Date:
June 25th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 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 678)
---------------------------------------
Vector Time (GMT): 2009/173/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -357740
72 A = 6731258
21 meter
Y = -6506111
97 meter E =
0010045
Z = -1698748
36 I = 51
33059
XDOT = 4878
589949 Wp = 92
70969
YDOT = -1745
320832 meter/sec RA = 278
89523 deg
ZDOT = 5685
593949 TA = 248
43908
MA = 248
54617
Ha = 192
950 n
mi
Hp = 181
673
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1173690
03 X = -276709
48
Y = -21345511
70 feet Y = -6509658
96 meter
Z = -5573321
40 Z = -1700290
98
XDOT = 16005
872535 XDOT = 4870
124257
YDOT = -5726
118216 feet/sec YDOT = -1690
814269 meter/sec
ZDOT = 18653
523455 ZDOT = 5709
273165
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21344842
72 X = -6505908
06
Y = 1155627
03 feet Y = 352235
12 meter
Z = -5579654
55 Z = -1700678
71
XDOT = -5652
170115 XDOT = -1722
781451
YDOT = -14336
958080 feet/sec YDOT = -4369
904823 meter/sec
ZDOT = 18746
249583 ZDOT = 5713
856873
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 09173
50332302
00010596 00000-0 82463-4 0 9008
2 25544 51
6432 279
6143 0008466 141
1119 219
0654 15
73877565 6790
Satellite: ISS
Catalog Number: 25544
Epoch time: 09173
50332302 = yrday
fracday
Element set: 900
Inclination: 51
6432 deg
RA of node: 279
6143 deg
Eccentricity:
0008466
Arg of perigee: 141
1119 deg
Mean anomaly: 219
0654 deg
Mean motion: 15
73877565 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 679
Checksum: 308
Coasting Arc #2 (Orbit 694)
---------------------------------------
Vector Time (GMT): 2009/174/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4121055
84 A = 6721596
64 meter
Y = 1888372
67 meter E =
0017862
Z = -4976909
81 I = 51
29475
XDOT = -1061
381373 Wp = 102
02022
YDOT = -7367
708991 meter/sec RA = 273
76920 deg
ZDOT = -1926
141442 TA = 149
30803
MA = 149
20343
Ha = 192
788 n
mi
Hp = 181
659
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13520524
42 X = -4117688
92
Y = 6195448
39 feet Y = 1842308
58 meter
Z = -16328444
26 Z = -4996921
14
XDOT = -3482
222351 XDOT = -969
558742
YDOT = -24172
273592 feet/sec YDOT = -7379
064129 meter/sec
ZDOT = -6319
361687 ZDOT = -1931
076246
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6434101
52 X = 1961114
14
Y = 13312612
49 feet Y = 4057684
29 meter
Z = -16406795
53 Z = -5000791
28
XDOT = -23136
179389 XDOT = -7051
907478
YDOT = 3407
743328 feet/sec YDOT = 1038
680166 meter/sec
ZDOT = -6339
038249 ZDOT = -1932
138858
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 09174
51921234
00010596 00000-0 82463-4 0 9019
2 25544 51
6430 274
3986 0008463 145
7570 214
4141 15
73906760 6951
Satellite: ISS
Catalog Number: 25544
Epoch time: 09174
51921234 = yrday
fracday
Element set: 901
Inclination: 51
6430 deg
RA of node: 274
3986 deg
Eccentricity:
0008463
Arg of perigee: 145
7570 deg
Mean anomaly: 214
4141 deg
Mean motion: 15
73906760 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 695
Checksum: 310
Coasting Arc #3 (Orbit 710)
---------------------------------------
Vector Time (GMT): 2009/175/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1499374
69 A = 6731149
41 meter
Y = 6331208
28 meter E =
0021803
Z = 1676624
94 I = 51
32560
XDOT = -4500
250649 Wp = 127
98889
YDOT = 2585
210077 meter/sec RA = 268
57983 deg
ZDOT = -5700
699039 TA = 33
37049
MA = 33
23325
Ha = 192
726 n
mi
Hp = 181
815
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4919208
31 X = 1420321
98
Y = 20771680
71 feet Y = 6347532
81 meter
Z = 5500738
00 Z = 1683718
10
XDOT = -14764
601868 XDOT = -4501
131836
YDOT = 8481
660356 feet/sec YDOT = 2534
881892 meter/sec
ZDOT = -18703
080835 ZDOT = -5722
562587
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20587620
70 X = 6275106
79
Y = -5612596
70 feet Y = -1710719
48 meter
Z = 5528840
77 Z = 1685190
67
XDOT = 8580
775357 XDOT = 2615
420329
YDOT = 12848
022740 feet/sec YDOT = 3916
077331 meter/sec
ZDOT = -18788
665023 ZDOT = -5726
785099
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 09175
53508682
00010596 00000-0 82463-4 0 9021
2 25544 51
6422 269
1831 0008546 148
5228 211
6448 15
73929388 7115
Satellite: ISS
Catalog Number: 25544
Epoch time: 09175
53508682 = yrday
fracday
Element set: 902
Inclination: 51
6422 deg
RA of node: 269
1831 deg
Eccentricity:
0008546
Arg of perigee: 148
5228 deg
Mean anomaly: 211
6448 deg
Mean motion: 15
73929388 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 711
Checksum: 326
Coasting Arc #4 (Orbit 726)
---------------------------------------
Vector Time (GMT): 2009/176/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3704467
48 A = 6721359
06 meter
Y = -2602927
72 meter E =
0013752
Z = 4963416
22 I = 51
29537
XDOT = 2367
612162 Wp = 141
10723
YDOT = 7073
436905 meter/sec RA = 263
45261 deg
ZDOT = 1928
931516 TA = 290
10616
MA = 290
25410
Ha = 192
443 n
mi
Hp = 181
897
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12153764
71 X = 3709187
52
Y = -8539789
11 feet Y = -2561476
68 meter
Z = 16284173
95 Z = 4981423
26
XDOT = 7767
756437 XDOT = 2278
969565
YDOT = 23206
813992 feet/sec YDOT = 7099
416961 meter/sec
ZDOT = 6328
515471 ZDOT = 1940
219142
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9157956
52 X = -2791345
15
Y = -11596286
90 feet Y = -3534548
25 meter
Z = 16354640
88 Z = 4984894
54
XDOT = 21925
643479 XDOT = 6682
936132
YDOT = -8265
141834 feet/sec YDOT = -2519
215231 meter/sec
ZDOT = 6373
112563 ZDOT = 1942
524709
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 09176
55094344
00010596 00000-0 82463-4 0 9030
2 25544 51
6423 263
9664 0008372 152
6816 207
4789 15
73996935 7278
Satellite: ISS
Catalog Number: 25544
Epoch time: 09176
55094344 = yrday
fracday
Element set: 903
Inclination: 51
6423 deg
RA of node: 263
9664 deg
Eccentricity:
0008372
Arg of perigee: 152
6816 deg
Mean anomaly: 207
4789 deg
Mean motion: 15
73996935 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 727
Checksum: 348
Coasting Arc #5 (Orbit 741)
---------------------------------------
Vector Time (GMT): 2009/177/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2609412
59 A = 6731044
63 meter
Y = -5977706
89 meter E =
0008187
Z = -1673049
28 I = 51
33167
XDOT = 3965
390992 Wp = 98
88361
YDOT = -3318
679657 meter/sec RA = 258
26278 deg
ZDOT = 5695
232935 TA = 242
56069
MA = 242
64398
Ha = 192
433 n
mi
Hp = 182
125
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8561064
93 X = -2534247
66
Y = -19611899
25 feet Y = -6006466
35 meter
Z = -5489006
82 Z = -1685543
94
XDOT = 13009
812967 XDOT = 3974
540288
YDOT = -10888
056619 feet/sec YDOT = -3274
286025 meter/sec
ZDOT = 18685
147423 ZDOT = 5714
518273
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18972561
39 X = -5782836
71
Y = 9869995
26 feet Y = 3008374
55 meter
Z = -5538296
55 Z = -1688072
79
XDOT = -11037
365355 XDOT = -3364
188960
YDOT = -10730
569439 feet/sec YDOT = -3270
677565 meter/sec
ZDOT = 18760
589460 ZDOT = 5718
227667
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 09177
50329778
00010596 00000-0 82463-4 0 9049
2 25544 51
6416 259
0765 0008117 155
5925 204
5624 15
73959243 7422
Satellite: ISS
Catalog Number: 25544
Epoch time: 09177
50329778 = yrday
fracday
Element set: 904
Inclination: 51
6416 deg
RA of node: 259
0765 deg
Eccentricity:
0008117
Arg of perigee: 155
5925 deg
Mean anomaly: 204
5624 deg
Mean motion: 15
73959243 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 742
Checksum: 331
Coasting Arc #6 (Orbit 757)
---------------------------------------
Vector Time (GMT): 2009/178/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3222576
01 A = 6721292
47 meter
Y = 3157993
75 meter E =
0016275
Z = -4993958
86 I = 51
30531
XDOT = -3551
423754 Wp = 106
03189
YDOT = -6561
050464 meter/sec RA = 253
13528 deg
ZDOT = -1866
718228 TA = 145
90120
MA = 145
79653
Ha = 192
278 n
mi
Hp = 182
132
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10572755
93 X = -3233390
23
Y = 10360871
89 feet Y = 3121897
20 meter
Z = -16384379
46 Z = -5009639
83
XDOT = -11651
652737 XDOT = -3468
724939
YDOT = -21525
756117 feet/sec YDOT = -6600
301927 meter/sec
ZDOT = -6124
403634 ZDOT = -1883
770842
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11228749
28 X = 3422522
78
Y = 9541120
54 feet Y = 2908133
54 meter
Z = -16445696
49 Z = -5012648
29
XDOT = -19743
671766 XDOT = -6017
871154
YDOT = 12617
018546 feet/sec YDOT = 3845
667253 meter/sec
ZDOT = -6191
606264 ZDOT = -1887
201589
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 09178
51912734
00010596 00000-0 82463-4 0 9052
2 25544 51
6406 253
8596 0008189 159
7073 200
4417 15
73993255 7587
Satellite: ISS
Catalog Number: 25544
Epoch time: 09178
51912734 = yrday
fracday
Element set: 905
Inclination: 51
6406 deg
RA of node: 253
8596 deg
Eccentricity:
0008189
Arg of perigee: 159
7073 deg
Mean anomaly: 200
4417 deg
Mean motion: 15
73993255 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 758
Checksum: 339
Coasting Arc #7 (Orbit 773)
---------------------------------------
Vector Time (GMT): 2009/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3587364
08 A = 6730910
88 meter
Y = 5451606
68 meter E =
0020581
Z = 1597923
95 I = 51
34823
XDOT = -3365
167562 Wp = 132
98988
YDOT = 3904
291393 meter/sec RA = 247
94658 deg
ZDOT = -5732
773621 TA = 29
27998
MA = 29
16479
Ha = 192
084 n
mi
Hp = 182
265
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11769567
18 X = 3518374
29
Y = 17885848
68 feet Y = 5491336
74 meter
Z = 5242532
66 Z = 1615184
35
XDOT = -11040
575992 XDOT = -3380
727300
YDOT = 12809
354965 feet/sec YDOT = 3866
573818 meter/sec
ZDOT = -18808
312406 ZDOT = -5749
158828
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16572224
83 X = 5051214
13
Y = -13530350
55 feet Y = -4124050
85 meter
Z = 5310501
04 Z = 1618640
72
XDOT = 12886
851490 XDOT = 3927
912334
YDOT = 8335
480660 feet/sec YDOT = 2540
654505 meter/sec
ZDOT = -18872
349808 ZDOT = -5752
292222
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 09179
53494207
00010596 00000-0 82463-4 0 9066
2 25544 51
6407 248
6427 0008062 162
1216 198
0232 15
74046642 7745
Satellite: ISS
Catalog Number: 25544
Epoch time: 09179
53494207 = yrday
fracday
Element set: 906
Inclination: 51
6407 deg
RA of node: 248
6427 deg
Eccentricity:
0008062
Arg of perigee: 162
1216 deg
Mean anomaly: 198
0232 deg
Mean motion: 15
74046642 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 774
Checksum: 311
Coasting Arc #8 (Orbit 789)
---------------------------------------
Vector Time (GMT): 2009/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2637156
88 A = 6721001
95 meter
Y = -3628983
43 meter E =
0012696
Z = 5002277
82 I = 51
32740
XDOT = 4641
283548 Wp = 149
96936
YDOT = 5877
335805 meter/sec RA = 242
81918 deg
ZDOT = 1804
143085 TA = 282
50298
MA = 282
64499
Ha = 191
932 n
mi
Hp = 182
412
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8652089
49 X = 2653240
67
Y = -11906113
62 feet Y = -3599403
89 meter
Z = 16411672
65 Z = 5015127
72
XDOT = 15227
308229 XDOT = 4566
453046
YDOT = 19282
597784 feet/sec YDOT = 5928
818729 meter/sec
ZDOT = 5919
104611 ZDOT = 1826
509367
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12852208
75 X = -3917353
23
Y = -7055848
57 feet Y = -2150622
64 meter
Z = 16461862
73 Z = 5017575
76
XDOT = 16791
866943 XDOT = 5118
161044
YDOT = -16473
393936 feet/sec YDOT = -5021
090472 meter/sec
ZDOT = 6007
123772 ZDOT = 1830
971326
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 09180
55074150
00010596 00000-0 82463-4 0 9072
2 25544 51
6407 243
4255 0008033 166
7341 193
4035 15
74073720 7909
Satellite: ISS
Catalog Number: 25544
Epoch time: 09180
55074150 = yrday
fracday
Element set: 907
Inclination: 51
6407 deg
RA of node: 243
4255 deg
Eccentricity:
0008033
Arg of perigee: 166
7341 deg
Mean anomaly: 193
4035 deg
Mean motion: 15
74073720 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 790
Checksum: 291
Coasting Arc #9 (Orbit 804)
---------------------------------------
Vector Time (GMT): 2009/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4483632
55 A = 6730953
21 meter
Y = -4782596
70 meter E =
0006483
Z = -1535273
46 I = 51
37503
XDOT = 2680
346664 Wp = 101
00044
YDOT = -4352
253540 meter/sec RA = 237
63270 deg
ZDOT = 5749
497060 TA = 242
02967
MA = 242
09530
Ha = 191
872 n
mi
Hp = 182
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14710080
55 X = -4422361
42
Y = -15690934
07 feet Y = -4832392
51 meter
Z = -5036986
41 Z = -1556906
80
XDOT = 8793
788268 XDOT = 2700
885041
YDOT = -14279
047048 feet/sec YDOT = -4322
166278 meter/sec
ZDOT = 18863
179330 ZDOT = 5762
567502
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13517542
87 X = -4120147
07
Y = 16703396
55 feet Y = 5091195
27 meter
Z = -5122078
88 Z = -1561209
64
XDOT = -14121
450142 XDOT = -4304
218003
YDOT = -5647
152520 feet/sec YDOT = -1721
252088 meter/sec
ZDOT = 18914
196347 ZDOT = 5765
047046
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 09181
50304217
00010596 00000-0 82463-4 0 9089
2 25544 51
6401 238
5344 0007828 169
5143 190
6185 15
74054369 8059
Satellite: ISS
Catalog Number: 25544
Epoch time: 09181
50304217 = yrday
fracday
Element set: 908
Inclination: 51
6401 deg
RA of node: 238
5344 deg
Eccentricity:
0007828
Arg of perigee: 169
5143 deg
Mean anomaly: 190
6185 deg
Mean motion: 15
74054369 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 805
Checksum: 308
Coasting Arc #10 (Orbit 820)
---------------------------------------
Vector Time (GMT): 2009/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2058958
75 A = 6720829
27 meter
Y = 3945439
94 meter E =
0014963
Z = -5047194
30 I = 51
35830
XDOT = -5561
124980 Wp = 109
02122
YDOT = -5041
038226 meter/sec RA = 232
50529 deg
ZDOT = -1680
875392 TA = 144
78106
MA = 144
68208
Ha = 191
728 n
mi
Hp = 182
641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6755114
01 X = -2078405
87
Y = 12944356
77 feet Y = 3922307
50 meter
Z = -16559036
42 Z = -5057243
39
XDOT = -18245
160697 XDOT = -5496
176505
YDOT = -16538
839323 feet/sec YDOT = -5102
862576 meter/sec
ZDOT = -5514
683045 ZDOT = -1707
734430
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13819113
47 X = 4212065
79
Y = 4573891
28 feet Y = 1394122
06 meter
Z = -16598230
21 Z = -5059140
57
XDOT = -13185
354944 XDOT = -4018
896187
YDOT = 19546
681345 feet/sec YDOT = 5957
828474 meter/sec
ZDOT = -5620
289681 ZDOT = -1713
064295
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 09182
51881553
00010596 00000-0 82463-4 0 9095
2 25544 51
6404 233
3168 0007895 172
9350 187
1926 15
74082893 8216
Satellite: ISS
Catalog Number: 25544
Epoch time: 09182
51881553 = yrday
fracday
Element set: 909
Inclination: 51
6404 deg
RA of node: 233
3168 deg
Eccentricity:
0007895
Arg of perigee: 172
9350 deg
Mean anomaly: 187
1926 deg
Mean motion: 15
74082893 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 821
Checksum: 331
Coasting Arc #11 (Orbit 836)
---------------------------------------
Vector Time (GMT): 2009/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5214346
35 A = 6730869
29 meter
Y = 3996399
91 meter E =
0019342
Z = 1409295
39 I = 51
41206
XDOT = -1998
066481 Wp = 138
75474
YDOT = 4664
330612 meter/sec RA = 227
32335 deg
ZDOT = -5803
312312 TA = 25
68011
MA = 25
58419
Ha = 191
466 n
mi
Hp = 182
771
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17107435
53 X = 5162424
26
Y = 13111548
25 feet Y = 4054419
22 meter
Z = 4623672
55 Z = 1434501
33
XDOT = -6555
336225 XDOT = -2021
883803
YDOT = 15302
921954 feet/sec YDOT = 4641
854886 meter/sec
ZDOT = -19039
738556 ZDOT = -5813
076003
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9981607
33 X = 3042393
91
Y = -19079270
38 feet Y = -5815361
61 meter
Z = 4722748
44 Z = 1439493
73
XDOT = 14791
093451 XDOT = 4508
325284
YDOT = 2991
354078 feet/sec YDOT = 911
764723 meter/sec
ZDOT = -19077
777140 ZDOT = -5814
906472
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 09183
53457366
00010596 00000-0 82463-4 0 9101
2 25544 51
6405 228
0997 0007705 176
1115 184
0109 15
74144949 8370
Satellite: ISS
Catalog Number: 25544
Epoch time: 09183
53457366 = yrday
fracday
Element set: 910
Inclination: 51
6405 deg
RA of node: 228
0997 deg
Eccentricity:
0007705
Arg of perigee: 176
1115 deg
Mean anomaly: 184
0109 deg
Mean motion: 15
74144949 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 837
Checksum: 321
Coasting Arc #12 (Orbit 852)
---------------------------------------
Vector Time (GMT): 2009/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1428421
34 A = 6720505
49 meter
Y = -4170403
36 meter E =
0011383
Z = 5071667
58 I = 51
39738
XDOT = 6346
229435 Wp = 159
04111
YDOT = 4078
414600 meter/sec RA = 222
19721 deg
ZDOT = 1554
705703 TA = 275
92553
MA = 276
05526
Ha = 191
417 n
mi
Hp = 182
899
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4686421
72 X = 1450312
08
Y = -13682425
72 feet Y = -4154308
47 meter
Z = 16639329
32 Z = 5078659
25
XDOT = 20820
962713 XDOT = 6292
599759
YDOT = 13380
625327 feet/sec YDOT = 4149
081697 meter/sec
ZDOT = 5100
740495 ZDOT = 1585
406212
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14302499
45 X = -4359401
83
Y = -1924586
15 feet Y = -586613
86 meter
Z = 16666525
73 Z = 5079957
04
XDOT = 9075
435127 XDOT = 2766
192627
YDOT = -21899
969212 feet/sec YDOT = -6675
110616 meter/sec
ZDOT = 5221
383907 ZDOT = 1591
477815
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 09184
55031877
00010596 00000-0 82463-4 0 9110
2 25544 51
6396 222
8826 0007737 179
3325 180
7850 15
74152485 8533
Satellite: ISS
Catalog Number: 25544
Epoch time: 09184
55031877 = yrday
fracday
Element set: 911
Inclination: 51
6396 deg
RA of node: 222
8826 deg
Eccentricity:
0007737
Arg of perigee: 179
3325 deg
Mean anomaly: 180
7850 deg
Mean motion: 15
74152485 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 853
Checksum: 333
Coasting Arc #13 (Orbit 867)
---------------------------------------
Vector Time (GMT): 2009/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5829941
10 A = 6730898
25 meter
Y = -3109832
78 meter E =
0005033
Z = -1289293
40 I = 51
45611
XDOT = 1297
605018 Wp = 97
14115
YDOT = -4843
987438 meter/sec RA = 217
01967 deg
ZDOT = 5835
229128 TA = 248
68522
MA = 248
73896
Ha = 191
270 n
mi
Hp = 183
023
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19127103
35 X = -5788469
99
Y = -10202863
45 feet Y = -3174794
46 meter
Z = -4229965
21 Z = -1317515
07
XDOT = 4257
234310 XDOT = 1323
328456
YDOT = -15892
347239 feet/sec YDOT = -4829
334188 meter/sec
ZDOT = 19144
452520 ZDOT = 5841
594402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6057136
49 X = -1846215
20
Y = 20791951
74 feet Y = 6337386
89 meter
Z = -4340846
84 Z = -1323090
12
XDOT = -14888
726158 XDOT = -4538
083733
YDOT = -347
930381 feet/sec YDOT = -106
049180 meter/sec
ZDOT = 19169
157075 ZDOT = 5842
759076
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 09185
50256731
00010596 00000-0 82463-4 0 9125
2 25544 51
6400 217
9912 0007679 182
9280 177
1839 15
74178616 8682
Satellite: ISS
Catalog Number: 25544
Epoch time: 09185
50256731 = yrday
fracday
Element set: 912
Inclination: 51
6400 deg
RA of node: 217
9912 deg
Eccentricity:
0007679
Arg of perigee: 182
9280 deg
Mean anomaly: 177
1839 deg
Mean motion: 15
74178616 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 868
Checksum: 337
Coasting Arc #14 (Orbit 883)
---------------------------------------
Vector Time (GMT): 2009/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -860355
20 A = 6720256
12 meter
Y = 4274457
90 meter E =
0013781
Z = -5123766
30 I = 51
44464
XDOT = -6936
849902 Wp = 111
57102
YDOT = -3029
882072 meter/sec RA = 211
89330 deg
ZDOT = -1370
787537 TA = 145
30264
MA = 145
21267
Ha = 191
122 n
mi
Hp = 183
215
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2822687
67 X = -883198
81
Y = 14023812
00 feet Y = 4264710
21 meter
Z = -16810256
88 Z = -5128000
50
XDOT = -22758
693905 XDOT = -6895
794689
YDOT = -9940
557979 feet/sec YDOT = -3107
224156 meter/sec
ZDOT = -4497
334438 ZDOT = -1404
387432
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14278310
66 X = 4352029
09
Y = -462455
80 feet Y = -140956
53 meter
Z = -16826633
18 Z = -5128757
79
XDOT = -4669
194616 XDOT = -1423
170519
YDOT = 23332
577360 feet/sec YDOT = 7111
769579 meter/sec
ZDOT = -4629
328503 ZDOT = -1411
019328
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 09186
51828507
00010596 00000-0 82463-4 0 9134
2 25544 51
6400 212
7734 0007656 187
0424 173
0633 15
74174657 8844
Satellite: ISS
Catalog Number: 25544
Epoch time: 09186
51828507 = yrday
fracday
Element set: 913
Inclination: 51
6400 deg
RA of node: 212
7734 deg
Eccentricity:
0007656
Arg of perigee: 187
0424 deg
Mean anomaly: 173
0633 deg
Mean motion: 15
74174657 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 884
Checksum: 318
Coasting Arc #15 (Orbit 899)
---------------------------------------
Vector Time (GMT): 2009/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6263942
81 A = 6731018
56 meter
Y = 2163794
31 meter E =
0018167
Z = 1111509
32 I = 51
50586
XDOT = -648
655464 Wp = 145
45354
YDOT = 4922
936511 meter/sec RA = 206
72192 deg
ZDOT = -5895
915204 TA = 22
34553
MA = 22
26648
Ha = 190
932 n
mi
Hp = 183
325
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20550993
49 X = 6233881
89
Y = 7099062
69 feet Y = 2233673
08 meter
Z = 3646684
13 Z = 1141866
66
XDOT = -2128
134724 XDOT = -675
015380
YDOT = 16151
366505 feet/sec YDOT = 4915
536644 meter/sec
ZDOT = -19343
553820 ZDOT = -5899
129396
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1983278
37 X = 604503
25
Y = -21631521
88 feet Y = -6593287
87 meter
Z = 3765925
83 Z = 1147854
19
XDOT = 14586
986293 XDOT = 4446
113422
YDOT = -2050
121347 feet/sec YDOT = -624
876987 meter/sec
ZDOT = -19355
890819 ZDOT = -5899
675522
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 09187
53398895
00010596 00000-0 82463-4 0 9140
2 25544 51
6386 207
5555 0007557 189
9194 170
1821 15
74207851 9004
Satellite: ISS
Catalog Number: 25544
Epoch time: 09187
53398895 = yrday
fracday
Element set: 914
Inclination: 51
6386 deg
RA of node: 207
5555 deg
Eccentricity:
0007557
Arg of perigee: 189
9194 deg
Mean anomaly: 170
1821 deg
Mean motion: 15
74207851 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 900
Checksum: 344
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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