Date:
March 30th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 23680 6 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 1091)
---------------------------------------
Vector Time (GMT): 2010/088/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2740499
66 A = 6729835
67 meter
Y = -5705904
49 meter E =
0018398
Z = 2267058
37 I = 51
32074
XDOT = 3763
503846 Wp = 85
61603
YDOT = 3975
304830 meter/sec RA = 278
99292 deg
ZDOT = 5419
516090 TA = 299
97314
MA = 300
15564
Ha = 192
003 n
mi
Hp = 181
826
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8991140
61 X = 2793087
47
Y = -18720159
10 feet Y = -5674964
30 meter
Z = 7437855
56 Z = 2280500
12
XDOT = 12347
453564 XDOT = 3692
444546
YDOT = 13042
338682 feet/sec YDOT = 4016
993891 meter/sec
ZDOT = 17780
564600 ZDOT = 5437
626109
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6938066
59 X = 2114722
70
Y = -19553869
04 feet Y = -5960019
28 meter
Z = 7491067
93 Z = 2283277
51
XDOT = 12115
015988 XDOT = 3692
656873
YDOT = 11183
339239 feet/sec YDOT = 3408
681800 meter/sec
ZDOT = 17852
604160 ZDOT = 5441
473748
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 10088
55896497
00016717 00000-0 10270-3 0 9007
2 25544 51
6409 279
3986 0005751 119
8697 240
3039 15
74028235 10920
Satellite: ISS
Catalog Number: 25544
Epoch time: 10088
55896497 = yrday
fracday
Element set: 900
Inclination: 51
6409 deg
RA of node: 279
3986 deg
Eccentricity:
0005751
Arg of perigee: 119
8697 deg
Mean anomaly: 240
3039 deg
Mean motion: 15
74028235 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1092
Checksum: 341
Coasting Arc #2 (Orbit 1106)
---------------------------------------
Vector Time (GMT): 2010/089/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3576991
66 A = 6722278
55 meter
Y = -3207193
81 meter E =
0017083
Z = -4718306
65 I = 51
29162
XDOT = 2567
862825 Wp = 113
37217
YDOT = -6747
357784 meter/sec RA = 273
79088 deg
ZDOT = 2640
585914 TA = 182
73961
MA = 182
74898
Ha = 191
983 n
mi
Hp = 181
699
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11735536
95 X = -3517941
60
Y = -10522289
39 feet Y = -3246864
18 meter
Z = -15480008
70 Z = -4735539
99
XDOT = 8424
746801 XDOT = 2630
294581
YDOT = -22137
000604 feet/sec YDOT = -6718
293063 meter/sec
ZDOT = 8663
339614 ZDOT = 2653
213008
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12839132
89 X = -3913367
70
Y = -9026156
07 feet Y = -2751172
37 meter
Z = -15548544
76 Z = -4739196
44
XDOT = 4957
027601 XDOT = 1510
902013
YDOT = -22055
592591 feet/sec YDOT = -6722
544622 meter/sec
ZDOT = 8713
282187 ZDOT = 2655
808411
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 10089
51128724
00016717 00000-0 10270-3 0 9016
2 25544 51
6405 274
5064 0005838 122
6387 237
5341 15
74057197 11074
Satellite: ISS
Catalog Number: 25544
Epoch time: 10089
51128724 = yrday
fracday
Element set: 901
Inclination: 51
6405 deg
RA of node: 274
5064 deg
Eccentricity:
0005838
Arg of perigee: 122
6387 deg
Mean anomaly: 237
5341 deg
Mean motion: 15
74057197 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1107
Checksum: 304
Coasting Arc #3 (Orbit 1122)
---------------------------------------
Vector Time (GMT): 2010/090/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1758396
10 A = 6729364
63 meter
Y = 6045772
81 meter E =
0011310
Z = -2370420
50 I = 51
31573
XDOT = -4375
134803 Wp = 129
24614
YDOT = -3366
638493 meter/sec RA = 268
67241 deg
ZDOT = -5365
251561 TA = 77
58515
MA = 77
45860
Ha = 191
801 n
mi
Hp = 181
770
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5769016
08 X = -1814355
15
Y = 19835212
65 feet Y = 6025796
30 meter
Z = -7776970
15 Z = -2379099
29
XDOT = -14354
116808 XDOT = -4311
099628
YDOT = -11045
401879 feet/sec YDOT = -3415
206258 meter/sec
ZDOT = -17602
531367 ZDOT = -5386
350323
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2913699
20 X = -888095
52
Y = 20437542
61 feet Y = 6229362
99 meter
Z = -7811253
49 Z = -2380870
06
XDOT = -14155
607754 XDOT = -4314
629244
YDOT = -8747
760587 feet/sec YDOT = -2666
317427 meter/sec
ZDOT = -17686
424276 ZDOT = -5390
822119
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 10090
52706773
00016717 00000-0 10270-3 0 9026
2 25544 51
6408 269
2893 0005731 124
8978 235
2724 15
74120054 11231
Satellite: ISS
Catalog Number: 25544
Epoch time: 10090
52706773 = yrday
fracday
Element set: 902
Inclination: 51
6408 deg
RA of node: 269
2893 deg
Eccentricity:
0005731
Arg of perigee: 124
8978 deg
Mean anomaly: 235
2724 deg
Mean motion: 15
74120054 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1123
Checksum: 301
Coasting Arc #4 (Orbit 1138)
---------------------------------------
Vector Time (GMT): 2010/091/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4054715
74 A = 6722287
97 meter
Y = 2650627
85 meter E =
0011422
Z = 4650873
71 I = 51
29354
XDOT = -1426
306652 Wp = 90
47032
YDOT = 7050
794769 meter/sec RA = 263
46893 deg
ZDOT = -2769
152311 TA = 26
96979
MA = 26
91047
Ha = 191
655 n
mi
Hp = 181
868
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13302873
15 X = 4002181
26
Y = 8696285
59 feet Y = 2695676
62 meter
Z = 15258772
03 Z = 4670443
95
XDOT = -4679
483766 XDOT = -1491
591724
YDOT = 23132
528769 feet/sec YDOT = 7034
479773 meter/sec
ZDOT = -9085
145378 ZDOT = -2776
240355
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14406848
47 X = 4391207
41
Y = 6531011
31 feet Y = 1990652
25 meter
Z = 15336575
55 Z = 4674588
23
XDOT = -487
746499 XDOT = -148
665133
YDOT = 22520
048580 feet/sec YDOT = 6864
110807 meter/sec
ZDOT = -9113
081731 ZDOT = -2777
667312
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 10091
54281939
00016717 00000-0 10270-3 0 9032
2 25544 51
6405 264
0713 0005762 130
2979 229
8688 15
74125309 11391
Satellite: ISS
Catalog Number: 25544
Epoch time: 10091
54281939 = yrday
fracday
Element set: 903
Inclination: 51
6405 deg
RA of node: 264
0713 deg
Eccentricity:
0005762
Arg of perigee: 130
2979 deg
Mean anomaly: 229
8688 deg
Mean motion: 15
74125309 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1139
Checksum: 317
Coasting Arc #5 (Orbit 1154)
---------------------------------------
Vector Time (GMT): 2010/092/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 741676
63 A = 6728945
66 meter
Y = -6208101
19 meter E =
0017592
Z = 2473252
72 I = 51
32158
XDOT = 4889
890905 Wp = 91
67357
YDOT = 2708
522495 meter/sec RA = 258
35093 deg
ZDOT = 5299
316007 TA = 296
43811
MA = 296
61851
Ha = 191
621 n
mi
Hp = 181
811
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2433322
28 X = 799026
89
Y = -20367786
06 feet Y = -6199486
58 meter
Z = 8114346
19 Z = 2476995
32
XDOT = 16042
949162 XDOT = 4833
496968
YDOT = 8886
228658 feet/sec YDOT = 2762
889023 meter/sec
ZDOT = 17386
207373 ZDOT = 5322
934211
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1170468
64 X = -356758
84
Y = -20473382
30 feet Y = -6240286
92 meter
Z = 8129022
12 Z = 2477725
94
XDOT = 15743
415558 XDOT = 4798
593062
YDOT = 6083
329659 feet/sec YDOT = 1854
198880 meter/sec
ZDOT = 17480
094521 ZDOT = 5327
932810
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 10092
55853980
00016717 00000-0 10270-3 0 9046
2 25544 51
6408 258
8533 0005788 134
1187 226
0453 15
74199228 11555
Satellite: ISS
Catalog Number: 25544
Epoch time: 10092
55853980 = yrday
fracday
Element set: 904
Inclination: 51
6408 deg
RA of node: 258
8533 deg
Eccentricity:
0005788
Arg of perigee: 134
1187 deg
Mean anomaly: 226
0453 deg
Mean motion: 15
74199228 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1155
Checksum: 325
Coasting Arc #6 (Orbit 1169)
---------------------------------------
Vector Time (GMT): 2010/093/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4468234
98 A = 6722289
33 meter
Y = -2089133
01 meter E =
0015943
Z = -4582987
70 I = 51
30783
XDOT = 307
024687 Wp = 119
52511
YDOT = -7098
567720 meter/sec RA = 253
14668 deg
ZDOT = 2936
439611 TA = 179
77325
MA = 179
77253
Ha = 191
541 n
mi
Hp = 181
682
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14659563
59 X = -4422278
40
Y = -6854110
94 feet Y = -2138842
59 meter
Z = -15036048
88 Z = -4604582
82
XDOT = 1007
298843 XDOT = 372
114562
YDOT = -23289
264173 feet/sec YDOT = -7094
770404 meter/sec
ZDOT = 9633
988225 ZDOT = 2938
089360
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15606728
52 X = -4756930
85
Y = -3965211
48 feet Y = -1208596
46 meter
Z = -15121889
10 Z = -4609151
80
XDOT = -3774
818827 XDOT = -1150
564779
YDOT = -21908
250820 feet/sec YDOT = -6677
634850 meter/sec
ZDOT = 9640
323255 ZDOT = 2938
370528
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 10093
51075071
00016717 00000-0 10270-3 0 9051
2 25544 51
6417 253
9619 0005817 136
8725 223
2895 15
74237173 11704
Satellite: ISS
Catalog Number: 25544
Epoch time: 10093
51075071 = yrday
fracday
Element set: 905
Inclination: 51
6417 deg
RA of node: 253
9619 deg
Eccentricity:
0005817
Arg of perigee: 136
8725 deg
Mean anomaly: 223
2895 deg
Mean motion: 15
74237173 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1170
Checksum: 309
Coasting Arc #7 (Orbit 1185)
---------------------------------------
Vector Time (GMT): 2010/094/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 176766
36 A = 6728189
92 meter
Y = 6167677
24 meter E =
0010476
Z = -2679015
83 I = 51
33817
XDOT = -5305
264116 Wp = 132
73589
YDOT = -2086
707148 meter/sec RA = 248
03159 deg
ZDOT = -5173
903716 TA = 77
93080
MA = 77
81343
Ha = 191
336 n
mi
Hp = 181
815
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 579942
11 X = 120799
33
Y = 20235161
56 feet Y = 6169341
00 meter
Z = -8789422
01 Z = -2678293
09
XDOT = -17405
722164 XDOT = -5256
401970
YDOT = -6846
152059 feet/sec YDOT = -2145
760604 meter/sec
ZDOT = -16974
749724 ZDOT = -5199
558008
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4798698
04 X = 1462643
16
Y = 19667852
96 feet Y = 5994761
58 meter
Z = -8786358
31 Z = -2678082
01
XDOT = -16912
482407 XDOT = -5154
924638
YDOT = -3473
351852 feet/sec YDOT = -1058
677644 meter/sec
ZDOT = -17076
722705 ZDOT = -5204
985080
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 10094
52641150
00016717 00000-0 10270-3 0 9061
2 25544 51
6417 248
7440 0005664 139
7317 220
4267 15
74302928 11867
Satellite: ISS
Catalog Number: 25544
Epoch time: 10094
52641150 = yrday
fracday
Element set: 906
Inclination: 51
6417 deg
RA of node: 248
7440 deg
Eccentricity:
0005664
Arg of perigee: 139
7317 deg
Mean anomaly: 220
4267 deg
Mean motion: 15
74302928 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1186
Checksum: 302
Coasting Arc #8 (Orbit 1201)
---------------------------------------
Vector Time (GMT): 2010/095/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4790278
80 A = 6722561
10 meter
Y = 1535438
96 meter E =
0011689
Z = 4448977
18 I = 51
33141
XDOT = 722
542041 Wp = 96
13630
YDOT = 6983
506349 meter/sec RA = 242
82569 deg
ZDOT = -3182
215580 TA = 25
81352
MA = 25
75523
Ha = 191
176 n
mi
Hp = 181
897
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15716137
79 X = 4751140
95
Y = 5037529
40 feet Y = 1588787
92 meter
Z = 14596381
83 Z = 4472153
21
XDOT = 2370
544753 XDOT = 659
856107
YDOT = 22911
766236 feet/sec YDOT = 6991
235715 meter/sec
ZDOT = -10440
339830 ZDOT = -3178
857817
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16360413
27 X = 4986653
97
Y = 1418738
97 feet Y = 432431
64 meter
Z = 14688502
62 Z = 4477055
60
XDOT = 7592
507486 XDOT = 2314
196282
YDOT = 20596
097698 feet/sec YDOT = 6277
690578 meter/sec
ZDOT = -10426
776187 ZDOT = -3178
081382
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 10095
54204275
00016717 00000-0 10270-3 0 9078
2 25544 51
6413 243
5260 0005741 144
1544 216
0005 15
74306443 12020
Satellite: ISS
Catalog Number: 25544
Epoch time: 10095
54204275 = yrday
fracday
Element set: 907
Inclination: 51
6413 deg
RA of node: 243
5260 deg
Eccentricity:
0005741
Arg of perigee: 144
1544 deg
Mean anomaly: 216
0005 deg
Mean motion: 15
74306443 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1202
Checksum: 262
Coasting Arc #9 (Orbit 1217)
---------------------------------------
Vector Time (GMT): 2010/096/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1052217
55 A = 6727408
81 meter
Y = -5981153
38 meter E =
0016472
Z = 2884064
27 I = 51
36452
XDOT = 5658
883996 Wp = 100
14306
YDOT = 1439
685497 meter/sec RA = 237
71428 deg
ZDOT = 5023
116439 TA = 293
16766
MA = 293
34110
Ha = 191
052 n
mi
Hp = 181
885
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3452157
31 X = -999267
20
Y = -19623206
61 feet Y = -5992623
78 meter
Z = 9462153
10 Z = 2879081
36
XDOT = 18565
892375 XDOT = 5617
963335
YDOT = 4723
377616 feet/sec YDOT = 1502
737810 meter/sec
ZDOT = 16480
040812 ZDOT = 5050
507719
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8117397
16 X = -2474182
66
Y = -18206413
65 feet Y = -5549314
88 meter
Z = 9442157
30 Z = 2877969
55
XDOT = 17734
886222 XDOT = 5405
593320
YDOT = 742
461472 feet/sec YDOT = 226
302257 meter/sec
ZDOT = 16588
915443 ZDOT = 5056
301427
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 10096
55763955
00016717 00000-0 10270-3 0 9086
2 25544 51
6424 238
3081 0005650 148
9162 211
2337 15
74411112 12184
Satellite: ISS
Catalog Number: 25544
Epoch time: 10096
55763955 = yrday
fracday
Element set: 908
Inclination: 51
6424 deg
RA of node: 238
3081 deg
Eccentricity:
0005650
Arg of perigee: 148
9162 deg
Mean anomaly: 211
2337 deg
Mean motion: 15
74411112 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1218
Checksum: 294
Coasting Arc #10 (Orbit 1232)
---------------------------------------
Vector Time (GMT): 2010/097/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5086145
40 A = 6722848
48 meter
Y = -985665
80 meter E =
0013505
Z = -4298652
38 I = 51
36688
XDOT = -1631
777926 Wp = 126
29837
YDOT = -6670
585305 meter/sec RA = 232
50833 deg
ZDOT = 3459
933289 TA = 178
87279
MA = 178
86975
Ha = 190
929 n
mi
Hp = 181
847
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16686828
73 X = -5053863
56
Y = -3233811
67 feet Y = -1042361
76 meter
Z = -14103190
21 Z = -4323282
25
XDOT = -5353
602118 XDOT = -1573
872587
YDOT = -21885
122391 feet/sec YDOT = -6688
508924 meter/sec
ZDOT = 11351
487169 ZDOT = 3452
147060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16877249
95 X = -5144185
79
Y = 1138114
47 feet Y = 346897
29 meter
Z = -14201087
80 Z = -4328491
56
XDOT = -10775
627415 XDOT = -3284
411236
YDOT = -18528
254598 feet/sec YDOT = -5647
412001 meter/sec
ZDOT = 11320
320090 ZDOT = 3450
433563
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
50973555
00016717 00000-0 10270-3 0 9092
2 25544 51
6426 233
4165 0005483 151
4273 208
7192 15
74420808 12330
Satellite: ISS
Catalog Number: 25544
Epoch time: 10097
50973555 = yrday
fracday
Element set: 909
Inclination: 51
6426 deg
RA of node: 233
4165 deg
Eccentricity:
0005483
Arg of perigee: 151
4273 deg
Mean anomaly: 208
7192 deg
Mean motion: 15
74420808 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1233
Checksum: 306
Coasting Arc #11 (Orbit 1248)
---------------------------------------
Vector Time (GMT): 2010/098/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1757919
53 A = 6726455
70 meter
Y = 5660852
83 meter E =
0008903
Z = -3178774
95 I = 51
39886
XDOT = -5965
135033 Wp = 130
76002
YDOT = -831
929175 meter/sec RA = 227
40010 deg
ZDOT = -4794
823175 TA = 86
44967
MA = 86
34785
Ha = 190
771 n
mi
Hp = 182
022
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5767452
54 X = 1709930
03
Y = 18572351
81 feet Y = 5680242
45 meter
Z = -10429051
69 Z = -3170351
90
XDOT = -19570
652997 XDOT = -5932
096671
YDOT = -2729
426427 feet/sec YDOT = -898
450387 meter/sec
ZDOT = -15731
047163 ZDOT = -4823
721322
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10684084
15 X = 3256508
85
Y = 16271057
38 feet Y = 4959418
29 meter
Z = -10395379
62 Z = -3168511
71
XDOT = -18295
482424 XDOT = -5576
463043
YDOT = 1920
063688 feet/sec YDOT = 585
235412 meter/sec
ZDOT = -15845
908189 ZDOT = -4829
832816
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
52527287
00016717 00000-0 10270-3 0 9104
2 25544 51
6427 228
1973 0005438 155
2453 204
8972 15
74474089 12491
Satellite: ISS
Catalog Number: 25544
Epoch time: 10098
52527287 = yrday
fracday
Element set: 910
Inclination: 51
6427 deg
RA of node: 228
1973 deg
Eccentricity:
0005438
Arg of perigee: 155
2453 deg
Mean anomaly: 204
8972 deg
Mean motion: 15
74474089 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1249
Checksum: 329
Coasting Arc #12 (Orbit 1264)
---------------------------------------
Vector Time (GMT): 2010/099/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5325061
67 A = 6723424
20 meter
Y = 445853
14 meter E =
0012499
Z = 4068061
92 I = 51
41097
XDOT = 2388
213553 Wp = 101
73236
YDOT = 6263
633289 meter/sec RA = 222
19396 deg
ZDOT = -3805
309130 TA = 27
46735
MA = 27
40135
Ha = 190
551 n
mi
Hp = 182
039
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17470674
76 X = 5299918
46
Y = 1462772
78 feet Y = 505260
84 meter
Z = 13346659
85 Z = 4093869
85
XDOT = 7835
346302 XDOT = 2336
480410
YDOT = 20549
977983 feet/sec YDOT = 6290
050208 meter/sec
ZDOT = -12484
610005 ZDOT = -3793
833313
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17069125
52 X = 5202669
46
Y = -3641503
61 feet Y = -1109930
30 meter
Z = 13449234
75 Z = 4099326
75
XDOT = 13260
775766 XDOT = 4041
884454
YDOT = 16129
858764 feet/sec YDOT = 4916
380951 meter/sec
ZDOT = -12438
775744 ZDOT = -3791
338847
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
54077936
00016717 00000-0 10270-3 0 9119
2 25544 51
6433 222
9790 0005434 157
9884 202
1514 15
74500405 12653
Satellite: ISS
Catalog Number: 25544
Epoch time: 10099
54077936 = yrday
fracday
Element set: 911
Inclination: 51
6433 deg
RA of node: 222
9790 deg
Eccentricity:
0005434
Arg of perigee: 157
9884 deg
Mean anomaly: 202
1514 deg
Mean motion: 15
74500405 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1265
Checksum: 306
Coasting Arc #13 (Orbit 1280)
---------------------------------------
Vector Time (GMT): 2010/100/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2364420
02 A = 6725255
52 meter
Y = -5251318
91 meter E =
0014979
Z = 3466346
81 I = 51
44213
XDOT = 6232
318418 Wp = 111
18785
YDOT = 192
891827 meter/sec RA = 217
09039 deg
ZDOT = 4522
324892 TA = 290
07130
MA = 290
23246
Ha = 190
406 n
mi
Hp = 182
052
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7757283
53 X = -2322361
97
Y = -17228736
58 feet Y = -5277523
84 meter
Z = 11372528
90 Z = 3454963
03
XDOT = 20447
238904 XDOT = 6207
729652
YDOT = 632
847201 feet/sec YDOT = 262
448181 meter/sec
ZDOT = 14837
023923 ZDOT = 4552
541714
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12725309
50 X = -3878674
34
Y = -14003669
17 feet Y = -4268318
36 meter
Z = 11327090
24 Z = 3452497
11
XDOT = 18553
672012 XDOT = 5655
159229
YDOT = -4705
688307 feet/sec YDOT = -1434
293796 meter/sec
ZDOT = 14957
116882 ZDOT = 4558
929226
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
55625082
00016717 00000-0 10270-3 0 9125
2 25544 51
6442 217
7599 0005297 162
6774 197
4571 15
74610677 12810
Satellite: ISS
Catalog Number: 25544
Epoch time: 10100
55625082 = yrday
fracday
Element set: 912
Inclination: 51
6442 deg
RA of node: 217
7599 deg
Eccentricity:
0005297
Arg of perigee: 162
6774 deg
Mean anomaly: 197
4571 deg
Mean motion: 15
74610677 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1281
Checksum: 319
Coasting Arc #14 (Orbit 1295)
---------------------------------------
Vector Time (GMT): 2010/101/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5553668
34 A = 6724045
02 meter
Y = 110344
80 meter E =
0009860
Z = -3800861
74 I = 51
46342
XDOT = -2963
309118 Wp = 132
27337
YDOT = -5748
794395 meter/sec RA = 211
88591 deg
ZDOT = 4163
328148 TA = 181
51191
MA = 181
51489
Ha = 190
223 n
mi
Hp = 182
076
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18220696
65 X = -5536025
52
Y = 362023
63 feet Y = 48338
72 meter
Z = -12470018
83 Z = -3827798
69
XDOT = -9722
142776 XDOT = -2919
029586
YDOT = -18860
874000 feet/sec YDOT = -5781
683964 meter/sec
ZDOT = 13659
213084 ZDOT = 4149
040373
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17059782
83 X = -5199821
81
Y = 6197363
13 feet Y = 1888956
28 meter
Z = -12577071
10 Z = -3833491
27
XDOT = -14911
458541 XDOT = -4545
012563
YDOT = -13445
204835 feet/sec YDOT = -4098
098434 meter/sec
ZDOT = 13602
208209 ZDOT = 4145
953062
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
50822989
00016717 00000-0 10270-3 0 9137
2 25544 51
6444 212
8678 0005055 166
3098 193
8203 15
74614011 12962
Satellite: ISS
Catalog Number: 25544
Epoch time: 10101
50822989 = yrday
fracday
Element set: 913
Inclination: 51
6444 deg
RA of node: 212
8678 deg
Eccentricity:
0005055
Arg of perigee: 166
3098 deg
Mean anomaly: 193
8203 deg
Mean motion: 15
74614011 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1296
Checksum: 303
Coasting Arc #15 (Orbit 1311)
---------------------------------------
Vector Time (GMT): 2010/102/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 782570
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2763840
41 A = 6723998
32 meter
Y = 4798188
47 meter E =
0007744
Z = -3817653
25 I = 51
49023
XDOT = -6468
854131 Wp = 116
63776
YDOT = 432
747989 meter/sec RA = 206
78613 deg
ZDOT = -4149
196177 TA = 109
86324
MA = 109
77976
Ha = 190
104 n
mi
Hp = 182
246
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9067717
88 X = 2728526
40
Y = 15742088
15 feet Y = 4828897
62 meter
Z = -12525109
08 Z = -3804312
57
XDOT = -21223
274708 XDOT = -6453
056213
YDOT = 1419
776867 feet/sec YDOT = 360
497411 meter/sec
ZDOT = -13612
848350 ZDOT = -4180
583767
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13934930
75 X = 4247366
89
Y = 11712582
90 feet Y = 3569995
27 meter
Z = -12471900
87 Z = -3801435
38
XDOT = -18556
662469 XDOT = -5656
070721
YDOT = 7484
090821 feet/sec YDOT = 2281
150882 meter/sec
ZDOT = -13737
582568 ZDOT = -4187
215167
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
52364249
00016717 00000-0 10270-3 0 9141
2 25544 51
6449 207
6485 0005083 169
8128 190
3140 15
74663860 13125
Satellite: ISS
Catalog Number: 25544
Epoch time: 10102
52364249 = yrday
fracday
Element set: 914
Inclination: 51
6449 deg
RA of node: 207
6485 deg
Eccentricity:
0005083
Arg of perigee: 169
8128 deg
Mean anomaly: 190
3140 deg
Mean motion: 15
74663860 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1312
Checksum: 300
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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