Date:
September 26th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 88 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 ET - UTC (sec) : 66 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 3909)
---------------------------------------
Vector Time (GMT): 2010/267/12:02:11
060
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 66552
68 A = 6739352
55 meter
Y = 6632121
36 meter E =
0019880
Z = 1131769
78 I = 51
99556
XDOT = -4821
579568 Wp = 47
00169
YDOT = -972
127901 meter/sec RA = 81
76238 deg
ZDOT = 5928
443644 TA = 325
32433
MA = 325
45378
Ha = 196
136 n
mi
Hp = 186
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 218348
68 X = -13111
88
Y = 21758928
35 feet Y = 6632420
29 meter
Z = 3713155
44 Z = 1131898
88
XDOT = -15818
830605 XDOT = -4839
150368
YDOT = -3189
396001 feet/sec YDOT = -1026
143314 meter/sec
ZDOT = 19450
274421 ZDOT = 5904
977548
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1328023
44 X = -404781
54
Y = -21719367
03 feet Y = -6620063
07 meter
Z = 3713705
98 Z = 1131937
58
XDOT = 14494
455541 XDOT = 4417
910049
YDOT = 2452
381418 feet/sec YDOT = 747
485856 meter/sec
ZDOT = 19356
185353 ZDOT = 5899
765296
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 10267
56293320
00016717 00000-0 10270-3 0 9003
2 25544 51
6404 82
1784 0006744 25
8964 334
2534 15
71290510 39105
Satellite: ISS
Catalog Number: 25544
Epoch time: 10267
56293320 = yrday
fracday
Element set: 900
Inclination: 51
6404 deg
RA of node: 82
1784 deg
Eccentricity:
0006744
Arg of perigee: 25
8964 deg
Mean anomaly: 334
2534 deg
Mean motion: 15
71290510 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3910
Checksum: 292
Coasting Arc #2 (Orbit 3924)
---------------------------------------
Vector Time (GMT): 2010/268/12:02:11
060
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4114701
96 A = 6727762
20 meter
Y = -628876
13 meter E =
0019122
Z = -5301001
84 I = 51
95193
XDOT = 1537
158670 Wp = 74
18291
YDOT = 7521
696799 meter/sec RA = 76
65740 deg
ZDOT = 306
832972 TA = 198
68873
MA = 198
75904
Ha = 196
163 n
mi
Hp = 186
478
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13499678
35 X = 4147180
07
Y = -2063241
89 feet Y = -582681
96 meter
Z = -17391738
33 Z = -5280933
36
XDOT = 5043
171491 XDOT = 1451
444860
YDOT = 24677
482935 feet/sec YDOT = 7538
407007 meter/sec
ZDOT = 1006
669856 ZDOT = 314
091695
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13427217
05 X = -4092615
76
Y = 3000051
35 feet Y = 914415
65 meter
Z = -17311278
95 Z = -5276477
83
XDOT = -6513
793014 XDOT = -1985
404111
YDOT = -23290
706768 feet/sec YDOT = -7099
007423 meter/sec
ZDOT = 1035
796300 ZDOT = 315
710712
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 10268
51690637
00016717 00000-0 10270-3 0 9012
2 25544 51
6409 77
2989 0006758 30
6660 329
4896 15
71329228 39256
Satellite: ISS
Catalog Number: 25544
Epoch time: 10268
51690637 = yrday
fracday
Element set: 901
Inclination: 51
6409 deg
RA of node: 77
2989 deg
Eccentricity:
0006758
Arg of perigee: 30
6660 deg
Mean anomaly: 329
4896 deg
Mean motion: 15
71329228 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3925
Checksum: 342
Coasting Arc #3 (Orbit 3940)
---------------------------------------
Vector Time (GMT): 2010/269/12:02:11
060
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2549290
59 A = 6739443
84 meter
Y = -6208621
00 meter E =
0014116
Z = 581663
60 I = 51
98387
XDOT = 4197
391485 Wp = 99
89860
YDOT = -2299
137527 meter/sec RA = 71
56144 deg
ZDOT = -6023
877957 TA = 73
80955
MA = 73
65425
Ha = 196
112 n
mi
Hp = 186
201
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8363814
26 X = -2482500
84
Y = -20369491
48 feet Y = -6236755
21 meter
Z = 1908345
13 Z = 569441
63
XDOT = 13770
969440 XDOT = 4252
052333
YDOT = -7543
102123 feet/sec YDOT = -2251
894610 meter/sec
ZDOT = -19763
379123 ZDOT = -6003
353722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10102476
16 X = 3079234
73
Y = 19570237
60 feet Y = 5965008
42 meter
Z = 1859335
57 Z = 566725
48
XDOT = -11757
678092 XDOT = -3583
740282
YDOT = 7978
002005 feet/sec YDOT = 2431
695011 meter/sec
ZDOT = -19681
093199 ZDOT = -5998
797207
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 10269
53445641
00016717 00000-0 10270-3 0 9029
2 25544 51
6409 72
0931 0006899 32
0589 328
0991 15
71400377 39412
Satellite: ISS
Catalog Number: 25544
Epoch time: 10269
53445641 = yrday
fracday
Element set: 902
Inclination: 51
6409 deg
RA of node: 72
0931 deg
Eccentricity:
0006899
Arg of perigee: 32
0589 deg
Mean anomaly: 328
0991 deg
Mean motion: 15
71400377 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3941
Checksum: 315
Coasting Arc #4 (Orbit 3956)
---------------------------------------
Vector Time (GMT): 2010/270/12:02:11
060
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2932620
20 A = 6728415
52 meter
Y = 3260689
00 meter E =
0008545
Z = 5095284
89 I = 51
93636
XDOT = -4137
662655 Wp = 72
47727
YDOT = -6286
960450 meter/sec RA = 66
48712 deg
ZDOT = 1642
112383 TA = 1
81553
MA = 1
81243
Ha = 196
306 n
mi
Hp = 186
069
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9621457
34 X = -2993616
29
Y = 10697798
54 feet Y = 3227553
92 meter
Z = 16716813
93 Z = 5080889
61
XDOT = -13575
008709 XDOT = -4075
030409
YDOT = -20626
510663 feet/sec YDOT = -6332
879990 meter/sec
ZDOT = 5387
507819 ZDOT = 1622
163747
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8561365
31 X = 2609504
15
Y = -11646663
32 feet Y = -3549902
98 meter
Z = 16659095
43 Z = 5077692
29
XDOT = 14818
574230 XDOT = 4516
701425
YDOT = 18483
475225 feet/sec YDOT = 5633
763248 meter/sec
ZDOT = 5307
530841 ZDOT = 1617
735400
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 10270
55198938
00016717 00000-0 10270-3 0 9038
2 25544 51
6413 66
8878 0006818 37
2275 322
9358 15
71385740 39571
Satellite: ISS
Catalog Number: 25544
Epoch time: 10270
55198938 = yrday
fracday
Element set: 903
Inclination: 51
6413 deg
RA of node: 66
8878 deg
Eccentricity:
0006818
Arg of perigee: 37
2275 deg
Mean anomaly: 322
9358 deg
Mean motion: 15
71385740 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3957
Checksum: 343
Coasting Arc #5 (Orbit 3971)
---------------------------------------
Vector Time (GMT): 2010/271/12:02:11
060
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4465730
05 A = 6737389
76 meter
Y = 4512986
06 meter E =
0012890
Z = -2244324
41 I = 51
95517
XDOT = -2216
343863 Wp = 42
06918
YDOT = 4911
726880 meter/sec RA = 61
36039 deg
ZDOT = 5494
066161 TA = 292
89402
MA = 293
03004
Ha = 196
257 n
mi
Hp = 185
929
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14651345
31 X = 4425835
81
Y = 14806384
70 feet Y = 4562701
38 meter
Z = -7363269
05 Z = -2222726
61
XDOT = -7271
469366 XDOT = -2297
792603
YDOT = 16114
589500 feet/sec YDOT = 4886
487198 meter/sec
ZDOT = 18025
151448 ZDOT = 5483
100953
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16372638
91 X = -4990380
34
Y = -12926531
81 feet Y = -3940006
90 meter
Z = -7276685
27 Z = -2217933
67
XDOT = 4438
986447 XDOT = 1353
003069
YDOT = -15693
244982 feet/sec YDOT = -4783
301071 meter/sec
ZDOT = 17981
174157 ZDOT = 5480
661883
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 10271
50590593
00016717 00000-0 10270-3 0 9048
2 25544 51
6429 62
0086 0006805 41
7506 318
4174 15
71420025 39729
Satellite: ISS
Catalog Number: 25544
Epoch time: 10271
50590593 = yrday
fracday
Element set: 904
Inclination: 51
6429 deg
RA of node: 62
0086 deg
Eccentricity:
0006805
Arg of perigee: 41
7506 deg
Mean anomaly: 318
4174 deg
Mean motion: 15
71420025 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3972
Checksum: 291
Coasting Arc #6 (Orbit 3987)
---------------------------------------
Vector Time (GMT): 2010/272/12:02:11
060
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 785893
92 A = 6731050
66 meter
Y = -5042967
43 meter E =
0015750
Z = -4404609
81 I = 51
91912
XDOT = 5736
666676 Wp = 58
60601
YDOT = 3839
664502 meter/sec RA = 56
30926 deg
ZDOT = -3373
389155 TA = 177
49493
MA = 177
48703
Ha = 196
209 n
mi
Hp = 185
770
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2578392
13 X = 863624
00
Y = -16545168
74 feet Y = -5033744
60 meter
Z = -14450819
58 Z = -4400602
94
XDOT = 18821
084895 XDOT = 5709
692015
YDOT = 12597
324482 feet/sec YDOT = 3903
664442 meter/sec
ZDOT = -11067
549720 ZDOT = -3345
585665
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -361743
22 X = -110259
33
Y = 16754836
12 feet Y = 5106874
05 meter
Z = -14434732
75 Z = -4399706
54
XDOT = -19218
527526 XDOT = -5857
807190
YDOT = -9851
597364 feet/sec YDOT = -3002
766876 meter/sec
ZDOT = -10956
085735 ZDOT = -3339
414932
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 10272
52339633
00016717 00000-0 10270-3 0 9058
2 25544 51
6433 56
8039 0006883 44
8618 315
3099 15
71459979 39886
Satellite: ISS
Catalog Number: 25544
Epoch time: 10272
52339633 = yrday
fracday
Element set: 905
Inclination: 51
6433 deg
RA of node: 56
8039 deg
Eccentricity:
0006883
Arg of perigee: 44
8618 deg
Mean anomaly: 315
3099 deg
Mean motion: 15
71459979 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3988
Checksum: 348
Coasting Arc #7 (Orbit 4003)
---------------------------------------
Vector Time (GMT): 2010/273/12:02:11
060
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5293754
13 A = 6733895
49 meter
Y = -2087425
61 meter E =
0018025
Z = 3590686
11 I = 51
91054
XDOT = -564
302795 Wp = 73
02661
YDOT = -6259
863152 meter/sec RA = 51
16242 deg
ZDOT = -4447
676621 TA = 64
28330
MA = 64
09732
Ha = 196
310 n
mi
Hp = 185
684
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17367959
75 X = -5287461
79
Y = -6848509
23 feet Y = -2146588
29 meter
Z = 11780466
25 Z = 3564984
13
XDOT = -1851
387123 XDOT = -472
655683
YDOT = -20537
608767 feet/sec YDOT = -6265
661196 meter/sec
ZDOT = -14592
114899 ZDOT = -4450
195281
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18286781
02 X = 5573810
86
Y = 4069272
71 feet Y = 1240314
32 meter
Z = 11677420
48 Z = 3559277
76
XDOT = 5216
214914 XDOT = 1589
902306
YDOT = 18684
645919 feet/sec YDOT = 5695
080076 meter/sec
ZDOT = -14602
180048 ZDOT = -4450
744479
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 10273
54086596
00016717 00000-0 10270-3 0 9069
2 25544 51
6430 51
5978 0006839 48
9104 311
2648 15
71469554 40048
Satellite: ISS
Catalog Number: 25544
Epoch time: 10273
54086596 = yrday
fracday
Element set: 906
Inclination: 51
6430 deg
RA of node: 51
5978 deg
Eccentricity:
0006839
Arg of perigee: 48
9104 deg
Mean anomaly: 311
2648 deg
Mean motion: 15
71469554 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4004
Checksum: 321
Coasting Arc #8 (Orbit 4019)
---------------------------------------
Vector Time (GMT): 2010/274/12:02:11
060
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1810550
70 A = 6734472
67 meter
Y = 5587211
98 meter E =
0018647
Z = 3274680
54 I = 51
89480
XDOT = -5999
551442 Wp = 75
53509
YDOT = -854
966512 meter/sec RA = 46
11552 deg
ZDOT = 4757
994450 TA = 322
69890
MA = 322
82824
Ha = 196
123 n
mi
Hp = 185
464
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5940126
96 X = 1732030
99
Y = 18330747
96 feet Y = 5607019
71 meter
Z = 10743702
55 Z = 3283285
36
XDOT = -19683
567722 XDOT = -6012
658765
YDOT = -2805
008241 feet/sec YDOT = -922
130252 meter/sec
ZDOT = 15610
218013 ZDOT = 4728
816638
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8934859
86 X = -2723345
29
Y = -17050744
07 feet Y = -5197066
79 meter
Z = 10778171
43 Z = 3285186
65
XDOT = 18720
403857 XDOT = 5705
979096
YDOT = 20
744626 feet/sec YDOT = 6
322962 meter/sec
ZDOT = 15493
225932 ZDOT = 4722
335264
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 10274
55831166
00016717 00000-0 10270-3 0 9073
2 25544 51
6443 46
3927 0006788 52
1742 308
0033 15
71550789 40207
Satellite: ISS
Catalog Number: 25544
Epoch time: 10274
55831166 = yrday
fracday
Element set: 907
Inclination: 51
6443 deg
RA of node: 46
3927 deg
Eccentricity:
0006788
Arg of perigee: 52
1742 deg
Mean anomaly: 308
0033 deg
Mean motion: 15
71550789 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4020
Checksum: 304
Coasting Arc #9 (Orbit 4034)
---------------------------------------
Vector Time (GMT): 2010/275/12:02:11
060
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4883204
40 A = 6730074
64 meter
Y = -554963
81 meter E =
0015335
Z = -4610717
32 I = 51
85804
XDOT = 3509
254703 Wp = 88
06048
YDOT = 6151
905040 meter/sec RA = 40
96918 deg
ZDOT = 2985
188851 TA = 211
48721
MA = 211
57909
Ha = 196
223 n
mi
Hp = 185
490
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16021011
81 X = 4911445
28
Y = -1820747
41 feet Y = -500199
19 meter
Z = -15127025
33 Z = -4586926
02
XDOT = 11513
302832 XDOT = 3425
700592
YDOT = 20183
415484 feet/sec YDOT = 6190
680588 meter/sec
ZDOT = 9793
926677 ZDOT = 3002
033640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15478248
52 X = -4717770
15
Y = 4825869
12 feet Y = 1470924
91 meter
Z = -15031621
54 Z = -4581638
24
XDOT = -14702
872276 XDOT = -4481
435470
YDOT = -16533
504413 feet/sec YDOT = -5039
412145 meter/sec
ZDOT = 9861
431114 ZDOT = 3005
764203
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 10275
51214958
00016717 00000-0 10270-3 0 9085
2 25544 51
6444 41
5134 0006892 54
7662 305
4144 15
71550859 40358
Satellite: ISS
Catalog Number: 25544
Epoch time: 10275
51214958 = yrday
fracday
Element set: 908
Inclination: 51
6444 deg
RA of node: 41
5134 deg
Eccentricity:
0006892
Arg of perigee: 54
7662 deg
Mean anomaly: 305
4144 deg
Mean motion: 15
71550859 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4035
Checksum: 307
Coasting Arc #10 (Orbit 4050)
---------------------------------------
Vector Time (GMT): 2010/276/12:02:11
060
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4203749
05 A = 6737381
76 meter
Y = -4904680
04 meter E =
0010457
Z = -1919610
70 I = 51
85989
XDOT = 4847
188871 Wp = 99
02522
YDOT = -1957
937168 meter/sec RA = 35
90633 deg
ZDOT = -5639
835709 TA = 102
20900
MA = 102
09186
Ha = 196
175 n
mi
Hp = 185
212
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13791827
60 X = -4139266
44
Y = -16091469
94 feet Y = -4951328
47 meter
Z = -6297935
36 Z = -1939875
59
XDOT = 15902
850627 XDOT = 4896
119995
YDOT = -6423
678374 feet/sec YDOT = -1903
459782 meter/sec
ZDOT = -18503
397995 ZDOT = -5616
169031
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16766091
34 X = 5110304
64
Y = 12923559
24 feet Y = 3939100
86 meter
Z = -6379161
47 Z = -1944368
42
XDOT = -13409
085601 XDOT = -4087
089291
YDOT = 8353
543770 feet/sec YDOT = 2546
160141 meter/sec
ZDOT = -18408
484343 ZDOT = -5610
906028
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 10276
52955385
00016717 00000-0 10270-3 0 9094
2 25544 51
6447 36
3067 0006968 58
4028 301
7814 15
71595916 40513
Satellite: ISS
Catalog Number: 25544
Epoch time: 10276
52955385 = yrday
fracday
Element set: 909
Inclination: 51
6447 deg
RA of node: 36
3067 deg
Eccentricity:
0006968
Arg of perigee: 58
4028 deg
Mean anomaly: 301
7814 deg
Mean motion: 15
71595916 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4051
Checksum: 331
Coasting Arc #11 (Orbit 4066)
---------------------------------------
Vector Time (GMT): 2010/277/12:02:11
060
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3349034
70 A = 6727477
79 meter
Y = 2724272
69 meter E =
0011433
Z = 5152429
86 I = 51
80233
XDOT = -5920
822008 Wp = 58
15940
YDOT = -4745
251883 meter/sec RA = 30
77419 deg
ZDOT = -1331
439138 TA = 44
59096
MA = 44
49904
Ha = 196
304 n
mi
Hp = 185
101
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10987646
65 X = -3404278
77
Y = 8937902
53 feet Y = 2686513
36 meter
Z = 16904297
44 Z = 5136025
75
XDOT = -19425
269054 XDOT = -5860
851758
YDOT = -15568
411689 feet/sec YDOT = -4811
126883 meter/sec
ZDOT = -4368
238641 ZDOT = -1360
056484
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8824498
91 X = 2689707
27
Y = -11178677
10 feet Y = -3407260
78 meter
Z = 16838502
00 Z = 5132375
41
XDOT = 21558
197749 XDOT = 6570
938674
YDOT = 10225
450163 feet/sec YDOT = 3116
717210 meter/sec
ZDOT = -4482
954960 ZDOT = -1366
404672
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 10277
54693587
00016717 00000-0 10270-3 0 9102
2 25544 51
6456 31
1011 0007053 61
1299 299
0570 15
71628525 40670
Satellite: ISS
Catalog Number: 25544
Epoch time: 10277
54693587 = yrday
fracday
Element set: 910
Inclination: 51
6456 deg
RA of node: 31
1011 deg
Eccentricity:
0007053
Arg of perigee: 61
1299 deg
Mean anomaly: 299
0570 deg
Mean motion: 15
71628525 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4067
Checksum: 306
Coasting Arc #12 (Orbit 4082)
---------------------------------------
Vector Time (GMT): 2010/278/12:02:11
060
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5917135
05 A = 6738805
31 meter
Y = 3183241
10 meter E =
0019946
Z = 386753
81 I = 51
81469
XDOT = -2575
517747 Wp = 54
26414
YDOT = 4029
242858 meter/sec RA = 25
68413 deg
ZDOT = 6036
047759 TA = 309
92850
MA = 310
10361
Ha = 196
220 n
mi
Hp = 184
981
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19413172
72 X = 5879220
88
Y = 10443704
40 feet Y = 3249198
11 meter
Z = 1268877
33 Z = 415407
02
XDOT = -8449
861375 XDOT = -2649
704319
YDOT = 13219
300715 feet/sec YDOT = 4000
027737 meter/sec
ZDOT = 19803
306295 ZDOT = 6023
355157
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21338622
31 X = -6504012
08
Y = -5504610
92 feet Y = -1677805
41 meter
Z = 1383742
33 Z = 421764
66
XDOT = 4758
971572 XDOT = 1450
534535
YDOT = -13328
008669 feet/sec YDOT = -4062
377042 meter/sec
ZDOT = 19752
385548 ZDOT = 6020
527115
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 10278
56429542
00016717 00000-0 10270-3 0 9114
2 25544 51
6462 25
8955 0007106 64
4266 295
7630 15
71649062 40830
Satellite: ISS
Catalog Number: 25544
Epoch time: 10278
56429542 = yrday
fracday
Element set: 911
Inclination: 51
6462 deg
RA of node: 25
8955 deg
Eccentricity:
0007106
Arg of perigee: 64
4266 deg
Mean anomaly: 295
7630 deg
Mean motion: 15
71649062 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4083
Checksum: 318
Coasting Arc #13 (Orbit 4097)
---------------------------------------
Vector Time (GMT): 2010/279/12:02:11
060
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1041194
25 A = 6726744
59 meter
Y = -4057307
41 meter E =
0021705
Z = -5281942
52 I = 51
74696
XDOT = 7286
649105 Wp = 80
43951
YDOT = 2396
562894 meter/sec RA = 20
57648 deg
ZDOT = -402
417110 TA = 185
72276
MA = 185
74760
Ha = 196
135 n
mi
Hp = 184
941
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3415991
62 X = 1112145
49
Y = -13311376
03 feet Y = -4045268
05 meter
Z = -17329207
76 Z = -5276711
53
XDOT = 23906
329086 XDOT = 7261
263627
YDOT = 7862
739154 feet/sec YDOT = 2477
904600 meter/sec
ZDOT = -1320
266108 ZDOT = -367
080043
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 692
26 X = 211
00
Y = 13769141
12 feet Y = 4196834
21 meter
Z = -17308203
96 Z = -5275540
57
XDOT = -24125
043729 XDOT = -7353
313329
YDOT = -1489
108095 feet/sec YDOT = -453
880147 meter/sec
ZDOT = -1178
605736 ZDOT = -359
239028
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 10279
51804861
00016717 00000-0 10270-3 0 9122
2 25544 51
6466 21
0156 0007026 67
2780 292
9124 15
71689478 40986
Satellite: ISS
Catalog Number: 25544
Epoch time: 10279
51804861 = yrday
fracday
Element set: 912
Inclination: 51
6466 deg
RA of node: 21
0156 deg
Eccentricity:
0007026
Arg of perigee: 67
2780 deg
Mean anomaly: 292
9124 deg
Mean motion: 15
71689478 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4098
Checksum: 322
Coasting Arc #14 (Orbit 4113)
---------------------------------------
Vector Time (GMT): 2010/280/12:02:11
060
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6579263
23 A = 6738234
08 meter
Y = -943204
14 meter E =
0018947
Z = 1070857
24 I = 51
75675
XDOT = -271
911595 Wp = 106
21339
YDOT = -4914
890979 meter/sec RA = 15
45359 deg
ZDOT = -5918
638715 TA = 62
10174
MA = 61
90998
Ha = 196
166 n
mi
Hp = 184
843
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21585509
30 X = -6573429
29
Y = -3094501
76 feet Y = -1016744
68 meter
Z = 3513311
15 Z = 1038908
84
XDOT = -892
098408 XDOT = -188
179933
YDOT = -16124
970404 feet/sec YDOT = -4917
464110 meter/sec
ZDOT = -19418
106021 ZDOT = -5919
755784
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21632458
99 X = 6593573
50
Y = -2903516
96 feet Y = -884991
97 meter
Z = 3385234
89 Z = 1031819
59
XDOT = 4925
102358 XDOT = 1501
171199
YDOT = 13727
802423 feet/sec YDOT = 4184
234179 meter/sec
ZDOT = -19422
542386 ZDOT = -5919
990919
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 10280
53536452
00016717 00000-0 10270-3 0 9135
2 25544 51
6463 15
8098 0007106 71
8143 288
3792 15
71713190 41140
Satellite: ISS
Catalog Number: 25544
Epoch time: 10280
53536452 = yrday
fracday
Element set: 913
Inclination: 51
6463 deg
RA of node: 15
8098 deg
Eccentricity:
0007106
Arg of perigee: 71
8143 deg
Mean anomaly: 288
3792 deg
Mean motion: 15
71713190 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4114
Checksum: 299
Coasting Arc #15 (Orbit 4129)
---------------------------------------
Vector Time (GMT): 2010/281/12:02:11
060
Vector Time (MET): N/A
Weight (LBS) : 828874
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1538083
53 A = 6727725
53 meter
Y = 4265156
97 meter E =
0011802
Z = 4960774
16 I = 51
69339
XDOT = -7422
448938 Wp = 96
47436
YDOT = 287
336669 meter/sec RA = 10
36788 deg
ZDOT = 2048
823147 TA = 333
68906
MA = 333
74895
Ha = 196
013 n
mi
Hp = 184
673
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5046205
80 X = 1466176
33
Y = 13993297
16 feet Y = 4281955
10 meter
Z = 16275505
79 Z = 4968071
33
XDOT = -24351
866595 XDOT = -7435
063377
YDOT = 942
705607 feet/sec YDOT = 204
264023 meter/sec
ZDOT = 6721
860720 ZDOT = 2012
733385
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8778882
74 X = -2675803
46
Y = -11968961
88 feet Y = -3648139
58 meter
Z = 16304717
61 Z = 4969677
93
XDOT = 22207
663564 XDOT = 6768
895854
YDOT = -7304
573063 feet/sec YDOT = -2226
433870 meter/sec
ZDOT = 6577
178004 ZDOT = 2004
723856
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 10281
55265536
00016717 00000-0 10270-3 0 9141
2 25544 51
6470 10
6036 0007070 74
5704 285
6239 15
71790126 41304
Satellite: ISS
Catalog Number: 25544
Epoch time: 10281
55265536 = yrday
fracday
Element set: 914
Inclination: 51
6470 deg
RA of node: 10
6036 deg
Eccentricity:
0007070
Arg of perigee: 74
5704 deg
Mean anomaly: 285
6239 deg
Mean motion: 15
71790126 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 4130
Checksum: 289
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics 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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