Date:
June 19th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 4305 56 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 1094)
---------------------------------------
Vector Time (GMT): 2007/169/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -942416
42 A = 6720067
40 meter
Y = 6642320
93 meter E =
0017046
Z = 63633
85 I = 51
97287
XDOT = -4696
620728 Wp = 18
25513
YDOT = -728
570552 meter/sec RA = 97
65025 deg
ZDOT = 6076
104426 TA = 342
43477
MA = 342
49364
Ha = 184
463 n
mi
Hp = 177
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3091917
38 X = -1016930
90
Y = 21792391
49 feet Y = 6631365
65 meter
Z = 208772
48 Z = 58875
97
XDOT = -15408
860657 XDOT = -4717
640932
YDOT = -2390
323332 feet/sec YDOT = -781
209532 meter/sec
ZDOT = 19934
725807 ZDOT = 6053
237317
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4843168
19 X = -1476197
66
Y = 21471350
68 feet Y = 6544467
69 meter
Z = 191539
90 Z = 58381
36
XDOT = -13710
632438 XDOT = -4179
000767
YDOT = -3283
013668 feet/sec YDOT = -1000
662566 meter/sec
ZDOT = 19848
206171 ZDOT = 6049
733241
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
31320898
00020000 00000-0 20000-3 0 9006
2 25544 51
6347 98
0925 0008343 334
8738 25
2020 15
78270042 10957
Satellite: ISS
Catalog Number: 25544
Epoch time: 07169
31320898 = yrday
fracday
Element set: 900
Inclination: 51
6347 deg
RA of node: 98
0925 deg
Eccentricity:
0008343
Arg of perigee: 334
8738 deg
Mean anomaly: 25
2020 deg
Mean motion: 15
78270042 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1095
Checksum: 285
Coasting Arc #2 (Orbit 1109)
---------------------------------------
Vector Time (GMT): 2007/170/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 480788
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3889191
90 A = 6708913
42 meter
Y = 2048430
32 meter E =
0011194
Z = -5075720
33 I = 51
93758
XDOT = -1650
976860 Wp = 64
60576
YDOT = 7327
951064 meter/sec RA = 92
48959 deg
ZDOT = 1699
920405 TA = 221
63216
MA = 221
71743
Ha = 184
655 n
mi
Hp = 177
727
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12759815
96 X = 3890653
62
Y = 6720571
91 feet Y = 2091930
50 meter
Z = -16652625
75 Z = -5056822
96
XDOT = -5416
590749 XDOT = -1741
054178
YDOT = 24041
834201 feet/sec YDOT = 7308
984973 meter/sec
ZDOT = 5577
166683 ZDOT = 1691
682534
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12399207
57 X = 3779278
47
Y = 7524655
78 feet Y = 2293515
08 meter
Z = -16580957
19 Z = -5053875
75
XDOT = -6417
410041 XDOT = -1956
026581
YDOT = 22742
392365 feet/sec YDOT = 6931
881193 meter/sec
ZDOT = 5546
855279 ZDOT = 1690
681489
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
26297360
00020000 00000-0 20000-3 0 9010
2 25544 51
6345 93
1835 0008413 338
0322 22
0482 15
78263552 11107
Satellite: ISS
Catalog Number: 25544
Epoch time: 07170
26297360 = yrday
fracday
Element set: 901
Inclination: 51
6345 deg
RA of node: 93
1835 deg
Eccentricity:
0008413
Arg of perigee: 338
0322 deg
Mean anomaly: 22
0482 deg
Mean motion: 15
78263552 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1110
Checksum: 259
Coasting Arc #3 (Orbit 1125)
---------------------------------------
Vector Time (GMT): 2007/171/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 514726
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1932207
60 A = 6716570
06 meter
Y = -5792898
18 meter E =
0005851
Z = -2805655
54 I = 51
96242
XDOT = 4204
786341 Wp = 14
98499
YDOT = 3894
176640 meter/sec RA = 87
38007 deg
ZDOT = -5141
465149 TA = 197
02530
MA = 197
04494
Ha = 184
673 n
mi
Hp = 177
440
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6339263
77 X = 2010470
24
Y = -19005571
46 feet Y = -5770853
14 meter
Z = -9204906
62 Z = -2796079
75
XDOT = 13795
230779 XDOT = 4185
904611
YDOT = 12776
170079 feet/sec YDOT = 3941
092128 meter/sec
ZDOT = -16868
323980 ZDOT = -5121
083790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7266388
10 X = 2214795
09
Y = -18688251
18 feet Y = -5696178
96 meter
Z = -9169361
44 Z = -2794821
37
XDOT = 11918
307423 XDOT = 3632
700102
YDOT = 12877
594769 feet/sec YDOT = 3925
090885 meter/sec
ZDOT = -16790
833218 ZDOT = -5117
845965
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
27604048
00020000 00000-0 20000-3 0 9028
2 25544 51
6332 87
9464 0008374 342
1996 17
8875 15
78295412 11266
Satellite: ISS
Catalog Number: 25544
Epoch time: 07171
27604048 = yrday
fracday
Element set: 902
Inclination: 51
6332 deg
RA of node: 87
9464 deg
Eccentricity:
0008374
Arg of perigee: 342
1996 deg
Mean anomaly: 17
8875 deg
Mean motion: 15
78295412 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1126
Checksum: 306
Coasting Arc #4 (Orbit 1141)
---------------------------------------
Vector Time (GMT): 2007/172/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 514726
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3426076
55 A = 6714382
76 meter
Y = -4558108
33 meter E =
0013460
Z = 3544966
57 I = 51
95241
XDOT = 2782
815766 Wp = 48
66916
YDOT = -5604
015025 meter/sec RA = 82
18395 deg
ZDOT = -4496
499928 TA = 89
22925
MA = 89
07502
Ha = 184
785 n
mi
Hp = 177
126
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11240408
62 X = -3392073
15
Y = -14954423
64 feet Y = -4596231
00 meter
Z = 11630467
74 Z = 3528404
78
XDOT = 9129
972985 XDOT = 2867
116868
YDOT = -18385
876066 feet/sec YDOT = -5572
424050 meter/sec
ZDOT = -14752
296351 ZDOT = -4482
777115
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10863044
08 X = -3311055
83
Y = -15278751
40 feet Y = -4656963
43 meter
Z = 11567341
14 Z = 3525725
58
XDOT = 8632
077156 XDOT = 2631
057117
YDOT = -17316
344791 feet/sec YDOT = -5278
021892 meter/sec
ZDOT = -14701
048812 ZDOT = -4480
879678
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
28909125
00020000 00000-0 20000-3 0 9035
2 25544 51
6327 82
7093 0008569 345
8486 14
2438 15
78356383 11420
Satellite: ISS
Catalog Number: 25544
Epoch time: 07172
28909125 = yrday
fracday
Element set: 903
Inclination: 51
6327 deg
RA of node: 82
7093 deg
Eccentricity:
0008569
Arg of perigee: 345
8486 deg
Mean anomaly: 14
2438 deg
Mean motion: 15
78356383 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1142
Checksum: 307
Coasting Arc #5 (Orbit 1157)
---------------------------------------
Vector Time (GMT): 2007/173/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 514726
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2945884
90 A = 6710098
91 meter
Y = 3729372
31 meter E =
0006991
Z = 4730613
49 I = 51
93212
XDOT = -3603
016723 Wp = 46
89595
YDOT = -6263
462075 meter/sec RA = 77
08311 deg
ZDOT = 2696
293836 TA = 16
75233
MA = 16
72925
Ha = 185
001 n
mi
Hp = 176
901
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9664976
71 X = -3010348
72
Y = 12235473
45 feet Y = 3696068
71 meter
Z = 15520385
46 Z = 4716146
34
XDOT = -11820
921008 XDOT = -3545
808044
YDOT = -20549
416258 feet/sec YDOT = -6303
433515 meter/sec
ZDOT = 8846
108386 ZDOT = 2678
928585
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9898420
02 X = -3017038
42
Y = 12117000
32 feet Y = 3693261
70 meter
Z = 15466109
22 Z = 4714070
09
XDOT = -10738
119766 XDOT = -3272
978905
YDOT = -19969
212970 feet/sec YDOT = -6086
616113 meter/sec
ZDOT = 8779
754476 ZDOT = 2676
069164
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
30212891
00020000 00000-0 20000-3 0 9047
2 25544 51
6321 77
4723 0008574 349
4442 10
6542 15
78347565 11588
Satellite: ISS
Catalog Number: 25544
Epoch time: 07173
30212891 = yrday
fracday
Element set: 904
Inclination: 51
6321 deg
RA of node: 77
4723 deg
Eccentricity:
0008574
Arg of perigee: 349
4442 deg
Mean anomaly: 10
6542 deg
Mean motion: 15
78347565 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1158
Checksum: 287
Coasting Arc #6 (Orbit 1172)
---------------------------------------
Vector Time (GMT): 2007/174/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 514726
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2769245
04 A = 6719276
48 meter
Y = 6033687
46 meter E =
0017058
Z = -969153
34 I = 51
95596
XDOT = -4005
092160 Wp = 17
93474
YDOT = 2790
564997 meter/sec RA = 71
90608 deg
ZDOT = 5972
615637 TA = 331
49613
MA = 331
58931
Ha = 184
951 n
mi
Hp = 176
606
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9085449
61 X = 2706277
62
Y = 19795562
54 feet Y = 6064302
78 meter
Z = -3179636
96 Z = -955852
49
XDOT = -13140
066142 XDOT = -4065
012884
YDOT = 9155
396973 feet/sec YDOT = 2745
441972 meter/sec
ZDOT = 19595
195660 ZDOT = 5953
013723
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9204920
11 X = 2805659
65
Y = 19748432
66 feet Y = 6019322
27 meter
Z = -3128679
48 Z = -953621
51
XDOT = -11762
101538 XDOT = -3585
088549
YDOT = 8552
203671 feet/sec YDOT = 2606
711679 meter/sec
ZDOT = 19521
397941 ZDOT = 5950
122092
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
25183723
00020000 00000-0 20000-3 0 9054
2 25544 51
6323 72
5634 0008432 353
7690 6
3369 15
78403956 11736
Satellite: ISS
Catalog Number: 25544
Epoch time: 07174
25183723 = yrday
fracday
Element set: 905
Inclination: 51
6323 deg
RA of node: 72
5634 deg
Eccentricity:
0008432
Arg of perigee: 353
7690 deg
Mean anomaly: 6
3369 deg
Mean motion: 15
78403956 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1173
Checksum: 292
Coasting Arc #7 (Orbit 1188)
---------------------------------------
Vector Time (GMT): 2007/175/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 514726
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4041517
20 A = 6707770
74 meter
Y = -1043472
25 meter E =
0016181
Z = -5262478
86 I = 51
90654
XDOT = 2606
605879 Wp = 62
47428
YDOT = 7220
335310 meter/sec RA = 66
76132 deg
ZDOT = 578
815056 TA = 212
95744
MA = 213
05842
Ha = 185
149 n
mi
Hp = 176
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13259570
87 X = 4078449
34
Y = -3423465
38 feet Y = -998070
47 meter
Z = -17265350
59 Z = -5242755
54
XDOT = 8551
856557 XDOT = 2522
861514
YDOT = 23688
764142 feet/sec YDOT = 7249
015518 meter/sec
ZDOT = 1898
999528 ZDOT = 591
275627
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13276123
30 X = 4046562
38
Y = -3721057
71 feet Y = -1134178
39 meter
Z = -17190897
17 Z = -5239785
46
XDOT = 8797
065052 XDOT = 2681
345428
YDOT = 22523
835647 feet/sec YDOT = 6865
265105 meter/sec
ZDOT = 1946
904583 ZDOT = 593
416517
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
26484562
00020000 00000-0 20000-3 0 9062
2 25544 51
6322 67
3257 0008638 356
8074 3
3035 15
78376820 11899
Satellite: ISS
Catalog Number: 25544
Epoch time: 07175
26484562 = yrday
fracday
Element set: 906
Inclination: 51
6322 deg
RA of node: 67
3257 deg
Eccentricity:
0008638
Arg of perigee: 356
8074 deg
Mean anomaly: 3
3035 deg
Mean motion: 15
78376820 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1189
Checksum: 303
Coasting Arc #8 (Orbit 1204)
---------------------------------------
Vector Time (GMT): 2007/176/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 514726
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1620580
64 A = 6717923
32 meter
Y = -6223286
22 meter E =
0005623
Z = -1954163
63 I = 51
92926
XDOT = 5232
551823 Wp = 51
95558
YDOT = 403
942126 meter/sec RA = 61
63445 deg
ZDOT = -5633
254050 TA = 149
71808
MA = 149
68558
Ha = 185
191 n
mi
Hp = 176
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5316865
61 X = -1541377
47
Y = -20417605
70 feet Y = -6240965
30 meter
Z = -6411298
00 Z = -1961845
08
XDOT = 17167
164774 XDOT = 5255
011470
YDOT = 1325
269441 feet/sec YDOT = 462
581947 meter/sec
ZDOT = -18481
804626 ZDOT = -5607
779543
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6084164
48 X = -1854453
33
Y = -20192787
47 feet Y = -6154761
62 meter
Z = -6441017
08 Z = -1963222
01
XDOT = 15836
735926 XDOT = 4827
037110
YDOT = 1085
023496 feet/sec YDOT = 330
715162 meter/sec
ZDOT = -18385
446544 ZDOT = -5603
884107
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
27783901
00020000 00000-0 20000-3 0 9074
2 25544 51
6326 62
0883 0008771
6714 359
4462 15
78426056 12058
Satellite: ISS
Catalog Number: 25544
Epoch time: 07176
27783901 = yrday
fracday
Element set: 907
Inclination: 51
6326 deg
RA of node: 62
0883 deg
Eccentricity:
0008771
Arg of perigee:
6714 deg
Mean anomaly: 359
4462 deg
Mean motion: 15
78426056 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1205
Checksum: 294
Coasting Arc #9 (Orbit 1220)
---------------------------------------
Vector Time (GMT): 2007/177/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 514726
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5003041
72 A = 6712070
57 meter
Y = -1634244
76 meter E =
0015582
Z = 4164113
94 I = 51
89453
XDOT = -930
848174 Wp = 42
30182
YDOT = -6684
138035 meter/sec RA = 56
44110 deg
ZDOT = -3722
336433 TA = 85
65087
MA = 85
47284
Ha = 185
311 n
mi
Hp = 176
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16414178
88 X = -5004624
16
Y = -5361695
39 feet Y = -1690201
18 meter
Z = 13661791
15 Z = 4139804
86
XDOT = -3053
963827 XDOT = -837
953429
YDOT = -21929
586728 feet/sec YDOT = -6694
027226 meter/sec
ZDOT = -12212
389872 ZDOT = -3726
634093
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16767971
09 X = -5110877
59
Y = -4417673
47 feet Y = -1346506
87 meter
Z = 13569704
84 Z = 4136046
04
XDOT = -4546
880409 XDOT = -1385
889149
YDOT = -20502
138905 feet/sec YDOT = -6249
051938 meter/sec
ZDOT = -12229
356748 ZDOT = -3727
507937
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
29081759
00020000 00000-0 20000-3 0 9080
2 25544 51
6325 56
8514 0008819 3
3562 356
7661 15
78449422 12214
Satellite: ISS
Catalog Number: 25544
Epoch time: 07177
29081759 = yrday
fracday
Element set: 908
Inclination: 51
6325 deg
RA of node: 56
8514 deg
Eccentricity:
0008819
Arg of perigee: 3
3562 deg
Mean anomaly: 356
7661 deg
Mean motion: 15
78449422 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1221
Checksum: 306
Coasting Arc #10 (Orbit 1236)
---------------------------------------
Vector Time (GMT): 2007/178/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 514726
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -158009
30 A = 6711414
78 meter
Y = 5165780
71 meter E =
0011752
Z = 4269410
04 I = 51
87675
XDOT = -6085
435656 Wp = 61
26964
YDOT = -3131
750451 meter/sec RA = 51
33989 deg
ZDOT = 3562
261738 TA = 352
78528
MA = 352
80218
Ha = 185
261 n
mi
Hp = 175
809
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -518403
20 X = -236502
20
Y = 16948099
43 feet Y = 5163574
02 meter
Z = 14007250
78 Z = 4268452
80
XDOT = -19965
340079 XDOT = -6067
268594
YDOT = -10274
771820 feet/sec YDOT = -3199
700346 meter/sec
ZDOT = 11687
210426 ZDOT = 3532
742023
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 657154
98 X = 200300
84
Y = 16945825
60 feet Y = 5165087
64 meter
Z = 14004179
12 Z = 4268473
80
XDOT = -19499
185481 XDOT = -5943
351735
YDOT = -8814
567254 feet/sec YDOT = -2686
680099 meter/sec
ZDOT = 11575
261496 ZDOT = 3528
139704
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 07178
30378081
00020000 00000-0 20000-3 0 9091
2 25544 51
6333 51
6149 0008701 6
5357 353
5920 15
78500651 12379
Satellite: ISS
Catalog Number: 25544
Epoch time: 07178
30378081 = yrday
fracday
Element set: 909
Inclination: 51
6333 deg
RA of node: 51
6149 deg
Eccentricity:
0008701
Arg of perigee: 6
5357 deg
Mean anomaly: 353
5920 deg
Mean motion: 15
78500651 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1237
Checksum: 282
Coasting Arc #11 (Orbit 1251)
---------------------------------------
Vector Time (GMT): 2007/179/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 514726
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5384937
57 A = 6718112
88 meter
Y = 3584304
23 meter E =
0015969
Z = -1783899
17 I = 51
87971
XDOT = -1432
134930 Wp = 22
96415
YDOT = 4978
975575 meter/sec RA = 46
14550 deg
ZDOT = 5712
316516 TA = 317
28559
MA = 317
40961
Ha = 185
493 n
mi
Hp = 175
609
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17667118
00 X = 5353123
01
Y = 11759528
30 feet Y = 3644344
12 meter
Z = -5852687
55 Z = -1757815
56
XDOT = -4698
605412 XDOT = -1515
453593
YDOT = 16335
221703 feet/sec YDOT = 4962
493538 meter/sec
ZDOT = 18741
195918 ZDOT = 5705
157886
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18696628
97 X = 5698732
51
Y = 10099442
05 feet Y = 3078309
94 meter
Z = -5753681
54 Z = -1753722
13
XDOT = -2559
954337 XDOT = -780
274082
YDOT = 15341
240398 feet/sec YDOT = 4676
010073 meter/sec
ZDOT = 18714
648952 ZDOT = 5704
225001
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 07179
25342297
00020000 00000-0 20000-3 0 9108
2 25544 51
6331 46
7049 0008872 10
8829 349
2526 15
78478566 12522
Satellite: ISS
Catalog Number: 25544
Epoch time: 07179
25342297 = yrday
fracday
Element set: 910
Inclination: 51
6331 deg
RA of node: 46
7049 deg
Eccentricity:
0008872
Arg of perigee: 10
8829 deg
Mean anomaly: 349
2526 deg
Mean motion: 15
78478566 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1252
Checksum: 312
Coasting Arc #12 (Orbit 1267)
---------------------------------------
Vector Time (GMT): 2007/180/06:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 514726
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2429955
28 A = 6707345
87 meter
Y = -3381524
03 meter E =
0019495
Z = -5273288
97 I = 51
82331
XDOT = 5973
978061 Wp = 61
27300
YDOT = 4838
744008 meter/sec RA = 41
00981 deg
ZDOT = -341
808199 TA = 205
43983
MA = 205
53592
Ha = 185
489 n
mi
Hp = 175
499
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7972294
21 X = 2493204
01
Y = -11094238
94 feet Y = -3353996
06 meter
Z = -17300816
84 Z = -5261331
41
XDOT = 19599
665553 XDOT = 5921
086956
YDOT = 15875
144382 feet/sec YDOT = 4905
252731 meter/sec
ZDOT = -1121
417977 ZDOT = -312
914024
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6821834
57 X = 2079295
18
Y = -11901791
09 feet Y = -3627665
92 meter
Z = -17255950
22 Z = -5259613
63
XDOT = 20339
657577 XDOT = 6199
527630
YDOT = 13164
208201 feet/sec YDOT = 4012
450660 meter/sec
ZDOT = -1011
649813 ZDOT = -308
350863
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 07180
26635917
00020000 00000-0 20000-3 0 9116
2 25544 51
6338 41
4673 0008895 13
8608 346
2800 15
78499056 12683
Satellite: ISS
Catalog Number: 25544
Epoch time: 07180
26635917 = yrday
fracday
Element set: 911
Inclination: 51
6338 deg
RA of node: 41
4673 deg
Eccentricity:
0008895
Arg of perigee: 13
8608 deg
Mean anomaly: 346
2800 deg
Mean motion: 15
78499056 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1268
Checksum: 311
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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