Date:
July 2nd 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5381 96 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 82 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 ET - UTC (sec) : 65 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 1239)
---------------------------------------
Vector Time (GMT): 2007/178/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5227037
68 A = 6717693
12 meter
Y = -3610416
57 meter E =
0014215
Z = 2178947
02 I = 51
89499
XDOT = 1289
553197 Wp = 75
69846
YDOT = -5218
445385 meter/sec RA = 50
23779 deg
ZDOT = -5520
008633 TA = 79
95138
MA = 79
79102
Ha = 185
152 n
mi
Hp = 176
274
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17149073
74 X = -5196861
96
Y = -11845198
72 feet Y = -3668699
96 meter
Z = 7148776
30 Z = 2153626
49
XDOT = 4230
817574 XDOT = 1374
626108
YDOT = -17120
883810 feet/sec YDOT = -5203
548081 meter/sec
ZDOT = -18110
264543 ZDOT = -5513
538376
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14793980
90 X = -4509205
38
Y = 14727615
73 feet Y = 4488977
27 meter
Z = 7052654
08 Z = 2149648
96
XDOT = -14963
354364 XDOT = -4560
830410
YDOT = -6316
797025 feet/sec YDOT = -1925
359733 meter/sec
ZDOT = -18086
351519 ZDOT = -5512
719943
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 07178
49427289
00020000 00000-0 20000-3 0 9007
2 25544 51
6351 50
6458 0008166 3
6630 356
4593 15
78392080 12405
Satellite: ISS
Catalog Number: 25544
Epoch time: 07178
49427289 = yrday
fracday
Element set: 900
Inclination: 51
6351 deg
RA of node: 50
6458 deg
Eccentricity:
0008166
Arg of perigee: 3
6630 deg
Mean anomaly: 356
4593 deg
Mean motion: 15
78392080 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1240
Checksum: 294
Coasting Arc #2 (Orbit 1255)
---------------------------------------
Vector Time (GMT): 2007/179/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2224419
38 A = 6707666
52 meter
Y = 3575447
96 meter E =
0007534
Z = 5217233
85 I = 51
84272
XDOT = -5872
881015 Wp = 29
34140
YDOT = -4921
707958 meter/sec RA = 45
11125 deg
ZDOT = 874
871993 TA = 52
39802
MA = 52
32964
Ha = 185
237 n
mi
Hp = 175
981
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7297963
86 X = -2289579
66
Y = 11730472
30 feet Y = 3550207
77 meter
Z = 17116908
96 Z = 5206270
11
XDOT = -19267
982332 XDOT = -5821
659246
YDOT = -16147
335821 feet/sec YDOT = -4987
095606 meter/sec
ZDOT = 2870
314938 ZDOT = 846
464812
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10337714
46 X = 3150935
37
Y = 9241248
80 feet Y = 2816732
64 meter
Z = 17075825
29 Z = 5204711
55
XDOT = -18455
151654 XDOT = -5625
130224
YDOT = 15576
489643 feet/sec YDOT = 4747
714043 meter/sec
ZDOT = 2762
382125 ZDOT = 841
974072
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 07179
50725348
00020000 00000-0 20000-3 0 9018
2 25544 51
6355 45
4085 0008262 6
4303 353
6967 15
78452016 12569
Satellite: ISS
Catalog Number: 25544
Epoch time: 07179
50725348 = yrday
fracday
Element set: 901
Inclination: 51
6355 deg
RA of node: 45
4085 deg
Eccentricity:
0008262
Arg of perigee: 6
4303 deg
Mean anomaly: 353
6967 deg
Mean motion: 15
78452016 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1256
Checksum: 289
Coasting Arc #3 (Orbit 1271)
---------------------------------------
Vector Time (GMT): 2007/180/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4731479
03 A = 6719224
78 meter
Y = 4699365
94 meter E =
0020342
Z = 717853
50 I = 51
86038
XDOT = -3841
828110 Wp = 36
07322
YDOT = 2939
224125 meter/sec RA = 39
95616 deg
ZDOT = 6011
390598 TA = 331
74782
MA = 331
85801
Ha = 185
207 n
mi
Hp = 175
783
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15523225
18 X = 4675091
19
Y = 15417867
25 feet Y = 4751960
55 meter
Z = 2355162
39 Z = 740703
08
XDOT = -12604
422933 XDOT = -3903
611577
YDOT = 9643
123769 feet/sec YDOT = 2895
915822 meter/sec
ZDOT = 19722
410099 ZDOT = 5992
577644
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17560571
24 X = 5352462
11
Y = -13034209
90 feet Y = -3972827
18 meter
Z = 2442058
70 Z = 744339
49
XDOT = 6686
334928 XDOT = 2037
994886
YDOT = 12731
233346 feet/sec YDOT = 3880
479924 meter/sec
ZDOT = 19651
571946 ZDOT = 5989
799129
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 07180
52021685
00020000 00000-0 20000-3 0 9026
2 25544 51
6353 40
1711 0008326 9
3080 350
8238 15
78483011 12727
Satellite: ISS
Catalog Number: 25544
Epoch time: 07180
52021685 = yrday
fracday
Element set: 902
Inclination: 51
6353 deg
RA of node: 40
1711 deg
Eccentricity:
0008326
Arg of perigee: 9
3080 deg
Mean anomaly: 350
8238 deg
Mean motion: 15
78483011 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1272
Checksum: 255
Coasting Arc #4 (Orbit 1286)
---------------------------------------
Vector Time (GMT): 2007/181/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4419060
39 A = 6709352
96 meter
Y = -1544642
56 meter E =
0013761
Z = -4815697
27 I = 51
80366
XDOT = 4654
589536 Wp = 70
46513
YDOT = 5609
372047 meter/sec RA = 34
77252 deg
ZDOT = 2482
226200 TA = 223
69676
MA = 223
80578
Ha = 185
291 n
mi
Hp = 175
710
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14498229
64 X = 4459397
98
Y = -5067724
93 feet Y = -1494999
51 meter
Z = -15799531
74 Z = -4794132
01
XDOT = 15270
963046 XDOT = 4579
460667
YDOT = 18403
451597 feet/sec YDOT = 5661
001644 meter/sec
ZDOT = 8143
786747 ZDOT = 2504
656824
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3093931
20 X = -943030
23
Y = -15128567
15 feet Y = -4611187
27 meter
Z = -15718134
36 Z = -4790887
35
XDOT = 19152
264632 XDOT = 5837
610260
YDOT = -12431
692349 feet/sec YDOT = -3789
179828 meter/sec
ZDOT = 8229
196874 ZDOT = 2508
259207
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 07181
46985408
00020000 00000-0 20000-3 0 9033
2 25544 51
6347 35
2607 0008345 12
2318 347
9049 15
78508125 12874
Satellite: ISS
Catalog Number: 25544
Epoch time: 07181
46985408 = yrday
fracday
Element set: 903
Inclination: 51
6347 deg
RA of node: 35
2607 deg
Eccentricity:
0008345
Arg of perigee: 12
2318 deg
Mean anomaly: 347
9049 deg
Mean motion: 15
78508125 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1287
Checksum: 299
Coasting Arc #5 (Orbit 1302)
---------------------------------------
Vector Time (GMT): 2007/182/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3079629
47 A = 6714129
55 meter
Y = -4878076
03 meter E =
0011050
Z = -3449561
32 I = 51
79488
XDOT = 6151
813607 Wp = 40
60400
YDOT = -645
024717 meter/sec RA = 29
65932 deg
ZDOT = -4579
902675 TA = 180
17196
MA = 180
17234
Ha = 185
299 n
mi
Hp = 175
468
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10103771
22 X = -3008096
09
Y = -16004186
44 feet Y = -4912113
46 meter
Z = -11317458
39 Z = -3464349
29
XDOT = 20183
115508 XDOT = 6180
817212
YDOT = -2116
222825 feet/sec YDOT = -576
068518 meter/sec
ZDOT = -15025
927410 ZDOT = -4549
947220
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17054176
67 X = -5198113
05
Y = 8129861
97 feet Y = 2477981
93 meter
Z = -11373893
06 Z = -3466762
60
XDOT = 825
334076 XDOT = 251
561826
YDOT = -19132
169608 feet/sec YDOT = -5831
485296 meter/sec
ZDOT = -14912
698897 ZDOT = -4545
390624
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 07182
48278287
00020000 00000-0 20000-3 0 9047
2 25544 51
6341 30
0231 0008295 15
2913 344
8502 15
78509884 13034
Satellite: ISS
Catalog Number: 25544
Epoch time: 07182
48278287 = yrday
fracday
Element set: 904
Inclination: 51
6341 deg
RA of node: 30
0231 deg
Eccentricity:
0008295
Arg of perigee: 15
2913 deg
Mean anomaly: 344
8502 deg
Mean motion: 15
78509884 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1303
Checksum: 283
Coasting Arc #6 (Orbit 1318)
---------------------------------------
Vector Time (GMT): 2007/183/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6077651
98 A = 6715725
75 meter
Y = -311027
75 meter E =
0017106
Z = 2834230
39 I = 51
77530
XDOT = -2117
638662 Wp = 69
94516
YDOT = -5375
721239 meter/sec RA = 24
44899 deg
ZDOT = -5100
459406 TA = 77
54719
MA = 77
35583
Ha = 185
370 n
mi
Hp = 175
237
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19939803
07 X = -6087490
27
Y = -1020432
24 feet Y = -379047
04 meter
Z = 9298656
14 Z = 2804681
66
XDOT = -6947
633407 XDOT = -2032
592459
YDOT = -17636
880707 feet/sec YDOT = -5398
925333 meter/sec
ZDOT = -16733
790703 ZDOT = -5110
541228
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2976475
11 X = -907229
61
Y = 19795055
30 feet Y = 6033532
86 meter
Z = 9186861
05 Z = 2800155
25
XDOT = -16780
583053 XDOT = -5114
721715
YDOT = 5307
860348 feet/sec YDOT = 1617
835834 meter/sec
ZDOT = -16772
481700 ZDOT = -5112
252422
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 07183
49569272
00020000 00000-0 20000-3 0 9057
2 25544 51
6344 24
7848 0008505 18
9262 341
2218 15
78590101 13196
Satellite: ISS
Catalog Number: 25544
Epoch time: 07183
49569272 = yrday
fracday
Element set: 905
Inclination: 51
6344 deg
RA of node: 24
7848 deg
Eccentricity:
0008505
Arg of perigee: 18
9262 deg
Mean anomaly: 341
2218 deg
Mean motion: 15
78590101 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1319
Checksum: 295
Coasting Arc #7 (Orbit 1334)
---------------------------------------
Vector Time (GMT): 2007/184/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 418568
36 A = 6708019
28 meter
Y = 4376988
41 meter E =
0008807
Z = 5058540
84 I = 51
72136
XDOT = -7434
469751 Wp = 56
29672
YDOT = -1212
643555 meter/sec RA = 19
32266 deg
ZDOT = 1667
165409 TA = 17
74016
MA = 17
70943
Ha = 185
478 n
mi
Hp = 175
085
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1373255
79 X = 345020
08
Y = 14360198
18 feet Y = 4381256
97 meter
Z = 16596262
61 Z = 5060396
32
XDOT = -24391
304957 XDOT = -7428
455897
YDOT = -3978
489354 feet/sec YDOT = -1295
746633 meter/sec
ZDOT = 5469
702786 ZDOT = 1631
063768
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14416658
17 X = 4394197
41
Y = -113569
50 feet Y = -34615
98 meter
Z = 16603738
28 Z = 5060819
43
XDOT = -5950
784764 XDOT = -1813
799196
YDOT = 22968
031690 feet/sec YDOT = 7000
656059 meter/sec
ZDOT = 5333
023425 ZDOT = 1625
505540
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 07184
50858692
00020000 00000-0 20000-3 0 9068
2 25544 51
6335 19
5461 0008428 23
2509 336
9036 15
78552569 13359
Satellite: ISS
Catalog Number: 25544
Epoch time: 07184
50858692 = yrday
fracday
Element set: 906
Inclination: 51
6335 deg
RA of node: 19
5461 deg
Eccentricity:
0008428
Arg of perigee: 23
2509 deg
Mean anomaly: 336
9036 deg
Mean motion: 15
78552569 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1335
Checksum: 309
Coasting Arc #8 (Orbit 1350)
---------------------------------------
Vector Time (GMT): 2007/185/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6493175
64 A = 6719120
13 meter
Y = 1683328
48 meter E =
0020555
Z = 57798
32 I = 51
73067
XDOT = -1258
877698 Wp = 37
59294
YDOT = 4610
031131 meter/sec RA = 14
14426 deg
ZDOT = 6056
528863 TA = 323
03587
MA = 323
17733
Ha = 185
440 n
mi
Hp = 174
904
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21303069
70 X = 6473589
06
Y = 5522731
23 feet Y = 1755829
29 meter
Z = 189627
05 Z = 89294
34
XDOT = -4130
176176 XDOT = -1339
755227
YDOT = 15124
774053 feet/sec YDOT = 4595
500564 meter/sec
ZDOT = 19870
501518 ZDOT = 6050
217554
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6870494
10 X = 2094126
60
Y = -20905936
13 feet Y = -6372129
33 meter
Z = 308937
73 Z = 94164
22
XDOT = 13298
814375 XDOT = 4053
478622
YDOT = 4696
672361 feet/sec YDOT = 1431
545736 meter/sec
ZDOT = 19847
113907 ZDOT = 6049
400319
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 07185
52146046
00020000 00000-0 20000-3 0 9075
2 25544 51
6327 14
3073 0008384 26
0391 334
1195 15
78603774 13512
Satellite: ISS
Catalog Number: 25544
Epoch time: 07185
52146046 = yrday
fracday
Element set: 907
Inclination: 51
6327 deg
RA of node: 14
3073 deg
Eccentricity:
0008384
Arg of perigee: 26
0391 deg
Mean anomaly: 334
1195 deg
Mean motion: 15
78603774 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1351
Checksum: 279
Coasting Arc #9 (Orbit 1365)
---------------------------------------
Vector Time (GMT): 2007/186/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2617709
31 A = 6708051
58 meter
Y = -3609829
53 meter E =
0017526
Z = -5024893
41 I = 51
66445
XDOT = 7023
253541 Wp = 76
27956
YDOT = 2567
361592 meter/sec RA = 8
96033 deg
ZDOT = 1823
756897 TA = 211
25049
MA = 211
35480
Ha = 185
447 n
mi
Hp = 174
775
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8588285
15 X = 2682290
12
Y = -11843272
74 feet Y = -3580195
13 meter
Z = -16485870
78 Z = -5012020
32
XDOT = 23042
170411 XDOT = 6985
163577
YDOT = 8423
102335 feet/sec YDOT = 2645
686362 meter/sec
ZDOT = 5983
454385 ZDOT = 1857
783234
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11425626
28 X = -3482530
89
Y = -9223196
87 feet Y = -2811230
41 meter
Z = -16437560
34 Z = -5010168
39
XDOT = 8814
065124 XDOT = 2686
527050
YDOT = -21757
404049 feet/sec YDOT = -6631
656754 meter/sec
ZDOT = 6112
429627 ZDOT = 1863
068550
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 07186
47101364
00020000 00000-0 20000-3 0 9085
2 25544 51
6319 9
3955 0008347 30
0032 330
1610 15
78640389 13669
Satellite: ISS
Catalog Number: 25544
Epoch time: 07186
47101364 = yrday
fracday
Element set: 908
Inclination: 51
6319 deg
RA of node: 9
3955 deg
Eccentricity:
0008347
Arg of perigee: 30
0032 deg
Mean anomaly: 330
1610 deg
Mean motion: 15
78640389 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1366
Checksum: 276
Coasting Arc #10 (Orbit 1381)
---------------------------------------
Vector Time (GMT): 2007/187/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5355203
28 A = 6714906
16 meter
Y = -2737458
12 meter E =
0010566
Z = -3001017
42 I = 51
65922
XDOT = 4631
573741 Wp = 57
26422
YDOT = -3625
396605 meter/sec RA = 3
83109 deg
ZDOT = -4964
864891 TA = 157
43376
MA = 157
38726
Ha = 185
475 n
mi
Hp = 174
478
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17569564
58 X = -5309616
33
Y = -8981161
82 feet Y = -2797087
79 meter
Z = -9845857
67 Z = -3026922
38
XDOT = 15195
451905 XDOT = 4695
887461
YDOT = -11894
345816 feet/sec YDOT = -3573
243589 meter/sec
ZDOT = -16288
926809 ZDOT = -4942
209066
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9492731
87 X = -2893384
67
Y = 17242218
03 feet Y = 5255428
05 meter
Z = -9944130
92 Z = -3030971
11
XDOT = -10181
880147 XDOT = -3103
437069
YDOT = -14937
679417 feet/sec YDOT = -4553
004686 meter/sec
ZDOT = -16203
617427 ZDOT = -4938
862592
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 07187
48385287
00020000 00000-0 20000-3 0 9096
2 25544 51
6318 4
1577 0008424 33
4564 326
7132 15
78670346 13828
Satellite: ISS
Catalog Number: 25544
Epoch time: 07187
48385287 = yrday
fracday
Element set: 909
Inclination: 51
6318 deg
RA of node: 4
1577 deg
Eccentricity:
0008424
Arg of perigee: 33
4564 deg
Mean anomaly: 326
7132 deg
Mean motion: 15
78670346 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1382
Checksum: 306
Coasting Arc #11 (Orbit 1397)
---------------------------------------
Vector Time (GMT): 2007/188/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5216662
82 A = 6714271
59 meter
Y = 2697542
19 meter E =
0018779
Z = 3245994
72 I = 51
62859
XDOT = -4857
607232 Wp = 70
63863
YDOT = -3644
093537 meter/sec RA = 358
60896 deg
ZDOT = -4749
995008 TA = 71
26302
MA = 71
05933
Ha = 185
466 n
mi
Hp = 174
459
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17115035
50 X = -5262207
83
Y = 8850204
03 feet Y = 2638951
50 meter
Z = 10649588
98 Z = 3220541
92
XDOT = -15937
031602 XDOT = -4793
422856
YDOT = -11955
687458 feet/sec YDOT = -3698
054601 meter/sec
ZDOT = -15583
973123 ZDOT = -4773
437734
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8639373
34 X = 2633280
99
Y = 17281405
58 feet Y = 5267372
42 meter
Z = 10553603
48 Z = 3216738
34
XDOT = -10888
473450 XDOT = -3318
806707
YDOT = 15072
048277 feet/sec YDOT = 4593
960315 meter/sec
ZDOT = -15673
026982 ZDOT = -4777
138624
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 07188
49667254
00020000 00000-0 20000-3 0 9107
2 25544 51
6321 358
9184 0008306 36
0324 324
1400 15
78715700 13989
Satellite: ISS
Catalog Number: 25544
Epoch time: 07188
49667254 = yrday
fracday
Element set: 910
Inclination: 51
6321 deg
RA of node: 358
9184 deg
Eccentricity:
0008306
Arg of perigee: 36
0324 deg
Mean anomaly: 324
1400 deg
Mean motion: 15
78715700 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1398
Checksum: 288
Coasting Arc #12 (Orbit 1413)
---------------------------------------
Vector Time (GMT): 2007/189/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2836576
87 A = 6708260
97 meter
Y = 3586316
31 meter E =
0011132
Z = 4898289
93 I = 51
57849
XDOT = -6957
935104 Wp = 74
34463
YDOT = 2531
693266 meter/sec RA = 353
47722 deg
ZDOT = 2174
600220 TA = 354
56875
MA = 354
58081
Ha = 185
519 n
mi
Hp = 174
266
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9306354
55 X = 2772468
29
Y = 11766129
64 feet Y = 3617677
39 meter
Z = 16070505
00 Z = 4911914
81
XDOT = -22827
871077 XDOT = -6996
291571
YDOT = 8306
080270 feet/sec YDOT = 2453
670967 meter/sec
ZDOT = 7134
515159 ZDOT = 2140
705694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11720151
74 X = 3572302
25
Y = -9274530
35 feet Y = -2826876
85 meter
Z = 16122416
16 Z = 4914112
45
XDOT = 7743
222497 XDOT = 2360
134217
YDOT = 21971
286881 feet/sec YDOT = 6696
848241 meter/sec
ZDOT = 7006
582638 ZDOT = 2135
606388
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 07189
50947729
00020000 00000-0 20000-3 0 9119
2 25544 51
6312 353
6793 0008426 41
0622 319
1177 15
78691883 14146
Satellite: ISS
Catalog Number: 25544
Epoch time: 07189
50947729 = yrday
fracday
Element set: 911
Inclination: 51
6312 deg
RA of node: 353
6793 deg
Eccentricity:
0008426
Arg of perigee: 41
0622 deg
Mean anomaly: 319
1177 deg
Mean motion: 15
78691883 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1414
Checksum: 307
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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