Date:
July 20th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 7265 64 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
202/01:19:29
720 -1
0 3
4 3
4
N/A 3
2 0
1 186
9
000/00:04:59
440 0
0 0
2 172
6
204/22:26:57
898 0
4 11
8 11
8
N/A -11
8 -0
0 187
3
000/00:21:55
796 -0
3 0
4 180
3
Coasting Arc #1 (Orbit 1572)
---------------------------------------
Vector Time (GMT): 2007/199/12:24:19
861
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4991701
64 A = 6711362
18 meter
Y = -2515588
27 meter E =
0019817
Z = 3697050
19 I = 51
36075
XDOT = 71
651771 Wp = 88
72958
YDOT = 6433
798546 meter/sec RA = 301
33433 deg
ZDOT = 4261
852768 TA = 316
20183
MA = 316
35883
Ha = 185
049 n
mi
Hp = 172
806
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16376973
90 X = 5001501
06
Y = -8253242
35 feet Y = -2459713
84 meter
Z = 12129429
76 Z = 3721322
98
XDOT = 235
077990 XDOT = -21
000165
YDOT = 21108
262946 feet/sec YDOT = 6434
081316 meter/sec
ZDOT = 13982
456589 ZDOT = 4261
976459
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15521626
31 X = -4730991
70
Y = -9652497
28 feet Y = -2942081
17 meter
Z = 12220996
79 Z = 3724959
82
XDOT = 17254
456654 XDOT = 5259
158388
YDOT = -9962
260132 feet/sec YDOT = -3036
496888 meter/sec
ZDOT = 13983
640123 ZDOT = 4262
213510
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 07199
57225510
00020000 00000-0 20000-3 0 9002
2 25544 51
6355 301
6264 0008354 78
3527 281
8576 15
79192875 15738
Satellite: ISS
Catalog Number: 25544
Epoch time: 07199
57225510 = yrday
fracday
Element set: 900
Inclination: 51
6355 deg
RA of node: 301
6264 deg
Eccentricity:
0008354
Arg of perigee: 78
3527 deg
Mean anomaly: 281
8576 deg
Mean motion: 15
79192875 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1573
Checksum: 312
Coasting Arc #2 (Orbit 1587)
---------------------------------------
Vector Time (GMT): 2007/200/12:24:19
861
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 991318
06 A = 6715157
70 meter
Y = -6226451
69 meter E =
0013473
Z = -2311857
61 I = 51
35918
XDOT = 5370
141968 Wp = 65
22410
YDOT = -1140
714887 meter/sec RA = 296
09240 deg
ZDOT = 5405
095984 TA = 268
62376
MA = 268
77811
Ha = 185
152 n
mi
Hp = 172
854
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3252355
84 X = 1072099
91
Y = -20427991
10 feet Y = -6214914
32 meter
Z = -7584834
66 Z = -2306846
21
XDOT = 17618
576012 XDOT = 5356
241891
YDOT = -3742
502911 feet/sec YDOT = -1080
741160 meter/sec
ZDOT = 17733
254542 ZDOT = 5431
149894
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19032277
84 X = -5801038
29
Y = 8119714
15 feet Y = 2474888
87 meter
Z = -7566571
10 Z = -2306290
87
XDOT = -11925
200197 XDOT = -3634
801020
YDOT = -11427
607830 feet/sec YDOT = -3483
134867 meter/sec
ZDOT = 17831
712909 ZDOT = 5435
106095
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 07200
52146865
00020000 00000-0 20000-3 0 9016
2 25544 51
6353 296
7145 0008296 79
9385 280
2716 15
79173738 15884
Satellite: ISS
Catalog Number: 25544
Epoch time: 07200
52146865 = yrday
fracday
Element set: 901
Inclination: 51
6353 deg
RA of node: 296
7145 deg
Eccentricity:
0008296
Arg of perigee: 79
9385 deg
Mean anomaly: 280
2716 deg
Mean motion: 15
79173738 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1588
Checksum: 322
Coasting Arc #3 (Orbit 1603)
---------------------------------------
Vector Time (GMT): 2007/201/12:24:19
861
Vector Time (MET): N/A
Weight (LBS) : 509098
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4182982
13 A = 6705430
40 meter
Y = -737839
36 meter E =
0023094
Z = -5208543
55 I = 51
31450
XDOT = 2189
324823 Wp = 84
16528
YDOT = -7338
966256 meter/sec RA = 290
92207 deg
ZDOT = -719
030468 TA = 178
95951
MA = 178
95469
Ha = 185
076 n
mi
Hp = 172
622
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13723694
66 X = -4149118
71
Y = -2420732
80 feet Y = -784426
00 meter
Z = -17088397
49 Z = -5228782
09
XDOT = 7182
824224 XDOT = 2274
720395
YDOT = -24077
973282 feet/sec YDOT = -7314
006458 meter/sec
ZDOT = -2359
023844 ZDOT = -708
188087
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5448141
76 X = 1660593
61
Y = 12723657
04 feet Y = 3878170
66 meter
Z = -17165062
60 Z = -5231911
08
XDOT = -23153
424579 XDOT = -7057
163812
YDOT = 6787
649247 feet/sec YDOT = 2068
875490 meter/sec
ZDOT = -2318
826887 ZDOT = -706
778435
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 07201
53393802
00020000 00000-0 20000-3 0 9024
2 25544 51
6346 291
4740 0008262 84
0234 276
1873 15
79222670 16049
Satellite: ISS
Catalog Number: 25544
Epoch time: 07201
53393802 = yrday
fracday
Element set: 902
Inclination: 51
6346 deg
RA of node: 291
4740 deg
Eccentricity:
0008262
Arg of perigee: 84
0234 deg
Mean anomaly: 276
1873 deg
Mean motion: 15
79222670 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1604
Checksum: 275
Coasting Arc #4 (Orbit 1612)
---------------------------------------
Vector Time (GMT): 2007/202/01:21:59
440
Vector Time (MET): N/A
Weight (LBS) : 508908
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3759684
86 A = 6706951
46 meter
Y = 1910887
00 meter E =
0013827
Z = 5203533
29 I = 51
30973
XDOT = -2829
703547 Wp = 79
90455
YDOT = 7158
571142 meter/sec RA = 288
10516 deg
ZDOT = -580
599944 TA = 15
64642
MA = 15
60373
Ha = 186
851 n
mi
Hp = 172
616
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12334924
08 X = 3712760
00
Y = 6269314
32 feet Y = 1952667
05 meter
Z = 17071959
63 Z = 5221683
90
XDOT = -9283
804289 XDOT = -2906
721010
YDOT = 23486
125794 feet/sec YDOT = 7126
497234 meter/sec
ZDOT = -1904
855458 ZDOT = -594
532925
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4945162
54 X = 1507285
54
Y = 12831322
03 feet Y = 3910986
95 meter
Z = 17140857
68 Z = 5224533
42
XDOT = -21631
462928 XDOT = -6593
269901
YDOT = 10966
836107 feet/sec YDOT = 3342
691646 meter/sec
ZDOT = -1956
765405 ZDOT = -596
422095
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 07202
10346545
00020000 00000-0 20000-3 0 9031
2 25544 51
6352 288
5276 0011086 83
9932 276
2497 15
78661594 16132
Satellite: ISS
Catalog Number: 25544
Epoch time: 07202
10346545 = yrday
fracday
Element set: 903
Inclination: 51
6352 deg
RA of node: 288
5276 deg
Eccentricity:
0011086
Arg of perigee: 83
9932 deg
Mean anomaly: 276
2497 deg
Mean motion: 15
78661594 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1613
Checksum: 305
Coasting Arc #5 (Orbit 1628)
---------------------------------------
Vector Time (GMT): 2007/203/01:21:59
440
Vector Time (MET): N/A
Weight (LBS) : 508908
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2938263
54 A = 6717229
94 meter
Y = -5692930
28 meter E =
0024971
Z = 1986509
76 I = 51
33642
XDOT = 3684
513509 Wp = 76
48384
YDOT = 3863
303362 meter/sec RA = 282
93449 deg
ZDOT = 5568
967778 TA = 305
80644
MA = 306
03825
Ha = 186
972 n
mi
Hp = 172
580
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9639972
24 X = 2992054
29
Y = -18677592
79 feet Y = -5659772
42 meter
Z = 6517420
47 Z = 2000913
82
XDOT = 12088
298915 XDOT = 3613
986745
YDOT = 12674
879797 feet/sec YDOT = 3904
110740 meter/sec
ZDOT = 18270
891661 ZDOT = 5586
696155
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19476013
93 X = 5936289
05
Y = -7858848
37 feet Y = -2395376
98 meter
Z = 6571277
71 Z = 2002925
45
XDOT = 213
553690 XDOT = 65
091165
YDOT = 16006
453977 feet/sec YDOT = 4878
767172 meter/sec
ZDOT = 18338
416218 ZDOT = 5589
549263
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 07203
11630965
00020000 00000-0 20000-3 0 9046
2 25544 51
6351 283
2893 0011140 87
0703 273
1738 15
78652610 16290
Satellite: ISS
Catalog Number: 25544
Epoch time: 07203
11630965 = yrday
fracday
Element set: 904
Inclination: 51
6351 deg
RA of node: 283
2893 deg
Eccentricity:
0011140
Arg of perigee: 87
0703 deg
Mean anomaly: 273
1738 deg
Mean motion: 15
78652610 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1629
Checksum: 278
Coasting Arc #6 (Orbit 1643)
---------------------------------------
Vector Time (GMT): 2007/204/01:21:59
440
Vector Time (MET): N/A
Weight (LBS) : 508908
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2640436
08 A = 6711635
04 meter
Y = -4671389
90 meter E =
0018235
Z = -4048747
17 I = 51
31268
XDOT = 3829
643153 Wp = 97
99750
YDOT = -5469
036924 meter/sec RA = 277
69542 deg
ZDOT = 3824
747446 TA = 211
50236
MA = 211
61168
Ha = 186
861 n
mi
Hp = 172
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8662848
02 X = -2568335
65
Y = -15326082
35 feet Y = -4700513
12 meter
Z = -13283291
24 Z = -4061399
80
XDOT = 12564
446039 XDOT = 3871
934236
YDOT = -17943
034528 feet/sec YDOT = -5425
975704 meter/sec
ZDOT = 12548
384009 ZDOT = 3843
453852
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3220927
67 X = 981738
75
Y = -17270519
89 feet Y = -5264054
46 meter
Z = -13331703
94 Z = -4063503
36
XDOT = 19827
964933 XDOT = 6043
563712
YDOT = -6012
036694 feet/sec YDOT = -1832
468784 meter/sec
ZDOT = 12618
547630 ZDOT = 3846
133318
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 07204
06582754
00020000 00000-0 20000-3 0 9054
2 25544 51
6349 278
3782 0010989 90
5694 269
6731 15
78698120 16443
Satellite: ISS
Catalog Number: 25544
Epoch time: 07204
06582754 = yrday
fracday
Element set: 905
Inclination: 51
6349 deg
RA of node: 278
3782 deg
Eccentricity:
0010989
Arg of perigee: 90
5694 deg
Mean anomaly: 269
6731 deg
Mean motion: 15
78698120 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1644
Checksum: 329
Coasting Arc #7 (Orbit 1657)
---------------------------------------
Vector Time (GMT): 2007/204/22:37:55
796
Vector Time (MET): N/A
Weight (LBS) : 508072
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3044108
45 A = 6719044
27 meter
Y = -4384588
28 meter E =
0009005
Z = -4090694
22 I = 51
30926
XDOT = 3334
171040 Wp = 116
36325
YDOT = -5824
930690 meter/sec RA = 273
09199 deg
ZDOT = 3764
737842 TA = 192
43814
MA = 192
46039
Ha = 187
327 n
mi
Hp = 180
251
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9987232
46 X = -2974981
31
Y = -14385132
15 feet Y = -4418242
14 meter
Z = -13420912
79 Z = -4105315
15
XDOT = 10938
881364 XDOT = 3380
770114
YDOT = -19110
664993 feet/sec YDOT = -5787
386082 meter/sec
ZDOT = 12351
502106 ZDOT = 3781
047587
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12439170
69 X = 3791459
23
Y = -12265485
37 feet Y = -3738519
94 meter
Z = -13476744
42 Z = -4107711
70
XDOT = 19817
156774 XDOT = 6040
269385
YDOT = 6468
254143 feet/sec YDOT = 1971
523863 meter/sec
ZDOT = 12412
557223 ZDOT = 3783
347442
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 07204
95203512
00020000 00000-0 20000-3 0 9065
2 25544 51
6344 273
7945 0001649 150
2607 209
8651 15
76035637 16587
Satellite: ISS
Catalog Number: 25544
Epoch time: 07204
95203512 = yrday
fracday
Element set: 906
Inclination: 51
6344 deg
RA of node: 273
7945 deg
Eccentricity:
0001649
Arg of perigee: 150
2607 deg
Mean anomaly: 209
8651 deg
Mean motion: 15
76035637 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1658
Checksum: 294
Coasting Arc #8 (Orbit 1673)
---------------------------------------
Vector Time (GMT): 2007/205/22:37:55
796
Vector Time (MET): N/A
Weight (LBS) : 508072
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2885342
09 A = 6719915
90 meter
Y = 4728731
52 meter E =
0006806
Z = -3810170
19 I = 51
31278
XDOT = -3506
330747 Wp = 87
77646
YDOT = -5465
493086 meter/sec RA = 267
96887 deg
ZDOT = -4133
965127 TA = 138
77703
MA = 138
72561
Ha = 187
202 n
mi
Hp = 180
269
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9466345
45 X = -2919495
99
Y = 15514211
04 feet Y = 4696275
63 meter
Z = -12500558
36 Z = -3824269
35
XDOT = -11503
709800 XDOT = -3424
872235
YDOT = -17931
407761 feet/sec YDOT = -5504
246753 meter/sec
ZDOT = -13562
877712 ZDOT = -4150
801790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17023671
22 X = -5188814
99
Y = -6258896
21 feet Y = -1907711
56 meter
Z = -12553375
48 Z = -3826268
85
XDOT = 14961
313073 XDOT = 4560
208225
YDOT = -13401
533628 feet/sec YDOT = -4084
787450 meter/sec
ZDOT = -13627
223846 ZDOT = -4153
577828
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 07205
96654806
00020000 00000-0 20000-3 0 9074
2 25544 51
6349 268
5680 0001557 154
4339 205
6902 15
76069743 16742
Satellite: ISS
Catalog Number: 25544
Epoch time: 07205
96654806 = yrday
fracday
Element set: 907
Inclination: 51
6349 deg
RA of node: 268
5680 deg
Eccentricity:
0001557
Arg of perigee: 154
4339 deg
Mean anomaly: 205
6902 deg
Mean motion: 15
76069743 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1674
Checksum: 318
Coasting Arc #9 (Orbit 1689)
---------------------------------------
Vector Time (GMT): 2007/206/22:37:55
796
Vector Time (MET): N/A
Weight (LBS) : 508072
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3117795
32 A = 6722155
66 meter
Y = 5100919
35 meter E =
0013998
Z = 3058634
03 I = 51
32206
XDOT = -3309
503131 Wp = 101
00839
YDOT = 4961
078798 meter/sec RA = 262
74325 deg
ZDOT = -4883
901094 TA = 43
29897
MA = 43
18904
Ha = 187
161 n
mi
Hp = 180
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10228987
27 X = 3045666
19
Y = 16735299
69 feet Y = 5135380
48 meter
Z = 10034888
56 Z = 3073605
83
XDOT = -10857
949906 XDOT = -3341
007747
YDOT = 16276
505242 feet/sec YDOT = 4923
894737 meter/sec
ZDOT = -16023
297553 ZDOT = -4900
054241
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14254522
17 X = -4344778
36
Y = 13429768
58 feet Y = 4093393
46 meter
Z = 10092142
39 Z = 3076085
00
XDOT = -17180
369656 XDOT = -5236
576671
YDOT = -6109
037168 feet/sec YDOT = -1862
034529 meter/sec
ZDOT = -16083
864249 ZDOT = -4902
361823
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 07206
98104292
00020000 00000-0 20000-3 0 9087
2 25544 51
6342 263
3415 0001603 155
9214 204
2026 15
76074737 16903
Satellite: ISS
Catalog Number: 25544
Epoch time: 07206
98104292 = yrday
fracday
Element set: 908
Inclination: 51
6342 deg
RA of node: 263
3415 deg
Eccentricity:
0001603
Arg of perigee: 155
9214 deg
Mean anomaly: 204
2026 deg
Mean motion: 15
76074737 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1690
Checksum: 272
Coasting Arc #10 (Orbit 1705)
---------------------------------------
Vector Time (GMT): 2007/207/22:37:55
796
Vector Time (MET): N/A
Weight (LBS) : 508072
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2942869
51 A = 6716754
29 meter
Y = -3874131
06 meter E =
0009212
Z = 4626574
49 I = 51
30949
XDOT = 3666
445144 Wp = 123
08974
YDOT = 6164
298330 meter/sec RA = 257
61462 deg
ZDOT = 2820
600477 TA = 298
90209
MA = 298
99448
Ha = 187
025 n
mi
Hp = 180
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9655083
71 X = 2963497
10
Y = -12710403
73 feet Y = -3841107
70 meter
Z = 15179050
15 Z = 4640920
22
XDOT = 12029
019501 XDOT = 3583
540748
YDOT = 20224
075885 feet/sec YDOT = 6204
834553 meter/sec
ZDOT = 9253
938572 ZDOT = 2838
211553
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14535827
12 X = 4430520
11
Y = 6468921
51 feet Y = 1971727
28 meter
Z = 15232903
61 Z = 4642989
02
XDOT = -16543
777986 XDOT = -5042
543530
YDOT = 15155
202722 feet/sec YDOT = 4619
305790 meter/sec
ZDOT = 9321
315347 ZDOT = 2841
136918
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 07207
99551705
00020000 00000-0 20000-3 0 9095
2 25544 51
6346 258
1145 0001482 160
3767 199
7454 15
76116167 17062
Satellite: ISS
Catalog Number: 25544
Epoch time: 07207
99551705 = yrday
fracday
Element set: 909
Inclination: 51
6346 deg
RA of node: 258
1145 deg
Eccentricity:
0001482
Arg of perigee: 160
3767 deg
Mean anomaly: 199
7454 deg
Mean motion: 15
76116167 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1706
Checksum: 309
Coasting Arc #11 (Orbit 1720)
---------------------------------------
Vector Time (GMT): 2007/208/22:37:55
796
Vector Time (MET): N/A
Weight (LBS) : 508072
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3282748
31 A = 6724586
68 meter
Y = -5583581
52 meter E =
0006546
Z = -1801373
50 I = 51
34384
XDOT = 3510
221896 Wp = 47
83659
YDOT = -3880
904501 meter/sec RA = 252
40120 deg
ZDOT = 5649
891936 TA = 292
09638
MA = 292
16587
Ha = 186
937 n
mi
Hp = 180
301
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10770171
62 X = -3211317
30
Y = -18318837
00 feet Y = -5619891
36 meter
Z = -5910018
03 Z = -1817148
26
XDOT = 11516
476037 XDOT = 3525
912161
YDOT = -12732
626314 feet/sec YDOT = -3841
564443 meter/sec
ZDOT = 18536
390867 ZDOT = 5666
981777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15184597
39 X = 4628265
29
Y = -14842073
84 feet Y = -4523864
11 meter
Z = -5970389
01 Z = -1819774
57
XDOT = 14029
083465 XDOT = 4276
064640
YDOT = 6893
301454 feet/sec YDOT = 2101
078283 meter/sec
ZDOT = 18600
633291 ZDOT = 5669
473027
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 07208
94656922
00020000 00000-0 20000-3 0 9100
2 25544 51
6345 253
2142 0001389 167
3976 192
7224 15
76160116 17217
Satellite: ISS
Catalog Number: 25544
Epoch time: 07208
94656922 = yrday
fracday
Element set: 910
Inclination: 51
6345 deg
RA of node: 253
2142 deg
Eccentricity:
0001389
Arg of perigee: 167
3976 deg
Mean anomaly: 192
7224 deg
Mean motion: 15
76160116 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1721
Checksum: 289
Coasting Arc #12 (Orbit 1736)
---------------------------------------
Vector Time (GMT): 2007/209/22:37:55
796
Vector Time (MET): N/A
Weight (LBS) : 508072
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3256337
53 A = 6714369
24 meter
Y = 2868150
41 meter E =
0014236
Z = -5136152
59 I = 51
31898
XDOT = -3825
813567 Wp = 85
65682
YDOT = -6559
380590 meter/sec RA = 247
25417 deg
ZDOT = -1239
224049 TA = 172
44698
MA = 172
42551
Ha = 186
825 n
mi
Hp = 180
207
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10683522
09 X = -3263217
62
Y = 9409942
28 feet Y = 2831698
52 meter
Z = -16850894
33 Z = -5151987
83
XDOT = -12551
881780 XDOT = -3746
161464
YDOT = -21520
277527 feet/sec YDOT = -6601
717444 meter/sec
ZDOT = -4065
695698 ZDOT = -1257
616990
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11824115
91 X = -3603990
53
Y = -7801429
38 feet Y = -2377875
67 meter
Z = -16910507
99 Z = -5154322
83
XDOT = 16988
628225 XDOT = 5178
133883
YDOT = -16796
428242 feet/sec YDOT = -5119
551328 meter/sec
ZDOT = -4136
109100 ZDOT = -1260
686054
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 07209
96100637
00020000 00000-0 20000-3 0 9111
2 25544 51
6339 247
9868 0001283 173
0627 187
0555 15
76199206 17378
Satellite: ISS
Catalog Number: 25544
Epoch time: 07209
96100637 = yrday
fracday
Element set: 911
Inclination: 51
6339 deg
RA of node: 247
9868 deg
Eccentricity:
0001283
Arg of perigee: 173
0627 deg
Mean anomaly: 187
0555 deg
Mean motion: 15
76199206 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1737
Checksum: 311
Coasting Arc #13 (Orbit 1752)
---------------------------------------
Vector Time (GMT): 2007/210/22:37:55
796
Vector Time (MET): N/A
Weight (LBS) : 508072
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3377959
51 A = 6725970
14 meter
Y = 5798194
72 meter E =
0014006
Z = 335689
16 I = 51
36993
XDOT = -4007
415466 Wp = 135
78603
YDOT = 2690
604100 meter/sec RA = 242
06658 deg
ZDOT = -6007
542500 TA = 40
54701
MA = 40
44276
Ha = 186
871 n
mi
Hp = 180
377
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11082544
33 X = 3311241
51
Y = 19022948
54 feet Y = 5835595
88 meter
Z = 1101342
40 Z = 351937
59
XDOT = -13147
688537 XDOT = -4008
021509
YDOT = 8827
441274 feet/sec YDOT = 2645
788305 meter/sec
ZDOT = -19709
785104 ZDOT = -6027
011188
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15248920
38 X = -4647870
93
Y = 15875291
03 feet Y = 4838788
70 meter
Z = 1163562
30 Z = 354653
79
XDOT = -10911
263441 XDOT = -3325
753097
YDOT = -8998
835251 feet/sec YDOT = -2742
844985 meter/sec
ZDOT = -19783
178815 ZDOT = -6029
912903
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 07210
97542619
00020000 00000-0 20000-3 0 9125
2 25544 51
6336 242
7597 0001483 176
3894 183
7281 15
76166176 17538
Satellite: ISS
Catalog Number: 25544
Epoch time: 07210
97542619 = yrday
fracday
Element set: 912
Inclination: 51
6336 deg
RA of node: 242
7597 deg
Eccentricity:
0001483
Arg of perigee: 176
3894 deg
Mean anomaly: 183
7281 deg
Mean motion: 15
76166176 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 1753
Checksum: 315
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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