Date:
July 6th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6189 25 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 1318)
---------------------------------------
Vector Time (GMT): 2007/183/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6083396
80 A = 6715676
45 meter
Y = -326351
16 meter E =
0017098
Z = 2820025
42 I = 51
77611
XDOT = -2095
090700 Wp = 70
14479
YDOT = -5374
656187 meter/sec RA = 24
45221 deg
ZDOT = -5110
929075 TA = 77
53050
MA = 77
33924
Ha = 185
325 n
mi
Hp = 175
191
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19958650
91 X = -6092994
31
Y = -1070705
89 feet Y = -394433
34 meter
Z = 9252051
89 Z = 2790449
36
XDOT = -6873
657152 XDOT = -2010
007223
YDOT = -17633
386439 feet/sec YDOT = -5397
607926 meter/sec
ZDOT = -16768
140011 ZDOT = -5120
901270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3028329
31 X = -923034
77
Y = 19808621
03 feet Y = 6037667
69 meter
Z = 9140151
85 Z = 2785918
28
XDOT = -16768
841355 XDOT = -5111
142845
YDOT = 5238
174606 feet/sec YDOT = 1596
595620 meter/sec
ZDOT = -16806
416253 ZDOT = -5122
595674
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
49565983
00020000 00000-0 20000-3 0 9007
2 25544 51
6351 24
7883 0008503 18
9543 341
1937 15
78619751 13193
Satellite: ISS
Catalog Number: 25544
Epoch time: 07183
49565983 = yrday
fracday
Element set: 900
Inclination: 51
6351 deg
RA of node: 24
7883 deg
Eccentricity:
0008503
Arg of perigee: 18
9543 deg
Mean anomaly: 341
1937 deg
Mean motion: 15
78619751 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1319
Checksum: 312
Coasting Arc #2 (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 = 384644
07 A = 6707889
15 meter
Y = 4371338
67 meter E =
0008772
Z = 5066001
59 I = 51
72192
XDOT = -7436
847124 Wp = 55
86299
YDOT = -1239
260609 meter/sec RA = 19
32542 deg
ZDOT = 1636
819038 TA = 18
47302
MA = 18
44119
Ha = 185
424 n
mi
Hp = 175
034
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1261955
60 X = 311125
23
Y = 14341662
30 feet Y = 4375228
04 meter
Z = 16620740
13 Z = 5067692
34
XDOT = -24399
104737 XDOT = -7430
388043
YDOT = -4065
815645 feet/sec YDOT = -1322
387777 meter/sec
ZDOT = 5370
141202 ZDOT = 1600
706925
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14389161
75 X = 4385816
50
Y = -4000
34 feet Y = -1219
30 meter
Z = 16627592
13 Z = 5068090
08
XDOT = -6030
420489 XDOT = -1838
072165
YDOT = 22970
185642 feet/sec YDOT = 7001
312584 meter/sec
ZDOT = 5233
419445 ZDOT = 1595
146247
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
50853336
00020000 00000-0 20000-3 0 9013
2 25544 51
6341 19
5495 0008424 23
2341 336
9203 15
78586956 13356
Satellite: ISS
Catalog Number: 25544
Epoch time: 07184
50853336 = yrday
fracday
Element set: 901
Inclination: 51
6341 deg
RA of node: 19
5495 deg
Eccentricity:
0008424
Arg of perigee: 23
2341 deg
Mean anomaly: 336
9203 deg
Mean motion: 15
78586956 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1335
Checksum: 291
Coasting Arc #3 (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 = 6484592
28 A = 6719006
02 meter
Y = 1713644
52 meter E =
0020610
Z = 97252
77 I = 51
73132
XDOT = -1315
027014 Wp = 37
83362
YDOT = 4595
296546 meter/sec RA = 14
14744 deg
ZDOT = 6055
962002 TA = 323
22449
MA = 323
36570
Ha = 185
377 n
mi
Hp = 174
847
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21274909
05 X = 6464475
68
Y = 5622193
30 feet Y = 1786046
38 meter
Z = 319070
77 Z = 128705
81
XDOT = -4314
393089 XDOT = -1395
732851
YDOT = 15076
432237 feet/sec YDOT = 4580
139045 meter/sec
ZDOT = 19868
641740 ZDOT = 6049
378340
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6967910
27 X = 2123819
05
Y = -20870764
40 feet Y = -6361408
99 meter
Z = 438222
07 Z = 133570
09
XDOT = 13241
383900 XDOT = 4035
973813
YDOT = 4870
312877 feet/sec YDOT = 1484
471365 meter/sec
ZDOT = 19844
222399 ZDOT = 6048
518987
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
52138348
00020000 00000-0 20000-3 0 9026
2 25544 51
6333 14
3106 0008379 25
9967 334
1618 15
78642730 13512
Satellite: ISS
Catalog Number: 25544
Epoch time: 07185
52138348 = yrday
fracday
Element set: 902
Inclination: 51
6333 deg
RA of node: 14
3106 deg
Eccentricity:
0008379
Arg of perigee: 25
9967 deg
Mean anomaly: 334
1618 deg
Mean motion: 15
78642730 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1351
Checksum: 290
Coasting Arc #4 (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 = 2679012
74 A = 6708002
37 meter
Y = -3586970
78 meter E =
0017371
Z = -5008670
53 I = 51
66534
XDOT = 6992
880768 Wp = 76
34904
YDOT = 2608
927708 meter/sec RA = 8
96245 deg
ZDOT = 1881
379960 TA = 211
75459
MA = 211
85947
Ha = 185
380 n
mi
Hp = 174
716
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8789411
89 X = 2743254
58
Y = -11768276
82 feet Y = -3556652
74 meter
Z = -16432646
09 Z = -4995500
45
XDOT = 22942
522206 XDOT = 6954
048344
YDOT = 8559
474109 feet/sec YDOT = 2686
908675 meter/sec
ZDOT = 6172
506429 ZDOT = 1915
256949
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11341349
07 X = -3456843
20
Y = -9420307
50 feet Y = -2871309
73 meter
Z = -16383209
88 Z = -4993602
37
XDOT = 8931
219219 XDOT = 2722
235618
YDOT = -21656
595801 feet/sec YDOT = -6600
930400 meter/sec
ZDOT = 6300
921165 ZDOT = 1920
520771
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
47091224
00020000 00000-0 20000-3 0 9033
2 25544 51
6326 9
3987 0008343 29
9061 330
2580 15
78682891 13668
Satellite: ISS
Catalog Number: 25544
Epoch time: 07186
47091224 = yrday
fracday
Element set: 903
Inclination: 51
6326 deg
RA of node: 9
3987 deg
Eccentricity:
0008343
Arg of perigee: 29
9061 deg
Mean anomaly: 330
2580 deg
Mean motion: 15
78682891 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1366
Checksum: 303
Coasting Arc #5 (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 = -5302761
14 A = 6714626
19 meter
Y = -2777927
99 meter E =
0010733
Z = -3056214
70 I = 51
65934
XDOT = 4709
980386 Wp = 56
39690
YDOT = -3584
685696 meter/sec RA = 3
83358 deg
ZDOT = -4920
396801 TA = 159
03456
MA = 158
99052
Ha = 185
400 n
mi
Hp = 174
409
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17397510
31 X = -5256457
41
Y = -9113936
97 feet Y = -2836967
20 meter
Z = -10026951
12 Z = -3081863
17
XDOT = 15452
691554 XDOT = 4773
617027
YDOT = -11760
779842 feet/sec YDOT = -3531
659684 meter/sec
ZDOT = -16143
034125 ZDOT = -4897
361719
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9620354
93 X = -2932284
18
Y = 17065319
28 feet Y = 5201509
32 meter
Z = -10124258
48 Z = -3085873
99
XDOT = -10053
725020 XDOT = -3064
375386
YDOT = -15180
749217 feet/sec YDOT = -4627
092361 meter/sec
ZDOT = -16056
285923 ZDOT = -4893
955949
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
48372269
00020000 00000-0 20000-3 0 9047
2 25544 51
6324 4
1607 0008421 33
3401 326
8294 15
78717503 13822
Satellite: ISS
Catalog Number: 25544
Epoch time: 07187
48372269 = yrday
fracday
Element set: 904
Inclination: 51
6324 deg
RA of node: 4
1607 deg
Eccentricity:
0008421
Arg of perigee: 33
3401 deg
Mean anomaly: 326
8294 deg
Mean motion: 15
78717503 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1382
Checksum: 281
Coasting Arc #6 (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 = -5283360
09 A = 6714307
40 meter
Y = 2646346
19 meter E =
0018778
Z = 3179709
19 I = 51
62983
XDOT = -4761
473830 Wp = 71
43583
YDOT = -3693
161358 meter/sec RA = 358
61114 deg
ZDOT = -4808
991352 TA = 71
37867
MA = 71
17484
Ha = 185
379 n
mi
Hp = 174
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17333858
57 X = -5328005
67
Y = 8682238
15 feet Y = 2587014
69 meter
Z = 10432116
75 Z = 3153934
55
XDOT = -15621
633302 XDOT = -4696
461323
YDOT = -12116
671122 feet/sec YDOT = -3746
042767 meter/sec
ZDOT = -15777
530681 ZDOT = -4831
965057
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8468758
48 X = 2581277
59
Y = 17496935
94 feet Y = 5333066
08 meter
Z = 10334908
54 Z = 3150080
12
XDOT = -11029
855526 XDOT = -3361
899964
YDOT = 14766
066413 feet/sec YDOT = 4500
697043 meter/sec
ZDOT = -15864
815740 ZDOT = -4835
595838
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
49651074
00020000 00000-0 20000-3 0 9054
2 25544 51
6327 358
9213 0008306 35
8177 324
3544 15
78768627 13988
Satellite: ISS
Catalog Number: 25544
Epoch time: 07188
49651074 = yrday
fracday
Element set: 905
Inclination: 51
6327 deg
RA of node: 358
9213 deg
Eccentricity:
0008306
Arg of perigee: 35
8177 deg
Mean anomaly: 324
3544 deg
Mean motion: 15
78768627 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1398
Checksum: 324
Coasting Arc #7 (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 = 2718996
71 A = 6707958
44 meter
Y = 3628149
79 meter E =
0010883
Z = 4933820
13 I = 51
57857
XDOT = -7019
757515 Wp = 73
41580
YDOT = 2451
340587 meter/sec RA = 353
47808 deg
ZDOT = 2065
243406 TA = 356
60659
MA = 356
61396
Ha = 185
438 n
mi
Hp = 174
189
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8920592
87 X = 2654256
48
Y = 11903378
58 feet Y = 3658192
49 meter
Z = 16187073
92 Z = 4946872
28
XDOT = -23030
700508 XDOT = -7056
679635
YDOT = 8042
455995 feet/sec YDOT = 2372
634990 meter/sec
ZDOT = 6775
732958 ZDOT = 2031
052019
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11859317
82 X = 3614720
07
Y = -8888808
31 feet Y = -2709308
77 meter
Z = 16236823
23 Z = 4948983
72
XDOT = 7508
727474 XDOT = 2288
660134
YDOT = 22163
262475 feet/sec YDOT = 6755
362402 meter/sec
ZDOT = 6646
669156 ZDOT = 2025
904759
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
50928123
00020000 00000-0 20000-3 0 9060
2 25544 51
6318 353
6820 0008428 40
9112 319
2684 15
78745092 14143
Satellite: ISS
Catalog Number: 25544
Epoch time: 07189
50928123 = yrday
fracday
Element set: 906
Inclination: 51
6318 deg
RA of node: 353
6820 deg
Eccentricity:
0008428
Arg of perigee: 40
9112 deg
Mean anomaly: 319
2684 deg
Mean motion: 15
78745092 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1414
Checksum: 295
Coasting Arc #8 (Orbit 1428)
---------------------------------------
Vector Time (GMT): 2007/190/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6523229
66 A = 6718525
32 meter
Y = -1549581
37 meter E =
0020201
Z = -242730
16 I = 51
58615
XDOT = 1310
056857 Wp = 43
72367
YDOT = 4617
922327 meter/sec RA = 348
28225 deg
ZDOT = 6037
632788 TA = 313
62984
MA = 313
79722
Ha = 185
443 n
mi
Hp = 173
990
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21401672
10 X = 6541251
62
Y = -5083928
39 feet Y = -1476534
15 meter
Z = -796358
79 Z = -210996
69
XDOT = 4298
086801 XDOT = 1228
991394
YDOT = 15150
663804 feet/sec YDOT = 4632
117862 meter/sec
ZDOT = 19808
506521 ZDOT = 6043
800918
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5557183
96 X = -1693829
67
Y = -21287840
33 feet Y = -6488533
73 meter
Z = -676494
36 Z = -206195
48
XDOT = 13501
725120 XDOT = 4115
325817
YDOT = -4116
655211 feet/sec YDOT = -1254
756508 meter/sec
ZDOT = 19832
319612 ZDOT = 6044
891018
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 07190
45873082
00020000 00000-0 20000-3 0 9070
2 25544 51
6318 348
7701 0008326 45
0825 315
1015 15
78803188 14290
Satellite: ISS
Catalog Number: 25544
Epoch time: 07190
45873082 = yrday
fracday
Element set: 907
Inclination: 51
6318 deg
RA of node: 348
7701 deg
Eccentricity:
0008326
Arg of perigee: 45
0825 deg
Mean anomaly: 315
1015 deg
Mean motion: 15
78803188 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1429
Checksum: 292
Coasting Arc #9 (Orbit 1444)
---------------------------------------
Vector Time (GMT): 2007/191/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 495276
39 A = 6707205
31 meter
Y = -4370673
64 meter E =
0019963
Z = -5079783
12 I = 51
52030
XDOT = 7470
812180 Wp = 82
25423
YDOT = -967
596767 meter/sec RA = 343
09219 deg
ZDOT = 1568
814129 TA = 202
79747
MA = 202
88623
Ha = 185
454 n
mi
Hp = 173
814
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1624922
55 X = 568789
80
Y = -14339480
45 feet Y = -4364723
16 meter
Z = -16665955
11 Z = -5077199
34
XDOT = 24510
538648 XDOT = 7473
455718
YDOT = -3174
530074 feet/sec YDOT = -884
039473 meter/sec
ZDOT = 5147
027983 ZDOT = 1605
113625
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14395948
51 X = -4387885
11
Y = -1152501
98 feet Y = -351282
60 meter
Z = -16656636
46 Z = -5076942
79
XDOT = -4219
738707 XDOT = -1286
176358
YDOT = -23287
629641 feet/sec YDOT = -7098
069515 meter/sec
ZDOT = 5284
228836 ZDOT = 1610
632949
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 07191
47145750
00020000 00000-0 20000-3 0 9088
2 25544 51
6320 343
5309 0008387 49
4995 310
6900 15
78838090 14454
Satellite: ISS
Catalog Number: 25544
Epoch time: 07191
47145750 = yrday
fracday
Element set: 908
Inclination: 51
6320 deg
RA of node: 343
5309 deg
Eccentricity:
0008387
Arg of perigee: 49
4995 deg
Mean anomaly: 310
6900 deg
Mean motion: 15
78838090 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1445
Checksum: 304
Coasting Arc #10 (Orbit 1460)
---------------------------------------
Vector Time (GMT): 2007/192/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6078665
59 A = 6714603
42 meter
Y = 4277
62 meter E =
0011401
Z = -2866128
80 I = 51
51903
XDOT = 2373
850671 Wp = 72
79569
YDOT = -5297
558545 meter/sec RA = 337
94790 deg
ZDOT = -5055
698218 TA = 140
21523
MA = 140
13157
Ha = 185
442 n
mi
Hp = 173
550
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19943128
58 X = -6064338
55
Y = 14034
19 feet Y = -63616
71 meter
Z = -9403309
73 Z = -2895624
08
XDOT = 7788
223986 XDOT = 2457
471910
YDOT = -17380
441419 feet/sec YDOT = -5270
544179 meter/sec
ZDOT = -16586
936410 ZDOT = -5043
964104
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1138692
15 X = 347073
37
Y = 19857523
53 feet Y = 6052573
17 meter
Z = -9514880
33 Z = -2900135
53
XDOT = -16350
171861 XDOT = -4983
532383
YDOT = -6968
701961 feet/sec YDOT = -2124
060358 meter/sec
ZDOT = -16543
098555 ZDOT = -5042
336439
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 07192
48416164
00020000 00000-0 20000-3 0 9091
2 25544 51
6323 338
2912 0008522 52
4572 307
7367 15
78895811 14610
Satellite: ISS
Catalog Number: 25544
Epoch time: 07192
48416164 = yrday
fracday
Element set: 909
Inclination: 51
6323 deg
RA of node: 338
2912 deg
Eccentricity:
0008522
Arg of perigee: 52
4572 deg
Mean anomaly: 307
7367 deg
Mean motion: 15
78895811 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1461
Checksum: 303
Coasting Arc #11 (Orbit 1476)
---------------------------------------
Vector Time (GMT): 2007/193/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3424911
60 A = 6713576
14 meter
Y = 4726111
90 meter E =
0020207
Z = 3305217
78 I = 51
48838
XDOT = -6033
608210 Wp = 77
45146
YDOT = -1079
028581 meter/sec RA = 332
71444 deg
ZDOT = -4680
927567 TA = 63
51722
MA = 63
31009
Ha = 185
494 n
mi
Hp = 173
605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11236586
63 X = -3493561
14
Y = 15505616
47 feet Y = 4687428
04 meter
Z = 10843890
37 Z = 3288414
01
XDOT = -19795
302527 XDOT = -5998
355034
YDOT = -3540
120015 feet/sec YDOT = -1146
301627 meter/sec
ZDOT = -15357
373908 ZDOT = -4710
153190
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16296106
61 X = 4967053
29
Y = 10123535
87 feet Y = 3085653
73 meter
Z = 10780812
13 Z = 3285991
54
XDOT = -1339
505752 XDOT = -408
281353
YDOT = 18727
944822 feet/sec YDOT = 5708
277582 meter/sec
ZDOT = -15468
044620 ZDOT = -4714
660000
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 07193
49684514
00020000 00000-0 20000-3 0 9101
2 25544 51
6318 333
0512 0008374 56
6965 303
5002 15
78890512 14770
Satellite: ISS
Catalog Number: 25544
Epoch time: 07193
49684514 = yrday
fracday
Element set: 910
Inclination: 51
6318 deg
RA of node: 333
0512 deg
Eccentricity:
0008374
Arg of perigee: 56
6965 deg
Mean anomaly: 303
5002 deg
Mean motion: 15
78890512 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1477
Checksum: 293
Coasting Arc #12 (Orbit 1492)
---------------------------------------
Vector Time (GMT): 2007/194/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4136235
06 A = 6707523
12 meter
Y = 1982981
20 meter E =
0012492
Z = 4882933
52 I = 51
44461
XDOT = -5138
644534 Wp = 86
21678
YDOT = 5327
951839 meter/sec RA = 327
57213 deg
ZDOT = 2185
172368 TA = 342
53554
MA = 342
57846
Ha = 185
258 n
mi
Hp = 173
427
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13570324
99 X = 4090033
61
Y = 6505843
84 feet Y = 2028975
53 meter
Z = 16020123
11 Z = 4902915
26
XDOT = -16859
069993 XDOT = -5208
455570
YDOT = 17480
156951 feet/sec YDOT = 5270
097826 meter/sec
ZDOT = 7169
200681 ZDOT = 2160
040785
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5254170
83 X = 1601471
27
Y = -14015667
91 feet Y = -4271975
58 meter
Z = 16095925
28 Z = 4906038
03
XDOT = 17921
117419 XDOT = 5462
356589
YDOT = 14857
835875 feet/sec YDOT = 4528
668375 meter/sec
ZDOT = 7074
676925 ZDOT = 2156
361527
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 07194
50950555
00020000 00000-0 20000-3 0 9116
2 25544 51
6326 327
8117 0008329 59
8370 300
3620 15
78963042 14934
Satellite: ISS
Catalog Number: 25544
Epoch time: 07194
50950555 = yrday
fracday
Element set: 911
Inclination: 51
6326 deg
RA of node: 327
8117 deg
Eccentricity:
0008329
Arg of perigee: 59
8370 deg
Mean anomaly: 300
3620 deg
Mean motion: 15
78963042 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1493
Checksum: 292
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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