Date:
December 19th 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 2203)
---------------------------------------
Vector Time (GMT): 2006/351/04:14:33
797
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1995388
22 A = 6714517
55 meter
Y = 3713034
13 meter E =
0023957
Z = 5231758
69 I = 51
42697
XDOT = -6419
955315 Wp = 350
30678
YDOT = 4219
314287 meter/sec RA = 323
57395 deg
ZDOT = -523
009813 TA = 104
81001
MA = 104
54449
Ha = 193
117 n
mi
Hp = 176
688
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6546549
29 X = 1928304
93
Y = 12181870
50 feet Y = 3734971
87 meter
Z = 17164562
65 Z = 5241290
00
XDOT = -21062
845522 XDOT = -6464
118408
YDOT = 13842
894644 feet/sec YDOT = 4147
275925 meter/sec
ZDOT = -1715
911459 ZDOT = -554
305128
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 847782
39 X = 258404
07
Y = -13758529
62 feet Y = -4193599
83 meter
Z = 17200628
33 Z = 5242751
52
XDOT = 24179
279771 XDOT = 7369
844474
YDOT = -894
819695 feet/sec YDOT = -272
741043 meter/sec
ZDOT = -1832
470676 ZDOT = -558
537062
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
22343171
00020000 00000-0 20000-3 0 9007
2 25544 51
6363 323
8655 0023413 344
0911 15
9515 15
76000429 22041
Satellite: ISS
Catalog Number: 25544
Epoch time: 06351
22343171 = yrday
fracday
Element set: 900
Inclination: 51
6363 deg
RA of node: 323
8655 deg
Eccentricity:
0023413
Arg of perigee: 344
0911 deg
Mean anomaly: 15
9515 deg
Mean motion: 15
76000429 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2204
Checksum: 250
Coasting Arc #2 (Orbit 2219)
---------------------------------------
Vector Time (GMT): 2006/352/04:14:33
797
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5491121
81 A = 6725934
26 meter
Y = -3682393
89 meter E =
0031129
Z = 1115590
04 I = 51
44328
XDOT = 1891
728606 Wp = 12
45964
YDOT = 4608
605710 meter/sec RA = 318
42473 deg
ZDOT = 5900
463455 TA = 359
82491
MA = 359
82600
Ha = 193
267 n
mi
Hp = 176
490
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18015491
52 X = 5526471
34
Y = -12081344
77 feet Y = -3620791
64 meter
Z = 3660072
30 Z = 1142351
55
XDOT = 6206
458681 XDOT = 1811
390162
YDOT = 15120
097475 feet/sec YDOT = 4629
309936 meter/sec
ZDOT = 19358
475902 ZDOT = 5909
459188
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21635504
63 X = -6594501
81
Y = 1297006
89 feet Y = 395327
70 meter
Z = 3759743
04 Z = 1145969
68
XDOT = 2498
107482 XDOT = 761
423161
YDOT = -14547
965755 feet/sec YDOT = -4434
219962 meter/sec
ZDOT = 19392
639753 ZDOT = 5910
876597
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
23798433
00020000 00000-0 20000-3 0 9015
2 25544 51
6362 318
6398 0023399 348
3480 11
7140 15
76002524 22201
Satellite: ISS
Catalog Number: 25544
Epoch time: 06352
23798433 = yrday
fracday
Element set: 901
Inclination: 51
6362 deg
RA of node: 318
6398 deg
Eccentricity:
0023399
Arg of perigee: 348
3480 deg
Mean anomaly: 11
7140 deg
Mean motion: 15
76002524 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2220
Checksum: 278
Coasting Arc #3 (Orbit 2234)
---------------------------------------
Vector Time (GMT): 2006/353/04:14:33
797
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1332049
32 A = 6715566
11 meter
Y = -4347445
27 meter E =
0021759
Z = -4943757
83 I = 51
38793
XDOT = 6148
859643 Wp = 24
57921
YDOT = -4170
224692 meter/sec RA = 313
23054 deg
ZDOT = 2033
152925 TA = 265
03923
MA = 265
28767
Ha = 193
340 n
mi
Hp = 176
131
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4370240
55 X = -1259320
46
Y = -14263271
88 feet Y = -4361933
46 meter
Z = -16219677
92 Z = -4950053
11
XDOT = 20173
424024 XDOT = 6185
157896
YDOT = -13681
839542 feet/sec YDOT = -4101
262138 meter/sec
ZDOT = 6670
449229 ZDOT = 2063
111818
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3288032
37 X = -1002192
27
Y = 14524066
20 feet Y = 4426935
38 meter
Z = -16243713
35 Z = -4951083
83
XDOT = -23202
398144 XDOT = -7072
090954
YDOT = 2249
210065 feet/sec YDOT = 685
559228 meter/sec
ZDOT = 6782
031071 ZDOT = 2067
163070
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
18909497
00020000 00000-0 20000-3 0 9025
2 25544 51
6355 313
7409 0023353 352
0047 8
0742 15
76079297 22357
Satellite: ISS
Catalog Number: 25544
Epoch time: 06353
18909497 = yrday
fracday
Element set: 902
Inclination: 51
6355 deg
RA of node: 313
7409 deg
Eccentricity:
0023353
Arg of perigee: 352
0047 deg
Mean anomaly: 8
0742 deg
Mean motion: 15
76079297 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2235
Checksum: 294
Coasting Arc #4 (Orbit 2250)
---------------------------------------
Vector Time (GMT): 2006/354/04:14:33
797
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5215686
72 A = 6723513
29 meter
Y = 3495434
59 meter E =
0019768
Z = -2439485
54 I = 51
39606
XDOT = -1142
008149 Wp = 6
56165
YDOT = -5427
536101 meter/sec RA = 308
09912 deg
ZDOT = -5320
146423 TA = 201
04709
MA = 201
12855
Ha = 193
482 n
mi
Hp = 175
815
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17111833
07 X = -5242534
88
Y = 11467961
26 feet Y = 3436960
23 meter
Z = -8003561
47 Z = -2464888
03
XDOT = -3746
745896 XDOT = -1055
387366
YDOT = -17806
876972 feet/sec YDOT = -5439
821342 meter/sec
ZDOT = -17454
548633 ZDOT = -5325
484952
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20470169
16 X = 6239307
56
Y = -1943588
94 feet Y = -592405
91 meter
Z = -8098184
93 Z = -2468326
77
XDOT = -5423
001896 XDOT = -1652
930978
YDOT = 15900
170787 feet/sec YDOT = 4846
372056 meter/sec
ZDOT = -17475
129500 ZDOT = -5326
419472
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
20358184
00020000 00000-0 20000-3 0 9031
2 25544 51
6349 308
5139 0023267 355
9736 4
1238 15
76114929 22510
Satellite: ISS
Catalog Number: 25544
Epoch time: 06354
20358184 = yrday
fracday
Element set: 903
Inclination: 51
6349 deg
RA of node: 308
5139 deg
Eccentricity:
0023267
Arg of perigee: 355
9736 deg
Mean anomaly: 4
1238 deg
Mean motion: 15
76114929 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2251
Checksum: 293
Coasting Arc #5 (Orbit 2266)
---------------------------------------
Vector Time (GMT): 2006/355/04:14:33
797
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 712201
37 A = 6718037
69 meter
Y = 5159112
81 meter E =
0027892
Z = 4252137
50 I = 51
36254
XDOT = -5749
575947 Wp = 19
09756
YDOT = 3717
869449 meter/sec RA = 302
88133 deg
ZDOT = -3515
360681 TA = 106
83954
MA = 106
53344
Ha = 193
520 n
mi
Hp = 175
472
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2336618
67 X = 633802
42
Y = 16926223
12 feet Y = 5166637
88 meter
Z = 13950582
35 Z = 4255407
92
XDOT = -18863
438145 XDOT = -5773
645395
YDOT = 12197
734414 feet/sec YDOT = 3653
440588 meter/sec
ZDOT = -11533
335567 ZDOT = -3543
349862
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5808520
06 X = 1770436
91
Y = -16058022
57 feet Y = -4894485
28 meter
Z = 13963401
08 Z = 4256044
65
XDOT = 21136
064358 XDOT = 6442
272416
YDOT = -2566
917792 feet/sec YDOT = -782
396543 meter/sec
ZDOT = -11637
616929 ZDOT = -3547
145640
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
21803313
00020000 00000-0 20000-3 0 9043
2 25544 51
6358 303
2865 0023352 359
5050
6087 15
76204757 22671
Satellite: ISS
Catalog Number: 25544
Epoch time: 06355
21803313 = yrday
fracday
Element set: 904
Inclination: 51
6358 deg
RA of node: 303
2865 deg
Eccentricity:
0023352
Arg of perigee: 359
5050 deg
Mean anomaly:
6087 deg
Mean motion: 15
76204757 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2267
Checksum: 276
Coasting Arc #6 (Orbit 2282)
---------------------------------------
Vector Time (GMT): 2006/356/04:14:33
797
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4818286
68 A = 6719981
17 meter
Y = -2921269
48 meter E =
0025753
Z = 3630720
89 I = 51
35459
XDOT = 583
236791 Wp = 30
83700
YDOT = 6354
352183 meter/sec RA = 297
76018 deg
ZDOT = 4346
971886 TA = 13
07131
MA = 13
00469
Ha = 193
483 n
mi
Hp = 175
243
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15808027
18 X = 4832957
35
Y = -9584217
46 feet Y = -2867307
35 meter
Z = 11911813
95 Z = 3654163
10
XDOT = 1913
506532 XDOT = 491
021517
YDOT = 20847
612150 feet/sec YDOT = 6360
357878 meter/sec
ZDOT = 14261
718786 ZDOT = 4349
582387
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18364430
64 X = -5597478
46
Y = 1552286
67 feet Y = 473136
98 meter
Z = 11999181
33 Z = 3657350
47
XDOT = 7774
744996 XDOT = 2369
742275
YDOT = -18136
102989 feet/sec YDOT = -5527
884191 meter/sec
ZDOT = 14272
211335 ZDOT = 4350
170015
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
23245314
00020000 00000-0 20000-3 0 9058
2 25544 51
6352 298
0597 0023210 3
7815 356
3520 15
76230061 22836
Satellite: ISS
Catalog Number: 25544
Epoch time: 06356
23245314 = yrday
fracday
Element set: 905
Inclination: 51
6352 deg
RA of node: 298
0597 deg
Eccentricity:
0023210
Arg of perigee: 3
7815 deg
Mean anomaly: 356
3520 deg
Mean motion: 15
76230061 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2283
Checksum: 266
Coasting Arc #7 (Orbit 2297)
---------------------------------------
Vector Time (GMT): 2006/357/04:14:33
797
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -363979
01 A = 6721092
60 meter
Y = -5870373
72 meter E =
0024787
Z = -3233236
64 I = 51
34609
XDOT = 5325
759695 Wp = 17
91955
YDOT = -2926
983211 meter/sec RA = 292
53553 deg
ZDOT = 4747
640206 TA = 303
99312
MA = 304
22837
Ha = 193
620 n
mi
Hp = 174
893
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1194156
85 X = -282602
30
Y = -19259756
31 feet Y = -5873988
42 meter
Z = -10607731
76 Z = -3234808
11
XDOT = 17472
964878 XDOT = 5335
030879
YDOT = -9602
963291 feet/sec YDOT = -2867
376528 meter/sec
ZDOT = 15576
247394 ZDOT = 4773
534533
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7272291
40 X = -2216594
42
Y = 17870053
64 feet Y = 5446792
35 meter
Z = -10614290
25 Z = -3235235
67
XDOT = -18524
162703 XDOT = -5646
164792
YDOT = 1706
714049 feet/sec YDOT = 520
206442 meter/sec
ZDOT = 15672
791947 ZDOT = 4777
066985
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
18344153
00020000 00000-0 20000-3 0 9065
2 25544 51
6346 293
1597 0023213 7
6437 352
5076 15
76286911 22986
Satellite: ISS
Catalog Number: 25544
Epoch time: 06357
18344153 = yrday
fracday
Element set: 906
Inclination: 51
6346 deg
RA of node: 293
1597 deg
Eccentricity:
0023213
Arg of perigee: 7
6437 deg
Mean anomaly: 352
5076 deg
Mean motion: 15
76286911 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2298
Checksum: 303
Coasting Arc #8 (Orbit 2313)
---------------------------------------
Vector Time (GMT): 2006/358/04:14:33
797
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4487018
84 A = 6716437
39 meter
Y = 2063398
84 meter E =
0030029
Z = -4577107
03 I = 51
32103
XDOT = -243
550835 Wp = 28
74742
YDOT = -7094
563831 meter/sec RA = 287
40791 deg
ZDOT = -2941
600948 TA = 211
79635
MA = 211
97801
Ha = 193
744 n
mi
Hp = 174
505
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14721190
41 X = -4487524
09
Y = 6769681
22 feet Y = 2013220
28 meter
Z = -15016755
34 Z = -4598905
65
XDOT = -799
051296 XDOT = -149
910734
YDOT = -23276
128056 feet/sec YDOT = -7096
763393 meter/sec
ZDOT = -9650
921744 ZDOT = -2942
557598
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16127195
88 X = 4915569
31
Y = -81017
15 feet Y = -24694
03 meter
Z = -15098078
06 Z = -4601894
19
XDOT = -8991
959108 XDOT = -2740
749136
YDOT = 20308
453752 feet/sec YDOT = 6190
016704 meter/sec
ZDOT = -9655
332845 ZDOT = -2942
945451
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 06358
19779646
00020000 00000-0 20000-3 0 9077
2 25544 51
6348 287
9318 0023183 11
6108 348
5586 15
76308472 23143
Satellite: ISS
Catalog Number: 25544
Epoch time: 06358
19779646 = yrday
fracday
Element set: 907
Inclination: 51
6348 deg
RA of node: 287
9318 deg
Eccentricity:
0023183
Arg of perigee: 11
6108 deg
Mean anomaly: 348
5586 deg
Mean motion: 15
76308472 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2314
Checksum: 322
Coasting Arc #9 (Orbit 2329)
---------------------------------------
Vector Time (GMT): 2006/359/04:14:33
797
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 93612
73 A = 6723892
71 meter
Y = 6477353
56 meter E =
0025383
Z = 1824278
44 I = 51
33947
XDOT = -4968
707097 Wp = 48
59388
YDOT = 1675
887676 meter/sec RA = 282
19216 deg
ZDOT = -5628
235627 TA = 111
09374
MA = 110
82218
Ha = 193
788 n
mi
Hp = 174
205
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 307128
39 X = 12313
18
Y = 21251159
96 feet Y = 6477945
62 meter
Z = 5985165
50 Z = 1824536
42
XDOT = -16301
532472 XDOT = -4959
737189
YDOT = 5498
319146 feet/sec YDOT = 1620
375578 meter/sec
ZDOT = -18465
339985 ZDOT = -5652
351369
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8238539
89 X = 2511106
96
Y = -19591115
83 feet Y = -5971372
11 meter
Z = 5986900
24 Z = 1824807
19
XDOT = 15618
125278 XDOT = 4760
404585
YDOT = 829
991490 feet/sec YDOT = 252
981406 meter/sec
ZDOT = -18555
379877 ZDOT = -5655
679787
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 06359
21211640
00020000 00000-0 20000-3 0 9087
2 25544 51
6344 282
7036 0023331 15
3870 344
7998 15
76405116 23307
Satellite: ISS
Catalog Number: 25544
Epoch time: 06359
21211640 = yrday
fracday
Element set: 908
Inclination: 51
6344 deg
RA of node: 282
7036 deg
Eccentricity:
0023331
Arg of perigee: 15
3870 deg
Mean anomaly: 344
7998 deg
Mean motion: 15
76405116 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2330
Checksum: 276
Coasting Arc #10 (Orbit 2345)
---------------------------------------
Vector Time (GMT): 2006/360/04:14:33
797
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4240247
74 A = 6713629
38 meter
Y = -818306
35 meter E =
0022487
Z = 5127474
73 I = 51
29965
XDOT = 32
519786 Wp = 29
29270
YDOT = 7621
663994 meter/sec RA = 277
04228 deg
ZDOT = 1206
628458 TA = 49
24672
MA = 49
05173
Ha = 193
715 n
mi
Hp = 173
946
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13911573
94 X = 4224174
87
Y = -2684732
13 feet Y = -770979
85 meter
Z = 16822423
66 Z = 5148034
58
XDOT = 106
692210 XDOT = -58
570686
YDOT = 25005
459298 feet/sec YDOT = 7621
518234 meter/sec
ZDOT = 3958
754784 ZDOT = 1206
565824
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13790722
36 X = -4203412
17
Y = -2822156
15 feet Y = -860193
19 meter
Z = 16899261
10 Z = 5150894
78
XDOT = 9309
653179 XDOT = 2837
582289
YDOT = -22118
707498 feet/sec YDOT = -6741
782045 meter/sec
ZDOT = 3959
435989 ZDOT = 1206
836090
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 06360
22640510
00020000 00000-0 20000-3 0 9093
2 25544 51
6336 277
4753 0023213 19
6226 340
5826 15
76434190 23461
Satellite: ISS
Catalog Number: 25544
Epoch time: 06360
22640510 = yrday
fracday
Element set: 909
Inclination: 51
6336 deg
RA of node: 277
4753 deg
Eccentricity:
0023213
Arg of perigee: 19
6226 deg
Mean anomaly: 340
5826 deg
Mean motion: 15
76434190 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2346
Checksum: 276
Coasting Arc #11 (Orbit 2360)
---------------------------------------
Vector Time (GMT): 2006/361/04:14:33
797
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 12209
14 A = 6725198
79 meter
Y = -6700683
81 meter E =
0034594
Z = -255441
41 I = 51
33705
XDOT = 4827
602618 Wp = 29
74162
YDOT = -206
449937 meter/sec RA = 271
85223 deg
ZDOT = 6022
332045 TA = 327
46203
MA = 327
67478
Ha = 193
883 n
mi
Hp = 173
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 40056
22 X = 88377
10
Y = -21983870
78 feet Y = -6700121
39 meter
Z = -838062
37 Z = -255197
59
XDOT = 15838
591266 XDOT = 4800
297076
YDOT = -677
329190 feet/sec YDOT = -152
618128 meter/sec
ZDOT = 19758
307233 ZDOT = 6045
718117
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8125547
79 X = -2476666
97
Y = 20427134
44 feet Y = 6226190
58 meter
Z = -837961
30 Z = -255410
60
XDOT = -13386
331886 XDOT = -4080
153959
YDOT = -4561
345260 feet/sec YDOT = -1390
298035 meter/sec
ZDOT = 19845
796018 ZDOT = 6048
998626
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 06361
17727125
00020000 00000-0 20000-3 0 9108
2 25544 51
6341 272
5740 0023314 23
0877 337
1330 15
76449937 23616
Satellite: ISS
Catalog Number: 25544
Epoch time: 06361
17727125 = yrday
fracday
Element set: 910
Inclination: 51
6341 deg
RA of node: 272
5740 deg
Eccentricity:
0023314
Arg of perigee: 23
0877 deg
Mean anomaly: 337
1330 deg
Mean motion: 15
76449937 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2361
Checksum: 276
Coasting Arc #12 (Orbit 2376)
---------------------------------------
Vector Time (GMT): 2006/362/04:14:33
797
Vector Time (MET): N/A
Weight (LBS) : 473517
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4217402
53 A = 6713143
17 meter
Y = -508710
03 meter E =
0031744
Z = -5217977
39 I = 51
29764
XDOT = 103
839465 Wp = 52
61134
YDOT = -7656
772348 meter/sec RA = 266
67062 deg
ZDOT = 684
381414 TA = 223
81234
MA = 224
06461
Ha = 193
852 n
mi
Hp = 173
324
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13836622
47 X = -4186052
60
Y = -1668996
17 feet Y = -555695
66 meter
Z = -17119348
38 Z = -5238389
45
XDOT = 340
680661 XDOT = 186
126250
YDOT = -25120
644186 feet/sec YDOT = -7655
151125 meter/sec
ZDOT = 2245
345845 ZDOT = 685
085111
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12276840
48 X = 3741980
98
Y = 6394803
19 feet Y = 1949136
01 meter
Z = -17195797
12 Z = -5241278
96
XDOT = -8675
196055 XDOT = -2644
199758
YDOT = 22505
355416 feet/sec YDOT = 6859
632331 meter/sec
ZDOT = 2247
048431 ZDOT = 684
900362
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 06362
19149664
00020000 00000-0 20000-3 0 9118
2 25544 51
6345 267
3451 0023131 26
8923 333
3435 15
76499674 23775
Satellite: ISS
Catalog Number: 25544
Epoch time: 06362
19149664 = yrday
fracday
Element set: 911
Inclination: 51
6345 deg
RA of node: 267
3451 deg
Eccentricity:
0023131
Arg of perigee: 26
8923 deg
Mean anomaly: 333
3435 deg
Mean motion: 15
76499674 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2377
Checksum: 305
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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