Date:
August 13th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16953 16 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
230/20:37:31
474 1
8 4
0 4
0
N/A -2
8 -0
0 191
7
000/00:10:58
948 2
3 0
3 191
1
Coasting Arc #1 (Orbit 3217)
---------------------------------------
Vector Time (GMT): 2010/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5255620
77 A = 6733195
05 meter
Y = -2311558
64 meter E =
0010346
Z = 3516029
13 I = 51
37874
XDOT = -245
284956 Wp = 126
74417
YDOT = 6260
472406 meter/sec RA = 306
96852 deg
ZDOT = 4467
312937 TA = 275
20242
MA = 275
32048
Ha = 193
715 n
mi
Hp = 188
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17242850
30 X = 5263998
56
Y = -7583853
79 feet Y = -2252740
29 meter
Z = 11535528
63 Z = 3541580
75
XDOT = -804
740668 XDOT = -336
973421
YDOT = 20539
607630 feet/sec YDOT = 6257
216826 meter/sec
ZDOT = 14656
538506 ZDOT = 4465
898658
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17943280
00 X = -5469111
74
Y = -5522823
23 feet Y = -1683356
52 meter
Z = 11637709
06 Z = 3547173
72
XDOT = 13728
037077 XDOT = 4184
305701
YDOT = -13625
099967 feet/sec YDOT = -4152
930470 meter/sec
ZDOT = 14650
865492 ZDOT = 4465
583802
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 10223
55612240
00016717 00000-0 10270-3 0 9000
2 25544 51
6472 307
2688 0006829 215
0506 145
0207 15
71729607 32183
Satellite: ISS
Catalog Number: 25544
Epoch time: 10223
55612240 = yrday
fracday
Element set: 900
Inclination: 51
6472 deg
RA of node: 307
2688 deg
Eccentricity:
0006829
Arg of perigee: 215
0506 deg
Mean anomaly: 145
0207 deg
Mean motion: 15
71729607 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3218
Checksum: 287
Coasting Arc #2 (Orbit 3232)
---------------------------------------
Vector Time (GMT): 2010/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -970607
93 A = 6730313
83 meter
Y = -5046066
89 meter E =
0009448
Z = -4355159
64 I = 51
35104
XDOT = 5642
125060 Wp = 152
71393
YDOT = -3995
203694 meter/sec RA = 301
78193 deg
ZDOT = 3366
199000 TA = 151
40499
MA = 151
35314
Ha = 193
516 n
mi
Hp = 188
415
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3184409
22 X = -892953
50
Y = -16555337
58 feet Y = -5056486
67 meter
Z = -14288581
51 Z = -4359686
11
XDOT = 18510
908988 XDOT = 5670
028688
YDOT = -13107
623668 feet/sec YDOT = -3931
954019 meter/sec
ZDOT = 11043
959975 ZDOT = 3393
675842
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8253725
10 X = -2515735
41
Y = 14682585
95 feet Y = 4475252
20 meter
Z = -14306673
88 Z = -4360674
20
XDOT = -21486
008789 XDOT = -6548
935479
YDOT = -1192
775169 feet/sec YDOT = -363
557872 meter/sec
ZDOT = 11153
835211 ZDOT = 3399
688972
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 10224
50984618
00016717 00000-0 10270-3 0 9018
2 25544 51
6463 302
3890 0006671 218
4759 141
5929 15
71764234 32330
Satellite: ISS
Catalog Number: 25544
Epoch time: 10224
50984618 = yrday
fracday
Element set: 901
Inclination: 51
6463 deg
RA of node: 302
3890 deg
Eccentricity:
0006671
Arg of perigee: 218
4759 deg
Mean anomaly: 141
5929 deg
Mean motion: 15
71764234 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3233
Checksum: 312
Coasting Arc #3 (Orbit 3248)
---------------------------------------
Vector Time (GMT): 2010/225/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4373381
62 A = 6736180
11 meter
Y = 4556084
99 meter E =
0008845
Z = -2327707
47 I = 51
35491
XDOT = -2322
240749 Wp = 182
65388
YDOT = -4979
980010 meter/sec RA = 296
68797 deg
ZDOT = -5392
224895 TA = 23
62826
MA = 23
58766
Ha = 193
263 n
mi
Hp = 188
649
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14348364
90 X = -4412696
09
Y = 14947785
39 feet Y = 4506959
38 meter
Z = -7636835
52 Z = -2349048
67
XDOT = -7618
900095 XDOT = -2240
186917
YDOT = -16338
517094 feet/sec YDOT = -5005
489949 meter/sec
ZDOT = -17691
026559 ZDOT = -5403
306882
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20520439
29 X = 6254629
89
Y = -2629213
56 feet Y = -801384
29 meter
Z = -7722171
17 Z = -2353717
77
XDOT = -4623
001984 XDOT = -1409
091005
YDOT = 15933
165622 feet/sec YDOT = 4856
428882 meter/sec
ZDOT = -17735
335728 ZDOT = -5405
730330
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 10225
52713554
00016717 00000-0 10270-3 0 9021
2 25544 51
6454 297
1826 0006623 222
9472 137
1174 15
71750822 32497
Satellite: ISS
Catalog Number: 25544
Epoch time: 10225
52713554 = yrday
fracday
Element set: 902
Inclination: 51
6454 deg
RA of node: 297
1826 deg
Eccentricity:
0006623
Arg of perigee: 222
9472 deg
Mean anomaly: 137
1174 deg
Mean motion: 15
71750822 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3249
Checksum: 302
Coasting Arc #4 (Orbit 3264)
---------------------------------------
Vector Time (GMT): 2010/226/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2931710
56 A = 6727541
84 meter
Y = 3441267
82 meter E =
0001172
Z = 4982104
62 I = 51
31440
XDOT = -4093
112673 Wp = 191
93033
YDOT = 6235
961271 meter/sec RA = 291
51131 deg
ZDOT = -1899
964546 TA = 276
49695
MA = 276
51030
Ha = 192
922 n
mi
Hp = 188
827
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9618472
95 X = 2868809
77
Y = 11290248
75 feet Y = 3473700
23 meter
Z = 16345487
60 Z = 4996194
01
XDOT = -13428
847351 XDOT = -4153
310498
YDOT = 20459
190523 feet/sec YDOT = 6189
853063 meter/sec
ZDOT = -6233
479483 ZDOT = -1919
994940
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -558009
49 X = -170081
29
Y = -14759013
76 feet Y = -4498547
39 meter
Z = 16401824
34 Z = 4999276
06
XDOT = 22069
007155 XDOT = 6726
633381
YDOT = -7846
314678 feet/sec YDOT = -2391
556714 meter/sec
ZDOT = -6313
570056 ZDOT = -1924
376153
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 10226
54440628
00016717 00000-0 10270-3 0 9034
2 25544 51
6459 291
9759 0006627 228
6626 131
3967 15
71818807 32659
Satellite: ISS
Catalog Number: 25544
Epoch time: 10226
54440628 = yrday
fracday
Element set: 903
Inclination: 51
6459 deg
RA of node: 291
9759 deg
Eccentricity:
0006627
Arg of perigee: 228
6626 deg
Mean anomaly: 131
3967 deg
Mean motion: 15
71818807 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3265
Checksum: 337
Coasting Arc #5 (Orbit 3280)
---------------------------------------
Vector Time (GMT): 2010/227/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2618514
05 A = 6738080
13 meter
Y = -6127241
34 meter E =
0007427
Z = 978137
13 I = 51
33876
XDOT = 4125
676151 Wp = 58
57521
YDOT = 2710
179049 meter/sec RA = 286
39527 deg
ZDOT = 5903
318159 TA = 312
14418
MA = 312
20726
Ha = 192
881 n
mi
Hp = 188
931
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8590925
36 X = 2682083
78
Y = -20102497
82 feet Y = -6097604
13 meter
Z = 3209111
32 Z = 991012
07
XDOT = 13535
682911 XDOT = 4066
386687
YDOT = 8891
663547 feet/sec YDOT = 2755
983181 meter/sec
ZDOT = 19367
841728 ZDOT = 5923
216650
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18941738
90 X = -5773442
02
Y = 10899169
75 feet Y = 3322066
94 meter
Z = 3260588
78 Z = 993827
46
XDOT = -4574
607121 XDOT = -1394
340250
YDOT = -13796
285631 feet/sec YDOT = -4205
107860 meter/sec
ZDOT = 19447
407956 ZDOT = 5927
569945
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 10227
56166509
00016717 00000-0 10270-3 0 9041
2 25544 51
6451 286
7691 0006297 232
3726 127
6865 15
71778085 32810
Satellite: ISS
Catalog Number: 25544
Epoch time: 10227
56166509 = yrday
fracday
Element set: 904
Inclination: 51
6451 deg
RA of node: 286
7691 deg
Eccentricity:
0006297
Arg of perigee: 232
3726 deg
Mean anomaly: 127
6865 deg
Mean motion: 15
71778085 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3281
Checksum: 335
Coasting Arc #6 (Orbit 3295)
---------------------------------------
Vector Time (GMT): 2010/228/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4049463
26 A = 6726382
01 meter
Y = -1190518
80 meter E =
0010555
Z = -5245784
77 I = 51
29212
XDOT = 1760
043077 Wp = 113
65266
YDOT = -7478
785295 meter/sec RA = 281
24052 deg
ZDOT = 334
994238 TA = 159
56848
MA = 159
52623
Ha = 192
606 n
mi
Hp = 188
915
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13285640
62 X = -4010366
76
Y = -3905901
58 feet Y = -1235583
51 meter
Z = -17210579
95 Z = -5265362
04
XDOT = 5774
419544 XDOT = 1841
914080
YDOT = -24536
697162 feet/sec YDOT = -7458
645688 meter/sec
ZDOT = 1099
062462 ZDOT = 343
743041
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8368634
02 X = 2550759
65
Y = 10910064
99 feet Y = 3325387
81 meter
Z = -17288864
13 Z = -5269645
79
XDOT = -18294
232712 XDOT = -5576
082131
YDOT = 15848
625134 feet/sec YDOT = 4830
660941 meter/sec
ZDOT = 1134
038238 ZDOT = 345
654855
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 10228
51532713
00016717 00000-0 10270-3 0 9052
2 25544 51
6450 281
8875 0006376 236
2742 123
7813 15
71812212 32965
Satellite: ISS
Catalog Number: 25544
Epoch time: 10228
51532713 = yrday
fracday
Element set: 905
Inclination: 51
6450 deg
RA of node: 281
8875 deg
Eccentricity:
0006376
Arg of perigee: 236
2742 deg
Mean anomaly: 123
7813 deg
Mean motion: 15
71812212 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3296
Checksum: 301
Coasting Arc #7 (Orbit 3311)
---------------------------------------
Vector Time (GMT): 2010/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -400612
13 A = 6738160
45 meter
Y = 6706798
32 meter E =
0012336
Z = 392354
20 I = 51
32821
XDOT = -4832
298310 Wp = 159
00100
YDOT = 64
809522 meter/sec RA = 276
09718 deg
ZDOT = -5995
027835 TA = 16
71675
MA = 16
67612
Ha = 192
300 n
mi
Hp = 189
043
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1314344
26 X = -477484
97
Y = 22003931
49 feet Y = 6701888
59 meter
Z = 1287251
32 Z = 390221
67
XDOT = -15853
997079 XDOT = -4803
541329
YDOT = 212
629666 feet/sec YDOT = 10
932977 meter/sec
ZDOT = -19668
726492 ZDOT = -6018
433113
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13709499
76 X = 4178655
53
Y = -17261864
64 feet Y = -5261416
34 meter
Z = 1278735
02 Z = 389758
43
XDOT = 11751
082266 XDOT = 3581
729875
YDOT = 7857
377281 feet/sec YDOT = 2394
928595 meter/sec
ZDOT = -19762
320971 ZDOT = -6023
555432
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 10229
53255165
00016717 00000-0 10270-3 0 9069
2 25544 51
6455 276
6808 0006174 240
5172 119
5375 15
71877713 33121
Satellite: ISS
Catalog Number: 25544
Epoch time: 10229
53255165 = yrday
fracday
Element set: 906
Inclination: 51
6455 deg
RA of node: 276
6808 deg
Eccentricity:
0006174
Arg of perigee: 240
5172 deg
Mean anomaly: 119
5375 deg
Mean motion: 15
71877713 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3312
Checksum: 314
Coasting Arc #8 (Orbit 3327)
---------------------------------------
Vector Time (GMT): 2010/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 828730
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4142408
36 A = 6726612
15 meter
Y = -1302918
41 meter E =
0005480
Z = 5139896
84 I = 51
28673
XDOT = 852
276591 Wp = 203
14536
YDOT = 7549
800225 meter/sec RA = 270
96870 deg
ZDOT = 1222
402154 TA = 235
08276
MA = 235
13426
Ha = 192
085 n
mi
Hp = 189
120
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13590578
62 X = 4131701
55
Y = -4274666
71 feet Y = -1256655
69 meter
Z = 16863178
61 Z = 5159994
36
XDOT = 2796
183042 XDOT = 761
851855
YDOT = 24769
685778 feet/sec YDOT = 7558
825229 meter/sec
ZDOT = 4010
505754 ZDOT = 1226
323271
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13571805
61 X = -4136686
35
Y = -4008201
03 feet Y = -1221699
67 meter
Z = 16943547
81 Z = 5164393
37
XDOT = 11273
211590 XDOT = 3436
074893
YDOT = -21089
031428 feet/sec YDOT = -6427
936779 meter/sec
ZDOT = 4026
206828 ZDOT = 1227
187841
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 10230
54976013
00016717 00000-0 10270-3 0 9075
2 25544 51
6448 271
4741 0006143 244
0371 116
0158 15
71892188 33289
Satellite: ISS
Catalog Number: 25544
Epoch time: 10230
54976013 = yrday
fracday
Element set: 907
Inclination: 51
6448 deg
RA of node: 271
4741 deg
Eccentricity:
0006143
Arg of perigee: 244
0371 deg
Mean anomaly: 116
0158 deg
Mean motion: 15
71892188 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3328
Checksum: 298
Coasting Arc #9 (Orbit 3332)
---------------------------------------
Vector Time (GMT): 2010/230/20:43:00
948
Vector Time (MET): N/A
Weight (LBS) : 828329
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1880010
10 A = 6738235
45 meter
Y = -6071942
71 meter E =
0005810
Z = -2224928
33 I = 51
31930
XDOT = 4303
833546 Wp = 318
51208
YDOT = -3328
249338 meter/sec RA = 269
07060 deg
ZDOT = 5442
497687 TA = 16
45022
MA = 16
43138
Ha = 191
667 n
mi
Hp = 191
116
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6168012
14 X = -1801164
63
Y = -19921071
87 feet Y = -6092525
12 meter
Z = -7299633
63 Z = -2233870
15
XDOT = 14120
188798 XDOT = 4314
292425
YDOT = -10919
453209 feet/sec YDOT = -3280
063135 meter/sec
ZDOT = 17855
963539 ZDOT = 5463
430663
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19014700
59 X = 5795680
74
Y = -8532936
79 feet Y = -2600839
13 meter
Z = -7335412
78 Z = -2235833
81
XDOT = 11940
427353 XDOT = 3639
442257
YDOT = 11175
173419 feet/sec YDOT = 3406
192858 meter/sec
ZDOT = 17939
669168 ZDOT = 5468
011162
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 10230
86763468
00016717 00000-0 10270-3 0 9089
2 25544 51
6458 269
8473 0007975 269
6940 90
3308 15
71113381 33330
Satellite: ISS
Catalog Number: 25544
Epoch time: 10230
86763468 = yrday
fracday
Element set: 908
Inclination: 51
6458 deg
RA of node: 269
8473 deg
Eccentricity:
0007975
Arg of perigee: 269
6940 deg
Mean anomaly: 90
3308 deg
Mean motion: 15
71113381 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3333
Checksum: 333
Coasting Arc #10 (Orbit 3348)
---------------------------------------
Vector Time (GMT): 2010/231/20:43:00
948
Vector Time (MET): N/A
Weight (LBS) : 828329
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3015310
35 A = 6732244
58 meter
Y = 4218963
65 meter E =
0003687
Z = -4295638
28 I = 51
30155
XDOT = -3414
269417 Wp = 4
07210
YDOT = -5963
972154 meter/sec RA = 263
97828 deg
ZDOT = -3457
438337 TA = 230
75108
MA = 230
78381
Ha = 192
106 n
mi
Hp = 191
302
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9892750
50 X = -3041396
38
Y = 13841744
27 feet Y = 4185099
02 meter
Z = -14093301
45 Z = -4310349
56
XDOT = -11201
671316 XDOT = -3330
530093
YDOT = -19566
837774 feet/sec YDOT = -6001
684162 meter/sec
ZDOT = -11343
301630 ZDOT = -3473
821508
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15080482
89 X = -4596531
18
Y = -7770331
48 feet Y = -2368397
04 meter
Z = -14152120
95 Z = -4313566
47
XDOT = 17245
111477 XDOT = 5256
309978
YDOT = -12669
457153 feet/sec YDOT = -3861
650540 meter/sec
ZDOT = -11408
853241 ZDOT = -3477
418468
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 10231
88533172
00016717 00000-0 10270-3 0 9090
2 25544 51
6462 264
6441 0007965 274
3337 85
6915 15
71148079 33495
Satellite: ISS
Catalog Number: 25544
Epoch time: 10231
88533172 = yrday
fracday
Element set: 909
Inclination: 51
6462 deg
RA of node: 264
6441 deg
Eccentricity:
0007965
Arg of perigee: 274
3337 deg
Mean anomaly: 85
6915 deg
Mean motion: 15
71148079 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3349
Checksum: 329
Coasting Arc #11 (Orbit 3364)
---------------------------------------
Vector Time (GMT): 2010/232/20:43:00
948
Vector Time (MET): N/A
Weight (LBS) : 828329
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3851234
21 A = 6734193
90 meter
Y = 4075624
62 meter E =
0004473
Z = 3728086
67 I = 51
31180
XDOT = -2262
732838 Wp = 56
19264
YDOT = 6014
514807 meter/sec RA = 258
79080 deg
ZDOT = -4231
626869 TA = 78
62898
MA = 78
57873
Ha = 192
577 n
mi
Hp = 191
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12635282
84 X = 3787263
57
Y = 13371471
84 feet Y = 4118333
59 meter
Z = 12231255
48 Z = 3746640
39
XDOT = -7423
664166 XDOT = -2309
263990
YDOT = 19732
660128 feet/sec YDOT = 5988
951575 meter/sec
ZDOT = -13883
290253 ZDOT = -4242
731794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11229365
01 X = -3422710
46
Y = 14509530
21 feet Y = 4422504
81 meter
Z = 12305492
14 Z = 3750714
00
XDOT = -19583
276733 XDOT = -5968
982748
YDOT = -3327
217992 feet/sec YDOT = -1014
136044 meter/sec
ZDOT = -13927
671313 ZDOT = -4245
154216
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 10232
90301390
00016717 00000-0 10270-3 0 9101
2 25544 51
6454 259
4406 0007930 278
2896 81
7366 15
71153962 33656
Satellite: ISS
Catalog Number: 25544
Epoch time: 10232
90301390 = yrday
fracday
Element set: 910
Inclination: 51
6454 deg
RA of node: 259
4406 deg
Eccentricity:
0007930
Arg of perigee: 278
2896 deg
Mean anomaly: 81
7366 deg
Mean motion: 15
71153962 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3365
Checksum: 311
Coasting Arc #12 (Orbit 3380)
---------------------------------------
Vector Time (GMT): 2010/233/20:43:00
948
Vector Time (MET): N/A
Weight (LBS) : 828329
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 755848
94 A = 6736334
40 meter
Y = -5978385
50 meter E =
0006259
Z = 3002333
06 I = 51
32630
XDOT = 5022
552236 Wp = 59
04999
YDOT = 3113
729598 meter/sec RA = 253
70354 deg
ZDOT = 4931
328185 TA = 335
78406
MA = 335
81347
Ha = 192
806 n
mi
Hp = 191
426
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2479819
37 X = 808059
68
Y = -19614125
66 feet Y = -5969641
29 meter
Z = 9850174
09 Z = 3006131
59
XDOT = 16478
189752 XDOT = 4963
405654
YDOT = 10215
648289 feet/sec YDOT = 3169
563970 meter/sec
ZDOT = 16178
898244 ZDOT = 4955
583639
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19735667
66 X = 6015431
50
Y = -1033547
59 feet Y = -315025
30 meter
Z = 9865321
12 Z = 3006949
88
XDOT = -7280
496547 XDOT = -2219
095347
YDOT = 16472
485725 feet/sec YDOT = 5020
813649 meter/sec
ZDOT = 16275
947353 ZDOT = 4960
908753
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 10233
92067956
00016717 00000-0 10270-3 0 9112
2 25544 51
6456 254
2361 0007975 282
7962 77
2308 15
71166699 33819
Satellite: ISS
Catalog Number: 25544
Epoch time: 10233
92067956 = yrday
fracday
Element set: 911
Inclination: 51
6456 deg
RA of node: 254
2361 deg
Eccentricity:
0007975
Arg of perigee: 282
7962 deg
Mean anomaly: 77
2308 deg
Mean motion: 15
71166699 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3381
Checksum: 335
Coasting Arc #13 (Orbit 3395)
---------------------------------------
Vector Time (GMT): 2010/234/20:43:00
948
Vector Time (MET): N/A
Weight (LBS) : 828329
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4590329
07 A = 6730165
71 meter
Y = -1246886
00 meter E =
0003588
Z = -4764637
01 I = 51
31562
XDOT = -665
420502 Wp = 112
53532
YDOT = -7233
180546 meter/sec RA = 248
52267 deg
ZDOT = 2534
135740 TA = 182
42399
MA = 182
42573
Ha = 192
892 n
mi
Hp = 191
133
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15060134
73 X = -4552899
74
Y = -4090833
34 feet Y = -1298008
52 meter
Z = -15632011
18 Z = -4786845
44
XDOT = -2183
138129 XDOT = -596
798410
YDOT = -23730
907302 feet/sec YDOT = -7240
237995 meter/sec
ZDOT = 8314
093635 ZDOT = 2531
069860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1154555
30 X = 351908
46
Y = -15473323
91 feet Y = -4716269
13 meter
Z = -15720865
06 Z = -4791719
67
XDOT = 21737
869240 XDOT = 6625
702544
YDOT = -6812
032021 feet/sec YDOT = -2076
307360 meter/sec
ZDOT = 8301
757762 ZDOT = 2530
375766
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 10234
87472538
00016717 00000-0 10270-3 0 9124
2 25544 51
6455 249
3574 0008119 286
1427 73
8841 15
71214378 33962
Satellite: ISS
Catalog Number: 25544
Epoch time: 10234
87472538 = yrday
fracday
Element set: 912
Inclination: 51
6455 deg
RA of node: 249
3574 deg
Eccentricity:
0008119
Arg of perigee: 286
1427 deg
Mean anomaly: 73
8841 deg
Mean motion: 15
71214378 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3396
Checksum: 330
Coasting Arc #14 (Orbit 3411)
---------------------------------------
Vector Time (GMT): 2010/235/20:43:00
948
Vector Time (MET): N/A
Weight (LBS) : 828329
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1922453
53 A = 6739356
61 meter
Y = 6306890
41 meter E =
0004953
Z = -1379343
46 I = 51
35837
XDOT = -5049
422251 Wp = 209
21202
YDOT = 269
824348 meter/sec RA = 243
41975 deg
ZDOT = -5799
363115 TA = 345
98654
MA = 346
00028
Ha = 193
223 n
mi
Hp = 191
159
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6307262
24 X = 1858486
31
Y = 20691897
67 feet Y = 6328030
75 meter
Z = -4525405
05 Z = -1370159
85
XDOT = -16566
345968 XDOT = -5023
892485
YDOT = 885
250484 feet/sec YDOT = 213
501326 meter/sec
ZDOT = -19026
781872 ZDOT = -5823
830721
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18921437
79 X = -5767254
24
Y = 10499867
35 feet Y = 3200359
57 meter
Z = -4488591
59 Z = -1368122
72
XDOT = -3522
377588 XDOT = -1073
620689
YDOT = -14529
529290 feet/sec YDOT = -4428
600528 meter/sec
ZDOT = -19124
662824 ZDOT = -5829
197229
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 10235
89236007
00016717 00000-0 10270-3 0 9137
2 25544 51
6454 244
1534 0008132 288
9134 71
1146 15
71195587 34128
Satellite: ISS
Catalog Number: 25544
Epoch time: 10235
89236007 = yrday
fracday
Element set: 913
Inclination: 51
6454 deg
RA of node: 244
1534 deg
Eccentricity:
0008132
Arg of perigee: 288
9134 deg
Mean anomaly: 71
1146 deg
Mean motion: 15
71195587 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3412
Checksum: 299
Coasting Arc #15 (Orbit 3427)
---------------------------------------
Vector Time (GMT): 2010/236/20:43:00
948
Vector Time (MET): N/A
Weight (LBS) : 828329
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3902845
01 A = 6727986
15 meter
Y = -1647348
83 meter E =
0006586
Z = 5231404
92 I = 51
33547
XDOT = 3633
342442 Wp = 312
32963
YDOT = 6756
184583 meter/sec RA = 238
26587 deg
ZDOT = -579
223251 TA = 143
22643
MA = 143
18123
Ha = 193
300 n
mi
Hp = 190
789
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12804609
62 X = 3895563
11
Y = -5404687
75 feet Y = -1603745
41 meter
Z = 17163401
98 Z = 5250347
00
XDOT = 11920
414835 XDOT = 3560
337223
YDOT = 22165
959919 feet/sec YDOT = 6796
406582 meter/sec
ZDOT = -1900
338750 ZDOT = -561
750330
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8121641
97 X = 2475476
47
Y = 11162493
53 feet Y = 3402328
03 meter
Z = 17239162
24 Z = 5254496
65
XDOT = -18102
011157 XDOT = -5517
493001
YDOT = 16017
167680 feet/sec YDOT = 4882
032709 meter/sec
ZDOT = -1830
343506 ZDOT = -557
888701
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 10236
90997633
00016717 00000-0 10270-3 0 9140
2 25544 51
6453 238
9485 0008164 293
9629 66
0678 15
71272896 34282
Satellite: ISS
Catalog Number: 25544
Epoch time: 10236
90997633 = yrday
fracday
Element set: 914
Inclination: 51
6453 deg
RA of node: 238
9485 deg
Eccentricity:
0008164
Arg of perigee: 293
9629 deg
Mean anomaly: 66
0678 deg
Mean motion: 15
71272896 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3428
Checksum: 356
Coasting Arc #16 (Orbit 3442)
---------------------------------------
Vector Time (GMT): 2010/237/20:43:00
948
Vector Time (MET): N/A
Weight (LBS) : 828329
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4268648
17 A = 6739824
38 meter
Y = -5191480
62 meter E =
0012296
Z = -375979
04 I = 51
39199
XDOT = 3504
320686 Wp = 1
82372
YDOT = -3314
773245 meter/sec RA = 233
13177 deg
ZDOT = 6001
496113 TA = 354
07757
MA = 354
09209
Ha = 193
496 n
mi
Hp = 190
570
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14004751
21 X = -4208452
41
Y = -17032416
73 feet Y = -5238878
65 meter
Z = -1233527
05 Z = -396569
41
XDOT = 11497
115111 XDOT = 3511
972831
YDOT = -10875
240305 feet/sec YDOT = -3275
542760 meter/sec
ZDOT = 19689
947878 ZDOT = 6018
538626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13147078
98 X = 4007229
67
Y = -17696902
70 feet Y = -5394015
94 meter
Z = -1315984
20 Z = -401111
98
XDOT = 12011
021578 XDOT = 3660
959377
YDOT = 7457
758020 feet/sec YDOT = 2273
124645 meter/sec
ZDOT = 19758
083970 ZDOT = 6022
263994
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 10237
86397768
00016717 00000-0 10270-3 0 9150
2 25544 51
6449 234
0687 0008224 297
7862 62
2466 15
71292329 34439
Satellite: ISS
Catalog Number: 25544
Epoch time: 10237
86397768 = yrday
fracday
Element set: 915
Inclination: 51
6449 deg
RA of node: 234
0687 deg
Eccentricity:
0008224
Arg of perigee: 297
7862 deg
Mean anomaly: 62
2466 deg
Mean motion: 15
71292329 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3443
Checksum: 343
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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