Date:
June 18th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 4843 76 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 82 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 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 1049)
---------------------------------------
Vector Time (GMT): 2007/166/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -164236
05 A = 6717063
66 meter
Y = 6126480
10 meter E =
0009367
Z = -2735337
22 I = 51
93750
XDOT = -5265
393281 Wp = 354
52954
YDOT = 2174
846511 meter/sec RA = 111
99148 deg
ZDOT = 5194
944536 TA = 334
29568
MA = 334
34220
Ha = 184
206 n
mi
Hp = 178
563
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -538832
19 X = -219443
26
Y = 20100000
33 feet Y = 6124335
50 meter
Z = -8974203
49 Z = -2736267
70
XDOT = -17274
912340 XDOT = -5314
557505
YDOT = 7135
323199 feet/sec YDOT = 2115
689784 meter/sec
ZDOT = 17043
781286 ZDOT = 5169
246343
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18399388
04 X = 5608133
47
Y = 8106312
47 feet Y = 2470804
04 meter
Z = -8977020
63 Z = -2736195
89
XDOT = 573
913854 XDOT = 174
928943
YDOT = 17436
672890 feet/sec YDOT = 5314
697897 meter/sec
ZDOT = 16946
921791 ZDOT = 5165
421762
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 07166
46384241
00020000 00000-0 20000-3 0 9001
2 25544 51
6309 112
8167 0008419 323
7097 36
3497 15
78167698 10501
Satellite: ISS
Catalog Number: 25544
Epoch time: 07166
46384241 = yrday
fracday
Element set: 900
Inclination: 51
6309 deg
RA of node: 112
8167 deg
Eccentricity:
0008419
Arg of perigee: 323
7097 deg
Mean anomaly: 36
3497 deg
Mean motion: 15
78167698 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1050
Checksum: 304
Coasting Arc #2 (Orbit 1065)
---------------------------------------
Vector Time (GMT): 2007/167/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4345835
88 A = 6709052
53 meter
Y = -598073
88 meter E =
0013304
Z = -5086029
31 I = 51
92138
XDOT = -913
505536 Wp = 41
00650
YDOT = 7464
593097 meter/sec RA = 106
88127 deg
ZDOT = -1650
927224 TA = 213
14464
MA = 213
22807
Ha = 184
303 n
mi
Hp = 178
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14257991
73 X = 4376907
50
Y = -1962184
63 feet Y = -549301
38 meter
Z = -16686447
86 Z = -5064842
02
XDOT = -2997
065407 XDOT = -988
887957
YDOT = 24490
134832 feet/sec YDOT = 7453
956669 meter/sec
ZDOT = -5416
427901 ZDOT = -1655
546360
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3409250
86 X = 1039139
66
Y = -14077680
41 feet Y = -4290876
99 meter
Z = -16606443
38 Z = -5061643
94
XDOT = 20692
874280 XDOT = 6307
188081
YDOT = 11449
044660 feet/sec YDOT = 3489
668812 meter/sec
ZDOT = -5433
037768 ZDOT = -1655
989912
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 07167
47697052
00020000 00000-0 20000-3 0 9011
2 25544 51
6320 107
5805 0008457 327
0826 32
9812 15
78206983 10664
Satellite: ISS
Catalog Number: 25544
Epoch time: 07167
47697052 = yrday
fracday
Element set: 901
Inclination: 51
6320 deg
RA of node: 107
5805 deg
Eccentricity:
0008457
Arg of perigee: 327
0826 deg
Mean anomaly: 32
9812 deg
Mean motion: 15
78206983 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1066
Checksum: 297
Coasting Arc #3 (Orbit 1081)
---------------------------------------
Vector Time (GMT): 2007/168/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1344146
07 A = 6720139
01 meter
Y = -6583421
65 meter E =
0004829
Z = 27224
42 I = 51
96700
XDOT = 4655
406623 Wp = 104
77451
YDOT = 921
747207 meter/sec RA = 101
72114 deg
ZDOT = -6066
863781 TA = 74
93076
MA = 74
87734
Ha = 184
379 n
mi
Hp = 178
092
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4409928
04 X = 1417530
70
Y = -21599152
40 feet Y = -6567980
35 meter
Z = 89318
96 Z = 33931
04
XDOT = 15273
643776 XDOT = 4674
224927
YDOT = 3024
105010 feet/sec YDOT = 973
913108 meter/sec
ZDOT = -19904
408730 ZDOT = -6044
202136
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18704814
39 X = -5701227
43
Y = -11666009
09 feet Y = -3555799
57 meter
Z = 113922
36 Z = 34723
54
XDOT = 7349
584930 XDOT = 2240
153487
YDOT = -11999
830639 feet/sec YDOT = -3657
548379 meter/sec
ZDOT = -19818
650173 ZDOT = -6040
724573
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 07168
49008068
00020000 00000-0 20000-3 0 9028
2 25544 51
6327 102
3446 0008511 330
8958 29
1732 15
78238597 10827
Satellite: ISS
Catalog Number: 25544
Epoch time: 07168
49008068 = yrday
fracday
Element set: 902
Inclination: 51
6327 deg
RA of node: 102
3446 deg
Eccentricity:
0008511
Arg of perigee: 330
8958 deg
Mean anomaly: 29
1732 deg
Mean motion: 15
78238597 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1082
Checksum: 297
Coasting Arc #4 (Orbit 1097)
---------------------------------------
Vector Time (GMT): 2007/169/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3762694
08 A = 6708804
96 meter
Y = -2213854
53 meter E =
0010571
Z = 5096192
99 I = 51
93389
XDOT = 2089
699347 Wp = 1
77764
YDOT = -7244
221843 meter/sec RA = 96
56266 deg
ZDOT = -1593
657924 TA = 103
50999
MA = 103
39218
Ha = 184
551 n
mi
Hp = 177
846
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12344796
84 X = -3762414
85
Y = -7263302
25 feet Y = -2255930
50 meter
Z = 16719793
28 Z = 5077914
30
XDOT = 6855
968986 XDOT = 2178
291588
YDOT = -23767
132031 feet/sec YDOT = -7220
358001 meter/sec
ZDOT = -5228
536497 ZDOT = -1583
292499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10986925
53 X = -3348814
90
Y = 9314026
46 feet Y = 2838915
27 meter
Z = 16650448
47 Z = 5075056
69
XDOT = -19444
576029 XDOT = -5926
706774
YDOT = -13597
244690 feet/sec YDOT = -4144
440182 meter/sec
ZDOT = -5190
175036 ZDOT = -1581
965351
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 07169
50317290
00020000 00000-0 20000-3 0 9032
2 25544 51
6330 97
1088 0008534 334
6818 25
3928 15
78266097 10984
Satellite: ISS
Catalog Number: 25544
Epoch time: 07169
50317290 = yrday
fracday
Element set: 903
Inclination: 51
6330 deg
RA of node: 97
1088 deg
Eccentricity:
0008534
Arg of perigee: 334
6818 deg
Mean anomaly: 25
3928 deg
Mean motion: 15
78266097 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1098
Checksum: 308
Coasting Arc #5 (Orbit 1113)
---------------------------------------
Vector Time (GMT): 2007/170/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2261063
24 A = 6716818
76 meter
Y = 5706109
69 meter E =
0014755
Z = 2704435
34 I = 51
96322
XDOT = -3981
042446 Wp = 43
89891
YDOT = -4053
835882 meter/sec RA = 91
45214 deg
ZDOT = 5218
448575 TA = 346
89457
MA = 346
93287
Ha = 184
649 n
mi
Hp = 177
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7418186
50 X = -2337839
24
Y = 18720832
31 feet Y = 5680395
48 meter
Z = 8872819
36 Z = 2693265
70
XDOT = -13061
162882 XDOT = -3960
765942
YDOT = -13299
986488 feet/sec YDOT = -4098
241639 meter/sec
ZDOT = 17120
894276 ZDOT = 5199
157477
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15397002
82 X = 4693006
46
Y = 13006439
29 feet Y = 3964362
70 meter
Z = 8831241
00 Z = 2691762
26
XDOT = -15830
638306 XDOT = -4825
178556
YDOT = 7150
892305 feet/sec YDOT = 2179
591975 meter/sec
ZDOT = 17047
509355 ZDOT = 5196
080852
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 07170
51624671
00020000 00000-0 20000-3 0 9040
2 25544 51
6330 91
8721 0008548 338
3300 21
7503 15
78295356 11149
Satellite: ISS
Catalog Number: 25544
Epoch time: 07170
51624671 = yrday
fracday
Element set: 904
Inclination: 51
6330 deg
RA of node: 91
8721 deg
Eccentricity:
0008548
Arg of perigee: 338
3300 deg
Mean anomaly: 21
7503 deg
Mean motion: 15
78295356 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1114
Checksum: 271
Coasting Arc #6 (Orbit 1128)
---------------------------------------
Vector Time (GMT): 2007/171/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3162059
45 A = 6714159
58 meter
Y = 4667220
34 meter E =
0007721
Z = -3642603
54 I = 51
95398
XDOT = -3090
535810 Wp = 21
11595
YDOT = 5521
186679 meter/sec RA = 86
25695 deg
ZDOT = 4401
310576 TA = 295
32234
MA = 295
40230
Ha = 184
758 n
mi
Hp = 177
376
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10374210
78 X = 3127329
82
Y = 15312402
70 feet Y = 4702386
62 meter
Z = -11950799
02 Z = -3627326
08
XDOT = -10139
553184 XDOT = -3173
425379
YDOT = 18114
129524 feet/sec YDOT = 5486
162463 meter/sec
ZDOT = 14439
995327 ZDOT = 4386
096387
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17739305
77 X = 5406940
40
Y = -5366621
65 feet Y = -1635746
28 meter
Z = -11892515
54 Z = -3624838
74
XDOT = 13822
642355 XDOT = 4213
141390
YDOT = 13889
799786 feet/sec YDOT = 4233
610975 meter/sec
ZDOT = 14383
103105 ZDOT = 4383
969826
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 07171
46598707
00020000 00000-0 20000-3 0 9056
2 25544 51
6331 86
9628 0008602 341
5671 18
5181 15
78319444 11296
Satellite: ISS
Catalog Number: 25544
Epoch time: 07171
46598707 = yrday
fracday
Element set: 905
Inclination: 51
6331 deg
RA of node: 86
9628 deg
Eccentricity:
0008602
Arg of perigee: 341
5671 deg
Mean anomaly: 18
5181 deg
Mean motion: 15
78319444 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1129
Checksum: 304
Coasting Arc #7 (Orbit 1144)
---------------------------------------
Vector Time (GMT): 2007/172/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3144390
35 A = 6710282
60 meter
Y = -3648723
44 meter E =
0014561
Z = -4684391
83 I = 51
93880
XDOT = 3224
094907 Wp = 34
49104
YDOT = 6398
778206 meter/sec RA = 81
15720 deg
ZDOT = -2812
396475 TA = 207
82101
MA = 207
89896
Ha = 184
774 n
mi
Hp = 177
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10316241
30 X = 3207712
98
Y = -11970877
44 feet Y = -3613206
42 meter
Z = -15368739
60 Z = -4668963
17
XDOT = 10577
739197 XDOT = 3165
965226
YDOT = 20993
366818 feet/sec YDOT = 6434
507206 meter/sec
ZDOT = -9227
022556 ZDOT = -2796
874263
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8530321
03 X = -2600041
85
Y = -13369265
29 feet Y = -4074952
06 meter
Z = -15310821
89 Z = -4666738
51
XDOT = 22170
683605 XDOT = 6757
624363
YDOT = -3618
782651 feet/sec YDOT = -1103
004952 meter/sec
ZDOT = -9167
618838 ZDOT = -2794
290222
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 07172
47902602
00020000 00000-0 20000-3 0 9062
2 25544 51
6337 81
7258 0008612 345
9486 14
1439 15
78366710 11451
Satellite: ISS
Catalog Number: 25544
Epoch time: 07172
47902602 = yrday
fracday
Element set: 906
Inclination: 51
6337 deg
RA of node: 81
7258 deg
Eccentricity:
0008612
Arg of perigee: 345
9486 deg
Mean anomaly: 14
1439 deg
Mean motion: 15
78366710 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1145
Checksum: 295
Coasting Arc #8 (Orbit 1160)
---------------------------------------
Vector Time (GMT): 2007/173/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2401785
30 A = 6719281
74 meter
Y = -6183697
47 meter E =
0009916
Z = 1063484
21 I = 51
96372
XDOT = 4133
107187 Wp = 85
44662
YDOT = -2635
485711 meter/sec RA = 75
97823 deg
ZDOT = -5942
060965 TA = 82
95934
MA = 82
84658
Ha = 184
863 n
mi
Hp = 176
907
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7879873
03 X = -2337625
98
Y = -20287721
36 feet Y = -6210196
99 meter
Z = 3489121
44 Z = 1051971
41
XDOT = 13560
062949 XDOT = 4191
135758
YDOT = -8646
606665 feet/sec YDOT = -2588
941754 meter/sec
ZDOT = -19494
950671 ZDOT = -5921
841784
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21660301
00 X = -6602059
75
Y = 2195907
10 feet Y = 669312
48 meter
Z = 3444903
19 Z = 1050006
49
XDOT = -4523
069447 XDOT = -1378
631567
YDOT = -13901
781607 feet/sec YDOT = -4237
263034 meter/sec
ZDOT = -19418
804789 ZDOT = -5918
851700
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 07173
49204728
00020000 00000-0 20000-3 0 9070
2 25544 51
6340 76
4887 0008583 349
3640 10
7343 15
78372298 11613
Satellite: ISS
Catalog Number: 25544
Epoch time: 07173
49204728 = yrday
fracday
Element set: 907
Inclination: 51
6340 deg
RA of node: 76
4887 deg
Eccentricity:
0008583
Arg of perigee: 349
3640 deg
Mean anomaly: 10
7343 deg
Mean motion: 15
78372298 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1161
Checksum: 305
Coasting Arc #9 (Orbit 1176)
---------------------------------------
Vector Time (GMT): 2007/174/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4066493
23 A = 6707534
82 meter
Y = 863589
46 meter E =
0009636
Z = 5263458
83 I = 51
91647
XDOT = -2179
916061 Wp = 7
60452
YDOT = -7380
042707 meter/sec RA = 70
83642 deg
ZDOT = -463
866300 TA = 86
83481
MA = 86
72457
Ha = 184
967 n
mi
Hp = 176
619
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13341513
24 X = -4101416
74
Y = 2833298
77 feet Y = 817919
67 meter
Z = 17268565
70 Z = 5243619
07
XDOT = -7151
955582 XDOT = -2094
975946
YDOT = -24212
738539 feet/sec YDOT = -7403
944765 meter/sec
ZDOT = -1521
871062 ZDOT = -474
251027
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -621501
96 X = -189433
80
Y = 13719289
93 feet Y = 4181639
57 meter
Z = 17193654
00 Z = 5240625
74
XDOT = -24229
614490 XDOT = -7385
186496
YDOT = 898
906983 feet/sec YDOT = 273
986848 meter/sec
ZDOT = -1561
951926 ZDOT = -476
082947
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 07174
50504879
00020000 00000-0 20000-3 0 9084
2 25544 51
6340 71
2518 0008666 352
0704 8
0323 15
78445174 11770
Satellite: ISS
Catalog Number: 25544
Epoch time: 07174
50504879 = yrday
fracday
Element set: 908
Inclination: 51
6340 deg
RA of node: 71
2518 deg
Eccentricity:
0008666
Arg of perigee: 352
0704 deg
Mean anomaly: 8
0323 deg
Mean motion: 15
78445174 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1177
Checksum: 286
Coasting Arc #10 (Orbit 1192)
---------------------------------------
Vector Time (GMT): 2007/175/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1272097
06 A = 6718141
67 meter
Y = 6321839
55 meter E =
0019022
Z = 1840821
24 I = 51
94194
XDOT = -5171
358964 Wp = 40
72266
YDOT = -622
599370 meter/sec RA = 65
70840 deg
ZDOT = 5693
285914 TA = 339
68016
MA = 339
75575
Ha = 185
081 n
mi
Hp = 176
391
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4173546
78 X = 1192368
37
Y = 20740943
42 feet Y = 6335618
80 meter
Z = 6039439
78 Z = 1846808
39
XDOT = -16966
400801 XDOT = -5191
669681
YDOT = -2042
648851 feet/sec YDOT = -680
542817 meter/sec
ZDOT = 18678
759560 ZDOT = 5668
113919
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21134039
94 X = 6441655
37
Y = 821726
17 feet Y = 250462
14 meter
Z = 6062770
11 Z = 1847932
33
XDOT = -5915
353268 XDOT = -1802
999676
YDOT = 14579
551928 feet/sec YDOT = 4443
847428 meter/sec
ZDOT = 18583
522487 ZDOT = 5664
257654
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 07175
51803597
00020000 00000-0 20000-3 0 9096
2 25544 51
6346 66
0144 0008723 356
7889 3
3218 15
78422218 11935
Satellite: ISS
Catalog Number: 25544
Epoch time: 07175
51803597 = yrday
fracday
Element set: 909
Inclination: 51
6346 deg
RA of node: 66
0144 deg
Eccentricity:
0008723
Arg of perigee: 356
7889 deg
Mean anomaly: 3
3218 deg
Mean motion: 15
78422218 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1193
Checksum: 303
Coasting Arc #11 (Orbit 1207)
---------------------------------------
Vector Time (GMT): 2007/176/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4864198
05 A = 6711726
86 meter
Y = 1844343
74 meter E =
0009698
Z = -4243783
71 I = 51
90830
XDOT = 575
483729 Wp = 52
86623
YDOT = 6778
219414 meter/sec RA = 60
51682 deg
ZDOT = 3616
770152 TA = 253
69891
MA = 253
80559
Ha = 185
174 n
mi
Hp = 176
253
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15958655
01 X = 4863828
46
Y = 6050996
54 feet Y = 1898736
57 meter
Z = -13923174
91 Z = -4220153
89
XDOT = 1888
069976 XDOT = 482
076196
YDOT = 22238
252669 feet/sec YDOT = 6784
131928 meter/sec
ZDOT = 11866
043806 ZDOT = 3619
340105
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9385606
99 X = 2860733
01
Y = -14341860
57 feet Y = -4371399
10 meter
Z = -13833634
56 Z = -4216491
82
XDOT = 21058
023649 XDOT = 6418
485608
YDOT = 2361
310650 feet/sec YDOT = 719
727486 meter/sec
ZDOT = 11876
495748 ZDOT = 3619
955904
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 07176
46769283
00020000 00000-0 20000-3 0 9106
2 25544 51
6353 61
1048 0008725 359
7171
3988 15
78463540 12082
Satellite: ISS
Catalog Number: 25544
Epoch time: 07176
46769283 = yrday
fracday
Element set: 910
Inclination: 51
6353 deg
RA of node: 61
1048 deg
Eccentricity:
0008725
Arg of perigee: 359
7171 deg
Mean anomaly:
3988 deg
Mean motion: 15
78463540 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1208
Checksum: 300
Coasting Arc #12 (Orbit 1223)
---------------------------------------
Vector Time (GMT): 2007/177/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 430745
87 A = 6711634
46 meter
Y = -5210367
02 meter E =
0014266
Z = -4223136
39 I = 51
89360
XDOT = 5841
759258 Wp = 35
00746
YDOT = 3439
873065 meter/sec RA = 55
41576 deg
ZDOT = -3642
759579 TA = 197
98704
MA = 198
03757
Ha = 185
142 n
mi
Hp = 175
992
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1413208
24 X = 509492
31
Y = -17094380
00 feet Y = -5205109
11 meter
Z = -13855434
34 Z = -4220853
50
XDOT = 19165
876831 XDOT = 5820
555898
YDOT = 11285
672787 feet/sec YDOT = 3505
081018 meter/sec
ZDOT = -11951
310954 ZDOT = -3614
430990
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16450322
55 X = -5014058
31
Y = -4881140
39 feet Y = -1487771
59 meter
Z = -13847360
84 Z = -4220675
58
XDOT = 14549
925982 XDOT = 4434
817439
YDOT = -15385
654843 feet/sec YDOT = -4689
547596 meter/sec
ZDOT = -11843
833362 ZDOT = -3610
000409
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 07177
48064357
00020000 00000-0 20000-3 0 9110
2 25544 51
6358 55
8677 0008763 2
9635 357
1581 15
78500226 12242
Satellite: ISS
Catalog Number: 25544
Epoch time: 07177
48064357 = yrday
fracday
Element set: 911
Inclination: 51
6358 deg
RA of node: 55
8677 deg
Eccentricity:
0008763
Arg of perigee: 2
9635 deg
Mean anomaly: 357
1581 deg
Mean motion: 15
78500226 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1224
Checksum: 304
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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