Date:
October 20th 2006
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 3767 37 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 75 5 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 08 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
299/14:46:00
000 0
0 0
0 0
0
N/A 0
0 0
0 189
1
000/00:00:00
000 0
0 0
0 175
3
Coasting Arc #1 (Orbit 1292)
---------------------------------------
Vector Time (GMT): 2006/293/11:33:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 163278
23 A = 6723067
46 meter
Y = 6628951
68 meter E =
0021746
Z = -1070090
85 I = 51
33679
XDOT = -4898
819344 Wp = 127
25383
YDOT = -815
435068 meter/sec RA = 261
17040 deg
ZDOT = -5893
779714 TA = 64
51917
MA = 64
29437
Ha = 189
906 n
mi
Hp = 174
784
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 535689
75 X = 94338
67
Y = 21748529
12 feet Y = 6630392
02 meter
Z = -3510796
77 Z = -1069465
46
XDOT = -16072
241943 XDOT = -4860
705374
YDOT = -2675
311904 feet/sec YDOT = -870
003611 meter/sec
ZDOT = -19336
547618 ZDOT = -5917
486089
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8421668
63 X = -2566924
60
Y = -20059505
81 feet Y = -6114137
37 meter
Z = -3507549
07 Z = -1069100
96
XDOT = 14382
940676 XDOT = 4383
920318
YDOT = -2696
329823 feet/sec YDOT = -821
841330 meter/sec
ZDOT = -19425
008720 ZDOT = -5920
742658
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 06293
51095707
00020000 00000-0 20000-3 0 9003
2 25544 51
6306 261
7734 0012659 116
0004 244
2466 15
77030684 12932
Satellite: ISS
Catalog Number: 25544
Epoch time: 06293
51095707 = yrday
fracday
Element set: 900
Inclination: 51
6306 deg
RA of node: 261
7734 deg
Eccentricity:
0012659
Arg of perigee: 116
0004 deg
Mean anomaly: 244
2466 deg
Mean motion: 15
77030684 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1293
Checksum: 277
Coasting Arc #2 (Orbit 1308)
---------------------------------------
Vector Time (GMT): 2006/294/11:33:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4377027
94 A = 6713201
58 meter
Y = 1581429
71 meter E =
0016809
Z = 4822921
33 I = 51
30931
XDOT = -84
744502 Wp = 99
29179
YDOT = 7357
169652 meter/sec RA = 255
95966 deg
ZDOT = -2331
295835 TA = 13
49759
MA = 13
45269
Ha = 189
683 n
mi
Hp = 174
895
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14360327
90 X = 4335589
35
Y = 5188417
67 feet Y = 1630144
59 meter
Z = 15823232
71 Z = 4844084
77
XDOT = -278
033142 XDOT = -155
681775
YDOT = 24137
695710 feet/sec YDOT = 7355
825255 meter/sec
ZDOT = -7648
608382 ZDOT = -2331
880186
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15174026
92 X = -4625043
40
Y = 615131
50 feet Y = 187492
08 meter
Z = 15902324
01 Z = 4847028
36
XDOT = -8895
410325 XDOT = -2711
321067
YDOT = -21315
792800 feet/sec YDOT = -6497
053646 meter/sec
ZDOT = -7649
768079 ZDOT = -2331
649310
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 06294
52482841
00020000 00000-0 20000-3 0 9015
2 25544 51
6305 256
5424 0012521 120
0641 240
1767 15
77052704 13093
Satellite: ISS
Catalog Number: 25544
Epoch time: 06294
52482841 = yrday
fracday
Element set: 901
Inclination: 51
6305 deg
RA of node: 256
5424 deg
Eccentricity:
0012521
Arg of perigee: 120
0641 deg
Mean anomaly: 240
1767 deg
Mean motion: 15
77052704 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1309
Checksum: 260
Coasting Arc #3 (Orbit 1324)
---------------------------------------
Vector Time (GMT): 2006/295/11:33:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 372579
48 A = 6719629
67 meter
Y = -6034923
60 meter E =
0024222
Z = 2918090
79 I = 51
34039
XDOT = 5187
138414 Wp = 102
75663
YDOT = 2753
985900 meter/sec RA = 250
82142 deg
ZDOT = 4993
193763 TA = 291
06538
MA = 291
32423
Ha = 189
680 n
mi
Hp = 174
897
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1222373
61 X = 425859
15
Y = -19799618
13 feet Y = -6030459
23 meter
Z = 9573788
68 Z = 2920030
44
XDOT = 17018
170651 XDOT = 5131
700672
YDOT = 9035
386812 feet/sec YDOT = 2811
681540 meter/sec
ZDOT = 16381
869302 ZDOT = 5018
258897
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6752222
41 X = 2058077
39
Y = 18649506
04 feet Y = 5684369
44 meter
Z = 9580183
81 Z = 2920040
03
XDOT = -17760
411020 XDOT = -5413
373279
YDOT = -2100
632091 feet/sec YDOT = -640
272661 meter/sec
ZDOT = 16475
665644 ZDOT = 5021
782888
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 06295
53868411
00020000 00000-0 20000-3 0 9029
2 25544 51
6313 251
3115 0012568 124
6653 235
5698 15
77110534 13251
Satellite: ISS
Catalog Number: 25544
Epoch time: 06295
53868411 = yrday
fracday
Element set: 902
Inclination: 51
6313 deg
RA of node: 251
3115 deg
Eccentricity:
0012568
Arg of perigee: 124
6653 deg
Mean anomaly: 235
5698 deg
Mean motion: 15
77110534 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1325
Checksum: 282
Coasting Arc #4 (Orbit 1339)
---------------------------------------
Vector Time (GMT): 2006/296/11:33:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4668126
35 A = 6717429
29 meter
Y = -3139494
39 meter E =
0017976
Z = -3692177
11 I = 51
34355
XDOT = 882
035469 Wp = 119
47425
YDOT = -6330
898968 meter/sec RA = 245
58970 deg
ZDOT = 4274
950650 TA = 195
88682
MA = 195
94328
Ha = 189
658 n
mi
Hp = 174
979
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15315375
16 X = -4614736
64
Y = -10300178
45 feet Y = -3191397
49 meter
Z = -12113441
98 Z = -3714725
88
XDOT = 2893
817157 XDOT = 931
995306
YDOT = -20770
665907 feet/sec YDOT = -6320
756182 meter/sec
ZDOT = 14025
428642 ZDOT = 4279
357127
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18134263
34 X = 5527323
47
Y = 3122372
70 feet Y = 951699
20 meter
Z = -12197915
83 Z = -3717924
75
XDOT = 6197
549389 XDOT = 1889
013054
YDOT = 18770
389019 feet/sec YDOT = 5721
214573 meter/sec
ZDOT = 14040
979736 ZDOT = 4279
690624
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 06296
48916324
00020000 00000-0 20000-3 0 9032
2 25544 51
6314 246
4068 0012454 127
2369 232
9933 15
77072753 13401
Satellite: ISS
Catalog Number: 25544
Epoch time: 06296
48916324 = yrday
fracday
Element set: 903
Inclination: 51
6314 deg
RA of node: 246
4068 deg
Eccentricity:
0012454
Arg of perigee: 127
2369 deg
Mean anomaly: 232
9933 deg
Mean motion: 15
77072753 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1340
Checksum: 295
Coasting Arc #5 (Orbit 1355)
---------------------------------------
Vector Time (GMT): 2006/297/11:33:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1265047
29 A = 6714817
63 meter
Y = 4916923
21 meter E =
0018804
Z = -4407444
05 I = 51
34886
XDOT = -5459
244570 Wp = 105
12014
YDOT = -4323
844137 meter/sec RA = 240
45905 deg
ZDOT = -3273
153185 TA = 131
95835
MA = 131
79796
Ha = 189
506 n
mi
Hp = 175
084
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4150417
60 X = -1298523
74
Y = 16131637
82 feet Y = 4902589
63 meter
Z = -14460118
28 Z = -4413671
09
XDOT = -17910
907382 XDOT = -5394
588107
YDOT = -14185
840344 feet/sec YDOT = -4384
530876 meter/sec
ZDOT = -10738
691551 ZDOT = -3299
518043
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3201082
38 X = -975689
91
Y = -16326559
66 feet Y = -4976335
38 meter
Z = -14482653
32 Z = -4414312
73
XDOT = 21006
817414 XDOT = 6402
877948
YDOT = 5447
097068 feet/sec YDOT = 1660
275186 meter/sec
ZDOT = -10837
555910 ZDOT = -3303
287041
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 06297
50299187
00020000 00000-0 20000-3 0 9048
2 25544 51
6323 241
1750 0012436 131
1765 229
0474 15
77121757 13568
Satellite: ISS
Catalog Number: 25544
Epoch time: 06297
50299187 = yrday
fracday
Element set: 904
Inclination: 51
6323 deg
RA of node: 241
1750 deg
Eccentricity:
0012436
Arg of perigee: 131
1765 deg
Mean anomaly: 229
0474 deg
Mean motion: 15
77121757 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1356
Checksum: 288
Coasting Arc #6 (Orbit 1371)
---------------------------------------
Vector Time (GMT): 2006/298/11:33:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4815575
83 A = 6721642
94 meter
Y = 4259038
65 meter E =
0026051
Z = 1913004
16 I = 51
38756
XDOT = -2069
027326 Wp = 123
12323
YDOT = 4877
824986 meter/sec RA = 235
23850 deg
ZDOT = -5610
656237 TA = 35
46888
MA = 35
29593
Ha = 189
387 n
mi
Hp = 175
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15799133
30 X = 4758299
46
Y = 13973223
91 feet Y = 4312568
77 meter
Z = 6276260
37 Z = 1936259
95
XDOT = -6788
147395 XDOT = -2096
161703
YDOT = 16003
362816 feet/sec YDOT = 4854
536465 meter/sec
ZDOT = -18407
664820 ZDOT = -5620
773605
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20317757
86 X = -6192852
60
Y = -5563201
06 feet Y = -1695663
68 meter
Z = 6363533
08 Z = 1939604
88
XDOT = -1484
109748 XDOT = -452
356651
YDOT = -15829
047411 feet/sec YDOT = -4824
693651 meter/sec
ZDOT = -18444
710698 ZDOT = -5621
947821
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 06298
51680620
00020000 00000-0 20000-3 0 9057
2 25544 51
6326 235
9440 0012418 135
0221 225
1952 15
77133478 13727
Satellite: ISS
Catalog Number: 25544
Epoch time: 06298
51680620 = yrday
fracday
Element set: 905
Inclination: 51
6326 deg
RA of node: 235
9440 deg
Eccentricity:
0012418
Arg of perigee: 135
0221 deg
Mean anomaly: 225
1952 deg
Mean motion: 15
77133478 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1372
Checksum: 276
Coasting Arc #7 (Orbit 1387)
---------------------------------------
Vector Time (GMT): 2006/299/11:33:00
000
Vector Time (MET): N/A
Weight (LBS) : 454754
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2407322
49 A = 6711379
44 meter
Y = -3545420
44 meter E =
0015940
Z = 5157258
86 I = 51
37098
XDOT = 5515
948453 Wp = 136
06769
YDOT = 5289
004581 meter/sec RA = 230
08824 deg
ZDOT = 1047
972042 TA = 303
84103
MA = 303
99264
Ha = 189
172 n
mi
Hp = 175
337
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7898039
67 X = 2421735
27
Y = -11631956
81 feet Y = -3518420
11 meter
Z = 16920140
61 Z = 5168988
76
XDOT = 18096
943745 XDOT = 5451
305117
YDOT = 17352
377234 feet/sec YDOT = 5350
325480 meter/sec
ZDOT = 3438
228485 ZDOT = 1074
612478
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1618101
64 X = -493197
38
Y = 13913947
15 feet Y = 4240971
09 meter
Z = 16963384
98 Z = 5170439
74
XDOT = -22998
941635 XDOT = -7010
077410
YDOT = -7041
283314 feet/sec YDOT = -2146
183154 meter/sec
ZDOT = 3538
268181 ZDOT = 1078
464142
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 06299
53060353
00020000 00000-0 20000-3 0 9066
2 25544 51
6327 230
7135 0012276 139
6825 220
5252 15
77199869 13889
Satellite: ISS
Catalog Number: 25544
Epoch time: 06299
53060353 = yrday
fracday
Element set: 906
Inclination: 51
6327 deg
RA of node: 230
7135 deg
Eccentricity:
0012276
Arg of perigee: 139
6825 deg
Mean anomaly: 220
5252 deg
Mean motion: 15
77199869 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1388
Checksum: 307
Coasting Arc #8 (Orbit 1389)
---------------------------------------
Vector Time (GMT): 2006/299/14:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4990221
15 A = 6714250
93 meter
Y = 342078
34 meter E =
0017126
Z = 4462135
36 I = 51
38493
XDOT = 2370
645702 Wp = 110
05370
YDOT = 6632
312346 meter/sec RA = 229
36215 deg
ZDOT = -3155
698285 TA = 11
51945
MA = 11
48031
Ha = 189
088 n
mi
Hp = 175
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16372116
64 X = 4964348
30
Y = 1122304
27 feet Y = 397736
86 meter
Z = 14639551
69 Z = 4486315
64
XDOT = 7777
708996 XDOT = 2311
636275
YDOT = 21759
554941 feet/sec YDOT = 6658
492453 meter/sec
ZDOT = -10353
340830 ZDOT = -3144
324371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5136124
71 X = -1565490
81
Y = 15500873
97 feet Y = 4724666
38 meter
Z = 14729744
50 Z = 4489626
12
XDOT = -21893
807212 XDOT = -6673
232438
YDOT = 2555
012429 feet/sec YDOT = 778
767788 meter/sec
ZDOT = -10310
030696 ZDOT = -3142
497356
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 06299
65732765
00020000 00000-0 20000-3 0 9073
2 25544 51
6344 230
0598 0012233 139
4300 220
7779 15
77199770 13903
Satellite: ISS
Catalog Number: 25544
Epoch time: 06299
65732765 = yrday
fracday
Element set: 907
Inclination: 51
6344 deg
RA of node: 230
0598 deg
Eccentricity:
0012233
Arg of perigee: 139
4300 deg
Mean anomaly: 220
7779 deg
Mean motion: 15
77199770 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1390
Checksum: 308
Coasting Arc #9 (Orbit 1405)
---------------------------------------
Vector Time (GMT): 2006/300/14:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1522301
47 A = 6717582
74 meter
Y = -5470736
60 meter E =
0022165
Z = 3581854
61 I = 51
41529
XDOT = 6223
471195 Wp = 118
72117
YDOT = 1165
775897 meter/sec RA = 224
23434 deg
ZDOT = 4394
533421 TA = 284
31809
MA = 284
56410
Ha = 189
212 n
mi
Hp = 175
520
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4994427
39 X = -1478414
16
Y = -17948610
91 feet Y = -5487514
65 meter
Z = 11751491
50 Z = 3574565
39
XDOT = 20418
212581 XDOT = 6188
624486
YDOT = 3824
724070 feet/sec YDOT = 1235
175101 meter/sec
ZDOT = 14417
760566 ZDOT = 4424
683105
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18632634
82 X = 5679227
09
Y = -759901
64 feet Y = -231618
02 meter
Z = 11723564
31 Z = 3573342
40
XDOT = -8491
297637 XDOT = -2588
147520
YDOT = 17538
614737 feet/sec YDOT = 5345
769772 meter/sec
ZDOT = 14530
333274 ZDOT = 4428
845582
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 06300
67111121
00020000 00000-0 20000-3 0 9086
2 25544 51
6344 224
8280 0012268 143
1788 217
0222 15
77178389 14065
Satellite: ISS
Catalog Number: 25544
Epoch time: 06300
67111121 = yrday
fracday
Element set: 908
Inclination: 51
6344 deg
RA of node: 224
8280 deg
Eccentricity:
0012268
Arg of perigee: 143
1788 deg
Mean anomaly: 217
0222 deg
Mean motion: 15
77178389 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1406
Checksum: 273
Coasting Arc #10 (Orbit 1420)
---------------------------------------
Vector Time (GMT): 2006/301/14:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5796417
27 A = 6718996
32 meter
Y = -1598395
90 meter E =
0014032
Z = -3018915
62 I = 51
44176
XDOT = -955
714920 Wp = 129
66082
YDOT = -5828
542892 meter/sec RA = 219
00781 deg
ZDOT = 4927
351256 TA = 195
32300
MA = 195
36553
Ha = 188
999 n
mi
Hp = 175
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19017117
02 X = -5763447
39
Y = -5244081
04 feet Y = -1663030
14 meter
Z = -9904578
80 Z = -3046995
08
XDOT = -3135
547639 XDOT = -914
404888
YDOT = -19122
516050 feet/sec YDOT = -5838
999519 meter/sec
ZDOT = 16165
850576 ZDOT = 4922
808342
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9199761
76 X = 2804087
38
Y = -17390399
77 feet Y = -5300593
85 meter
Z = -10009504
80 Z = -3050897
06
XDOT = 18100
578576 XDOT = 5517
056350
YDOT = 292
878647 feet/sec YDOT = 89
269412 meter/sec
ZDOT = 16148
108980 ZDOT = 4921
943617
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 06301
62151835
00020000 00000-0 20000-3 0 9099
2 25544 51
6342 219
9231 0012125 147
4357 212
7558 15
77210488 14213
Satellite: ISS
Catalog Number: 25544
Epoch time: 06301
62151835 = yrday
fracday
Element set: 909
Inclination: 51
6342 deg
RA of node: 219
9231 deg
Eccentricity:
0012125
Arg of perigee: 147
4357 deg
Mean anomaly: 212
7558 deg
Mean motion: 15
77210488 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1421
Checksum: 274
Coasting Arc #11 (Orbit 1436)
---------------------------------------
Vector Time (GMT): 2006/302/14:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 22766
97 A = 6712756
17 meter
Y = 4662883
42 meter E =
0018663
Z = -4841105
34 I = 51
44321
XDOT = -6926
078707 Wp = 112
38685
YDOT = -2392
650809 meter/sec RA = 213
87644 deg
ZDOT = -2351
334733 TA = 134
69008
MA = 134
53789
Ha = 188
827 n
mi
Hp = 175
824
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 74694
78 X = -5858
21
Y = 15298173
94 feet Y = 4662978
15 meter
Z = -15882891
55 Z = -4841064
09
XDOT = -22723
355339 XDOT = -6887
386482
YDOT = -7849
904230 feet/sec YDOT = -2469
885630 meter/sec
ZDOT = -7714
352798 ZDOT = -2384
888175
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15026854
39 X = -4580185
22
Y = -2873799
34 feet Y = -875934
04 meter
Z = -15882092
86 Z = -4840861
90
XDOT = 11980
991478 XDOT = 3651
806203
YDOT = -19578
141452 feet/sec YDOT = -5967
417515 meter/sec
ZDOT = -7839
815456 ZDOT = -2389
575751
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 06302
63527268
00020000 00000-0 20000-3 0 9100
2 25544 51
6337 214
6907 0012056 151
6349 208
5475 15
77241975 14373
Satellite: ISS
Catalog Number: 25544
Epoch time: 06302
63527268 = yrday
fracday
Element set: 910
Inclination: 51
6337 deg
RA of node: 214
6907 deg
Eccentricity:
0012056
Arg of perigee: 151
6349 deg
Mean anomaly: 208
5475 deg
Mean motion: 15
77241975 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1437
Checksum: 295
Coasting Arc #12 (Orbit 1452)
---------------------------------------
Vector Time (GMT): 2006/303/14:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6159799
64 A = 6722566
21 meter
Y = 2458830
23 meter E =
0025082
Z = 1003868
60 I = 51
50082
XDOT = -959
011598 Wp = 138
92670
YDOT = 4848
496919 meter/sec RA = 208
67531 deg
ZDOT = -5926
509431 TA = 30
04921
MA = 29
90552
Ha = 188
820 n
mi
Hp = 175
954
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20209316
40 X = 6126970
17
Y = 8067028
32 feet Y = 2527528
95 meter
Z = 3293532
16 Z = 1033713
56
XDOT = -3146
363511 XDOT = -984
366636
YDOT = 15907
142124 feet/sec YDOT = 4837
631050 meter/sec
ZDOT = -19443
928581 ZDOT = -5931
229874
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11595163
90 X = -3534205
96
Y = 18392869
48 feet Y = 5606146
62 meter
Z = 3405186
58 Z = 1037900
87
XDOT = -13751
122095 XDOT = -4191
342015
YDOT = -5028
054597 feet/sec YDOT = -1532
551041 meter/sec
ZDOT = -19460
859090 ZDOT = -5931
669851
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 06303
64901483
00020000 00000-0 20000-3 0 9118
2 25544 51
6339 209
4591 0012257 155
3470 204
8283 15
77222426 14539
Satellite: ISS
Catalog Number: 25544
Epoch time: 06303
64901483 = yrday
fracday
Element set: 911
Inclination: 51
6339 deg
RA of node: 209
4591 deg
Eccentricity:
0012257
Arg of perigee: 155
3470 deg
Mean anomaly: 204
8283 deg
Mean motion: 15
77222426 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1453
Checksum: 279
Coasting Arc #13 (Orbit 1468)
---------------------------------------
Vector Time (GMT): 2006/304/14:46:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1743566
08 A = 6710769
83 meter
Y = -3795123
84 meter E =
0013028
Z = 5247009
76 I = 51
48688
XDOT = 7044
760796 Wp = 149
83362
YDOT = 3137
080910 meter/sec RA = 203
51335 deg
ZDOT = -82
938277 TA = 300
88987
MA = 301
01791
Ha = 188
591 n
mi
Hp = 176
129
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5720361
16 X = 1760384
74
Y = -12451193
69 feet Y = -3775532
23 meter
Z = 17214598
96 Z = 5255521
00
XDOT = 23112
732270 XDOT = 7009
560842
YDOT = 10292
260202 feet/sec YDOT = 3215
662519 meter/sec
ZDOT = -272
107209 ZDOT = -48
799908
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11356975
86 X = 3461606
24
Y = 7595932
31 feet Y = 2315240
17 meter
Z = 17245813
55 Z = 5256523
97
XDOT = -13398
765432 XDOT = -4083
943704
YDOT = 20278
831185 feet/sec YDOT = 6180
987745 meter/sec
ZDOT = -144
332957 ZDOT = -43
992685
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 06304
66274026
00020000 00000-0 20000-3 0 9128
2 25544 51
6336 204
2267 0012072 159
5625 200
6025 15
77276881 14691
Satellite: ISS
Catalog Number: 25544
Epoch time: 06304
66274026 = yrday
fracday
Element set: 912
Inclination: 51
6336 deg
RA of node: 204
2267 deg
Eccentricity:
0012072
Arg of perigee: 159
5625 deg
Mean anomaly: 200
6025 deg
Mean motion: 15
77276881 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1469
Checksum: 281
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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