[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 5th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13454 89 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 126 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 347 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 1409)
---------------------------------------
Vector Time (GMT): 2013/035/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2535894
71 A = 6782870
42 meter
Y = -3382287
19 meter E =
0007098
Z = -5307314
78 I = 51
88667
XDOT = 5585
871366 Wp = 145
55137
YDOT = 5205
387357 meter/sec RA = 46
83626 deg
ZDOT = -654
465930 TA = 118
25300
MA = 118
18133
Ha = 224
520 n
mi
Hp = 219
057
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8319864
52 X = 2599308
92
Y = -11096742
75 feet Y = -3353574
61 meter
Z = -17412450
06 Z = -5294841
75
XDOT = 18326
349627 XDOT = 5530
427653
YDOT = 17078
042510 feet/sec YDOT = 5267
542078 meter/sec
ZDOT = -2147
197933 ZDOT = -627
465172
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13836963
65 X = 4217506
52
Y = -1648315
22 feet Y = -502406
48 meter
Z = -17360090
91 Z = -5291355
71
XDOT = 336
013409 XDOT = 102
416887
YDOT = 24046
403989 feet/sec YDOT = 7329
343936 meter/sec
ZDOT = -2035
515082 ZDOT = -620
424997
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 13035
51716069
00016717 00000-0 10270-3 0 9004
2 25544 51
6464 47
3658 0012787 236
3450 123
6483 15
52276404 14108
Satellite: ISS
Catalog Number: 25544
Epoch time: 13035
51716069 = yrday
fracday
Element set: 900
Inclination: 51
6464 deg
RA of node: 47
3658 deg
Eccentricity:
0012787
Arg of perigee: 236
3450 deg
Mean anomaly: 123
6483 deg
Mean motion: 15
52276404 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1410
Checksum: 296
Coasting Arc #2 (Orbit 1425)
---------------------------------------
Vector Time (GMT): 2013/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3278236
51 A = 6782787
58 meter
Y = 2663949
27 meter E =
0009780
Z = 5313596
53 I = 51
86397
XDOT = -5366
097551 Wp = 238
28430
YDOT = -5434
119134 meter/sec RA = 41
87133 deg
ZDOT = -592
061380 TA = 217
32117
MA = 217
38916
Ha = 224
169 n
mi
Hp = 219
262
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10755369
14 X = -3333593
36
Y = 8739991
05 feet Y = 2626980
35 meter
Z = 17433059
49 Z = 5297536
97
XDOT = -17605
306926 XDOT = -5302
057226
YDOT = -17828
474850 feet/sec YDOT = -5493
768123 meter/sec
ZDOT = -1942
458595 ZDOT = -617
973592
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13861668
53 X = -4225036
57
Y = -1502622
85 feet Y = -457999
44 meter
Z = 17365864
27 Z = 5293115
43
XDOT = 61
794359 XDOT = 18
834921
YDOT = -24036
034591 feet/sec YDOT = -7326
183343 meter/sec
ZDOT = -2049
575726 ZDOT = -624
710681
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 13036
54720650
00016717 00000-0 10270-3 0 9010
2 25544 51
6454 42
2448 0012699 240
3047 119
6841 15
52307155 14265
Satellite: ISS
Catalog Number: 25544
Epoch time: 13036
54720650 = yrday
fracday
Element set: 901
Inclination: 51
6454 deg
RA of node: 42
2448 deg
Eccentricity:
0012699
Arg of perigee: 240
3047 deg
Mean anomaly: 119
6841 deg
Mean motion: 15
52307155 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1426
Checksum: 289
Coasting Arc #3 (Orbit 1440)
---------------------------------------
Vector Time (GMT): 2013/037/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4054675
66 A = 6783813
05 meter
Y = -1947881
06 meter E =
0008766
Z = -5081440
80 I = 51
84385
XDOT = 4969
798036 Wp = 171
59370
YDOT = 5535
722521 meter/sec RA = 36
90572 deg
ZDOT = 1835
516819 TA = 116
18800
MA = 116
09783
Ha = 223
892 n
mi
Hp = 219
313
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13302741
66 X = 4100839
72
Y = -6390685
89 feet Y = -1902280
91 meter
Z = -16671393
71 Z = -5061631
84
XDOT = 16305
111668 XDOT = 4898
610774
YDOT = 18161
819294 feet/sec YDOT = 5590
899851 meter/sec
ZDOT = 6022
036807 ZDOT = 1859
486401
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14080958
81 X = 4291876
24
Y = 4720303
51 feet Y = 1438748
51 meter
Z = -16588686
01 Z = -5056231
50
XDOT = -581
095052 XDOT = -177
117772
YDOT = 23338
129945 feet/sec YDOT = 7113
462007 meter/sec
ZDOT = 6121
052723 ZDOT = 1865
696870
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 13037
51286167
00016717 00000-0 10270-3 0 9029
2 25544 51
6453 37
4442 0012707 244
2238 115
7603 15
52308216 14418
Satellite: ISS
Catalog Number: 25544
Epoch time: 13037
51286167 = yrday
fracday
Element set: 902
Inclination: 51
6453 deg
RA of node: 37
4442 deg
Eccentricity:
0012707
Arg of perigee: 244
2238 deg
Mean anomaly: 115
7603 deg
Mean motion: 15
52308216 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1441
Checksum: 281
Coasting Arc #4 (Orbit 1456)
---------------------------------------
Vector Time (GMT): 2013/038/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4785206
36 A = 6785531
45 meter
Y = 1308750
58 meter E =
0004257
Z = 4632391
66 I = 51
82420
XDOT = -4399
943070 Wp = 252
58178
YDOT = -5514
036699 meter/sec RA = 31
94058 deg
ZDOT = -2990
761243 TA = 227
17080
MA = 227
20658
Ha = 223
550 n
mi
Hp = 219
392
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15699495
93 X = -4821987
80
Y = 4293801
10 feet Y = 1255033
69 meter
Z = 15198135
37 Z = 4609056
79
XDOT = -14435
508760 XDOT = -4323
428971
YDOT = -18090
671584 feet/sec YDOT = -5562
811776 meter/sec
ZDOT = -9812
208802 ZDOT = -3011
949473
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14473946
11 X = -4411658
77
Y = -7639622
98 feet Y = -2328557
09 meter
Z = 15100836
52 Z = 4602734
97
XDOT = 1284
090817 XDOT = 391
390881
YDOT = -21978
056029 feet/sec YDOT = -6698
911478 meter/sec
ZDOT = -9899
651101 ZDOT = -3017
413656
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 13038
54288010
00016717 00000-0 10270-3 0 9033
2 25544 51
6446 32
3229 0012711 248
3421 111
6377 15
52354018 14572
Satellite: ISS
Catalog Number: 25544
Epoch time: 13038
54288010 = yrday
fracday
Element set: 903
Inclination: 51
6446 deg
RA of node: 32
3229 deg
Eccentricity:
0012711
Arg of perigee: 248
3421 deg
Mean anomaly: 111
6377 deg
Mean motion: 15
52354018 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1457
Checksum: 279
Coasting Arc #5 (Orbit 1471)
---------------------------------------
Vector Time (GMT): 2013/039/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5466003
19 A = 6787984
72 meter
Y = -714189
42 meter E =
0008070
Z = -3960617
09 I = 51
80573
XDOT = 3635
344190 Wp = 224
32001
YDOT = 5409
234343 meter/sec RA = 26
97727 deg
ZDOT = 4031
100127 TA = 87
74073
MA = 87
64833
Ha = 223
166 n
mi
Hp = 219
408
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17933081
35 X = 5492822
24
Y = -2343141
14 feet Y = -652915
22 meter
Z = -12994150
56 Z = -3933999
33
XDOT = 11926
982252 XDOT = 3555
005348
YDOT = 17746
831833 feet/sec YDOT = 5449
437875 meter/sec
ZDOT = 13225
394118 ZDOT = 4048
564636
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14944853
68 X = 4555191
40
Y = 10325038
91 feet Y = 3147071
86 meter
Z = -12883267
67 Z = -3926819
98
XDOT = -2339
826718 XDOT = -713
179184
YDOT = 20022
507656 feet/sec YDOT = 6102
860334 meter/sec
ZDOT = 13297
352699 ZDOT = 4053
033103
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 13039
50850987
00016717 00000-0 10270-3 0 9049
2 25544 51
6445 27
5217 0012613 252
0753 107
9024 15
52349276 14729
Satellite: ISS
Catalog Number: 25544
Epoch time: 13039
50850987 = yrday
fracday
Element set: 904
Inclination: 51
6445 deg
RA of node: 27
5217 deg
Eccentricity:
0012613
Arg of perigee: 252
0753 deg
Mean anomaly: 107
9024 deg
Mean motion: 15
52349276 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1472
Checksum: 302
Coasting Arc #6 (Orbit 1487)
---------------------------------------
Vector Time (GMT): 2013/040/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6024834
99 A = 6790328
90 meter
Y = 212700
07 meter E =
0004334
Z = 3119156
69 I = 51
78630
XDOT = -2712
785629 Wp = 171
38908
YDOT = -5245
891974 meter/sec RA = 22
01652 deg
ZDOT = -4885
480956 TA = 332
81780
MA = 332
84048
Ha = 222
831 n
mi
Hp = 219
313
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19766518
98 X = -6041917
25
Y = 697834
88 feet Y = 145231
17 meter
Z = 10233453
72 Z = 3089847
95
XDOT = -8900
215317 XDOT = -2630
191679
YDOT = -17210
931674 feet/sec YDOT = -5275
766392 meter/sec
ZDOT = -16028
480828 ZDOT = -4898
458263
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15408644
77 X = -4696554
93
Y = -12500330
74 feet Y = -3810100
81 meter
Z = 10111440
01 Z = 3081966
92
XDOT = 3760
581783 XDOT = 1146
225327
YDOT = -17635
105743 feet/sec YDOT = -5375
180230 meter/sec
ZDOT = -16081
786142 ZDOT = -4901
728416
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 13040
53850046
00016717 00000-0 10270-3 0 9051
2 25544 51
6444 22
4002 0012692 256
4056 103
5682 15
52403039 14882
Satellite: ISS
Catalog Number: 25544
Epoch time: 13040
53850046 = yrday
fracday
Element set: 905
Inclination: 51
6444 deg
RA of node: 22
4002 deg
Eccentricity:
0012692
Arg of perigee: 256
4056 deg
Mean anomaly: 103
5682 deg
Mean motion: 15
52403039 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1488
Checksum: 277
Coasting Arc #7 (Orbit 1502)
---------------------------------------
Vector Time (GMT): 2013/041/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6447029
77 A = 6792510
81 meter
Y = 236411
72 meter E =
0008499
Z = -2113420
16 I = 51
76505
XDOT = 1631
272324 Wp = 287
74791
YDOT = 5054
826374 meter/sec RA = 17
05826 deg
ZDOT = 5525
912086 TA = 48
90277
MA = 48
82941
Ha = 222
429 n
mi
Hp = 219
283
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21151672
47 X = 6454173
14
Y = 775629
02 feet Y = 308546
28 meter
Z = -6933793
17 Z = -2082084
61
XDOT = 5351
943320 XDOT = 1547
784310
YDOT = 16584
076031 feet/sec YDOT = 5072
601785 meter/sec
ZDOT = 18129
632829 ZDOT = 5533
633374
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15716709
07 X = 4790452
93
Y = 14239769
06 feet Y = 4340281
61 meter
Z = -6803408
68 Z = -2073678
97
XDOT = -5631
525506 XDOT = -1716
488974
YDOT = 14917
719259 feet/sec YDOT = 4546
920830 meter/sec
ZDOT = 18161
089009 ZDOT = 5535
499930
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 13041
50410414
00016717 00000-0 10270-3 0 9061
2 25544 51
6445 17
5989 0012549 259
5974 100
3763 15
52409575 15030
Satellite: ISS
Catalog Number: 25544
Epoch time: 13041
50410414 = yrday
fracday
Element set: 906
Inclination: 51
6445 deg
RA of node: 17
5989 deg
Eccentricity:
0012549
Arg of perigee: 259
5974 deg
Mean anomaly: 100
3763 deg
Mean motion: 15
52409575 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1503
Checksum: 305
Coasting Arc #8 (Orbit 1518)
---------------------------------------
Vector Time (GMT): 2013/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6683170
13 A = 6793832
48 meter
Y = -610519
25 meter E =
0009082
Z = 1019686
36 I = 51
74112
XDOT = -454
911924 Wp = 188
68134
YDOT = -4863
095375 meter/sec RA = 12
10130 deg
ZDOT = -5908
869500 TA = 340
28957
MA = 340
32465
Ha = 222
173 n
mi
Hp = 219
083
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21926411
20 X = -6680799
71
Y = -2003015
91 feet Y = -685241
32 meter
Z = 3345427
69 Z = 987226
74
XDOT = -1492
493188 XDOT = -371
794976
YDOT = -15955
037320 feet/sec YDOT = -4867
718201 meter/sec
ZDOT = -19386
054789 ZDOT = -5910
877114
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15769218
55 X = -4806457
81
Y = -15394687
54 feet Y = -4692300
76 meter
Z = 3210421
93 Z = 978536
61
XDOT = 7874
541018 XDOT = 2400
160102
YDOT = -12099
373425 feet/sec YDOT = -3687
889020 meter/sec
ZDOT = -19393
758156 ZDOT = -5911
217486
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 13042
53406677
00016717 00000-0 10270-3 0 9072
2 25544 51
6454 12
4774 0012655 264
0926 95
8783 15
52441359 15195
Satellite: ISS
Catalog Number: 25544
Epoch time: 13042
53406677 = yrday
fracday
Element set: 907
Inclination: 51
6454 deg
RA of node: 12
4774 deg
Eccentricity:
0012655
Arg of perigee: 264
0926 deg
Mean anomaly: 95
8783 deg
Mean motion: 15
52441359 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1519
Checksum: 321
Coasting Arc #9 (Orbit 1534)
---------------------------------------
Vector Time (GMT): 2013/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6719438
93 A = 6794124
91 meter
Y = 957928
47 meter E =
0008504
Z = 145416
53 I = 51
71242
XDOT = -795
206715 Wp = 335
48464
YDOT = 4685
297993 meter/sec RA = 7
14440 deg
ZDOT = 6014
463098 TA = 26
07911
MA = 26
03630
Ha = 221
923 n
mi
Hp = 219
005
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22045403
32 X = 6707521
39
Y = 3142809
94 feet Y = 1033002
84 meter
Z = 477088
34 Z = 178029
23
XDOT = -2608
945916 XDOT = -876
755635
YDOT = 15371
712576 feet/sec YDOT = 4675
950063 meter/sec
ZDOT = 19732
490479 ZDOT = 6010
401645
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15403146
14 X = 4694878
94
Y = 16077076
60 feet Y = 4900292
95 meter
Z = 612676
33 Z = 186743
75
XDOT = -10464
203396 XDOT = -3189
489195
YDOT = 9287
261273 feet/sec YDOT = 2830
757236 meter/sec
ZDOT = 19714
961944 ZDOT = 6009
120401
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 13043
56401402
00016717 00000-0 10270-3 0 9088
2 25544 51
6454 7
3562 0012626 267
1949 92
7758 15
52475233 15354
Satellite: ISS
Catalog Number: 25544
Epoch time: 13043
56401402 = yrday
fracday
Element set: 908
Inclination: 51
6454 deg
RA of node: 7
3562 deg
Eccentricity:
0012626
Arg of perigee: 267
1949 deg
Mean anomaly: 92
7758 deg
Mean motion: 15
52475233 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1535
Checksum: 306
Coasting Arc #10 (Orbit 1549)
---------------------------------------
Vector Time (GMT): 2013/044/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6540843
11 A = 6793371
44 meter
Y = -1272338
15 meter E =
0009870
Z = -1293206
62 I = 51
68063
XDOT = 2040
108841 Wp = 227
46634
YDOT = -4536
032635 meter/sec RA = 2
18511 deg
ZDOT = -5833
874916 TA = 326
58757
MA = 326
64981
Ha = 221
909 n
mi
Hp = 218
905
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21459459
02 X = -6519847
48
Y = -4174337
76 feet Y = -1345364
69 meter
Z = -4242803
87 Z = -1324929
79
XDOT = 6693
270477 XDOT = 2119
019003
YDOT = -14881
996833 feet/sec YDOT = -4512
778187 meter/sec
ZDOT = -19140
009568 ZDOT = -5823
772333
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14568987
43 X = -4440627
37
Y = -16264747
08 feet Y = -4957494
91 meter
Z = -4374639
35 Z = -1333390
07
XDOT = 13227
620292 XDOT = 4031
778665
YDOT = -6693
296725 feet/sec YDOT = -2040
116842 meter/sec
ZDOT = -19097
363944 ZDOT = -5820
876530
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 13044
52957728
00016717 00000-0 10270-3 0 9093
2 25544 51
6465 2
5553 0012697 271
5973 88
3724 15
52480855 15504
Satellite: ISS
Catalog Number: 25544
Epoch time: 13044
52957728 = yrday
fracday
Element set: 909
Inclination: 51
6465 deg
RA of node: 2
5553 deg
Eccentricity:
0012697
Arg of perigee: 271
5973 deg
Mean anomaly: 88
3724 deg
Mean motion: 15
52480855 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1550
Checksum: 331
Coasting Arc #11 (Orbit 1565)
---------------------------------------
Vector Time (GMT): 2013/045/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6143559
84 A = 6791504
59 meter
Y = 1604294
80 meter E =
0004771
Z = 2401298
56 I = 51
64430
XDOT = -3246
347465 Wp = 6
27095
YDOT = 4407
631133 meter/sec RA = 357
22143 deg
ZDOT = 5364
471518 TA = 20
54261
MA = 20
52343
Ha = 221
905 n
mi
Hp = 218
854
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20156036
23 X = 6113498
98
Y = 5263434
40 feet Y = 1672828
08 meter
Z = 7878276
12 Z = 2431069
85
XDOT = -10650
746277 XDOT = -3321
452051
YDOT = 14460
732063 feet/sec YDOT = 4370
908971 meter/sec
ZDOT = 17599
972173 ZDOT = 5348
518466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13133465
57 X = 4003080
31
Y = 16109557
91 feet Y = 4910193
25 meter
Z = 8001937
21 Z = 2438990
46
XDOT = -16043
118345 XDOT = -4889
942471
YDOT = 4376
127852 feet/sec YDOT = 1333
843769 meter/sec
ZDOT = 17533
002417 ZDOT = 5344
059137
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 13045
55949553
00016717 00000-0 10270-3 0 9106
2 25544 51
6466 357
4341 0012716 274
9794 84
9906 15
52515370 15664
Satellite: ISS
Catalog Number: 25544
Epoch time: 13045
55949553 = yrday
fracday
Element set: 910
Inclination: 51
6466 deg
RA of node: 357
4341 deg
Eccentricity:
0012716
Arg of perigee: 274
9794 deg
Mean anomaly: 84
9906 deg
Mean motion: 15
52515370 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1566
Checksum: 334
Coasting Arc #12 (Orbit 1580)
---------------------------------------
Vector Time (GMT): 2013/046/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5552519
59 A = 6789035
71 meter
Y = -1948502
07 meter E =
0007954
Z = -3381224
43 I = 51
60616
XDOT = 4336
939860 Wp = 284
32883
YDOT = -4296
675838 meter/sec RA = 352
25146 deg
ZDOT = -4634
834767 TA = 295
14064
MA = 295
22313
Ha = 222
143 n
mi
Hp = 218
917
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18216927
81 X = -5513893
48
Y = -6392723
31 feet Y = -2010378
11 meter
Z = -11093255
99 Z = -3408103
78
XDOT = 14228
805316 XDOT = 4407
178379
YDOT = -14096
705506 feet/sec YDOT = -4247
785073 meter/sec
ZDOT = -15206
150812 ZDOT = -4613
595631
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11156688
14 X = -3400558
54
Y = -15676854
21 feet Y = -4778305
16 meter
Z = -11204831
56 Z = -3415232
66
XDOT = 18683
983690 XDOT = 5694
878229
YDOT = -2466
221011 feet/sec YDOT = -751
704164 meter/sec
ZDOT = -15117
204868 ZDOT = -4607
724044
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 13046
52503109
00016717 00000-0 10270-3 0 9118
2 25544 51
6471 352
6330 0012725 279
2288 80
7425 15
52533139 15811
Satellite: ISS
Catalog Number: 25544
Epoch time: 13046
52503109 = yrday
fracday
Element set: 911
Inclination: 51
6471 deg
RA of node: 352
6330 deg
Eccentricity:
0012725
Arg of perigee: 279
2288 deg
Mean anomaly: 80
7425 deg
Mean motion: 15
52533139 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1581
Checksum: 293
Coasting Arc #13 (Orbit 1596)
---------------------------------------
Vector Time (GMT): 2013/047/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4775432
87 A = 6786265
62 meter
Y = 2349081
74 meter E =
0002821
Z = 4213263
19 I = 51
56722
XDOT = -5281
435079 Wp = 267
98551
YDOT = 4171
874656 meter/sec RA = 347
27445 deg
ZDOT = 3662
149702 TA = 144
42391
MA = 144
40511
Ha = 222
291 n
mi
Hp = 218
815
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15667430
68 X = 4728343
36
Y = 7706961
07 feet Y = 2402220
59 meter
Z = 13823041
97 Z = 4236347
03
XDOT = -17327
542911 XDOT = -5345
482871
YDOT = 13687
252807 feet/sec YDOT = 4112
456440 meter/sec
ZDOT = 12014
926843 ZDOT = 3636
337440
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8563178
27 X = 2610056
74
Y = 15128847
00 feet Y = 4611272
56 meter
Z = 13918767
51 Z = 4242440
34
XDOT = -20982
032628 XDOT = -6395
323545
YDOT = 927
655928 feet/sec YDOT = 282
749527 meter/sec
ZDOT = 11906
974256 ZDOT = 3629
245753
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 13047
55491983
00016717 00000-0 10270-3 0 9129
2 25544 51
6473 347
5117 0012760 282
4525 77
5199 15
52564634 15971
Satellite: ISS
Catalog Number: 25544
Epoch time: 13047
55491983 = yrday
fracday
Element set: 912
Inclination: 51
6473 deg
RA of node: 347
5117 deg
Eccentricity:
0012760
Arg of perigee: 282
4525 deg
Mean anomaly: 77
5199 deg
Mean motion: 15
52564634 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1597
Checksum: 334
Coasting Arc #14 (Orbit 1611)
---------------------------------------
Vector Time (GMT): 2013/048/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3874274
97 A = 6783884
85 meter
Y = -2786196
36 meter E =
0007265
Z = -4823545
71 I = 51
52988
XDOT = 6024
124552 Wp = 351
23526
YDOT = -4017
652940 meter/sec RA = 342
28981 deg
ZDOT = -2510
357713 TA = 253
99253
MA = 254
07257
Ha = 222
612 n
mi
Hp = 218
937
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12710875
90 X = -3819399
99
Y = -9141064
18 feet Y = -2829214
35 meter
Z = -15825281
21 Z = -4842232
94
XDOT = 19764
188164 XDOT = 6080
797567
YDOT = -13181
276049 feet/sec YDOT = -3949
970639 meter/sec
ZDOT = -8236
081736 ZDOT = -2480
955565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5552467
86 X = -1692392
20
Y = -14554746
82 feet Y = -4436286
83 meter
Z = -15902653
60 Z = -4847128
82
XDOT = 22736
610304 XDOT = 6930
118821
YDOT = 217
684287 feet/sec YDOT = 66
350171 meter/sec
ZDOT = -8113
217945 ZDOT = -2472
908829
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 13048
52042803
00016717 00000-0 10270-3 0 9131
2 25544 51
6474 342
7100 0012720 286
6981 73
2775 15
52582362 16128
Satellite: ISS
Catalog Number: 25544
Epoch time: 13048
52042803 = yrday
fracday
Element set: 913
Inclination: 51
6474 deg
RA of node: 342
7100 deg
Eccentricity:
0012720
Arg of perigee: 286
6981 deg
Mean anomaly: 73
2775 deg
Mean motion: 15
52582362 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1612
Checksum: 293
Coasting Arc #15 (Orbit 1627)
---------------------------------------
Vector Time (GMT): 2013/049/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903156
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2861679
01 A = 6782193
59 meter
Y = 3289265
67 meter E =
0009058
Z = 5202430
71 I = 51
49579
XDOT = -6548
169253 Wp = 283
24073
YDOT = 3784
981110 meter/sec RA = 337
29946 deg
ZDOT = 1212
661832 TA = 155
10970
MA = 155
06599
Ha = 222
851 n
mi
Hp = 218
714
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9388710
68 X = 2799413
41
Y = 10791554
05 feet Y = 3320918
83 meter
Z = 17068342
21 Z = 5216180
92
XDOT = -21483
494926 XDOT = -6595
897745
YDOT = 12417
917029 feet/sec YDOT = 3711
488553 meter/sec
ZDOT = 3978
549319 ZDOT = 1180
735770
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2104815
11 X = 641547
64
Y = 14079570
29 feet Y = 4291453
02 meter
Z = 17125106
91 Z = 5219732
59
XDOT = -23790
279759 XDOT = -7251
277271
YDOT = -1105
297771 feet/sec YDOT = -336
894761 meter/sec
ZDOT = 3845
220012 ZDOT = 1172
023060
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 13049
55028681
00016717 00000-0 10270-3 0 9144
2 25544 51
6475 337
5885 0012853 289
9555 70
0212 15
52622245 16284
Satellite: ISS
Catalog Number: 25544
Epoch time: 13049
55028681 = yrday
fracday
Element set: 914
Inclination: 51
6475 deg
RA of node: 337
5885 deg
Eccentricity:
0012853
Arg of perigee: 289
9555 deg
Mean anomaly: 70
0212 deg
Mean motion: 15
52622245 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1628
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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