Date:
October 21st 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5543 41 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 ET - UTC (sec) : 65 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 824)
---------------------------------------
Vector Time (GMT): 2008/294/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 489087
05 A = 6736329
21 meter
Y = 6625781
49 meter E =
0006633
Z = -1089848
60 I = 51
98663
XDOT = -4718
756999 Wp = 21
67573
YDOT = 1321
673336 meter/sec RA = 93
14528 deg
ZDOT = 5934
962525 TA = 326
46776
MA = 326
50973
Ha = 191
510 n
mi
Hp = 187
565
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1604616
30 X = 420254
50
Y = 21738128
24 feet Y = 6630865
91 meter
Z = -3575618
77 Z = -1087639
56
XDOT = -15481
486216 XDOT = -4762
016861
YDOT = 4336
198609 feet/sec YDOT = 1268
663399 meter/sec
ZDOT = 19471
661829 ZDOT = 5911
933423
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11820971
56 X = -3603032
13
Y = -18315320
58 feet Y = -5582509
71 meter
Z = -3566472
45 Z = -1087060
80
XDOT = 10286
164351 XDOT = 3135
222894
YDOT = -10401
974501 feet/sec YDOT = -3170
521828 meter/sec
ZDOT = 19382
537086 ZDOT = 5907
797304
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 08294
50210186
00020000 00000-0 20000-3 0 9005
2 25544 51
6399 93
9127 0003717 247
9897 112
0871 15
72360532 8259
Satellite: ISS
Catalog Number: 25544
Epoch time: 08294
50210186 = yrday
fracday
Element set: 900
Inclination: 51
6399 deg
RA of node: 93
9127 deg
Eccentricity:
0003717
Arg of perigee: 247
9897 deg
Mean anomaly: 112
0871 deg
Mean motion: 15
72360532 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 825
Checksum: 296
Coasting Arc #2 (Orbit 840)
---------------------------------------
Vector Time (GMT): 2008/295/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3887332
11 A = 6725771
66 meter
Y = -2154300
80 meter E =
0009757
Z = -5056835
24 I = 51
95220
XDOT = 1670
281553 Wp = 77
76939
YDOT = 7283
416957 meter/sec RA = 88
07140 deg
ZDOT = -1819
786122 TA = 174
75013
MA = 174
73989
Ha = 191
432 n
mi
Hp = 187
605
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12753714
26 X = 3935698
40
Y = -7067916
00 feet Y = -2110559
91 meter
Z = -16590666
79 Z = -5037832
91
XDOT = 5479
926355 XDOT = 1597
553358
YDOT = 23895
724925 feet/sec YDOT = 7301
688389 meter/sec
ZDOT = -5970
426909 ZDOT = -1811
848368
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7691766
41 X = -2344450
40
Y = 12485242
68 feet Y = 3805501
97 meter
Z = -16517213
25 Z = -5034446
60
XDOT = -15671
042210 XDOT = -4776
533666
YDOT = -17507
415461 feet/sec YDOT = -5336
260233 meter/sec
ZDOT = -5939
024648 ZDOT = -1810
214713
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 08295
51898991
00020000 00000-0 20000-3 0 9014
2 25544 51
6404 88
7041 0003580 252
7318 107
3453 15
72392629 8416
Satellite: ISS
Catalog Number: 25544
Epoch time: 08295
51898991 = yrday
fracday
Element set: 901
Inclination: 51
6404 deg
RA of node: 88
7041 deg
Eccentricity:
0003580
Arg of perigee: 252
7318 deg
Mean anomaly: 107
3453 deg
Mean motion: 15
72392629 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 841
Checksum: 302
Coasting Arc #3 (Orbit 856)
---------------------------------------
Vector Time (GMT): 2008/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2373659
25 A = 6734926
66 meter
Y = -5943391
53 meter E =
0011159
Z = 2078156
17 I = 51
97992
XDOT = 3957
048089 Wp = 121
34707
YDOT = -3536
744585 meter/sec RA = 82
93666 deg
ZDOT = -5578
969843 TA = 35
57164
MA = 35
49730
Ha = 191
356 n
mi
Hp = 187
602
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7787595
95 X = -2317118
27
Y = -19499316
05 feet Y = -5969619
00 meter
Z = 6818097
68 Z = 2066762
23
XDOT = 12982
441236 XDOT = 4023
404351
YDOT = -11603
492733 feet/sec YDOT = -3492
123635 meter/sec
ZDOT = -18303
706835 ZDOT = -5559
585083
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16647991
24 X = 5074307
73
Y = 12818799
31 feet Y = 3907170
03 meter
Z = 6773419
00 Z = 2064538
11
XDOT = -4442
230041 XDOT = -1353
991717
YDOT = 15429
510755 feet/sec YDOT = 4702
914878 meter/sec
ZDOT = -18228
887196 ZDOT = -5556
164817
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 08296
53586660
00020000 00000-0 20000-3 0 9025
2 25544 51
6396 83
4932 0003734 257
1835 102
8910 15
72386674 8579
Satellite: ISS
Catalog Number: 25544
Epoch time: 08296
53586660 = yrday
fracday
Element set: 902
Inclination: 51
6396 deg
RA of node: 83
4932 deg
Eccentricity:
0003734
Arg of perigee: 257
1835 deg
Mean anomaly: 102
8910 deg
Mean motion: 15
72386674 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 857
Checksum: 316
Coasting Arc #4 (Orbit 872)
---------------------------------------
Vector Time (GMT): 2008/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2873614
23 A = 6727333
39 meter
Y = 3927509
00 meter E =
0005546
Z = 4643623
30 I = 51
95102
XDOT = -3647
588853 Wp = 138
85589
YDOT = -6121
198747 meter/sec RA = 77
87625 deg
ZDOT = 2913
943112 TA = 282
38442
MA = 282
44648
Ha = 191
256 n
mi
Hp = 187
543
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9427868
21 X = -2939876
85
Y = 12885528
22 feet Y = 3895004
25 meter
Z = 15234984
59 Z = 4629502
03
XDOT = -11967
155030 XDOT = -3593
025096
YDOT = -20082
673056 feet/sec YDOT = -6161
683013 meter/sec
ZDOT = 9560
180815 ZDOT = 2896
355662
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1374600
65 X = 418978
28
Y = -15958893
62 feet Y = -4864270
77 meter
Z = 15180595
49 Z = 4627045
50
XDOT = 19583
497283 XDOT = 5969
049972
YDOT = 10734
311977 feet/sec YDOT = 3271
818290 meter/sec
ZDOT = 9491
483557 ZDOT = 2893
004188
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 08297
55273154
00020000 00000-0 20000-3 0 9030
2 25544 51
6406 78
2833 0003778 261
3084 98
7650 15
72437694 8735
Satellite: ISS
Catalog Number: 25544
Epoch time: 08297
55273154 = yrday
fracday
Element set: 903
Inclination: 51
6406 deg
RA of node: 78
2833 deg
Eccentricity:
0003778
Arg of perigee: 261
3084 deg
Mean anomaly: 98
7650 deg
Mean motion: 15
72437694 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 873
Checksum: 317
Coasting Arc #5 (Orbit 887)
---------------------------------------
Vector Time (GMT): 2008/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3882013
08 A = 6732854
29 meter
Y = 4619693
25 meter E =
0001536
Z = -2985323
72 I = 51
96297
XDOT = -2456
256274 Wp = 22
76318
YDOT = 5299
658669 meter/sec RA = 72
72972 deg
ZDOT = 5009
256215 TA = 302
97262
MA = 302
98739
Ha = 191
235 n
mi
Hp = 187
573
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12736263
38 X = 3844568
79
Y = 15156473
92 feet Y = 4662894
65 meter
Z = -9794369
17 Z = -2966555
79
XDOT = -8058
583577 XDOT = -2539
669804
YDOT = 17387
331592 feet/sec YDOT = 5271
725251 meter/sec
ZDOT = 16434
567636 ZDOT = 4997
120660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18933006
48 X = -5770780
38
Y = -5907599
15 feet Y = -1800636
22 meter
Z = -9721229
94 Z = -2963030
89
XDOT = -2899
059233 XDOT = -883
633254
YDOT = -17663
975673 feet/sec YDOT = -5383
979785 meter/sec
ZDOT = 16387
990363 ZDOT = 4995
059463
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 08298
50603389
00020000 00000-0 20000-3 0 9044
2 25544 51
6416 73
3995 0003637 266
0066 94
0680 15
72423525 8883
Satellite: ISS
Catalog Number: 25544
Epoch time: 08298
50603389 = yrday
fracday
Element set: 904
Inclination: 51
6416 deg
RA of node: 73
3995 deg
Eccentricity:
0003637
Arg of perigee: 266
0066 deg
Mean anomaly: 94
0680 deg
Mean motion: 15
72423525 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 888
Checksum: 309
Coasting Arc #6 (Orbit 903)
---------------------------------------
Vector Time (GMT): 2008/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1324089
31 A = 6729427
53 meter
Y = -5187787
59 meter E =
0004192
Z = -4081269
69 I = 51
94196
XDOT = 5049
277385 Wp = 53
33072
YDOT = 4329
575435 meter/sec RA = 67
67730 deg
ZDOT = -3865
550478 TA = 177
01626
MA = 177
01376
Ha = 191
166 n
mi
Hp = 187
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4344125
02 X = 1401828
06
Y = -17020300
50 feet Y = -5172546
42 meter
Z = -13389992
43 Z = -4074648
02
XDOT = 16565
870687 XDOT = 5019
266626
YDOT = 14204
643815 feet/sec YDOT = 4385
871362 meter/sec
ZDOT = -12682
252225 ZDOT = -3841
093724
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5705207
87 X = 1738947
36
Y = 16633924
21 feet Y = 5070020
10 meter
Z = -13364771
48 Z = -4073582
35
XDOT = -20501
150296 XDOT = -6248
750610
YDOT = -3080
941612 feet/sec YDOT = -939
071003 meter/sec
ZDOT = -12587
094495 ZDOT = -3836
546402
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 08299
52287765
00020000 00000-0 20000-3 0 9054
2 25544 51
6418 68
1897 0003700 270
7209 89
3530 15
72438824 9048
Satellite: ISS
Catalog Number: 25544
Epoch time: 08299
52287765 = yrday
fracday
Element set: 905
Inclination: 51
6418 deg
RA of node: 68
1897 deg
Eccentricity:
0003700
Arg of perigee: 270
7209 deg
Mean anomaly: 89
3530 deg
Mean motion: 15
72438824 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 904
Checksum: 314
Coasting Arc #7 (Orbit 919)
---------------------------------------
Vector Time (GMT): 2008/300/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4797112
43 A = 6730618
21 meter
Y = -2866397
39 meter E =
0008213
Z = 3745796
55 I = 51
93405
XDOT = 461
672108 Wp = 79
05386
YDOT = -6381
429625 meter/sec RA = 62
52350 deg
ZDOT = -4282
612819 TA = 55
93780
MA = 55
85987
Ha = 191
291 n
mi
Hp = 187
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15738557
82 X = -4782900
24
Y = -9404190
90 feet Y = -2919961
82 meter
Z = 12289358
75 Z = 3722526
25
XDOT = 1514
672270 XDOT = 553
800667
YDOT = -20936
448900 feet/sec YDOT = -6375
752038 meter/sec
ZDOT = -14050
566993 ZDOT = -4280
145852
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18355474
49 X = 5594748
62
Y = -1196669
78 feet Y = -364744
95 meter
Z = 12198929
68 Z = 3718233
77
XDOT = 10449
374522 XDOT = 3184
969354
YDOT = 16823
598962 feet/sec YDOT = 5127
832964 meter/sec
ZDOT = -14041
542414 ZDOT = -4279
862128
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 08300
53971084
00020000 00000-0 20000-3 0 9063
2 25544 51
6424 62
9798 0003603 274
3852 85
6899 15
72440803 9208
Satellite: ISS
Catalog Number: 25544
Epoch time: 08300
53971084 = yrday
fracday
Element set: 906
Inclination: 51
6424 deg
RA of node: 62
9798 deg
Eccentricity:
0003603
Arg of perigee: 274
3852 deg
Mean anomaly: 85
6899 deg
Mean motion: 15
72440803 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 920
Checksum: 303
Coasting Arc #8 (Orbit 935)
---------------------------------------
Vector Time (GMT): 2008/301/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 560802
06 A = 6731465
36 meter
Y = 5793500
17 meter E =
0008948
Z = 3373046
23 I = 51
92434
XDOT = -5724
012847 Wp = 85
86840
YDOT = -2170
781263 meter/sec RA = 57
47102 deg
ZDOT = 4670
249604 TA = 313
69556
MA = 313
76966
Ha = 191
110 n
mi
Hp = 187
386
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1839901
76 X = 479590
38
Y = 19007546
49 feet Y = 5799317
43 meter
Z = 11066424
64 Z = 3375573
20
XDOT = -18779
569707 XDOT = -5722
001295
YDOT = -7121
985772 feet/sec YDOT = -2234
779063 meter/sec
ZDOT = 15322
341220 ZDOT = 4642
446494
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12474560
08 X = -3802245
91
Y = -14450950
43 feet Y = -4404649
69 meter
Z = 11076696
21 Z = 3376177
01
XDOT = 18445
323568 XDOT = 5622
134624
YDOT = -4235
805534 feet/sec YDOT = -1291
073527 meter/sec
ZDOT = 15214
408111 ZDOT = 4637
351592
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 08301
55652985
00020000 00000-0 20000-3 0 9073
2 25544 51
6436 57
7699 0003681 279
3191 80
7555 15
72514065 9364
Satellite: ISS
Catalog Number: 25544
Epoch time: 08301
55652985 = yrday
fracday
Element set: 907
Inclination: 51
6436 deg
RA of node: 57
7699 deg
Eccentricity:
0003681
Arg of perigee: 279
3191 deg
Mean anomaly: 80
7555 deg
Mean motion: 15
72514065 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 936
Checksum: 319
Coasting Arc #9 (Orbit 950)
---------------------------------------
Vector Time (GMT): 2008/302/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5035456
91 A = 6728255
48 meter
Y = 907206
04 meter E =
0005268
Z = -4374648
05 I = 51
89669
XDOT = 1764
458110 Wp = 114
28707
YDOT = 6664
235847 meter/sec RA = 52
31779 deg
ZDOT = 3414
090786 TA = 190
03912
MA = 190
04965
Ha = 191
214 n
mi
Hp = 187
506
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16520527
94 X = 5046190
08
Y = 2976397
78 feet Y = 963575
36 meter
Z = -14352519
83 Z = -4350158
95
XDOT = 5788
904559 XDOT = 1673
220829
YDOT = 21864
290837 feet/sec YDOT = 6683
456967 meter/sec
ZDOT = 11201
085256 ZDOT = 3422
441055
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15123226
01 X = -4609559
29
Y = 7469422
73 feet Y = 2276680
05 meter
Z = -14257537
37 Z = -4345697
39
XDOT = -17049
673822 XDOT = -5196
740581
YDOT = -13083
784520 feet/sec YDOT = -3987
937522 meter/sec
ZDOT = 11233
985302 ZDOT = 3424
118720
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 08302
50979052
00020000 00000-0 20000-3 0 9087
2 25544 51
6439 52
8868 0003720 285
2477 74
8274 15
72500658 9510
Satellite: ISS
Catalog Number: 25544
Epoch time: 08302
50979052 = yrday
fracday
Element set: 908
Inclination: 51
6439 deg
RA of node: 52
8868 deg
Eccentricity:
0003720
Arg of perigee: 285
2477 deg
Mean anomaly: 74
8274 deg
Mean motion: 15
72500658 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 951
Checksum: 309
Coasting Arc #10 (Orbit 966)
---------------------------------------
Vector Time (GMT): 2008/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2500059
68 A = 6733471
05 meter
Y = -5691812
44 meter E =
0001926
Z = -2584691
85 I = 51
89618
XDOT = 5591
730884 Wp = 162
46981
YDOT = -56
965048 meter/sec RA = 47
25800 deg
ZDOT = -5286
004207 TA = 46
73137
MA = 46
71530
Ha = 191
233 n
mi
Hp = 187
311
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8202295
55 X = -2423670
71
Y = -18673925
32 feet Y = -5719342
43 meter
Z = -8479960
13 Z = -2596652
00
XDOT = 18345
573767 XDOT = 5617
631595
YDOT = -186
893202 feet/sec YDOT = 5
709749 meter/sec
ZDOT = -17342
533488 ZDOT = -5258
775754
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17825244
50 X = 5433134
52
Y = 9872074
57 feet Y = 3009008
33 meter
Z = -8526761
69 Z = -2598956
96
XDOT = -13812
597590 XDOT = -4210
079746
YDOT = 10060
219767 feet/sec YDOT = 3066
354985 meter/sec
ZDOT = -17237
011994 ZDOT = -5253
841256
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 08303
52658962
00020000 00000-0 20000-3 0 9095
2 25544 51
6445 47
6770 0003669 289
8194 70
2572 15
72516258 9670
Satellite: ISS
Catalog Number: 25544
Epoch time: 08303
52658962 = yrday
fracday
Element set: 909
Inclination: 51
6445 deg
RA of node: 47
6770 deg
Eccentricity:
0003669
Arg of perigee: 289
8194 deg
Mean anomaly: 70
2572 deg
Mean motion: 15
72516258 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 967
Checksum: 327
Coasting Arc #11 (Orbit 982)
---------------------------------------
Vector Time (GMT): 2008/304/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4579903
74 A = 6726318
33 meter
Y = 972896
85 meter E =
0006015
Z = 4828767
09 I = 51
85174
XDOT = -3915
445780 Wp = 28
60738
YDOT = -6151
826867 meter/sec RA = 42
10946 deg
ZDOT = -2467
756703 TA = 85
48204
MA = 85
41332
Ha = 191
447 n
mi
Hp = 187
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15025930
89 X = -4613900
48
Y = 3191918
81 feet Y = 921491
53 meter
Z = 15842411
71 Z = 4806434
63
XDOT = -12845
950722 XDOT = -3834
375735
YDOT = -20183
159014 feet/sec YDOT = -6195
158303 meter/sec
ZDOT = -8096
314643 ZDOT = -2486
581778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9859981
89 X = 3005322
48
Y = -11894546
60 feet Y = -3625457
81 meter
Z = 15755934
49 Z = 4802408
83
XDOT = 21702
797457 XDOT = 6615
012665
YDOT = 7140
495845 feet/sec YDOT = 2176
423134 meter/sec
ZDOT = -8169
748126 ZDOT = -2490
139229
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 08304
54337729
00020000 00000-0 20000-3 0 9105
2 25544 51
6449 42
4676 0003673 296
9629 63
1158 15
72540804 9832
Satellite: ISS
Catalog Number: 25544
Epoch time: 08304
54337729 = yrday
fracday
Element set: 910
Inclination: 51
6449 deg
RA of node: 42
4676 deg
Eccentricity:
0003673
Arg of perigee: 296
9629 deg
Mean anomaly: 63
1158 deg
Mean motion: 15
72540804 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 983
Checksum: 309
Coasting Arc #12 (Orbit 998)
---------------------------------------
Vector Time (GMT): 2008/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 642288
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4269104
13 A = 6734993
26 meter
Y = 4908741
19 meter E =
0012440
Z = 1715465
50 I = 51
85874
XDOT = -4706
283055 Wp = 50
30777
YDOT = 2084
230091 meter/sec RA = 37
03594 deg
ZDOT = 5728
550089 TA = 328
60934
MA = 328
68353
Ha = 191
406 n
mi
Hp = 187
133
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14006247
14 X = 4205562
82
Y = 16104793
93 feet Y = 4956125
43 meter
Z = 5628167
65 Z = 1736051
30
XDOT = -15440
561204 XDOT = -4757
068588
YDOT = 6838
025234 feet/sec YDOT = 2031
317530 meter/sec
ZDOT = 18794
455671 ZDOT = 5705
562981
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21020518
37 X = -6407054
00
Y = -3573299
49 feet Y = -1089141
68 meter
Z = 5708323
37 Z = 1739896
96
XDOT = 7412
248151 XDOT = 2259
253237
YDOT = -13620
786809 feet/sec YDOT = -4151
615819 meter/sec
ZDOT = 18705
521668 ZDOT = 5701
443004
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 08305
56015335
00020000 00000-0 20000-3 0 9115
2 25544 51
6451 37
2579 0003690 301
3792 58
7009 15
72552892 9992
Satellite: ISS
Catalog Number: 25544
Epoch time: 08305
56015335 = yrday
fracday
Element set: 911
Inclination: 51
6451 deg
RA of node: 37
2579 deg
Eccentricity:
0003690
Arg of perigee: 301
3792 deg
Mean anomaly: 58
7009 deg
Mean motion: 15
72552892 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 999
Checksum: 299
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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