Date:
June 22nd 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 9687 52 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 600)
---------------------------------------
Vector Time (GMT): 2009/168/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4426313
14 A = 6721677
83 meter
Y = 644554
01 meter E =
0014162
Z = 5009375
92 I = 51
35110
XDOT = -3023
802445 Wp = 124
45424
YDOT = 6863
159771 meter/sec RA = 304
70177 deg
ZDOT = 1777
296789 TA = 308
30905
MA = 308
43631
Ha = 193
301 n
mi
Hp = 181
234
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14522024
74 X = 4394441
76
Y = 2114678
51 feet Y = 693872
78 meter
Z = 16434960
36 Z = 5030801
83
XDOT = -9920
611695 XDOT = -3108
956597
YDOT = 22516
928382 feet/sec YDOT = 6828
869492 meter/sec
ZDOT = 5831
026212 ZDOT = 1762
401054
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3336918
91 X = 1017092
88
Y = -14193614
87 feet Y = -4326213
81 meter
Z = 16518936
37 Z = 5034971
81
XDOT = 20551
597130 XDOT = 6264
126805
YDOT = 11594
005171 feet/sec YDOT = 3533
852776 meter/sec
ZDOT = 5772
963215 ZDOT = 1759
599188
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 09168
55063554
00010596 00000-0 82463-4 0 9007
2 25544 51
6412 305
0379 0008829 124
5735 235
6262 15
73804412 6010
Satellite: ISS
Catalog Number: 25544
Epoch time: 09168
55063554 = yrday
fracday
Element set: 900
Inclination: 51
6412 deg
RA of node: 305
0379 deg
Eccentricity:
0008829
Arg of perigee: 124
5735 deg
Mean anomaly: 235
6262 deg
Mean motion: 15
73804412 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 601
Checksum: 297
Coasting Arc #2 (Orbit 615)
---------------------------------------
Vector Time (GMT): 2009/169/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2042219
81 A = 6731642
23 meter
Y = -6211983
36 meter E =
0012002
Z = -1606096
93 I = 51
36937
XDOT = 5134
311183 Wp = 85
00113
YDOT = 217
558045 meter/sec RA = 299
51847 deg
ZDOT = 5724
791224 TA = 257
22036
MA = 257
35451
Ha = 193
427 n
mi
Hp = 181
299
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6700196
22 X = 2119333
70
Y = -20380522
85 feet Y = -6188714
66 meter
Z = -5269346
88 Z = -1595989
30
XDOT = 16844
852962 XDOT = 5103
686458
YDOT = 713
773115 feet/sec YDOT = 274
800835 meter/sec
ZDOT = 18782
123439 ZDOT = 5749
659679
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19875060
90 X = -6057918
56
Y = -8102669
34 feet Y = -2469693
62 meter
Z = -5230015
40 Z = -1594108
69
XDOT = 1261
029813 XDOT = 384
361887
YDOT = -15198
782842 feet/sec YDOT = -4632
589010 meter/sec
ZDOT = 18879
569659 ZDOT = 5754
492832
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 09169
50310762
00010596 00000-0 82463-4 0 9010
2 25544 51
6420 300
1485 0008893 127
3522 232
8452 15
73796153 6167
Satellite: ISS
Catalog Number: 25544
Epoch time: 09169
50310762 = yrday
fracday
Element set: 901
Inclination: 51
6420 deg
RA of node: 300
1485 deg
Eccentricity:
0008893
Arg of perigee: 127
3522 deg
Mean anomaly: 232
8452 deg
Mean motion: 15
73796153 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 616
Checksum: 297
Coasting Arc #3 (Orbit 631)
---------------------------------------
Vector Time (GMT): 2009/170/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4503000
51 A = 6721744
29 meter
Y = 236710
28 meter E =
0019670
Z = -5000956
08 I = 51
32288
XDOT = 1667
515032 Wp = 97
35698
YDOT = -7271
208574 meter/sec RA = 294
39389 deg
ZDOT = -1854
363784 TA = 154
69199
MA = 154
59551
Ha = 193
266 n
mi
Hp = 181
257
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14773623
71 X = -4481018
69
Y = 776608
54 feet Y = 186478
88 meter
Z = -16407336
21 Z = -5022778
52
XDOT = 5470
849844 XDOT = 1757
707272
YDOT = -23855
671174 feet/sec YDOT = -7252
056833 meter/sec
ZDOT = -6083
870683 ZDOT = -1846
045068
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 27993
47 X = 8532
41
Y = 14698622
60 feet Y = 4480140
17 meter
Z = -16492830
86 Z = -5027014
85
XDOT = -22472
662431 XDOT = -6849
667509
YDOT = -6715
560366 feet/sec YDOT = -2046
902800 meter/sec
ZDOT = -6051
592521 ZDOT = -1844
525401
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 09170
51906250
00010596 00000-0 82463-4 0 9027
2 25544 51
6422 294
9328 0008758 131
1132 229
0789 15
73817693 6327
Satellite: ISS
Catalog Number: 25544
Epoch time: 09170
51906250 = yrday
fracday
Element set: 902
Inclination: 51
6422 deg
RA of node: 294
9328 deg
Eccentricity:
0008758
Arg of perigee: 131
1132 deg
Mean anomaly: 229
0789 deg
Mean motion: 15
73817693 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 632
Checksum: 314
Coasting Arc #4 (Orbit 647)
---------------------------------------
Vector Time (GMT): 2009/171/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -857289
84 A = 6731499
18 meter
Y = 6458618
02 meter E =
0022645
Z = 1644248
28 I = 51
34487
XDOT = -5114
137804 Wp = 123
32353
YDOT = 787
144329 meter/sec RA = 289
20681 deg
ZDOT = -5714
103774 TA = 38
41561
MA = 38
25458
Ha = 193
220 n
mi
Hp = 181
465
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2812630
70 X = -937435
04
Y = 21189691
66 feet Y = 6448582
85 meter
Z = 5394515
35 Z = 1639890
15
XDOT = -16778
667335 XDOT = -5094
801280
YDOT = 2582
494519 feet/sec YDOT = 730
064329 meter/sec
ZDOT = -18747
059626 ZDOT = -5738
901429
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21081815
47 X = 6425737
35
Y = 3556953
69 feet Y = 1084159
48 meter
Z = 5377718
56 Z = 1639128
62
XDOT = 2277
849259 XDOT = 694
288454
YDOT = 15209
848920 feet/sec YDOT = 4635
961951 meter/sec
ZDOT = -18844
193534 ZDOT = -5743
710189
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 09171
53500344
00010596 00000-0 82463-4 0 9035
2 25544 51
6424 289
7165 0008823 134
9555 225
2325 15
73830111 6484
Satellite: ISS
Catalog Number: 25544
Epoch time: 09171
53500344 = yrday
fracday
Element set: 903
Inclination: 51
6424 deg
RA of node: 289
7165 deg
Eccentricity:
0008823
Arg of perigee: 134
9555 deg
Mean anomaly: 225
2325 deg
Mean motion: 15
73830111 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 648
Checksum: 299
Coasting Arc #5 (Orbit 663)
---------------------------------------
Vector Time (GMT): 2009/172/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4382550
58 A = 6721615
54 meter
Y = -1133209
58 meter E =
0014318
Z = 4962609
70 I = 51
30461
XDOT = -274
668457 Wp = 132
76879
YDOT = 7454
881811 meter/sec RA = 284
08152 deg
ZDOT = 1931
757236 TA = 298
42423
MA = 298
56845
Ha = 192
918 n
mi
Hp = 181
497
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14378446
79 X = 4370788
98
Y = -3717879
19 feet Y = -1084268
22 meter
Z = 16281527
89 Z = 4983871
46
XDOT = -901
143230 XDOT = -367
393986
YDOT = 24458
273659 feet/sec YDOT = 7451
291415 meter/sec
ZDOT = 6337
786206 ZDOT = 1930
199343
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3480957
07 X = -1060995
71
Y = -14343180
00 feet Y = -4371801
26 meter
Z = 16364798
61 Z = 4987990
62
XDOT = 23393
620325 XDOT = 7130
375475
YDOT = 1595
944233 feet/sec YDOT = 486
443802 meter/sec
ZDOT = 6332
005792 ZDOT = 1929
995365
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 09172
55092786
00010596 00000-0 82463-4 0 9045
2 25544 51
6433 284
5009 0008665 138
6271 221
5550 15
73900421 6643
Satellite: ISS
Catalog Number: 25544
Epoch time: 09172
55092786 = yrday
fracday
Element set: 904
Inclination: 51
6433 deg
RA of node: 284
5009 deg
Eccentricity:
0008665
Arg of perigee: 138
6271 deg
Mean anomaly: 221
5550 deg
Mean motion: 15
73900421 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 664
Checksum: 308
Coasting Arc #6 (Orbit 678)
---------------------------------------
Vector Time (GMT): 2009/173/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -367997
40 A = 6731277
91 meter
Y = -6502569
62 meter E =
0010075
Z = -1710391
41 I = 51
33090
XDOT = 4877
473584 Wp = 93
04323
YDOT = -1762
884559 meter/sec RA = 278
89268 deg
ZDOT = 5681
025312 TA = 247
97172
MA = 248
07878
Ha = 192
989 n
mi
Hp = 181
674
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1207340
57 X = -286948
45
Y = -21333889
84 feet Y = -6506231
21 meter
Z = -5611520
36 Z = -1711983
81
XDOT = 16002
209920 XDOT = 4869
226569
YDOT = -5783
741990 feet/sec YDOT = -1708
389256 meter/sec
ZDOT = 18638
534487 ZDOT = 5704
699632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21333199
13 X = -6502359
10
Y = 1189047
40 feet Y = 362421
65 meter
Z = -5618048
47 Z = -1712381
17
XDOT = -5707
354698 XDOT = -1739
601712
YDOT = -14334
192971 feet/sec YDOT = -4369
062018 meter/sec
ZDOT = 18731
240648 ZDOT = 5709
282150
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 09173
50334673
00010596 00000-0 82463-4 0 9056
2 25544 51
6434 279
6116 0008515 140
9938 219
1841 15
73864554 6796
Satellite: ISS
Catalog Number: 25544
Epoch time: 09173
50334673 = yrday
fracday
Element set: 905
Inclination: 51
6434 deg
RA of node: 279
6116 deg
Eccentricity:
0008515
Arg of perigee: 140
9938 deg
Mean anomaly: 219
1841 deg
Mean motion: 15
73864554 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 679
Checksum: 332
Coasting Arc #7 (Orbit 694)
---------------------------------------
Vector Time (GMT): 2009/174/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4117977
99 A = 6721663
88 meter
Y = 1909248
24 meter E =
0017866
Z = -4971550
32 I = 51
29522
XDOT = -1076
775622 Wp = 102
06953
YDOT = -7360
657603 meter/sec RA = 273
76702 deg
ZDOT = -1944
420190 TA = 149
07479
MA = 148
96945
Ha = 192
832 n
mi
Hp = 181
664
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13510426
49 X = -4114870
77
Y = 6263937
80 feet Y = 1863217
12 meter
Z = -16310860
62 Z = -4991547
33
XDOT = -3532
728419 XDOT = -984
941903
YDOT = -24149
139116 feet/sec YDOT = -7372
184822 meter/sec
ZDOT = -6379
331331 ZDOT = -1949
429750
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6502401
66 X = 1981932
03
Y = 13301394
39 feet Y = 4054265
01 meter
Z = -16389154
80 Z = -4995414
38
XDOT = -23112
971332 XDOT = -7044
833662
YDOT = 3452
498323 feet/sec YDOT = 1052
321489 meter/sec
ZDOT = -6399
300592 ZDOT = -1950
506820
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 09174
51924521
00010596 00000-0 82463-4 0 9066
2 25544 51
6433 274
3959 0008516 145
6421 214
5295 15
73891373 6951
Satellite: ISS
Catalog Number: 25544
Epoch time: 09174
51924521 = yrday
fracday
Element set: 906
Inclination: 51
6433 deg
RA of node: 274
3959 deg
Eccentricity:
0008516
Arg of perigee: 145
6421 deg
Mean anomaly: 214
5295 deg
Mean motion: 15
73891373 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 695
Checksum: 327
Coasting Arc #8 (Orbit 710)
---------------------------------------
Vector Time (GMT): 2009/175/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1516345
25 A = 6731168
21 meter
Y = 6321492
69 meter E =
0021849
Z = 1697817
51 I = 51
32589
XDOT = -4492
730104 Wp = 127
82026
YDOT = 2616
358900 meter/sec RA = 268
57751 deg
ZDOT = -5692
456026 TA = 33
29467
MA = 33
15742
Ha = 192
774 n
mi
Hp = 181
823
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4974885
98 X = 1437296
96
Y = 20739805
41 feet Y = 6338007
02 meter
Z = 5570267
44 Z = 1704993
12
XDOT = -14739
928162 XDOT = -4494
000204
YDOT = 8583
854659 feet/sec YDOT = 2566
112639 meter/sec
ZDOT = -18676
036830 ZDOT = -5714
283978
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20553827
96 X = 6264806
76
Y = -5666717
88 feet Y = -1727215
61 meter
Z = 5598692
96 Z = 1706481
62
XDOT = 8678
100980 XDOT = 2645
085179
YDOT = 12822
402035 feet/sec YDOT = 3908
268140 meter/sec
ZDOT = -18761
480016 ZDOT = -5718
499109
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 09175
53513038
00010596 00000-0 82463-4 0 9077
2 25544 51
6425 269
1805 0008601 148
4119 211
7562 15
73911740 7110
Satellite: ISS
Catalog Number: 25544
Epoch time: 09175
53513038 = yrday
fracday
Element set: 907
Inclination: 51
6425 deg
RA of node: 269
1805 deg
Eccentricity:
0008601
Arg of perigee: 148
4119 deg
Mean anomaly: 211
7562 deg
Mean motion: 15
73911740 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 711
Checksum: 297
Coasting Arc #9 (Orbit 726)
---------------------------------------
Vector Time (GMT): 2009/176/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3693010
78 A = 6721456
91 meter
Y = -2636765
01 meter E =
0013881
Z = 4954204
80 I = 51
29590
XDOT = 2390
967564 Wp = 140
92988
YDOT = 7056
973031 meter/sec RA = 263
45087 deg
ZDOT = 1959
994227 TA = 289
96996
MA = 290
11941
Ha = 192
497 n
mi
Hp = 181
908
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12116177
10 X = 3698154
79
Y = -8650803
84 feet Y = -2595439
72 meter
Z = 16253952
75 Z = 4972157
21
XDOT = 7844
381771 XDOT = 2302
356438
YDOT = 23152
798657 feet/sec YDOT = 7083
214432 meter/sec
ZDOT = 6430
427254 ZDOT = 1971
395385
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9266865
26 X = -2824540
53
Y = -11553125
62 feet Y = -3521392
69 meter
Z = 16324203
85 Z = 4975617
33
XDOT = 21870
878176 XDOT = 6666
243668
YDOT = -8330
305948 feet/sec YDOT = -2539
077253 meter/sec
ZDOT = 6475
468631 ZDOT = 1973
722839
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 09176
55099923
00010596 00000-0 82463-4 0 9083
2 25544 51
6426 263
9640 0008430 152
5755 207
5854 15
73976865 7275
Satellite: ISS
Catalog Number: 25544
Epoch time: 09176
55099923 = yrday
fracday
Element set: 908
Inclination: 51
6426 deg
RA of node: 263
9640 deg
Eccentricity:
0008430
Arg of perigee: 152
5755 deg
Mean anomaly: 207
5854 deg
Mean motion: 15
73976865 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 727
Checksum: 348
Coasting Arc #10 (Orbit 741)
---------------------------------------
Vector Time (GMT): 2009/177/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2633084
36 A = 6731057
05 meter
Y = -5957912
03 meter E =
0008196
Z = -1706775
22 I = 51
33191
XDOT = 3944
904682 Wp = 99
91368
YDOT = -3364
958004 meter/sec RA = 258
26075 deg
ZDOT = 5682
090506 TA = 241
14293
MA = 241
22521
Ha = 192
490 n
mi
Hp = 182
140
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8638728
22 X = -2557975
19
Y = -19546955
48 feet Y = -5986936
51 meter
Z = -5599656
22 Z = -1719385
01
XDOT = 12942
600663 XDOT = 3954
636835
YDOT = -11039
888466 feet/sec YDOT = -3320
790201 meter/sec
ZDOT = 18642
029219 ZDOT = 5701
277733
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18902429
30 X = -5761460
45
Y = 9942320
22 feet Y = 3030419
20 meter
Z = -5649396
34 Z = -1721936
00
XDOT = -11178
908960 XDOT = -3407
331451
YDOT = -10658
343621 feet/sec YDOT = -3248
663136 meter/sec
ZDOT = 18717
084249 ZDOT = 5704
967279
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 09177
50336640
00010596 00000-0 82463-4 0 9090
2 25544 51
6419 259
0742 0008178 155
5107 204
6446 15
73937285 7424
Satellite: ISS
Catalog Number: 25544
Epoch time: 09177
50336640 = yrday
fracday
Element set: 909
Inclination: 51
6419 deg
RA of node: 259
0742 deg
Eccentricity:
0008178
Arg of perigee: 155
5107 deg
Mean anomaly: 204
6446 deg
Mean motion: 15
73937285 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 742
Checksum: 324
Coasting Arc #11 (Orbit 757)
---------------------------------------
Vector Time (GMT): 2009/178/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3196811
63 A = 6721421
17 meter
Y = 3205226
09 meter E =
0016206
Z = -4980448
32 I = 51
30592
XDOT = -3581
748328 Wp = 106
12684
YDOT = -6531
014927 meter/sec RA = 253
13408 deg
ZDOT = -1913
679196 TA = 145
33475
MA = 145
22901
Ha = 192
339 n
mi
Hp = 182
152
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10488227
15 X = -3208221
56
Y = 10515833
63 feet Y = 3169414
32 meter
Z = -16340053
55 Z = -4996005
58
XDOT = -11751
142807 XDOT = -3499
154996
YDOT = -21427
214328 feet/sec YDOT = -6570
606081 meter/sec
ZDOT = -6278
475053 ZDOT = -1930
879378
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11375834
48 X = 3467354
35
Y = 9443751
46 feet Y = 2878455
44 meter
Z = -16400883
03 Z = -4998989
15
XDOT = -19644
067351 XDOT = -5987
511729
YDOT = 12695
985360 feet/sec YDOT = 3869
736338 meter/sec
ZDOT = -6346
254699 ZDOT = -1934
338432
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 09178
51921109
00010596 00000-0 82463-4 0 9104
2 25544 51
6409 253
8574 0008252 159
6086 200
5408 15
73968868 7583
Satellite: ISS
Catalog Number: 25544
Epoch time: 09178
51921109 = yrday
fracday
Element set: 910
Inclination: 51
6409 deg
RA of node: 253
8574 deg
Eccentricity:
0008252
Arg of perigee: 159
6086 deg
Mean anomaly: 200
5408 deg
Mean motion: 15
73968868 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 758
Checksum: 337
Coasting Arc #12 (Orbit 773)
---------------------------------------
Vector Time (GMT): 2009/179/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 686867
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3616347
97 A = 6730914
78 meter
Y = 5417633
92 meter E =
0020605
Z = 1647233
99 I = 51
34841
XDOT = -3324
192923 Wp = 132
61712
YDOT = 3965
963083 meter/sec RA = 247
94486 deg
ZDOT = -5714
371202 TA = 29
08649
MA = 28
97186
Ha = 192
146 n
mi
Hp = 182
287
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11864658
68 X = 3547496
37
Y = 17774389
50 feet Y = 5457688
87 meter
Z = 5404311
00 Z = 1664635
53
XDOT = -10906
144759 XDOT = -3340
534724
YDOT = 13011
689906 feet/sec YDOT = 3928
699336 meter/sec
ZDOT = -18747
937013 ZDOT = -5730
559247
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16451606
24 X = 5014449
58
Y = -13612435
44 feet Y = -4149070
32 meter
Z = 5472830
96 Z = 1668118
88
XDOT = 13068
207433 XDOT = 3983
189625
YDOT = 8189
939220 feet/sec YDOT = 2496
293474 meter/sec
ZDOT = -18811
198059 ZDOT = -5733
653169
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 09179
53504240
00010596 00000-0 82463-4 0 9111
2 25544 51
6410 248
6406 0008123 162
0457 198
0995 15
74020370 7746
Satellite: ISS
Catalog Number: 25544
Epoch time: 09179
53504240 = yrday
fracday
Element set: 911
Inclination: 51
6410 deg
RA of node: 248
6406 deg
Eccentricity:
0008123
Arg of perigee: 162
0457 deg
Mean anomaly: 198
0995 deg
Mean motion: 15
74020370 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 774
Checksum: 297
Coasting Arc #13 (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 = 2589733
07 A = 6721167
59 meter
Y = -3688529
37 meter E =
0012899
Z = 4983702
48 I = 51
32809
XDOT = 4676
182753 Wp = 149
57004
YDOT = 5828
504007 meter/sec RA = 242
81862 deg
ZDOT = 1870
760007 TA = 282
23449
MA = 282
37892
Ha = 192
002 n
mi
Hp = 182
438
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8496499
58 X = 2606576
48
Y = -12101474
31 feet Y = -3659475
90 meter
Z = 16350729
93 Z = 4996323
84
XDOT = 15341
806931 XDOT = 4601
572090
YDOT = 19122
388476 feet/sec YDOT = 5880
378416 meter/sec
ZDOT = 6137
664064 ZDOT = 1893
296357
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13027389
41 X = -3970748
29
Y = -6878154
09 feet Y = -2096461
37 meter
Z = 16400020
62 Z = 4998726
29
XDOT = 16632
115407 XDOT = 5069
468776
YDOT = -16553
666405 feet/sec YDOT = -5045
557520 meter/sec
ZDOT = 6226
347446 ZDOT = 1897
790702
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
55085990
00010596 00000-0 82463-4 0 9122
2 25544 51
6410 243
4236 0008098 166
6442 193
4937 15
74044717 7909
Satellite: ISS
Catalog Number: 25544
Epoch time: 09180
55085990 = yrday
fracday
Element set: 912
Inclination: 51
6410 deg
RA of node: 243
4236 deg
Eccentricity:
0008098
Arg of perigee: 166
6442 deg
Mean anomaly: 193
4937 deg
Mean motion: 15
74044717 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 790
Checksum: 321
Coasting Arc #14 (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 = -4515043
84 A = 6730942
63 meter
Y = -4730806
76 meter E =
0006446
Z = -1602995
58 I = 51
37513
XDOT = 2610
777543 Wp = 103
37228
YDOT = -4425
592377 meter/sec RA = 237
63136 deg
ZDOT = 5725
182231 TA = 238
88550
MA = 238
94876
Ha = 191
943 n
mi
Hp = 182
617
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14813135
94 X = -4454020
51
Y = -15521019
57 feet Y = -4780955
21 meter
Z = -5259171
84 Z = -1624782
11
XDOT = 8565
543120 XDOT = 2632
259295
YDOT = -14519
660030 feet/sec YDOT = -4396
277800 meter/sec
ZDOT = 18783
406269 ZDOT = 5737
916987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13335226
54 X = -4064577
05
Y = 16780766
20 feet Y = 5114777
54 meter
Z = -5344862
21 Z = -1629114
00
XDOT = -14322
726923 XDOT = -4365
567166
YDOT = -5401
675672 feet/sec YDOT = -1646
430745 meter/sec
ZDOT = 18833
102948 ZDOT = 5740
329778
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
50317879
00010596 00000-0 82463-4 0 9133
2 25544 51
6405 238
5327 0007903 169
4489 190
6841 15
74025064 8059
Satellite: ISS
Catalog Number: 25544
Epoch time: 09181
50317879 = yrday
fracday
Element set: 913
Inclination: 51
6405 deg
RA of node: 238
5327 deg
Eccentricity:
0007903
Arg of perigee: 169
4489 deg
Mean anomaly: 190
6841 deg
Mean motion: 15
74025064 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 805
Checksum: 322
Coasting Arc #15 (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 = -1983245
62 A = 6721027
18 meter
Y = 4013369
81 meter E =
0014787
Z = -5023905
06 I = 51
35907
XDOT = -5596
951133 Wp = 109
10291
YDOT = -4970
475521 meter/sec RA = 232
50548 deg
ZDOT = -1770
231247 TA = 143
81071
MA = 143
71057
Ha = 191
803 n
mi
Hp = 182
677
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6506711
34 X = -2003571
11
Y = 13167223
80 feet Y = 3991079
12 meter
Z = -16482628
13 Z = -5033588
45
XDOT = -18362
700567 XDOT = -5532
354963
YDOT = -16307
334385 feet/sec YDOT = -5032
702456 meter/sec
ZDOT = -5807
845298 ZDOT = -1797
265173
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14000893
75 X = 4267472
41
Y = 4294413
67 feet Y = 1308937
29 meter
Z = -16520384
10 Z = -5035413
07
XDOT = -12959
089231 XDOT = -3949
930398
YDOT = 19612
011932 feet/sec YDOT = 5977
741237 meter/sec
ZDOT = -5914
133937 ZDOT = -1802
628024
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
51897297
00010596 00000-0 82463-4 0 9143
2 25544 51
6407 233
3153 0007964 172
8525 187
2754 15
74049783 8214
Satellite: ISS
Catalog Number: 25544
Epoch time: 09182
51897297 = yrday
fracday
Element set: 914
Inclination: 51
6407 deg
RA of node: 233
3153 deg
Eccentricity:
0007964
Arg of perigee: 172
8525 deg
Mean anomaly: 187
2754 deg
Mean motion: 15
74049783 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 821
Checksum: 337
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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