
21 meter E =
0021734
Z = 4549725
82 I = 51
88018
XDOT = 2979
172843 Wp = 148
96458
YDOT = -6322
114451 meter/sec RA = 135
90260 deg
ZDOT = 3144
206010 TA = 269
47771
MA = 269
72676
Ha = 228
881 n
mi
Hp = 214
793
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16519453
97 X = -5055826
69
Y = -302133
23 feet Y = -148511
93 meter
Z = 14926921
99 Z = 4525215
59
XDOT = 9774
189116 XDOT = 3034
373097
YDOT = -20741
845312 feet/sec YDOT = -6288
490847 meter/sec
ZDOT = 10315
636517 ZDOT = 3158
812462
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7080106
36 X = -2158016
42
Y = -15029569
94 feet Y = -4581012
92 meter
Z = 14825004
75 Z = 4518661
45
XDOT = 21800
907408 XDOT = 6644
916578
YDOT = 46
858048 feet/sec YDOT = 14
282333 meter/sec
ZDOT = 10377
078263 ZDOT = 3162
933454
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 13017
55397950
00016717 00000-0 10270-3 0 9136
2 25544 51
6472 136
6208 0015511 168
6972 191
4531 15
52058424 11311
Satellite: ISS
Catalog Number: 25544
Epoch time: 13017
55397950 = yrday
fracday
Element set: 913
Inclination: 51
6472 deg
RA of node: 136
6208 deg
Eccentricity:
0015511
Arg of perigee: 168
6972 deg
Mean anomaly: 191
4531 deg
Mean motion: 15
52058424 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1131
Checksum: 301
Coasting Arc #15 (Orbit 1145)
---------------------------------------
Vector Time (GMT): 2013/018/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4504202
72 A = 6784928
10 meter
Y = 812405
36 meter E =
0018536
Z = -5017127
21 I = 51
89518
XDOT = -3474
426727 Wp = 130
23643
YDOT = 6498
250487 meter/sec RA = 130
94464 deg
ZDOT = -2083
698186 TA = 119
62534
MA = 119
44057
Ha = 228
758 n
mi
Hp = 215
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14777567
97 X = 4519155
11
Y = 2665371
93 feet Y = 862857
86 meter
Z = -16460391
12 Z = -4995210
05
XDOT = -11399
037818 XDOT = -3536
711350
YDOT = 21319
719446 feet/sec YDOT = 6459
049047 meter/sec
ZDOT = -6836
280137 ZDOT = -2100
727692
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4443515
63 X = 1354383
56
Y = 14447330
68 feet Y = 4403546
39 meter
Z = -16369331
18 Z = -4989372
15
XDOT = -23099
588053 XDOT = -7040
754438
YDOT = -659
667285 feet/sec YDOT = -201
066589 meter/sec
ZDOT = -6907
831558 ZDOT = -2105
507059
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 13018
51981312
00016717 00000-0 10270-3 0 9145
2 25544 51
6471 131
8216 0015398 172
2815 187
8577 15
52027400 11461
Satellite: ISS
Catalog Number: 25544
Epoch time: 13018
51981312 = yrday
fracday
Element set: 914
Inclination: 51
6471 deg
RA of node: 131
8216 deg
Eccentricity:
0015398
Arg of perigee: 172
2815 deg
Mean anomaly: 187
8577 deg
Mean motion: 15
52027400 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1146
Checksum: 300
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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