Date:
April 10th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 29600 75 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 1236)
---------------------------------------
Vector Time (GMT): 2010/097/15:58:38
591
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4860918
57 A = 6730156
71 meter
Y = 4447972
69 meter E =
0018575
Z = 1321889
94 I = 51
39749
XDOT = -2441
912639 Wp = 128
55073
YDOT = 4413
473532 meter/sec RA = 231
67685 deg
ZDOT = -5827
589180 TA = 36
87086
MA = 36
74329
Ha = 190
756 n
mi
Hp = 182
021
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15947895
56 X = 4804397
80
Y = 14593086
24 feet Y = 4502014
40 meter
Z = 4336909
25 Z = 1345366
66
XDOT = -8011
524405 XDOT = -2462
774217
YDOT = 14479
900041 feet/sec YDOT = 4386
049742 meter/sec
ZDOT = -19119
387074 ZDOT = -5839
502755
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18276478
46 X = 5570670
64
Y = -11508461
63 feet Y = -3507779
11 meter
Z = 4430346
07 Z = 1350369
48
XDOT = 11043
637296 XDOT = 3366
100648
YDOT = 10105
940060 feet/sec YDOT = 3080
290530 meter/sec
ZDOT = -19166
571949 ZDOT = -5841
971130
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 10097
70012361
00016717 00000-0 10270-3 0 9004
2 25544 51
6456 232
4500 0005132 151
4151 208
7294 15
74433337 12379
Satellite: ISS
Catalog Number: 25544
Epoch time: 10097
70012361 = yrday
fracday
Element set: 900
Inclination: 51
6456 deg
RA of node: 232
4500 deg
Eccentricity:
0005132
Arg of perigee: 151
4151 deg
Mean anomaly: 208
7294 deg
Mean motion: 15
74433337 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1237
Checksum: 267
Coasting Arc #2 (Orbit 1252)
---------------------------------------
Vector Time (GMT): 2010/098/15:58:38
591
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1939224
30 A = 6719249
72 meter
Y = -3895615
95 meter E =
0009053
Z = 5116380
44 I = 51
38136
XDOT = 5941
396142 Wp = 142
18578
YDOT = 4720
921789 meter/sec RA = 226
54417 deg
ZDOT = 1334
290541 TA = 294
96184
MA = 295
05586
Ha = 190
496 n
mi
Hp = 182
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6362284
45 X = 1957787
35
Y = -12780892
22 feet Y = -3873826
32 meter
Z = 16786025
08 Z = 5125846
44
XDOT = 19492
769496 XDOT = 5881
682668
YDOT = 15488
588548 feet/sec YDOT = 4787
028213 meter/sec
ZDOT = 4377
593639 ZDOT = 1363
008363
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10835849
62 X = -3302766
96
Y = -9227930
33 feet Y = -2812673
16 meter
Z = 16823500
59 Z = 5127802
98
XDOT = 19146
718417 XDOT = 5835
919774
YDOT = -14244
233446 feet/sec YDOT = -4341
642354 meter/sec
ZDOT = 4491
878912 ZDOT = 1369
124692
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 10098
71565362
00016717 00000-0 10270-3 0 9011
2 25544 51
6458 227
2315 0004984 156
5689 203
5702 15
74514225 12534
Satellite: ISS
Catalog Number: 25544
Epoch time: 10098
71565362 = yrday
fracday
Element set: 901
Inclination: 51
6458 deg
RA of node: 227
2315 deg
Eccentricity:
0004984
Arg of perigee: 156
5689 deg
Mean anomaly: 203
5702 deg
Mean motion: 15
74514225 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1253
Checksum: 309
Coasting Arc #3 (Orbit 1267)
---------------------------------------
Vector Time (GMT): 2010/099/15:58:38
591
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5477578
04 A = 6730249
95 meter
Y = -3783893
10 meter E =
0008530
Z = -978843
80 I = 51
43968
XDOT = 2046
146451 Wp = 67
05601
YDOT = -4480
657156 meter/sec RA = 221
36745 deg
ZDOT = 5914
702722 TA = 282
22286
MA = 282
31837
Ha = 190
407 n
mi
Hp = 182
165
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17971056
57 X = -5430103
74
Y = -12414347
45 feet Y = -3844881
26 meter
Z = -3211429
79 Z = -1005338
20
XDOT = 6713
078907 XDOT = 2067
365441
YDOT = -14700
318753 feet/sec YDOT = -4457
656885 meter/sec
ZDOT = 19405
192659 ZDOT = 5924
694707
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16217461
86 X = -4943082
37
Y = 14607551
77 feet Y = 4452381
78 meter
Z = -3316857
03 Z = -1010978
02
XDOT = -11718
186969 XDOT = -3571
703388
YDOT = -8626
258340 feet/sec YDOT = -2629
283542 meter/sec
ZDOT = 19444
734742 ZDOT = 5926
755149
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 10099
66767701
00016717 00000-0 10270-3 0 9028
2 25544 51
6452 222
3392 0004685 157
8904 202
2462 15
74518184 12684
Satellite: ISS
Catalog Number: 25544
Epoch time: 10099
66767701 = yrday
fracday
Element set: 902
Inclination: 51
6452 deg
RA of node: 222
3392 deg
Eccentricity:
0004685
Arg of perigee: 157
8904 deg
Mean anomaly: 202
2462 deg
Mean motion: 15
74518184 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1268
Checksum: 316
Coasting Arc #4 (Orbit 1283)
---------------------------------------
Vector Time (GMT): 2010/100/15:58:38
591
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1682838
15 A = 6718652
17 meter
Y = 3915673
93 meter E =
0016251
Z = -5207237
67 I = 51
42481
XDOT = -6544
549825 Wp = 99
99798
YDOT = -3946
825649 meter/sec RA = 216
22962 deg
ZDOT = -857
908554 TA = 161
82757
MA = 161
76943
Ha = 190
218 n
mi
Hp = 182
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5521122
53 X = -1701203
03
Y = 12846699
26 feet Y = 3896752
35 meter
Z = -17084113
10 Z = -5215457
81
XDOT = -21471
620162 XDOT = -6495
761743
YDOT = -12948
903049 feet/sec YDOT = -4019
737978 meter/sec
ZDOT = -2814
660609 ZDOT = -889
583144
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11391257
61 X = 3472055
32
Y = 8040367
83 feet Y = 2450704
11 meter
Z = -17116633
18 Z = -5217149
79
XDOT = -16648
198459 XDOT = -5074
370890
YDOT = 17361
390623 feet/sec YDOT = 5291
751862 meter/sec
ZDOT = -2940
690087 ZDOT = -896
322339
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 10100
68312776
00016717 00000-0 10270-3 0 9032
2 25544 51
6453 217
1199 0004726 161
7946 198
3387 15
74601244 12847
Satellite: ISS
Catalog Number: 25544
Epoch time: 10100
68312776 = yrday
fracday
Element set: 903
Inclination: 51
6453 deg
RA of node: 217
1199 deg
Eccentricity:
0004726
Arg of perigee: 161
7946 deg
Mean anomaly: 198
3387 deg
Mean motion: 15
74601244 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1284
Checksum: 313
Coasting Arc #5 (Orbit 1299)
---------------------------------------
Vector Time (GMT): 2010/101/15:58:38
591
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5937991
47 A = 6730046
99 meter
Y = 3106857
86 meter E =
0017141
Z = 506004
05 I = 51
49013
XDOT = -1822
425261 Wp = 138
20325
YDOT = 4477
496567 meter/sec RA = 211
06373 deg
ZDOT = -6001
820263 TA = 36
27538
MA = 36
15929
Ha = 189
973 n
mi
Hp = 182
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19481599
31 X = 5900350
62
Y = 10193103
20 feet Y = 3173049
59 meter
Z = 1660118
27 Z = 534759
23
XDOT = -5979
085502 XDOT = -1843
202113
YDOT = 14689
949367 feet/sec YDOT = 4457
000465 meter/sec
ZDOT = -19691
011360 ZDOT = -6010
724468
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13826730
81 X = 4214387
55
Y = -17083929
49 feet Y = -5207181
71 meter
Z = 1774521
28 Z = 540874
09
XDOT = 12002
088161 XDOT = 3658
236472
YDOT = 7631
758070 feet/sec YDOT = 2326
159860 meter/sec
ZDOT = -19726
227887 ZDOT = -6012
554260
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 10101
69853586
00016717 00000-0 10270-3 0 9044
2 25544 51
6460 211
9008 0004534 163
4025 196
7288 15
74705840 13008
Satellite: ISS
Catalog Number: 25544
Epoch time: 10101
69853586 = yrday
fracday
Element set: 904
Inclination: 51
6460 deg
RA of node: 211
9008 deg
Eccentricity:
0004534
Arg of perigee: 163
4025 deg
Mean anomaly: 196
7288 deg
Mean motion: 15
74705840 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1300
Checksum: 296
Coasting Arc #6 (Orbit 1315)
---------------------------------------
Vector Time (GMT): 2010/102/15:58:38
591
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1525197
96 A = 6717956
26 meter
Y = -3903712
84 meter E =
0006146
Z = 5247584
35 I = 51
47600
XDOT = 7025
144570 Wp = 146
14251
YDOT = 3151
229690 meter/sec RA = 205
92020 deg
ZDOT = 297
186034 TA = 301
00153
MA = 301
06188
Ha = 189
791 n
mi
Hp = 182
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5003930
32 X = 1543244
59
Y = -12807456
82 feet Y = -3886555
85 meter
Z = 17216484
07 Z = 5255037
96
XDOT = 23048
374573 XDOT = 6987
941138
YDOT = 10338
680085 feet/sec YDOT = 3229
581046 meter/sec
ZDOT = 975
019797 ZDOT = 331
223852
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11715691
38 X = -3570942
73
Y = -7127208
01 feet Y = -2172373
00 meter
Z = 17245958
20 Z = 5256568
06
XDOT = 13796
869682 XDOT = 4205
285879
YDOT = -19951
173506 feet/sec YDOT = -6081
117685 meter/sec
ZDOT = 1110
427018 ZDOT = 338
458155
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 10102
71390242
00016717 00000-0 10270-3 0 9054
2 25544 51
6456 206
6818 0004503 167
1828 192
9451 15
74762214 13166
Satellite: ISS
Catalog Number: 25544
Epoch time: 10102
71390242 = yrday
fracday
Element set: 905
Inclination: 51
6456 deg
RA of node: 206
6818 deg
Eccentricity:
0004503
Arg of perigee: 167
1828 deg
Mean anomaly: 192
9451 deg
Mean motion: 15
74762214 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1316
Checksum: 294
Coasting Arc #7 (Orbit 1330)
---------------------------------------
Vector Time (GMT): 2010/103/15:58:38
591
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6285978
29 A = 6729942
76 meter
Y = -2395441
13 meter E =
0010471
Z = 13865
56 I = 51
54461
XDOT = 1723
531880 Wp = 65
07190
YDOT = -4467
397083 meter/sec RA = 200
76690 deg
ZDOT = 6029
298785 TA = 295
07891
MA = 295
18755
Ha = 189
668 n
mi
Hp = 182
150
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20623288
36 X = -6258792
20
Y = -7859058
83 feet Y = -2465582
68 meter
Z = 45490
68 Z = -16605
91
XDOT = 5654
632151 XDOT = 1744
069396
YDOT = -14656
814576 feet/sec YDOT = -4448
008277 meter/sec
ZDOT = 19781
163994 ZDOT = 6037
722003
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11115780
87 X = -3388090
01
Y = 19066215
68 feet Y = 5811382
54 meter
Z = -75718
87 Z = -23079
11
XDOT = -12167
170086 XDOT = -3708
553442
YDOT = -7042
601012 feet/sec YDOT = -2146
584789 meter/sec
ZDOT = 19814
472635 ZDOT = 6039
451259
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 10103
66577155
00016717 00000-0 10270-3 0 9060
2 25544 51
6459 201
7883 0004224 169
0563 191
0693 15
74783286 13311
Satellite: ISS
Catalog Number: 25544
Epoch time: 10103
66577155 = yrday
fracday
Element set: 906
Inclination: 51
6459 deg
RA of node: 201
7883 deg
Eccentricity:
0004224
Arg of perigee: 169
0563 deg
Mean anomaly: 191
0693 deg
Mean motion: 15
74783286 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1331
Checksum: 315
Coasting Arc #8 (Orbit 1346)
---------------------------------------
Vector Time (GMT): 2010/104/15:58:38
591
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1529925
95 A = 6717686
02 meter
Y = 3909627
29 meter E =
0016213
Z = -5257682
28 I = 51
53342
XDOT = -7312
642901 Wp = 108
07405
YDOT = -2352
673133 meter/sec RA = 195
61495 deg
ZDOT = 374
444088 TA = 165
51428
MA = 165
46775
Ha = 189
463 n
mi
Hp = 182
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5019442
09 X = -1547989
11
Y = 12826861
20 feet Y = 3892417
49 meter
Z = -17249613
77 Z = -5265158
85
XDOT = -23991
610569 XDOT = -7287
610403
YDOT = -7718
743875 feet/sec YDOT = -2434
307474 meter/sec
ZDOT = 1228
491102 ZDOT = 338
979624
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11970868
95 X = 3648720
86
Y = 6737981
49 feet Y = 2053736
76 meter
Z = -17279185
30 Z = -5266695
68
XDOT = -10648
832435 XDOT = -3245
764126
YDOT = 21741
216479 feet/sec YDOT = 6626
722783 meter/sec
ZDOT = 1087
429168 ZDOT = 331
448410
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 10104
68105780
00016717 00000-0 10270-3 0 9075
2 25544 51
6466 196
5683 0004266 173
9306 186
1911 15
74860671 13472
Satellite: ISS
Catalog Number: 25544
Epoch time: 10104
68105780 = yrday
fracday
Element set: 907
Inclination: 51
6466 deg
RA of node: 196
5683 deg
Eccentricity:
0004266
Arg of perigee: 173
9306 deg
Mean anomaly: 186
1911 deg
Mean motion: 15
74860671 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1347
Checksum: 321
Coasting Arc #9 (Orbit 1362)
---------------------------------------
Vector Time (GMT): 2010/105/15:58:38
591
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6463378
38 A = 6729347
31 meter
Y = 1724358
12 meter E =
0014475
Z = -656499
22 I = 51
60196
XDOT = -1801
257999 Wp = 149
97493
YDOT = 4496
490035 meter/sec RA = 190
47705 deg
ZDOT = -5992
252656 TA = 37
18416
MA = 37
08400
Ha = 189
325 n
mi
Hp = 182
078
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21205309
64 X = 6446805
13
Y = 5657342
91 feet Y = 1796542
78 meter
Z = -2153868
82 Z = -625139
87
XDOT = -5909
639105 XDOT = -1822
294879
YDOT = 14752
263895 feet/sec YDOT = 4476
229503 meter/sec
ZDOT = -19659
621575 ZDOT = -6001
054551
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8346660
54 X = 2544062
13
Y = -20310728
33 feet Y = -6190709
99 meter
Z = -2029140
03 Z = -618481
88
XDOT = 12400
188559 XDOT = 3779
577473
YDOT = 7039
423483 feet/sec YDOT = 2145
616278 meter/sec
ZDOT = -19694
445461 ZDOT = -6002
866977
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 10105
69630265
00016717 00000-0 10270-3 0 9089
2 25544 51
6457 191
3481 0004206 176
1318 183
9879 15
74936853 13635
Satellite: ISS
Catalog Number: 25544
Epoch time: 10105
69630265 = yrday
fracday
Element set: 908
Inclination: 51
6457 deg
RA of node: 191
3481 deg
Eccentricity:
0004206
Arg of perigee: 176
1318 deg
Mean anomaly: 183
9879 deg
Mean motion: 15
74936853 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1363
Checksum: 328
Coasting Arc #10 (Orbit 1378)
---------------------------------------
Vector Time (GMT): 2010/106/15:58:38
591
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1628317
26 A = 6717594
46 meter
Y = -3964710
10 meter E =
0003746
Z = 5169549
79 I = 51
59195
XDOT = 7454
543967 Wp = 122
09720
YDOT = 1592
096788 meter/sec RA = 185
31596 deg
ZDOT = -1128
378724 TA = 338
66527
MA = 338
68088
Ha = 189
052 n
mi
Hp = 182
066
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5342248
23 X = 1647417
15
Y = -13007579
06 feet Y = -3946394
47 meter
Z = 16960465
18 Z = 5177506
70
XDOT = 24457
165246 XDOT = 7441
668369
YDOT = 5223
414659 feet/sec YDOT = 1675
385938 meter/sec
ZDOT = -3702
029933 ZDOT = -1092
195189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12338822
89 X = -3760873
22
Y = -6664905
50 feet Y = -2031463
20 meter
Z = 16991956
71 Z = 5179148
40
XDOT = 7443
701794 XDOT = 2268
840307
YDOT = -22840
530801 feet/sec YDOT = -6961
793788 meter/sec
ZDOT = -3558
115380 ZDOT = -1084
513568
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 10106
71150609
00016717 00000-0 10270-3 0 9093
2 25544 51
6445 186
1277 0004059 179
4150 180
7020 15
75011982 13791
Satellite: ISS
Catalog Number: 25544
Epoch time: 10106
71150609 = yrday
fracday
Element set: 909
Inclination: 51
6445 deg
RA of node: 186
1277 deg
Eccentricity:
0004059
Arg of perigee: 179
4150 deg
Mean anomaly: 180
7020 deg
Mean motion: 15
75011982 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1379
Checksum: 298
Coasting Arc #11 (Orbit 1394)
---------------------------------------
Vector Time (GMT): 2010/107/15:58:38
591
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6502774
51 A = 6728394
90 meter
Y = -1075558
33 meter E =
0012156
Z = 1331992
31 I = 51
65891
XDOT = 1968
565033 Wp = 75
18284
YDOT = -4614
737295 meter/sec RA = 180
19434 deg
ZDOT = 5843
072399 TA = 299
44573
MA = 299
56698
Ha = 188
873 n
mi
Hp = 182
141
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21334562
05 X = -6496734
80
Y = -3528734
69 feet Y = -1148242
48 meter
Z = 4370053
50 Z = 1300415
99
XDOT = 6458
546697 XDOT = 1991
636513
YDOT = -15140
214224 feet/sec YDOT = -4592
594737 meter/sec
ZDOT = 19170
185035 ZDOT = 5852
691794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5537488
52 X = -1687826
50
Y = 20929253
33 feet Y = 6379236
41 meter
Z = 4244461
12 Z = 1293711
75
XDOT = -12943
846474 XDOT = -3945
284405
YDOT = -7348
322081 feet/sec YDOT = -2239
768570 meter/sec
ZDOT = 19208
271420 ZDOT = 5854
681129
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 10107
72666878
00016717 00000-0 10270-3 0 9107
2 25544 51
6444 180
9073 0003954 184
2467 175
8664 15
75074717 13956
Satellite: ISS
Catalog Number: 25544
Epoch time: 10107
72666878 = yrday
fracday
Element set: 910
Inclination: 51
6444 deg
RA of node: 180
9073 deg
Eccentricity:
0003954
Arg of perigee: 184
2467 deg
Mean anomaly: 175
8664 deg
Mean motion: 15
75074717 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1395
Checksum: 337
Coasting Arc #12 (Orbit 1409)
---------------------------------------
Vector Time (GMT): 2010/108/15:58:38
591
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1832136
23 A = 6718165
91 meter
Y = 4122337
67 meter E =
0014031
Z = -4990742
44 I = 51
65473
XDOT = -7383
444115 Wp = 120
52716
YDOT = -910
074558 meter/sec RA = 175
02330 deg
ZDOT = 1955
867090 TA = 168
40635
MA = 168
37401
Ha = 188
678 n
mi
Hp = 182
125
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6010945
65 X = -1853852
38
Y = 13524729
89 feet Y = 4101728
38 meter
Z = -16373826
91 Z = -4999695
68
XDOT = -24223
898014 XDOT = -7382
220099
YDOT = -2985
808918 feet/sec YDOT = -992
633843 meter/sec
ZDOT = 6416
886778 ZDOT = 1920
000842
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13024180
14 X = 3969770
11
Y = 6946793
14 feet Y = 2117382
55 meter
Z = -16409289
77 Z = -5001551
52
XDOT = -4354
051159 XDOT = -1327
114793
YDOT = 23006
413658 feet/sec YDOT = 7012
354883 meter/sec
ZDOT = 6274
224512 ZDOT = 1912
383631
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 10108
67834708
00016717 00000-0 10270-3 0 9112
2 25544 51
6440 176
0122 0003839 189
0418 171
0677 15
75105347 14108
Satellite: ISS
Catalog Number: 25544
Epoch time: 10108
67834708 = yrday
fracday
Element set: 911
Inclination: 51
6440 deg
RA of node: 176
0122 deg
Eccentricity:
0003839
Arg of perigee: 189
0418 deg
Mean anomaly: 171
0677 deg
Mean motion: 15
75105347 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1410
Checksum: 294
Coasting Arc #13 (Orbit 1425)
---------------------------------------
Vector Time (GMT): 2010/109/15:58:38
591
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6363952
72 A = 6726986
71 meter
Y = 548422
59 meter E =
0009396
Z = -2095572
95 I = 51
71378
XDOT = -2240
127189 Wp = 158
50807
YDOT = 4848
419170 meter/sec RA = 169
91656 deg
ZDOT = -5550
460786 TA = 44
89141
MA = 44
81546
Ha = 188
578 n
mi
Hp = 182
172
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20879109
98 X = 6367527
16
Y = 1799286
72 feet Y = 619608
16 meter
Z = -6875239
34 Z = -2064647
95
XDOT = -7349
498653 XDOT = -2267
213269
YDOT = 15906
887041 feet/sec YDOT = 4823
217502 meter/sec
ZDOT = -18210
173182 ZDOT = -5561
409006
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3061289
35 X = 933080
99
Y = -20772086
42 feet Y = -6331331
94 meter
Z = -6752223
00 Z = -2058077
57
XDOT = 13924
449239 XDOT = 4244
172128
YDOT = 7967
878938 feet/sec YDOT = 2428
609500 meter/sec
ZDOT = -18253
553024 ZDOT = -5563
682962
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 10109
69343175
00016717 00000-0 10270-3 0 9129
2 25544 51
6427 170
7901 0003792 191
6103 168
4974 15
75175231 14263
Satellite: ISS
Catalog Number: 25544
Epoch time: 10109
69343175 = yrday
fracday
Element set: 912
Inclination: 51
6427 deg
RA of node: 170
7901 deg
Eccentricity:
0003792
Arg of perigee: 191
6103 deg
Mean anomaly: 168
4974 deg
Mean motion: 15
75175231 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1426
Checksum: 306
Coasting Arc #14 (Orbit 1441)
---------------------------------------
Vector Time (GMT): 2010/110/15:58:38
591
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2067280
40 A = 6719091
56 meter
Y = -4374340
64 meter E =
0005955
Z = 4657319
02 I = 51
71735
XDOT = 7157
654985 Wp = 89
02819
YDOT = 363
892362 meter/sec RA = 164
73708 deg
ZDOT = -2832
144784 TA = 28
90541
MA = 28
87243
Ha = 188
205 n
mi
Hp = 182
155
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6782416
01 X = 2093416
95
Y = -14351511
30 feet Y = -4351077
09 meter
Z = 15279918
04 Z = 4667425
24
XDOT = 23483
120029 XDOT = 7166
811980
YDOT = 1193
872578 feet/sec YDOT = 443
984805 meter/sec
ZDOT = -9291
813597 ZDOT = -2797
350559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14047763
83 X = -4281758
42
Y = -7307649
40 feet Y = -2227371
54 meter
Z = 15319971
61 Z = 4669527
35
XDOT = 1679
143692 XDOT = 511
802997
YDOT = -22439
259632 feet/sec YDOT = -6839
486336 meter/sec
ZDOT = -9153
395880 ZDOT = -2789
955064
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 10110
70847526
00016717 00000-0 10270-3 0 9133
2 25544 51
6424 165
5682 0003658 197
6874 162
4163 15
75255744 14420
Satellite: ISS
Catalog Number: 25544
Epoch time: 10110
70847526 = yrday
fracday
Element set: 913
Inclination: 51
6424 deg
RA of node: 165
5682 deg
Eccentricity:
0003658
Arg of perigee: 197
6874 deg
Mean anomaly: 162
4163 deg
Mean motion: 15
75255744 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1442
Checksum: 317
Coasting Arc #15 (Orbit 1457)
---------------------------------------
Vector Time (GMT): 2010/111/15:58:38
591
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6086653
79 A = 6724916
22 meter
Y = -135035
94 meter E =
0012000
Z = 2847886
84 I = 51
76642
XDOT = 2506
888120 Wp = 96
18631
YDOT = -5208
580026 meter/sec RA = 159
64490 deg
ZDOT = 5091
361839 TA = 296
45773
MA = 296
58079
Ha = 188
051 n
mi
Hp = 182
180
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19969336
57 X = -6098525
93
Y = -443031
29 feet Y = -203166
94 meter
Z = 9343460
76 Z = 2818289
05
XDOT = 8224
698557 XDOT = 2540
212179
YDOT = -17088
517146 feet/sec YDOT = -5180
360257 meter/sec
ZDOT = 16703
943040 ZDOT = 5103
621166
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -965725
47 X = -294353
12
Y = 20005615
35 feet Y = 6097711
56 meter
Z = 9225706
89 Z = 2811995
46
XDOT = -15411
132520 XDOT = -4697
313192
YDOT = -8499
380145 feet/sec YDOT = -2590
611068 meter/sec
ZDOT = 16752
539272 ZDOT = 5106
173970
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 10111
72347837
00016717 00000-0 10270-3 0 9147
2 25544 51
6424 160
3466 0003731 202
3097 157
7905 15
75343502 14584
Satellite: ISS
Catalog Number: 25544
Epoch time: 10111
72347837 = yrday
fracday
Element set: 914
Inclination: 51
6424 deg
RA of node: 160
3466 deg
Eccentricity:
0003731
Arg of perigee: 202
3097 deg
Mean anomaly: 157
7905 deg
Mean motion: 15
75343502 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1458
Checksum: 295
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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