Date:
April 29th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5812 51 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
118/10:40:40
784 7
5 7
6 7
6
N/A 0
8 -0
0 188
9
000/00:01:17
567 1
0 -0
0 175
1
Coasting Arc #1 (Orbit 260)
---------------------------------------
Vector Time (GMT): 2007/116/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5644452
77 A = 6714446
54 meter
Y = 1556989
05 meter E =
0029860
Z = 3255650
58 I = 51
69811
XDOT = -4019
569544 Wp = 99
81826
YDOT = -4571
970549 meter/sec RA = 10
62840 deg
ZDOT = -4750
750598 TA = 41
92091
MA = 41
69268
Ha = 189
238 n
mi
Hp = 170
560
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18518545
83 X = -5677259
09
Y = 5108231
79 feet Y = 1493686
18 meter
Z = 10681268
32 Z = 3228150
17
XDOT = -13187
564121 XDOT = -3945
068094
YDOT = -14999
903376 feet/sec YDOT = -4616
503060 meter/sec
ZDOT = -15586
452092 ZDOT = -4770
096697
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16027832
95 X = -4885283
48
Y = 10692864
17 feet Y = 3259185
00 meter
Z = 10577867
99 Z = 3224134
16
XDOT = -16374
133389 XDOT = -4990
835857
YDOT = -8948
526368 feet/sec YDOT = -2727
510837 meter/sec
ZDOT = -15659
870932 ZDOT = -4773
128660
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 07116
49673213
00020000 00000-0 20000-3 0 9009
2 25544 51
6352 10
9408 0017178 106
0785 254
2273 15
78642941 2618
Satellite: ISS
Catalog Number: 25544
Epoch time: 07116
49673213 = yrday
fracday
Element set: 900
Inclination: 51
6352 deg
RA of node: 10
9408 deg
Eccentricity:
0017178
Arg of perigee: 106
0785 deg
Mean anomaly: 254
2273 deg
Mean motion: 15
78642941 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 261
Checksum: 279
Coasting Arc #2 (Orbit 276)
---------------------------------------
Vector Time (GMT): 2007/117/11:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 464586
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2079658
68 A = 6708283
58 meter
Y = 4082696
94 meter E =
0023292
Z = 4884494
97 I = 51
65015
XDOT = -7320
389444 Wp = 113
03457
YDOT = 1056
451684 meter/sec RA = 5
50299 deg
ZDOT = 2216
464462 TA = 315
40026
MA = 315
58744
Ha = 188
946 n
mi
Hp = 170
551
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6823027
16 X = 2010122
74
Y = 13394675
01 feet Y = 4105564
10 meter
Z = 16025245
96 Z = 4894429
04
XDOT = -24017
025734 XDOT = -7342
425987
YDOT = 3466
048833 feet/sec YDOT = 974
467793 meter/sec
ZDOT = 7271
865034 ZDOT = 2180
848375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10785947
29 X = 3287556
73
Y = 10412395
38 feet Y = 3173698
11 meter
Z = 16063153
18 Z = 4896049
09
XDOT = -20796
354430 XDOT = -6338
728830
YDOT = 10443
648166 feet/sec YDOT = 3183
223961 meter/sec
ZDOT = 7137
838506 ZDOT = 2175
613177
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 07117
50955147
00020000 00000-0 20000-3 0 9012
2 25544 51
6357 5
7029 0017039 110
0659 250
2342 15
78707598 2775
Satellite: ISS
Catalog Number: 25544
Epoch time: 07117
50955147 = yrday
fracday
Element set: 901
Inclination: 51
6357 deg
RA of node: 5
7029 deg
Eccentricity:
0017039
Arg of perigee: 110
0659 deg
Mean anomaly: 250
2342 deg
Mean motion: 15
78707598 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 277
Checksum: 289
Coasting Arc #3 (Orbit 291)
---------------------------------------
Vector Time (GMT): 2007/118/10:41:19
567
Vector Time (MET): N/A
Weight (LBS) : 464165
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1435756
38 A = 6711367
79 meter
Y = -4075403
41 meter E =
0024761
Z = -5156933
39 I = 51
61867
XDOT = 7510
961208 Wp = 108
77083
YDOT = 1047
141444 meter/sec RA =
37038 deg
ZDOT = 1260
721193 TA = 173
32129
MA = 173
28823
Ha = 188
905 n
mi
Hp = 175
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4710486
82 X = 1506273
06
Y = -13370746
09 feet Y = -4058953
75 meter
Z = -16919072
79 Z = -5149787
10
XDOT = 24642
261181 XDOT = 7492
569288
YDOT = 3435
503426 feet/sec YDOT = 1131
030400 meter/sec
ZDOT = 4136
224386 ZDOT = 1297
165023
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1026005
05 X = 312726
34
Y = -14170619
44 feet Y = -4319204
81 meter
Z = -16892643
94 Z = -5148877
87
XDOT = 23601
005744 XDOT = 7193
586551
YDOT = -3397
074298 feet/sec YDOT = -1035
428246 meter/sec
ZDOT = 4273
616209 ZDOT = 1302
598221
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 07118
45904855
00020000 00000-0 20000-3 0 9028
2 25544 51
6362
7919 0010998 121
1269 239
0976 15
77271257 2923
Satellite: ISS
Catalog Number: 25544
Epoch time: 07118
45904855 = yrday
fracday
Element set: 902
Inclination: 51
6362 deg
RA of node:
7919 deg
Eccentricity:
0010998
Arg of perigee: 121
1269 deg
Mean anomaly: 239
0976 deg
Mean motion: 15
77271257 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 292
Checksum: 303
Coasting Arc #4 (Orbit 307)
---------------------------------------
Vector Time (GMT): 2007/119/10:41:19
567
Vector Time (MET): N/A
Weight (LBS) : 464165
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6242209
60 A = 6720742
83 meter
Y = -1204972
49 meter E =
0016949
Z = -2170462
64 I = 51
62202
XDOT = 2791
036756 Wp = 129
52379
YDOT = -4609
044016 meter/sec RA = 355
23886 deg
ZDOT = -5507
162846 TA = 74
81590
MA = 74
62851
Ha = 188
758 n
mi
Hp = 175
212
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20479690
30 X = -6217727
65
Y = -3953321
83 feet Y = -1274639
50 meter
Z = -7120940
43 Z = -2200728
19
XDOT = 9156
944737 XDOT = 2869
121441
YDOT = -15121
535485 feet/sec YDOT = -4577
396502 meter/sec
ZDOT = -18068
119574 ZDOT = -5493
414143
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20716812
81 X = -6314484
54
Y = 2054653
33 feet Y = 626258
34 meter
Z = -7235076
19 Z = -2205251
22
XDOT = 4698
427157 XDOT = 1432
080598
YDOT = -15626
092891 feet/sec YDOT = -4762
833113 meter/sec
ZDOT = -18016
886538 ZDOT = -5491
547017
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 07119
47276343
00020000 00000-0 20000-3 0 9036
2 25544 51
6364 355
5599 0010912 125
8421 234
3759 15
77275932 3086
Satellite: ISS
Catalog Number: 25544
Epoch time: 07119
47276343 = yrday
fracday
Element set: 903
Inclination: 51
6364 deg
RA of node: 355
5599 deg
Eccentricity:
0010912
Arg of perigee: 125
8421 deg
Mean anomaly: 234
3759 deg
Mean motion: 15
77275932 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 308
Checksum: 304
Coasting Arc #5 (Orbit 323)
---------------------------------------
Vector Time (GMT): 2007/120/10:41:19
567
Vector Time (MET): N/A
Weight (LBS) : 464165
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3336710
63 A = 6714865
77 meter
Y = 3991694
88 meter E =
0018498
Z = 4227400
65 I = 51
57382
XDOT = -6614
224675 Wp = 101
50086
YDOT = -1723
798315 meter/sec RA = 350
03030 deg
ZDOT = -3583
446428 TA = 24
89230
MA = 24
80320
Ha = 188
664 n
mi
Hp = 175
239
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10947213
35 X = -3401634
63
Y = 13096111
80 feet Y = 3954018
86 meter
Z = 13869424
70 Z = 4211032
98
XDOT = -21700
212188 XDOT = -6577
049308
YDOT = -5655
506283 feet/sec YDOT = -1797
554387 meter/sec
ZDOT = -11756
714004 ZDOT = -3615
488572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6549593
65 X = -1996316
14
Y = 15815989
47 feet Y = 4820713
59 meter
Z = 13808253
55 Z = 4208755
68
XDOT = -21178
404974 XDOT = -6455
177836
YDOT = 1626
948125 feet/sec YDOT = 495
893788 meter/sec
ZDOT = -11877
598441 ZDOT = -3620
292005
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 07120
48645512
00020000 00000-0 20000-3 0 9048
2 25544 51
6360 350
3281 0010775 128
6166 231
5965 15
77362091 3246
Satellite: ISS
Catalog Number: 25544
Epoch time: 07120
48645512 = yrday
fracday
Element set: 904
Inclination: 51
6360 deg
RA of node: 350
3281 deg
Eccentricity:
0010775
Arg of perigee: 128
6166 deg
Mean anomaly: 231
5965 deg
Mean motion: 15
77362091 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 324
Checksum: 276
Coasting Arc #6 (Orbit 339)
---------------------------------------
Vector Time (GMT): 2007/121/10:41:19
567
Vector Time (MET): N/A
Weight (LBS) : 464165
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5110522
51 A = 6715784
93 meter
Y = 1856557
16 meter E =
0020965
Z = 3932638
91 I = 51
54914
XDOT = -4754
596820 Wp = 116
21069
YDOT = 4568
269215 meter/sec RA = 344
91430 deg
ZDOT = 3996
526317 TA = 292
23524
MA = 292
45748
Ha = 188
477 n
mi
Hp = 175
324
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16766806
14 X = 5070277
97
Y = 6091066
80 feet Y = 1913480
76 meter
Z = 12902358
61 Z = 3957368
60
XDOT = -15599
070931 XDOT = -4824
741275
YDOT = 14987
759893 feet/sec YDOT = 4514
708340 meter/sec
ZDOT = 13111
962983 ZDOT = 3973
257779
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17765229
20 X = 5414841
86
Y = 453614
26 feet Y = 138261
63 meter
Z = 12995714
93 Z = 3961093
91
XDOT = -10045
988008 XDOT = -3062
017145
YDOT = 17904
871694 feet/sec YDOT = 5457
404892 meter/sec
ZDOT = 13024
867997 ZDOT = 3969
979766
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 07121
50012602
00020000 00000-0 20000-3 0 9051
2 25544 51
6361 345
0956 0010757 132
5267 227
6808 15
77359071 3407
Satellite: ISS
Catalog Number: 25544
Epoch time: 07121
50012602 = yrday
fracday
Element set: 905
Inclination: 51
6361 deg
RA of node: 345
0956 deg
Eccentricity:
0010757
Arg of perigee: 132
5267 deg
Mean anomaly: 227
6808 deg
Mean motion: 15
77359071 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 340
Checksum: 270
Coasting Arc #7 (Orbit 354)
---------------------------------------
Vector Time (GMT): 2007/122/10:41:19
567
Vector Time (MET): N/A
Weight (LBS) : 464165
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4811965
84 A = 6719710
74 meter
Y = -3944176
41 meter E =
0012058
Z = -2554590
89 I = 51
53501
XDOT = 4948
715782 Wp = 110
62654
YDOT = 2633
905621 meter/sec RA = 339
69717 deg
ZDOT = 5270
867037 TA = 220
35549
MA = 220
44503
Ha = 188
340 n
mi
Hp = 175
529
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15787289
50 X = 4868122
56
Y = -12940211
33 feet Y = -3890052
20 meter
Z = -8381203
72 Z = -2531077
65
XDOT = 16235
944167 XDOT = 4893
289805
YDOT = 8641
422641 feet/sec YDOT = 2688
934773 meter/sec
ZDOT = 17292
870857 ZDOT = 5294
773905
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10585530
38 X = 3226469
66
Y = -17495799
95 feet Y = -5332719
82 meter
Z = -8293110
75 Z = -2527740
16
XDOT = 16825
458092 XDOT = 5128
399626
YDOT = 1965
089300 feet/sec YDOT = 598
959219 meter/sec
ZDOT = 17383
217302 ZDOT = 5298
404634
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 07122
45042068
00020000 00000-0 20000-3 0 9066
2 25544 51
6359 340
1899 0010546 136
7134 223
4861 15
77404576 3551
Satellite: ISS
Catalog Number: 25544
Epoch time: 07122
45042068 = yrday
fracday
Element set: 906
Inclination: 51
6359 deg
RA of node: 340
1899 deg
Eccentricity:
0010546
Arg of perigee: 136
7134 deg
Mean anomaly: 223
4861 deg
Mean motion: 15
77404576 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 355
Checksum: 289
Coasting Arc #8 (Orbit 370)
---------------------------------------
Vector Time (GMT): 2007/123/10:41:19
567
Vector Time (MET): N/A
Weight (LBS) : 464165
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3421800
08 A = 6711180
12 meter
Y = -2824709
89 meter E =
0020578
Z = -5050979
49 I = 51
47964
XDOT = 6092
458784 Wp = 104
05214
YDOT = -4384
265827 meter/sec RA = 334
56119 deg
ZDOT = -1686
134149 TA = 149
73893
MA = 149
61993
Ha = 188
128 n
mi
Hp = 175
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11226378
23 X = -3365422
19
Y = -9267420
89 feet Y = -2862658
79 meter
Z = -16571455
03 Z = -5067466
21
XDOT = 19988
381836 XDOT = 6149
222579
YDOT = -14384
074234 feet/sec YDOT = -4315
819037 meter/sec
ZDOT = -5531
936184 ZDOT = -1656
398789
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13678585
53 X = -4169232
87
Y = -4768671
05 feet Y = -1453490
94 meter
Z = -16633876
70 Z = -5070005
62
XDOT = 13347
114227 XDOT = 4068
200416
YDOT = -19499
102998 feet/sec YDOT = -5943
326594 meter/sec
ZDOT = -5420
456348 ZDOT = -1652
155095
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 07123
46404740
00020000 00000-0 20000-3 0 9078
2 25544 51
6352 334
9565 0010429 140
8391 219
3530 15
77452513 3715
Satellite: ISS
Catalog Number: 25544
Epoch time: 07123
46404740 = yrday
fracday
Element set: 907
Inclination: 51
6352 deg
RA of node: 334
9565 deg
Eccentricity:
0010429
Arg of perigee: 140
8391 deg
Mean anomaly: 219
3530 deg
Mean motion: 15
77452513 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 371
Checksum: 275
Coasting Arc #9 (Orbit 386)
---------------------------------------
Vector Time (GMT): 2007/124/10:41:19
567
Vector Time (MET): N/A
Weight (LBS) : 464165
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5634113
33 A = 6722402
90 meter
Y = 3630746
25 meter E =
0023243
Z = 318968
11 I = 51
49191
XDOT = -2855
183567 Wp = 137
56204
YDOT = -3880
519733 meter/sec RA = 329
37137 deg
ZDOT = -6024
852968 TA = 38
95536
MA = 38
78813
Ha = 188
128 n
mi
Hp = 175
736
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18484623
77 X = -5675843
63
Y = 11911897
15 feet Y = 3567509
09 meter
Z = 1046483
31 Z = 291496
03
XDOT = -9367
400154 XDOT = -2782
310619
YDOT = -12731
363953 feet/sec YDOT = -3912
039984 meter/sec
ZDOT = -19766
577979 ZDOT = -6038
547066
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12825846
78 X = -3909318
10
Y = 17868332
96 feet Y = 5446267
89 meter
Z = 943434
51 Z = 287558
84
XDOT = -11981
586446 XDOT = -3651
987549
YDOT = -7508
459904 feet/sec YDOT = -2288
578579 meter/sec
ZDOT = -19818
603907 ZDOT = -6040
710471
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 07124
47765390
00020000 00000-0 20000-3 0 9082
2 25544 51
6353 329
7240 0010576 145
2300 214
9558 15
77432237 3879
Satellite: ISS
Catalog Number: 25544
Epoch time: 07124
47765390 = yrday
fracday
Element set: 908
Inclination: 51
6353 deg
RA of node: 329
7240 deg
Eccentricity:
0010576
Arg of perigee: 145
2300 deg
Mean anomaly: 214
9558 deg
Mean motion: 15
77432237 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 387
Checksum: 293
Coasting Arc #10 (Orbit 402)
---------------------------------------
Vector Time (GMT): 2007/125/10:41:19
567
Vector Time (MET): N/A
Weight (LBS) : 464165
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1554777
22 A = 6710409
13 meter
Y = 3967740
56 meter E =
0010813
Z = 5175440
81 I = 51
42781
XDOT = -6623
492018 Wp = 129
35866
YDOT = 3837
203583 meter/sec RA = 324
19022 deg
ZDOT = -957
430639 TA = 329
74418
MA = 329
80657
Ha = 187
803 n
mi
Hp = 175
828
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5100975
13 X = 1485152
06
Y = 13017521
52 feet Y = 3984737
09 meter
Z = 16979792
69 Z = 5182825
35
XDOT = -21730
616856 XDOT = -6661
256811
YDOT = 12589
250602 feet/sec YDOT = 3762
924937 meter/sec
ZDOT = -3141
176636 ZDOT = -989
699397
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9610910
71 X = 2929405
58
Y = 10106696
21 feet Y = 3080521
00 meter
Z = 17008064
58 Z = 5184058
08
XDOT = -14496
870288 XDOT = -4418
646064
YDOT = 19245
663266 feet/sec YDOT = 5866
078163 meter/sec
ZDOT = -3262
274162 ZDOT = -994
341165
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 07125
49123531
00020000 00000-0 20000-3 0 9091
2 25544 51
6349 324
4905 0010312 149
1572 211
0200 15
77516865 4037
Satellite: ISS
Catalog Number: 25544
Epoch time: 07125
49123531 = yrday
fracday
Element set: 909
Inclination: 51
6349 deg
RA of node: 324
4905 deg
Eccentricity:
0010312
Arg of perigee: 149
1572 deg
Mean anomaly: 211
0200 deg
Mean motion: 15
77516865 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 403
Checksum: 260
Coasting Arc #11 (Orbit 418)
---------------------------------------
Vector Time (GMT): 2007/126/10:41:19
567
Vector Time (MET): N/A
Weight (LBS) : 464165
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5731473
23 A = 6720320
16 meter
Y = -2904661
94 meter E =
0018138
Z = 1961651
97 I = 51
43832
XDOT = 736
272667 Wp = 102
26551
YDOT = 5255
895095 meter/sec RA = 319
03852 deg
ZDOT = 5584
148393 TA = 279
66097
MA = 279
86582
Ha = 187
653 n
mi
Hp = 175
905
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18804046
03 X = 5753998
14
Y = -9529730
78 feet Y = -2840443
69 meter
Z = 6435866
03 Z = 1989550
17
XDOT = 2415
592738 XDOT = 650
318662
YDOT = 17243
750313 feet/sec YDOT = 5263
647263 meter/sec
ZDOT = 18320
696829 ZDOT = 5587
517079
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13408495
19 X = 4086909
33
Y = -16225316
55 feet Y = -4945476
48 meter
Z = 6540615
21 Z = 1993579
52
XDOT = 7816
727551 XDOT = 2382
538558
YDOT = 13911
714594 feet/sec YDOT = 4240
290608 meter/sec
ZDOT = 18333
992239 ZDOT = 5588
200834
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 07126
50479536
00020000 00000-0 20000-3 0 9105
2 25544 51
6339 319
2564 0010237 153
7835 206
3850 15
77567262 4190
Satellite: ISS
Catalog Number: 25544
Epoch time: 07126
50479536 = yrday
fracday
Element set: 910
Inclination: 51
6339 deg
RA of node: 319
2564 deg
Eccentricity:
0010237
Arg of perigee: 153
7835 deg
Mean anomaly: 206
3850 deg
Mean motion: 15
77567262 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 419
Checksum: 297
Coasting Arc #12 (Orbit 433)
---------------------------------------
Vector Time (GMT): 2007/127/10:41:19
567
Vector Time (MET): N/A
Weight (LBS) : 464165
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 209642
53 A = 6713987
72 meter
Y = -5171361
75 meter E =
0017366
Z = -4294749
23 I = 51
39521
XDOT = 6347
952783 Wp = 135
47965
YDOT = -2622
018282 meter/sec RA = 313
81523 deg
ZDOT = 3463
332649 TA = 169
71934
MA = 169
68377
Ha = 187
549 n
mi
Hp = 176
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 687803
57 X = 288317
13
Y = -16966409
93 feet Y = -5168577
02 meter
Z = -14090384
61 Z = -4293540
27
XDOT = 20826
616741 XDOT = 6359
976409
YDOT = -8602
422184 feet/sec YDOT = -2550
965090 meter/sec
ZDOT = 11362
639923 ZDOT = 3494
200141
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6337143
64 X = -1931561
38
Y = -15757036
38 feet Y = -4802744
69 meter
Z = -14086429
39 Z = -4293543
68
XDOT = 14178
344283 XDOT = 4321
559337
YDOT = -15974
814697 feet/sec YDOT = -4869
123520 meter/sec
ZDOT = 11478
611916 ZDOT = 3498
680912
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 07127
45498954
00020000 00000-0 20000-3 0 9116
2 25544 51
6331 314
3490 0010183 157
0716 203
0906 15
77578769 4348
Satellite: ISS
Catalog Number: 25544
Epoch time: 07127
45498954 = yrday
fracday
Element set: 911
Inclination: 51
6331 deg
RA of node: 314
3490 deg
Eccentricity:
0010183
Arg of perigee: 157
0716 deg
Mean anomaly: 203
0906 deg
Mean motion: 15
77578769 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 434
Checksum: 296
Coasting Arc #13 (Orbit 448)
---------------------------------------
Vector Time (GMT): 2007/128/10:41:19
567
Vector Time (MET): N/A
Weight (LBS) : 464165
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5232179
45 A = 6715072
95 meter
Y = 1507779
40 meter E =
0012419
Z = -3932762
48 I = 51
37958
XDOT = 1115
884104 Wp = 126
35060
YDOT = -6493
285610 meter/sec RA = 308
68513 deg
ZDOT = -3990
011638 TA = 102
18832
MA = 102
04919
Ha = 187
310 n
mi
Hp = 176
155
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17165943
06 X = -5229546
06
Y = 4946782
79 feet Y = 1449285
37 meter
Z = -12902764
05 Z = -3958173
96
XDOT = 3661
037086 XDOT = 1207
792859
YDOT = -21303
430479 feet/sec YDOT = -6480
292863 meter/sec
ZDOT = -13090
589364 ZDOT = -3984
368085
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13302750
30 X = -4054678
29
Y = 11819567
44 feet Y = 3602604
16 meter
Z = -12998316
86 Z = -3961886
98
XDOT = -4932
240314 XDOT = -1503
346848
YDOT = -19867
503181 feet/sec YDOT = -6055
614970 meter/sec
ZDOT = -13070
086117 ZDOT = -3983
762248
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 07128
46850758
00020000 00000-0 20000-3 0 9123
2 25544 51
6323 309
1157 0010108 160
9405 199
2140 15
77607401 4494
Satellite: ISS
Catalog Number: 25544
Epoch time: 07128
46850758 = yrday
fracday
Element set: 912
Inclination: 51
6323 deg
RA of node: 309
1157 deg
Eccentricity:
0010108
Arg of perigee: 160
9405 deg
Mean anomaly: 199
2140 deg
Mean motion: 15
77607401 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 449
Checksum: 279
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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