Date:
April 22nd 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17222 26 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 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
113/20:49:49
789 -7
0 7
9 7
9
N/A 3
3 -0
4 189
3
000/00:19:35
579 1
8 0
2 188
2
Coasting Arc #1 (Orbit 1422)
---------------------------------------
Vector Time (GMT): 2010/109/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5955715
89 A = 6727793
08 meter
Y = 2487804
26 meter E =
0004135
Z = -1897798
93 I = 51
71218
XDOT = -3442
982397 Wp = 66
14777
YDOT = -3949
356263 meter/sec RA = 170
75018 deg
ZDOT = 5638
947235 TA = 272
78941
MA = 272
83674
Ha = 188
859 n
mi
Hp = 182
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19539750
28 X = -5973873
08
Y = 8162087
48 feet Y = 2421102
46 meter
Z = -6226374
44 Z = -1926776
03
XDOT = -11295
874006 XDOT = -3425
957292
YDOT = -12957
205586 feet/sec YDOT = -3987
762763 meter/sec
ZDOT = 18500
483055 ZDOT = 5622
262301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13753725
33 X = -4192135
48
Y = 16056437
69 feet Y = 4894002
21 meter
Z = -6341537
67 Z = -1932900
68
XDOT = -14840
273747 XDOT = -4523
315438
YDOT = -5445
755446 feet/sec YDOT = -1659
866260 meter/sec
ZDOT = 18433
989518 ZDOT = 5618
680005
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 10109
50379545
00016717 00000-0 10270-3 0 9006
2 25544 51
6453 171
7844 0003761 189
6507 170
4585 15
74967196 14236
Satellite: ISS
Catalog Number: 25544
Epoch time: 10109
50379545 = yrday
fracday
Element set: 900
Inclination: 51
6453 deg
RA of node: 171
7844 deg
Eccentricity:
0003761
Arg of perigee: 189
6507 deg
Mean anomaly: 170
4585 deg
Mean motion: 15
74967196 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1423
Checksum: 326
Coasting Arc #2 (Orbit 1438)
---------------------------------------
Vector Time (GMT): 2010/110/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2903169
72 A = 6718326
39 meter
Y = 3368947
07 meter E =
0012185
Z = -5045898
24 I = 51
71012
XDOT = -6775
376906 Wp = 92
94968
YDOT = 3182
619788 meter/sec RA = 165
64439 deg
ZDOT = -1777
608138 TA = 159
95473
MA = 159
90683
Ha = 188
772 n
mi
Hp = 182
488
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9524835
03 X = 2889793
91
Y = 11052975
96 feet Y = 3401337
42 meter
Z = -16554784
25 Z = -5031826
98
XDOT = -22228
926858 XDOT = -6801
826643
YDOT = 10441
665972 feet/sec YDOT = 3106
705664 meter/sec
ZDOT = -5832
047698 ZDOT = -1810
587161
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13656464
99 X = 4162490
53
Y = 5314653
21 feet Y = 1619906
30 meter
Z = -16498698
94 Z = -5028803
44
XDOT = -14411
671104 XDOT = -4392
677353
YDOT = 18564
077250 feet/sec YDOT = 5658
330746 meter/sec
ZDOT = -5963
122464 ZDOT = -1817
559727
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 10110
51897852
00016717 00000-0 10270-3 0 9016
2 25544 51
6453 166
5633 0003768 192
2105 167
8968 15
75004840 14396
Satellite: ISS
Catalog Number: 25544
Epoch time: 10110
51897852 = yrday
fracday
Element set: 901
Inclination: 51
6453 deg
RA of node: 166
5633 deg
Eccentricity:
0003768
Arg of perigee: 192
2105 deg
Mean anomaly: 167
8968 deg
Mean motion: 15
75004840 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1439
Checksum: 316
Coasting Arc #3 (Orbit 1454)
---------------------------------------
Vector Time (GMT): 2010/111/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5853668
76 A = 6728439
06 meter
Y = -3075164
74 meter E =
0015287
Z = 1196933
89 I = 51
77472
XDOT = 3204
175434 Wp = 134
74089
YDOT = 3790
864207 meter/sec RA = 160
48220 deg
ZDOT = -5895
540736 TA = 32
15396
MA = 32
06083
Ha = 188
514 n
mi
Hp = 182
342
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19204950
00 X = 5881806
26
Y = -10089123
15 feet Y = -3009548
22 meter
Z = 3926948
47 Z = 1225439
30
XDOT = 10512
386593 XDOT = 3190
186630
YDOT = 12437
218526 feet/sec YDOT = 3826
617088 meter/sec
ZDOT = -19342
325248 ZDOT = -5880
008770
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11986620
88 X = 3653522
04
Y = -18056543
52 feet Y = -5503634
47 meter
Z = 4040246
36 Z = 1231467
09
XDOT = 13974
218871 XDOT = 4259
341912
YDOT = 4937
442815 feet/sec YDOT = 1504
932570 meter/sec
ZDOT = -19280
407815 ZDOT = -5876
668302
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 10111
53413738
00016717 00000-0 10270-3 0 9027
2 25544 51
6459 161
3425 0003532 195
5452 164
5604 15
75083651 14550
Satellite: ISS
Catalog Number: 25544
Epoch time: 10111
53413738 = yrday
fracday
Element set: 902
Inclination: 51
6459 deg
RA of node: 161
3425 deg
Eccentricity:
0003532
Arg of perigee: 195
5452 deg
Mean anomaly: 164
5604 deg
Mean motion: 15
75083651 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1455
Checksum: 291
Coasting Arc #4 (Orbit 1470)
---------------------------------------
Vector Time (GMT): 2010/112/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2681543
20 A = 6717278
93 meter
Y = -3285226
86 meter E =
0005663
Z = 5208578
94 I = 51
76492
XDOT = 6599
469851 Wp = 160
56297
YDOT = -3857
283943 meter/sec RA = 155
36829 deg
ZDOT = 959
163910 TA = 280
28499
MA = 280
34884
Ha = 188
530 n
mi
Hp = 182
398
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8797713
90 X = -2669910
20
Y = -10778303
35 feet Y = -3315148
40 meter
Z = 17088513
59 Z = 5195580
30
XDOT = 21651
803972 XDOT = 6637
452764
YDOT = -12655
131046 feet/sec YDOT = -3783
272365 meter/sec
ZDOT = 3146
863222 ZDOT = 991
316372
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13066176
86 X = -3982570
71
Y = -4961375
77 feet Y = -1512227
33 meter
Z = 17036685
79 Z = 5192781
83
XDOT = 12172
597221 XDOT = 3710
207633
YDOT = -20750
228653 feet/sec YDOT = -6324
669694 meter/sec
ZDOT = 3274
657221 ZDOT = 998
115521
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 10112
54927414
00016717 00000-0 10270-3 0 9031
2 25544 51
6455 156
1218 0003553 198
2831 161
8205 15
75103875 14718
Satellite: ISS
Catalog Number: 25544
Epoch time: 10112
54927414 = yrday
fracday
Element set: 903
Inclination: 51
6455 deg
RA of node: 156
1218 deg
Eccentricity:
0003553
Arg of perigee: 198
2831 deg
Mean anomaly: 161
8205 deg
Mean motion: 15
75103875 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1471
Checksum: 293
Coasting Arc #5 (Orbit 1485)
---------------------------------------
Vector Time (GMT): 2010/113/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 797575
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5637241
80 A = 6728914
15 meter
Y = 3639749
82 meter E =
0008091
Z = -457423
91 I = 51
83166
XDOT = -2928
284140 Wp = 49
34669
YDOT = -3786
660424 meter/sec RA = 150
22276 deg
ZDOT = 6031
529625 TA = 305
69067
MA = 305
76594
Ha = 188
309 n
mi
Hp = 182
484
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18494887
80 X = -5675301
08
Y = 11941436
42 feet Y = 3576498
01 meter
Z = -1500734
62 Z = -484902
18
XDOT = -9607
231430 XDOT = -2915
023476
YDOT = -12423
426588 feet/sec YDOT = -3819
331929 meter/sec
ZDOT = 19788
483023 ZDOT = 6017
336333
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9815531
89 X = -2991774
12
Y = 19697065
32 feet Y = 6003665
51 meter
Z = -1609948
56 Z = -490712
32
XDOT = -13261
989740 XDOT = -4042
254473
YDOT = -5014
570513 feet/sec YDOT = -1528
441092 meter/sec
ZDOT = 19731
880694 ZDOT = 6014
277236
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 10113
50094450
00016717 00000-0 10270-3 0 9044
2 25544 51
6459 151
2270 0003354 202
4221 157
6797 15
75108282 14868
Satellite: ISS
Catalog Number: 25544
Epoch time: 10113
50094450 = yrday
fracday
Element set: 904
Inclination: 51
6459 deg
RA of node: 151
2270 deg
Eccentricity:
0003354
Arg of perigee: 202
4221 deg
Mean anomaly: 157
6797 deg
Mean motion: 15
75108282 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1486
Checksum: 286
Coasting Arc #6 (Orbit 1491)
---------------------------------------
Vector Time (GMT): 2010/113/20:59:37
579
Vector Time (MET): N/A
Weight (LBS) : 796736
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3115868
44 A = 6729087
96 meter
Y = 4970722
53 meter E =
0003540
Z = -3294350
98 I = 51
82717
XDOT = -6036
057868 Wp = 251
82500
YDOT = -643
347535 meter/sec RA = 148
27850 deg
ZDOT = 4733
093219 TA = 69
65273
MA = 69
61469
Ha = 189
300 n
mi
Hp = 188
161
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10222665
48 X = -3155216
98
Y = 16308144
78 feet Y = 4935658
91 meter
Z = -10808238
13 Z = -3309583
64
XDOT = -19803
339462 XDOT = -6051
407773
YDOT = -2110
720259 feet/sec YDOT = -710
931992 meter/sec
ZDOT = 15528
521059 ZDOT = 4703
732743
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13819524
83 X = 4212191
17
Y = -13347993
25 feet Y = -4068468
34 meter
Z = -10868684
23 Z = -3312774
95
XDOT = 17810
757326 XDOT = 5428
718833
YDOT = 5877
032358 feet/sec YDOT = 1791
319463 meter/sec
ZDOT = 15411
670981 ZDOT = 4697
477315
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 10113
88160858
00016717 00000-0 10270-3 0 9052
2 25544 51
6473 149
2684 0008213 260
1787 99
8448 15
73409420 14920
Satellite: ISS
Catalog Number: 25544
Epoch time: 10113
88160858 = yrday
fracday
Element set: 905
Inclination: 51
6473 deg
RA of node: 149
2684 deg
Eccentricity:
0008213
Arg of perigee: 260
1787 deg
Mean anomaly: 99
8448 deg
Mean motion: 15
73409420 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1492
Checksum: 326
Coasting Arc #7 (Orbit 1507)
---------------------------------------
Vector Time (GMT): 2010/114/20:59:37
579
Vector Time (MET): N/A
Weight (LBS) : 796736
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5388848
83 A = 6726850
61 meter
Y = -80734
36 meter E =
0002088
Z = -4025215
75 I = 51
84482
XDOT = -2845
072818 Wp = 313
64584
YDOT = 5979
010836 meter/sec RA = 143
21266 deg
ZDOT = -3926
156530 TA = 275
90527
MA = 275
92907
Ha = 189
191 n
mi
Hp = 188
494
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17679950
22 X = 5408904
99
Y = -264876
53 feet Y = -20361
08 meter
Z = -13206088
41 Z = -3998987
84
XDOT = -9334
228404 XDOT = -2892
647058
YDOT = 19616
177285 feet/sec YDOT = 5946
929365 meter/sec
ZDOT = -12881
090977 ZDOT = -3940
093798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17356186
93 X = -5290165
78
Y = -3762877
27 feet Y = -1146924
99 meter
Z = -13101721
28 Z = -3993404
65
XDOT = 13185
347238 XDOT = 4018
893838
YDOT = -15744
094202 feet/sec YDOT = -4798
799913 meter/sec
ZDOT = -12936
355565 ZDOT = -3943
001176
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 10114
89781923
00016717 00000-0 10270-3 0 9067
2 25544 51
6474 144
0552 0008309 264
6694 95
3521 15
73436195 15080
Satellite: ISS
Catalog Number: 25544
Epoch time: 10114
89781923 = yrday
fracday
Element set: 906
Inclination: 51
6474 deg
RA of node: 144
0552 deg
Eccentricity:
0008309
Arg of perigee: 264
6694 deg
Mean anomaly: 95
3521 deg
Mean motion: 15
73436195 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1508
Checksum: 321
Coasting Arc #8 (Orbit 1523)
---------------------------------------
Vector Time (GMT): 2010/115/20:59:37
579
Vector Time (MET): N/A
Weight (LBS) : 796736
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1837595
09 A = 6728156
91 meter
Y = -5405624
45 meter E =
0003951
Z = 3556694
91 I = 51
87261
XDOT = 6201
881247 Wp = 82
69259
YDOT = -844
256357 meter/sec RA = 138
04579 deg
ZDOT = -4482
675426 TA = 55
07340
MA = 55
03629
Ha = 188
086 n
mi
Hp = 187
689
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6028855
28 X = 1880627
19
Y = -17734988
34 feet Y = -5384834
62 meter
Z = 11668946
56 Z = 3565726
80
XDOT = 20347
379420 XDOT = 6232
637219
YDOT = -2769
869938 feet/sec YDOT = -774
731441 meter/sec
ZDOT = -14706
940374 ZDOT = -4452
471591
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9545877
78 X = -2909583
55
Y = 16090898
83 feet Y = 4904505
96 meter
Z = 11704717
57 Z = 3567597
92
XDOT = -19386
934513 XDOT = -5909
137640
YDOT = -879
426913 feet/sec YDOT = -268
049323 meter/sec
ZDOT = -14586
769937 ZDOT = -4446
047477
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 10115
91401016
00016717 00000-0 10270-3 0 9074
2 25544 51
6468 138
8415 0008195 268
8433 91
1792 15
73469082 15245
Satellite: ISS
Catalog Number: 25544
Epoch time: 10115
91401016 = yrday
fracday
Element set: 907
Inclination: 51
6468 deg
RA of node: 138
8415 deg
Eccentricity:
0008195
Arg of perigee: 268
8433 deg
Mean anomaly: 91
1792 deg
Mean motion: 15
73469082 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1524
Checksum: 313
Coasting Arc #9 (Orbit 1539)
---------------------------------------
Vector Time (GMT): 2010/116/20:59:37
579
Vector Time (MET): N/A
Weight (LBS) : 796736
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5369014
86 A = 6727457
13 meter
Y = 1377228
66 meter E =
0003437
Z = 3810654
39 I = 51
89168
XDOT = 1368
753795 Wp = 108
26035
YDOT = -6303
485416 meter/sec RA = 132
98224 deg
ZDOT = 4202
548195 TA = 297
79363
MA = 297
82847
Ha = 188
597 n
mi
Hp = 187
987
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17614878
16 X = -5402528
02
Y = 4518466
75 feet Y = 1317001
85 meter
Z = 12502146
94 Z = 3784489
84
XDOT = 4490
662056 XDOT = 1418
723205
YDOT = -20680
726431 feet/sec YDOT = -6287
899702 meter/sec
ZDOT = 13787
887780 ZDOT = 4209
319243
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18227582
50 X = 5555767
14
Y = -1023465
12 feet Y = -311952
17 meter
Z = 12398060
65 Z = 3778928
89
XDOT = -8388
730940 XDOT = -2556
885190
YDOT = 18112
935145 feet/sec YDOT = 5520
822632 meter/sec
ZDOT = 13814
644633 ZDOT = 4210
703684
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 10116
93018017
00016717 00000-0 10270-3 0 9083
2 25544 51
6467 133
6267 0008215 273
2215 86
8008 15
73478259 15408
Satellite: ISS
Catalog Number: 25544
Epoch time: 10116
93018017 = yrday
fracday
Element set: 908
Inclination: 51
6467 deg
RA of node: 133
6267 deg
Eccentricity:
0008215
Arg of perigee: 273
2215 deg
Mean anomaly: 86
8008 deg
Mean motion: 15
73478259 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1540
Checksum: 305
Coasting Arc #10 (Orbit 1554)
---------------------------------------
Vector Time (GMT): 2010/117/20:59:37
579
Vector Time (MET): N/A
Weight (LBS) : 796736
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -551993
66 A = 6727310
65 meter
Y = 5538738
85 meter E =
0002454
Z = -3776500
98 I = 51
91111
XDOT = -5996
539572 Wp = 258
48653
YDOT = 2298
962133 meter/sec RA = 127
81703 deg
ZDOT = 4245
429029 TA = 56
00530
MA = 55
98199
Ha = 189
041 n
mi
Hp = 188
251
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1811002
83 X = -595541
88
Y = 18171715
40 feet Y = 5532322
64 meter
Z = -12390095
08 Z = -3779288
40
XDOT = -19673
686259 XDOT = -6042
425241
YDOT = 7542
526684 feet/sec YDOT = 2231
648700 meter/sec
ZDOT = 13928
572931 ZDOT = 4216
185795
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4907365
54 X = 1495765
02
Y = -17582308
45 feet Y = -5359087
62 meter
Z = -12401033
05 Z = -3779834
87
XDOT = 19492
061017 XDOT = 5941
180198
YDOT = -4308
018806 feet/sec YDOT = -1313
084132 meter/sec
ZDOT = 13812
250670 ZDOT = 4209
974004
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 10117
88281929
00016717 00000-0 10270-3 0 9093
2 25544 51
6463 128
7382 0008425 276
7933 83
2271 15
73527091 15553
Satellite: ISS
Catalog Number: 25544
Epoch time: 10117
88281929 = yrday
fracday
Element set: 909
Inclination: 51
6463 deg
RA of node: 128
7382 deg
Eccentricity:
0008425
Arg of perigee: 276
7933 deg
Mean anomaly: 83
2271 deg
Mean motion: 15
73527091 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1555
Checksum: 330
Coasting Arc #11 (Orbit 1570)
---------------------------------------
Vector Time (GMT): 2010/118/20:59:37
579
Vector Time (MET): N/A
Weight (LBS) : 796736
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5041532
60 A = 6727905
35 meter
Y = -2606211
21 meter E =
0003769
Z = -3612728
24 I = 51
93016
XDOT = 75
819960 Wp = 307
11388
YDOT = 6294
614570 meter/sec RA = 122
75653 deg
ZDOT = -4429
735622 TA = 275
89485
MA = 275
93781
Ha = 189
261 n
mi
Hp = 188
260
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16540461
28 X = 5087851
37
Y = -8550561
71 feet Y = -2549574
72 meter
Z = -11852782
95 Z = -3588123
53
XDOT = 248
753150 XDOT = 26
946117
YDOT = 20651
622604 feet/sec YDOT = 6295
189280 meter/sec
ZDOT = -14533
253352 ZDOT = -4429
485835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17757971
38 X = -5412629
68
Y = 5802050
61 feet Y = 1768465
03 meter
Z = -11754917
69 Z = -3582898
91
XDOT = 3375
457497 XDOT = 1028
839445
YDOT = -19146
902307 feet/sec YDOT = -5835
975823 meter/sec
ZDOT = -14532
095791 ZDOT = -4429
382797
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 10118
89894865
00016717 00000-0 10270-3 0 9106
2 25544 51
6458 123
5240 0008508 280
2003 79
8201 15
73540851 15714
Satellite: ISS
Catalog Number: 25544
Epoch time: 10118
89894865 = yrday
fracday
Element set: 910
Inclination: 51
6458 deg
RA of node: 123
5240 deg
Eccentricity:
0008508
Arg of perigee: 280
2003 deg
Mean anomaly: 79
8201 deg
Mean motion: 15
73540851 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1571
Checksum: 304
Coasting Arc #12 (Orbit 1586)
---------------------------------------
Vector Time (GMT): 2010/119/20:59:37
579
Vector Time (MET): N/A
Weight (LBS) : 796736
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -670160
50 A = 6726437
58 meter
Y = -5400924
34 meter E =
0005031
Z = 3953954
07 I = 51
94204
XDOT = 5459
348894 Wp = 31
70712
YDOT = -3632
925285 meter/sec RA = 117
59346 deg
ZDOT = -4030
612280 TA = 100
00621
MA = 99
94943
Ha = 189
351 n
mi
Hp = 187
743
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2198689
30 X = -628924
54
Y = -17719568
05 feet Y = -5408188
11 meter
Z = 12972290
25 Z = 3950798
26
XDOT = 17911
249652 XDOT = 5519
147521
YDOT = -11919
046209 feet/sec YDOT = -3571
541041 meter/sec
ZDOT = -13223
793571 ZDOT = -4003
945186
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -263064
05 X = -80181
92
Y = 17862732
36 feet Y = 5444560
82 meter
Z = 12959599
93 Z = 3950086
06
XDOT = -18195
987924 XDOT = -5546
137119
YDOT = 9264
540024 feet/sec YDOT = 2823
831799 meter/sec
ZDOT = -13117
729023 ZDOT = -3998
283806
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 10119
91505594
00016717 00000-0 10270-3 0 9119
2 25544 51
6463 118
3091 0008517 285
2338 74
7883 15
73634728 15876
Satellite: ISS
Catalog Number: 25544
Epoch time: 10119
91505594 = yrday
fracday
Element set: 911
Inclination: 51
6463 deg
RA of node: 118
3091 deg
Eccentricity:
0008517
Arg of perigee: 285
2338 deg
Mean anomaly: 74
7883 deg
Mean motion: 15
73634728 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1587
Checksum: 329
Coasting Arc #13 (Orbit 1602)
---------------------------------------
Vector Time (GMT): 2010/120/20:59:37
579
Vector Time (MET): N/A
Weight (LBS) : 796736
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4444387
62 A = 6728232
70 meter
Y = 3696706
75 meter E =
0005165
Z = 3436091
45 I = 51
95984
XDOT = -1420
085196 Wp = 59
58707
YDOT = -5999
053493 meter/sec RA = 112
53316 deg
ZDOT = 4614
710510 TA = 340
86082
MA = 340
88022
Ha = 189
690 n
mi
Hp = 187
538
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14581324
22 X = -4502086
71
Y = 12128302
98 feet Y = 3646684
11 meter
Z = 11273265
90 Z = 3414360
38
XDOT = -4659
072165 XDOT = -1375
314935
YDOT = -19681
934032 feet/sec YDOT = -6014
683730 meter/sec
ZDOT = 15140
126346 ZDOT = 4607
919957
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16047579
44 X = 4891302
21
Y = -10204272
49 feet Y = -3110262
26 meter
Z = 11186835
58 Z = 3409747
48
XDOT = 1508
803328 XDOT = 459
883254
YDOT = 18950
220891 feet/sec YDOT = 5776
027328 meter/sec
ZDOT = 15112
962733 ZDOT = 4606
431041
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 10120
93114486
00016717 00000-0 10270-3 0 9120
2 25544 51
6455 113
0936 0008500 288
9928 71
0314 15
73609900 16036
Satellite: ISS
Catalog Number: 25544
Epoch time: 10120
93114486 = yrday
fracday
Element set: 912
Inclination: 51
6455 deg
RA of node: 113
0936 deg
Eccentricity:
0008500
Arg of perigee: 288
9928 deg
Mean anomaly: 71
0314 deg
Mean motion: 15
73609900 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1603
Checksum: 290
Coasting Arc #14 (Orbit 1617)
---------------------------------------
Vector Time (GMT): 2010/121/20:59:37
579
Vector Time (MET): N/A
Weight (LBS) : 796736
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1788397
68 A = 6725866
22 meter
Y = 5023065
14 meter E =
0000958
Z = -4098665
93 I = 51
96244
XDOT = -4646
664733 Wp = 311
01507
YDOT = 4788
532488 meter/sec RA = 107
37169 deg
ZDOT = 3841
048416 TA = 358
28895
MA = 358
28928
Ha = 189
721 n
mi
Hp = 187
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5867446
47 X = 1752006
75
Y = 16479872
52 feet Y = 5042860
93 meter
Z = -13447066
71 Z = -4090065
79
XDOT = -15244
963034 XDOT = -4718
524939
YDOT = 15710
408424 feet/sec YDOT = 4736
168616 meter/sec
ZDOT = 12601
864883 ZDOT = 3818
300499
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4135280
47 X = -1260433
49
Y = -17024540
32 feet Y = -5189079
89 meter
Z = -13412725
74 Z = -4088198
81
XDOT = 15681
960163 XDOT = 4779
861458
YDOT = -13666
130778 feet/sec YDOT = -4165
436661 meter/sec
ZDOT = 12511
393161 ZDOT = 3813
472635
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 10121
88370678
00016717 00000-0 10270-3 0 9133
2 25544 51
6450 108
2042 0008485 291
7288 68
2972 15
73662962 16189
Satellite: ISS
Catalog Number: 25544
Epoch time: 10121
88370678 = yrday
fracday
Element set: 913
Inclination: 51
6450 deg
RA of node: 108
2042 deg
Eccentricity:
0008485
Arg of perigee: 291
7288 deg
Mean anomaly: 68
2972 deg
Mean motion: 15
73662962 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1618
Checksum: 326
Coasting Arc #15 (Orbit 1633)
---------------------------------------
Vector Time (GMT): 2010/122/20:59:37
579
Vector Time (MET): N/A
Weight (LBS) : 796736
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3635681
85 A = 6728446
36 meter
Y = -4611694
16 meter E =
0004403
Z = -3285098
47 I = 51
97864
XDOT = 2615
951776 Wp = 316
66757
YDOT = 5455
623254 meter/sec RA = 102
31327 deg
ZDOT = -4756
733176 TA = 261
62861
MA = 261
67853
Ha = 189
819 n
mi
Hp = 187
144
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11928090
07 X = 3702938
96
Y = -15130230
18 feet Y = -4570661
48 meter
Z = -10777882
12 Z = -3267273
21
XDOT = 8582
518949 XDOT = 2577
859103
YDOT = 17899
026424 feet/sec YDOT = 5484
663781 meter/sec
ZDOT = -15606
079975 ZDOT = -4744
116877
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13314177
08 X = -4058161
17
Y = 13980662
96 feet Y = 4261306
07 meter
Z = -10706992
71 Z = -3263491
38
XDOT = -5995
838665 XDOT = -1827
531625
YDOT = -17640
632054 feet/sec YDOT = -5376
864650 meter/sec
ZDOT = -15555
743578 ZDOT = -4741
390642
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 10122
89975298
00016717 00000-0 10270-3 0 9145
2 25544 51
6445 102
9901 0008500 295
6803 64
3481 15
73684819 16347
Satellite: ISS
Catalog Number: 25544
Epoch time: 10122
89975298 = yrday
fracday
Element set: 914
Inclination: 51
6445 deg
RA of node: 102
9901 deg
Eccentricity:
0008500
Arg of perigee: 295
6803 deg
Mean anomaly: 64
3481 deg
Mean motion: 15
73684819 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1634
Checksum: 326
Coasting Arc #16 (Orbit 1649)
---------------------------------------
Vector Time (GMT): 2010/123/20:59:37
579
Vector Time (MET): N/A
Weight (LBS) : 796736
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2752102
23 A = 6725299
04 meter
Y = -4472460
53 meter E =
0007311
Z = 4204075
10 I = 51
97446
XDOT = 3621
982841 Wp = 18
42516
YDOT = -5702
991618 meter/sec RA = 97
15316 deg
ZDOT = -3687
506836 TA = 109
07349
MA = 108
99430
Ha = 189
917 n
mi
Hp = 186
834
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9029206
79 X = -2722308
54
Y = -14673426
93 feet Y = -4503069
89 meter
Z = 13792897
32 Z = 4190777
39
XDOT = 11883
145804 XDOT = 3703
398833
YDOT = -18710
602421 feet/sec YDOT = -5662
032964 meter/sec
ZDOT = -12098
119541 ZDOT = -3669
713825
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8006482
37 X = 2440375
83
Y = 15303344
25 feet Y = 4664459
33 meter
Z = 13739866
97 Z = 4187911
45
XDOT = -12182
054394 XDOT = -3713
090179
YDOT = 17197
219902 feet/sec YDOT = 5241
712626 meter/sec
ZDOT = -12027
366558 ZDOT = -3665
941327
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 10123
91577649
00016717 00000-0 10270-3 0 9158
2 25544 51
6451 97
7744 0008589 299
0471 60
9831 15
73739611 16506
Satellite: ISS
Catalog Number: 25544
Epoch time: 10123
91577649 = yrday
fracday
Element set: 915
Inclination: 51
6451 deg
RA of node: 97
7744 deg
Eccentricity:
0008589
Arg of perigee: 299
0471 deg
Mean anomaly: 60
9831 deg
Mean motion: 15
73739611 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1650
Checksum: 338
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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