Date:
May 14th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8072 93 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 17)
---------------------------------------
Vector Time (GMT): 2009/131/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 657345
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3741851
40 A = 6724235
76 meter
Y = 2028675
38 meter E =
0016944
Z = -5218191
52 I = 51
85497
XDOT = -4696
886661 Wp = 49
01553
YDOT = 5999
264976 meter/sec RA = 134
13450 deg
ZDOT = -1026
992200 TA = 211
15479
MA = 211
25535
Ha = 193
878 n
mi
Hp = 185
521
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12276415
36 X = 3744237
73
Y = 6655759
12 feet Y = 2070532
91 meter
Z = -17120050
93 Z = -5200007
29
XDOT = -15409
733141 XDOT = -4758
633348
YDOT = 19682
627874 feet/sec YDOT = 5946
396528 meter/sec
ZDOT = -3369
396981 ZDOT = -1049
959299
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13172712
44 X = 4015042
75
Y = -4891355
23 feet Y = -1490885
07 meter
Z = -17048751
81 Z = -5196459
55
XDOT = 4248
183970 XDOT = 1294
846474
YDOT = 23596
505036 feet/sec YDOT = 7192
214735 meter/sec
ZDOT = -3458
879371 ZDOT = -1054
266432
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 09131
51767387
00010596 00000-0 82463-4 0 9008
2 25544 51
6367 134
9785 0009266 350
2895 9
8087 15
72682441 183
Satellite: ISS
Catalog Number: 25544
Epoch time: 09131
51767387 = yrday
fracday
Element set: 900
Inclination: 51
6367 deg
RA of node: 134
9785 deg
Eccentricity:
0009266
Arg of perigee: 350
2895 deg
Mean anomaly: 9
8087 deg
Mean motion: 15
72682441 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 18
Checksum: 331
Coasting Arc #2 (Orbit 33)
---------------------------------------
Vector Time (GMT): 2009/132/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 657345
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3324981
04 A = 6735047
83 meter
Y = -5712673
73 meter E =
0011338
Z = 1290663
99 I = 51
91133
XDOT = 4760
394137 Wp = 78
58152
YDOT = 1433
951287 meter/sec RA = 129
00431 deg
ZDOT = -5871
276754 TA = 87
32558
MA = 87
19580
Ha = 193
965 n
mi
Hp = 185
099
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10908730
43 X = 3382344
11
Y = -18742367
87 feet Y = -5675171
28 meter
Z = 4234461
92 Z = 1306955
57
XDOT = 15618
091002 XDOT = 4772
527578
YDOT = 4704
564591 feet/sec YDOT = 1487
253366 meter/sec
ZDOT = -19262
719009 ZDOT = -5848
120835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7228937
69 X = -2203380
21
Y = -20432286
72 feet Y = -6227760
99 meter
Z = 4297852
97 Z = 1309985
58
XDOT = 12282
676273 XDOT = 3743
759728
YDOT = -8409
275436 feet/sec YDOT = -2563
147153 meter/sec
ZDOT = -19171
993963 ZDOT = -5843
623760
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 09132
53434476
00010596 00000-0 82463-4 0 9012
2 25544 51
6363 129
7664 0009436 354
5741 5
5317 15
72729357 348
Satellite: ISS
Catalog Number: 25544
Epoch time: 09132
53434476 = yrday
fracday
Element set: 901
Inclination: 51
6363 deg
RA of node: 129
7664 deg
Eccentricity:
0009436
Arg of perigee: 354
5741 deg
Mean anomaly: 5
5317 deg
Mean motion: 15
72729357 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 34
Checksum: 310
Coasting Arc #3 (Orbit 49)
---------------------------------------
Vector Time (GMT): 2009/133/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 657345
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4456400
45 A = 6724988
19 meter
Y = -419315
00 meter E =
0007551
Z = 5013462
91 I = 51
89467
XDOT = 2817
956929 Wp = 35
54374
YDOT = -6904
408840 meter/sec RA = 123
92485 deg
ZDOT = 1931
943944 TA = 35
89656
MA = 35
84586
Ha = 194
201 n
mi
Hp = 184
952
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14620736
38 X = -4475735
08
Y = -1375705
39 feet Y = -469257
79 meter
Z = 16448369
13 Z = 4991766
52
XDOT = 9245
265516 XDOT = 2885
568644
YDOT = -22652
259975 feet/sec YDOT = -6872
519001 meter/sec
ZDOT = 6338
398768 ZDOT = 1945
797080
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10400868
21 X = -3170184
63
Y = 10500855
49 feet Y = 3200660
75 meter
Z = 16363414
04 Z = 4987568
60
XDOT = -10898
737702 XDOT = -3321
935251
YDOT = -20732
374075 feet/sec YDOT = -6319
227618 meter/sec
ZDOT = 6392
180646 ZDOT = 1948
336661
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 09133
55100475
00010596 00000-0 82463-4 0 9025
2 25544 51
6360 124
5548 0009440 357
7379 2
3739 15
72721760 507
Satellite: ISS
Catalog Number: 25544
Epoch time: 09133
55100475 = yrday
fracday
Element set: 902
Inclination: 51
6360 deg
RA of node: 124
5548 deg
Eccentricity:
0009440
Arg of perigee: 357
7379 deg
Mean anomaly: 2
3739 deg
Mean motion: 15
72721760 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 50
Checksum: 292
Coasting Arc #4 (Orbit 64)
---------------------------------------
Vector Time (GMT): 2009/134/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 657345
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1553059
04 A = 6733850
47 meter
Y = 6205751
90 meter E =
0015056
Z = -2078086
50 I = 51
94054
XDOT = -5281
476391 Wp = 17
97943
YDOT = 538
770858 meter/sec RA = 118
78488 deg
ZDOT = 5580
674035 TA = 318
91749
MA = 319
03077
Ha = 194
185 n
mi
Hp = 184
668
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5095338
05 X = -1612242
35
Y = 20360078
40 feet Y = 6188054
01 meter
Z = -6817869
11 Z = -2085774
36
XDOT = -17327
678449 XDOT = -5314
218540
YDOT = 1767
620924 feet/sec YDOT = 479
526605 meter/sec
ZDOT = 18309
298016 ZDOT = 5554
937006
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12815482
69 X = 3906159
12
Y = 16608816
41 feet Y = 5062367
24 meter
Z = -6847570
55 Z = -2087139
50
XDOT = -8232
257021 XDOT = -2509
191940
YDOT = 13826
015207 feet/sec YDOT = 4214
169435 meter/sec
ZDOT = 18208
577412 ZDOT = 5549
974395
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 09134
50411220
00010596 00000-0 82463-4 0 9035
2 25544 51
6362 119
6697 0009443 2
1768 357
9434 15
72746265 659
Satellite: ISS
Catalog Number: 25544
Epoch time: 09134
50411220 = yrday
fracday
Element set: 903
Inclination: 51
6362 deg
RA of node: 119
6697 deg
Eccentricity:
0009443
Arg of perigee: 2
1768 deg
Mean anomaly: 357
9434 deg
Mean motion: 15
72746265 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 65
Checksum: 304
Coasting Arc #5 (Orbit 80)
---------------------------------------
Vector Time (GMT): 2009/135/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 657345
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4622909
68 A = 6726225
66 meter
Y = -1345776
13 meter E =
0017255
Z = -4712197
36 I = 51
92816
XDOT = -758
946856 Wp = 40
93650
YDOT = 7127
734445 meter/sec RA = 113
71849 deg
ZDOT = -2773
169262 TA = 201
74710
MA = 201
82045
Ha = 194
288 n
mi
Hp = 184
623
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15167026
51 X = 4660505
89
Y = -4415276
02 feet Y = -1293869
37 meter
Z = -15459965
08 Z = -4689647
98
XDOT = -2489
983123 XDOT = -825
122366
YDOT = 23384
955528 feet/sec YDOT = 7118
877728 meter/sec
ZDOT = -9098
324350 ZDOT = -2777
016272
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5762430
46 X = 1756388
81
Y = -14800238
82 feet Y = -4511112
79 meter
Z = -15371766
39 Z = -4685314
39
XDOT = 16013
503059 XDOT = 4880
915733
YDOT = 15723
768709 feet/sec YDOT = 4792
604703 meter/sec
ZDOT = -9112
936935 ZDOT = -2777
623178
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 09135
52074918
00010596 00000-0 82463-4 0 9048
2 25544 51
6363 114
4573 0009486 5
4780 354
6485 15
72754108 816
Satellite: ISS
Catalog Number: 25544
Epoch time: 09135
52074918 = yrday
fracday
Element set: 904
Inclination: 51
6363 deg
RA of node: 114
4573 deg
Eccentricity:
0009486
Arg of perigee: 5
4780 deg
Mean anomaly: 354
6485 deg
Mean motion: 15
72754108 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 81
Checksum: 314
Coasting Arc #6 (Orbit 96)
---------------------------------------
Vector Time (GMT): 2009/136/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 657345
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -212403
75 A = 6732319
55 meter
Y = -6137640
86 meter E =
0016338
Z = 2755500
91 I = 51
95997
XDOT = 5113
940680 Wp = 64
63287
YDOT = -2513
090637 meter/sec RA = 108
56979 deg
ZDOT = -5172
947577 TA = 84
04995
MA = 83
86376
Ha = 194
345 n
mi
Hp = 184
281
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -696862
70 X = -157141
61
Y = -20136616
98 feet Y = -6139707
33 meter
Z = 9040357
31 Z = 2754602
76
XDOT = 16778
020604 XDOT = 5166
791754
YDOT = -8245
048021 feet/sec YDOT = -2455
607621 meter/sec
ZDOT = -16971
612786 ZDOT = -5147
975781
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16646552
61 X = -5073869
24
Y = -11354811
07 feet Y = -3460946
41 meter
Z = 9036457
99 Z = 2754312
40
XDOT = 2559
414758 XDOT = 780
109618
YDOT = -17260
748188 feet/sec YDOT = -5261
076048 meter/sec
ZDOT = -16873
995191 ZDOT = -5143
193734
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 09136
53737313
00010596 00000-0 82463-4 0 9056
2 25544 51
6364 109
2457 0009621 8
4468 351
6855 15
72794897 971
Satellite: ISS
Catalog Number: 25544
Epoch time: 09136
53737313 = yrday
fracday
Element set: 905
Inclination: 51
6364 deg
RA of node: 109
2457 deg
Eccentricity:
0009621
Arg of perigee: 8
4468 deg
Mean anomaly: 351
6855 deg
Mean motion: 15
72794897 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 97
Checksum: 337
Coasting Arc #7 (Orbit 112)
---------------------------------------
Vector Time (GMT): 2009/137/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 657345
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4187093
02 A = 6727523
37 meter
Y = 3019707
04 meter E =
0012875
Z = 4300410
03 I = 51
95300
XDOT = -1226
314685 Wp = 61
10511
YDOT = -6737
804924 meter/sec RA = 103
51366 deg
ZDOT = 3535
404470 TA = 353
26034
MA = 353
27764
Ha = 194
439 n
mi
Hp = 184
077
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13737181
83 X = -4241439
44
Y = 9907175
34 feet Y = 2972580
35 meter
Z = 14108956
78 Z = 4279937
21
XDOT = -4023
342143 XDOT = -1168
054730
YDOT = -22105
659198 feet/sec YDOT = -6751
192795 meter/sec
ZDOT = 11599
096029 ZDOT = 3529
588028
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 57921
56 X = 17654
49
Y = 17003214
94 feet Y = 5182579
91 meter
Z = 14028979
87 Z = 4276033
06
XDOT = -19141
233441 XDOT = -5834
247953
YDOT = -9490
768307 feet/sec YDOT = -2892
786180 meter/sec
ZDOT = 11575
905776 ZDOT = 3528
336081
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 09137
55398433
00010596 00000-0 82463-4 0 9066
2 25544 51
6369 104
0345 0009459 11
8099 348
3284 15
72837246 1136
Satellite: ISS
Catalog Number: 25544
Epoch time: 09137
55398433 = yrday
fracday
Element set: 906
Inclination: 51
6369 deg
RA of node: 104
0345 deg
Eccentricity:
0009459
Arg of perigee: 11
8099 deg
Mean anomaly: 348
3284 deg
Mean motion: 15
72837246 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 113
Checksum: 322
Coasting Arc #8 (Orbit 127)
---------------------------------------
Vector Time (GMT): 2009/138/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 657345
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1879277
89 A = 6730599
63 meter
Y = 5495290
24 meter E =
0011945
Z = -3398559
78 I = 51
96864
XDOT = -4320
510445 Wp = 39
06930
YDOT = 4346
686008 meter/sec RA = 98
35957 deg
ZDOT = 4657
139913 TA = 281
04919
MA = 281
18350
Ha = 194
587 n
mi
Hp = 183
912
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6165609
86 X = 1834198
69
Y = 18029167
46 feet Y = 5516053
58 meter
Z = -11150130
52 Z = -3389539
33
XDOT = -14174
903035 XDOT = -4391
418457
YDOT = 14260
780865 feet/sec YDOT = 4297
974781 meter/sec
ZDOT = 15279
330423 ZDOT = 4635
978714
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18390671
47 X = 5605476
66
Y = 5063860
66 feet Y = 1543464
73 meter
Z = -11114474
93 Z = -3387691
96
XDOT = 4057
896347 XDOT = 1236
846806
YDOT = 18488
428539 feet/sec YDOT = 5635
273019 meter/sec
ZDOT = 15196
733055 ZDOT = 4631
964235
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 09138
50704813
00010596 00000-0 82463-4 0 9076
2 25544 51
6368 99
1481 0009660 15
8261 344
3202 15
72801017 1288
Satellite: ISS
Catalog Number: 25544
Epoch time: 09138
50704813 = yrday
fracday
Element set: 907
Inclination: 51
6368 deg
RA of node: 99
1481 deg
Eccentricity:
0009660
Arg of perigee: 15
8261 deg
Mean anomaly: 344
3202 deg
Mean motion: 15
72801017 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 128
Checksum: 294
Coasting Arc #9 (Orbit 143)
---------------------------------------
Vector Time (GMT): 2009/139/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 657345
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3263417
23 A = 6729141
80 meter
Y = -4477942
89 meter E =
0014181
Z = -3835027
68 I = 51
96802
XDOT = 2947
336826 Wp = 40
89982
YDOT = 5733
272285 meter/sec RA = 93
30660 deg
ZDOT = -4184
585498 TA = 185
36360
MA = 185
37881
Ha = 194
560 n
mi
Hp = 183
737
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10706749
43 X = 3331877
91
Y = -14691413
69 feet Y = -4441066
45 meter
Z = -12582111
82 Z = -3819007
76
XDOT = 9669
740244 XDOT = 2903
335580
YDOT = 18809
948442 feet/sec YDOT = 5765
985347 meter/sec
ZDOT = -13728
955046 ZDOT = -4170
373692
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6309758
66 X = -1923214
44
Y = -17094649
03 feet Y = -5210449
03 meter
Z = -12519647
66 Z = -3815988
61
XDOT = 19820
613473 XDOT = 6041
322987
YDOT = 2702
096160 feet/sec YDOT = 823
598910 meter/sec
ZDOT = -13672
962456 ZDOT = -4167
518957
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 09139
52363583
00010596 00000-0 82463-4 0 9085
2 25544 51
6375 93
9357 0009679 19
5448 340
6083 15
72851395 1446
Satellite: ISS
Catalog Number: 25544
Epoch time: 09139
52363583 = yrday
fracday
Element set: 908
Inclination: 51
6375 deg
RA of node: 93
9357 deg
Eccentricity:
0009679
Arg of perigee: 19
5448 deg
Mean anomaly: 340
6083 deg
Mean motion: 15
72851395 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 144
Checksum: 341
Coasting Arc #10 (Orbit 159)
---------------------------------------
Vector Time (GMT): 2009/140/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 657345
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3200834
04 A = 6728828
29 meter
Y = -4442439
00 meter E =
0018326
Z = 3906827
91 I = 51
96794
XDOT = 3012
740846 Wp = 53
93773
YDOT = -5787
067061 meter/sec RA = 88
15152 deg
ZDOT = -4088
335492 TA = 78
55202
MA = 78
34625
Ha = 194
647 n
mi
Hp = 183
519
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10501424
02 X = -3169899
04
Y = -14574931
09 feet Y = -4478059
88 meter
Z = 12817676
86 Z = 3891352
84
XDOT = 9884
320360 XDOT = 3097
089635
YDOT = -18986
440490 feet/sec YDOT = -5752
904954 meter/sec
ZDOT = -13413
174186 ZDOT = -4073
494821
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17974188
50 X = -5478532
65
Y = 1092449
79 feet Y = 332978
69 meter
Z = 12756820
30 Z = 3888278
83
XDOT = -10585
282339 XDOT = -3226
394057
YDOT = -17290
115955 feet/sec YDOT = -5270
027343 meter/sec
ZDOT = -13355
395965 ZDOT = -4070
724690
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 09140
54021077
00010596 00000-0 82463-4 0 9099
2 25544 51
6379 88
7238 0009669 22
8658 337
2934 15
72870914 1602
Satellite: ISS
Catalog Number: 25544
Epoch time: 09140
54021077 = yrday
fracday
Element set: 909
Inclination: 51
6379 deg
RA of node: 88
7238 deg
Eccentricity:
0009669
Arg of perigee: 22
8658 deg
Mean anomaly: 337
2934 deg
Mean motion: 15
72870914 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 160
Checksum: 331
Coasting Arc #11 (Orbit 175)
---------------------------------------
Vector Time (GMT): 2009/141/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 657345
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1917100
80 A = 6730678
97 meter
Y = 5538786
90 meter E =
0019293
Z = 3284626
77 I = 51
97272
XDOT = -4270
050275 Wp = 62
17578
YDOT = -4307
250857 meter/sec RA = 83
09867 deg
ZDOT = 4758
698945 TA = 336
18547
MA = 336
27462
Ha = 194
702 n
mi
Hp = 183
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6289700
79 X = -1994850
44
Y = 18171873
04 feet Y = 5516913
78 meter
Z = 10776334
54 Z = 3275124
88
XDOT = -14009
351296 XDOT = -4244
685907
YDOT = -14131
400451 feet/sec YDOT = -4354
859614 meter/sec
ZDOT = 15612
529346 ZDOT = 4738
015855
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12174968
68 X = 3710930
46
Y = 14911114
18 feet Y = 4544907
60 meter
Z = 10739436
84 Z = 3273380
35
XDOT = -18328
577348 XDOT = -5586
550376
YDOT = 3750
153356 feet/sec YDOT = 1143
046743 meter/sec
ZDOT = 15531
293229 ZDOT = 4733
938176
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 09141
55677291
00010596 00000-0 82463-4 0 9108
2 25544 51
6384 83
5119 0009596 26
9166 333
2493 15
72888925 1761
Satellite: ISS
Catalog Number: 25544
Epoch time: 09141
55677291 = yrday
fracday
Element set: 910
Inclination: 51
6384 deg
RA of node: 83
5119 deg
Eccentricity:
0009596
Arg of perigee: 26
9166 deg
Mean anomaly: 333
2493 deg
Mean motion: 15
72888925 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 176
Checksum: 339
Coasting Arc #12 (Orbit 190)
---------------------------------------
Vector Time (GMT): 2009/142/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 657345
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4140998
45 A = 6727115
17 meter
Y = 3011237
64 meter E =
0014199
Z = -4371542
81 I = 51
95637
XDOT = -1304
187628 Wp = 68
44280
YDOT = 6757
871055 meter/sec RA = 77
94510 deg
ZDOT = 3433
555384 TA = 236
01980
MA = 236
15480
Ha = 194
767 n
mi
Hp = 183
233
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13585952
94 X = 4128255
19
Y = 9879388
59 feet Y = 3057473
92 meter
Z = -14342332
05 Z = -4351455
98
XDOT = -4278
830800 XDOT = -1396
338346
YDOT = 22171
492961 feet/sec YDOT = 6742
771261 meter/sec
ZDOT = 11264
945487 ZDOT = 3426
996365
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15451479
40 X = 4709610
92
Y = -6759219
37 feet Y = -2060210
07 meter
Z = -14263508
08 Z = -4347517
26
XDOT = 16402
023639 XDOT = 4999
336805
YDOT = 13873
767404 feet/sec YDOT = 4228
724305 meter/sec
ZDOT = 11239
624932 ZDOT = 3425
837679
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 09142
50978875
00010596 00000-0 82463-4 0 9117
2 25544 51
6388 78
6255 0009658 29
9961 330
1753 15
72897038 1913
Satellite: ISS
Catalog Number: 25544
Epoch time: 09142
50978875 = yrday
fracday
Element set: 911
Inclination: 51
6388 deg
RA of node: 78
6255 deg
Eccentricity:
0009658
Arg of perigee: 29
9961 deg
Mean anomaly: 330
1753 deg
Mean motion: 15
72897038 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 191
Checksum: 350
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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