Date:
June 3rd 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 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
156/03:22:07
072 -1
4 14
0 14
0
N/A -11
9 -0
0 190
9
000/00:04:10
144 -7
2 0
1 187
7
158/23:59:56
244 -0
7 2
6 2
6
N/A -2
2 0
0 191
2
000/00:09:52
488 -1
2 0
2 188
9
159/01:30:56
155 -0
8 2
7 2
7
N/A -2
2 0
0 191
1
000/00:09:52
310 -1
3 0
2 190
1
Coasting Arc #1 (Orbit 2084)
---------------------------------------
Vector Time (GMT): 2010/151/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 816195
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4718032
70 A = 6729089
62 meter
Y = 4796096
12 meter E =
0009987
Z = 150739
33 I = 51
42928
XDOT = -3521
416011 Wp = 85
48363
YDOT = -3264
296915 meter/sec RA = 315
55368 deg
ZDOT = -6014
451576 TA = 92
87459
MA = 92
76029
Ha = 190
672 n
mi
Hp = 180
944
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15479109
91 X = -4772045
12
Y = 15735223
48 feet Y = 4743034
24 meter
Z = 494551
61 Z = 127688
71
XDOT = -11553
202137 XDOT = -3455
435229
YDOT = -10709
635548 feet/sec YDOT = -3303
305595 meter/sec
ZDOT = -19732
452678 ZDOT = -6031
398873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8826432
90 X = 2690296
75
Y = 20233056
78 feet Y = 6167035
71 meter
Z = 402714
02 Z = 122747
23
XDOT = -12727
249212 XDOT = -3879
265560
YDOT = 5973
688901 feet/sec YDOT = 1820
780377 meter/sec
ZDOT = -19799
943281 ZDOT = -6035
022712
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 10151
53200013
00016717 00000-0 10270-3 0 9009
2 25544 51
6449 315
9719 0009390 5
5914 354
5353 15
75080810 20859
Satellite: ISS
Catalog Number: 25544
Epoch time: 10151
53200013 = yrday
fracday
Element set: 900
Inclination: 51
6449 deg
RA of node: 315
9719 deg
Eccentricity:
0009390
Arg of perigee: 5
5914 deg
Mean anomaly: 354
5353 deg
Mean motion: 15
75080810 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2085
Checksum: 282
Coasting Arc #2 (Orbit 2100)
---------------------------------------
Vector Time (GMT): 2010/152/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 816195
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3008891
77 A = 6717211
44 meter
Y = 2927153
82 meter E =
0010460
Z = 5240794
82 I = 51
36781
XDOT = -5138
527906 Wp = 23
01760
YDOT = 5737
567519 meter/sec RA = 310
39200 deg
ZDOT = -244
778320 TA = 69
36889
MA = 69
25675
Ha = 190
779 n
mi
Hp = 180
813
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9871692
15 X = 2950477
40
Y = 9603523
03 feet Y = 2960473
67 meter
Z = 17194208
72 Z = 5255270
52
XDOT = -16858
687355 XDOT = -5201
115428
YDOT = 18824
040416 feet/sec YDOT = 5679
755530 meter/sec
ZDOT = -803
078479 ZDOT = -269
892432
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12458598
30 X = 3797380
76
Y = -5698719
05 feet Y = -1736969
57 meter
Z = 17251860
87 Z = 5258367
19
XDOT = 11153
290983 XDOT = 3399
523092
YDOT = 21553
714495 feet/sec YDOT = 6569
572178 meter/sec
ZDOT = -903
135827 ZDOT = -275
275800
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 10152
54715960
00016717 00000-0 10270-3 0 9014
2 25544 51
6448 310
7507 0009202 10
9366 349
1997 15
75019292 21018
Satellite: ISS
Catalog Number: 25544
Epoch time: 10152
54715960 = yrday
fracday
Element set: 901
Inclination: 51
6448 deg
RA of node: 310
7507 deg
Eccentricity:
0009202
Arg of perigee: 10
9366 deg
Mean anomaly: 349
1997 deg
Mean motion: 15
75019292 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2101
Checksum: 296
Coasting Arc #3 (Orbit 2116)
---------------------------------------
Vector Time (GMT): 2010/153/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 816195
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4227668
91 A = 6728887
63 meter
Y = -5187071
77 meter E =
0021251
Z = 576220
59 I = 51
39042
XDOT = 3412
599929 Wp = 36
06803
YDOT = 3457
135762 meter/sec RA = 305
23840 deg
ZDOT = 5988
212918 TA = 330
23522
MA = 330
35594
Ha = 190
730 n
mi
Hp = 180
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13870304
84 X = 4282558
31
Y = -17017952
00 feet Y = -5139488
63 meter
Z = 1890487
49 Z = 596891
23
XDOT = 11196
193994 XDOT = 3344
598390
YDOT = 11342
308929 feet/sec YDOT = 3494
916506 meter/sec
ZDOT = 19646
367842 ZDOT = 6004
626560
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11276109
17 X = -3436958
08
Y = -18828894
33 feet Y = -5739046
99 meter
Z = 1972837
98 Z = 601321
02
XDOT = 13066
916031 XDOT = 3982
796006
YDOT = -5728
900566 feet/sec YDOT = -1746
168892 meter/sec
ZDOT = 19711
743186 ZDOT = 6008
139323
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 10153
56229468
00016717 00000-0 10270-3 0 9021
2 25544 51
6460 305
5301 0009094 14
3713 345
7708 15
75105211 21175
Satellite: ISS
Catalog Number: 25544
Epoch time: 10153
56229468 = yrday
fracday
Element set: 902
Inclination: 51
6460 deg
RA of node: 305
5301 deg
Eccentricity:
0009094
Arg of perigee: 14
3713 deg
Mean anomaly: 345
7708 deg
Mean motion: 15
75105211 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2117
Checksum: 280
Coasting Arc #4 (Orbit 2131)
---------------------------------------
Vector Time (GMT): 2010/154/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 816195
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2959225
80 A = 6717294
95 meter
Y = -3136171
99 meter E =
0018297
Z = -5164289
59 I = 51
33528
XDOT = 4552
375667 Wp = 68
79809
YDOT = -6099
925565 meter/sec RA = 300
06066 deg
ZDOT = 1105
439728 TA = 211
75375
MA = 211
86422
Ha = 190
812 n
mi
Hp = 180
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9708746
07 X = -2898849
46
Y = -10289278
19 feet Y = -3168925
65 meter
Z = -16943207
30 Z = -5178519
19
XDOT = 14935
615706 XDOT = 4614
877771
YDOT = -20012
879151 feet/sec YDOT = -6048
668845 meter/sec
ZDOT = 3626
770762 ZDOT = 1127
706288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12851412
81 X = -3917110
63
Y = 5748588
27 feet Y = 1752169
70 meter
Z = -16999887
98 Z = -5181565
86
XDOT = -13669
422266 XDOT = -4166
439907
YDOT = -19664
985631 feet/sec YDOT = -5993
887620 meter/sec
ZDOT = 3715
473364 ZDOT = 1132
476281
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 10154
51396830
00016717 00000-0 10270-3 0 9036
2 25544 51
6462 300
6365 0009176 18
1083 342
0406 15
75132136 21324
Satellite: ISS
Catalog Number: 25544
Epoch time: 10154
51396830 = yrday
fracday
Element set: 903
Inclination: 51
6462 deg
RA of node: 300
6365 deg
Eccentricity:
0009176
Arg of perigee: 18
1083 deg
Mean anomaly: 342
0406 deg
Mean motion: 15
75132136 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2132
Checksum: 274
Coasting Arc #5 (Orbit 2147)
---------------------------------------
Vector Time (GMT): 2010/155/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 816195
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3732561
69 A = 6727986
50 meter
Y = 5430089
10 meter E =
0008789
Z = -1372567
44 I = 51
35718
XDOT = -3363
266316 Wp = 78
17808
YDOT = -3771
018473 meter/sec RA = 294
91719 deg
ZDOT = -5802
232288 TA = 116
95684
MA = 116
86703
Ha = 190
902 n
mi
Hp = 180
077
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12245937
30 X = -3786336
82
Y = 17815252
95 feet Y = 5388048
84 meter
Z = -4503174
01 Z = -1390830
33
XDOT = -11034
338306 XDOT = -3292
661889
YDOT = -12372
107852 feet/sec YDOT = -3808
233156 meter/sec
ZDOT = -19036
195171 ZDOT = -5818
399959
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13180967
25 X = 4017558
82
Y = 17115719
07 feet Y = 5216871
17 meter
Z = -4575921
49 Z = -1394740
87
XDOT = -13888
800079 XDOT = -4233
306264
YDOT = 5614
830194 feet/sec YDOT = 1711
400243 meter/sec
ZDOT = -19100
600087 ZDOT = -5821
862906
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 10155
52906674
00016717 00000-0 10270-3 0 9042
2 25544 51
6457 295
4140 0009309 21
2796 338
8753 15
75172635 21487
Satellite: ISS
Catalog Number: 25544
Epoch time: 10155
52906674 = yrday
fracday
Element set: 904
Inclination: 51
6457 deg
RA of node: 295
4140 deg
Eccentricity:
0009309
Arg of perigee: 21
2796 deg
Mean anomaly: 338
8753 deg
Mean motion: 15
75172635 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2148
Checksum: 323
Coasting Arc #6 (Orbit 2157)
---------------------------------------
Vector Time (GMT): 2010/156/03:24:12
144
Vector Time (MET): N/A
Weight (LBS) : 814961
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4630612
31 A = 6727826
95 meter
Y = 2117309
74 meter E =
0006518
Z = -4403882
01 I = 51
32633
XDOT = -63
365021 Wp = 38
80302
YDOT = -6959
257861 meter/sec RA = 291
61790 deg
ZDOT = -3276
877841 TA = 198
11717
MA = 198
14040
Ha = 190
939 n
mi
Hp = 187
665
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15192297
60 X = -4632550
94
Y = 6946554
25 feet Y = 2065517
07 meter
Z = -14448431
78 Z = -4426382
11
XDOT = -207
890488 XDOT = 30
377913
YDOT = -22832
210831 feet/sec YDOT = -6959
441976 meter/sec
ZDOT = -10750
911551 ZDOT = -3276
958659
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14165159
76 X = -4317540
69
Y = -8706940
84 feet Y = -2653875
57 meter
Z = -14538058
11 Z = -4431200
11
XDOT = 18274
079145 XDOT = 5569
939323
YDOT = -11765
330999 feet/sec YDOT = -3586
072888 meter/sec
ZDOT = -10751
240870 ZDOT = -3276
978217
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 10156
16351579
00016717 00000-0 10270-3 0 9052
2 25544 51
6485 292
1567 0005054 290
0987 69
9631 15
72537704 21583
Satellite: ISS
Catalog Number: 25544
Epoch time: 10156
16351579 = yrday
fracday
Element set: 905
Inclination: 51
6485 deg
RA of node: 292
1567 deg
Eccentricity:
0005054
Arg of perigee: 290
0987 deg
Mean anomaly: 69
9631 deg
Mean motion: 15
72537704 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2158
Checksum: 329
Coasting Arc #7 (Orbit 2173)
---------------------------------------
Vector Time (GMT): 2010/157/03:24:12
144
Vector Time (MET): N/A
Weight (LBS) : 814961
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 987697
79 A = 6731790
79 meter
Y = 5815550
10 meter E =
0008349
Z = 3238150
54 I = 51
32888
XDOT = -4973
790531 Wp = 79
65047
YDOT = 3485
058963 meter/sec RA = 286
42255 deg
ZDOT = -4730
062902 TA = 62
29962
MA = 62
21494
Ha = 191
075 n
mi
Hp = 187
736
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3240478
32 X = 906863
38
Y = 19079888
79 feet Y = 5826142
84 meter
Z = 10623853
47 Z = 3242753
04
XDOT = -16318
210402 XDOT = -4989
413456
YDOT = 11433
920482 feet/sec YDOT = 3429
352193 meter/sec
ZDOT = -15518
579076 ZDOT = -4754
263368
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13874225
39 X = -4228863
90
Y = 13478078
42 feet Y = 4108118
30 meter
Z = 10642198
57 Z = 3243742
12
XDOT = -17656
163213 XDOT = -5381
598547
YDOT = -5815
065944 feet/sec YDOT = -1772
432100 meter/sec
ZDOT = -15614
974490 ZDOT = -4759
444225
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 10157
18029886
00016717 00000-0 10270-3 0 9069
2 25544 51
6479 286
9471 0005032 294
0005 66
0630 15
72532323 21749
Satellite: ISS
Catalog Number: 25544
Epoch time: 10157
18029886 = yrday
fracday
Element set: 906
Inclination: 51
6479 deg
RA of node: 286
9471 deg
Eccentricity:
0005032
Arg of perigee: 294
0005 deg
Mean anomaly: 66
0630 deg
Mean motion: 15
72532323 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2174
Checksum: 302
Coasting Arc #8 (Orbit 2189)
---------------------------------------
Vector Time (GMT): 2010/158/03:24:12
144
Vector Time (MET): N/A
Weight (LBS) : 814961
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3913116
33 A = 6729812
29 meter
Y = -3901545
38 meter E =
0006726
Z = 3834989
64 I = 51
31570
XDOT = 2116
836223 Wp = 83
86362
YDOT = 6162
129095 meter/sec RA = 281
32602 deg
ZDOT = 4103
655195 TA = 323
05696
MA = 323
10326
Ha = 191
093 n
mi
Hp = 187
645
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12838308
15 X = 3937823
38
Y = -12800345
74 feet Y = -3857648
85 meter
Z = 12581987
01 Z = 3854059
37
XDOT = 6945
000733 XDOT = 2027
837814
YDOT = 20216
958974 feet/sec YDOT = 6185
302762 meter/sec
ZDOT = 13463
435680 ZDOT = 4113
723386
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17842860
25 X = 5438503
81
Y = 2895902
30 feet Y = 882671
02 meter
Z = 12657941
87 Z = 3858140
68
XDOT = -12200
687507 XDOT = -3718
769552
YDOT = 16071
909539 feet/sec YDOT = 4898
718028 meter/sec
ZDOT = 13503
557833 ZDOT = 4115
884428
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 10158
19706440
00016717 00000-0 10270-3 0 9070
2 25544 51
6484 281
7368 0005139 299
0148 61
0499 15
72560043 21900
Satellite: ISS
Catalog Number: 25544
Epoch time: 10158
19706440 = yrday
fracday
Element set: 907
Inclination: 51
6484 deg
RA of node: 281
7368 deg
Eccentricity:
0005139
Arg of perigee: 299
0148 deg
Mean anomaly: 61
0499 deg
Mean motion: 15
72560043 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2190
Checksum: 314
Coasting Arc #9 (Orbit 2202)
---------------------------------------
Vector Time (GMT): 2010/159/00:04:52
488
Vector Time (MET): N/A
Weight (LBS) : 814706
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4175424
99 A = 6727241
34 meter
Y = 2048859
71 meter E =
0007647
Z = -4867181
64 I = 51
29653
XDOT = -942
598692 Wp = 49
44032
YDOT = -7292
226804 meter/sec RA = 276
88212 deg
ZDOT = -2258
485927 TA = 198
44463
MA = 198
47237
Ha = 191
225 n
mi
Hp = 188
871
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13698900
88 X = -4174381
17
Y = 6721980
67 feet Y = 2002174
04 meter
Z = -15968443
69 Z = -4887463
35
XDOT = -3092
515395 XDOT = -850
014171
YDOT = -23924
628623 feet/sec YDOT = -7302
249566 meter/sec
ZDOT = -7409
730730 ZDOT = -2262
841119
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3416041
25 X = -1041209
37
Y = -14784753
00 feet Y = -4506392
71 meter
Z = -16049231
89 Z = -4891805
88
XDOT = 22907
185706 XDOT = 6982
110203
YDOT = 2778
695620 feet/sec YDOT = 846
946425 meter/sec
ZDOT = -7427
100520 ZDOT = -2263
780239
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 10159
02317855
00016717 00000-0 10270-3 0 9082
2 25544 51
6467 277
5031 0006206 283
5928 76
4543 15
72091706 22031
Satellite: ISS
Catalog Number: 25544
Epoch time: 10159
02317855 = yrday
fracday
Element set: 908
Inclination: 51
6467 deg
RA of node: 277
5031 deg
Eccentricity:
0006206
Arg of perigee: 283
5928 deg
Mean anomaly: 76
4543 deg
Mean motion: 15
72091706 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2203
Checksum: 307
Coasting Arc #10 (Orbit 2203)
---------------------------------------
Vector Time (GMT): 2010/159/01:35:52
310
Vector Time (MET): N/A
Weight (LBS) : 814451
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4129058
65 A = 6729024
44 meter
Y = 2306590
79 meter E =
0005190
Z = -4791068
00 I = 51
29860
XDOT = -1159
097937 Wp = 45
32834
YDOT = -7195
023046 meter/sec RA = 276
55896 deg
ZDOT = -2463
041474 TA = 200
43980
MA = 200
46058
Ha = 191
075 n
mi
Hp = 190
141
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13546780
36 X = -4131270
02
Y = 7567555
10 feet Y = 2260405
42 meter
Z = -15718727
04 Z = -4811132
34
XDOT = -3802
814755 XDOT = -1066
590566
YDOT = -23605
718656 feet/sec YDOT = -7207
467235 meter/sec
ZDOT = -8080
844732 ZDOT = -2468
448619
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9689898
89 X = -2953481
18
Y = -12015410
41 feet Y = -3662297
09 meter
Z = -15798648
69 Z = -4815428
12
XDOT = 21782
427325 XDOT = 6639
283849
YDOT = -6904
581581 feet/sec YDOT = -2104
516466 meter/sec
ZDOT = -8102
404947 ZDOT = -2469
613028
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 10159
08674999
00016717 00000-0 10270-3 0 9094
2 25544 51
6479 277
1783 0007594 270
3793 89
6499 15
71579575 22040
Satellite: ISS
Catalog Number: 25544
Epoch time: 10159
08674999 = yrday
fracday
Element set: 909
Inclination: 51
6479 deg
RA of node: 277
1783 deg
Eccentricity:
0007594
Arg of perigee: 270
3793 deg
Mean anomaly: 89
6499 deg
Mean motion: 15
71579575 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2204
Checksum: 378
Coasting Arc #11 (Orbit 2219)
---------------------------------------
Vector Time (GMT): 2010/160/01:35:52
310
Vector Time (MET): N/A
Weight (LBS) : 814451
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2136320
28 A = 6735576
52 meter
Y = 5718769
05 meter E =
0005896
Z = 2838996
53 I = 51
31803
XDOT = -4145
589858 Wp = 105
53149
YDOT = 4061
476197 meter/sec RA = 271
37567 deg
ZDOT = -5054
600252 TA = 41
77269
MA = 41
72770
Ha = 191
369 n
mi
Hp = 190
469
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7008924
79 X = 2058421
65
Y = 18762365
64 feet Y = 5742222
70 meter
Z = 9314293
09 Z = 2849186
53
XDOT = -13601
016594 XDOT = -4166
143199
YDOT = 13325
053139 feet/sec YDOT = 4015
003541 meter/sec
ZDOT = -16583
334159 ZDOT = -5074
789186
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17178609
37 X = -5236040
14
Y = 10261022
63 feet Y = 3127559
70 meter
Z = 9354904
68 Z = 2851374
95
XDOT = -14816
653085 XDOT = -4516
115860
YDOT = -9591
902265 feet/sec YDOT = -2923
611810 meter/sec
ZDOT = -16663
749399 ZDOT = -5079
110817
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 10160
10415400
00016717 00000-0 10270-3 0 9101
2 25544 51
6476 271
9730 0007624 274
1000 85
9291 15
71570004 22203
Satellite: ISS
Catalog Number: 25544
Epoch time: 10160
10415400 = yrday
fracday
Element set: 910
Inclination: 51
6476 deg
RA of node: 271
9730 deg
Eccentricity:
0007624
Arg of perigee: 274
1000 deg
Mean anomaly: 85
9291 deg
Mean motion: 15
71570004 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2220
Checksum: 258
Coasting Arc #12 (Orbit 2235)
---------------------------------------
Vector Time (GMT): 2010/161/01:35:52
310
Vector Time (MET): N/A
Weight (LBS) : 814451
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2875250
36 A = 6732170
14 meter
Y = -4624365
73 meter E =
0003339
Z = 3956554
04 I = 51
30787
XDOT = 3533
238766 Wp = 107
02137
YDOT = 5580
131117 meter/sec RA = 266
28413 deg
ZDOT = 3950
642319 TA = 301
83885
MA = 301
87135
Ha = 191
673 n
mi
Hp = 190
580
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9433236
08 X = 2907526
65
Y = -15171803
58 feet Y = -4592033
16 meter
Z = 12980820
36 Z = 3970599
85
XDOT = 11591
990701 XDOT = 3451
386340
YDOT = 18307
516788 feet/sec YDOT = 5619
183576 meter/sec
ZDOT = 12961
424930 ZDOT = 3967
609161
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16732227
55 X = 5099982
96
Y = 6143826
56 feet Y = 1872638
33 meter
Z = 13036764
19 Z = 3973605
72
XDOT = -15196
516261 XDOT = -4631
898156
YDOT = 13714
081512 feet/sec YDOT = 4180
052045 meter/sec
ZDOT = 13029
037880 ZDOT = 3971
250746
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 10161
12154212
00016717 00000-0 10270-3 0 9116
2 25544 51
6482 266
7671 0007655 278
9646 81
0650 15
71599732 22360
Satellite: ISS
Catalog Number: 25544
Epoch time: 10161
12154212 = yrday
fracday
Element set: 911
Inclination: 51
6482 deg
RA of node: 266
7671 deg
Eccentricity:
0007655
Arg of perigee: 278
9646 deg
Mean anomaly: 81
0650 deg
Mean motion: 15
71599732 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2236
Checksum: 310
Coasting Arc #13 (Orbit 2250)
---------------------------------------
Vector Time (GMT): 2010/162/01:35:52
310
Vector Time (MET): N/A
Weight (LBS) : 814451
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3837094
54 A = 6731925
20 meter
Y = -3826767
82 meter E =
0000907
Z = -3993654
82 I = 51
31104
XDOT = 2182
220715 Wp = 235
26860
YDOT = -6262
444484 meter/sec RA = 261
09218 deg
ZDOT = 3902
938912 TA = 75
26312
MA = 75
25307
Ha = 191
959 n
mi
Hp = 190
468
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12588892
85 X = -3774617
06
Y = -12555012
53 feet Y = -3869326
41 meter
Z = -13102542
06 Z = -4012144
63
XDOT = 7159
516780 XDOT = 2233
126312
YDOT = -20546
077704 feet/sec YDOT = -6237
757706 meter/sec
ZDOT = 12804
917689 ZDOT = 3913
662733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9553538
74 X = 2911918
61
Y = -14929909
33 feet Y = -4550636
36 meter
Z = -13176223
90 Z = -4016113
04
XDOT = 20502
550840 XDOT = 6249
177496
YDOT = 1777
629099 feet/sec YDOT = 541
821349 meter/sec
ZDOT = 12847
624094 ZDOT = 3915
955824
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 10162
07532948
00016717 00000-0 10270-3 0 9128
2 25544 51
6486 261
8872 0007777 283
0844 76
9449 15
71633061 22515
Satellite: ISS
Catalog Number: 25544
Epoch time: 10162
07532948 = yrday
fracday
Element set: 912
Inclination: 51
6486 deg
RA of node: 261
8872 deg
Eccentricity:
0007777
Arg of perigee: 283
0844 deg
Mean anomaly: 76
9449 deg
Mean motion: 15
71633061 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2251
Checksum: 327
Coasting Arc #14 (Orbit 2266)
---------------------------------------
Vector Time (GMT): 2010/163/01:35:52
310
Vector Time (MET): N/A
Weight (LBS) : 814451
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -803596
61 A = 6735492
23 meter
Y = 6067757
86 meter E =
0003476
Z = -2808254
63 I = 51
32890
XDOT = -4937
647489 Wp = 269
44283
YDOT = -3006
434621 meter/sec RA = 256
00139 deg
ZDOT = -5077
642379 TA = 302
84148
MA = 302
87493
Ha = 192
354 n
mi
Hp = 190
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2636471
83 X = -857745
56
Y = 19907342
06 feet Y = 6058469
38 meter
Z = -9213433
82 Z = -2812288
81
XDOT = -16199
630871 XDOT = -4878
995564
YDOT = -9863
630645 feet/sec YDOT = -3061
321349 meter/sec
ZDOT = -16658
931689 ZDOT = -5101
487810
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19960829
59 X = -6084060
86
Y = 2126611
57 feet Y = 648191
21 meter
Z = -9229486
44 Z = -2813147
47
XDOT = 5996
911469 XDOT = 1827
858616
YDOT = -16500
407507 feet/sec YDOT = -5029
324208 meter/sec
ZDOT = -16753
960493 ZDOT = -5106
607158
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 10163
09268897
00016717 00000-0 10270-3 0 9131
2 25544 51
6487 256
6819 0007897 286
3988 73
6306 15
71632246 22674
Satellite: ISS
Catalog Number: 25544
Epoch time: 10163
09268897 = yrday
fracday
Element set: 913
Inclination: 51
6487 deg
RA of node: 256
6819 deg
Eccentricity:
0007897
Arg of perigee: 286
3988 deg
Mean anomaly: 73
6306 deg
Mean motion: 15
71632246 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2267
Checksum: 359
Coasting Arc #15 (Orbit 2282)
---------------------------------------
Vector Time (GMT): 2010/164/01:35:52
310
Vector Time (MET): N/A
Weight (LBS) : 814451
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4530928
67 A = 6728609
42 meter
Y = 1342628
90 meter E =
0006651
Z = 4793451
80 I = 51
31478
XDOT = 448
788451 Wp = 348
66759
YDOT = 7277
177973 meter/sec RA = 250
81855 deg
ZDOT = -2456
669466 TA = 125
50907
MA = 125
44701
Ha = 192
490 n
mi
Hp = 190
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14865251
53 X = 4492292
64
Y = 4404950
46 feet Y = 1393079
41 meter
Z = 15726547
89 Z = 4815369
53
XDOT = 1472
403054 XDOT = 379
314449
YDOT = 23875
255816 feet/sec YDOT = 7281
808660 meter/sec
ZDOT = -8059
939193 ZDOT = -2454
656467
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -578007
46 X = -176176
67
Y = 15404221
88 feet Y = 4695206
83 meter
Z = 15813900
71 Z = 4820076
94
XDOT = -21616
216459 XDOT = -6588
622777
YDOT = 7474
529068 feet/sec YDOT = 2278
236460 meter/sec
ZDOT = -8051
884208 ZDOT = -2454
214307
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 10164
11003228
00016717 00000-0 10270-3 0 9141
2 25544 51
6484 251
4763 0007968 291
6635 68
3678 15
71717743 22836
Satellite: ISS
Catalog Number: 25544
Epoch time: 10164
11003228 = yrday
fracday
Element set: 914
Inclination: 51
6484 deg
RA of node: 251
4763 deg
Eccentricity:
0007968
Arg of perigee: 291
6635 deg
Mean anomaly: 68
3678 deg
Mean motion: 15
71717743 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2283
Checksum: 321
Coasting Arc #16 (Orbit 2298)
---------------------------------------
Vector Time (GMT): 2010/165/01:35:52
310
Vector Time (MET): N/A
Weight (LBS) : 814451
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1602501
19 A = 6737831
92 meter
Y = -6373414
78 meter E =
0011412
Z = 1451944
75 I = 51
35605
XDOT = 5087
641041 Wp = 26
60285
YDOT = 39
194923 meter/sec RA = 245
71178 deg
ZDOT = 5779
779784 TA = 349
43143
MA = 349
45539
Ha = 192
727 n
mi
Hp = 190
018
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5257549
84 X = -1538166
67
Y = -20910153
46 feet Y = -6390975
48 meter
Z = 4763598
27 Z = 1444314
81
XDOT = 16691
735698 XDOT = 5058
747622
YDOT = 128
592267 feet/sec YDOT = 95
925231 meter/sec
ZDOT = 18962
532100 ZDOT = 5804
425277
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18747656
02 X = 5714285
56
Y = -10662592
97 feet Y = -3249958
34 meter
Z = 4733151
32 Z = 1442664
52
XDOT = 3512
638961 XDOT = 1070
652355
YDOT = 14648
205095 feet/sec YDOT = 4464
772913 meter/sec
ZDOT = 19060
761903 ZDOT = 5809
720228
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 10165
12736314
00016717 00000-0 10270-3 0 9153
2 25544 51
6479 246
2701 0007973 295
8388 64
1952 15
71699992 22992
Satellite: ISS
Catalog Number: 25544
Epoch time: 10165
12736314 = yrday
fracday
Element set: 915
Inclination: 51
6479 deg
RA of node: 246
2701 deg
Eccentricity:
0007973
Arg of perigee: 295
8388 deg
Mean anomaly: 64
1952 deg
Mean motion: 15
71699992 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2299
Checksum: 349
Coasting Arc #17 (Orbit 2313)
---------------------------------------
Vector Time (GMT): 2010/166/01:35:52
310
Vector Time (MET): N/A
Weight (LBS) : 814451
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4087344
81 A = 6726768
35 meter
Y = 1232233
54 meter E =
0007962
Z = -5204810
95 I = 51
33197
XDOT = -3161
226087 Wp = 73
20692
YDOT = -6962
439170 meter/sec RA = 240
55183 deg
ZDOT = 837
488561 TA = 204
78960
MA = 204
82787
Ha = 192
803 n
mi
Hp = 189
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13409923
92 X = -4075536
27
Y = 4042760
96 feet Y = 1186593
40 meter
Z = -17076151
40 Z = -5224638
20
XDOT = -10371
476664 XDOT = -3087
204217
YDOT = -22842
648194 feet/sec YDOT = -6997
376159 meter/sec
ZDOT = 2747
665884 ZDOT = 822
309961
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7641143
99 X = -2329020
69
Y = -11622294
51 feet Y = -3542475
37 meter
Z = -17155177
39 Z = -5228898
07
XDOT = 18124
709314 XDOT = 5524
411399
YDOT = -15866
503137 feet/sec YDOT = -4836
110156 meter/sec
ZDOT = 2687
111269 ZDOT = 819
031515
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 10166
08109628
00016717 00000-0 10270-3 0 9162
2 25544 51
6471 241
3893 0008026 299
4864 60
5497 15
71739166 23141
Satellite: ISS
Catalog Number: 25544
Epoch time: 10166
08109628 = yrday
fracday
Element set: 916
Inclination: 51
6471 deg
RA of node: 241
3893 deg
Eccentricity:
0008026
Arg of perigee: 299
4864 deg
Mean anomaly: 60
5497 deg
Mean motion: 15
71739166 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2314
Checksum: 327
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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