Date:
December 15th 2006
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10225 71 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 12 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 2131)
---------------------------------------
Vector Time (GMT): 2006/346/15:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6433624
60 A = 6726961
85 meter
Y = 1918089
90 meter E =
0012320
Z = 540505
75 I = 51
58130
XDOT = -1830
591681 Wp = 347
07522
YDOT = -4455
688533 meter/sec RA = 347
05993 deg
ZDOT = -5992
097939 TA = 187
04580
MA = 187
06314
Ha = 192
788 n
mi
Hp = 177
701
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21107692
25 X = -6457220
47
Y = 6292945
87 feet Y = 1846013
56 meter
Z = 1773312
84 Z = 509193
93
XDOT = -6005
878220 XDOT = -1751
522859
YDOT = -14618
400699 feet/sec YDOT = -4475
716629 meter/sec
ZDOT = -19659
113973 ZDOT = -6000
799301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17372157
66 X = -5295033
65
Y = -13555251
33 feet Y = -4131640
61 meter
Z = 1656435
22 Z = 504881
45
XDOT = 7501
710056 XDOT = 2286
521225
YDOT = -12014
188795 feet/sec YDOT = -3661
924745 meter/sec
ZDOT = -19692
163580 ZDOT = -6002
171459
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 06346
65766587
00020000 00000-0 20000-3 0 9008
2 25544 51
6333 347
3813 0024092 328
1115 31
8590 15
75790757 21327
Satellite: ISS
Catalog Number: 25544
Epoch time: 06346
65766587 = yrday
fracday
Element set: 900
Inclination: 51
6333 deg
RA of node: 347
3813 deg
Eccentricity:
0024092
Arg of perigee: 328
1115 deg
Mean anomaly: 31
8590 deg
Mean motion: 15
75790757 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2132
Checksum: 297
Coasting Arc #2 (Orbit 2147)
---------------------------------------
Vector Time (GMT): 2006/347/15:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1171781
62 A = 6714893
44 meter
Y = 4016691
64 meter E =
0023298
Z = 5260098
51 I = 51
51387
XDOT = -7341
948165 Wp = 336
94725
YDOT = 2309
190336 meter/sec RA = 341
90812 deg
ZDOT = -106
859876 TA = 114
19087
MA = 113
94716
Ha = 192
924 n
mi
Hp = 177
398
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3844427
89 X = 1101226
52
Y = 13178122
16 feet Y = 4029400
22 meter
Z = 17257541
06 Z = 5265620
03
XDOT = -24087
756446 XDOT = -7366
705075
YDOT = 7576
083778 feet/sec YDOT = 2226
950178 meter/sec
ZDOT = -350
590144 ZDOT = -142
587272
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8377166
71 X = -2553360
41
Y = 10841430
36 feet Y = 3304467
97 meter
Z = 17278649
21 Z = 5266532
28
XDOT = -19607
176008 XDOT = -5976
267247
YDOT = -14269
912002 feet/sec YDOT = -4349
469178 meter/sec
ZDOT = -483
934458 ZDOT = -147
503223
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 06347
67233388
00020000 00000-0 20000-3 0 9010
2 25544 51
6337 342
1560 0024040 331
9532 28
0335 15
75833994 21484
Satellite: ISS
Catalog Number: 25544
Epoch time: 06347
67233388 = yrday
fracday
Element set: 901
Inclination: 51
6337 deg
RA of node: 342
1560 deg
Eccentricity:
0024040
Arg of perigee: 331
9532 deg
Mean anomaly: 28
0335 deg
Mean motion: 15
75833994 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2148
Checksum: 286
Coasting Arc #3 (Orbit 2163)
---------------------------------------
Vector Time (GMT): 2006/348/15:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6329825
59 A = 6726603
56 meter
Y = -2096064
61 meter E =
0029980
Z = 719657
23 I = 51
52691
XDOT = 907
793608 Wp = 1
27716
YDOT = 4788
788057 meter/sec RA = 336
75797 deg
ZDOT = 5987
885827 TA = 6
60074
MA = 6
56134
Ha = 193
003 n
mi
Hp = 177
195
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20767144
31 X = 6349297
63
Y = -6876852
41 feet Y = -2025172
18 meter
Z = 2361080
16 Z = 750454
98
XDOT = 2978
325486 XDOT = 825
088853
YDOT = 15711
246905 feet/sec YDOT = 4798
476543 meter/sec
ZDOT = 19645
294707 ZDOT = 5992
095477
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18071142
44 X = 5508084
22
Y = 12306228
17 feet Y = 3750938
35 meter
Z = 2476013
06 Z = 754688
78
XDOT = -9838
285706 XDOT = -2998
709483
YDOT = 10506
730821 feet/sec YDOT = 3202
451554 meter/sec
ZDOT = 19661
584638 ZDOT = 5992
850998
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 06348
68696937
00020000 00000-0 20000-3 0 9026
2 25544 51
6335 336
9299 0023979 335
8603 24
1435 15
75881457 21647
Satellite: ISS
Catalog Number: 25544
Epoch time: 06348
68696937 = yrday
fracday
Element set: 902
Inclination: 51
6335 deg
RA of node: 336
9299 deg
Eccentricity:
0023979
Arg of perigee: 335
8603 deg
Mean anomaly: 24
1435 deg
Mean motion: 15
75881457 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2164
Checksum: 335
Coasting Arc #4 (Orbit 2178)
---------------------------------------
Vector Time (GMT): 2006/349/15:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -426724
19 A = 6715413
47 meter
Y = -4370222
85 meter E =
0020248
Z = -5080714
66 I = 51
46434
XDOT = 7134
770902 Wp = 14
14025
YDOT = -2465
135436 meter/sec RA = 331
57738 deg
ZDOT = 1541
783996 TA = 270
56650
MA = 270
79852
Ha = 193
171 n
mi
Hp = 176
912
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1400013
74 X = -353142
50
Y = -14338001
47 feet Y = -4374582
77 meter
Z = -16669011
34 Z = -5082609
44
XDOT = 23408
041018 XDOT = 7154
316309
YDOT = -8087
714685 feet/sec YDOT = -2385
241342 meter/sec
ZDOT = 5058
346443 ZDOT = 1576
492411
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10424550
78 X = 3177403
08
Y = -9930466
80 feet Y = -3026806
28 meter
Z = -16676595
39 Z = -5083026
28
XDOT = 20136
013017 XDOT = 6137
456768
YDOT = 12539
244552 feet/sec YDOT = 3821
961739 meter/sec
ZDOT = 5187
862681 ZDOT = 1581
260545
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 06349
63816045
00020000 00000-0 20000-3 0 9037
2 25544 51
6339 332
0308 0023975 339
4897 20
5303 15
75928288 21794
Satellite: ISS
Catalog Number: 25544
Epoch time: 06349
63816045 = yrday
fracday
Element set: 903
Inclination: 51
6339 deg
RA of node: 332
0308 deg
Eccentricity:
0023975
Arg of perigee: 339
4897 deg
Mean anomaly: 20
5303 deg
Mean motion: 15
75928288 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2179
Checksum: 313
Coasting Arc #5 (Orbit 2194)
---------------------------------------
Vector Time (GMT): 2006/350/15:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6072865
14 A = 6724727
07 meter
Y = 2128672
14 meter E =
0017998
Z = -1987741
33 I = 51
47265
XDOT = -27
894790 Wp = 351
53239
YDOT = -5300
558407 meter/sec RA = 326
44580 deg
ZDOT = -5567
223188 TA = 210
63132
MA = 210
73652
Ha = 193
307 n
mi
Hp = 176
540
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19924098
21 X = -6086560
66
Y = 6983832
48 feet Y = 2060685
66 meter
Z = -6521461
04 Z = -2017276
76
XDOT = -91
518339 XDOT = 58
423842
YDOT = -17390
283487 feet/sec YDOT = -5300
387018 meter/sec
ZDOT = -18265
167941 ZDOT = -5567
149692
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18016918
65 X = -5491556
80
Y = -10940046
27 feet Y = -3334526
10 meter
Z = -6631673
23 Z = -2021334
00
XDOT = 12649
428056 XDOT = 3855
545671
YDOT = -9713
039038 feet/sec YDOT = -2960
534299 meter/sec
ZDOT = -18265
495066 ZDOT = -5567
322896
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 06350
65273244
00020000 00000-0 20000-3 0 9040
2 25544 51
6344 326
8045 0023947 343
5181 16
5203 15
75993737 21953
Satellite: ISS
Catalog Number: 25544
Epoch time: 06350
65273244 = yrday
fracday
Element set: 904
Inclination: 51
6344 deg
RA of node: 326
8045 deg
Eccentricity:
0023947
Arg of perigee: 343
5181 deg
Mean anomaly: 16
5203 deg
Mean motion: 15
75993737 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2195
Checksum: 295
Coasting Arc #6 (Orbit 2210)
---------------------------------------
Vector Time (GMT): 2006/351/15:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -348715
69 A = 6717408
42 meter
Y = 4936939
06 meter E =
0026899
Z = 4553017
33 I = 51
42496
XDOT = -6698
932592 Wp = 5
19777
YDOT = 2314
772243 meter/sec RA = 321
23990 deg
ZDOT = -2995
249484 TA = 114
80488
MA = 114
52484
Ha = 193
417 n
mi
Hp = 176
339
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1144080
35 X = -426013
37
Y = 16197306
63 feet Y = 4932606
67 meter
Z = 14937720
90 Z = 4551136
21
XDOT = -21978
125303 XDOT = -6709
768228
YDOT = 7594
397122 feet/sec YDOT = 2239
800913 meter/sec
ZDOT = -9826
934003 ZDOT = -3027
819361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13135001
89 X = -4003548
58
Y = 9556507
53 feet Y = 2912823
49 meter
Z = 14931244
32 Z = 4551043
27
XDOT = -19289
299612 XDOT = -5879
378522
YDOT = -10826
162683 feet/sec YDOT = -3299
814386 meter/sec
ZDOT = -9948
478235 ZDOT = -3032
296166
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 06351
66727165
00020000 00000-0 20000-3 0 9059
2 25544 51
6343 321
5780 0023838 347
3854 12
6711 15
76030152 22112
Satellite: ISS
Catalog Number: 25544
Epoch time: 06351
66727165 = yrday
fracday
Element set: 905
Inclination: 51
6343 deg
RA of node: 321
5780 deg
Eccentricity:
0023838
Arg of perigee: 347
3854 deg
Mean anomaly: 12
6711 deg
Mean motion: 15
76030152 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2211
Checksum: 273
Coasting Arc #7 (Orbit 2226)
---------------------------------------
Vector Time (GMT): 2006/352/15:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5598425
55 A = 6721733
84 meter
Y = -1850031
57 meter E =
0025813
Z = 3192778
96 I = 51
41901
XDOT = -738
109034 Wp = 20
56065
YDOT = 6009
751052 meter/sec RA = 316
12035 deg
ZDOT = 4788
734234 TA = 16
96557
MA = 16
87941
Ha = 193
403 n
mi
Hp = 176
050
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18367537
89 X = 5603186
64
Y = -6069657
39 feet Y = -1787400
79 meter
Z = 10474996
59 Z = 3219987
70
XDOT = -2421
617567 XDOT = -828
519143
YDOT = 19717
031010 feet/sec YDOT = 6000
990793 meter/sec
ZDOT = 15711
070323 ZDOT = 4784
929859
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16653459
72 X = 5075974
52
Y = 9733016
81 feet Y = 2966623
52 meter
Z = 10576549
80 Z = 3223732
38
XDOT = -15747
857647 XDOT = -4799
947011
YDOT = 9930
050485 feet/sec YDOT = 3026
679388 meter/sec
ZDOT = 15697
519558 ZDOT = 4784
603961
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 06352
68177748
00020000 00000-0 20000-3 0 9069
2 25544 51
6346 316
3507 0023816 351
3679 8
7072 15
76075314 22272
Satellite: ISS
Catalog Number: 25544
Epoch time: 06352
68177748 = yrday
fracday
Element set: 906
Inclination: 51
6346 deg
RA of node: 316
3507 deg
Eccentricity:
0023816
Arg of perigee: 351
3679 deg
Mean anomaly: 8
7072 deg
Mean motion: 15
76075314 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2227
Checksum: 303
Coasting Arc #8 (Orbit 2241)
---------------------------------------
Vector Time (GMT): 2006/353/15:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 873557
81 A = 6720094
75 meter
Y = -5526874
64 meter E =
0022704
Z = -3705272
35 I = 51
39492
XDOT = 6139
528509 Wp = 8
89988
YDOT = -1877
021557 meter/sec RA = 310
90035 deg
ZDOT = 4272
844963 TA = 306
14841
MA = 306
35829
Ha = 193
542 n
mi
Hp = 175
747
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2866003
30 X = 953294
85
Y = -18132790
82 feet Y = -5516659
52 meter
Z = -12156405
34 Z = -3700835
90
XDOT = 20142
810068 XDOT = 6139
304454
YDOT = -6158
207207 feet/sec YDOT = -1808
367980 meter/sec
ZDOT = 14018
520220 ZDOT = 4302
670146
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15378535
72 X = 4687377
69
Y = -10044936
94 feet Y = -3061696
78 meter
Z = -12140434
48 Z = -3700404
43
XDOT = 17333
862472 XDOT = 5283
361282
YDOT = 9561
702917 feet/sec YDOT = 2914
407049 meter/sec
ZDOT = 14129
864234 ZDOT = 4306
782618
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 06353
63284556
00020000 00000-0 20000-3 0 9072
2 25544 51
6351 311
4507 0023749 354
8974 5
1945 15
76141193 22421
Satellite: ISS
Catalog Number: 25544
Epoch time: 06353
63284556 = yrday
fracday
Element set: 907
Inclination: 51
6351 deg
RA of node: 311
4507 deg
Eccentricity:
0023749
Arg of perigee: 354
8974 deg
Mean anomaly: 5
1945 deg
Mean motion: 15
76141193 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2242
Checksum: 295
Coasting Arc #9 (Orbit 2257)
---------------------------------------
Vector Time (GMT): 2006/354/15:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5089169
22 A = 6718118
42 meter
Y = 1308437
30 meter E =
0027642
Z = -4209276
25 I = 51
37200
XDOT = 1272
346501 Wp = 15
14823
YDOT = -6674
741234 meter/sec RA = 305
78113 deg
ZDOT = -3592
159901 TA = 218
00922
MA = 218
20458
Ha = 193
615 n
mi
Hp = 175
281
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16696749
42 X = -5082974
16
Y = 4292773
29 feet Y = 1251562
83 meter
Z = -13809961
44 Z = -4233984
20
XDOT = 4174
365160 XDOT = 1364
339935
YDOT = -21898
757329 feet/sec YDOT = -6659
998102 meter/sec
ZDOT = -11785
301514 ZDOT = -3585
756648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14526714
57 X = -4427742
60
Y = -9144766
01 feet Y = -2787324
68 meter
Z = -13902237
12 Z = -4237401
87
XDOT = 18172
524507 XDOT = 5538
985470
YDOT = -10882
438864 feet/sec YDOT = -3316
967366 meter/sec
ZDOT = -11762
103317 ZDOT = -3585
089091
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 06354
64728591
00020000 00000-0 20000-3 0 9087
2 25544 51
6358 306
2238 0023741 358
8937 1
2171 15
76206761 22584
Satellite: ISS
Catalog Number: 25544
Epoch time: 06354
64728591 = yrday
fracday
Element set: 908
Inclination: 51
6358 deg
RA of node: 306
2238 deg
Eccentricity:
0023741
Arg of perigee: 358
8937 deg
Mean anomaly: 1
2171 deg
Mean motion: 15
76206761 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2258
Checksum: 303
Coasting Arc #10 (Orbit 2273)
---------------------------------------
Vector Time (GMT): 2006/355/15:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1306939
32 A = 6723175
63 meter
Y = 6117166
61 meter E =
0024731
Z = 2484213
00 I = 51
37312
XDOT = -5494
896849 Wp = 35
68410
YDOT = 992
935211 meter/sec RA = 300
56210 deg
ZDOT = -5289
551624 TA = 116
12172
MA = 115
86706
Ha = 193
709 n
mi
Hp = 175
182
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4287858
65 X = -1387313
01
Y = 20069444
26 feet Y = 6102101
83 meter
Z = 8150305
11 Z = 2477669
82
XDOT = -18027
876801 XDOT = -5479
896004
YDOT = 3257
661452 feet/sec YDOT = 931
573086 meter/sec
ZDOT = -17354
171994 ZDOT = -5316
209126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17387440
45 X = -5299691
85
Y = 10919356
24 feet Y = 3328219
78 meter
Z = 8126522
75 Z = 2476964
14
XDOT = -14061
098256 XDOT = -4285
822748
YDOT = -9287
112302 feet/sec YDOT = -2830
711830 meter/sec
ZDOT = -17453
784300 ZDOT = -5319
913455
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 06355
66169327
00020000 00000-0 20000-3 0 9097
2 25544 51
6354 300
9962 0023603 2
7369 357
3920 15
76229434 22743
Satellite: ISS
Catalog Number: 25544
Epoch time: 06355
66169327 = yrday
fracday
Element set: 909
Inclination: 51
6354 deg
RA of node: 300
9962 deg
Eccentricity:
0023603
Arg of perigee: 2
7369 deg
Mean anomaly: 357
3920 deg
Mean motion: 15
76229434 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2274
Checksum: 302
Coasting Arc #11 (Orbit 2289)
---------------------------------------
Vector Time (GMT): 2006/356/15:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4535380
43 A = 6714900
96 meter
Y = -359165
83 meter E =
0021442
Z = 4926059
84 I = 51
33308
XDOT = -1633
345555 Wp = 20
47157
YDOT = 7256
393430 meter/sec RA = 295
42673 deg
ZDOT = 2050
038531 TA = 49
72627
MA = 49
53900
Ha = 193
612 n
mi
Hp = 174
828
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14879857
05 X = 4515129
89
Y = -1178365
58 feet Y = -308562
76 meter
Z = 16161613
65 Z = 4948043
29
XDOT = -5358
745260 XDOT = -1724
324805
YDOT = 23807
065059 feet/sec YDOT = 7237
619410 meter/sec
ZDOT = 6725
848199 ZDOT = 2041
884064
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11341288
73 X = 3456824
81
Y = 9566083
27 feet Y = 2915742
18 meter
Z = 16243819
38 Z = 4951116
15
XDOT = -19884
143397 XDOT = -6060
686907
YDOT = 12298
675465 feet/sec YDOT = 3748
636282 meter/sec
ZDOT = 6696
173235 ZDOT = 2040
993602
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 06356
67606567
00020000 00000-0 20000-3 0 9103
2 25544 51
6358 295
7685 0023568 6
5190 353
6277 15
76300169 22901
Satellite: ISS
Catalog Number: 25544
Epoch time: 06356
67606567 = yrday
fracday
Element set: 910
Inclination: 51
6358 deg
RA of node: 295
7685 deg
Eccentricity:
0023568
Arg of perigee: 6
5190 deg
Mean anomaly: 353
6277 deg
Mean motion: 15
76300169 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2290
Checksum: 316
Coasting Arc #12 (Orbit 2304)
---------------------------------------
Vector Time (GMT): 2006/357/15:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1482205
12 A = 6725041
47 meter
Y = -6455050
42 meter E =
0032484
Z = -1051630
90 I = 51
35681
XDOT = 4965
042172 Wp = 17
89869
YDOT = 190
137804 meter/sec RA = 290
22552 deg
ZDOT = 5909
295569 TA = 330
51874
MA = 330
70154
Ha = 193
737 n
mi
Hp = 174
541
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4862877
70 X = 1559384
82
Y = -21177986
96 feet Y = -6438043
89 meter
Z = -3450232
61 Z = -1044243
92
XDOT = 16289
508439 XDOT = 4933
841060
YDOT = 623
811692 feet/sec YDOT = 245
484334 meter/sec
ZDOT = 19387
452654 ZDOT = 5933
339710
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18164450
87 X = 5536524
63
Y = -11932822
53 feet Y = -3637124
31 meter
Z = -3423344
43 Z = -1043435
38
XDOT = 10394
449082 XDOT = 3168
228080
YDOT = 10309
370596 feet/sec YDOT = 3142
296158 meter/sec
ZDOT = 19477
438279 ZDOT = 5936
723188
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 06357
62701002
00020000 00000-0 20000-3 0 9110
2 25544 51
6360 290
8680 0023578 9
9348 350
2277 15
76346264 23054
Satellite: ISS
Catalog Number: 25544
Epoch time: 06357
62701002 = yrday
fracday
Element set: 911
Inclination: 51
6360 deg
RA of node: 290
8680 deg
Eccentricity:
0023578
Arg of perigee: 9
9348 deg
Mean anomaly: 350
2277 deg
Mean motion: 15
76346264 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2305
Checksum: 286
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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