Date:
February 12th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 3498 27 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 19 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
044/07:19:00
000 0
0 0
0 0
0
N/A 0
0 0
0 197
2
000/00:00:00
000 0
0 0
0 186
9
Coasting Arc #1 (Orbit 2617)
---------------------------------------
Vector Time (GMT): 2009/042/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 624260
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5353023
32 A = 6738482
15 meter
Y = -3262275
94 meter E =
0013441
Z = -2457141
45 I = 51
39522
XDOT = 910
762370 Wp = 25
88941
YDOT = -5485
787570 meter/sec RA = 229
59672 deg
ZDOT = 5322
012884 TA = 306
27185
MA = 306
39595
Ha = 197
087 n
mi
Hp = 187
254
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17562412
45 X = -5304210
12
Y = -10703005
05 feet Y = -3321863
75 meter
Z = -8061487
71 Z = -2483027
04
XDOT = 2988
065517 XDOT = 946
184959
YDOT = -17997
990715 feet/sec YDOT = -5475
404578 meter/sec
ZDOT = 17460
672190 ZDOT = 5326
523559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6850579
49 X = -2088056
63
Y = -19349968
95 feet Y = -5897870
54 meter
Z = -8162627
92 Z = -2487968
99
XDOT = 12175
476246 XDOT = 3711
085160
YDOT = -11652
201460 feet/sec YDOT = -3551
591005 meter/sec
ZDOT = 17477
792421 ZDOT = 5327
231130
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 09042
50496662
00010596 00000-0 82463-4 0 9003
2 25544 51
6365 230
5200 0008810 11
6717 348
4647 15
70844933 26187
Satellite: ISS
Catalog Number: 25544
Epoch time: 09042
50496662 = yrday
fracday
Element set: 900
Inclination: 51
6365 deg
RA of node: 230
5200 deg
Eccentricity:
0008810
Arg of perigee: 11
6717 deg
Mean anomaly: 348
4647 deg
Mean motion: 15
70844933 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2618
Checksum: 300
Coasting Arc #2 (Orbit 2633)
---------------------------------------
Vector Time (GMT): 2009/043/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 624260
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 714776
86 A = 6733832
16 meter
Y = 5300689
38 meter E =
0014717
Z = -4107053
06 I = 51
39976
XDOT = -6375
158145 Wp = 41
38861
YDOT = -2057
145353 meter/sec RA = 224
51465 deg
ZDOT = -3761
358345 TA = 189
80712
MA = 189
83587
Ha = 197
296 n
mi
Hp = 187
012
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2345068
44 X = 675401
46
Y = 17390713
18 feet Y = 5308462
04 meter
Z = -13474583
54 Z = -4103676
68
XDOT = -20915
873179 XDOT = -6333
409367
YDOT = -6749
164543 feet/sec YDOT = -2128
202855 meter/sec
ZDOT = -12340
414517 ZDOT = -3792
226703
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8821686
51 X = -2688850
05
Y = 15181584
72 feet Y = 4627347
02 meter
Z = -13460980
09 Z = -4102906
73
XDOT = -11134
302282 XDOT = -3393
735336
YDOT = -17527
744771 feet/sec YDOT = -5342
456606 meter/sec
ZDOT = -12460
877615 ZDOT = -3798
075497
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 09043
52283872
00010596 00000-0 82463-4 0 9014
2 25544 51
6366 225
3167 0008937 16
3974 343
7475 15
70869038 26347
Satellite: ISS
Catalog Number: 25544
Epoch time: 09043
52283872 = yrday
fracday
Element set: 901
Inclination: 51
6366 deg
RA of node: 225
3167 deg
Eccentricity:
0008937
Arg of perigee: 16
3974 deg
Mean anomaly: 343
7475 deg
Mean motion: 15
70869038 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2634
Checksum: 331
Coasting Arc #3 (Orbit 2646)
---------------------------------------
Vector Time (GMT): 2009/044/07:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 637863
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4023813
23 A = 6729807
28 meter
Y = -1874800
18 meter E =
0013448
Z = 5054991
51 I = 51
40869
XDOT = 4789
969146 Wp = 30
85882
YDOT = 5797
022491 meter/sec RA = 220
35189 deg
ZDOT = -1649
535165 TA = 75
12557
MA = 74
97666
Ha = 197
227 n
mi
Hp = 186
852
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13201486
97 X = 4019922
68
Y = -6150919
23 feet Y = -1829825
06 meter
Z = 16584617
83 Z = 5074529
51
XDOT = 15715
121869 XDOT = 4732
802888
YDOT = 19019
102662 feet/sec YDOT = 5850
266995 meter/sec
ZDOT = -5411
860776 ZDOT = -1626
405038
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1913188
66 X = 583139
90
Y = 14350148
49 feet Y = 4373925
26 meter
Z = 16660599
08 Z = 5078150
60
XDOT = -21835
071188 XDOT = -6655
329698
YDOT = 9139
549537 feet/sec YDOT = 2785
734699 meter/sec
ZDOT = -5321
231999 ZDOT = -1621
911513
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 09044
34985476
00010596 00000-0 82463-4 0 9025
2 25544 51
6411 221
0924 0009108 17
7854 342
3625 15
70905656 26478
Satellite: ISS
Catalog Number: 25544
Epoch time: 09044
34985476 = yrday
fracday
Element set: 902
Inclination: 51
6411 deg
RA of node: 221
0924 deg
Eccentricity:
0009108
Arg of perigee: 17
7854 deg
Mean anomaly: 342
3625 deg
Mean motion: 15
70905656 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2647
Checksum: 313
Coasting Arc #4 (Orbit 2662)
---------------------------------------
Vector Time (GMT): 2009/045/07:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 637863
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5280602
72 A = 6741005
19 meter
Y = -4148527
02 meter E =
0021467
Z = 428187
71 I = 51
46948
XDOT = 3278
839219 Wp = 38
11545
YDOT = -3538
958795 meter/sec RA = 215
24331 deg
ZDOT = 6005
671997 TA = 326
55041
MA = 326
68582
Ha = 197
436 n
mi
Hp = 186
739
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17324812
08 X = -5235900
77
Y = -13610652
95 feet Y = -4207327
83 meter
Z = 1404815
31 Z = 402643
63
XDOT = 10757
346518 XDOT = 3288
994684
YDOT = -11610
757200 feet/sec YDOT = -3502
235902 meter/sec
ZDOT = 19703
648283 ZDOT = 6021
625176
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17986734
96 X = 5482356
82
Y = -12733697
91 feet Y = -3881231
12 meter
Z = 1304912
30 Z = 397737
27
XDOT = 7166
315374 XDOT = 2184
292926
YDOT = 12199
906251 feet/sec YDOT = 3718
531425 meter/sec
ZDOT = 19765
521431 ZDOT = 6024
530932
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 09045
36771714
00010596 00000-0 82463-4 0 9037
2 25544 51
6412 215
8892 0009145 21
7100 338
4447 15
70882255 26639
Satellite: ISS
Catalog Number: 25544
Epoch time: 09045
36771714 = yrday
fracday
Element set: 903
Inclination: 51
6412 deg
RA of node: 215
8892 deg
Eccentricity:
0009145
Arg of perigee: 21
7100 deg
Mean anomaly: 338
4447 deg
Mean motion: 15
70882255 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2663
Checksum: 306
Coasting Arc #5 (Orbit 2677)
---------------------------------------
Vector Time (GMT): 2009/046/07:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 637863
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1455219
51 A = 6729121
23 meter
Y = 3983641
00 meter E =
0020967
Z = -5241313
13 I = 51
45404
XDOT = -6866
524464 Wp = 62
66091
YDOT = -3380
153338 meter/sec RA = 210
12037 deg
ZDOT = -655
172476 TA = 201
03500
MA = 201
12137
Ha = 197
527 n
mi
Hp = 186
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4774342
22 X = -1474196
05
Y = 13069688
31 feet Y = 3967261
68 meter
Z = -17195909
22 Z = -5248428
67
XDOT = -22527
967402 XDOT = -6825
034025
YDOT = -11089
741922 feet/sec YDOT = -3456
706834 meter/sec
ZDOT = -2149
515997 ZDOT = -688
428790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11334145
08 X = -3454647
42
Y = -8012822
76 feet Y = -2442308
38 meter
Z = -17223304
46 Z = -5249663
20
XDOT = 16144
099096 XDOT = 4920
721405
YDOT = -17883
842547 feet/sec YDOT = -5450
995208 meter/sec
ZDOT = -2279
419626 ZDOT = -694
767102
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 09046
32195726
00010596 00000-0 82463-4 0 9048
2 25544 51
6408 211
0111 0009203 24
8587 335
3016 15
70900096 26782
Satellite: ISS
Catalog Number: 25544
Epoch time: 09046
32195726 = yrday
fracday
Element set: 904
Inclination: 51
6408 deg
RA of node: 211
0111 deg
Eccentricity:
0009203
Arg of perigee: 24
8587 deg
Mean anomaly: 335
3016 deg
Mean motion: 15
70900096 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2678
Checksum: 290
Coasting Arc #6 (Orbit 2693)
---------------------------------------
Vector Time (GMT): 2009/047/07:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 637863
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6358136
25 A = 6740000
43 meter
Y = 1606394
34 meter E =
0017078
Z = 1545550
28 I = 51
51673
XDOT = 122
937666 Wp = 84
94917
YDOT = 5103
986799 meter/sec RA = 204
97752 deg
ZDOT = -5754
656340 TA = 78
01052
MA = 77
81914
Ha = 197
650 n
mi
Hp = 186
376
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20860027
08 X = 6332192
83
Y = 5270322
62 feet Y = 1677349
66 meter
Z = 5070703
01 Z = 1576374
69
XDOT = 403
338800 XDOT = 93
809623
YDOT = 16745
363513 feet/sec YDOT = 5105
198690 meter/sec
ZDOT = -18880
106101 ZDOT = -5754
129873
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10347952
25 X = -3154055
85
Y = 18830894
36 feet Y = 5739656
60 meter
Z = 5190988
48 Z = 1582213
29
XDOT = -14961
020971 XDOT = -4560
119192
YDOT = -2968
032058 feet/sec YDOT = -904
656171 meter/sec
ZDOT = -18877
621726 ZDOT = -5753
899102
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 09047
33980901
00010596 00000-0 82463-4 0 9058
2 25544 51
6409 205
8083 0009202 29
3245 330
8431 15
70875460 26947
Satellite: ISS
Catalog Number: 25544
Epoch time: 09047
33980901 = yrday
fracday
Element set: 905
Inclination: 51
6409 deg
RA of node: 205
8083 deg
Eccentricity:
0009202
Arg of perigee: 29
3245 deg
Mean anomaly: 330
8431 deg
Mean motion: 15
70875460 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2694
Checksum: 305
Coasting Arc #7 (Orbit 2709)
---------------------------------------
Vector Time (GMT): 2009/048/07:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 637863
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1731526
02 A = 6731782
72 meter
Y = -4548177
82 meter E =
0013042
Z = 4638560
71 I = 51
51540
XDOT = 7156
916025 Wp = 71
19988
YDOT = 182
077681 meter/sec RA = 199
89239 deg
ZDOT = 2847
758925 TA = 350
61236
MA = 350
63671
Ha = 197
794 n
mi
Hp = 186
285
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5680859
65 X = -1703071
81
Y = -14921843
24 feet Y = -4567381
71 meter
Z = 15218375
02 Z = 4630218
13
XDOT = 23480
695619 XDOT = 7140
514392
YDOT = 597
367719 feet/sec YDOT = 262
018733 meter/sec
ZDOT = 9343
041094 ZDOT = 2882
486871
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15859953
05 X = 4834113
69
Y = -2096651
46 feet Y = -639059
36 meter
Z = 15185468
45 Z = 4628530
78
XDOT = -6244
268430 XDOT = -1903
253018
YDOT = 21471
922987 feet/sec YDOT = 6544
642127 meter/sec
ZDOT = 9478
435431 ZDOT = 2889
027119
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 09048
35765406
00010596 00000-0 82463-4 0 9063
2 25544 51
6401 200
6044 0009320 32
4435 327
7298 15
70870976 27108
Satellite: ISS
Catalog Number: 25544
Epoch time: 09048
35765406 = yrday
fracday
Element set: 906
Inclination: 51
6401 deg
RA of node: 200
6044 deg
Eccentricity:
0009320
Arg of perigee: 32
4435 deg
Mean anomaly: 327
7298 deg
Mean motion: 15
70870976 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2710
Checksum: 301
Coasting Arc #8 (Orbit 2724)
---------------------------------------
Vector Time (GMT): 2009/049/07:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 637863
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5716849
84 A = 6736053
77 meter
Y = 1239493
34 meter E =
0012646
Z = -3340860
66 I = 51
55762
XDOT = -3761
381852 Wp = 53
60603
YDOT = -4819
747035 meter/sec RA = 194
72572 deg
ZDOT = 4667
857151 TA = 267
10807
MA = 267
25281
Ha = 197
649 n
mi
Hp = 186
093
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18756069
04 X = -5714056
16
Y = 4066579
19 feet Y = 1175579
89 meter
Z = -10960828
92 Z = -3368625
81
XDOT = -12340
491641 XDOT = -3729
882294
YDOT = -15812
818357 feet/sec YDOT = -4861
632963 meter/sec
ZDOT = 15314
491965 ZDOT = 4649
661097
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 115716
60 X = 35270
42
Y = -19129334
08 feet Y = -5830621
03 meter
Z = -11068972
40 Z = -3373822
79
XDOT = 16751
157458 XDOT = 5105
752793
YDOT = -8682
113100 feet/sec YDOT = -2646
308073 meter/sec
ZDOT = 15243
142216 ZDOT = 4646
109747
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 09049
31187700
00010596 00000-0 82463-4 0 9076
2 25544 51
6392 195
7259 0009188 35
0757 325
1008 15
70908051 27250
Satellite: ISS
Catalog Number: 25544
Epoch time: 09049
31187700 = yrday
fracday
Element set: 907
Inclination: 51
6392 deg
RA of node: 195
7259 deg
Eccentricity:
0009188
Arg of perigee: 35
0757 deg
Mean anomaly: 325
1008 deg
Mean motion: 15
70908051 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2725
Checksum: 316
Coasting Arc #9 (Orbit 2740)
---------------------------------------
Vector Time (GMT): 2009/050/07:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 637863
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4638111
45 A = 6736066
75 meter
Y = 3523920
93 meter E =
0012763
Z = -3399348
33 I = 51
58533
XDOT = -5483
659031 Wp = 56
61027
YDOT = 2775
353701 meter/sec RA = 189
65962 deg
ZDOT = -4610
466821 TA = 163
42660
MA = 163
38484
Ha = 197
789 n
mi
Hp = 186
099
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15216901
08 X = 4614874
74
Y = 11561420
38 feet Y = 3575657
13 meter
Z = -11152717
60 Z = -3376873
22
XDOT = -17991
007319 XDOT = -5491
889595
YDOT = 9105
491145 feet/sec YDOT = 2713
986307 meter/sec
ZDOT = -15126
203482 ZDOT = -4637
125818
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14405403
96 X = -4390767
13
Y = 12635605
85 feet Y = 3851332
66 meter
Z = -11064783
38 Z = -3372545
98
XDOT = -4386
428885 XDOT = -1336
983524
YDOT = -18321
297338 feet/sec YDOT = -5584
331429 meter/sec
ZDOT = -15229
915848 ZDOT = -4642
078350
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 09050
32971055
00010596 00000-0 82463-4 0 9084
2 25544 51
6383 190
5226 0009208 38
9106 321
2717 15
70909811 27417
Satellite: ISS
Catalog Number: 25544
Epoch time: 09050
32971055 = yrday
fracday
Element set: 908
Inclination: 51
6383 deg
RA of node: 190
5226 deg
Eccentricity:
0009208
Arg of perigee: 38
9106 deg
Mean anomaly: 321
2717 deg
Mean motion: 15
70909811 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2741
Checksum: 301
Coasting Arc #10 (Orbit 2756)
---------------------------------------
Vector Time (GMT): 2009/051/07:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 637863
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3563131
85 A = 6731641
36 meter
Y = -3376518
34 meter E =
0017086
Z = 4599526
94 I = 51
60064
XDOT = 6520
612920 Wp = 53
00342
YDOT = 2850
853631 meter/sec RA = 184
49629 deg
ZDOT = -2940
930122 TA = 66
25159
MA = 66
07247
Ha = 197
710 n
mi
Hp = 185
882
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11690065
13 X = 3578280
69
Y = -11077816
09 feet Y = -3336588
68 meter
Z = 15090311
47 Z = 4616872
97
XDOT = 21393
087009 XDOT = 6502
535741
YDOT = 9353
194326 feet/sec YDOT = 2923
669875 meter/sec
ZDOT = -9648
720874 ZDOT = -2909
297623
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8742891
06 X = 2664833
19
Y = 13449912
27 feet Y = 4099533
26 meter
Z = 15157666
31 Z = 4620056
69
XDOT = -12174
601180 XDOT = -3710
818440
YDOT = 18713
224742 feet/sec YDOT = 5703
790901 meter/sec
ZDOT = -9525
121199 ZDOT = -2903
256941
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 09051
34753733
00010596 00000-0 82463-4 0 9099
2 25544 51
6387 185
3184 0009171 42
3034 317
8834 15
70938383 27578
Satellite: ISS
Catalog Number: 25544
Epoch time: 09051
34753733 = yrday
fracday
Element set: 909
Inclination: 51
6387 deg
RA of node: 185
3184 deg
Eccentricity:
0009171
Arg of perigee: 42
3034 deg
Mean anomaly: 317
8834 deg
Mean motion: 15
70938383 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2757
Checksum: 327
Coasting Arc #11 (Orbit 2772)
---------------------------------------
Vector Time (GMT): 2009/052/07:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 637863
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6407928
70 A = 6739790
15 meter
Y = -1231198
37 meter E =
0023010
Z = 1638506
00 I = 51
65634
XDOT = 2356
772507 Wp = 57
01818
YDOT = -4565
157552 meter/sec RA = 179
41963 deg
ZDOT = 5740
968789 TA = 321
07268
MA = 321
23814
Ha = 197
869 n
mi
Hp = 185
783
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21023388
12 X = -6401644
34
Y = -4039364
72 feet Y = -1302820
41 meter
Z = 5375675
85 Z = 1607392
38
XDOT = 7732
193265 XDOT = 2379
757851
YDOT = -14977
551022 feet/sec YDOT = -4538
674224 meter/sec
ZDOT = 18835
199440 ZDOT = 5752
473521
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7515987
30 X = 2290872
93
Y = -20077357
35 feet Y = -6119578
52 meter
Z = 5254223
35 Z = 1601487
28
XDOT = 12021
222480 XDOT = 3664
068612
YDOT = 9481
057053 feet/sec YDOT = 2889
826190 meter/sec
ZDOT = 18879
675704 ZDOT = 5754
525155
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 09052
36535927
00010596 00000-0 82463-4 0 9107
2 25544 51
6377 180
1142 0009172 46
7853 313
4073 15
70942338 27732
Satellite: ISS
Catalog Number: 25544
Epoch time: 09052
36535927 = yrday
fracday
Element set: 910
Inclination: 51
6377 deg
RA of node: 180
1142 deg
Eccentricity:
0009172
Arg of perigee: 46
7853 deg
Mean anomaly: 313
4073 deg
Mean motion: 15
70942338 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2773
Checksum: 309
Coasting Arc #12 (Orbit 2787)
---------------------------------------
Vector Time (GMT): 2009/053/07:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 637863
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -443506
49 A = 6729013
19 meter
Y = 4214878
88 meter E =
0022297
Z = -5244955
42 I = 51
64914
XDOT = -7639
747253 Wp = 79
00885
YDOT = 149
628095 meter/sec RA = 174
28607 deg
ZDOT = 773
186460 TA = 198
32640
MA = 198
40687
Ha = 197
932 n
mi
Hp = 185
580
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1455073
78 X = -465126
67
Y = 13828342
78 feet Y = 4209798
34 meter
Z = -17207858
99 Z = -5247162
51
XDOT = -25064
787577 XDOT = -7644
608515
YDOT = 490
905823 feet/sec YDOT = 64
168832 meter/sec
ZDOT = 2536
700983 ZDOT = 736
061805
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13465369
99 X = -4104244
77
Y = -3426423
35 feet Y = -1044373
84 meter
Z = -17216101
44 Z = -5247467
72
XDOT = 3048
515629 XDOT = 929
187564
YDOT = -23884
109026 feet/sec YDOT = -7279
876431 meter/sec
ZDOT = 2391
908626 ZDOT = 729
053749
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 09053
31956235
00010596 00000-0 82463-4 0 9113
2 25544 51
6372 175
2351 0009265 50
8475 309
3509 15
70942439 27889
Satellite: ISS
Catalog Number: 25544
Epoch time: 09053
31956235 = yrday
fracday
Element set: 911
Inclination: 51
6372 deg
RA of node: 175
2351 deg
Eccentricity:
0009265
Arg of perigee: 50
8475 deg
Mean anomaly: 309
3509 deg
Mean motion: 15
70942439 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2788
Checksum: 322
Coasting Arc #13 (Orbit 2803)
---------------------------------------
Vector Time (GMT): 2009/054/07:19:00
000
Vector Time (MET): N/A
Weight (LBS) : 637863
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6564570
65 A = 6740691
71 meter
Y = -1490377
32 meter E =
0017333
Z = 293466
33 I = 51
71905
XDOT = 1325
141626 Wp = 99
93321
YDOT = 4590
943353 meter/sec RA = 169
18047 deg
ZDOT = -6028
896863 TA = 76
88617
MA = 76
69278
Ha = 197
920 n
mi
Hp = 185
434
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21537305
29 X = 6579322
84
Y = -4889689
38 feet Y = -1416885
98 meter
Z = 962816
05 Z = 325392
01
XDOT = 4347
577513 XDOT = 1302
992916
YDOT = 15062
150109 feet/sec YDOT = 4605
637772 meter/sec
ZDOT = -19779
845352 ZDOT = -6022
513492
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1963844
56 X = 598579
82
Y = 21992108
95 feet Y = 6703194
81 meter
Z = 1087223
45 Z = 331385
71
XDOT = -13919
938545 XDOT = -4242
797269
YDOT = 2262
434819 feet/sec YDOT = 689
590133 meter/sec
ZDOT = -19754
542038 ZDOT = -6021
184413
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 09054
33737124
00010596 00000-0 82463-4 0 9121
2 25544 51
6381 170
0316 0009359 53
1053 307
0965 15
70994959 28049
Satellite: ISS
Catalog Number: 25544
Epoch time: 09054
33737124 = yrday
fracday
Element set: 912
Inclination: 51
6381 deg
RA of node: 170
0316 deg
Eccentricity:
0009359
Arg of perigee: 53
1053 deg
Mean anomaly: 307
0965 deg
Mean motion: 15
70994959 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 2804
Checksum: 310
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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