Date:
April 27th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 ET - UTC (sec) : 66 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 1533)
---------------------------------------
Vector Time (GMT): 2010/116/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 793683
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3669773
55 A = 6722242
50 meter
Y = -2125211
81 meter E =
0008696
Z = 5221591
15 I = 51
86222
XDOT = 4819
371407 Wp = 220
76490
YDOT = -5919
922259 meter/sec RA = 134
88732 deg
ZDOT = 972
114112 TA = 219
96060
MA = 220
02463
Ha = 190
757 n
mi
Hp = 187
367
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12039939
46 X = -3671102
23
Y = -6972479
68 feet Y = -2166256
67 meter
Z = 17131204
54 Z = 5203759
95
XDOT = 15811
585982 XDOT = 4880
488425
YDOT = -19422
317124 feet/sec YDOT = -5865
687425 meter/sec
ZDOT = 3189
350760 ZDOT = 995
675611
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13970340
83 X = -4258159
88
Y = 913081
23 feet Y = 278307
16 meter
Z = 17060177
14 Z = 5199941
99
XDOT = 2469
364233 XDOT = 752
662218
YDOT = -23898
200502 feet/sec YDOT = -7284
171513 meter/sec
ZDOT = 3282
934968 ZDOT = 1000
638578
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 10116
54931956
00016717 00000-0 10270-3 0 9008
2 25544 51
6438 135
5875 0009852 241
9344 118
0823 15
73365358 15346
Satellite: ISS
Catalog Number: 25544
Epoch time: 10116
54931956 = yrday
fracday
Element set: 900
Inclination: 51
6438 deg
RA of node: 135
5875 deg
Eccentricity:
0009852
Arg of perigee: 241
9344 deg
Mean anomaly: 118
0823 deg
Mean motion: 15
73365358 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1534
Checksum: 318
Coasting Arc #2 (Orbit 1548)
---------------------------------------
Vector Time (GMT): 2010/117/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 793683
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3599902
17 A = 6733283
36 meter
Y = 5592438
58 meter E =
0004600
Z = -1032558
71 I = 51
92116
XDOT = -4539
803073 Wp = 319
15158
YDOT = -1823
023789 meter/sec RA = 129
75647 deg
ZDOT = 5942
449351 TA = 29
60992
MA = 29
58389
Ha = 190
391 n
mi
Hp = 187
376
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11810702
64 X = -3657154
18
Y = 18347895
62 feet Y = 5551862
21 meter
Z = -3387659
80 Z = -1050186
49
XDOT = -14894
367036 XDOT = -4547
948181
YDOT = -5981
049176 feet/sec YDOT = -1873
836052 meter/sec
ZDOT = 19496
224904 ZDOT = 5920
374798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 710655
22 X = 216607
71
Y = 21798022
97 feet Y = 6644037
40 meter
Z = -3457654
26 Z = -1053893
02
XDOT = -14161
339397 XDOT = -4316
376248
YDOT = 3546
091366 feet/sec YDOT = 1080
848648 meter/sec
ZDOT = 19408
318314 ZDOT = 5915
655422
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 10117
50203694
00016717 00000-0 10270-3 0 9017
2 25544 51
6443 130
7002 0009909 245
1816 114
8316 15
73440076 15492
Satellite: ISS
Catalog Number: 25544
Epoch time: 10117
50203694 = yrday
fracday
Element set: 901
Inclination: 51
6443 deg
RA of node: 130
7002 deg
Eccentricity:
0009909
Arg of perigee: 245
1816 deg
Mean anomaly: 114
8316 deg
Mean motion: 15
73440076 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1549
Checksum: 283
Coasting Arc #3 (Orbit 1564)
---------------------------------------
Vector Time (GMT): 2010/118/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 793683
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4193736
35 A = 6722396
88 meter
Y = 1039827
50 meter E =
0004551
Z = -5153614
84 I = 51
90156
XDOT = -3373
600882 Wp = 100
12481
YDOT = 6779
492967 meter/sec RA = 124
66575 deg
ZDOT = -1379
187838 TA = 156
72420
MA = 156
70359
Ha = 190
202 n
mi
Hp = 187
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13758977
53 X = 4206832
97
Y = 3411507
55 feet Y = 1086797
67 meter
Z = -16908185
17 Z = -5133209
41
XDOT = -11068
244362 XDOT = -3442
459669
YDOT = 22242
430995 feet/sec YDOT = 6741
382366 meter/sec
ZDOT = -4524
894482 ZDOT = -1395
744287
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13255881
66 X = 4040392
73
Y = -5288688
76 feet Y = -1611992
33 meter
Z = -16826941
04 Z = -5128851
63
XDOT = 3575
020688 XDOT = 1089
666306
YDOT = 23547
561154 feet/sec YDOT = 7177
296640 meter/sec
ZDOT = -4590
609803 ZDOT = -1399
217868
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 10118
51824905
00016717 00000-0 10270-3 0 9024
2 25544 51
6432 125
4858 0009901 250
1256 109
8840 15
73419235 15653
Satellite: ISS
Catalog Number: 25544
Epoch time: 10118
51824905 = yrday
fracday
Element set: 902
Inclination: 51
6432 deg
RA of node: 125
4858 deg
Eccentricity:
0009901
Arg of perigee: 250
1256 deg
Mean anomaly: 109
8840 deg
Mean motion: 15
73419235 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1565
Checksum: 301
Coasting Arc #4 (Orbit 1580)
---------------------------------------
Vector Time (GMT): 2010/119/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 793683
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2268121
52 A = 6732852
35 meter
Y = -6181893
87 meter E =
0009912
Z = 1371605
77 I = 51
95286
XDOT = 4972
312308 Wp = 164
21349
YDOT = 524
383799 meter/sec RA = 119
52995 deg
ZDOT = -5858
407915 TA =
77902
MA =
77748
Ha = 189
757 n
mi
Hp = 187
780
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7441343
56 X = 2330416
85
Y = -20281804
04 feet Y = -6156182
13 meter
Z = 4500018
93 Z = 1382775
58
XDOT = 16313
360589 XDOT = 4994
538652
YDOT = 1720
419289 feet/sec YDOT = 580
111673 meter/sec
ZDOT = -19220
498410 ZDOT = -5834
197927
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6126723
06 X = -1867425
19
Y = -20707189
25 feet Y = -6311551
28 meter
Z = 4544328
04 Z = 1385111
19
XDOT = 12708
074755 XDOT = 3873
421185
YDOT = -7957
266852 feet/sec YDOT = -2425
374936 meter/sec
ZDOT = -19124
118646 ZDOT = -5829
031363
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 10119
53444054
00016717 00000-0 10270-3 0 9031
2 25544 51
6426 120
2714 0009790 254
6980 105
3101 15
73470228 15817
Satellite: ISS
Catalog Number: 25544
Epoch time: 10119
53444054 = yrday
fracday
Element set: 903
Inclination: 51
6426 deg
RA of node: 120
2714 deg
Eccentricity:
0009790
Arg of perigee: 254
6980 deg
Mean anomaly: 105
3101 deg
Mean motion: 15
73470228 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1581
Checksum: 282
Coasting Arc #5 (Orbit 1596)
---------------------------------------
Vector Time (GMT): 2010/120/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 793683
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4417389
42 A = 6722605
81 meter
Y = 118189
28 meter E =
0007323
Z = 5072033
13 I = 51
93178
XDOT = 1808
623982 Wp = 227
05042
YDOT = -7274
009237 meter/sec RA = 114
44677 deg
ZDOT = 1741
381094 TA = 206
22611
MA = 206
26321
Ha = 189
479 n
mi
Hp = 187
992
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14492747
44 X = -4443022
16
Y = 387760
09 feet Y = 68647
76 meter
Z = 16640528
66 Z = 5050510
83
XDOT = 5933
805715 XDOT = 1881
369379
YDOT = -23864
859702 feet/sec YDOT = -7253
377497 meter/sec
ZDOT = 5713
192564 ZDOT = 1750
343778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11331169
58 X = -3453740
49
Y = 9199927
15 feet Y = 2804137
79 meter
Z = 16554854
78 Z = 5045919
74
XDOT = -9195
660886 XDOT = -2802
837438
YDOT = -21690
069639 feet/sec YDOT = -6611
133226 meter/sec
ZDOT = 5748
707898 ZDOT = 1752
206167
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 10120
55061168
00016717 00000-0 10270-3 0 9047
2 25544 51
6422 115
0567 0009879 258
8777 101
1276 15
73478430 15976
Satellite: ISS
Catalog Number: 25544
Epoch time: 10120
55061168 = yrday
fracday
Element set: 904
Inclination: 51
6422 deg
RA of node: 115
0567 deg
Eccentricity:
0009879
Arg of perigee: 258
8777 deg
Mean anomaly: 101
1276 deg
Mean motion: 15
73478430 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1597
Checksum: 317
Coasting Arc #6 (Orbit 1611)
---------------------------------------
Vector Time (GMT): 2010/121/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 793683
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -886793
64 A = 6732282
16 meter
Y = 6459291
30 meter E =
0006892
Z = -1661046
61 I = 51
97668
XDOT = -5048
582560 Wp = 314
82142
YDOT = 790
372420 meter/sec RA = 109
30815 deg
ZDOT = 5759
106970 TA = 26
91461
MA = 26
87888
Ha = 188
948 n
mi
Hp = 187
772
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2909427
97 X = -950887
52
Y = 21191900
60 feet Y = 6449016
41 meter
Z = -5449627
99 Z = -1665509
89
XDOT = -16563
591077 XDOT = -5085
022483
YDOT = 2593
085368 feet/sec YDOT = 733
711972 meter/sec
ZDOT = 18894
707906 ZDOT = 5734
492185
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10951644
97 X = 3338061
39
Y = 18369277
77 feet Y = 5598955
86 meter
Z = -5467263
87 Z = -1666422
03
XDOT = -10088
023195 XDOT = -3074
829470
YDOT = 11618
364805 feet/sec YDOT = 3541
277593 meter/sec
ZDOT = 18796
727389 ZDOT = 5729
242508
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 10121
50325233
00016717 00000-0 10270-3 0 9050
2 25544 51
6424 110
1690 0009759 262
0682 97
9374 15
73538105 16125
Satellite: ISS
Catalog Number: 25544
Epoch time: 10121
50325233 = yrday
fracday
Element set: 905
Inclination: 51
6424 deg
RA of node: 110
1690 deg
Eccentricity:
0009759
Arg of perigee: 262
0682 deg
Mean anomaly: 97
9374 deg
Mean motion: 15
73538105 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1612
Checksum: 289
Coasting Arc #7 (Orbit 1627)
---------------------------------------
Vector Time (GMT): 2010/122/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 793683
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4339836
85 A = 6722786
37 meter
Y = -1245782
11 meter E =
0003803
Z = -4983995
81 I = 51
95363
XDOT = -226
438117 Wp = 42
81768
YDOT = 7416
259900 meter/sec RA = 104
23051 deg
ZDOT = -2049
095174 TA = 207
41530
MA = 207
43537
Ha = 188
444 n
mi
Hp = 187
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14238309
88 X = 4377656
42
Y = -4087211
64 feet Y = -1197039
60 meter
Z = -16351692
30 Z = -4962820
94
XDOT = -742
907207 XDOT = -299
397020
YDOT = 24331
561352 feet/sec YDOT = 7413
319968 meter/sec
ZDOT = -6722
753195 ZDOT = -2050
371829
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8456268
87 X = 2577470
75
Y = -12274999
57 feet Y = -3741419
87 meter
Z = -16267406
39 Z = -4958305
47
XDOT = 14045
817068 XDOT = 4281
165042
YDOT = 18599
995481 feet/sec YDOT = 5669
278622 meter/sec
ZDOT = -6727
694405 ZDOT = -2050
601255
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 10122
51938278
00016717 00000-0 10270-3 0 9062
2 25544 51
6425 104
9539 0009842 266
7342 93
2695 15
73544583 16285
Satellite: ISS
Catalog Number: 25544
Epoch time: 10122
51938278 = yrday
fracday
Element set: 906
Inclination: 51
6425 deg
RA of node: 104
9539 deg
Eccentricity:
0009842
Arg of perigee: 266
7342 deg
Mean anomaly: 93
2695 deg
Mean motion: 15
73544583 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1628
Checksum: 331
Coasting Arc #8 (Orbit 1643)
---------------------------------------
Vector Time (GMT): 2010/123/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 793683
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -482984
12 A = 6731728
50 meter
Y = -6432675
97 meter E =
0006058
Z = 1910331
85 I = 51
99090
XDOT = 4805
410369 Wp = 149
81267
YDOT = -2042
060787 meter/sec RA = 99
08830 deg
ZDOT = -5658
722441 TA = 9
06363
MA = 9
05270
Ha = 188
037 n
mi
Hp = 187
136
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1584593
56 X = -420296
97
Y = -21104579
94 feet Y = -6437726
62 meter
Z = 6267492
95 Z = 1908137
28
XDOT = 15765
782049 XDOT = 4855
377093
YDOT = -6699
674497 feet/sec YDOT = -1988
044018 meter/sec
ZDOT = -18565
362338 ZDOT = -5635
256427
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14940857
97 X = -4553973
51
Y = -14993195
03 feet Y = -4569925
85 meter
Z = 6258639
22 Z = 1907633
24
XDOT = 6624
924171 XDOT = 2019
276887
YDOT = -14316
131904 feet/sec YDOT = -4363
557004 meter/sec
ZDOT = -18471
958652 ZDOT = -5630
252997
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 10123
53549117
00016717 00000-0 10270-3 0 9076
2 25544 51
6428 99
7396 0009955 271
5690 88
4333 15
73601689 16449
Satellite: ISS
Catalog Number: 25544
Epoch time: 10123
53549117 = yrday
fracday
Element set: 907
Inclination: 51
6428 deg
RA of node: 99
7396 deg
Eccentricity:
0009955
Arg of perigee: 271
5690 deg
Mean anomaly: 88
4333 deg
Mean motion: 15
73601689 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1644
Checksum: 339
Coasting Arc #9 (Orbit 1659)
---------------------------------------
Vector Time (GMT): 2010/124/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 793683
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4002644
61 A = 6722882
67 meter
Y = 2283385
46 meter E =
0005124
Z = 4899781
54 I = 51
96532
XDOT = -1300
113272 Wp = 238
35920
YDOT = -7226
849011 meter/sec RA = 94
01583 deg
ZDOT = 2304
900224 TA = 189
28773
MA = 189
29721
Ha = 188
529 n
mi
Hp = 187
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13132036
13 X = -4051682
67
Y = 7491422
12 feet Y = 2238351
01 meter
Z = 16075398
76 Z = 4880217
67
XDOT = -4265
463491 XDOT = -1230
401536
YDOT = -23710
134549 feet/sec YDOT = -7240
998017 meter/sec
ZDOT = 7562
008609 ZDOT = 2298
753132
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4943851
63 X = -1506885
98
Y = 14374546
90 feet Y = 4381361
89 meter
Z = 15997529
69 Z = 4876047
05
XDOT = -17888
319482 XDOT = -5452
359778
YDOT = -14543
985518 feet/sec YDOT = -4433
006786 meter/sec
ZDOT = 7537
407636 ZDOT = 2297
401848
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 10124
55157838
00016717 00000-0 10270-3 0 9085
2 25544 51
6431 94
5254 0010056 275
0340 84
9675 15
73636568 16606
Satellite: ISS
Catalog Number: 25544
Epoch time: 10124
55157838 = yrday
fracday
Element set: 908
Inclination: 51
6431 deg
RA of node: 94
5254 deg
Eccentricity:
0010056
Arg of perigee: 275
0340 deg
Mean anomaly: 84
9675 deg
Mean motion: 15
73636568 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1660
Checksum: 315
Coasting Arc #10 (Orbit 1674)
---------------------------------------
Vector Time (GMT): 2010/125/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 793683
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1770390
79 A = 6731265
29 meter
Y = 6135900
35 meter E =
0008475
Z = -2110248
05 I = 51
99448
XDOT = -4288
069030 Wp = 319
04356
YDOT = 3153
603445 meter/sec RA = 88
86994 deg
ZDOT = 5565
911585 TA = 17
49146
MA = 17
46229
Ha = 188
968 n
mi
Hp = 187
554
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5808368
74 X = 1711897
69
Y = 20130906
65 feet Y = 6155370
96 meter
Z = -6923386
00 Z = -2101789
27
XDOT = -14068
467946 XDOT = -4350
052734
YDOT = 10346
467996 feet/sec YDOT = 3105
304875 meter/sec
ZDOT = 18260
864781 ZDOT = 5544
929694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17908224
01 X = 5458426
68
Y = 10897372
47 feet Y = 3321519
13 meter
Z = -6889601
58 Z = -2099950
56
XDOT = -2673
301923 XDOT = -814
822426
YDOT = 15898
396441 feet/sec YDOT = 4845
831235 meter/sec
ZDOT = 18177
356124 ZDOT = 5540
458147
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 10125
50414108
00016717 00000-0 10270-3 0 9098
2 25544 51
6430 89
6364 0009900 278
9703 81
0340 15
73646041 16753
Satellite: ISS
Catalog Number: 25544
Epoch time: 10125
50414108 = yrday
fracday
Element set: 909
Inclination: 51
6430 deg
RA of node: 89
6364 deg
Eccentricity:
0009900
Arg of perigee: 278
9703 deg
Mean anomaly: 81
0340 deg
Mean motion: 15
73646041 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1675
Checksum: 295
Coasting Arc #11 (Orbit 1690)
---------------------------------------
Vector Time (GMT): 2010/126/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 793683
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3446803
51 A = 6723056
50 meter
Y = -3181503
05 meter E =
0006032
Z = -4819871
07 I = 51
96620
XDOT = 2710
750470 Wp = 14
18954
YDOT = 6751
384789 meter/sec RA = 83
79930 deg
ZDOT = -2512
878117 TA = 231
29606
MA = 231
35002
Ha = 189
204 n
mi
Hp = 187
437
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11308410
46 X = 3505537
60
Y = -10438002
14 feet Y = -3142630
29 meter
Z = -15813225
28 Z = -4802983
88
XDOT = 8893
538289 XDOT = 2647
260944
YDOT = 22150
212562 feet/sec YDOT = 6781
343106 meter/sec
ZDOT = -8244
350776 ZDOT = -2499
863253
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1094855
21 X = 333711
87
Y = -15419283
77 feet Y = -4699797
69 meter
Z = -15746018
85 Z = -4799386
55
XDOT = 20602
543948 XDOT = 6279
655395
YDOT = 9845
927839 feet/sec YDOT = 3001
038805 meter/sec
ZDOT = -8192
416463 ZDOT = -2497
048538
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 10126
52018624
00016717 00000-0 10270-3 0 9106
2 25544 51
6438 84
4214 0009989 282
9738 77
0309 15
73687067 16919
Satellite: ISS
Catalog Number: 25544
Epoch time: 10126
52018624 = yrday
fracday
Element set: 910
Inclination: 51
6438 deg
RA of node: 84
4214 deg
Eccentricity:
0009989
Arg of perigee: 282
9738 deg
Mean anomaly: 77
0309 deg
Mean motion: 15
73687067 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1691
Checksum: 329
Coasting Arc #12 (Orbit 1706)
---------------------------------------
Vector Time (GMT): 2010/127/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 793683
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2935606
36 A = 6730765
40 meter
Y = -5613436
16 meter E =
0003988
Z = 2269079
38 I = 51
98831
XDOT = 3551
233095 Wp = 110
73546
YDOT = -4075
095382 meter/sec RA = 78
65079 deg
ZDOT = -5480
609865 TA = 43
92363
MA = 43
89193
Ha = 189
469 n
mi
Hp = 187
327
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9631254
45 X = -2883640
56
Y = -18416785
30 feet Y = -5645973
35 meter
Z = 7444486
15 Z = 2254944
24
XDOT = 11651
027213 XDOT = 3623
161562
YDOT = -13369
735504 feet/sec YDOT = -4034
981090 meter/sec
ZDOT = -17981
003493 ZDOT = -5463
183253
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19803328
13 X = -6036054
42
Y = -6372080
81 feet Y = -1942210
23 meter
Z = 7388111
95 Z = 2251896
52
XDOT = -1434
544589 XDOT = -437
249191
YDOT = -16333
562256 feet/sec YDOT = -4978
469776 meter/sec
ZDOT = -17911
656954 ZDOT = -5459
473040
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 10127
53620943
00016717 00000-0 10270-3 0 9112
2 25544 51
6441 79
2066 0010029 287
1021 72
9044 15
73721354 17075
Satellite: ISS
Catalog Number: 25544
Epoch time: 10127
53620943 = yrday
fracday
Element set: 911
Inclination: 51
6441 deg
RA of node: 79
2066 deg
Eccentricity:
0010029
Arg of perigee: 287
1021 deg
Mean anomaly: 72
9044 deg
Mean motion: 15
73721354 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1707
Checksum: 281
Coasting Arc #13 (Orbit 1722)
---------------------------------------
Vector Time (GMT): 2010/128/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 793683
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2735019
94 A = 6723004
92 meter
Y = 3887729
03 meter E =
0002928
Z = 4756943
37 I = 51
95638
XDOT = -3954
976250 Wp = 266
24015
YDOT = -6042
350154 meter/sec RA = 73
58146 deg
ZDOT = 2665
543225 TA = 157
68238
MA = 157
66964
Ha = 189
668 n
mi
Hp = 187
044
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8973162
54 X = -2801398
53
Y = 12755016
50 feet Y = 3856773
19 meter
Z = 15606769
60 Z = 4743495
35
XDOT = -12975
643865 XDOT = -3900
064499
YDOT = -19823
983444 feet/sec YDOT = -6086
270066 meter/sec
ZDOT = 8745
220555 ZDOT = 2646
463072
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2726450
76 X = 831022
19
Y = 15409149
29 feet Y = 4696708
70 meter
Z = 15553261
20 Z = 4740634
01
XDOT = -22141
065710 XDOT = -6748
596829
YDOT = -4828
631578 feet/sec YDOT = -1471
766905 meter/sec
ZDOT = 8669
152811 ZDOT = 2642
357777
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 10128
55220872
00016717 00000-0 10270-3 0 9123
2 25544 51
6447 73
9917 0010147 290
1099 69
8972 15
73789911 17233
Satellite: ISS
Catalog Number: 25544
Epoch time: 10128
55220872 = yrday
fracday
Element set: 912
Inclination: 51
6447 deg
RA of node: 73
9917 deg
Eccentricity:
0010147
Arg of perigee: 290
1099 deg
Mean anomaly: 69
8972 deg
Mean motion: 15
73789911 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1723
Checksum: 330
Coasting Arc #14 (Orbit 1737)
---------------------------------------
Vector Time (GMT): 2010/129/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 793683
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3941173
40 A = 6730394
50 meter
Y = 4898661
05 meter E =
0009692
Z = -2383516
28 I = 51
97109
XDOT = -2666
146307 Wp = 327
58379
YDOT = 4782
413266 meter/sec RA = 68
42912 deg
ZDOT = 5418
348160 TA = 5
67097
MA = 5
66001
Ha = 189
988 n
mi
Hp = 186
802
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12930358
94 X = 3897681
61
Y = 16071722
60 feet Y = 4942490
46 meter
Z = -7819935
32 Z = -2364475
39
XDOT = -8747
199169 XDOT = -2745
747650
YDOT = 15690
332238 feet/sec YDOT = 4752
153672 meter/sec
ZDOT = 17776
732807 ZDOT = 5405
202575
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20587773
97 X = 6275153
51
Y = 1679033
05 feet Y = 511769
27 meter
Z = -7744046
04 Z = -2360385
23
XDOT = 5386
918112 XDOT = 1641
932640
YDOT = 15727
816714 feet/sec YDOT = 4793
838534 meter/sec
ZDOT = 17724
434249 ZDOT = 5402
407559
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 10129
50469051
00016717 00000-0 10270-3 0 9134
2 25544 51
6445 69
1019 0010161 294
6928 65
3177 15
73774083 17385
Satellite: ISS
Catalog Number: 25544
Epoch time: 10129
50469051 = yrday
fracday
Element set: 913
Inclination: 51
6445 deg
RA of node: 69
1019 deg
Eccentricity:
0010161
Arg of perigee: 294
6928 deg
Mean anomaly: 65
3177 deg
Mean motion: 15
73774083 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1738
Checksum: 313
Coasting Arc #15 (Orbit 1753)
---------------------------------------
Vector Time (GMT): 2010/130/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 793683
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1910367
59 A = 6723064
22 meter
Y = -4410438
86 meter E =
0008626
Z = -4705961
09 I = 51
93592
XDOT = 5010
264163 Wp = 10
66879
YDOT = 5139
874747 meter/sec RA = 63
35905 deg
ZDOT = -2775
721138 TA = 232
02709
MA = 232
10505
Ha = 190
042 n
mi
Hp = 186
581
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6267610
19 X = 1982405
02
Y = -14469943
76 feet Y = -4388673
10 meter
Z = -15439504
89 Z = -4696505
49
XDOT = 16437
874552 XDOT = 4965
900960
YDOT = 16863
106124 feet/sec YDOT = 5195
654520 meter/sec
ZDOT = -9106
696648 ZDOT = -2751
488507
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6349103
18 X = -1935206
65
Y = -14474500
23 feet Y = -4411827
67 meter
Z = -15401891
21 Z = -4694496
44
XDOT = 22519
665420 XDOT = 6863
994020
YDOT = -264
423885 feet/sec YDOT = -80
596400 meter/sec
ZDOT = -9010
137400 ZDOT = -2746
289880
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 10130
52064823
00016717 00000-0 10270-3 0 9147
2 25544 51
6455 63
8864 0010100 298
6836 61
3311 15
73837647 17540
Satellite: ISS
Catalog Number: 25544
Epoch time: 10130
52064823 = yrday
fracday
Element set: 914
Inclination: 51
6455 deg
RA of node: 63
8864 deg
Eccentricity:
0010100
Arg of perigee: 298
6836 deg
Mean anomaly: 61
3311 deg
Mean motion: 15
73837647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1754
Checksum: 301
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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