Date:
June 11th 2008
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) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 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 2731)
---------------------------------------
Vector Time (GMT): 2008/161/11:51:09
605
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 154611
15 A = 6718030
48 meter
Y = 5515263
99 meter E =
0007819
Z = 3824286
86 I = 51
90834
XDOT = -5865
143157 Wp = 69
85155
YDOT = -2740
058769 meter/sec RA = 55
48437 deg
ZDOT = 4184
532662 TA = 336
51938
MA = 336
55506
Ha = 185
613 n
mi
Hp = 180
900
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 507254
43 X = 74349
51
Y = 18094698
12 feet Y = 5516543
66 meter
Z = 12546872
89 Z = 3824843
74
XDOT = -19242
595660 XDOT = -5854
395076
YDOT = -8989
694123 feet/sec YDOT = -2805
586624 meter/sec
ZDOT = 13728
781701 ZDOT = 4156
065676
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17610201
96 X = 5367589
56
Y = 4182196
09 feet Y = 1274733
37 meter
Z = 12549480
03 Z = 3825081
51
XDOT = -13304
322024 XDOT = -4055
157353
YDOT = 15113
487991 feet/sec YDOT = 4606
591140 meter/sec
ZDOT = 13618
955742 ZDOT = 4151
057710
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 08161
54904568
00020000 00000-0 20000-3 0 9006
2 25544 51
6405 55
7766 0005876 317
9274 42
1439 15
76730938 27324
Satellite: ISS
Catalog Number: 25544
Epoch time: 08161
54904568 = yrday
fracday
Element set: 900
Inclination: 51
6405 deg
RA of node: 55
7766 deg
Eccentricity:
0005876
Arg of perigee: 317
9274 deg
Mean anomaly: 42
1439 deg
Mean motion: 15
76730938 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2732
Checksum: 312
Coasting Arc #2 (Orbit 2746)
---------------------------------------
Vector Time (GMT): 2008/162/11:51:09
605
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5338599
80 A = 6720663
57 meter
Y = 2840905
60 meter E =
0006583
Z = -2923728
53 I = 51
90019
XDOT = -327
209511 Wp = 3
02149
YDOT = 5808
011900 meter/sec RA = 50
29634 deg
ZDOT = 5052
957690 TA = 323
39761
MA = 323
44257
Ha = 185
755 n
mi
Hp = 180
798
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17515091
21 X = 5320638
49
Y = 9320556
44 feet Y = 2900504
82 meter
Z = -9592285
20 Z = -2897836
92
XDOT = -1073
522019 XDOT = -416
677614
YDOT = 19055
157151 feet/sec YDOT = 5803
851992 meter/sec
ZDOT = 16577
945176 ZDOT = 5051
151505
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13230311
32 X = 4032598
89
Y = -14849813
26 feet Y = -4526223
08 meter
Z = -9492367
27 Z = -2893273
54
XDOT = 17148
331781 XDOT = 5226
811527
YDOT = 4699
976626 feet/sec YDOT = 1432
552875 meter/sec
ZDOT = 16571
476311 ZDOT = 5050
985980
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 08162
49972762
00020000 00000-0 20000-3 0 9013
2 25544 51
6410 50
8742 0005996 320
8050 39
2680 15
76764217 27476
Satellite: ISS
Catalog Number: 25544
Epoch time: 08162
49972762 = yrday
fracday
Element set: 901
Inclination: 51
6410 deg
RA of node: 50
8742 deg
Eccentricity:
0005996
Arg of perigee: 320
8050 deg
Mean anomaly: 39
2680 deg
Mean motion: 15
76764217 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2747
Checksum: 301
Coasting Arc #3 (Orbit 2762)
---------------------------------------
Vector Time (GMT): 2008/163/11:51:09
605
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 824238
71 A = 6713995
88 meter
Y = -4577348
80 meter E =
0011743
Z = -4852139
59 I = 51
85855
XDOT = 6316
226509 Wp = 42
97235
YDOT = 3686
269312 meter/sec RA = 45
19952 deg
ZDOT = -2399
532984 TA = 203
64793
MA = 203
70195
Ha = 185
762 n
mi
Hp = 180
604
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2704195
26 X = 898932
97
Y = -15017548
56 feet Y = -4567713
47 meter
Z = -15919093
13 Z = -4847954
55
XDOT = 20722
527917 XDOT = 6286
193155
YDOT = 12094
059423 feet/sec YDOT = 3756
733340 meter/sec
ZDOT = -7872
483543 ZDOT = -2368
921175
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14028620
64 X = -4275923
57
Y = -6044660
12 feet Y = -1842412
40 meter
Z = -15903359
70 Z = -4847344
04
XDOT = 15943
733999 XDOT = 4859
650123
YDOT = -16557
785802 feet/sec YDOT = -5046
813112 meter/sec
ZDOT = -7754
326527 ZDOT = -2363
518725
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 08163
51377638
00020000 00000-0 20000-3 0 9029
2 25544 51
6411 45
6451 0006110 324
4970 35
5788 15
76797000 27638
Satellite: ISS
Catalog Number: 25544
Epoch time: 08163
51377638 = yrday
fracday
Element set: 902
Inclination: 51
6411 deg
RA of node: 45
6451 deg
Eccentricity:
0006110
Arg of perigee: 324
4970 deg
Mean anomaly: 35
5788 deg
Mean motion: 15
76797000 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2763
Checksum: 289
Coasting Arc #4 (Orbit 2778)
---------------------------------------
Vector Time (GMT): 2008/164/11:51:09
605
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5615344
13 A = 6723737
48 meter
Y = -3495671
81 meter E =
0008895
Z = 1191003
54 I = 51
86951
XDOT = 1646
549111 Wp = 105
41839
YDOT = -4667
485047 meter/sec RA = 40
02849 deg
ZDOT = -5902
234641 TA = 61
56208
MA = 61
47248
Ha = 185
900 n
mi
Hp = 180
515
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18423045
06 X = -5581623
35
Y = -11468739
53 feet Y = -3558277
41 meter
Z = 3907491
94 Z = 1163805
48
XDOT = 5402
064014 XDOT = 1727
291463
YDOT = -15313
271151 feet/sec YDOT = -4648
620180 meter/sec
ZDOT = -19364
286881 ZDOT = -5894
040128
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14993410
62 X = -4569991
56
Y = 15714570
19 feet Y = 4789800
99 meter
Z = 3802497
98 Z = 1159001
38
XDOT = -12719
222166 XDOT = -3876
818916
YDOT = -7429
711033 feet/sec YDOT = -2264
575923 meter/sec
ZDOT = -19333
120236 ZDOT = -5892
735048
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 08164
52781450
00020000 00000-0 20000-3 0 9033
2 25544 51
6413 40
4160 0005939 327
9575 32
1228 15
76764480 27792
Satellite: ISS
Catalog Number: 25544
Epoch time: 08164
52781450 = yrday
fracday
Element set: 903
Inclination: 51
6413 deg
RA of node: 40
4160 deg
Eccentricity:
0005939
Arg of perigee: 327
9575 deg
Mean anomaly: 32
1228 deg
Mean motion: 15
76764480 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2779
Checksum: 297
Coasting Arc #5 (Orbit 2794)
---------------------------------------
Vector Time (GMT): 2008/165/11:51:09
605
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2110172
09 A = 6712076
90 meter
Y = 3582518
84 meter E =
0004919
Z = 5269501
17 I = 51
80770
XDOT = -6443
723411 Wp = 353
45329
YDOT = -4216
110952 meter/sec RA = 34
89902 deg
ZDOT = 290
790637 TA = 93
82280
MA = 93
76655
Ha = 186
053 n
mi
Hp = 180
238
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6923136
78 X = -2175674
07
Y = 11753670
72 feet Y = 3558554
69 meter
Z = 17288389
65 Z = 5259091
26
XDOT = -21140
824839 XDOT = -6397
511901
YDOT = -13832
385014 feet/sec YDOT = -4287
910018 meter/sec
ZDOT = 954
037523 ZDOT = 259
598375
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10230395
44 X = 3118224
53
Y = 9098998
62 feet Y = 2773374
78 meter
Z = 17248601
34 Z = 5257373
69
XDOT = -16885
130948 XDOT = -5146
587913
YDOT = 17434
467598 feet/sec YDOT = 5314
025724 meter/sec
ZDOT = 833
613435 ZDOT = 254
085375
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 08165
54183726
00020000 00000-0 20000-3 0 9049
2 25544 51
6415 35
1865 0006155 331
6492 28
4337 15
76825098 27958
Satellite: ISS
Catalog Number: 25544
Epoch time: 08165
54183726 = yrday
fracday
Element set: 904
Inclination: 51
6415 deg
RA of node: 35
1865 deg
Eccentricity:
0006155
Arg of perigee: 331
6492 deg
Mean anomaly: 28
4337 deg
Mean motion: 15
76825098 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2795
Checksum: 309
Coasting Arc #6 (Orbit 2810)
---------------------------------------
Vector Time (GMT): 2008/166/11:51:09
605
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5507689
59 A = 6723844
28 meter
Y = 3776499
24 meter E =
0015951
Z = 692804
11 I = 51
82241
XDOT = -3227
661835 Wp = 29
70135
YDOT = 3596
745620 meter/sec RA = 29
75862 deg
ZDOT = 6008
555250 TA = 337
84150
MA = 337
91037
Ha = 186
054 n
mi
Hp = 180
056
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18069847
74 X = 5461685
28
Y = 12390089
38 feet Y = 3837832
05 meter
Z = 2272979
37 Z = 719449
63
XDOT = -10589
441716 XDOT = -3296
830108
YDOT = 11800
346522 feet/sec YDOT = 3560
264338 meter/sec
ZDOT = 19713
107774 ZDOT = 5992
707672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15285713
97 X = 4659085
62
Y = -15681275
07 feet Y = -4779652
64 meter
Z = 2375859
43 Z = 724161
95
XDOT = 8660
831351 XDOT = 2639
821396
YDOT = 11441
228437 feet/sec YDOT = 3487
286428 meter/sec
ZDOT = 19652
381399 ZDOT = 5990
045850
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 08166
55584830
00020000 00000-0 20000-3 0 9053
2 25544 51
6410 29
9567 0006250 334
6371 25
4486 15
76856945 28114
Satellite: ISS
Catalog Number: 25544
Epoch time: 08166
55584830 = yrday
fracday
Element set: 905
Inclination: 51
6410 deg
RA of node: 29
9567 deg
Eccentricity:
0006250
Arg of perigee: 334
6371 deg
Mean anomaly: 25
4486 deg
Mean motion: 15
76856945 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2811
Checksum: 309
Coasting Arc #7 (Orbit 2825)
---------------------------------------
Vector Time (GMT): 2008/167/11:51:09
605
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3532519
69 A = 6713134
69 meter
Y = -2733752
69 meter E =
0010744
Z = -5019537
97 I = 51
75937
XDOT = 6043
862004 Wp = 75
48529
YDOT = 4386
627550 meter/sec RA = 24
58915 deg
ZDOT = 1870
290870 TA = 212
49931
MA = 212
56551
Ha = 186
208 n
mi
Hp = 179
988
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11589631
54 X = 3587210
66
Y = -8969004
90 feet Y = -2693943
33 meter
Z = -16468300
44 Z = -5002244
46
XDOT = 19828
943583 XDOT = 5985
275219
YDOT = 14391
822670 feet/sec YDOT = 4453
885558 meter/sec
ZDOT = 6136
124901 ZDOT = 1899
510756
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7070409
43 X = -2155060
79
Y = -12921043
96 feet Y = -3938334
20 meter
Z = -16401934
68 Z = -4999309
69
XDOT = 16316
054379 XDOT = 4973
133375
YDOT = -16835
675209 feet/sec YDOT = -5131
513804 meter/sec
ZDOT = 6248
960453 ZDOT = 1904
683146
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 08167
50647375
00020000 00000-0 20000-3 0 9064
2 25544 51
6402 25
0536 0006319 338
0784 22
0110 15
76866848 28266
Satellite: ISS
Catalog Number: 25544
Epoch time: 08167
50647375 = yrday
fracday
Element set: 906
Inclination: 51
6402 deg
RA of node: 25
0536 deg
Eccentricity:
0006319
Arg of perigee: 338
0784 deg
Mean anomaly: 22
0110 deg
Mean motion: 15
76866848 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2826
Checksum: 292
Coasting Arc #8 (Orbit 2841)
---------------------------------------
Vector Time (GMT): 2008/168/11:51:09
605
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4899661
53 A = 6721203
32 meter
Y = -3847238
37 meter E =
0003375
Z = -2529220
41 I = 51
75893
XDOT = 4870
777649 Wp = 34
98392
YDOT = -2714
227498 meter/sec RA = 19
47853 deg
ZDOT = -5307
888274 TA = 173
63332
MA = 173
62903
Ha = 186
282 n
mi
Hp = 179
755
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16075005
01 X = -4843990
35
Y = -12622173
12 feet Y = -3901717
41 meter
Z = -8297967
24 Z = -2552888
72
XDOT = 15980
241632 XDOT = 4926
551541
YDOT = -8904
945861 feet/sec YDOT = -2659
446769 meter/sec
ZDOT = -17414
331607 ZDOT = -5284
090892
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14690435
79 X = -4477644
83
Y = 14155938
63 feet Y = 4314730
10 meter
Z = -8389386
06 Z = -2557084
87
XDOT = -5596
284244 XDOT = -1705
747437
YDOT = -16072
382126 feet/sec YDOT = -4898
862072 meter/sec
ZDOT = -17322
919303 ZDOT = -5280
025804
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 08168
52046198
00020000 00000-0 20000-3 0 9074
2 25544 51
6396 19
8247 0006331 341
0722 19
0206 15
76858200 28421
Satellite: ISS
Catalog Number: 25544
Epoch time: 08168
52046198 = yrday
fracday
Element set: 907
Inclination: 51
6396 deg
RA of node: 19
8247 deg
Eccentricity:
0006331
Arg of perigee: 341
0722 deg
Mean anomaly: 19
0206 deg
Mean motion: 15
76858200 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2842
Checksum: 287
Coasting Arc #9 (Orbit 2857)
---------------------------------------
Vector Time (GMT): 2008/169/11:51:09
605
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4917465
76 A = 6716698
04 meter
Y = 2070366
77 meter E =
0012255
Z = 4078702
29 I = 51
71617
XDOT = -5037
735960 Wp = 44
60430
YDOT = -4398
084910 meter/sec RA = 14
27938 deg
ZDOT = -3825
753566 TA = 84
70829
MA = 84
56846
Ha = 186
375 n
mi
Hp = 179
572
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16133417
86 X = -4960065
16
Y = 6792541
89 feet Y = 2015137
80 meter
Z = 13381569
18 Z = 4054710
06
XDOT = -16528
005118 XDOT = -4969
596546
YDOT = -14429
412434 feet/sec YDOT = -4454
037961 meter/sec
ZDOT = -12551
684927 ZDOT = -3850
062446
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4809599
92 X = 1465966
05
Y = 16904232
00 feet Y = 5152409
91 meter
Z = 13289352
12 Z = 4050594
53
XDOT = -15057
600392 XDOT = -4589
556599
YDOT = 14265
812844 feet/sec YDOT = 4348
219755 meter/sec
ZDOT = -12645
612118 ZDOT = -3854
382573
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 08169
53443623
00020000 00000-0 20000-3 0 9081
2 25544 51
6398 14
5941 0006492 344
4185 15
6779 15
76929429 28580
Satellite: ISS
Catalog Number: 25544
Epoch time: 08169
53443623 = yrday
fracday
Element set: 908
Inclination: 51
6398 deg
RA of node: 14
5941 deg
Eccentricity:
0006492
Arg of perigee: 344
4185 deg
Mean anomaly: 15
6779 deg
Mean motion: 15
76929429 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2858
Checksum: 333
Coasting Arc #10 (Orbit 2873)
---------------------------------------
Vector Time (GMT): 2008/170/11:51:09
605
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3763720
31 A = 6716795
42 meter
Y = 3829416
39 meter E =
0009958
Z = 4024820
99 I = 51
68633
XDOT = -6311
675423 Wp = 66
30797
YDOT = 2101
312619 meter/sec RA = 9
17664 deg
ZDOT = 3899
304285 TA = 343
54797
MA = 343
58027
Ha = 186
439 n
mi
Hp = 179
403
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12348163
75 X = 3701067
57
Y = 12563702
06 feet Y = 3871153
28 meter
Z = 13204793
29 Z = 4042953
83
XDOT = -20707
596532 XDOT = -6353
645675
YDOT = 6894
070273 feet/sec YDOT = 2030
496334 meter/sec
ZDOT = 12792
993060 ZDOT = 3868
540623
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13752767
37 X = 4191843
49
Y = -10923769
94 feet Y = -3329565
08 meter
Z = 13274899
74 Z = 4046189
44
XDOT = 3936
741346 XDOT = 1199
918762
YDOT = 20373
313448 feet/sec YDOT = 6209
785939 meter/sec
ZDOT = 12674
700779 ZDOT = 3863
248797
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 08170
54840146
00020000 00000-0 20000-3 0 9096
2 25544 51
6384 9
3633 0006481 348
7686 11
3333 15
76895650 28741
Satellite: ISS
Catalog Number: 25544
Epoch time: 08170
54840146 = yrday
fracday
Element set: 909
Inclination: 51
6384 deg
RA of node: 9
3633 deg
Eccentricity:
0006481
Arg of perigee: 348
7686 deg
Mean anomaly: 11
3333 deg
Mean motion: 15
76895650 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2874
Checksum: 309
Coasting Arc #11 (Orbit 2888)
---------------------------------------
Vector Time (GMT): 2008/171/11:51:09
605
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5974067
41 A = 6720991
66 meter
Y = -1640829
17 meter E =
0010014
Z = -2593978
38 I = 51
67055
XDOT = 3491
692976 Wp = 17
95967
YDOT = 4414
198014 meter/sec RA = 3
97260 deg
ZDOT = 5264
047140 TA = 312
54637
MA = 312
63087
Ha = 186
584 n
mi
Hp = 179
255
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19599958
70 X = 6004572
46
Y = -5383297
79 feet Y = -1573852
60 meter
Z = -8510427
75 Z = -2564882
69
XDOT = 11455
685617 XDOT = 3416
501491
YDOT = 14482
276950 feet/sec YDOT = 4452
822560 meter/sec
ZDOT = 17270
495866 ZDOT = 5280
828066
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3691358
41 X = -1125126
04
Y = -20035079
98 feet Y = -6106692
38 meter
Z = -8398517
72 Z = -2559868
20
XDOT = 13935
542872 XDOT = 4247
553467
YDOT = -9813
904471 feet/sec YDOT = -2991
278083 meter/sec
ZDOT = 17335
443500 ZDOT = 5283
843179
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 08171
49898043
00020000 00000-0 20000-3 0 9102
2 25544 51
6376 4
4593 0006346 352
1475 7
9589 15
76927728 28890
Satellite: ISS
Catalog Number: 25544
Epoch time: 08171
49898043 = yrday
fracday
Element set: 910
Inclination: 51
6376 deg
RA of node: 4
4593 deg
Eccentricity:
0006346
Arg of perigee: 352
1475 deg
Mean anomaly: 7
9589 deg
Mean motion: 15
76927728 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2889
Checksum: 334
Coasting Arc #12 (Orbit 2904)
---------------------------------------
Vector Time (GMT): 2008/172/11:51:09
605
Vector Time (MET): N/A
Weight (LBS) : 629075
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2225577
94 A = 6712892
94 meter
Y = -3912296
50 meter E =
0015714
Z = -4993740
43 I = 51
61351
XDOT = 7260
783585 Wp = 52
11506
YDOT = -1669
077863 meter/sec RA = 358
85272 deg
ZDOT = -1922
938564 TA = 199
26262
MA = 199
32209
Ha = 186
607 n
mi
Hp = 178
932
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7301764
88 X = -2157406
08
Y = -12835618
44 feet Y = -3936801
97 meter
Z = -16383662
84 Z = -5004387
46
XDOT = 23821
468456 XDOT = 7288
249067
YDOT = -5475
977240 feet/sec YDOT = -1587
729653 meter/sec
ZDOT = -6308
853558 ZDOT = -1887
599534
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13295958
99 X = -4052608
30
Y = 6319141
45 feet Y = 1926074
31 meter
Z = -16424956
77 Z = -5006326
82
XDOT = -3381
023694 XDOT = -1030
536022
YDOT = -23204
520803 feet/sec YDOT = -7072
737941 meter/sec
ZDOT = -6172
900209 ZDOT = -1881
499984
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 08172
51292034
00020000 00000-0 20000-3 0 9115
2 25544 51
6369 359
2290 0006348 356
9855 3
1270 15
76947989 29058
Satellite: ISS
Catalog Number: 25544
Epoch time: 08172
51292034 = yrday
fracday
Element set: 911
Inclination: 51
6369 deg
RA of node: 359
2290 deg
Eccentricity:
0006348
Arg of perigee: 356
9855 deg
Mean anomaly: 3
1270 deg
Mean motion: 15
76947989 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2905
Checksum: 315
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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