Date:
April 10th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21527 82 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
102/11:47:15
071 -0
2 0
8 0
8
N/A 0
5 -0
0 190
5
000/00:00:30
143 -0
6 -0
0 182
3
Coasting Arc #1 (Orbit 1266)
---------------------------------------
Vector Time (GMT): 2010/099/13:43:10
815
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5193584
97 A = 6730601
79 meter
Y = 4249355
30 meter E =
0017746
Z = 377235
52 I = 51
43977
XDOT = -2778
874927 Wp = 138
84179
YDOT = 3942
915127 meter/sec RA = 221
85824 deg
ZDOT = -6010
121625 TA = 37
04207
MA = 36
91970
Ha = 190
527 n
mi
Hp = 182
051
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17039320
78 X = 5143849
39
Y = 13941454
40 feet Y = 4307155
00 meter
Z = 1237649
34 Z = 402344
75
XDOT = -9117
043723 XDOT = -2793
562813
YDOT = 12936
073251 feet/sec YDOT = 3911
757568 meter/sec
ZDOT = -19718
246800 ZDOT = -6023
657281
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21971034
07 X = 6696771
19
Y = -1311067
79 feet Y = -399613
46 meter
Z = 1337588
25 Z = 407696
90
XDOT = 2066
671387 XDOT = 629
921439
YDOT = 14007
735264 feet/sec YDOT = 4269
557708 meter/sec
ZDOT = -19771
891212 ZDOT = -6026
472442
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
60421431
00016717 00000-0 10270-3 0 9007
2 25544 51
6463 222
6654 0005184 158
5133 201
6249 15
74530156 12675
Satellite: ISS
Catalog Number: 25544
Epoch time: 10099
60421431 = yrday
fracday
Element set: 900
Inclination: 51
6463 deg
RA of node: 222
6654 deg
Eccentricity:
0005184
Arg of perigee: 158
5133 deg
Mean anomaly: 201
6249 deg
Mean motion: 15
74530156 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1267
Checksum: 286
Coasting Arc #2 (Orbit 1282)
---------------------------------------
Vector Time (GMT): 2010/100/13:43:10
815
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2313396
26 A = 6718325
56 meter
Y = -3495581
59 meter E =
0006537
Z = 5247075
64 I = 51
42340
XDOT = 6272
538446 Wp = 143
78081
YDOT = 4470
598294 meter/sec RA = 216
70935 deg
ZDOT = 207
450749 TA = 304
21469
MA = 304
27662
Ha = 190
197 n
mi
Hp = 182
081
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7589882
73 X = 2326823
21
Y = -11468443
52 feet Y = -3469636
34 meter
Z = 17214815
08 Z = 5258346
99
XDOT = 20579
194377 XDOT = 6221
073467
YDOT = 14667
317237 feet/sec YDOT = 4540
453812 meter/sec
ZDOT = 680
612693 ZDOT = 237
797359
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2509858
83 X = -765004
97
Y = -13464487
84 feet Y = -4103975
89 meter
Z = 17259477
13 Z = 5260688
63
XDOT = 24026
303105 XDOT = 7323
217186
YDOT = -3429
032303 feet/sec YDOT = -1045
169046 meter/sec
ZDOT = 801
383462 ZDOT = 244
261679
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
61967811
00016717 00000-0 10270-3 0 9019
2 25544 51
6470 217
4464 0004975 162
8011 197
3322 15
74625794 12838
Satellite: ISS
Catalog Number: 25544
Epoch time: 10100
61967811 = yrday
fracday
Element set: 901
Inclination: 51
6470 deg
RA of node: 217
4464 deg
Eccentricity:
0004975
Arg of perigee: 162
8011 deg
Mean anomaly: 197
3322 deg
Mean motion: 15
74625794 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1283
Checksum: 301
Coasting Arc #3 (Orbit 1298)
---------------------------------------
Vector Time (GMT): 2010/101/13:43:10
815
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5717661
18 A = 6730426
40 meter
Y = -3545295
52 meter E =
0010779
Z = 36339
93 I = 51
48906
XDOT = 2560
433375 Wp = 68
46986
YDOT = -4052
977856 meter/sec RA = 211
55514 deg
ZDOT = 6024
039185 TA = 291
92566
MA = 292
04021
Ha = 190
171 n
mi
Hp = 182
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18758730
90 X = -5677768
63
Y = -11631546
99 feet Y = -3609010
76 meter
Z = 119225
50 Z = 8660
63
XDOT = 8400
371966 XDOT = 2576
300409
YDOT = -13297
171444 feet/sec YDOT = -4024
256360 meter/sec
ZDOT = 19763
908087 ZDOT = 6036
516680
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21516519
39 X = -6558235
11
Y = 4923047
44 feet Y = 1500544
86 meter
Z = 9082
26 Z = 2768
27
XDOT = -3102
582082 XDOT = -945
667019
YDOT = -13709
800523 feet/sec YDOT = -4178
747199 meter/sec
ZDOT = 19813
342417 ZDOT = 6039
106769
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
63511531
00016717 00000-0 10270-3 0 9027
2 25544 51
6470 212
2281 0004777 164
8521 195
2786 15
74615143 12991
Satellite: ISS
Catalog Number: 25544
Epoch time: 10101
63511531 = yrday
fracday
Element set: 902
Inclination: 51
6470 deg
RA of node: 212
2281 deg
Eccentricity:
0004777
Arg of perigee: 164
8521 deg
Mean anomaly: 195
2786 deg
Mean motion: 15
74615143 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1299
Checksum: 292
Coasting Arc #4 (Orbit 1312)
---------------------------------------
Vector Time (GMT): 2010/102/11:47:30
143
Vector Time (MET): N/A
Weight (LBS) : 797508
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6073831
49 A = 6730671
63 meter
Y = 2868338
09 meter E =
0017551
Z = 226186
76 I = 51
51294
XDOT = -1858
938406 Wp = 143
64079
YDOT = 4429
271322 meter/sec RA = 206
81295 deg
ZDOT = -6026
636658 TA = 33
89500
MA = 33
78296
Ha = 190
460 n
mi
Hp = 182
310
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19927268
67 X = 6040207
01
Y = 9410558
04 feet Y = 2936071
30 meter
Z = 742082
54 Z = 255611
75
XDOT = -6098
879285 XDOT = -1879
052614
YDOT = 14531
730059 feet/sec YDOT = 4408
370620 meter/sec
ZDOT = -19772
429979 ZDOT = -6035
716660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21785091
20 X = 6640095
80
Y = 3298029
60 feet Y = 1005239
42 meter
Z = 859143
80 Z = 261867
03
XDOT = -1320
546178 XDOT = -402
502475
YDOT = 14048
189820 feet/sec YDOT = 4281
888257 meter/sec
ZDOT = -19808
347611 ZDOT = -6037
584352
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
52359934
00016717 00000-0 10270-3 0 9034
2 25544 51
6468 207
6597 0005600 169
2884 190
8400 15
74520577 13130
Satellite: ISS
Catalog Number: 25544
Epoch time: 10102
52359934 = yrday
fracday
Element set: 903
Inclination: 51
6468 deg
RA of node: 207
6597 deg
Eccentricity:
0005600
Arg of perigee: 169
2884 deg
Mean anomaly: 190
8400 deg
Mean motion: 15
74520577 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1313
Checksum: 308
Coasting Arc #5 (Orbit 1328)
---------------------------------------
Vector Time (GMT): 2010/103/11:47:30
143
Vector Time (MET): N/A
Weight (LBS) : 797508
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1498666
87 A = 6718349
60 meter
Y = -3903359
04 meter E =
0006294
Z = 5256196
06 I = 51
50049
XDOT = 7172
084242 Wp = 151
91458
YDOT = 2815
044153 meter/sec RA = 201
66716 deg
ZDOT = 40
091239 TA = 297
67255
MA = 297
73641
Ha = 190
151 n
mi
Hp = 182
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4916886
04 X = 1516669
58
Y = -12806296
07 feet Y = -3886499
02 meter
Z = 17244737
72 Z = 5263520
67
XDOT = 23530
460111 XDOT = 7139
878106
YDOT = 9235
709165 feet/sec YDOT = 2895
066597 meter/sec
ZDOT = 131
532936 ZDOT = 74
855210
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 703206
91 X = 214337
47
Y = -13663188
62 feet Y = -4164539
89 meter
Z = 17273700
90 Z = 5265024
04
XDOT = 24225
941861 XDOT = 7384
067079
YDOT = 1610
678847 feet/sec YDOT = 490
934913 meter/sec
ZDOT = 269
819136 ZDOT = 82
240873
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
53907358
00016717 00000-0 10270-3 0 9046
2 25544 51
6474 202
4413 0005395 173
4856 186
6379 15
74611207 13290
Satellite: ISS
Catalog Number: 25544
Epoch time: 10103
53907358 = yrday
fracday
Element set: 904
Inclination: 51
6474 deg
RA of node: 202
4413 deg
Eccentricity:
0005395
Arg of perigee: 173
4856 deg
Mean anomaly: 186
6379 deg
Mean motion: 15
74611207 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1329
Checksum: 310
Coasting Arc #6 (Orbit 1344)
---------------------------------------
Vector Time (GMT): 2010/104/11:47:30
143
Vector Time (MET): N/A
Weight (LBS) : 797508
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6406504
68 A = 6730437
00 meter
Y = -2047200
22 meter E =
0010082
Z = 177466
00 I = 51
56971
XDOT = 1615
410125 Wp = 70
82890
YDOT = -4508
999517 meter/sec RA = 196
52164 deg
ZDOT = 6027
111648 TA = 291
10071
MA = 291
20846
Ha = 190
081 n
mi
Hp = 182
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21018716
16 X = -6383998
49
Y = -6716536
14 feet Y = -2118715
72 meter
Z = 582237
52 Z = 146397
49
XDOT = 5299
901985 XDOT = 1636
431425
YDOT = -14793
305501 feet/sec YDOT = -4490
817172 meter/sec
ZDOT = 19773
988347 ZDOT = 6035
010741
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -22065792
56 X = -6725653
57
Y = 357371
85 feet Y = 108926
94 meter
Z = 458662
60 Z = 139800
36
XDOT = 207
644772 XDOT = 63
290127
YDOT = -14064
542933 feet/sec YDOT = -4286
872686 meter/sec
ZDOT = 19805
215672 ZDOT = 6036
629737
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
55452105
00016717 00000-0 10270-3 0 9055
2 25544 51
6474 197
2232 0005242 176
0226 184
0980 15
74608381 13458
Satellite: ISS
Catalog Number: 25544
Epoch time: 10104
55452105 = yrday
fracday
Element set: 905
Inclination: 51
6474 deg
RA of node: 197
2232 deg
Eccentricity:
0005242
Arg of perigee: 176
0226 deg
Mean anomaly: 184
0980 deg
Mean motion: 15
74608381 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1345
Checksum: 287
Coasting Arc #7 (Orbit 1359)
---------------------------------------
Vector Time (GMT): 2010/105/11:47:30
143
Vector Time (MET): N/A
Weight (LBS) : 797508
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1355172
58 A = 6718278
51 meter
Y = 3980557
56 meter E =
0016082
Z = -5252822
91 I = 51
55797
XDOT = -7439
821860 Wp = 112
56057
YDOT = -1887
984004 meter/sec RA = 191
37131 deg
ZDOT = 483
808365 TA = 162
07458
MA = 162
01780
Ha = 189
856 n
mi
Hp = 182
485
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4446104
27 X = -1374065
45
Y = 13059572
04 feet Y = 3965297
40 meter
Z = -17233670
97 Z = -5259452
48
XDOT = -24408
864370 XDOT = -7420
507430
YDOT = -6194
173243 feet/sec YDOT = -1971
072511 meter/sec
ZDOT = 1587
297787 ZDOT = 447
712049
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 295631
82 X = 90108
58
Y = 13759684
56 feet Y = 4193951
85 meter
Z = -17259877
25 Z = -5260810
59
XDOT = -24076
084877 XDOT = -7338
390671
YDOT = 2348
343028 feet/sec YDOT = 715
774955 meter/sec
ZDOT = 1443
733668 ZDOT = 440
050022
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
50647385
00016717 00000-0 10270-3 0 9068
2 25544 51
6468 192
3312 0005166 180
4962 179
6197 15
74662435 13604
Satellite: ISS
Catalog Number: 25544
Epoch time: 10105
50647385 = yrday
fracday
Element set: 906
Inclination: 51
6468 deg
RA of node: 192
3312 deg
Eccentricity:
0005166
Arg of perigee: 180
4962 deg
Mean anomaly: 179
6197 deg
Mean motion: 15
74662435 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1360
Checksum: 316
Coasting Arc #8 (Orbit 1375)
---------------------------------------
Vector Time (GMT): 2010/106/11:47:30
143
Vector Time (MET): N/A
Weight (LBS) : 797508
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6568094
82 A = 6730019
01 meter
Y = 1257443
04 meter E =
0015010
Z = -677247
14 I = 51
62664
XDOT = -1493
727032 Wp = 153
95137
YDOT = 4609
307390 meter/sec RA = 186
23843 deg
ZDOT = -5991
575503 TA = 33
43268
MA = 33
33801
Ha = 189
780 n
mi
Hp = 182
572
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21548867
52 X = 6556835
71
Y = 4125469
28 feet Y = 1330828
42 meter
Z = -2221939
43 Z = -645366
12
XDOT = -4900
679239 XDOT = -1516
051602
YDOT = 15122
399574 feet/sec YDOT = 4592
478775 meter/sec
ZDOT = -19657
399945 ZDOT = -5998
886423
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21633243
90 X = 6593812
74
Y = -3731397
69 feet Y = -1137330
02 meter
Z = -2095144
92 Z = -638600
17
XDOT = 574
451236 XDOT = 175
092737
YDOT = 14260
724017 feet/sec YDOT = 4346
668680 meter/sec
ZDOT = -19686
298439 ZDOT = -6000
383764
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
52186302
00016717 00000-0 10270-3 0 9079
2 25544 51
6458 187
1125 0005185 183
4129 176
7000 15
74697024 13766
Satellite: ISS
Catalog Number: 25544
Epoch time: 10106
52186302 = yrday
fracday
Element set: 907
Inclination: 51
6458 deg
RA of node: 187
1125 deg
Eccentricity:
0005185
Arg of perigee: 183
4129 deg
Mean anomaly: 176
7000 deg
Mean motion: 15
74697024 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1376
Checksum: 299
Coasting Arc #9 (Orbit 1391)
---------------------------------------
Vector Time (GMT): 2010/107/11:47:30
143
Vector Time (MET): N/A
Weight (LBS) : 797508
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1256292
89 A = 6718181
60 meter
Y = -4082431
48 meter E =
0003753
Z = 5183125
14 I = 51
61826
XDOT = 7567
591566 Wp = 143
41000
YDOT = 983
967661 meter/sec RA = 181
08101 deg
ZDOT = -1061
800927 TA = 316
70062
MA = 316
73011
Ha = 189
416 n
mi
Hp = 182
632
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4121695
83 X = 1276670
91
Y = -13393804
07 feet Y = -4068269
00 meter
Z = 17005003
75 Z = 5189277
75
XDOT = 24828
056320 XDOT = 7561
184338
YDOT = 3228
240356 feet/sec YDOT = 1068
557162 meter/sec
ZDOT = -3483
598841 ZDOT = -1025
052525
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1192184
99 X = -363377
98
Y = -13933175
08 feet Y = -4246831
76 meter
Z = 17029323
05 Z = 5190537
67
XDOT = 23275
171142 XDOT = 7094
272164
YDOT = -6060
316040 feet/sec YDOT = -1847
184329 meter/sec
ZDOT = -3337
447326 ZDOT = -1017
253945
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
53722042
00016717 00000-0 10270-3 0 9089
2 25544 51
6461 181
8928 0005032 189
1199 170
9874 15
74789224 13920
Satellite: ISS
Catalog Number: 25544
Epoch time: 10107
53722042 = yrday
fracday
Element set: 908
Inclination: 51
6461 deg
RA of node: 181
8928 deg
Eccentricity:
0005032
Arg of perigee: 189
1199 deg
Mean anomaly: 170
9874 deg
Mean motion: 15
74789224 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1392
Checksum: 323
Coasting Arc #10 (Orbit 1407)
---------------------------------------
Vector Time (GMT): 2010/108/11:47:30
143
Vector Time (MET): N/A
Weight (LBS) : 797508
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6602073
36 A = 6729378
03 meter
Y = -478712
56 meter E =
0011126
Z = 1192807
04 I = 51
68520
XDOT = 1416
070174 Wp = 76
45955
YDOT = -4760
886563 meter/sec RA = 175
96119 deg
ZDOT = 5883
942787 TA = 296
60356
MA = 296
71751
Ha = 189
356 n
mi
Hp = 182
758
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21660345
67 X = -6602024
14
Y = -1570579
26 feet Y = -552540
63 meter
Z = 3913408
92 Z = 1160733
87
XDOT = 4645
899520 XDOT = 1440
618529
YDOT = -15619
706571 feet/sec YDOT = -4744
914151 meter/sec
ZDOT = 19304
274236 ZDOT = 5890
881621
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20622808
11 X = -6285831
91
Y = 6878895
21 feet Y = 2096687
26 meter
Z = 3785848
60 Z = 1153926
65
XDOT = -1313
576811 XDOT = -400
378212
YDOT = -14657
997244 feet/sec YDOT = -4467
757560 meter/sec
ZDOT = 19331
703057 ZDOT = 5892
303092
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
55255242
00016717 00000-0 10270-3 0 9096
2 25544 51
6453 176
6735 0004838 191
0532 169
0526 15
74781028 14080
Satellite: ISS
Catalog Number: 25544
Epoch time: 10108
55255242 = yrday
fracday
Element set: 909
Inclination: 51
6453 deg
RA of node: 176
6735 deg
Eccentricity:
0004838
Arg of perigee: 191
0532 deg
Mean anomaly: 169
0526 deg
Mean motion: 15
74781028 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1408
Checksum: 310
Coasting Arc #11 (Orbit 1422)
---------------------------------------
Vector Time (GMT): 2010/109/11:47:30
143
Vector Time (MET): N/A
Weight (LBS) : 797508
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1232179
56 A = 6718642
24 meter
Y = 4254309
31 meter E =
0014205
Z = -5064194
69 I = 51
67883
XDOT = -7500
540265 Wp = 122
40466
YDOT = -145
167489 meter/sec RA = 170
79753 deg
ZDOT = 1699
006110 TA = 163
97000
MA = 163
92500
Ha = 189
124 n
mi
Hp = 182
742
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4042583
86 X = -1255059
30
Y = 13957707
70 feet Y = 4240402
61 meter
Z = -16614811
97 Z = -5070236
08
XDOT = -24608
071735 XDOT = -7506
613044
YDOT = -476
271289 feet/sec YDOT = -229
077011 meter/sec
ZDOT = 5574
167027 ZDOT = 1662
553446
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1966694
35 X = 599448
44
Y = 14370038
25 feet Y = 4379987
66 meter
Z = -16638695
25 Z = -5071474
31
XDOT = -21726
493164 XDOT = -6622
235116
YDOT = 9275
040665 feet/sec YDOT = 2827
032395 meter/sec
ZDOT = 5429
182709 ZDOT = 1654
814890
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
50439753
00016717 00000-0 10270-3 0 9105
2 25544 51
6444 171
7799 0004739 195
3723 164
7297 15
74831312 14231
Satellite: ISS
Catalog Number: 25544
Epoch time: 10109
50439753 = yrday
fracday
Element set: 910
Inclination: 51
6444 deg
RA of node: 171
7799 deg
Eccentricity:
0004739
Arg of perigee: 195
3723 deg
Mean anomaly: 164
7297 deg
Mean motion: 15
74831312 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1423
Checksum: 320
Coasting Arc #12 (Orbit 1438)
---------------------------------------
Vector Time (GMT): 2010/110/11:47:30
143
Vector Time (MET): N/A
Weight (LBS) : 797508
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6478196
61 A = 6728320
05 meter
Y = -200210
44 meter E =
0010894
Z = -1784369
65 I = 51
74179
XDOT = -1408
951843 Wp = 163
17002
YDOT = 4993
523310 meter/sec RA = 165
69097 deg
ZDOT = -5694
346597 TA = 36
58722
MA = 36
51286
Ha = 189
032 n
mi
Hp = 182
788
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21253925
90 X = 6488622
10
Y = -656858
39 feet Y = -127709
04 meter
Z = -5854231
12 Z = -1752873
15
XDOT = -4622
545417 XDOT = -1437
023408
YDOT = 16382
950491 feet/sec YDOT = 4977
610806 meter/sec
ZDOT = -18682
239491 ZDOT = -5701
259326
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19088882
26 X = 5818291
31
Y = -9445979
10 feet Y = -2879134
43 meter
Z = -5728953
13 Z = -1746184
91
XDOT = 2016
409691 XDOT = 614
601674
YDOT = 15383
859471 feet/sec YDOT = 4689
000367 meter/sec
ZDOT = -18709
568217 ZDOT = -5702
676392
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
51967231
00016717 00000-0 10270-3 0 9116
2 25544 51
6447 166
5597 0004654 197
7811 162
3191 15
74888570 14394
Satellite: ISS
Catalog Number: 25544
Epoch time: 10110
51967231 = yrday
fracday
Element set: 911
Inclination: 51
6447 deg
RA of node: 166
5597 deg
Eccentricity:
0004654
Arg of perigee: 197
7811 deg
Mean anomaly: 162
3191 deg
Mean motion: 15
74888570 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1439
Checksum: 324
Coasting Arc #13 (Orbit 1454)
---------------------------------------
Vector Time (GMT): 2010/111/11:47:30
143
Vector Time (MET): N/A
Weight (LBS) : 797508
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1214053
99 A = 6719160
75 meter
Y = -4485757
39 meter E =
0003950
Z = 4849373
60 I = 51
74094
XDOT = 7304
828773 Wp = 100
20601
YDOT = -594
671054 meter/sec RA = 160
52126 deg
ZDOT = -2377
921638 TA = 12
94235
MA = 12
93222
Ha = 188
683 n
mi
Hp = 182
838
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3983116
75 X = 1240566
93
Y = -14717051
79 feet Y = -4472032
95 meter
Z = 15910018
37 Z = 4855335
79
XDOT = 23965
973665 XDOT = 7322
487089
YDOT = -1951
020518 feet/sec YDOT = -512
885339 meter/sec
ZDOT = -7801
580177 ZDOT = -2342
391908
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2837209
40 X = -864781
43
Y = -14955152
29 feet Y = -4558330
42 meter
Z = 15933586
53 Z = 4856557
17
XDOT = 19732
140107 XDOT = 6014
356305
YDOT = -11908
190297 feet/sec YDOT = -3629
616403 meter/sec
ZDOT = -7660
254548 ZDOT = -2334
845586
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
53491661
00016717 00000-0 10270-3 0 9129
2 25544 51
6448 161
3396 0004620 203
8760 156
2190 15
74959424 14556
Satellite: ISS
Catalog Number: 25544
Epoch time: 10111
53491661 = yrday
fracday
Element set: 912
Inclination: 51
6448 deg
RA of node: 161
3396 deg
Eccentricity:
0004620
Arg of perigee: 203
8760 deg
Mean anomaly: 156
2190 deg
Mean motion: 15
74959424 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1455
Checksum: 299
Coasting Arc #14 (Orbit 1470)
---------------------------------------
Vector Time (GMT): 2010/112/11:47:30
143
Vector Time (MET): N/A
Weight (LBS) : 797508
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6239853
85 A = 6727105
12 meter
Y = 799450
48 meter E =
0011583
Z = 2373163
95 I = 51
79521
XDOT = 1383
672690 Wp = 90
02136
YDOT = -5309
787018 meter/sec RA = 155
42695 deg
ZDOT = 5404
285687 TA = 296
66910
MA = 296
78767
Ha = 188
670 n
mi
Hp = 182
903
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20471961
46 X = -6259858
08
Y = 2622869
02 feet Y = 729560
88 meter
Z = 7785970
96 Z = 2342802
19
XDOT = 4539
608562 XDOT = 1416
691835
YDOT = -17420
561084 feet/sec YDOT = -5294
129318 meter/sec
ZDOT = 17730
596087 ZDOT = 5411
087792
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17185025
01 X = -5237995
62
Y = 11511804
18 feet Y = 3508797
91 meter
Z = 7665198
72 Z = 2336352
57
XDOT = -2973
917471 XDOT = -906
450045
YDOT = -16313
524425 feet/sec YDOT = -4972
362245 meter/sec
ZDOT = 17757
480561 ZDOT = 5412
480075
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 10112
55013631
00016717 00000-0 10270-3 0 9130
2 25544 51
6446 156
1187 0004354 204
5819 155
5138 15
74949152 14710
Satellite: ISS
Catalog Number: 25544
Epoch time: 10112
55013631 = yrday
fracday
Element set: 913
Inclination: 51
6446 deg
RA of node: 156
1187 deg
Eccentricity:
0004354
Arg of perigee: 204
5819 deg
Mean anomaly: 155
5138 deg
Mean motion: 15
74949152 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1471
Checksum: 294
Coasting Arc #15 (Orbit 1485)
---------------------------------------
Vector Time (GMT): 2010/113/11:47:30
143
Vector Time (MET): N/A
Weight (LBS) : 797508
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1195218
12 A = 6720274
05 meter
Y = 4807754
88 meter E =
0010476
Z = -4550917
16 I = 51
80085
XDOT = -6951
883965 Wp = 134
68037
YDOT = 1185
638747 meter/sec RA = 150
25183 deg
ZDOT = 3075
438073 TA = 165
90861
MA = 165
87936
Ha = 188
406 n
mi
Hp = 182
876
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3921319
30 X = -1226782
93
Y = 15773474
01 feet Y = 4794212
62 meter
Z = -14930830
57 Z = -4556800
33
XDOT = -22808
018259 XDOT = -6979
565236
YDOT = 3889
890903 feet/sec YDOT = 1107
743953 meter/sec
ZDOT = 10090
019923 ZDOT = 3041
598543
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3887745
74 X = 1184984
90
Y = 15759755
80 feet Y = 4803573
57 meter
Z = -14954078
34 Z = -4558003
08
XDOT = -17333
617598 XDOT = -5283
286644
YDOT = 13731
491272 feet/sec YDOT = 4185
358540 meter/sec
ZDOT = 9955
412202 ZDOT = 3034
409639
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 10113
50187601
00016717 00000-0 10270-3 0 9146
2 25544 51
6454 151
2243 0004336 209
3879 150
7041 15
75010063 14864
Satellite: ISS
Catalog Number: 25544
Epoch time: 10113
50187601 = yrday
fracday
Element set: 914
Inclination: 51
6454 deg
RA of node: 151
2243 deg
Eccentricity:
0004336
Arg of perigee: 209
3879 deg
Mean anomaly: 150
7041 deg
Mean motion: 15
75010063 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1486
Checksum: 274
Coasting Arc #16 (Orbit 1501)
---------------------------------------
Vector Time (GMT): 2010/114/11:47:30
143
Vector Time (MET): N/A
Weight (LBS) : 797508
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5889753
49 A = 6725300
89 meter
Y = -1225236
53 meter E =
0005603
Z = -3001614
72 I = 51
84408
XDOT = -1349
089599 Wp = 160
28303
YDOT = 5711
628323 meter/sec RA = 145
16852 deg
ZDOT = -4986
467597 TA = 54
31245
MA = 54
26031
Ha = 188
314 n
mi
Hp = 182
956
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19323338
22 X = 5917597
93
Y = -4019804
90 feet Y = -1159218
24 meter
Z = -9847817
32 Z = -2972934
49
XDOT = -4426
146979 XDOT = -1388
634322
YDOT = 18738
938068 feet/sec YDOT = 5696
320687 meter/sec
ZDOT = -16359
801829 ZDOT = -4993
117794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15113520
00 X = 4606600
90
Y = -12781459
77 feet Y = -3895788
94 meter
Z = -9733731
91 Z = -2966841
49
XDOT = 4205
095117 XDOT = 1281
712992
YDOT = 17431
336271 feet/sec YDOT = 5313
071295 meter/sec
ZDOT = -16386
075286 ZDOT = -4994
475747
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 10114
51703835
00016717 00000-0 10270-3 0 9152
2 25544 51
6457 146
0035 0004297 212
6245 147
4654 15
75068673 15020
Satellite: ISS
Catalog Number: 25544
Epoch time: 10114
51703835 = yrday
fracday
Element set: 915
Inclination: 51
6457 deg
RA of node: 146
0035 deg
Eccentricity:
0004297
Arg of perigee: 212
6245 deg
Mean anomaly: 147
4654 deg
Mean motion: 15
75068673 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1502
Checksum: 296
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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