[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 22nd 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 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
080/00:30:36
723 1
7 4
6 4
6
N/A 3
3 -0
8 228
3
000/00:11:13
445 -2
7 0
2 214
0
Coasting Arc #1 (Orbit 2091)
---------------------------------------
Vector Time (GMT): 2013/079/09:17:42
880
Vector Time (MET): N/A
Weight (LBS) : 907286
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5885760
46 A = 6790679
25 meter
Y = 2598319
24 meter E =
0012888
Z = -2193605
38 I = 51
60287
XDOT = -3728
008507 Wp = 63
57156
YDOT = 3844
464400 meter/sec RA = 188
14288 deg
ZDOT = -5468
389861 TA = 140
74417
MA = 140
65065
Ha = 226
950 n
mi
Hp = 213
016
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19310237
74 X = 5866923
93
Y = 8524669
42 feet Y = 2664032
01 meter
Z = -7196868
05 Z = -2165059
05
XDOT = -12230
999038 XDOT = -3744
157263
YDOT = 12613
072179 feet/sec YDOT = 3802
684705 meter/sec
ZDOT = -17940
911618 ZDOT = -5486
539624
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8235393
75 X = 2510148
02
Y = 19478886
42 feet Y = 5937164
58 meter
Z = -7078238
03 Z = -2157446
95
XDOT = -16049
857624 XDOT = -4891
996604
YDOT = 262
140517 feet/sec YDOT = 79
900430 meter/sec
ZDOT = -18016
890128 ZDOT = -5491
548111
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 13079
41526500
00016717 00000-0 10270-3 0 9000
2 25544 51
6443 189
0712 0012772 34
9433 325
2555 15
52984815 20926
Satellite: ISS
Catalog Number: 25544
Epoch time: 13079
41526500 = yrday
fracday
Element set: 900
Inclination: 51
6443 deg
RA of node: 189
0712 deg
Eccentricity:
0012772
Arg of perigee: 34
9433 deg
Mean anomaly: 325
2555 deg
Mean motion: 15
52984815 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2092
Checksum: 300
Coasting Arc #2 (Orbit 2101)
---------------------------------------
Vector Time (GMT): 2013/080/00:36:13
445
Vector Time (MET): N/A
Weight (LBS) : 906812
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6759903
46 A = 6795071
28 meter
Y = 56825
13 meter E =
0019954
Z = 664767
11 I = 51
62920
XDOT = 560
861512 Wp = 92
57842
YDOT = 4783
749699 meter/sec RA = 184
94713 deg
ZDOT = -5958
316951 TA = 80
25091
MA = 80
02561
Ha = 228
348 n
mi
Hp = 214
022
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22178160
94 X = 6755536
38
Y = 186434
17 feet Y = 132394
27 meter
Z = 2180994
44 Z = 697595
25
XDOT = 1840
096825 XDOT = 536
270593
YDOT = 15694
716859 feet/sec YDOT = 4789
883579 meter/sec
ZDOT = -19548
283961 ZDOT = -5955
652513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22024265
46 X = -6712996
11
Y = 2494434
85 feet Y = 760303
74 meter
Z = 2317723
69 Z = 706442
18
XDOT = -3661
672820 XDOT = -1116
077875
YDOT = -13735
153268 feet/sec YDOT = -4186
474716 meter/sec
ZDOT = -19537
666666 ZDOT = -5955
080800
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 13080
05879101
00016717 00000-0 10270-3 0 9011
2 25544 51
6452 185
8748 0011926 52
4646 307
7588 15
52082267 21023
Satellite: ISS
Catalog Number: 25544
Epoch time: 13080
05879101 = yrday
fracday
Element set: 901
Inclination: 51
6452 deg
RA of node: 185
8748 deg
Eccentricity:
0011926
Arg of perigee: 52
4646 deg
Mean anomaly: 307
7588 deg
Mean motion: 15
52082267 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2102
Checksum: 308
Coasting Arc #3 (Orbit 2117)
---------------------------------------
Vector Time (GMT): 2013/081/00:36:13
445
Vector Time (MET): N/A
Weight (LBS) : 906812
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6770101
50 A = 6795189
74 meter
Y = -269049
51 meter E =
0024603
Z = 342307
07 I = 51
66038
XDOT = 506
415302 Wp = 52
18038
YDOT = -4748
466683 meter/sec RA = 179
98584 deg
ZDOT = 6003
902564 TA = 311
50802
MA = 311
71890
Ha = 228
359 n
mi
Hp = 213
926
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22211619
10 X = -6768252
58
Y = -882708
38 feet Y = -344746
68 meter
Z = 1123054
68 Z = 309423
34
XDOT = 1661
467526 XDOT = 530
310954
YDOT = -15578
958933 feet/sec YDOT = -4742
669425 meter/sec
ZDOT = 19697
843059 ZDOT = 6006
421174
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22127444
08 X = 6744444
96
Y = -2190952
87 feet Y = -667802
43 meter
Z = 986099
91 Z = 300563
25
XDOT = 464
053282 XDOT = 141
443440
YDOT = 14027
513044 feet/sec YDOT = 4275
585976 meter/sec
ZDOT = 19708
809709 ZDOT = 6007
245199
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 13081
08896616
00016717 00000-0 10270-3 0 9026
2 25544 51
6453 180
7551 0012011 55
4427 304
7856 15
52104279 21186
Satellite: ISS
Catalog Number: 25544
Epoch time: 13081
08896616 = yrday
fracday
Element set: 902
Inclination: 51
6453 deg
RA of node: 180
7551 deg
Eccentricity:
0012011
Arg of perigee: 55
4427 deg
Mean anomaly: 304
7856 deg
Mean motion: 15
52104279 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2118
Checksum: 296
Coasting Arc #4 (Orbit 2132)
---------------------------------------
Vector Time (GMT): 2013/082/00:36:13
445
Vector Time (MET): N/A
Weight (LBS) : 906812
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6623559
54 A = 6794352
79 meter
Y = 550415
06 meter E =
0015531
Z = -1420934
75 I = 51
68924
XDOT = -1624
428937 Wp = 93
15871
YDOT = 4735
708237 meter/sec RA = 175
02608 deg
ZDOT = -5793
292904 TA = 102
29392
MA = 102
11999
Ha = 228
377 n
mi
Hp = 213
848
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21730838
38 X = 6623814
86
Y = 1805823
70 feet Y = 624485
14 meter
Z = -4661859
41 Z = -1388757
84
XDOT = -5329
491263 XDOT = -1649
121913
YDOT = 15537
100515 feet/sec YDOT = 4717
404124 meter/sec
ZDOT = -19006
866482 ZDOT = -5801
244676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21776103
48 X = -6637356
34
Y = 1588408
26 feet Y = 484146
84 meter
Z = -4527863
23 Z = -1380092
71
XDOT = 2857
379560 XDOT = 870
929290
YDOT = -14567
880786 feet/sec YDOT = -4440
290064 meter/sec
ZDOT = -19040
465935 ZDOT = -5803
534017
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 13082
05473960
00016717 00000-0 10270-3 0 9038
2 25544 51
6462 175
9548 0011910 59
2695 300
9628 15
52122152 21336
Satellite: ISS
Catalog Number: 25544
Epoch time: 13082
05473960 = yrday
fracday
Element set: 903
Inclination: 51
6462 deg
RA of node: 175
9548 deg
Eccentricity:
0011910
Arg of perigee: 59
2695 deg
Mean anomaly: 300
9628 deg
Mean motion: 15
52122152 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2133
Checksum: 298
Coasting Arc #5 (Orbit 2148)
---------------------------------------
Vector Time (GMT): 2013/083/00:36:13
445
Vector Time (MET): N/A
Weight (LBS) : 906812
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6298092
19 A = 6792771
44 meter
Y = -802536
97 meter E =
0025768
Z = 2377908
98 I = 51
71469
XDOT = 2656
443378 Wp = 68
38033
YDOT = -4780
416345 meter/sec RA = 170
06640 deg
ZDOT = 5384
898289 TA = 318
16067
MA = 318
35735
Ha = 228
460 n
mi
Hp = 213
670
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20663032
12 X = -6300201
11
Y = -2632995
32 feet Y = -872977
69 meter
Z = 7801538
66 Z = 2347308
66
XDOT = 8715
365412 XDOT = 2683
543412
YDOT = -15683
780660 feet/sec YDOT = -4750
558093 meter/sec
ZDOT = 17666
989136 ZDOT = 5397
869394
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20854943
36 X = 6356586
74
Y = -967845
50 feet Y = -294999
31 meter
Z = 7674123
96 Z = 2339072
98
XDOT = -5852
105838 XDOT = -1783
721860
YDOT = 15408
000964 feet/sec YDOT = 4696
358694 meter/sec
ZDOT = 17721
507423 ZDOT = 5401
515463
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 13083
08488285
00016717 00000-0 10270-3 0 9049
2 25544 51
6463 170
8350 0012087 62
3267 297
9105 15
52152323 21493
Satellite: ISS
Catalog Number: 25544
Epoch time: 13083
08488285 = yrday
fracday
Element set: 904
Inclination: 51
6463 deg
RA of node: 170
8350 deg
Eccentricity:
0012087
Arg of perigee: 62
3267 deg
Mean anomaly: 297
9105 deg
Mean motion: 15
52152323 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2149
Checksum: 306
Coasting Arc #6 (Orbit 2163)
---------------------------------------
Vector Time (GMT): 2013/084/00:36:13
445
Vector Time (MET): N/A
Weight (LBS) : 906812
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5822551
10 A = 6790459
76 meter
Y = 1156758
60 meter E =
0016049
Z = -3315062
23 I = 51
73785
XDOT = -3630
779167 Wp = 74
55024
YDOT = 4811
900084 meter/sec RA = 165
10546 deg
ZDOT = -4712
891027 TA = 143
83547
MA = 143
72684
Ha = 228
338 n
mi
Hp = 213
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19102857
93 X = 5825286
82
Y = 3795139
78 feet Y = 1221884
85 meter
Z = -10876188
43 Z = -3286770
49
XDOT = -11912
005140 XDOT = -3661
423187
YDOT = 15787
073765 feet/sec YDOT = 4771
126397 meter/sec
ZDOT = -15462
240902 ZDOT = -4730
604058
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19541213
29 X = -5956161
81
Y = -105656
84 feet Y = -32204
21 meter
Z = -10758418
17 Z = -3279165
86
XDOT = 8614
638687 XDOT = 2625
741872
YDOT = -16308
617660 feet/sec YDOT = -4970
866663 meter/sec
ZDOT = -15536
524765 ZDOT = -4735
532748
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 13084
05062631
00016717 00000-0 10270-3 0 9051
2 25544 51
6468 166
0348 0011899 65
6364 294
6028 15
52179157 21645
Satellite: ISS
Catalog Number: 25544
Epoch time: 13084
05062631 = yrday
fracday
Element set: 905
Inclination: 51
6468 deg
RA of node: 166
0348 deg
Eccentricity:
0011899
Arg of perigee: 65
6364 deg
Mean anomaly: 294
6028 deg
Mean motion: 15
52179157 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2164
Checksum: 320
Coasting Arc #7 (Orbit 2179)
---------------------------------------
Vector Time (GMT): 2013/085/00:36:13
445
Vector Time (MET): N/A
Weight (LBS) : 906812
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5205087
89 A = 6788043
21 meter
Y = -1523506
26 meter E =
0021927
Z = 4061784
89 I = 51
75920
XDOT = 4475
230278 Wp = 84
79795
YDOT = -4875
697325 meter/sec RA = 160
14248 deg
ZDOT = 3890
021393 TA = 324
95151
MA = 325
09561
Ha = 228
500 n
mi
Hp = 213
447
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17077060
00 X = -5207395
88
Y = -4998380
11 feet Y = -1581725
11 meter
Z = 13326065
92 Z = 4036493
71
XDOT = 14682
514034 XDOT = 4510
522111
YDOT = -15996
382300 feet/sec YDOT = -4825
454556 meter/sec
ZDOT = 12762
537377 ZDOT = 3911
848092
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17820005
54 X = 5431537
69
Y = 1360486
73 feet Y = 414676
36 meter
Z = 13220828
00 Z = 4029708
37
XDOT = -10901
208467 XDOT = -3322
688341
YDOT = 17358
223056 feet/sec YDOT = 5290
786388 meter/sec
ZDOT = 12853
975832 ZDOT = 3917
891833
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 13085
08073844
00016717 00000-0 10270-3 0 9064
2 25544 51
6467 160
9146 0012094 69
1492 291
0954 15
52202739 21802
Satellite: ISS
Catalog Number: 25544
Epoch time: 13085
08073844 = yrday
fracday
Element set: 906
Inclination: 51
6467 deg
RA of node: 160
9146 deg
Eccentricity:
0012094
Arg of perigee: 69
1492 deg
Mean anomaly: 291
0954 deg
Mean motion: 15
52202739 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2180
Checksum: 310
Coasting Arc #8 (Orbit 2194)
---------------------------------------
Vector Time (GMT): 2013/086/00:36:13
445
Vector Time (MET): N/A
Weight (LBS) : 906812
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4486764
12 A = 6785613
84 meter
Y = 2003762
43 meter E =
0022450
Z = -4701302
74 I = 51
77968
XDOT = -5161
776103 Wp = 71
63644
YDOT = 4866
120203 meter/sec RA = 155
17681 deg
ZDOT = -2856
537496 TA = 169
99740
MA = 169
95265
Ha = 228
278 n
mi
Hp = 213
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14720354
74 X = 4486861
89
Y = 6574023
73 feet Y = 2053936
09 meter
Z = -15424221
59 Z = -4679506
44
XDOT = -16934
960969 XDOT = -5201
930130
YDOT = 15964
961296 feet/sec YDOT = 4808
173024 meter/sec
ZDOT = -9371
842180 ZDOT = -2881
711285
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15906415
88 X = -4848275
56
Y = -3111297
98 feet Y = -948323
62 meter
Z = -15333590
64 Z = -4673678
43
XDOT = 12674
228982 XDOT = 3863
104994
YDOT = -18159
705295 feet/sec YDOT = -5535
078174 meter/sec
ZDOT = -9477
237140 ZDOT = -2888
661880
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 13086
04645221
00016717 00000-0 10270-3 0 9076
2 25544 51
6464 156
1142 0011924 72
0542 288
1908 15
52245083 21953
Satellite: ISS
Catalog Number: 25544
Epoch time: 13086
04645221 = yrday
fracday
Element set: 907
Inclination: 51
6464 deg
RA of node: 156
1142 deg
Eccentricity:
0011924
Arg of perigee: 72
0542 deg
Mean anomaly: 288
1908 deg
Mean motion: 15
52245083 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2195
Checksum: 293
Coasting Arc #9 (Orbit 2210)
---------------------------------------
Vector Time (GMT): 2013/087/00:36:13
445
Vector Time (MET): N/A
Weight (LBS) : 906812
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3681893
31 A = 6783825
72 meter
Y = -2515252
88 meter E =
0016041
Z = 5098690
43 I = 51
80101
XDOT = 5706
225987 Wp = 90
68915
YDOT = -4835
580566 meter/sec RA = 150
20964 deg
ZDOT = 1730
272859 TA = 342
61738
MA = 342
67224
Ha = 228
441 n
mi
Hp = 213
278
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12079702
47 X = -3678261
82
Y = -8252142
01 feet Y = -2556405
12 meter
Z = 16727986
96 Z = 5080813
16
XDOT = 18721
213868 XDOT = 5751
469118
YDOT = -15864
765636 feet/sec YDOT = -4771
516742 meter/sec
ZDOT = 5676
748225 ZDOT = 1758
103967
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13802984
57 X = 4207149
70
Y = 5096396
28 feet Y = 1553381
59 meter
Z = 16653737
40 Z = 5076059
16
XDOT = -13975
618953 XDOT = -4259
768657
YDOT = 18867
949880 feet/sec YDOT = 5750
951124 meter/sec
ZDOT = 5793
226872 ZDOT = 1765
775550
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 13087
07653309
00016717 00000-0 10270-3 0 9087
2 25544 51
6461 150
9937 0012035 75
9971 284
2518 15
52256320 22115
Satellite: ISS
Catalog Number: 25544
Epoch time: 13087
07653309 = yrday
fracday
Element set: 908
Inclination: 51
6461 deg
RA of node: 150
9937 deg
Eccentricity:
0012035
Arg of perigee: 75
9971 deg
Mean anomaly: 284
2518 deg
Mean motion: 15
52256320 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2211
Checksum: 306
Coasting Arc #10 (Orbit 2225)
---------------------------------------
Vector Time (GMT): 2013/088/00:36:13
445
Vector Time (MET): N/A
Weight (LBS) : 906812
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2855446
44 A = 6782793
02 meter
Y = 3117057
75 meter E =
0026580
Z = -5327418
33 I = 51
82295
XDOT = -6034
242322 Wp = 83
09209
YDOT = 4668
076338 meter/sec RA = 145
24056 deg
ZDOT = -502
060973 TA = 182
11054
MA = 182
12178
Ha = 228
222 n
mi
Hp = 213
287
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9368262
58 X = 2846258
04
Y = 10226567
42 feet Y = 3148937
13 meter
Z = -17478406
59 Z = -5313569
38
XDOT = -19797
382945 XDOT = -6083
554365
YDOT = 15315
211082 feet/sec YDOT = 4600
321860 meter/sec
ZDOT = -1647
181671 ZDOT = -531
495427
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11777307
79 X = -3589723
41
Y = -7459574
52 feet Y = -2273678
31 meter
Z = -17421007
18 Z = -5309922
99
XDOT = 14664
214464 XDOT = 4469
652569
YDOT = -19010
321210 feet/sec YDOT = -5794
345905 meter/sec
ZDOT = -1770
341229 ZDOT = -539
600007
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 13088
04221802
00016717 00000-0 10270-3 0 9095
2 25544 51
6450 146
1923 0011922 78
9738 281
2754 15
52299629 22267
Satellite: ISS
Catalog Number: 25544
Epoch time: 13088
04221802 = yrday
fracday
Element set: 909
Inclination: 51
6450 deg
RA of node: 146
1923 deg
Eccentricity:
0011922
Arg of perigee: 78
9738 deg
Mean anomaly: 281
2754 deg
Mean motion: 15
52299629 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2226
Checksum: 316
Coasting Arc #11 (Orbit 2241)
---------------------------------------
Vector Time (GMT): 2013/089/00:36:13
445
Vector Time (MET): N/A
Weight (LBS) : 906812
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2000422
91 A = 6782778
56 meter
Y = -3735115
30 meter E =
0014830
Z = 5284292
91 I = 51
84774
XDOT = 6236
384718 Wp = 78
99723
YDOT = -4412
701369 meter/sec RA = 140
27312 deg
ZDOT = -753
646703 TA = 18
20094
MA = 18
14792
Ha = 228
276 n
mi
Hp = 213
171
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6563067
29 X = -1984177
34
Y = -12254315
30 feet Y = -3757393
95 meter
Z = 17336918
99 Z = 5274614
74
XDOT = 20460
579783 XDOT = 6288
926037
YDOT = -14477
366696 feet/sec YDOT = -4342
668485 meter/sec
ZDOT = -2472
594170 ZDOT = -723
222509
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9756691
62 X = 2973839
60
Y = 9971592
40 feet Y = 3039341
36 meter
Z = 17296969
95 Z = 5272116
44
XDOT = -15027
795946 XDOT = -4580
472204
YDOT = 18798
135451 feet/sec YDOT = 5729
671685 meter/sec
ZDOT = -2345
317387 ZDOT = -714
852739
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 13089
07226717
00016717 00000-0 10270-3 0 9101
2 25544 51
6449 141
0715 0011900 82
8672 277
3833 15
52319224 22421
Satellite: ISS
Catalog Number: 25544
Epoch time: 13089
07226717 = yrday
fracday
Element set: 910
Inclination: 51
6449 deg
RA of node: 141
0715 deg
Eccentricity:
0011900
Arg of perigee: 82
8672 deg
Mean anomaly: 277
3833 deg
Mean motion: 15
52319224 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2242
Checksum: 296
Coasting Arc #12 (Orbit 2256)
---------------------------------------
Vector Time (GMT): 2013/090/00:36:13
445
Vector Time (MET): N/A
Weight (LBS) : 906812
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1208928
70 A = 6783815
44 meter
Y = 4384827
82 meter E =
0024477
Z = -5054856
14 I = 51
87307
XDOT = -6224
112439 Wp = 95
97662
YDOT = 3981
655518 meter/sec RA = 135
30682 deg
ZDOT = 1971
039772 TA = 193
11812
MA = 193
18189
Ha = 228
163 n
mi
Hp = 213
161
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3966301
51 X = 1184362
15
Y = 14385918
06 feet Y = 4398209
09 meter
Z = -16584173
68 Z = -5049043
21
XDOT = -20420
316400 XDOT = -6277
748446
YDOT = 13063
174271 feet/sec YDOT = 3911
753824 meter/sec
ZDOT = 6466
665919 ZDOT = 1940
672710
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8052567
64 X = -2454422
62
Y = -12594839
69 feet Y = -3838907
14 meter
Z = -16560409
73 Z = -5047612
89
XDOT = 14892
295095 XDOT = 4539
171545
YDOT = -17832
444050 feet/sec YDOT = -5435
328946 meter/sec
ZDOT = 6339
652836 ZDOT = 1932
326184
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 13090
03792411
00016717 00000-0 10270-3 0 9119
2 25544 51
6437 136
2694 0011872 86
1811 274
0698 15
52337943 22577
Satellite: ISS
Catalog Number: 25544
Epoch time: 13090
03792411 = yrday
fracday
Element set: 911
Inclination: 51
6437 deg
RA of node: 136
2694 deg
Eccentricity:
0011872
Arg of perigee: 86
1811 deg
Mean anomaly: 274
0698 deg
Mean motion: 15
52337943 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2257
Checksum: 310
Coasting Arc #13 (Orbit 2272)
---------------------------------------
Vector Time (GMT): 2013/091/00:36:13
445
Vector Time (MET): N/A
Weight (LBS) : 906812
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -433797
15 A = 6785629
71 meter
Y = -5000792
53 meter E =
0020076
Z = 4550759
20 I = 51
90108
XDOT = 6121
696172 Wp = 80
25023
YDOT = -3402
931694 meter/sec RA = 130
34554 deg
ZDOT = -3140
832827 TA = 41
15480
MA = 41
00357
Ha = 228
089 n
mi
Hp = 213
102
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1423219
01 X = -399951
50
Y = -16406799
63 feet Y = -5005454
02 meter
Z = 14930312
33 Z = 4548734
33
XDOT = 20084
305025 XDOT = 6174
550926
YDOT = -11164
474063 feet/sec YDOT = -3334
179685 meter/sec
ZDOT = -10304
569642 ZDOT = -3110
965393
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6454155
21 X = 1967226
51
Y = 15158770
57 feet Y = 4620393
27 meter
Z = 14922412
94 Z = 4548351
46
XDOT = -14668
640724 XDOT = -4471
001693
YDOT = 16315
147743 feet/sec YDOT = 4972
857032 meter/sec
ZDOT = -10179
681867 ZDOT = -3102
767033
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 13091
06794188
00016717 00000-0 10270-3 0 9127
2 25544 51
6440 131
1482 0011770 89
7329 270
5171 15
52381377 22735
Satellite: ISS
Catalog Number: 25544
Epoch time: 13091
06794188 = yrday
fracday
Element set: 912
Inclination: 51
6440 deg
RA of node: 131
1482 deg
Eccentricity:
0011770
Arg of perigee: 89
7329 deg
Mean anomaly: 270
5171 deg
Mean motion: 15
52381377 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2273
Checksum: 306
Coasting Arc #14 (Orbit 2287)
---------------------------------------
Vector Time (GMT): 2013/092/00:36:13
445
Vector Time (MET): N/A
Weight (LBS) : 906812
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -213829
54 A = 6788010
20 meter
Y = 5568218
49 meter E =
0018199
Z = -3894009
83 I = 51
92695
XDOT = -5862
736620 Wp = 98
09078
YDOT = 2657
856298 meter/sec RA = 125
38859 deg
ZDOT = 4136
566057 TA = 215
22111
MA = 215
34152
Ha = 228
093 n
mi
Hp = 213
077
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -701540
49 X = -257162
56
Y = 18268433
36 feet Y = 5565584
83 meter
Z = -12775622
79 Z = -3895154
13
XDOT = -19234
700197 XDOT = -5912
115981
YDOT = 8720
000979 feet/sec YDOT = 2592
019599 meter/sec
ZDOT = 13571
410948 ZDOT = 4107
965257
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5288774
56 X = -1612018
49
Y = -17496259
45 feet Y = -5332859
88 meter
Z = -12781006
34 Z = -3895650
73
XDOT = 14208
342499 XDOT = 4330
702794
YDOT = -14087
844162 feet/sec YDOT = -4293
974901 meter/sec
ZDOT = 13451
867624 ZDOT = 4100
129252
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 13092
03357110
00016717 00000-0 10270-3 0 9136
2 25544 51
6428 126
3461 0011866 93
6645 266
5864 15
52380343 22887
Satellite: ISS
Catalog Number: 25544
Epoch time: 13092
03357110 = yrday
fracday
Element set: 913
Inclination: 51
6428 deg
RA of node: 126
3461 deg
Eccentricity:
0011866
Arg of perigee: 93
6645 deg
Mean anomaly: 266
5864 deg
Mean motion: 15
52380343 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2288
Checksum: 307
Coasting Arc #15 (Orbit 2303)
---------------------------------------
Vector Time (GMT): 2013/093/00:36:13
445
Vector Time (MET): N/A
Weight (LBS) : 906812
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 825268
72 A = 6790443
99 meter
Y = -6026966
14 meter E =
0024848
Z = 2992298
20 I = 51
95319
XDOT = 5557
851490 Wp = 97
02954
YDOT = -1736
850359 meter/sec RA = 120
43812 deg
ZDOT = -4998
643274 TA = 48
88113
MA = 48
66689
Ha = 227
947 n
mi
Hp = 213
046
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2707574
54 X = 878066
45
Y = -19773510
96 feet Y = -6017442
09 meter
Z = 9817251
32 Z = 2996435
85
XDOT = 18234
420899 XDOT = 5601
142276
YDOT = -5698
327951 feet/sec YDOT = -1674
457190 meter/sec
ZDOT = -16399
748273 ZDOT = -4971
538520
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4192700
18 X = 1277935
01
Y = 19503633
23 feet Y = 5944707
41 meter
Z = 9835175
38 Z = 2997761
46
XDOT = -13907
109148 XDOT = -4238
886868
YDOT = 11256
147578 feet/sec YDOT = 3430
873782 meter/sec
ZDOT = -16286
530250 ZDOT = -4964
134420
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 13093
06355795
00016717 00000-0 10270-3 0 9148
2 25544 51
6435 121
2247 0011714 96
7681 263
4804 15
52438528 23045
Satellite: ISS
Catalog Number: 25544
Epoch time: 13093
06355795 = yrday
fracday
Element set: 914
Inclination: 51
6435 deg
RA of node: 121
2247 deg
Eccentricity:
0011714
Arg of perigee: 96
7681 deg
Mean anomaly: 263
4804 deg
Mean motion: 15
52438528 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2304
Checksum: 307
Coasting Arc #16 (Orbit 2318)
---------------------------------------
Vector Time (GMT): 2013/094/00:36:13
445
Vector Time (MET): N/A
Weight (LBS) : 906812
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1285003
31 A = 6792553
93 meter
Y = 6360134
47 meter E =
0016218
Z = -2017066
54 I = 51
97355
XDOT = -5183
871824 Wp = 80
41935
YDOT = 712
862000 meter/sec RA = 115
49201 deg
ZDOT = 5591
084319 TA = 257
44242
MA = 257
62387
Ha = 228
016 n
mi
Hp = 213
054
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4215890
12 X = -1346229
86
Y = 20866582
91 feet Y = 6345422
28 meter
Z = -6617672
37 Z = -2023458
11
XDOT = -17007
453490 XDOT = -5218
617786
YDOT = 2338
786089 feet/sec YDOT = 654
698800 meter/sec
ZDOT = 18343
452491 ZDOT = 5565
817196
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3485802
86 X = -1062472
71
Y = -20992241
60 feet Y = -6398435
24 meter
Z = -6645041
06 Z = -2025408
52
XDOT = 13651
017952 XDOT = 4160
830272
YDOT = -7997
721123 feet/sec YDOT = -2437
705398 meter/sec
ZDOT = 18238
001146 ZDOT = 5558
942749
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 13094
02915899
00016717 00000-0 10270-3 0 9153
2 25544 51
6422 116
4227 0011889 101
2842 258
9647 15
52420677 23195
Satellite: ISS
Catalog Number: 25544
Epoch time: 13094
02915899 = yrday
fracday
Element set: 915
Inclination: 51
6422 deg
RA of node: 116
4227 deg
Eccentricity:
0011889
Arg of perigee: 101
2842 deg
Mean anomaly: 258
9647 deg
Mean motion: 15
52420677 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2319
Checksum: 322
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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