Date:
February 8th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12486 14 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 15 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 775)
---------------------------------------
Vector Time (GMT): 2008/037/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 525189
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6185148
79 A = 6717964
89 meter
Y = -724729
58 meter E =
0017205
Z = 2492973
44 I = 51
51165
XDOT = -1517
158928 Wp = 58
06310
YDOT = 5384
625150 meter/sec RA = 334
75711 deg
ZDOT = 5311
802800 TA = 330
28353
MA = 330
38116
Ha = 185
100 n
mi
Hp = 176
860
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20292482
89 X = 6180683
11
Y = -2377721
73 feet Y = -655588
78 meter
Z = 8179046
72 Z = 2523009
07
XDOT = -4977
555538 XDOT = -1603
060831
YDOT = 17666
093011 feet/sec YDOT = 5367
178947 meter/sec
ZDOT = 17427
174541 ZDOT = 5304
224197
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17560652
41 X = 5352486
85
Y = 10352312
80 feet Y = 3155384
94 meter
Z = 8293873
31 Z = 2527972
58
XDOT = -13972
871332 XDOT = -4258
931182
YDOT = 9717
215872 feet/sec YDOT = 2961
807398 meter/sec
ZDOT = 17398
715174 ZDOT = 5303
128385
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 08037
57911776
00020000 00000-0 20000-3 0 9000
2 25544 51
6398 334
9456 0005806 12
3023 347
8283 15
78024144 7769
Satellite: ISS
Catalog Number: 25544
Epoch time: 08037
57911776 = yrday
fracday
Element set: 900
Inclination: 51
6398 deg
RA of node: 334
9456 deg
Eccentricity:
0005806
Arg of perigee: 12
3023 deg
Mean anomaly: 347
8283 deg
Mean motion: 15
78024144 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 776
Checksum: 301
Coasting Arc #2 (Orbit 790)
---------------------------------------
Vector Time (GMT): 2008/038/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 525189
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2414113
14 A = 6714198
49 meter
Y = -4959586
83 meter E =
0008603
Z = -3831581
49 I = 51
47385
XDOT = 6503
915915 Wp = 62
80527
YDOT = -14
016695 meter/sec RA = 329
53197 deg
ZDOT = 4126
921570 TA = 250
37179
MA = 250
46466
Ha = 185
157 n
mi
Hp = 176
701
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7920318
70 X = 2488005
12
Y = -16271610
34 feet Y = -4932177
68 meter
Z = -12570805
40 Z = -3819674
64
XDOT = 21338
306807 XDOT = 6483
542064
YDOT = -45
986533 feet/sec YDOT = 58
599863 meter/sec
ZDOT = 13539
768930 ZDOT = 4158
467109
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16063657
17 X = 4896202
71
Y = -8401565
67 feet Y = -2560797
21 meter
Z = -12525753
96 Z = -3817849
81
XDOT = 16564
340798 XDOT = 5048
811075
YDOT = 11358
345447 feet/sec YDOT = 3462
023692 meter/sec
ZDOT = 13660
442504 ZDOT = 4163
702875
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 08038
52901019
00020000 00000-0 20000-3 0 9016
2 25544 51
6401 330
0382 0005752 15
7271 344
4072 15
78086989 7912
Satellite: ISS
Catalog Number: 25544
Epoch time: 08038
52901019 = yrday
fracday
Element set: 901
Inclination: 51
6401 deg
RA of node: 330
0382 deg
Eccentricity:
0005752
Arg of perigee: 15
7271 deg
Mean anomaly: 344
4072 deg
Mean motion: 15
78086989 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 791
Checksum: 280
Coasting Arc #3 (Orbit 806)
---------------------------------------
Vector Time (GMT): 2008/039/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 525189
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4943213
84 A = 6711547
13 meter
Y = -847449
33 meter E =
0014369
Z = -4474360
51 I = 51
44173
XDOT = 3863
228644 Wp = 51
34371
YDOT = -5859
608842 meter/sec RA = 324
40191 deg
ZDOT = -3156
195635 TA = 187
01266
MA = 187
03279
Ha = 185
128 n
mi
Hp = 176
312
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16217893
19 X = -4911635
14
Y = -2780345
57 feet Y = -902550
69 meter
Z = -14679660
47 Z = -4498297
23
XDOT = 12674
634658 XDOT = 3943
796357
YDOT = -19224
438457 feet/sec YDOT = -5815
957606 meter/sec
ZDOT = -10354
972557 ZDOT = -3137
232799
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11571994
89 X = -3527144
04
Y = -11581883
82 feet Y = -3530158
19 meter
Z = -14771313
87 Z = -4502296
47
XDOT = 20648
684142 XDOT = 6293
718927
YDOT = -7507
830505 feet/sec YDOT = -2288
386738 meter/sec
ZDOT = -10283
028349 ZDOT = -3134
267041
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 08039
54219511
00020000 00000-0 20000-3 0 9029
2 25544 51
6407 324
8033 0005768 19
9008 340
2381 15
78154075 8070
Satellite: ISS
Catalog Number: 25544
Epoch time: 08039
54219511 = yrday
fracday
Element set: 902
Inclination: 51
6407 deg
RA of node: 324
8033 deg
Eccentricity:
0005768
Arg of perigee: 19
9008 deg
Mean anomaly: 340
2381 deg
Mean motion: 15
78154075 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 807
Checksum: 281
Coasting Arc #4 (Orbit 822)
---------------------------------------
Vector Time (GMT): 2008/040/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 525189
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4114561
55 A = 6719400
54 meter
Y = 5100355
12 meter E =
0014651
Z = 1468626
54 I = 51
44496
XDOT = -4651
576110 Wp = 96
00705
YDOT = -2073
385488 meter/sec RA = 319
18311 deg
ZDOT = -5783
670049 TA = 67
75381
MA = 67
59847
Ha = 185
127 n
mi
Hp = 176
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13499217
70 X = -4178422
86
Y = 16733448
56 feet Y = 5053986
74 meter
Z = 4818328
55 Z = 1448483
18
XDOT = -15261
076478 XDOT = -4599
950136
YDOT = -6802
445827 feet/sec YDOT = -2125
113624 meter/sec
ZDOT = -18975
295436 ZDOT = -5806
141383
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20599618
54 X = -6278763
73
Y = 6214863
43 feet Y = 1894290
37 meter
Z = 4741799
03 Z = 1445300
34
XDOT = -8241
099241 XDOT = -2511
887049
YDOT = -12650
775095 feet/sec YDOT = -3855
956249 meter/sec
ZDOT = -19061
468455 ZDOT = -5809
935585
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 08040
55534551
00020000 00000-0 20000-3 0 9037
2 25544 51
6403 319
5681 0005648 23
4945 336
6477 15
78179791 8238
Satellite: ISS
Catalog Number: 25544
Epoch time: 08040
55534551 = yrday
fracday
Element set: 903
Inclination: 51
6403 deg
RA of node: 319
5681 deg
Eccentricity:
0005648
Arg of perigee: 23
4945 deg
Mean anomaly: 336
6477 deg
Mean motion: 15
78179791 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 823
Checksum: 307
Coasting Arc #5 (Orbit 838)
---------------------------------------
Vector Time (GMT): 2008/041/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 525189
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3079524
01 A = 6707913
11 meter
Y = 2833819
93 meter E =
0006840
Z = 5238208
40 I = 51
38578
XDOT = -5303
898717 Wp = 43
77909
YDOT = 5598
158649 meter/sec RA = 314
01405 deg
ZDOT = 94
394722 TA = 45
35125
MA = 45
29551
Ha = 184
897 n
mi
Hp = 176
123
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10103425
23 X = 3022161
12
Y = 9297309
50 feet Y = 2867936
42 meter
Z = 17185723
09 Z = 5253028
99
XDOT = -17401
242511 XDOT = -5366
562538
YDOT = 18366
662235 feet/sec YDOT = 5538
497065 meter/sec
ZDOT = 309
693970 ZDOT = 68
476415
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3264148
04 X = 994912
32
Y = 13262826
56 feet Y = 4042509
53 meter
Z = 17242708
96 Z = 5255577
69
XDOT = -23659
460593 XDOT = -7211
403589
YDOT = 5568
812834 feet/sec YDOT = 1697
374152 meter/sec
ZDOT = 211
132059 ZDOT = 64
353052
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 08041
56845881
00020000 00000-0 20000-3 0 9041
2 25544 51
6401 314
3326 0005583 25
5479 334
5961 15
78283095 8393
Satellite: ISS
Catalog Number: 25544
Epoch time: 08041
56845881 = yrday
fracday
Element set: 904
Inclination: 51
6401 deg
RA of node: 314
3326 deg
Eccentricity:
0005583
Arg of perigee: 25
5479 deg
Mean anomaly: 334
5961 deg
Mean motion: 15
78283095 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 839
Checksum: 306
Coasting Arc #6 (Orbit 854)
---------------------------------------
Vector Time (GMT): 2008/042/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 525189
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4893567
88 A = 6719225
62 meter
Y = -4394661
16 meter E =
0019165
Z = 1322372
74 I = 51
40474
XDOT = 2400
503474 Wp = 51
02419
YDOT = 4441
405742 meter/sec RA = 308
84038 deg
ZDOT = 5832
437266 TA = 323
58325
MA = 323
71348
Ha = 185
044 n
mi
Hp = 175
956
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16055012
73 X = 4935922
20
Y = -14418179
64 feet Y = -4339701
63 meter
Z = 4338493
23 Z = 1346248
40
XDOT = 7875
667566 XDOT = 2322
328035
YDOT = 14571
541149 feet/sec YDOT = 4467
812645 meter/sec
ZDOT = 19135
292867 ZDOT = 5843
908712
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21253475
67 X = 6478059
38
Y = -3624966
12 feet Y = -1104889
67 meter
Z = 4429362
75 Z = 1350069
77
XDOT = -1482
626390 XDOT = -451
904524
YDOT = 14917
495411 feet/sec YDOT = 4546
852601 meter/sec
ZDOT = 19179
635471 ZDOT = 5845
952892
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 08042
58154085
00020000 00000-0 20000-3 0 9054
2 25544 51
6402 309
0965 0005701 29
7405 330
4084 15
78286083 8550
Satellite: ISS
Catalog Number: 25544
Epoch time: 08042
58154085 = yrday
fracday
Element set: 905
Inclination: 51
6402 deg
RA of node: 309
0965 deg
Eccentricity:
0005701
Arg of perigee: 29
7405 deg
Mean anomaly: 330
4084 deg
Mean motion: 15
78286083 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 855
Checksum: 286
Coasting Arc #7 (Orbit 869)
---------------------------------------
Vector Time (GMT): 2008/043/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 525189
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1124875
16 A = 6710861
56 meter
Y = -4838265
29 meter E =
0012537
Z = -4522455
67 I = 51
35998
XDOT = 5704
909166 Wp = 84
24978
YDOT = -4172
338930 meter/sec RA = 303
61709 deg
ZDOT = 3053
191586 TA = 216
21911
MA = 216
30406
Ha = 184
966 n
mi
Hp = 175
786
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3690535
30 X = -1048720
28
Y = -15873573
78 feet Y = -4850418
55 meter
Z = -14837452
97 Z = -4527735
20
XDOT = 18716
893589 XDOT = 5736
309198
YDOT = -13688
776016 feet/sec YDOT = -4108
367772 meter/sec
ZDOT = 10017
032762 ZDOT = 3080
982089
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5166359
92 X = 1574706
50
Y = -15436464
26 feet Y = -4705034
31 meter
Z = -14858152
73 Z = -4528764
95
XDOT = 21930
171954 XDOT = 6684
316412
YDOT = -2377
203079 feet/sec YDOT = -724
571498 meter/sec
ZDOT = 10122
899344 ZDOT = 3085
459720
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 08043
53127103
00020000 00000-0 20000-3 0 9062
2 25544 51
6404 304
1877 0005589 32
2930 327
8577 15
78353365 8708
Satellite: ISS
Catalog Number: 25544
Epoch time: 08043
53127103 = yrday
fracday
Element set: 906
Inclination: 51
6404 deg
RA of node: 304
1877 deg
Eccentricity:
0005589
Arg of perigee: 32
2930 deg
Mean anomaly: 327
8577 deg
Mean motion: 15
78353365 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 870
Checksum: 292
Coasting Arc #8 (Orbit 885)
---------------------------------------
Vector Time (GMT): 2008/044/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 525189
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4882512
65 A = 6713234
88 meter
Y = 2599268
76 meter E =
0011229
Z = -3817368
53 I = 51
35348
XDOT = -232
064051 Wp = 56
03948
YDOT = -6493
034695 meter/sec RA = 298
47676 deg
ZDOT = -4126
812888 TA = 170
61813
MA = 170
59714
Ha = 184
918 n
mi
Hp = 175
617
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16018742
28 X = -4892671
28
Y = 8527784
63 feet Y = 2544612
96 meter
Z = -12524174
96 Z = -3841112
20
XDOT = -761
364998 XDOT = -139
393565
YDOT = -21302
607268 feet/sec YDOT = -6495
111575 meter/sec
ZDOT = -13539
412363 ZDOT = -4127
715223
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18071300
90 X = -5508132
51
Y = -689125
49 feet Y = -210045
45 meter
Z = -12614728
04 Z = -3844969
11
XDOT = 10112
632528 XDOT = 3082
330395
YDOT = -17416
805745 feet/sec YDOT = -5308
642391 meter/sec
ZDOT = -13543
541493 ZDOT = -4128
071447
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 08044
54428376
00020000 00000-0 20000-3 0 9071
2 25544 51
6404 298
9510 0005481 34
9598 325
1927 15
78400019 8868
Satellite: ISS
Catalog Number: 25544
Epoch time: 08044
54428376 = yrday
fracday
Element set: 907
Inclination: 51
6404 deg
RA of node: 298
9510 deg
Eccentricity:
0005481
Arg of perigee: 34
9598 deg
Mean anomaly: 325
1927 deg
Mean motion: 15
78400019 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 886
Checksum: 311
Coasting Arc #9 (Orbit 901)
---------------------------------------
Vector Time (GMT): 2008/045/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 525189
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -611249
90 A = 6717092
33 meter
Y = 6246250
55 meter E =
0017001
Z = 2379794
62 I = 51
35384
XDOT = -5323
549531 Wp = 88
66726
YDOT = 1534
073325 meter/sec RA = 293
23896 deg
ZDOT = -5360
543115 TA = 64
33466
MA = 64
15916
Ha = 184
951 n
mi
Hp = 175
508
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2005413
07 X = -692611
49
Y = 20492948
01 feet Y = 6238960
21 meter
Z = 7807725
14 Z = 2376627
81
XDOT = -17465
713686 XDOT = -5314
267871
YDOT = 5033
048965 feet/sec YDOT = 1474
594455 meter/sec
ZDOT = -17587
083710 ZDOT = -5386
382019
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11826160
43 X = -3604613
70
Y = 16861298
32 feet Y = 5139323
73 meter
Z = 7796263
21 Z = 2376301
03
XDOT = -16375
303256 XDOT = -4991
192433
YDOT = -3257
234498 feet/sec YDOT = -992
805075 meter/sec
ZDOT = -17685
767067 ZDOT = -5390
621802
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 08045
55726315
00020000 00000-0 20000-3 0 9088
2 25544 51
6402 293
7143 0005553 40
2786 319
8782 15
78446149 9022
Satellite: ISS
Catalog Number: 25544
Epoch time: 08045
55726315 = yrday
fracday
Element set: 908
Inclination: 51
6402 deg
RA of node: 293
7143 deg
Eccentricity:
0005553
Arg of perigee: 40
2786 deg
Mean anomaly: 319
8782 deg
Mean motion: 15
78446149 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 902
Checksum: 302
Coasting Arc #10 (Orbit 917)
---------------------------------------
Vector Time (GMT): 2008/046/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 525189
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4300231
34 A = 6707667
61 meter
Y = 92819
89 meter E =
0007127
Z = 5140849
41 I = 51
31246
XDOT = -1499
522286 Wp = 74
33081
YDOT = 7483
749203 meter/sec RA = 288
07763 deg
ZDOT = 1119
821268 TA = 4
95492
MA = 4
94787
Ha = 184
727 n
mi
Hp = 175
379
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14108370
55 X = 4273900
90
Y = 304527
19 feet Y = 140760
03 meter
Z = 16866303
83 Z = 5161675
64
XDOT = -4919
692540 XDOT = -1588
535077
YDOT = 24552
982949 feet/sec YDOT = 7466
482936 meter/sec
ZDOT = 3673
954291 ZDOT = 1112
320895
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12187598
14 X = 3714779
91
Y = 6921490
22 feet Y = 2109670
22 meter
Z = 16945987
31 Z = 5165136
93
XDOT = -15501
601722 XDOT = -4724
888205
YDOT = 18374
033770 feet/sec YDOT = 5600
405493 meter/sec
ZDOT = 3646
044986 ZDOT = 1111
314512
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 08046
57020654
00020000 00000-0 20000-3 0 9095
2 25544 51
6402 288
4772 0005489 42
5574 317
6016 15
78512566 9189
Satellite: ISS
Catalog Number: 25544
Epoch time: 08046
57020654 = yrday
fracday
Element set: 909
Inclination: 51
6402 deg
RA of node: 288
4772 deg
Eccentricity:
0005489
Arg of perigee: 42
5574 deg
Mean anomaly: 317
6016 deg
Mean motion: 15
78512566 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 918
Checksum: 306
Coasting Arc #11 (Orbit 933)
---------------------------------------
Vector Time (GMT): 2008/047/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 525189
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1897271
23 A = 6719046
95 meter
Y = -6414676
60 meter E =
0018579
Z = 524564
78 I = 51
34311
XDOT = 4498
068307 Wp = 48
76288
YDOT = 1830
592029 meter/sec RA = 282
88027 deg
ZDOT = 5991
817464 TA = 316
98275
MA = 317
12784
Ha = 184
717 n
mi
Hp = 175
239
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6224643
15 X = 1966311
94
Y = -21045526
91 feet Y = -6393074
24 meter
Z = 1721013
05 Z = 533948
86
XDOT = 14757
441952 XDOT = 4448
157518
YDOT = 6005
879359 feet/sec YDOT = 1880
612593 meter/sec
ZDOT = 19658
193781 ZDOT = 6013
547469
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15192311
95 X = 4630616
68
Y = -15834505
21 feet Y = -4826357
19 meter
Z = 1756238
43 Z = 535301
47
XDOT = 9092
139169 XDOT = 2771
284019
YDOT = 10957
495373 feet/sec YDOT = 3339
844590 meter/sec
ZDOT = 19741
525226 ZDOT = 6017
216889
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 08047
58311523
00020000 00000-0 20000-3 0 9107
2 25544 51
6396 283
2398 0005379 44
8674 315
2925 15
78586086 9341
Satellite: ISS
Catalog Number: 25544
Epoch time: 08047
58311523 = yrday
fracday
Element set: 910
Inclination: 51
6396 deg
RA of node: 283
2398 deg
Eccentricity:
0005379
Arg of perigee: 44
8674 deg
Mean anomaly: 315
2925 deg
Mean motion: 15
78586086 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 934
Checksum: 320
Coasting Arc #12 (Orbit 948)
---------------------------------------
Vector Time (GMT): 2008/048/12:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 525189
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3498674
48 A = 6708735
03 meter
Y = -3076633
45 meter E =
0015662
Z = -4840524
95 I = 51
30249
XDOT = 2783
230677 Wp = 89
72865
YDOT = -6793
322276 meter/sec RA = 277
66210 deg
ZDOT = 2312
658021 TA = 202
87901
MA = 202
94886
Ha = 184
671 n
mi
Hp = 175
029
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11478590
81 X = -3440497
32
Y = -10093941
76 feet Y = -3115432
13 meter
Z = -15880987
38 Z = -4857379
87
XDOT = 9131
334243 XDOT = 2847
753637
YDOT = -22287
802744 feet/sec YDOT = -6761
837939 meter/sec
ZDOT = 7587
460700 ZDOT = 2326
335011
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5718347
29 X = -1742952
25
Y = -14102594
58 feet Y = -4298470
83 meter
Z = -15945808
15 Z = -4860282
32
XDOT = 17015
473027 XDOT = 5186
316179
YDOT = -15512
892433 feet/sec YDOT = -4728
329614 meter/sec
ZDOT = 7639
066110 ZDOT = 2328
387350
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 08048
53268740
00020000 00000-0 20000-3 0 9116
2 25544 51
6386 278
3293 0005350 47
4100 312
7517 15
78626933 9492
Satellite: ISS
Catalog Number: 25544
Epoch time: 08048
53268740 = yrday
fracday
Element set: 911
Inclination: 51
6386 deg
RA of node: 278
3293 deg
Eccentricity:
0005350
Arg of perigee: 47
4100 deg
Mean anomaly: 312
7517 deg
Mean motion: 15
78626933 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 949
Checksum: 300
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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