Date:
January 29th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6996 54 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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 2839)
---------------------------------------
Vector Time (GMT): 2007/026/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4685718
22 A = 6713277
43 meter
Y = 1584099
03 meter E =
0030907
Z = 4528552
65 I = 51
91242
XDOT = 654
551153 Wp = 129
31059
YDOT = -7031
303584 meter/sec RA = 115
46732 deg
ZDOT = 3103
648006 TA = 289
77842
MA = 290
11143
Ha = 192
589 n
mi
Hp = 171
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15373091
29 X = -4725082
26
Y = 5197175
31 feet Y = 1531480
33 meter
Z = 14857456
21 Z = 4505694
16
XDOT = 2147
477535 XDOT = 718
050733
YDOT = -23068
581311 feet/sec YDOT = -7023
629188 meter/sec
ZDOT = 10182
572198 ZDOT = 3106
981561
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11677112
53 X = -3559183
90
Y = -11380819
66 feet Y = -3468873
83 meter
Z = 14771884
07 Z = 4502470
26
XDOT = 20651
001519 XDOT = 6294
425263
YDOT = -7814
825420 feet/sec YDOT = -2381
958788 meter/sec
ZDOT = 10194
179721 ZDOT = 3107
185979
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 07026
53214443
00020000 00000-0 20000-3 0 9000
2 25544 51
6345 116
0096 0022569 135
4273 224
8712 15
77532657 28406
Satellite: ISS
Catalog Number: 25544
Epoch time: 07026
53214443 = yrday
fracday
Element set: 900
Inclination: 51
6345 deg
RA of node: 116
0096 deg
Eccentricity:
0022569
Arg of perigee: 135
4273 deg
Mean anomaly: 224
8712 deg
Mean motion: 15
77532657 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2840
Checksum: 278
Coasting Arc #2 (Orbit 2854)
---------------------------------------
Vector Time (GMT): 2007/027/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1023744
92 A = 6721034
71 meter
Y = 6450548
90 meter E =
0022221
Z = -1630729
39 I = 51
94978
XDOT = -5047
743569 Wp = 118
20515
YDOT = 643
663037 meter/sec RA = 110
28750 deg
ZDOT = 5763
941830 TA = 223
87887
MA = 224
05558
Ha = 192
388 n
mi
Hp = 171
486
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3358743
19 X = -1087878
10
Y = 21163218
17 feet Y = 6438742
37 meter
Z = -5350162
05 Z = -1635857
89
XDOT = -16560
838482 XDOT = -5082
565795
YDOT = 2111
755370 feet/sec YDOT = 587
021139 meter/sec
ZDOT = 18910
570308 ZDOT = 5739
335657
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20232250
17 X = -6166789
85
Y = 7044252
40 feet Y = 2147088
13 meter
Z = -5368589
60 Z = -1636346
11
XDOT = -9207
342458 XDOT = -2806
397981
YDOT = -12225
135731 feet/sec YDOT = -3726
221371 meter/sec
ZDOT = 18818
310649 ZDOT = 5735
821086
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 07027
48236090
00020000 00000-0 20000-3 0 9018
2 25544 51
6346 111
1042 0022347 138
5769 221
7095 15
77505130 28554
Satellite: ISS
Catalog Number: 25544
Epoch time: 07027
48236090 = yrday
fracday
Element set: 901
Inclination: 51
6346 deg
RA of node: 111
1042 deg
Eccentricity:
0022347
Arg of perigee: 138
5769 deg
Mean anomaly: 221
7095 deg
Mean motion: 15
77505130 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2855
Checksum: 274
Coasting Arc #3 (Orbit 2870)
---------------------------------------
Vector Time (GMT): 2007/028/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4131186
83 A = 6710106
21 meter
Y = 571006
00 meter E =
0033040
Z = -5279810
81 I = 51
92152
XDOT = -1635
429175 Wp = 120
51662
YDOT = 7494
691380 meter/sec RA = 105
16499 deg
ZDOT = -487
725620 TA = 144
96882
MA = 144
75105
Ha = 192
263 n
mi
Hp = 171
686
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13553762
56 X = 4150142
68
Y = 1873379
27 feet Y = 617309
78 meter
Z = -17322213
94 Z = -5259695
72
XDOT = -5365
581283 XDOT = -1716
745085
YDOT = 24588
882480 feet/sec YDOT = 7475
948492 meter/sec
ZDOT = -1600
149672 ZDOT = -495
867126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5006184
12 X = 1525884
92
Y = 12836058
83 feet Y = 3912430
73 meter
Z = -17246647
19 Z = -5256778
06
XDOT = -23151
443733 XDOT = -7056
560050
YDOT = 6921
989071 feet/sec YDOT = 2109
822269 meter/sec
ZDOT = -1629
763371 ZDOT = -496
751875
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 07028
49590320
00020000 00000-0 20000-3 0 9020
2 25544 51
6343 105
8709 0022321 142
6132 217
6591 15
77544805 28718
Satellite: ISS
Catalog Number: 25544
Epoch time: 07028
49590320 = yrday
fracday
Element set: 902
Inclination: 51
6343 deg
RA of node: 105
8709 deg
Eccentricity:
0022321
Arg of perigee: 142
6132 deg
Mean anomaly: 217
6591 deg
Mean motion: 15
77544805 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2871
Checksum: 280
Coasting Arc #4 (Orbit 2886)
---------------------------------------
Vector Time (GMT): 2007/029/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1765363
04 A = 6721740
09 meter
Y = -6420544
07 meter E =
0032835
Z = -793205
58 I = 51
96704
XDOT = 4432
736698 Wp = 144
37760
YDOT = 1943
219943 meter/sec RA = 100
02741 deg
ZDOT = -6012
914505 TA = 44
25936
MA = 43
99723
Ha = 192
159 n
mi
Hp = 171
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5791873
49 X = 1840880
44
Y = -21064777
13 feet Y = -6400380
47 meter
Z = -2602380
50 Z = -784446
91
XDOT = 14543
099402 XDOT = 4439
886916
YDOT = 6375
393514 feet/sec YDOT = 1992
829923 meter/sec
ZDOT = -19727
409792 ZDOT = -5991
363141
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21135407
66 X = 6442072
26
Y = -5543562
38 feet Y = -1689677
81 meter
Z = -2570306
84 Z = -783429
53
XDOT = 1430
310784 XDOT = 435
958727
YDOT = 14332
548282 feet/sec YDOT = 4368
560716 meter/sec
ZDOT = -19646
272624 ZDOT = -5988
183896
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 07029
50942492
00020000 00000-0 20000-3 0 9035
2 25544 51
6340 100
6380 0022406 146
1020 214
1582 15
77584043 28879
Satellite: ISS
Catalog Number: 25544
Epoch time: 07029
50942492 = yrday
fracday
Element set: 903
Inclination: 51
6340 deg
RA of node: 100
6380 deg
Eccentricity:
0022406
Arg of perigee: 146
1020 deg
Mean anomaly: 214
1582 deg
Mean motion: 15
77584043 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2887
Checksum: 266
Coasting Arc #5 (Orbit 2902)
---------------------------------------
Vector Time (GMT): 2007/030/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3620629
17 A = 6711254
60 meter
Y = -2768821
00 meter E =
0022748
Z = 4906705
80 I = 51
93703
XDOT = 2349
593929 Wp = 133
48667
YDOT = -7010
383804 meter/sec RA = 94
86093 deg
ZDOT = -2231
128062 TA = 337
99095
MA = 338
08848
Ha = 191
945 n
mi
Hp = 171
837
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11878704
63 X = -3613233
98
Y = -9084058
41 feet Y = -2809268
06 meter
Z = 16098116
14 Z = 4889134
92
XDOT = 7708
641500 XDOT = 2438
648537
YDOT = -22999
946864 feet/sec YDOT = -6983
611173 meter/sec
ZDOT = -7319
973956 ZDOT = -2219
498466
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1598512
32 X = 487226
55
Y = -14939842
13 feet Y = -4553663
88 meter
Z = 16031810
87 Z = 4886495
95
XDOT = 22608
002162 XDOT = 6890
919059
YDOT = -5358
407793 feet/sec YDOT = -1633
242695 meter/sec
ZDOT = -7277
190515 ZDOT = -2218
087669
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 07030
52292293
00020000 00000-0 20000-3 0 9047
2 25544 51
6348 95
4047 0022124 150
0510 210
1925 15
77671081 29038
Satellite: ISS
Catalog Number: 25544
Epoch time: 07030
52292293 = yrday
fracday
Element set: 904
Inclination: 51
6348 deg
RA of node: 95
4047 deg
Eccentricity:
0022124
Arg of perigee: 150
0510 deg
Mean anomaly: 210
1925 deg
Mean motion: 15
77671081 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2903
Checksum: 257
Coasting Arc #6 (Orbit 2918)
---------------------------------------
Vector Time (GMT): 2007/031/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2328781
34 A = 6717845
94 meter
Y = 5539648
94 meter E =
0029540
Z = 3005801
93 I = 51
95977
XDOT = -3916
134025 Wp = 128
29048
YDOT = -4376
978756 meter/sec RA = 89
76181 deg
ZDOT = 4981
875702 TA = 266
32128
MA = 266
65914
Ha = 191
779 n
mi
Hp = 172
039
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7640358
74 X = -2405154
60
Y = 18174701
26 feet Y = 5513179
92 meter
Z = 9861554
88 Z = 2994304
04
XDOT = -12848
208744 XDOT = -3891
099272
YDOT = -14360
166523 feet/sec YDOT = -4420
631612 meter/sec
ZDOT = 16344
736556 ZDOT = 4962
912134
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19486443
23 X = -5939467
90
Y = 3131986
58 feet Y = 954629
51 meter
Z = 9819078
50 Z = 2992855
13
XDOT = 5524
640655 XDOT = 1683
910472
YDOT = -17168
823637 feet/sec YDOT = -5233
057444 meter/sec
ZDOT = 16272
996050 ZDOT = 4960
009196
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 07031
53640273
00020000 00000-0 20000-3 0 9055
2 25544 51
6342 90
1715 0022205 153
5295 206
7009 15
77675078 29195
Satellite: ISS
Catalog Number: 25544
Epoch time: 07031
53640273 = yrday
fracday
Element set: 905
Inclination: 51
6342 deg
RA of node: 90
1715 deg
Eccentricity:
0022205
Arg of perigee: 153
5295 deg
Mean anomaly: 206
7009 deg
Mean motion: 15
77675078 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2919
Checksum: 282
Coasting Arc #7 (Orbit 2933)
---------------------------------------
Vector Time (GMT): 2007/032/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3219309
78 A = 6716273
60 meter
Y = 4751216
04 meter E =
0025042
Z = -3520571
73 I = 51
95281
XDOT = -3041
454956 Wp = 146
18820
YDOT = 5416
589440 meter/sec RA = 84
56985 deg
ZDOT = 4523
807685 TA = 172
20753
MA = 172
16855
Ha = 191
584 n
mi
Hp = 172
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10562039
96 X = 3183043
47
Y = 15587979
13 feet Y = 4787013
61 meter
Z = -11550432
18 Z = -3505020
63
XDOT = -9978
526757 XDOT = -3123
773080
YDOT = 17770
962731 feet/sec YDOT = 5382
117639 meter/sec
ZDOT = 14841
888730 ZDOT = 4508
833203
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7266445
55 X = -2214812
60
Y = 17409755
61 feet Y = 5306493
51 meter
Z = -11491450
88 Z = -3502594
23
XDOT = -19112
483408 XDOT = -5825
484943
YDOT = 1793
607576 feet/sec YDOT = 546
691589 meter/sec
ZDOT = 14786
341853 ZDOT = 4506
876997
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 07032
48652095
00020000 00000-0 20000-3 0 9066
2 25544 51
6335 85
2648 0022176 156
7083 203
5092 15
77720630 29343
Satellite: ISS
Catalog Number: 25544
Epoch time: 07032
48652095 = yrday
fracday
Element set: 906
Inclination: 51
6335 deg
RA of node: 85
2648 deg
Eccentricity:
0022176
Arg of perigee: 156
7083 deg
Mean anomaly: 203
5092 deg
Mean motion: 15
77720630 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2934
Checksum: 291
Coasting Arc #8 (Orbit 2949)
---------------------------------------
Vector Time (GMT): 2007/033/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3031281
59 A = 6712150
88 meter
Y = -3746299
40 meter E =
0024659
Z = -4679588
95 I = 51
93496
XDOT = 3427
494082 Wp = 134
01079
YDOT = 6284
725228 meter/sec RA = 79
47390 deg
ZDOT = -2837
003377 TA = 108
22163
MA = 107
95307
Ha = 191
510 n
mi
Hp = 172
433
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9945149
57 X = 3095679
77
Y = -12291008
53 feet Y = -3712041
67 meter
Z = -15352982
11 Z = -4664707
22
XDOT = 11245
059324 XDOT = 3370
743831
YDOT = 20619
177257 feet/sec YDOT = 6322
736182 meter/sec
ZDOT = -9307
753862 ZDOT = -2820
490778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15799733
82 X = 4815758
87
Y = 1428849
56 feet Y = 435513
35 meter
Z = -15297573
36 Z = -4662700
36
XDOT = -10654
862338 XDOT = -3247
602041
YDOT = 19752
636171 feet/sec YDOT = 6020
603505 meter/sec
ZDOT = -9244
965324 ZDOT = -2817
865431
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 07033
49996001
00020000 00000-0 20000-3 0 9077
2 25544 51
6337 80
0300 0022070 160
5697 199
6314 15
77708106 29504
Satellite: ISS
Catalog Number: 25544
Epoch time: 07033
49996001 = yrday
fracday
Element set: 907
Inclination: 51
6337 deg
RA of node: 80
0300 deg
Eccentricity:
0022070
Arg of perigee: 160
5697 deg
Mean anomaly: 199
6314 deg
Mean motion: 15
77708106 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2950
Checksum: 283
Coasting Arc #9 (Orbit 2965)
---------------------------------------
Vector Time (GMT): 2007/034/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2736333
70 A = 6720749
99 meter
Y = -5975363
73 meter E =
0033495
Z = 1299755
59 I = 51
95815
XDOT = 3923
533361 Wp = 147
25626
YDOT = -3088
255828 meter/sec RA = 74
29736 deg
ZDOT = -5895
393698 TA = 18
48246
MA = 18
36107
Ha = 191
211 n
mi
Hp = 172
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8977472
76 X = -2675626
73
Y = -19604211
72 feet Y = -6005623
53 meter
Z = 4264290
00 Z = 1286610
29
XDOT = 12872
484781 XDOT = 3986
412888
YDOT = -10132
072927 feet/sec YDOT = -3044
029026 meter/sec
ZDOT = -19341
842842 ZDOT = -5876
181118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10884634
69 X = 3317636
65
Y = -18624438
71 feet Y = -5676728
92 meter
Z = 4214180
10 Z = 1284482
10
XDOT = 14389
319743 XDOT = 4385
864658
YDOT = 4017
579821 feet/sec YDOT = 1224
558330 meter/sec
ZDOT = -19270
088911 ZDOT = -5873
523100
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 07034
51337723
00020000 00000-0 20000-3 0 9082
2 25544 51
6339 74
7958 0021887 164
0664 196
1194 15
77776354 29668
Satellite: ISS
Catalog Number: 25544
Epoch time: 07034
51337723 = yrday
fracday
Element set: 908
Inclination: 51
6339 deg
RA of node: 74
7958 deg
Eccentricity:
0021887
Arg of perigee: 164
0664 deg
Mean anomaly: 196
1194 deg
Mean motion: 15
77776354 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2966
Checksum: 332
Coasting Arc #10 (Orbit 2981)
---------------------------------------
Vector Time (GMT): 2007/035/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3831118
48 A = 6709277
74 meter
Y = 1560646
74 meter E =
0022662
Z = 5276329
75 I = 51
91002
XDOT = -2797
053178 Wp = 161
70421
YDOT = -7187
688650 meter/sec RA = 69
16702 deg
ZDOT = 73
894023 TA = 287
47457
MA = 287
72215
Ha = 191
130 n
mi
Hp = 172
757
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12569286
34 X = -3873915
81
Y = 5120232
09 feet Y = 1517565
77 meter
Z = 17310793
14 Z = 5257614
77
XDOT = -9176
683654 XDOT = -2716
830493
YDOT = -23581
655677 feet/sec YDOT = -7218
518311 meter/sec
ZDOT = 242
434459 ZDOT = 60
501234
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11589344
07 X = -3532432
07
Y = -7232712
85 feet Y = -2204530
88 meter
Z = 17240715
29 Z = 5254970
02
XDOT = 13148
179483 XDOT = 4007
565106
YDOT = -20445
881541 feet/sec YDOT = -6231
904694 meter/sec
ZDOT = 191
241068 ZDOT = 58
290277
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 07035
52677437
00020000 00000-0 20000-3 0 9094
2 25544 51
6331 69
5618 0021902 167
8184 192
3515 15
77802840 29824
Satellite: ISS
Catalog Number: 25544
Epoch time: 07035
52677437 = yrday
fracday
Element set: 909
Inclination: 51
6331 deg
RA of node: 69
5618 deg
Eccentricity:
0021902
Arg of perigee: 167
8184 deg
Mean anomaly: 192
3515 deg
Mean motion: 15
77802840 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2982
Checksum: 310
Coasting Arc #11 (Orbit 2997)
---------------------------------------
Vector Time (GMT): 2007/036/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2020894
10 A = 6720749
24 meter
Y = 6302899
41 meter E =
0020781
Z = 1204161
96 I = 51
93739
XDOT = -4922
619419 Wp = 132
60420
YDOT = 437
002293 meter/sec RA = 64
03259 deg
ZDOT = 5896
191246 TA = 240
53595
MA = 240
74344
Ha = 190
867 n
mi
Hp = 173
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6630230
00 X = 1944414
54
Y = 20678803
83 feet Y = 6325070
57 meter
Z = 3950662
59 Z = 1213793
34
XDOT = -16150
326178 XDOT = -4955
782079
YDOT = 1433
734556 feet/sec YDOT = 381
769494 meter/sec
ZDOT = 19344
459468 ZDOT = 5872
197220
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12535913
41 X = -3820946
41
Y = 17723723
41 feet Y = 5402190
90 meter
Z = 3987620
35 Z = 1215426
68
XDOT = -9637
888213 XDOT = -2937
628327
YDOT = -11205
775693 feet/sec YDOT = -3415
520431 meter/sec
ZDOT = 19254
417658 ZDOT = 5868
746502
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 07036
54015266
00020000 00000-0 20000-3 0 9105
2 25544 51
6332 64
3267 0021708 171
2471 188
9077 15
77796980 29988
Satellite: ISS
Catalog Number: 25544
Epoch time: 07036
54015266 = yrday
fracday
Element set: 910
Inclination: 51
6332 deg
RA of node: 64
3267 deg
Eccentricity:
0021708
Arg of perigee: 171
2471 deg
Mean anomaly: 188
9077 deg
Mean motion: 15
77796980 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2998
Checksum: 315
Coasting Arc #12 (Orbit 3012)
---------------------------------------
Vector Time (GMT): 2007/037/11:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 479216
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4758921
80 A = 6711813
45 meter
Y = 757856
92 meter E =
0028033
Z = -4693579
64 I = 51
89487
XDOT = 1658
026645 Wp = 154
06598
YDOT = 6971
200806 meter/sec RA = 58
85329 deg
ZDOT = 2788
296468 TA = 143
47174
MA = 143
28021
Ha = 190
668 n
mi
Hp = 173
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15613260
51 X = 4772893
72
Y = 2486407
23 feet Y = 811151
86 meter
Z = -15398883
32 Z = -4670427
37
XDOT = 5439
719963 XDOT = 1566
405706
YDOT = 22871
393722 feet/sec YDOT = 6989
229565 meter/sec
ZDOT = 9147
954292 ZDOT = 2796
128302
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7703676
26 X = 2348080
52
Y = 13902598
98 feet Y = 4237512
17 meter
Z = -15311853
11 Z = -4667052
83
XDOT = -13693
920312 XDOT = -4173
906911
YDOT = 17763
615048 feet/sec YDOT = 5414
349867 meter/sec
ZDOT = 9178
236227 ZDOT = 2797
526402
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 07037
49017330
00020000 00000-0 20000-3 0 9115
2 25544 51
6344 59
4187 0021704 175
1696 184
9683 15
77836686 30131
Satellite: ISS
Catalog Number: 25544
Epoch time: 07037
49017330 = yrday
fracday
Element set: 911
Inclination: 51
6344 deg
RA of node: 59
4187 deg
Eccentricity:
0021704
Arg of perigee: 175
1696 deg
Mean anomaly: 184
9683 deg
Mean motion: 15
77836686 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3013
Checksum: 308
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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