Date:
November 26th 2006
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 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
333/23:12:24
825 6
6 12
0 12
0
N/A 9
9 0
1 188
6
000/00:20:49
650 1
0 -0
2 179
3
Coasting Arc #1 (Orbit 1813)
---------------------------------------
Vector Time (GMT): 2006/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3682176
36 A = 6710089
98 meter
Y = 2995558
11 meter E =
0008274
Z = -4746531
25 I = 51
93695
XDOT = -2166
521891 Wp = 177
12699
YDOT = 6896
744274 meter/sec RA = 90
66734 deg
ZDOT = 2663
972876 TA = 118
96593
MA = 118
88296
Ha = 183
041 n
mi
Hp = 179
516
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12080631
11 X = 3671464
29
Y = 9827946
55 feet Y = 3036675
00 meter
Z = -15572609
10 Z = -4728668
41
XDOT = -7108
011453 XDOT = -2256
422640
YDOT = 22627
113759 feet/sec YDOT = 6872
013999 meter/sec
ZDOT = 8740
068492 ZDOT = 2653
230227
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14534335
87 X = -4430065
57
Y = 5776583
83 feet Y = 1760702
75 meter
Z = -15505498
88 Z = -4726076
06
XDOT = -15780
574783 XDOT = -4809
919194
YDOT = -16280
747146 feet/sec YDOT = -4962
371730 meter/sec
ZDOT = 8700
780564 ZDOT = 2651
997916
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 06326
51125139
00020000 00000-0 20000-3 0 9003
2 25544 51
6325 91
3612 0011361 246
0678 113
9298 15
78340597 18147
Satellite: ISS
Catalog Number: 25544
Epoch time: 06326
51125139 = yrday
fracday
Element set: 900
Inclination: 51
6325 deg
RA of node: 91
3612 deg
Eccentricity:
0011361
Arg of perigee: 246
0678 deg
Mean anomaly: 113
9298 deg
Mean motion: 15
78340597 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1814
Checksum: 282
Coasting Arc #2 (Orbit 1829)
---------------------------------------
Vector Time (GMT): 2006/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2370059
47 A = 6714330
74 meter
Y = -5190049
54 meter E =
0006363
Z = -3531804
39 I = 51
95134
XDOT = 3921
688791 Wp = 239
11007
YDOT = 4865
302927 meter/sec RA = 85
56635 deg
ZDOT = -4515
203867 TA = 342
83100
MA = 342
85251
Ha = 182
714 n
mi
Hp = 179
527
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7775785
65 X = 2445076
37
Y = -17027721
58 feet Y = -5163126
26 meter
Z = -11587284
74 Z = -3520108
95
XDOT = 12866
433042 XDOT = 3888
927291
YDOT = 15962
279945 feet/sec YDOT = 4908
974907 meter/sec
ZDOT = -14813
660981 ZDOT = -4496
230800
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11247385
29 X = 3428203
04
Y = 14996623
18 feet Y = 4570970
74 meter
Z = -11544216
28 Z = -3518677
12
XDOT = -19106
724421 XDOT = -5823
729603
YDOT = 2974
626993 feet/sec YDOT = 906
666308 meter/sec
ZDOT = -14742
170601 ZDOT = -4493
413599
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 06327
52427401
00020000 00000-0 20000-3 0 9013
2 25544 51
6332 86
1241 0011341 250
3870 109
6071 15
78377601 18300
Satellite: ISS
Catalog Number: 25544
Epoch time: 06327
52427401 = yrday
fracday
Element set: 901
Inclination: 51
6332 deg
RA of node: 86
1241 deg
Eccentricity:
0011341
Arg of perigee: 250
3870 deg
Mean anomaly: 109
6071 deg
Mean motion: 15
78377601 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1830
Checksum: 255
Coasting Arc #3 (Orbit 1845)
---------------------------------------
Vector Time (GMT): 2006/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3112799
13 A = 6716235
97 meter
Y = -5246268
32 meter E =
0005966
Z = 2800267
44 I = 51
95505
XDOT = 3289
578115 Wp = 154
36108
YDOT = -4699
530196 meter/sec RA = 80
37036 deg
ZDOT = -5149
012553 TA = 353
65081
MA = 353
65837
Ha = 182
307 n
mi
Hp = 179
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10212595
58 X = -3067506
66
Y = -17212166
39 feet Y = -5280824
52 meter
Z = 9187229
13 Z = 2785254
51
XDOT = 10792
579118 XDOT = 3366
897752
YDOT = -15418
406156 feet/sec YDOT = -4662
311252 meter/sec
ZDOT = -16893
085804 ZDOT = -5132
844419
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20004898
01 X = 6097492
91
Y = -1182876
21 feet Y = -360540
67 meter
Z = 9130488
43 Z = 2782972
87
XDOT = 8586
027107 XDOT = 2617
021062
YDOT = 15304
783209 feet/sec YDOT = 4664
897922 meter/sec
ZDOT = -16833
234863 ZDOT = -5130
769986
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 06328
53726323
00020000 00000-0 20000-3 0 9021
2 25544 51
6336 80
8878 0011211 254
4881 105
5047 15
78422539 18460
Satellite: ISS
Catalog Number: 25544
Epoch time: 06328
53726323 = yrday
fracday
Element set: 902
Inclination: 51
6336 deg
RA of node: 80
8878 deg
Eccentricity:
0011211
Arg of perigee: 254
4881 deg
Mean anomaly: 105
5047 deg
Mean motion: 15
78422539 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1846
Checksum: 293
Coasting Arc #4 (Orbit 1861)
---------------------------------------
Vector Time (GMT): 2006/329/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3392673
07 A = 6708112
73 meter
Y = 2770491
43 meter E =
0008572
Z = 5087763
68 I = 51
92333
XDOT = -3128
299797 Wp = 234
10105
YDOT = -6845
051028 meter/sec RA = 75
25855 deg
ZDOT = 1638
349713 TA = 200
20491
MA = 200
23885
Ha = 181
641 n
mi
Hp = 179
492
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11130817
17 X = -3448116
62
Y = 9089538
81 feet Y = 2732242
01 meter
Z = 16692138
06 Z = 5071147
61
XDOT = -10263
450777 XDOT = -3059
483859
YDOT = -22457
516496 feet/sec YDOT = -6879
648858 meter/sec
ZDOT = 5375
163099 ZDOT = 1623
318540
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3142244
24 X = -957756
04
Y = -14096073
51 feet Y = -4296483
21 meter
Z = 16630372
59 Z = 5068937
56
XDOT = 23663
732079 XDOT = 7212
705538
YDOT = 1010
964456 feet/sec YDOT = 308
141966 meter/sec
ZDOT = 5318
157820 ZDOT = 1620
974504
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 06329
55021665
00020000 00000-0 20000-3 0 9032
2 25544 51
6344 75
6502 0011215 259
4253 100
5649 15
78524483 18629
Satellite: ISS
Catalog Number: 25544
Epoch time: 06329
55021665 = yrday
fracday
Element set: 903
Inclination: 51
6344 deg
RA of node: 75
6502 deg
Eccentricity:
0011215
Arg of perigee: 259
4253 deg
Mean anomaly: 100
5649 deg
Mean motion: 15
78524483 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1862
Checksum: 283
Coasting Arc #5 (Orbit 1877)
---------------------------------------
Vector Time (GMT): 2006/330/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2229170
59 A = 6719307
35 meter
Y = 6332978
34 meter E =
0007769
Z = 76557
96 I = 51
95278
XDOT = -4503
640187 Wp = 344
82127
YDOT = 1513
633574 meter/sec RA = 70
09691 deg
ZDOT = 6069
307983 TA = 16
00835
MA = 15
98381
Ha = 181
109 n
mi
Hp = 179
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7313551
80 X = 2157816
75
Y = 20777487
98 feet Y = 6357507
19 meter
Z = 251174
41 Z = 87214
73
XDOT = -14775
722398 XDOT = -4549
714932
YDOT = 4965
989415 feet/sec YDOT = 1463
013086 meter/sec
ZDOT = 19912
427767 ZDOT = 6047
317395
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21903349
05 X = -6676140
79
Y = -2326651
11 feet Y = -709163
26 meter
Z = 291771
05 Z = 88931
82
XDOT = 1743
487529 XDOT = 531
414999
YDOT = -13977
833010 feet/sec YDOT = -4260
443501 meter/sec
ZDOT = 19830
417673 ZDOT = 6044
311307
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 06330
56313967
00020000 00000-0 20000-3 0 9045
2 25544 51
6345 70
4129 0011056 264
2933 95
6972 15
78535181 18787
Satellite: ISS
Catalog Number: 25544
Epoch time: 06330
56313967 = yrday
fracday
Element set: 904
Inclination: 51
6345 deg
RA of node: 70
4129 deg
Eccentricity:
0011056
Arg of perigee: 264
2933 deg
Mean anomaly: 95
6972 deg
Mean motion: 15
78535181 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1878
Checksum: 304
Coasting Arc #6 (Orbit 1892)
---------------------------------------
Vector Time (GMT): 2006/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4430877
17 A = 6708063
54 meter
Y = 153051
13 meter E =
0004036
Z = -5036718
71 I = 51
90450
XDOT = 1821
761151 Wp = 150
58651
YDOT = 7263
130914 meter/sec RA = 64
93164 deg
ZDOT = 1820
503988 TA = 136
89778
MA = 136
86617
Ha = 180
808 n
mi
Hp = 179
041
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14536998
60 X = 4453304
06
Y = 502136
27 feet Y = 202725
49 meter
Z = -16524667
67 Z = -5015138
87
XDOT = 5976
906664 XDOT = 1731
564669
YDOT = 23829
169665 feet/sec YDOT = 7282
998390 meter/sec
ZDOT = 5972
782113 ZDOT = 1829
135693
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6515442
34 X = -1985906
82
Y = 13106692
69 feet Y = 3994919
93 meter
Z = -16443987
61 Z = -5012127
42
XDOT = -23195
328653 XDOT = -7069
936174
YDOT = -3983
686632 feet/sec YDOT = -1214
227686 meter/sec
ZDOT = 6005
923715 ZDOT = 1830
605548
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 06331
51272280
00020000 00000-0 20000-3 0 9054
2 25544 51
6343 65
5034 0010990 268
1728 91
8179 15
78622099 18935
Satellite: ISS
Catalog Number: 25544
Epoch time: 06331
51272280 = yrday
fracday
Element set: 905
Inclination: 51
6343 deg
RA of node: 65
5034 deg
Eccentricity:
0010990
Arg of perigee: 268
1728 deg
Mean anomaly: 91
8179 deg
Mean motion: 15
78622099 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1893
Checksum: 301
Coasting Arc #7 (Orbit 1908)
---------------------------------------
Vector Time (GMT): 2006/332/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -772622
91 A = 6715127
10 meter
Y = -5966598
85 meter E =
0006874
Z = -2975310
45 I = 51
91497
XDOT = 5579
152436 Wp = 260
10025
YDOT = 1780
944974 meter/sec RA = 59
81935 deg
ZDOT = -5011
669444 TA = 314
17676
MA = 314
23323
Ha = 180
694 n
mi
Hp = 179
005
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2534852
08 X = -691392
50
Y = -19575455
54 feet Y = -5974784
38 meter
Z = -9761517
24 Z = -2978866
96
XDOT = 18304
305892 XDOT = 5583
169012
YDOT = 5842
995321 feet/sec YDOT = 1843
356928 meter/sec
ZDOT = -16442
485052 ZDOT = -4984
555802
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18942926
61 X = 5773804
03
Y = 5524098
73 feet Y = 1683745
29 meter
Z = -9775531
61 Z = -2979582
04
XDOT = -12285
643308 XDOT = -3744
664080
YDOT = 13162
408187 feet/sec YDOT = 4011
902015 meter/sec
ZDOT = -16340
921570 ZDOT = -4980
712895
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 06332
52558036
00020000 00000-0 20000-3 0 9063
2 25544 51
6340 60
2655 0011026 272
2702 87
7201 15
78638629 19096
Satellite: ISS
Catalog Number: 25544
Epoch time: 06332
52558036 = yrday
fracday
Element set: 906
Inclination: 51
6340 deg
RA of node: 60
2655 deg
Eccentricity:
0011026
Arg of perigee: 272
2702 deg
Mean anomaly: 87
7201 deg
Mean motion: 15
78638629 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1909
Checksum: 281
Coasting Arc #8 (Orbit 1924)
---------------------------------------
Vector Time (GMT): 2006/333/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 470356
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5145733
08 A = 6714160
74 meter
Y = -2776122
94 meter E =
0002184
Z = 3300003
82 I = 51
89686
XDOT = 239
127723 Wp = 64
55154
YDOT = -6074
798815 meter/sec RA = 54
61695 deg
ZDOT = -4734
207856 TA = 76
79328
MA = 76
76892
Ha = 180
921 n
mi
Hp = 179
213
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16882326
36 X = -5130338
68
Y = -9108014
89 feet Y = -2833579
48 meter
Z = 10826784
19 Z = 3275042
76
XDOT = 784
539772 XDOT = 330
037438
YDOT = -19930
442307 feet/sec YDOT = -6071
616212 meter/sec
ZDOT = -15532
178005 ZDOT = -4732
825647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14897058
53 X = 4540623
44
Y = -12168209
85 feet Y = -3708870
36 meter
Z = 10733147
29 Z = 3271463
30
XDOT = 17193
577573 XDOT = 5240
602444
YDOT = 7343
217854 feet/sec YDOT = 2238
212802 meter/sec
ZDOT = -15527
742377 ZDOT = -4732
855877
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 06333
53840503
00020000 00000-0 20000-3 0 9079
2 25544 51
6342 55
0274 0010902 277
2504 82
7422 15
78699254 19253
Satellite: ISS
Catalog Number: 25544
Epoch time: 06333
53840503 = yrday
fracday
Element set: 907
Inclination: 51
6342 deg
RA of node: 55
0274 deg
Eccentricity:
0010902
Arg of perigee: 277
2504 deg
Mean anomaly: 82
7422 deg
Mean motion: 15
78699254 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1925
Checksum: 284
Coasting Arc #9 (Orbit 1931)
---------------------------------------
Vector Time (GMT): 2006/333/23:22:49
650
Vector Time (MET): N/A
Weight (LBS) : 469585
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5249658
25 A = 6721026
52 meter
Y = 2252528
51 meter E =
0016099
Z = -3524842
85 I = 51
88652
XDOT = 362
601884 Wp = 280
29542
YDOT = 6241
080586 meter/sec RA = 52
17382 deg
ZDOT = 4513
874643 TA = 37
83643
MA = 37
72337
Ha = 188
589 n
mi
Hp = 179
270
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17223288
21 X = 5241203
31
Y = 7390185
41 feet Y = 2311186
01 meter
Z = -11564445
04 Z = -3499360
02
XDOT = 1189
638726 XDOT = 270
858360
YDOT = 20475
986176 feet/sec YDOT = 6244
622209 meter/sec
ZDOT = 14809
300010 ZDOT = 4515
413660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15299507
50 X = 4663289
89
Y = -10926197
55 feet Y = -3330305
01 meter
Z = -11468921
64 Z = -3495727
32
XDOT = 17271
051731 XDOT = 5264
216568
YDOT = 8581
926923 feet/sec YDOT = 2615
771326 meter/sec
ZDOT = 14815
801606 ZDOT = 4515
856329
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 06333
98151044
00020000 00000-0 20000-3 0 9084
2 25544 51
6342 52
7370 0021259 279
2530 80
6230 15
76044818 19322
Satellite: ISS
Catalog Number: 25544
Epoch time: 06333
98151044 = yrday
fracday
Element set: 908
Inclination: 51
6342 deg
RA of node: 52
7370 deg
Eccentricity:
0021259
Arg of perigee: 279
2530 deg
Mean anomaly: 80
6230 deg
Mean motion: 15
76044818 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1932
Checksum: 278
Coasting Arc #10 (Orbit 1947)
---------------------------------------
Vector Time (GMT): 2006/334/23:22:49
650
Vector Time (MET): N/A
Weight (LBS) : 469585
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -84678
33 A = 6717942
22 meter
Y = -5111408
84 meter E =
0014652
Z = -4352875
13 I = 51
85912
XDOT = 6299
285662 Wp = 303
58274
YDOT = 2826
149334 meter/sec RA = 47
08951 deg
ZDOT = -3425
029140 TA = 291
93436
MA = 292
09004
Ha = 188
563 n
mi
Hp = 179
185
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -277816
05 X = -6369
62
Y = -16769714
04 feet Y = -5111917
65 meter
Z = -14281086
37 Z = -4353096
60
XDOT = 20666
947711 XDOT = 6283
853607
YDOT = 9272
143484 feet/sec YDOT = 2896
505370 meter/sec
ZDOT = -11236
972245 ZDOT = -3394
463877
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14574067
81 X = -4442175
87
Y = -8297953
14 feet Y = -2529216
12 meter
Z = -14282522
18 Z = -4353312
76
XDOT = 17866
782827 XDOT = 5445
795406
YDOT = -12145
086281 feet/sec YDOT = -3701
822298 meter/sec
ZDOT = -11122
385261 ZDOT = -3390
103028
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 06334
99601685
00020000 00000-0 20000-3 0 9098
2 25544 51
6350 47
5110 0021245 283
5579 76
3219 15
76097862 19484
Satellite: ISS
Catalog Number: 25544
Epoch time: 06334
99601685 = yrday
fracday
Element set: 909
Inclination: 51
6350 deg
RA of node: 47
5110 deg
Eccentricity:
0021245
Arg of perigee: 283
5579 deg
Mean anomaly: 76
3219 deg
Mean motion: 15
76097862 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1948
Checksum: 314
Coasting Arc #11 (Orbit 1963)
---------------------------------------
Vector Time (GMT): 2006/335/23:22:49
650
Vector Time (MET): N/A
Weight (LBS) : 469585
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5719401
49 A = 6723811
54 meter
Y = -2628322
56 meter E =
0007191
Z = 2373912
23 I = 51
85826
XDOT = 270
811834 Wp = 287
70371
YDOT = -5465
908585 meter/sec RA = 41
90827 deg
ZDOT = -5410
443468 TA = 225
63703
MA = 225
69596
Ha = 188
709 n
mi
Hp = 179
273
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18764440
57 X = -5701118
45
Y = -8623105
52 feet Y = -2692178
06 meter
Z = 7788425
96 Z = 2346170
88
XDOT = 888
490270 XDOT = 358
195865
YDOT = -17932
770947 feet/sec YDOT = -5462
391164 meter/sec
ZDOT = -17750
798781 ZDOT = -5408
916040
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16734382
74 X = -5100639
86
Y = 12166834
67 feet Y = 3708451
21 meter
Z = 7684420
98 Z = 2342211
52
XDOT = -14260
141965 XDOT = -4346
491271
YDOT = -8429
113550 feet/sec YDOT = -2569
193810 meter/sec
ZDOT = -17745
731494 ZDOT = -5408
898959
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 06336
01049670
00020000 00000-0 20000-3 0 9105
2 25544 51
6349 42
2842 0021163 287
3248 72
5602 15
76101628 19648
Satellite: ISS
Catalog Number: 25544
Epoch time: 06336
01049670 = yrday
fracday
Element set: 910
Inclination: 51
6349 deg
RA of node: 42
2842 deg
Eccentricity:
0021163
Arg of perigee: 287
3248 deg
Mean anomaly: 72
5602 deg
Mean motion: 15
76101628 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1964
Checksum: 275
Coasting Arc #12 (Orbit 1979)
---------------------------------------
Vector Time (GMT): 2006/336/23:22:49
650
Vector Time (MET): N/A
Weight (LBS) : 469585
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -649374
98 A = 6715125
39 meter
Y = 4436832
40 meter E =
0015761
Z = 5010232
51 I = 51
80830
XDOT = -6748
003632 Wp = 286
28078
YDOT = -3154
604969 meter/sec RA = 36
80571 deg
ZDOT = 1928
272433 TA = 145
17707
MA = 145
07384
Ha = 188
866 n
mi
Hp = 179
092
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2130495
33 X = -723279
42
Y = 14556536
74 feet Y = 4429156
92 meter
Z = 16437770
69 Z = 5006898
76
XDOT = -22139
119527 XDOT = -6721
594306
YDOT = -10349
753835 feet/sec YDOT = -3229
917456 meter/sec
ZDOT = 6326
353128 ZDOT = 1895
553566
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11753620
92 X = 3582503
66
Y = 8869995
13 feet Y = 2703574
51 meter
Z = 16425822
93 Z = 5006590
83
XDOT = -18994
491058 XDOT = -5789
520875
YDOT = 13737
924254 feet/sec YDOT = 4187
319313 meter/sec
ZDOT = 6203
682308 ZDOT = 1890
882368
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 06337
02494733
00020000 00000-0 20000-3 0 9112
2 25544 51
6356 37
0567 0021202 291
5707 68
3198 15
76163775 19805
Satellite: ISS
Catalog Number: 25544
Epoch time: 06337
02494733 = yrday
fracday
Element set: 911
Inclination: 51
6356 deg
RA of node: 37
0567 deg
Eccentricity:
0021202
Arg of perigee: 291
5707 deg
Mean anomaly: 68
3198 deg
Mean motion: 15
76163775 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1980
Checksum: 299
Coasting Arc #13 (Orbit 1994)
---------------------------------------
Vector Time (GMT): 2006/337/23:22:49
650
Vector Time (MET): N/A
Weight (LBS) : 469585
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6015448
32 A = 6725510
50 meter
Y = 2820354
00 meter E =
0021371
Z = -959534
04 I = 51
82038
XDOT = -1258
552127 Wp = 322
25486
YDOT = 4730
292542 meter/sec RA = 31
64069 deg
ZDOT = 5960
961374 TA = 27
26802
MA = 27
15598
Ha = 189
062 n
mi
Hp = 178
958
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19735722
83 X = 5988124
99
Y = 9253129
92 feet Y = 2887469
45 meter
Z = -3148077
57 Z = -930376
26
XDOT = -4129
108028 XDOT = -1340
311330
YDOT = 15519
332487 feet/sec YDOT = 4715
760692 meter/sec
ZDOT = 19556
959890 ZDOT = 5954
649287
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17300236
76 X = 5273112
16
Y = -13285229
81 feet Y = -4049338
05 meter
Z = -3038756
03 Z = -926212
84
XDOT = 10863
620326 XDOT = 3311
231475
YDOT = 9637
755270 feet/sec YDOT = 2937
587806 meter/sec
ZDOT = 19533
904058 ZDOT = 5953
933957
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 06337
97597031
00020000 00000-0 20000-3 0 9122
2 25544 51
6358 32
1561 0021289 295
3418 64
5541 15
76215882 19956
Satellite: ISS
Catalog Number: 25544
Epoch time: 06337
97597031 = yrday
fracday
Element set: 912
Inclination: 51
6358 deg
RA of node: 32
1561 deg
Eccentricity:
0021289
Arg of perigee: 295
3418 deg
Mean anomaly: 64
5541 deg
Mean motion: 15
76215882 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1995
Checksum: 310
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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