Date:
March 20th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6458 35 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 6 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 3659)
---------------------------------------
Vector Time (GMT): 2007/078/10:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6150007
04 A = 6718675
69 meter
Y = -820667
19 meter E =
0015720
Z = -2550760
31 I = 51
49989
XDOT = -1460
997447 Wp = 344
01898
YDOT = -5433
197012 meter/sec RA = 206
68847 deg
ZDOT = 5277
792776 TA = 346
91243
MA = 346
95318
Ha = 186
545 n
mi
Hp = 177
955
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20177188
44 X = -6127982
08
Y = -2692477
64 feet Y = -889317
15 meter
Z = -8368636
20 Z = -2580583
26
XDOT = -4793
298712 XDOT = -1425
772476
YDOT = -17825
449513 feet/sec YDOT = -5449
337150 meter/sec
ZDOT = 17315
593098 ZDOT = 5270
781476
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17176068
17 X = -5235265
58
Y = -10837894
93 feet Y = -3303390
38 meter
Z = -8480870
05 Z = -2584969
19
XDOT = 2194
976539 XDOT = 669
028849
YDOT = -16988
926569 feet/sec YDOT = -5178
224818 meter/sec
ZDOT = 17288
452395 ZDOT = 5269
520290
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 07078
44822690
00020000 00000-0 20000-3 0 9006
2 25544 51
6327 207
6431 0014653 324
7980 35
2215 15
77723459 36604
Satellite: ISS
Catalog Number: 25544
Epoch time: 07078
44822690 = yrday
fracday
Element set: 900
Inclination: 51
6327 deg
RA of node: 207
6431 deg
Eccentricity:
0014653
Arg of perigee: 324
7980 deg
Mean anomaly: 35
2215 deg
Mean motion: 15
77723459 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3660
Checksum: 292
Coasting Arc #2 (Orbit 3675)
---------------------------------------
Vector Time (GMT): 2007/079/10:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 178795
44 A = 6710246
87 meter
Y = 4404842
52 meter E =
0016615
Z = -5067638
40 I = 51
49838
XDOT = -7372
123509 Wp = 20
74745
YDOT = -1549
176044 meter/sec RA = 201
55136 deg
ZDOT = -1592
956783 TA = 233
84673
MA = 234
00057
Ha = 186
822 n
mi
Hp = 177
586
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 586599
23 X = 154144
25
Y = 14451583
08 feet Y = 4406703
57 meter
Z = -16626110
22 Z = -5066830
13
XDOT = -24186
756920 XDOT = -7346
514192
YDOT = -5082
598569 feet/sec YDOT = -1631
472226 meter/sec
ZDOT = -5226
236166 ZDOT = -1628
708191
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5174673
26 X = -1577240
41
Y = 13510633
25 feet Y = 4118041
01 meter
Z = -16622437
82 Z = -5066519
05
XDOT = -19104
865086 XDOT = -5823
162878
YDOT = -13968
231723 feet/sec YDOT = -4257
517029 meter/sec
ZDOT = -5360
866591 ZDOT = -1633
992137
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 07079
46164728
00020000 00000-0 20000-3 0 9011
2 25544 51
6331 202
4102 0014730 329
1621 30
8677 15
77779084 36769
Satellite: ISS
Catalog Number: 25544
Epoch time: 07079
46164728 = yrday
fracday
Element set: 901
Inclination: 51
6331 deg
RA of node: 202
4102 deg
Eccentricity:
0014730
Arg of perigee: 329
1621 deg
Mean anomaly: 30
8677 deg
Mean motion: 15
77779084 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3676
Checksum: 292
Coasting Arc #3 (Orbit 3691)
---------------------------------------
Vector Time (GMT): 2007/080/10:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6478140
00 A = 6721316
82 meter
Y = 1798551
37 meter E =
0005158
Z = 125143
37 I = 51
56292
XDOT = -1170
342414 Wp = 27
93439
YDOT = 4642
083680 meter/sec RA = 196
36290 deg
ZDOT = -6027
602100 TA = 150
70417
MA = 150
67524
Ha = 186
977 n
mi
Hp = 177
300
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21253740
17 X = 6456938
95
Y = 5900759
07 feet Y = 1870875
02 meter
Z = 410575
37 Z = 156562
66
XDOT = -3839
706084 XDOT = -1192
882765
YDOT = 15229
933332 feet/sec YDOT = 4628
869788 meter/sec
ZDOT = -19775
597441 ZDOT = -6033
342732
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17336829
55 X = 5284265
65
Y = 13633178
03 feet Y = 4155392
66 meter
Z = 528960
10 Z = 161227
04
XDOT = -8315
581629 XDOT = -2534
589281
YDOT = 11353
043757 feet/sec YDOT = 3460
407737 meter/sec
ZDOT = -19796
515702 ZDOT = -6033
977986
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 07080
47504341
00020000 00000-0 20000-3 0 9024
2 25544 51
6326 197
1747 0014842 332
9002 27
1387 15
77817531 36922
Satellite: ISS
Catalog Number: 25544
Epoch time: 07080
47504341 = yrday
fracday
Element set: 902
Inclination: 51
6326 deg
RA of node: 197
1747 deg
Eccentricity:
0014842
Arg of perigee: 332
9002 deg
Mean anomaly: 27
1387 deg
Mean motion: 15
77817531 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3692
Checksum: 288
Coasting Arc #4 (Orbit 3707)
---------------------------------------
Vector Time (GMT): 2007/081/10:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2246435
97 A = 6709808
40 meter
Y = -3705749
08 meter E =
0016257
Z = 5127726
46 I = 51
55283
XDOT = 7168
108546 Wp = 352
26688
YDOT = 2489
860852 meter/sec RA = 191
18281 deg
ZDOT = -1325
560098 TA = 110
51298
MA = 110
33843
Ha = 187
138 n
mi
Hp = 177
031
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7370196
74 X = 2262797
55
Y = -12157969
41 feet Y = -3680536
48 meter
Z = 16823249
56 Z = 5138679
59
XDOT = 23517
416489 XDOT = 7146
173173
YDOT = 8168
834816 feet/sec YDOT = 2569
895950 meter/sec
ZDOT = -4348
950452 ZDOT = -1290
790667
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11252668
94 X = 3429813
49
Y = -8610683
11 feet Y = -2624536
21 meter
Z = 16863905
95 Z = 5140118
53
XDOT = 18231
292454 XDOT = 5556
897940
YDOT = 15466
018652 feet/sec YDOT = 4714
042485 meter/sec
ZDOT = -4217
863247 ZDOT = -1285
604718
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 07081
48841740
00020000 00000-0 20000-3 0 9034
2 25544 51
6334 191
9405 0014823 337
3076 22
7432 15
77815046 37082
Satellite: ISS
Catalog Number: 25544
Epoch time: 07081
48841740 = yrday
fracday
Element set: 903
Inclination: 51
6334 deg
RA of node: 191
9405 deg
Eccentricity:
0014823
Arg of perigee: 337
3076 deg
Mean anomaly: 22
7432 deg
Mean motion: 15
77815046 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3708
Checksum: 288
Coasting Arc #5 (Orbit 3723)
---------------------------------------
Vector Time (GMT): 2007/082/10:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5755585
29 A = 6718725
35 meter
Y = -2495826
79 meter E =
0019922
Z = 2367637
79 I = 51
61254
XDOT = 3907
741180 Wp = 25
66228
YDOT = -3888
842311 meter/sec RA = 186
04603 deg
ZDOT = 5400
934943 TA = 1
11202
MA = 1
10759
Ha = 187
269 n
mi
Hp = 176
710
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18883153
84 X = -5738750
41
Y = -8188408
09 feet Y = -2560094
80 meter
Z = 7767840
53 Z = 2339718
04
XDOT = 12820
673164 XDOT = 3924
699527
YDOT = -12758
668999 feet/sec YDOT = -3845
048863 meter/sec
ZDOT = 17719
602832 ZDOT = 5419
960034
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14812153
63 X = -4514744
43
Y = -14347441
99 feet Y = -4373100
32 meter
Z = 7662498
68 Z = 2335529
60
XDOT = 15363
067252 XDOT = 4682
662899
YDOT = -6360
799414 feet/sec YDOT = -1938
771661 meter/sec
ZDOT = 17790
594330 ZDOT = 5422
573152
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 07082
50176373
00020000 00000-0 20000-3 0 9042
2 25544 51
6339 186
7061 0014814 340
9221 19
1387 15
77899830 37249
Satellite: ISS
Catalog Number: 25544
Epoch time: 07082
50176373 = yrday
fracday
Element set: 904
Inclination: 51
6339 deg
RA of node: 186
7061 deg
Eccentricity:
0014814
Arg of perigee: 340
9221 deg
Mean anomaly: 19
1387 deg
Mean motion: 15
77899830 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3724
Checksum: 303
Coasting Arc #6 (Orbit 3738)
---------------------------------------
Vector Time (GMT): 2007/083/10:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4435894
99 A = 6714089
73 meter
Y = 3086012
49 meter E =
0012505
Z = -3978213
31 I = 51
62565
XDOT = -5778
331784 Wp = 13
35163
YDOT = -3219
931396 meter/sec RA = 180
83324 deg
ZDOT = 3959
733779 TA = 297
51567
MA = 297
64270
Ha = 187
378 n
mi
Hp = 176
375
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14553461
25 X = -4450748
14
Y = 10124712
90 feet Y = 3036324
79 meter
Z = -13051880
93 Z = -3999798
92
XDOT = -18957
781444 XDOT = -5761
132219
YDOT = -10564
079383 feet/sec YDOT = -3284
451766 meter/sec
ZDOT = 12991
252555 ZDOT = 3931
704484
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17046487
16 X = -5195769
29
Y = 4649306
49 feet Y = 1417108
62 meter
Z = -13132626
02 Z = -4002824
41
XDOT = -14014
313638 XDOT = -4271
562797
YDOT = -15119
046140 feet/sec YDOT = -4608
285263 meter/sec
ZDOT = 12885
385796 ZDOT = 3927
465591
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 07083
45175684
00020000 00000-0 20000-3 0 9052
2 25544 51
6337 181
7996 0015024 344
4275 15
6426 15
77897723 37391
Satellite: ISS
Catalog Number: 25544
Epoch time: 07083
45175684 = yrday
fracday
Element set: 905
Inclination: 51
6337 deg
RA of node: 181
7996 deg
Eccentricity:
0015024
Arg of perigee: 344
4275 deg
Mean anomaly: 15
6426 deg
Mean motion: 15
77897723 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3739
Checksum: 325
Coasting Arc #7 (Orbit 3754)
---------------------------------------
Vector Time (GMT): 2007/084/10:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4072309
86 A = 6712902
82 meter
Y = 3133961
75 meter E =
0018546
Z = -4334549
64 I = 51
65073
XDOT = -6110
948156 Wp = 16
74437
YDOT = 3178
338912 meter/sec RA = 175
71796 deg
ZDOT = -3429
422251 TA = 218
55681
MA = 218
68941
Ha = 187
564 n
mi
Hp = 176
205
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13360596
66 X = 4058019
10
Y = 10282026
75 feet Y = 3179420
71 meter
Z = -14220963
39 Z = -4314801
20
XDOT = -20049
042508 XDOT = -6129
375222
YDOT = 10427
621102 feet/sec YDOT = 3109
899850 meter/sec
ZDOT = -11251
385339 ZDOT = -3459
153783
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9428673
15 X = 2873859
58
Y = 14051524
61 feet Y = 4282904
70 meter
Z = -14146243
16 Z = -4311774
92
XDOT = -21250
820333 XDOT = -6477
250038
YDOT = 2774
219602 feet/sec YDOT = 845
582135 meter/sec
ZDOT = -11362
767473 ZDOT = -3463
371526
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 07084
46505873
00020000 00000-0 20000-3 0 9062
2 25544 51
6340 176
5645 0014989 348
4340 11
6478 15
77936435 37559
Satellite: ISS
Catalog Number: 25544
Epoch time: 07084
46505873 = yrday
fracday
Element set: 906
Inclination: 51
6340 deg
RA of node: 176
5645 deg
Eccentricity:
0014989
Arg of perigee: 348
4340 deg
Mean anomaly: 11
6478 deg
Mean motion: 15
77936435 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3755
Checksum: 323
Coasting Arc #8 (Orbit 3770)
---------------------------------------
Vector Time (GMT): 2007/085/10:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5999883
79 A = 6719420
49 meter
Y = -2441940
26 meter E =
0014340
Z = 1797719
59 I = 51
70186
XDOT = 3335
873709 Wp = 50
67564
YDOT = 3988
080610 meter/sec RA = 170
51337 deg
ZDOT = -5677
285732 TA = 109
40221
MA = 109
24716
Ha = 187
664 n
mi
Hp = 175
753
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19684658
12 X = 6018011
10
Y = -8011615
02 feet Y = -2374744
84 meter
Z = 5898030
15 Z = 1826910
74
XDOT = 10944
467549 XDOT = 3318
609410
YDOT = 13084
253970 feet/sec YDOT = 4025
287656 meter/sec
ZDOT = -18626
265526 ZDOT = -5661
122196
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21158028
42 X = 6448967
06
Y = -1645090
35 feet Y = -501423
54 meter
Z = 6007496
25 Z = 1831084
86
XDOT = 6417
543084 XDOT = 1956
067132
YDOT = 14285
028574 feet/sec YDOT = 4354
076709 meter/sec
ZDOT = -18564
901418 ZDOT = -5658
581952
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 07085
47833683
00020000 00000-0 20000-3 0 9078
2 25544 51
6339 171
3297 0015020 352
8134 7
2814 15
77977086 37710
Satellite: ISS
Catalog Number: 25544
Epoch time: 07085
47833683 = yrday
fracday
Element set: 907
Inclination: 51
6339 deg
RA of node: 171
3297 deg
Eccentricity:
0015020
Arg of perigee: 352
8134 deg
Mean anomaly: 7
2814 deg
Mean motion: 15
77977086 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3771
Checksum: 310
Coasting Arc #9 (Orbit 3786)
---------------------------------------
Vector Time (GMT): 2007/086/10:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1638809
13 A = 6708663
41 meter
Y = -3850620
52 meter E =
0014025
Z = 5240811
19 I = 51
69514
XDOT = 7316
367803 Wp = 7
06760
YDOT = -2367
908965 meter/sec RA = 165
37282 deg
ZDOT = 561
563034 TA = 77
68554
MA = 77
52856
Ha = 187
751 n
mi
Hp = 175
419
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5376670
39 X = -1621087
69
Y = -12633269
41 feet Y = -3868847
40 meter
Z = 17194262
45 Z = 5232893
10
XDOT = 24003
831376 XDOT = 7339
574403
YDOT = -7768
730199 feet/sec YDOT = -2285
963480 meter/sec
ZDOT = 1842
398405 ZDOT = 597
161860
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1599610
44 X = -487561
26
Y = -13674482
73 feet Y = -4167982
34 meter
Z = 17163930
49 Z = 5231566
01
XDOT = 24216
950649 XDOT = 7381
326558
YDOT = -408
376917 feet/sec YDOT = -124
473284 meter/sec
ZDOT = 1975
992494 ZDOT = 602
282512
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 07086
49158935
00020000 00000-0 20000-3 0 9082
2 25544 51
6347 166
0940 0015164 356
5218 3
5839 15
78060316 37871
Satellite: ISS
Catalog Number: 25544
Epoch time: 07086
49158935 = yrday
fracday
Element set: 908
Inclination: 51
6347 deg
RA of node: 166
0940 deg
Eccentricity:
0015164
Arg of perigee: 356
5218 deg
Mean anomaly: 3
5839 deg
Mean motion: 15
78060316 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3787
Checksum: 315
Coasting Arc #10 (Orbit 3802)
---------------------------------------
Vector Time (GMT): 2007/087/10:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6452088
05 A = 6720414
95 meter
Y = 1608468
89 meter E =
0025877
Z = 850600
89 I = 51
76227
XDOT = -417
034323 Wp = 25
83412
YDOT = -4860
859605 meter/sec RA = 160
21667 deg
ZDOT = 5983
735932 TA = 343
46239
MA = 343
54664
Ha = 187
974 n
mi
Hp = 175
118
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21168267
89 X = -6473726
66
Y = 5277128
90 feet Y = 1536197
08 meter
Z = 2790685
33 Z = 819204
50
XDOT = -1368
222845 XDOT = -391
715961
YDOT = -15947
702117 feet/sec YDOT = -4865
381304 meter/sec
ZDOT = 19631
679567 ZDOT = 5981
771711
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21820422
14 X = -6650864
67
Y = -676003
27 feet Y = -206045
80 meter
Z = 2672784
45 Z = 814664
70
XDOT = 2861
085517 XDOT = 872
058865
YDOT = -14158
370091 feet/sec YDOT = -4315
471204 meter/sec
ZDOT = 19623
601658 ZDOT = 5981
273785
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 07087
50482154
00020000 00000-0 20000-3 0 9099
2 25544 51
6350 160
8595 0015313
9521 359
1671 15
78047609 38039
Satellite: ISS
Catalog Number: 25544
Epoch time: 07087
50482154 = yrday
fracday
Element set: 909
Inclination: 51
6350 deg
RA of node: 160
8595 deg
Eccentricity:
0015313
Arg of perigee:
9521 deg
Mean anomaly: 359
1671 deg
Mean motion: 15
78047609 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3803
Checksum: 290
Coasting Arc #11 (Orbit 3817)
---------------------------------------
Vector Time (GMT): 2007/088/10:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -882463
80 A = 6710326
45 meter
Y = 4596914
34 meter E =
0017228
Z = -4814599
41 I = 51
75534
XDOT = -7193
888856 Wp = 47
82247
YDOT = 1195
844226 meter/sec RA = 155
03182 deg
ZDOT = 2477
289913 TA = 246
26344
MA = 246
44425
Ha = 187
979 n
mi
Hp = 174
731
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2895222
43 X = -910413
45
Y = 15081739
95 feet Y = 4586889
56 meter
Z = -15795929
81 Z = -4818954
53
XDOT = -23601
997560 XDOT = -7218
760351
YDOT = 3923
373444 feet/sec YDOT = 1115
259225 meter/sec
ZDOT = 8127
591577 ZDOT = 2442
282019
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6561174
47 X = -1999845
98
Y = 13867041
13 feet Y = 4226674
14 meter
Z = -15811665
04 Z = -4819395
51
XDOT = -22854
256162 XDOT = -6965
977278
YDOT = -1759
471694 feet/sec YDOT = -536
286972 meter/sec
ZDOT = 7996
035251 ZDOT = 2437
191544
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 07088
45470291
00020000 00000-0 20000-3 0 9105
2 25544 51
6346 155
9523 0015309 4
7234 355
4073 15
78120569 38186
Satellite: ISS
Catalog Number: 25544
Epoch time: 07088
45470291 = yrday
fracday
Element set: 910
Inclination: 51
6346 deg
RA of node: 155
9523 deg
Eccentricity:
0015309
Arg of perigee: 4
7234 deg
Mean anomaly: 355
4073 deg
Mean motion: 15
78120569 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3818
Checksum: 293
Coasting Arc #12 (Orbit 3833)
---------------------------------------
Vector Time (GMT): 2007/089/10:38:00
000
Vector Time (MET): N/A
Weight (LBS) : 478698
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5824824
62 A = 6715680
40 meter
Y = -329233
79 meter E =
0016427
Z = -3347736
23 I = 51
79797
XDOT = -2373
007677 Wp = 25
42022
YDOT = 5627
329056 meter/sec RA = 149
91953 deg
ZDOT = -4676
187895 TA = 193
87686
MA = 193
92206
Ha = 188
097 n
mi
Hp = 174
658
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19110316
99 X = 5844335
76
Y = -1080163
34 feet Y = -263988
51 meter
Z = -10983386
58 Z = -3319392
14
XDOT = -7785
458257 XDOT = -2413
041097
YDOT = 18462
365668 feet/sec YDOT = 5600
568548 meter/sec
ZDOT = -15341
823802 ZDOT = -4687
813517
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18875950
46 X = 5753389
70
Y = 3521361
51 feet Y = 1073310
99 meter
Z = -10876776
02 Z = -3315241
33
XDOT = -11622
432775 XDOT = -3542
517510
YDOT = 14718
168796 feet/sec YDOT = 4486
097849 meter/sec
ZDOT = -15384
770970 ZDOT = -4689
278192
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 07089
46788784
00020000 00000-0 20000-3 0 9117
2 25544 51
6338 150
7166 0015306 8
4627 351
6794 15
78123288 38344
Satellite: ISS
Catalog Number: 25544
Epoch time: 07089
46788784 = yrday
fracday
Element set: 911
Inclination: 51
6338 deg
RA of node: 150
7166 deg
Eccentricity:
0015306
Arg of perigee: 8
4627 deg
Mean anomaly: 351
6794 deg
Mean motion: 15
78123288 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3834
Checksum: 323
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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