Date:
June 30th 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10225 71 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
There are no maneuvers
Coasting Arc #1 (Orbit 789)
---------------------------------------
Vector Time (GMT): 2009/180/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2638769
29 A = 6721000
10 meter
Y = -3627247
60 meter E =
0012573
Z = 5002738
05 I = 51
32650
XDOT = 4639
948619 Wp = 150
14123
YDOT = 5878
872522 meter/sec RA = 242
82325 deg
ZDOT = 1802
376732 TA = 282
34907
MA = 282
48978
Ha = 191
885 n
mi
Hp = 182
456
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8657379
56 X = 2654831
32
Y = -11900418
64 feet Y = -3597650
15 meter
Z = 16413182
57 Z = 5015595
73
XDOT = 15222
928541 XDOT = 4565
109613
YDOT = 19287
639507 feet/sec YDOT = 5930
340470 meter/sec
ZDOT = 5913
309489 ZDOT = 1824
736509
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12847193
36 X = -3915824
54
Y = -7061779
01 feet Y = -2152430
24 meter
Z = 16463403
25 Z = 5018045
31
XDOT = 16796
964144 XDOT = 5119
714671
YDOT = -16470
054514 feet/sec YDOT = -5020
072616 meter/sec
ZDOT = 6001
303219 ZDOT = 1829
197221
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 09180
55073838
00010596 00000-0 82463-4 0 9007
2 25544 51
6400 243
4299 0007929 167
2284 192
9081 15
74073678 7902
Satellite: ISS
Catalog Number: 25544
Epoch time: 09180
55073838 = yrday
fracday
Element set: 900
Inclination: 51
6400 deg
RA of node: 243
4299 deg
Eccentricity:
0007929
Arg of perigee: 167
2284 deg
Mean anomaly: 192
9081 deg
Mean motion: 15
74073678 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 790
Checksum: 329
Coasting Arc #2 (Orbit 804)
---------------------------------------
Vector Time (GMT): 2009/181/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4484180
82 A = 6731011
94 meter
Y = -4781484
21 meter E =
0006382
Z = -1537120
09 I = 51
37414
XDOT = 2678
809514 Wp = 100
51897
YDOT = -4354
196974 meter/sec RA = 237
63676 deg
ZDOT = 5748
792523 TA = 242
48988
MA = 242
55476
Ha = 191
862 n
mi
Hp = 182
667
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14711879
32 X = -4422913
11
Y = -15687284
15 feet Y = -4831286
17 meter
Z = -5043044
90 Z = -1558756
10
XDOT = 8788
745126 XDOT = 2699
373160
YDOT = -14285
423142 feet/sec YDOT = -4324
126760 meter/sec
ZDOT = 18860
867857 ZDOT = 5761
855558
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13513684
80 X = -4118971
13
Y = 16704640
15 feet Y = 5091574
32 meter
Z = -5128147
78 Z = -1563059
44
XDOT = -14126
981398 XDOT = -4305
903930
YDOT = -5641
573305 feet/sec YDOT = -1719
551543 meter/sec
ZDOT = 18911
855728 ZDOT = 5764
333626
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 09181
50304592
00010596 00000-0 82463-4 0 9018
2 25544 51
6394 238
5388 0007738 170
0392 190
0926 15
74032874 8055
Satellite: ISS
Catalog Number: 25544
Epoch time: 09181
50304592 = yrday
fracday
Element set: 901
Inclination: 51
6394 deg
RA of node: 238
5388 deg
Eccentricity:
0007738
Arg of perigee: 170
0392 deg
Mean anomaly: 190
0926 deg
Mean motion: 15
74032874 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 805
Checksum: 313
Coasting Arc #3 (Orbit 820)
---------------------------------------
Vector Time (GMT): 2009/182/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2047575
38 A = 6720967
15 meter
Y = 3956024
78 meter E =
0014830
Z = -5043630
96 I = 51
35749
XDOT = -5566
403822 Wp = 108
83911
YDOT = -5030
558105 meter/sec RA = 232
50962 deg
ZDOT = -1694
741894 TA = 144
82469
MA = 144
72670
Ha = 191
754 n
mi
Hp = 182
746
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6717767
00 X = -2067159
02
Y = 12979083
91 feet Y = 3933018
86 meter
Z = -16547345
66 Z = -5053625
08
XDOT = -18262
479730 XDOT = -5501
504784
YDOT = -16504
455725 feet/sec YDOT = -5092
441760 meter/sec
ZDOT = -5560
176819 ZDOT = -1721
626695
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13847648
75 X = 4220763
34
Y = 4531684
53 feet Y = 1381257
44 meter
Z = -16586323
29 Z = -5055511
34
XDOT = -13151
823596 XDOT = -4008
675832
YDOT = 19556
124542 feet/sec YDOT = 5960
706761 meter/sec
ZDOT = -5665
883911 ZDOT = -1726
961416
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 09182
51884015
00010596 00000-0 82463-4 0 9024
2 25544 51
6397 233
3212 0007814 173
4584 186
6682 15
74040148 8213
Satellite: ISS
Catalog Number: 25544
Epoch time: 09182
51884015 = yrday
fracday
Element set: 902
Inclination: 51
6397 deg
RA of node: 233
3212 deg
Eccentricity:
0007814
Arg of perigee: 173
4584 deg
Mean anomaly: 186
6682 deg
Mean motion: 15
74040148 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 821
Checksum: 307
Coasting Arc #4 (Orbit 836)
---------------------------------------
Vector Time (GMT): 2009/183/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5224217
32 A = 6731013
29 meter
Y = 3973391
39 meter E =
0019218
Z = 1438491
59 I = 51
41108
XDOT = -1963
936651 Wp = 138
52438
YDOT = 4690
474049 meter/sec RA = 227
32764 deg
ZDOT = -5793
674478 TA = 25
57985
MA = 25
48489
Ha = 191
524 n
mi
Hp = 182
907
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17139820
61 X = 5172409
96
Y = 13036060
98 feet Y = 4031521
72 meter
Z = 4719460
61 Z = 1463745
75
XDOT = -6443
361717 XDOT = -1988
095668
YDOT = 15388
694386 feet/sec YDOT = 4668
378071 meter/sec
ZDOT = -19008
118365 ZDOT = -5803
273191
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9901775
39 X = 3018061
14
Y = -19097653
89 feet Y = -5820964
91 meter
Z = 4818724
39 Z = 1468747
19
XDOT = 14855
040797 XDOT = 4527
816435
YDOT = 2872
310540 feet/sec YDOT = 875
480253 meter/sec
ZDOT = -19045
508483 ZDOT = -5805
070986
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 09183
53463301
00010596 00000-0 82463-4 0 9039
2 25544 51
6398 228
1042 0007629 176
6604 183
4612 15
74081304 8373
Satellite: ISS
Catalog Number: 25544
Epoch time: 09183
53463301 = yrday
fracday
Element set: 903
Inclination: 51
6398 deg
RA of node: 228
1042 deg
Eccentricity:
0007629
Arg of perigee: 176
6604 deg
Mean anomaly: 183
4612 deg
Mean motion: 15
74081304 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 837
Checksum: 302
Coasting Arc #5 (Orbit 852)
---------------------------------------
Vector Time (GMT): 2009/184/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1371135
52 A = 6720813
11 meter
Y = -4207342
65 meter E =
0011407
Z = 5057421
38 I = 51
39676
XDOT = 6362
453249 Wp = 158
82447
YDOT = 4028
910609 meter/sec RA = 222
20268 deg
ZDOT = 1615
144409 TA = 275
54503
MA = 275
67511
Ha = 191
511 n
mi
Hp = 183
066
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4498476
11 X = 1393512
78
Y = -13803617
63 feet Y = -4191885
64 meter
Z = 16592589
83 Z = 5064135
93
XDOT = 20874
190451 XDOT = 6309
082329
YDOT = 13218
210658 feet/sec YDOT = 4099
760566 meter/sec
ZDOT = 5299
030214 ZDOT = 1645
924353
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14386089
77 X = -4384880
16
Y = -1717413
02 feet Y = -523467
49 meter
Z = 16618697
24 Z = 5065378
92
XDOT = 8921
221455 XDOT = 2719
188299
YDOT = -21914
356383 feet/sec YDOT = -6679
495826 meter/sec
ZDOT = 5419
982489 ZDOT = 1652
010663
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 09184
55042666
00010596 00000-0 82463-4 0 9040
2 25544 51
6389 222
8874 0007665 179
8804 180
2362 15
74067604 8536
Satellite: ISS
Catalog Number: 25544
Epoch time: 09184
55042666 = yrday
fracday
Element set: 904
Inclination: 51
6389 deg
RA of node: 222
8874 deg
Eccentricity:
0007665
Arg of perigee: 179
8804 deg
Mean anomaly: 180
2362 deg
Mean motion: 15
74067604 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 853
Checksum: 336
Coasting Arc #6 (Orbit 867)
---------------------------------------
Vector Time (GMT): 2009/185/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5847707
94 A = 6731094
51 meter
Y = -3040628
30 meter E =
0004819
Z = -1372719
26 I = 51
45498
XDOT = 1188
642216 Wp = 99
01698
YDOT = -4901
501582 meter/sec RA = 217
02457 deg
ZDOT = 5810
070127 TA = 245
87153
MA = 245
92193
Ha = 191
395 n
mi
Hp = 183
214
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19185393
50 X = -5806604
10
Y = -9975814
62 feet Y = -3105790
69 meter
Z = -4503672
12 Z = -1401028
12
XDOT = 3899
744804 XDOT = 1215
139103
YDOT = -16081
041937 feet/sec YDOT = -4888
062489 meter/sec
ZDOT = 19061
909867 ZDOT = 5815
907929
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5823285
77 X = -1774937
50
Y = 20800754
28 feet Y = 6340069
90 meter
Z = -4614891
97 Z = -1406619
07
XDOT = -14999
341410 XDOT = -4571
799262
YDOT = 23
192005 feet/sec YDOT = 7
068923 meter/sec
ZDOT = 19084
542044 ZDOT = 5816
968415
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 09185
50273323
00010596 00000-0 82463-4 0 9053
2 25544 51
6393 217
9963 0007617 183
4761 176
6351 15
74074912 8688
Satellite: ISS
Catalog Number: 25544
Epoch time: 09185
50273323 = yrday
fracday
Element set: 905
Inclination: 51
6393 deg
RA of node: 217
9963 deg
Eccentricity:
0007617
Arg of perigee: 183
4761 deg
Mean anomaly: 176
6351 deg
Mean motion: 15
74074912 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 868
Checksum: 331
Coasting Arc #7 (Orbit 883)
---------------------------------------
Vector Time (GMT): 2009/186/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -716787
17 A = 6720750
82 meter
Y = 4336273
21 meter E =
0013380
Z = -5094103
60 I = 51
44429
XDOT = -6957
768941 Wp = 110
97815
YDOT = -2913
969617 meter/sec RA = 211
90085 deg
ZDOT = -1509
343794 TA = 144
53586
MA = 144
44683
Ha = 191
279 n
mi
Hp = 183
448
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2351663
96 X = -740476
77
Y = 14226618
13 feet Y = 4328126
24 meter
Z = -16712938
33 Z = -5097642
40
XDOT = -22827
325921 XDOT = -6917
335249
YDOT = -9560
267773 feet/sec YDOT = -2991
549077 meter/sec
ZDOT = -4951
915334 ZDOT = -1543
046799
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14371399
36 X = 4380402
52
Y = -966230
54 feet Y = -294507
07 meter
Z = -16726582
84 Z = -5098262
45
XDOT = -4320
497027 XDOT = -1316
887494
YDOT = 23305
542005 feet/sec YDOT = 7103
529203 meter/sec
ZDOT = -5084
307526 ZDOT = -1549
696934
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 09186
51852620
00010596 00000-0 82463-4 0 9069
2 25544 51
6394 212
7789 0007587 187
5972 172
5078 15
74048638 8848
Satellite: ISS
Catalog Number: 25544
Epoch time: 09186
51852620 = yrday
fracday
Element set: 906
Inclination: 51
6394 deg
RA of node: 212
7789 deg
Eccentricity:
0007587
Arg of perigee: 187
5972 deg
Mean anomaly: 172
5078 deg
Mean motion: 15
74048638 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 884
Checksum: 357
Coasting Arc #8 (Orbit 899)
---------------------------------------
Vector Time (GMT): 2009/187/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6279244
33 A = 6731257
85 meter
Y = 2024313
19 meter E =
0017969
Z = 1277600
08 I = 51
50445
XDOT = -416
054057 Wp = 143
86991
YDOT = 5000
584561 meter/sec RA = 206
72783 deg
ZDOT = -5851
070004 TA = 22
07153
MA = 21
99425
Ha = 191
110 n
mi
Hp = 183
588
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20601195
29 X = 6249935
14
Y = 6641447
48 feet Y = 2094367
25 meter
Z = 4191601
30 Z = 1308033
55
XDOT = -1365
006749 XDOT = -443
517382
YDOT = 16406
117327 feet/sec YDOT = 4995
779601 meter/sec
ZDOT = -19196
423897 ZDOT = -5853
156895
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1527704
12 X = 465644
22
Y = -21567749
95 feet Y = -6573850
18 meter
Z = 4311133
94 Z = 1314033
63
XDOT = 14656
694694 XDOT = 4467
360543
YDOT = -2817
966639 feet/sec YDOT = -858
916232 meter/sec
ZDOT = -19204
333083 ZDOT = -5853
480724
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 09187
53431908
00010596 00000-0 82463-4 0 9075
2 25544 51
6379 207
5615 0007474 190
5071 169
5938 15
74061086 9002
Satellite: ISS
Catalog Number: 25544
Epoch time: 09187
53431908 = yrday
fracday
Element set: 907
Inclination: 51
6379 deg
RA of node: 207
5615 deg
Eccentricity:
0007474
Arg of perigee: 190
5071 deg
Mean anomaly: 169
5938 deg
Mean motion: 15
74061086 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 900
Checksum: 327
Coasting Arc #9 (Orbit 915)
---------------------------------------
Vector Time (GMT): 2009/188/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 9162
54 A = 6720654
43 meter
Y = -4367624
75 meter E =
0010060
Z = 5108396
40 I = 51
49510
XDOT = 7374
214014 Wp = 169
28225
YDOT = 1698
187563 meter/sec RA = 201
60618 deg
ZDOT = 1428
526636 TA = 266
94791
MA = 267
06304
Ha = 191
033 n
mi
Hp = 183
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 30060
84 X = 33186
07
Y = -14329477
52 feet Y = -4367388
92 meter
Z = 16759830
72 Z = 5108498
45
XDOT = 24193
615533 XDOT = 7347
737098
YDOT = 5571
481507 feet/sec YDOT = 1780
502028 meter/sec
ZDOT = 4686
767180 ZDOT = 1464
286089
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13835103
40 X = -4216939
52
Y = 3730901
61 feet Y = 1137178
81 meter
Z = 16759983
36 Z = 5108442
93
XDOT = -524
092940 XDOT = -159
743528
YDOT = -23778
272149 feet/sec YDOT = -7247
617351 meter/sec
ZDOT = 4827
200483 ZDOT = 1471
330707
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 09188
55011168
00010596 00000-0 82463-4 0 9081
2 25544 51
6373 202
3439 0007399 194
6248 165
4702 15
74057705 9164
Satellite: ISS
Catalog Number: 25544
Epoch time: 09188
55011168 = yrday
fracday
Element set: 908
Inclination: 51
6373 deg
RA of node: 202
3439 deg
Eccentricity:
0007399
Arg of perigee: 194
6248 deg
Mean anomaly: 165
4702 deg
Mean motion: 15
74057705 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 916
Checksum: 325
Coasting Arc #10 (Orbit 930)
---------------------------------------
Vector Time (GMT): 2009/189/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6555985
02 A = 6731187
81 meter
Y = -933861
86 meter E =
0003229
Z = -1208993
11 I = 51
56008
XDOT = -372
181453 Wp = 88
21953
YDOT = -4964
958421 meter/sec RA = 196
43890 deg
ZDOT = 5866
860887 TA = 258
52480
MA = 258
56106
Ha = 190
849 n
mi
Hp = 183
877
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21509137
21 X = -6539182
19
Y = -3063851
26 feet Y = -1007080
56 meter
Z = -3966512
82 Z = -1240800
92
XDOT = -1221
067759 XDOT = -345
134467
YDOT = -16289
233664 feet/sec YDOT = -4968
970160 meter/sec
ZDOT = 19248
231255 ZDOT = 5865
117694
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2905061
93 X = 885462
88
Y = 21507774
44 feet Y = 6555569
65 meter
Z = -4091411
24 Z = -1247062
15
XDOT = -13741
336979 XDOT = -4188
359511
YDOT = 5508
066222 feet/sec YDOT = 1678
858584 meter/sec
ZDOT = 19241
102741 ZDOT = 5864
688115
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 09189
50241697
00010596 00000-0 82463-4 0 9090
2 25544 51
6379 197
4533 0007486 198
0435 162
0463 15
74107007 9317
Satellite: ISS
Catalog Number: 25544
Epoch time: 09189
50241697 = yrday
fracday
Element set: 909
Inclination: 51
6379 deg
RA of node: 197
4533 deg
Eccentricity:
0007486
Arg of perigee: 198
0435 deg
Mean anomaly: 162
0463 deg
Mean motion: 15
74107007 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 931
Checksum: 327
Coasting Arc #11 (Orbit 946)
---------------------------------------
Vector Time (GMT): 2009/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 645880
65 A = 6720574
92 meter
Y = 4291345
21 meter E =
0011740
Z = -5140161
78 I = 51
55171
XDOT = -7565
936842 Wp = 111
30793
YDOT = -441
133469 meter/sec RA = 191
31935 deg
ZDOT = -1325
588565 TA = 146
02106
MA = 145
94582
Ha = 190
709 n
mi
Hp = 184
259
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2119031
01 X = 622815
64
Y = 14079216
57 feet Y = 4298439
66 meter
Z = -16864047
85 Z = -5137079
51
XDOT = -24822
627435 XDOT = -7554
002338
YDOT = -1447
288285 feet/sec YDOT = -525
673267 meter/sec
ZDOT = -4349
043848 ZDOT = -1362
314345
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12837895
97 X = 3912990
69
Y = -6190273
37 feet Y = -1886795
32 meter
Z = -16851696
77 Z = -5136397
18
XDOT = 5327
507983 XDOT = 1623
824433
YDOT = 23221
385268 feet/sec YDOT = 7077
878230 meter/sec
ZDOT = -4493
233634 ZDOT = -1369
537612
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 09190
51820959
00010596 00000-0 82463-4 0 9109
2 25544 51
6371 192
2352 0007326 203
2025 156
8809 15
74049663 9473
Satellite: ISS
Catalog Number: 25544
Epoch time: 09190
51820959 = yrday
fracday
Element set: 910
Inclination: 51
6371 deg
RA of node: 192
2352 deg
Eccentricity:
0007326
Arg of perigee: 203
2025 deg
Mean anomaly: 156
8809 deg
Mean motion: 15
74049663 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 947
Checksum: 312
Coasting Arc #12 (Orbit 962)
---------------------------------------
Vector Time (GMT): 2009/191/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6625010
91 A = 6731400
66 meter
Y = -176484
15 meter E =
0016162
Z = 1118587
38 I = 51
61772
XDOT = 1129
252017 Wp = 148
98222
YDOT = 4824
590546 meter/sec RA = 186
15699 deg
ZDOT = -5902
946117 TA = 18
75983
MA = 18
70034
Ha = 190
455 n
mi
Hp = 184
402
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21735600
10 X = 6621058
20
Y = -579016
23 feet Y = -102421
65 meter
Z = 3669906
09 Z = 1150761
53
XDOT = 3704
895070 XDOT = 1103
893667
YDOT = 15828
709140 feet/sec YDOT = 4837
077509 meter/sec
ZDOT = -19366
621120 ZDOT = -5897
521247
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7181720
71 X = -2188988
47
Y = -20500036
46 feet Y = -6248411
11 meter
Z = 3796205
38 Z = 1157083
40
XDOT = 12411
840482 XDOT = 3783
128979
YDOT = -7944
642469 feet/sec YDOT = -2421
527025 meter/sec
ZDOT = -19345
036373 ZDOT = -5896
367087
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 09191
53400218
00010596 00000-0 82463-4 0 9115
2 25544 51
6368 187
0175 0007153 207
3683 152
7104 15
74069907 9631
Satellite: ISS
Catalog Number: 25544
Epoch time: 09191
53400218 = yrday
fracday
Element set: 911
Inclination: 51
6368 deg
RA of node: 187
0175 deg
Eccentricity:
0007153
Arg of perigee: 207
3683 deg
Mean anomaly: 152
7104 deg
Mean motion: 15
74069907 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 963
Checksum: 306
Coasting Arc #13 (Orbit 978)
---------------------------------------
Vector Time (GMT): 2009/192/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1316982
29 A = 6720514
10 meter
Y = -4108592
28 meter E =
0008522
Z = 5154588
12 I = 51
61013
XDOT = 7550
929131 Wp = 182
72891
YDOT = -848
878672 meter/sec RA = 181
04079 deg
ZDOT = 1244
341422 TA = 255
32494
MA = 255
41942
Ha = 190
401 n
mi
Hp = 184
684
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4320808
03 X = -1295981
13
Y = -13479633
45 feet Y = -4123202
71 meter
Z = 16911378
35 Z = 5148240
85
XDOT = 24773
389538 XDOT = 7553
815537
YDOT = -2785
035013 feet/sec YDOT = -764
423767 meter/sec
ZDOT = 4082
484979 ZDOT = 1281
030229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11341295
78 X = -3456826
95
Y = 8520301
75 feet Y = 2596987
97 meter
Z = 16886209
93 Z = 5146916
79
XDOT = -9977
161906 XDOT = -3041
038949
YDOT = -21710
796469 feet/sec YDOT = -6617
450764 meter/sec
ZDOT = 4226
480180 ZDOT = 1288
231159
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 09192
54979517
00010596 00000-0 82463-4 0 9121
2 25544 51
6365 181
8000 0007174 212
2126 147
8599 15
74048062 9796
Satellite: ISS
Catalog Number: 25544
Epoch time: 09192
54979517 = yrday
fracday
Element set: 912
Inclination: 51
6365 deg
RA of node: 181
8000 deg
Eccentricity:
0007174
Arg of perigee: 212
2126 deg
Mean anomaly: 147
8599 deg
Mean motion: 15
74048062 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 979
Checksum: 327
Coasting Arc #14 (Orbit 993)
---------------------------------------
Vector Time (GMT): 2009/193/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6520140
98 A = 6731414
29 meter
Y = 1299810
61 meter E =
0002475
Z = -1048268
87 I = 51
67729
XDOT = -1857
979149 Wp = 48
23063
YDOT = -4555
895372 meter/sec RA = 175
88469 deg
ZDOT = 5917
898662 TA = 300
31877
MA = 300
34325
Ha = 190
209 n
mi
Hp = 184
739
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21391538
64 X = -6529098
84
Y = 4264470
52 feet Y = 1226848
60 meter
Z = -3439202
34 Z = -1079965
00
XDOT = -6095
732117 XDOT = -1835
644028
YDOT = -14947
163293 feet/sec YDOT = -4576
548102 meter/sec
ZDOT = 19415
678025 ZDOT = 5908
926485
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11235460
29 X = 3424568
30
Y = 18672897
30 feet Y = 5691499
10 meter
Z = -3563577
60 Z = -1086178
45
XDOT = -10607
860361 XDOT = -3233
275838
YDOT = 10074
914669 feet/sec YDOT = 3070
833991 meter/sec
ZDOT = 19380
171906 ZDOT = 5907
076397
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 09193
50210041
00010596 00000-0 82463-4 0 9139
2 25544 51
6366 176
9093 0007169 214
5175 145
5523 15
74085138 9941
Satellite: ISS
Catalog Number: 25544
Epoch time: 09193
50210041 = yrday
fracday
Element set: 913
Inclination: 51
6366 deg
RA of node: 176
9093 deg
Eccentricity:
0007169
Arg of perigee: 214
5175 deg
Mean anomaly: 145
5523 deg
Mean motion: 15
74085138 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 994
Checksum: 310
Coasting Arc #15 (Orbit 1009)
---------------------------------------
Vector Time (GMT): 2009/194/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1913891
24 A = 6720426
02 meter
Y = 3838933
57 meter E =
0010100
Z = -5181036
77 I = 51
66961
XDOT = -7311
698144 Wp = 108
60349
YDOT = 2105
751554 meter/sec RA = 170
77056 deg
ZDOT = -1145
664990 TA = 150
48372
MA = 150
42665
Ha = 190
041 n
mi
Hp = 185
118
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6279170
74 X = 1895989
75
Y = 12594926
40 feet Y = 3860236
23 meter
Z = -16998152
15 Z = -5171782
27
XDOT = -23988
510970 XDOT = -7329
136199
YDOT = 6908
633708 feet/sec YDOT = 2023
890474 meter/sec
ZDOT = -3758
743404 ZDOT = -1181
227135
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9520551
40 X = 2901864
07
Y = -10424073
03 feet Y = -3177257
46 meter
Z = -16961578
20 Z = -5169889
04
XDOT = 14186
559591 XDOT = 4324
063363
YDOT = 19273
371978 feet/sec YDOT = 5874
523779 meter/sec
ZDOT = -3898
259679 ZDOT = -1188
189550
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 09194
51789332
00010596 00000-0 82463-4 0 9146
2 25544 51
6368 171
6912 0007071 220
0570 140
0072 15
74048295 10100
Satellite: ISS
Catalog Number: 25544
Epoch time: 09194
51789332 = yrday
fracday
Element set: 914
Inclination: 51
6368 deg
RA of node: 171
6912 deg
Eccentricity:
0007071
Arg of perigee: 220
0570 deg
Mean anomaly: 140
0072 deg
Mean motion: 15
74048295 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1010
Checksum: 286
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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