Date:
August 20th 2009
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) : 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 1560)
---------------------------------------
Vector Time (GMT): 2009/229/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6289780
88 A = 6732527
89 meter
Y = -1980929
92 meter E =
0015233
Z = -1310478
59 I = 51
61007
XDOT = 2569
461145 Wp = 11
52838
YDOT = 4305
469123 meter/sec RA = 351
57755 deg
ZDOT = 5850
512743 TA = 334
07221
MA = 334
14845
Ha = 191
832 n
mi
Hp = 184
518
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20635764
04 X = 6317830
47
Y = -6499113
93 feet Y = -1910436
97 meter
Z = -4299470
45 Z = -1279855
38
XDOT = 8429
990632 XDOT = 2492
705434
YDOT = 14125
554865 feet/sec YDOT = 4333
772714 meter/sec
ZDOT = 19194
595612 ZDOT = 5862
808881
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20678172
28 X = -6302706
91
Y = -6442594
94 feet Y = -1963702
94 meter
Z = -4179096
43 Z = -1273788
59
XDOT = 752
333380 XDOT = 229
311214
YDOT = -14839
501653 feet/sec YDOT = -4523
080104 meter/sec
ZDOT = 19243
133035 ZDOT = 5865
306949
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 09229
50246627
00010596 00000-0 82463-4 0 9004
2 25544 51
6409 352
0796 0008069 343
1995 16
8900 15
73628694 15614
Satellite: ISS
Catalog Number: 25544
Epoch time: 09229
50246627 = yrday
fracday
Element set: 900
Inclination: 51
6409 deg
RA of node: 352
0796 deg
Eccentricity:
0008069
Arg of perigee: 343
1995 deg
Mean anomaly: 16
8900 deg
Mean motion: 15
73628694 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1561
Checksum: 328
Coasting Arc #2 (Orbit 1576)
---------------------------------------
Vector Time (GMT): 2009/230/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2685933
44 A = 6721914
68 meter
Y = -3503932
81 meter E =
0015798
Z = -5081213
32 I = 51
54557
XDOT = 6911
111496 Wp = 46
80882
YDOT = -2969
021172 meter/sec RA = 346
46650 deg
ZDOT = -1598
318426 TA = 207
75723
MA = 207
84163
Ha = 191
871 n
mi
Hp = 184
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8812117
58 X = -2621869
15
Y = -11495842
55 feet Y = -3533610
02 meter
Z = -16670647
39 Z = -5094105
89
XDOT = 22674
250316 XDOT = 6951
562130
YDOT = -9740
883111 feet/sec YDOT = -2891
510810 meter/sec
ZDOT = -5243
826858 ZDOT = -1564
646867
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 851283
14 X = 259471
10
Y = 14400865
00 feet Y = 4389383
65 meter
Z = -16721504
14 Z = -5096714
46
XDOT = -23237
192425 XDOT = -7082
696251
YDOT = -4590
076819 feet/sec YDOT = -1399
055414 meter/sec
ZDOT = -5111
501540 ZDOT = -1557
985669
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 09230
51852923
00010596 00000-0 82463-4 0 9010
2 25544 51
6412 346
8649 0008123 346
6619 13
4328 15
73648399 15776
Satellite: ISS
Catalog Number: 25544
Epoch time: 09230
51852923 = yrday
fracday
Element set: 901
Inclination: 51
6412 deg
RA of node: 346
8649 deg
Eccentricity:
0008123
Arg of perigee: 346
6619 deg
Mean anomaly: 13
4328 deg
Mean motion: 15
73648399 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1577
Checksum: 326
Coasting Arc #3 (Orbit 1592)
---------------------------------------
Vector Time (GMT): 2009/231/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5745553
71 A = 6732253
66 meter
Y = 3181072
96 meter E =
0011063
Z = 1474970
24 I = 51
55178
XDOT = -3519
849135 Wp = 83
50243
YDOT = -3657
460182 meter/sec RA = 341
30021 deg
ZDOT = -5784
771966 TA = 80
24927
MA = 80
12435
Ha = 192
012 n
mi
Hp = 184
136
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18850241
84 X = -5787862
97
Y = 10436591
08 feet Y = 3116586
21 meter
Z = 4839141
21 Z = 1446956
27
XDOT = -11548
061467 XDOT = -3450
588448
YDOT = -11999
541278 feet/sec YDOT = -3696
433825 meter/sec
ZDOT = -18978
910648 ZDOT = -5801
702849
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21522038
49 X = 6559917
33
Y = 1452231
50 feet Y = 442640
16 meter
Z = 4729082
49 Z = 1441424
34
XDOT = 3220
421754 XDOT = 981
584551
YDOT = 14712
731540 feet/sec YDOT = 4484
440573 meter/sec
ZDOT = -19045
663954 ZDOT = -5805
118373
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 09231
53458467
00010596 00000-0 82463-4 0 9029
2 25544 51
6413 341
6496 0008065 350
9890 9
1127 15
73655283 15931
Satellite: ISS
Catalog Number: 25544
Epoch time: 09231
53458467 = yrday
fracday
Element set: 902
Inclination: 51
6413 deg
RA of node: 341
6496 deg
Eccentricity:
0008065
Arg of perigee: 350
9890 deg
Mean anomaly: 9
1127 deg
Mean motion: 15
73655283 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1593
Checksum: 320
Coasting Arc #4 (Orbit 1608)
---------------------------------------
Vector Time (GMT): 2009/232/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3436565
89 A = 6721932
51 meter
Y = 2850107
53 meter E =
0006190
Z = 5020690
97 I = 51
49055
XDOT = -6154
975371 Wp = 34
51207
YDOT = 4273
832017 meter/sec RA = 336
18718 deg
ZDOT = 1790
772236 TA = 38
22976
MA = 38
18589
Ha = 191
995 n
mi
Hp = 183
812
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11274822
48 X = 3380050
98
Y = 9350746
50 feet Y = 2888221
29 meter
Z = 16472083
24 Z = 5037248
16
XDOT = -20193
488750 XDOT = -6211
007713
YDOT = 14021
758587 feet/sec YDOT = 4204
690193 meter/sec
ZDOT = 5875
236994 ZDOT = 1760
735841
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4570581
97 X = -1393113
39
Y = -13838855
68 feet Y = -4218083
21 meter
Z = 16537335
40 Z = 5040579
83
XDOT = 23571
074616 XDOT = 7184
463543
YDOT = -920
365255 feet/sec YDOT = -280
527330 meter/sec
ZDOT = 5757
277487 ZDOT = 1754
818178
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 09232
55063032
00010596 00000-0 82463-4 0 9033
2 25544 51
6421 336
4343 0008181 354
6568 5
4506 15
73709551 16091
Satellite: ISS
Catalog Number: 25544
Epoch time: 09232
55063032 = yrday
fracday
Element set: 903
Inclination: 51
6421 deg
RA of node: 336
4343 deg
Eccentricity:
0008181
Arg of perigee: 354
6568 deg
Mean anomaly: 5
4506 deg
Mean motion: 15
73709551 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1609
Checksum: 294
Coasting Arc #5 (Orbit 1623)
---------------------------------------
Vector Time (GMT): 2009/233/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4944654
73 A = 6732004
06 meter
Y = -4244552
11 meter E =
0015440
Z = -1655253
89 I = 51
49699
XDOT = 4321
392449 Wp = 16
98924
YDOT = 2812
496443 meter/sec RA = 331
01470 deg
ZDOT = 5724
918532 TA = 324
67483
MA = 324
77704
Ha = 192
378 n
mi
Hp = 183
665
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16222620
51 X = 4999791
34
Y = -13925695
90 feet Y = -4188949
84 meter
Z = -5430623
00 Z = -1631099
09
XDOT = 14177
796749 XDOT = 4261
811276
YDOT = 9227
350535 feet/sec YDOT = 2860
487834 meter/sec
ZDOT = 18782
541117 ZDOT = 5745
766715
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21093689
67 X = -6429356
61
Y = 3629810
12 feet Y = 1106366
12 meter
Z = -5335805
77 Z = -1626353
60
XDOT = -7087
767362 XDOT = -2160
351492
YDOT = -13594
680490 feet/sec YDOT = -4143
658613 meter/sec
ZDOT = 18864
670454 ZDOT = 5749
951554
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 09233
50316836
00010596 00000-0 82463-4 0 9043
2 25544 51
6421 331
5459 0008435 358
4886 1
6250 15
73655781 16248
Satellite: ISS
Catalog Number: 25544
Epoch time: 09233
50316836 = yrday
fracday
Element set: 904
Inclination: 51
6421 deg
RA of node: 331
5459 deg
Eccentricity:
0008435
Arg of perigee: 358
4886 deg
Mean anomaly: 1
6250 deg
Mean motion: 15
73655781 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1624
Checksum: 311
Coasting Arc #6 (Orbit 1639)
---------------------------------------
Vector Time (GMT): 2009/234/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4051271
72 A = 6722259
27 meter
Y = -2045348
77 meter E =
0017356
Z = -4973628
26 I = 51
43853
XDOT = 5136
237544 Wp = 47
85110
YDOT = -5371
587134 meter/sec RA = 325
90131 deg
ZDOT = -1967
649544 TA = 203
00451
MA = 203
08233
Ha = 192
353 n
mi
Hp = 183
354
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13291573
89 X = -4003938
43
Y = -6710461
83 feet Y = -2090388
00 meter
Z = -16317678
02 Z = -4993194
09
XDOT = 16851
173046 XDOT = 5205
480209
YDOT = -17623
317368 feet/sec YDOT = -5313
763627 meter/sec
ZDOT = -6455
543122 ZDOT = -1942
529559
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8107753
53 X = 2471243
28
Y = 12387094
17 feet Y = 3775586
30 meter
Z = -16394727
24 Z = -4997112
86
XDOT = -22515
067644 XDOT = -6862
592618
YDOT = 6292
595819 feet/sec YDOT = 1917
983206 meter/sec
ZDOT = -6356
989153 ZDOT = -1937
610294
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 09234
51920006
00010596 00000-0 82463-4 0 9056
2 25544 51
6416 326
3311 0008304 2
0058 358
1136 15
73682644 16408
Satellite: ISS
Catalog Number: 25544
Epoch time: 09234
51920006 = yrday
fracday
Element set: 905
Inclination: 51
6416 deg
RA of node: 326
3311 deg
Eccentricity:
0008304
Arg of perigee: 2
0058 deg
Mean anomaly: 358
1136 deg
Mean motion: 15
73682644 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1640
Checksum: 274
Coasting Arc #7 (Orbit 1655)
---------------------------------------
Vector Time (GMT): 2009/235/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4005911
05 A = 6731677
31 meter
Y = 5107252
70 meter E =
0014032
Z = 1778381
62 I = 51
44556
XDOT = -4877
868014 Wp = 79
89884
YDOT = -1840
353089 meter/sec RA = 320
72188 deg
ZDOT = -5662
178518 TA = 80
35215
MA = 80
19365
Ha = 192
512 n
mi
Hp = 183
222
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13142752
78 X = -4071362
51
Y = 16756078
42 feet Y = 5062090
35 meter
Z = 5834585
36 Z = 1758761
85
XDOT = -16003
503983 XDOT = -4829
420627
YDOT = -6037
903835 feet/sec YDOT = -1894
629578 meter/sec
ZDOT = -18576
701176 ZDOT = -5685
757346
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19626808
73 X = 5982251
30
Y = -8317346
69 feet Y = -2535127
27 meter
Z = 5757657
87 Z = 1754934
12
XDOT = 10401
350482 XDOT = 3170
331627
YDOT = 11527
887912 feet/sec YDOT = 3513
700236 meter/sec
ZDOT = -18669
521691 ZDOT = -5690
470211
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 09235
53522417
00010596 00000-0 82463-4 0 9064
2 25544 51
6408 321
1159 0008388 7
1309 352
9972 15
73705448 16564
Satellite: ISS
Catalog Number: 25544
Epoch time: 09235
53522417 = yrday
fracday
Element set: 906
Inclination: 51
6408 deg
RA of node: 321
1159 deg
Eccentricity:
0008388
Arg of perigee: 7
1309 deg
Mean anomaly: 352
9972 deg
Mean motion: 15
73705448 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1656
Checksum: 318
Coasting Arc #8 (Orbit 1671)
---------------------------------------
Vector Time (GMT): 2009/236/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4434401
54 A = 6722263
85 meter
Y = 1148410
93 meter E =
0008206
Z = 4912730
95 I = 51
39230
XDOT = -3968
175292 Wp = 53
04023
YDOT = 6256
256386 meter/sec RA = 315
60567 deg
ZDOT = 2121
767356 TA = 16
34304
MA = 16
31659
Ha = 192
413 n
mi
Hp = 182
993
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14548561
47 X = 4397365
11
Y = 3767752
38 feet Y = 1197792
02 meter
Z = 16117883
69 Z = 4934183
25
XDOT = -13018
947807 XDOT = -4048
146049
YDOT = 20525
775546 feet/sec YDOT = 6211
434821 meter/sec
ZDOT = 6961
178991 ZDOT = 2102
295617
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11016788
89 X = -3357917
25
Y = -10087536
81 feet Y = -3074681
22 meter
Z = 16202306
53 Z = 4938463
03
XDOT = 20403
699226 XDOT = 6219
047524
YDOT = -11237
698302 feet/sec YDOT = -3425
250442 meter/sec
ZDOT = 6884
890245 ZDOT = 2098
514547
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 09236
55123835
00010596 00000-0 82463-4 0 9079
2 25544 51
6410 315
8997 0008429 10
1173 350
0158 15
73746648 16726
Satellite: ISS
Catalog Number: 25544
Epoch time: 09236
55123835 = yrday
fracday
Element set: 907
Inclination: 51
6410 deg
RA of node: 315
8997 deg
Eccentricity:
0008429
Arg of perigee: 10
1173 deg
Mean anomaly: 350
0158 deg
Mean motion: 15
73746648 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1672
Checksum: 315
Coasting Arc #9 (Orbit 1686)
---------------------------------------
Vector Time (GMT): 2009/237/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2884588
53 A = 6731432
69 meter
Y = -5760106
99 meter E =
0015320
Z = -1927706
59 I = 51
40148
XDOT = 5232
153297 Wp = 24
50937
YDOT = 754
907613 meter/sec RA = 310
42080 deg
ZDOT = 5603
191948 TA = 313
97132
MA = 314
09756
Ha = 192
767 n
mi
Hp = 182
861
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9463873
12 X = 2958149
09
Y = -18897988
83 feet Y = -5727438
54 meter
Z = -6324496
70 Z = -1913514
57
XDOT = 17165
857272 XDOT = 5196
103630
YDOT = 2476
731015 feet/sec YDOT = 813
215077 meter/sec
ZDOT = 18383
175684 ZDOT = 5628
522181
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17018864
69 X = -5187349
96
Y = 12560120
99 feet Y = 3828324
88 meter
Z = -6268950
48 Z = -1910776
11
XDOT = -13179
159055 XDOT = -4017
007680
YDOT = -8681
480689 feet/sec YDOT = -2646
115314 meter/sec
ZDOT = 18482
830730 ZDOT = 5633
566807
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 09237
50374662
00010596 00000-0 82463-4 0 9082
2 25544 51
6403 311
0108 0008671 13
3221 346
8170 15
73702031 16879
Satellite: ISS
Catalog Number: 25544
Epoch time: 09237
50374662 = yrday
fracday
Element set: 908
Inclination: 51
6403 deg
RA of node: 311
0108 deg
Eccentricity:
0008671
Arg of perigee: 13
3221 deg
Mean anomaly: 346
8170 deg
Mean motion: 15
73702031 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1687
Checksum: 281
Coasting Arc #10 (Orbit 1702)
---------------------------------------
Vector Time (GMT): 2009/238/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4644492
10 A = 6722550
43 meter
Y = -184314
15 meter E =
0018650
Z = -4873265
68 I = 51
35267
XDOT = 2644
762196 Wp = 50
89417
YDOT = -6855
647138 meter/sec RA = 305
30406 deg
ZDOT = -2255
509912 TA = 197
00574
MA = 197
06833
Ha = 192
799 n
mi
Hp = 182
498
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15237834
98 X = -4618412
45
Y = -604705
21 feet Y = -236105
70 meter
Z = -15988404
47 Z = -4895765
27
XDOT = 8677
041324 XDOT = 2732
183509
YDOT = -22492
280636 feet/sec YDOT = -6825
583025 meter/sec
ZDOT = -7399
966903 ZDOT = -2242
449409
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13359439
12 X = 4071957
04
Y = 7158560
59 feet Y = 2181929
27 meter
Z = -16076901
37 Z = -4900239
54
XDOT = -17145
934322 XDOT = -5226
080781
YDOT = 15451
109036 feet/sec YDOT = 4709
498034 meter/sec
ZDOT = -7348
922666 ZDOT = -2239
951628
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 09238
51974733
00010596 00000-0 82463-4 0 9090
2 25544 51
6395 305
7949 0008602 17
7913 342
3549 15
73728027 17035
Satellite: ISS
Catalog Number: 25544
Epoch time: 09238
51974733 = yrday
fracday
Element set: 909
Inclination: 51
6395 deg
RA of node: 305
7949 deg
Eccentricity:
0008602
Arg of perigee: 17
7913 deg
Mean anomaly: 342
3549 deg
Mean motion: 15
73728027 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1703
Checksum: 335
Coasting Arc #11 (Orbit 1718)
---------------------------------------
Vector Time (GMT): 2009/239/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1727425
88 A = 6731040
03 meter
Y = 6184061
22 meter E =
0016643
Z = 2012320
30 I = 51
36599
XDOT = -5322
589316 Wp = 79
20398
YDOT = 333
294796 meter/sec RA = 300
11366 deg
ZDOT = -5551
359228 TA = 78
28570
MA = 78
09901
Ha = 192
893 n
mi
Hp = 182
343
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5667407
74 X = -1806224
19
Y = 20288914
75 feet Y = 6164303
49 meter
Z = 6602100
74 Z = 2003737
25
XDOT = -17462
563373 XDOT = -5298
953254
YDOT = 1093
486864 feet/sec YDOT = 273
906777 meter/sec
ZDOT = -18213
120828 ZDOT = -5577
158884
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13720912
62 X = 4182134
17
Y = -15998027
54 feet Y = -4876198
80 meter
Z = 6568635
92 Z = 2002120
23
XDOT = 15035
237072 XDOT = 4582
740260
YDOT = 5318
601338 feet/sec YDOT = 1621
109688 meter/sec
ZDOT = -18314
574713 ZDOT = -5582
282373
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 09239
53573884
00010596 00000-0 82463-4 0 9107
2 25544 51
6400 300
5788 0008855 21
6033 338
5497 15
73788096 17191
Satellite: ISS
Catalog Number: 25544
Epoch time: 09239
53573884 = yrday
fracday
Element set: 910
Inclination: 51
6400 deg
RA of node: 300
5788 deg
Eccentricity:
0008855
Arg of perigee: 21
6033 deg
Mean anomaly: 338
5497 deg
Mean motion: 15
73788096 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1719
Checksum: 338
Coasting Arc #12 (Orbit 1734)
---------------------------------------
Vector Time (GMT): 2009/240/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4614732
50 A = 6722549
71 meter
Y = -772597
98 meter E =
0010553
Z = 4817126
27 I = 51
32325
XDOT = -1269
700445 Wp = 65
44685
YDOT = 7222
569330 meter/sec RA = 294
99603 deg
ZDOT = 2375
008809 TA = 1
30938
MA = 1
30662
Ha = 192
818 n
mi
Hp = 182
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15140198
48 X = 4599628
24
Y = -2534770
28 feet Y = -721077
94 meter
Z = 15804220
05 Z = 4839507
81
XDOT = -4165
683876 XDOT = -1361
907392
YDOT = 23696
093604 feet/sec YDOT = 7207
855161 meter/sec
ZDOT = 7792
023651 ZDOT = 2368
616903
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14782707
83 X = -4505769
35
Y = -3785916
84 feet Y = -1153947
45 meter
Z = 15892212
71 Z = 4843946
43
XDOT = 13183
085978 XDOT = 4018
204606
YDOT = -18874
335537 feet/sec YDOT = -5752
897472 meter/sec
ZDOT = 7767
229631 ZDOT = 2367
451592
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 09240
55172312
00010596 00000-0 82463-4 0 9113
2 25544 51
6397 295
3629 0008780 25
6923 334
4674 15
73785884 17352
Satellite: ISS
Catalog Number: 25544
Epoch time: 09240
55172312 = yrday
fracday
Element set: 911
Inclination: 51
6397 deg
RA of node: 295
3629 deg
Eccentricity:
0008780
Arg of perigee: 25
6923 deg
Mean anomaly: 334
4674 deg
Mean motion: 15
73785884 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1735
Checksum: 335
Coasting Arc #13 (Orbit 1749)
---------------------------------------
Vector Time (GMT): 2009/241/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 476256
33 A = 6730818
72 meter
Y = -6360346
34 meter E =
0015193
Z = -2133189
64 I = 51
33919
XDOT = 5195
609037 Wp = 34
26670
YDOT = -1444
598857 meter/sec RA = 289
80208 deg
ZDOT = 5498
547370 TA = 301
76708
MA = 301
91501
Ha = 193
067 n
mi
Hp = 182
014
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1562520
76 X = 557705
98
Y = -20867278
02 feet Y = -6354565
09 meter
Z = -6998653
68 Z = -2130678
37
XDOT = 17045
961406 XDOT = 5184
665922
YDOT = -4739
497562 feet/sec YDOT = -1386
559866 meter/sec
ZDOT = 18039
853575 ZDOT = 5523
760794
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9609877
56 X = -2929090
68
Y = 18592171
12 feet Y = 5666893
76 meter
Z = -6989087
42 Z = -2130273
85
XDOT = -16092
205421 XDOT = -4904
904212
YDOT = -1537
689458 feet/sec YDOT = -468
687747 meter/sec
ZDOT = 18138
955263 ZDOT = 5528
753564
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 09241
50420198
00010596 00000-0 82463-4 0 9128
2 25544 51
6393 290
4732 0008926 29
4235 330
7429 15
73781539 17506
Satellite: ISS
Catalog Number: 25544
Epoch time: 09241
50420198 = yrday
fracday
Element set: 912
Inclination: 51
6393 deg
RA of node: 290
4732 deg
Eccentricity:
0008926
Arg of perigee: 29
4235 deg
Mean anomaly: 330
7429 deg
Mean motion: 15
73781539 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1750
Checksum: 314
Coasting Arc #14 (Orbit 1765)
---------------------------------------
Vector Time (GMT): 2009/242/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4415300
89 A = 6722749
23 meter
Y = 1710306
65 meter E =
0019658
Z = -4790663
56 I = 51
30356
XDOT = -136
899215 Wp = 55
65335
YDOT = -7276
839888 meter/sec RA = 284
68385 deg
ZDOT = -2468
012902 TA = 190
02987
MA = 190
06916
Ha = 193
174 n
mi
Hp = 181
711
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14485895
29 X = -4410825
77
Y = 5611242
30 feet Y = 1660957
30 meter
Z = -15717400
13 Z = -4812101
93
XDOT = -449
144406 XDOT = -43
529143
YDOT = -23874
146614 feet/sec YDOT = -7277
848657 meter/sec
ZDOT = -8097
155189 ZDOT = -2468
451330
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15447993
72 X = 4708548
49
Y = 177377
62 feet Y = 54064
70 meter
Z = -15801642
22 Z = -4816340
55
XDOT = -8540
075028 XDOT = -2603
014868
YDOT = 21166
759599 feet/sec YDOT = 6451
628326 meter/sec
ZDOT = -8099
245612 ZDOT = -2468
650062
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 09242
52017104
00010596 00000-0 82463-4 0 9131
2 25544 51
6398 285
2569 0008953 33
7678 326
4053 15
73783340 17664
Satellite: ISS
Catalog Number: 25544
Epoch time: 09242
52017104 = yrday
fracday
Element set: 913
Inclination: 51
6398 deg
RA of node: 285
2569 deg
Eccentricity:
0008953
Arg of perigee: 33
7678 deg
Mean anomaly: 326
4053 deg
Mean motion: 15
73783340 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1766
Checksum: 325
Coasting Arc #15 (Orbit 1781)
---------------------------------------
Vector Time (GMT): 2009/243/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 701645
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 713922
14 A = 6730581
82 meter
Y = 6323203
96 meter E =
0018984
Z = 2181675
22 I = 51
32336
XDOT = -4842
755569 Wp = 81
70889
YDOT = 2446
664825 meter/sec RA = 279
48718 deg
ZDOT = -5463
261984 TA = 73
74495
MA = 73
53619
Ha = 193
221 n
mi
Hp = 181
601
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2342264
23 X = 632563
88
Y = 20745419
82 feet Y = 6330732
54 meter
Z = 7157727
10 Z = 2184945
85
XDOT = -15888
305674 XDOT = -4843
215495
YDOT = 8027
115567 feet/sec YDOT = 2392
507769 meter/sec
ZDOT = -17924
087873 ZDOT = -5486
788862
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5275795
17 X = 1608062
37
Y = -20194939
55 feet Y = -6155417
57 meter
Z = 7170920
76 Z = 2185696
65
XDOT = 16138
150186 XDOT = 4918
908177
YDOT = -2231
693843 feet/sec YDOT = -680
220283 meter/sec
ZDOT = -18016
508407 ZDOT = -5491
431762
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 09243
53613053
00010596 00000-0 82463-4 0 9149
2 25544 51
6391 280
0408 0009132 37
2110 322
9685 15
73832109 17820
Satellite: ISS
Catalog Number: 25544
Epoch time: 09243
53613053 = yrday
fracday
Element set: 914
Inclination: 51
6391 deg
RA of node: 280
0408 deg
Eccentricity:
0009132
Arg of perigee: 37
2110 deg
Mean anomaly: 322
9685 deg
Mean motion: 15
73832109 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1782
Checksum: 289
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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