Date:
December 21st 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 86 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 17 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
363/07:06:12
689 -11
9 12
1 12
1
N/A -1
0 -0
0 186
4
000/00:02:25
377 2
1 0
0 183
5
Coasting Arc #1 (Orbit 4001)
---------------------------------------
Vector Time (GMT): 2007/353/12:14:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3189644
09 A = 6709254
05 meter
Y = -2714864
67 meter E =
0002293
Z = 5239640
61 I = 51
38104
XDOT = 5130
777676 Wp = 51
87085
YDOT = 5752
103970 meter/sec RA = 227
42708 deg
ZDOT = -141
542250 TA = 39
48403
MA = 39
46732
Ha = 183
990 n
mi
Hp = 178
119
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10464711
58 X = 3194311
46
Y = -8907036
33 feet Y = -2679170
69 meter
Z = 17190421
96 Z = 5255147
20
XDOT = 16833
260092 XDOT = 5066
763038
YDOT = 18871
732185 feet/sec YDOT = 5809
121327 meter/sec
ZDOT = -464
377460 ZDOT = -116
771490
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8992790
72 X = 2741002
61
Y = 10293170
09 feet Y = 3137358
24 meter
Z = 17249245
10 Z = 5257569
91
XDOT = -17980
731700 XDOT = -5480
527022
YDOT = 16335
932375 feet/sec YDOT = 4979
192188 meter/sec
ZDOT = -369
315299 ZDOT = -112
567303
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 07353
55705719
00020000 00000-0 20000-3 0 9006
2 25544 51
6402 228
1000 0001327 334
4721 25
6378 15
77812589 40020
Satellite: ISS
Catalog Number: 25544
Epoch time: 07353
55705719 = yrday
fracday
Element set: 900
Inclination: 51
6402 deg
RA of node: 228
1000 deg
Eccentricity:
0001327
Arg of perigee: 334
4721 deg
Mean anomaly: 25
6378 deg
Mean motion: 15
77812589 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4002
Checksum: 268
Coasting Arc #2 (Orbit 4017)
---------------------------------------
Vector Time (GMT): 2007/354/12:14:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4052828
36 A = 6720431
95 meter
Y = -5170279
55 meter E =
0014216
Z = 1381179
94 I = 51
43912
XDOT = 4623
654200 Wp = 54
58929
YDOT = -2061
963638 meter/sec RA = 222
25981 deg
ZDOT = 5814
856783 TA = 320
66600
MA = 320
76917
Ha = 184
027 n
mi
Hp = 178
079
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13296680
97 X = -4001421
92
Y = -16962859
40 feet Y = -5215313
32 meter
Z = 4531430
26 Z = 1361615
19
XDOT = 15169
469160 XDOT = 4618
119773
YDOT = -6764
972566 feet/sec YDOT = -2010
291004 meter/sec
ZDOT = 19077
614117 ZDOT = 5837
305153
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16617615
20 X = 5065049
11
Y = -13750296
88 feet Y = -4191090
49 meter
Z = 4456274
80 Z = 1358272
56
XDOT = 6144
157952 XDOT = 1872
739344
YDOT = 13672
301177 feet/sec YDOT = 4167
317399 meter/sec
ZDOT = 19162
981674 ZDOT = 5840
876814
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 07354
57042956
00020000 00000-0 20000-3 0 9017
2 25544 51
6396 222
8657 0001432 334
8154 25
2941 15
77856004 40181
Satellite: ISS
Catalog Number: 25544
Epoch time: 07354
57042956 = yrday
fracday
Element set: 901
Inclination: 51
6396 deg
RA of node: 222
8657 deg
Eccentricity:
0001432
Arg of perigee: 334
8154 deg
Mean anomaly: 25
2941 deg
Mean motion: 15
77856004 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4018
Checksum: 290
Coasting Arc #3 (Orbit 4032)
---------------------------------------
Vector Time (GMT): 2007/355/12:14:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4833892
72 A = 6711891
41 meter
Y = 920661
38 meter E =
0009622
Z = -4573710
59 I = 51
43235
XDOT = -3927
488893 Wp = 103
71747
YDOT = -5922
922222 meter/sec RA = 217
04398 deg
ZDOT = 2961
614316 TA = 195
73842
MA = 195
76835
Ha = 183
966 n
mi
Hp = 177
870
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15859228
07 X = -4821609
84
Y = 3020542
58 feet Y = 866675
46 meter
Z = -15005612
18 Z = -4597164
01
XDOT = -12885
462249 XDOT = -3875
353169
YDOT = -19432
159521 feet/sec YDOT = -5966
550600 meter/sec
ZDOT = 9716
582402 ZDOT = 2942
659981
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3691224
32 X = -1125085
17
Y = -15630887
84 feet Y = -4764294
61 meter
Z = -15094946
10 Z = -4600939
57
XDOT = 17722
159417 XDOT = 5401
714190
YDOT = -13488
783791 feet/sec YDOT = -4111
381299 meter/sec
ZDOT = 9643
667991 ZDOT = 2939
390004
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 07355
52044209
00020000 00000-0 20000-3 0 9027
2 25544 51
6386 217
9584 0001485 337
0666 23
0433 15
77890132 40334
Satellite: ISS
Catalog Number: 25544
Epoch time: 07355
52044209 = yrday
fracday
Element set: 902
Inclination: 51
6386 deg
RA of node: 217
9584 deg
Eccentricity:
0001485
Arg of perigee: 337
0666 deg
Mean anomaly: 23
0433 deg
Mean motion: 15
77890132 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4033
Checksum: 283
Coasting Arc #4 (Orbit 4048)
---------------------------------------
Vector Time (GMT): 2007/356/12:14:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2579596
94 A = 6715329
72 meter
Y = 5022789
51 meter E =
0005452
Z = -3641274
28 I = 51
46678
XDOT = -6356
722408 Wp = 64
71392
YDOT = 117
124478 meter/sec RA = 211
91418 deg
ZDOT = -4344
506546 TA = 159
13990
MA = 159
11764
Ha = 183
967 n
mi
Hp = 177
996
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8463244
56 X = 2540928
44
Y = 16478968
22 feet Y = 5051420
50 meter
Z = -11946437
93 Z = -3628835
46
XDOT = -20855
388477 XDOT = -6336
454638
YDOT = 384
266661 feet/sec YDOT = 46
154144 meter/sec
ZDOT = -14253
630399 ZDOT = -4375
338553
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15938647
28 X = -4858099
69
Y = 9501917
27 feet Y = 2896184
38 meter
Z = -11898460
92 Z = -3626650
89
XDOT = -934
490436 XDOT = -284
832685
YDOT = -19552
006002 feet/sec YDOT = -5959
451429 meter/sec
ZDOT = -14371
203724 ZDOT = -4380
342895
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 07356
53376209
00020000 00000-0 20000-3 0 9038
2 25544 51
6374 212
7244 0001519 337
5645 22
5445 15
77910647 40495
Satellite: ISS
Catalog Number: 25544
Epoch time: 07356
53376209 = yrday
fracday
Element set: 903
Inclination: 51
6374 deg
RA of node: 212
7244 deg
Eccentricity:
0001519
Arg of perigee: 337
5645 deg
Mean anomaly: 22
5445 deg
Mean motion: 15
77910647 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4049
Checksum: 295
Coasting Arc #5 (Orbit 4064)
---------------------------------------
Vector Time (GMT): 2007/357/12:14:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6090391
82 A = 6717404
48 meter
Y = 608120
14 meter E =
0012863
Z = 2755730
19 I = 51
50042
XDOT = 1785
565097 Wp = 93
44157
YDOT = 5467
239729 meter/sec RA = 206
68718 deg
ZDOT = -5132
978388 TA = 54
91860
MA = 54
79805
Ha = 183
812 n
mi
Hp = 177
758
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19981600
46 X = 6069752
21
Y = 1995144
81 feet Y = 676110
40 meter
Z = 9041109
55 Z = 2785267
37
XDOT = 5858
153204 XDOT = 1749
232015
YDOT = 17937
138220 feet/sec YDOT = 5487
004813 meter/sec
ZDOT = -16840
480277 ZDOT = -5124
391247
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -453925
82 X = -138356
59
Y = 20024679
15 feet Y = 6103522
20 meter
Z = 9153840
62 Z = 2790090
62
XDOT = -15964
997071 XDOT = -4866
131107
YDOT = 7350
369685 feet/sec YDOT = 2240
392680 meter/sec
ZDOT = -16807
140021 ZDOT = -5122
816278
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 07357
54705416
00020000 00000-0 20000-3 0 9047
2 25544 51
6375 207
4895 0001720 342
4112 17
6993 15
78005823 40650
Satellite: ISS
Catalog Number: 25544
Epoch time: 07357
54705416 = yrday
fracday
Element set: 904
Inclination: 51
6375 deg
RA of node: 207
4895 deg
Eccentricity:
0001720
Arg of perigee: 342
4112 deg
Mean anomaly: 17
6993 deg
Mean motion: 15
78005823 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4065
Checksum: 289
Coasting Arc #6 (Orbit 4080)
---------------------------------------
Vector Time (GMT): 2007/358/12:14:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -375299
26 A = 6709912
52 meter
Y = -4437725
66 meter E =
0004466
Z = 5015686
46 I = 51
49968
XDOT = 7372
263040 Wp = 111
14482
YDOT = 1390
101187 meter/sec RA = 201
54888 deg
ZDOT = 1778
696141 TA = 321
69504
MA = 321
72675
Ha = 183
990 n
mi
Hp = 177
778
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1231296
79 X = -350013
21
Y = -14559467
39 feet Y = -4441782
07 meter
Z = 16455664
24 Z = 5013923
81
XDOT = 24187
214697 XDOT = 7347
530259
YDOT = 4560
699432 feet/sec YDOT = 1472
403374 meter/sec
ZDOT = 5835
617259 ZDOT = 1814
450605
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14370035
69 X = 4379986
88
Y = -2689464
98 feet Y = -819748
93 meter
Z = 16448462
56 Z = 5013491
39
XDOT = -2461
922846 XDOT = -750
394083
YDOT = 23428
130684 feet/sec YDOT = 7140
894232 meter/sec
ZDOT = 5972
170326 ZDOT = 1820
317515
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 07358
56032253
00020000 00000-0 20000-3 0 9053
2 25544 51
6360 202
2538 0001600 349
1456 10
9674 15
77966650 40816
Satellite: ISS
Catalog Number: 25544
Epoch time: 07358
56032253 = yrday
fracday
Element set: 905
Inclination: 51
6360 deg
RA of node: 202
2538 deg
Eccentricity:
0001600
Arg of perigee: 349
1456 deg
Mean anomaly: 10
9674 deg
Mean motion: 15
77966650 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4081
Checksum: 281
Coasting Arc #7 (Orbit 4095)
---------------------------------------
Vector Time (GMT): 2007/359/12:14:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6487422
86 A = 6720699
94 meter
Y = -1714777
66 meter E =
0012729
Z = -228782
50 I = 51
56336
XDOT = 1032
550879 Wp = 37
31767
YDOT = -4686
697502 meter/sec RA = 196
35653 deg
ZDOT = 6032
767116 TA = 320
18908
MA = 320
28240
Ha = 183
848 n
mi
Hp = 177
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21284195
73 X = -6466654
42
Y = -5625910
95 feet Y = -1787207
53 meter
Z = -750598
76 Z = -260247
90
XDOT = 3387
634116 XDOT = 1055
575753
YDOT = -15376
304141 feet/sec YDOT = -4675
023263 meter/sec
ZDOT = 19792
543032 ZDOT = 6037
838288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3222894
12 X = 982338
13
Y = -21773512
45 feet Y = -6636566
59 meter
Z = -870844
15 Z = -265433
30
XDOT = 14057
563419 XDOT = 4284
745330
YDOT = 1309
252152 feet/sec YDOT = 399
060056 meter/sec
ZDOT = 19811
384770 ZDOT = 6038
510078
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 07359
51023344
00020000 00000-0 20000-3 0 9061
2 25544 51
6349 197
3451 0001626 347
4534 12
6590 15
78030059 40965
Satellite: ISS
Catalog Number: 25544
Epoch time: 07359
51023344 = yrday
fracday
Element set: 906
Inclination: 51
6349 deg
RA of node: 197
3451 deg
Eccentricity:
0001626
Arg of perigee: 347
4534 deg
Mean anomaly: 12
6590 deg
Mean motion: 15
78030059 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4096
Checksum: 288
Coasting Arc #8 (Orbit 4111)
---------------------------------------
Vector Time (GMT): 2007/360/12:14:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2212517
88 A = 6708995
38 meter
Y = 3720782
73 meter E =
0013925
Z = -5137626
46 I = 51
55212
XDOT = -7172
928382 Wp = 93
92284
YDOT = -2470
570693 meter/sec RA = 191
17465 deg
ZDOT = 1301
861826 TA = 188
53689
MA = 188
56060
Ha = 183
846 n
mi
Hp = 177
451
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7258916
93 X = -2229002
51
Y = 12207292
43 feet Y = 3695949
70 meter
Z = -16855729
87 Z = -5148414
20
XDOT = -23533
229599 XDOT = -7151
093094
YDOT = -8105
546894 feet/sec YDOT = -2550
660554 meter/sec
ZDOT = 4271
200215 ZDOT = 1267
068914
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13025818
02 X = -3970269
33
Y = -5537343
67 feet Y = -1687782
35 meter
Z = -16896490
25 Z = -5150050
23
XDOT = 4610
885289 XDOT = 1405
397836
YDOT = -23452
696353 feet/sec YDOT = -7148
381848 meter/sec
ZDOT = 4138
155659 ZDOT = 1261
309845
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 07360
52344740
00020000 00000-0 20000-3 0 9071
2 25544 51
6343 192
1087 0001542 354
3409 5
7738 15
78090211 41124
Satellite: ISS
Catalog Number: 25544
Epoch time: 07360
52344740 = yrday
fracday
Element set: 907
Inclination: 51
6343 deg
RA of node: 192
1087 deg
Eccentricity:
0001542
Arg of perigee: 354
3409 deg
Mean anomaly: 5
7738 deg
Mean motion: 15
78090211 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4112
Checksum: 267
Coasting Arc #9 (Orbit 4127)
---------------------------------------
Vector Time (GMT): 2007/361/12:14:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5717150
24 A = 6717887
64 meter
Y = 2548059
68 meter E =
0004500
Z = -2439496
12 I = 51
61169
XDOT = -3991
732423 Wp = 118
21998
YDOT = 3841
616200 meter/sec RA = 186
03644 deg
ZDOT = -5351
904515 TA = 89
37965
MA = 89
32809
Ha = 183
842 n
mi
Hp = 177
462
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18757054
58 X = 5700082
99
Y = 8359775
85 feet Y = 2611896
96 meter
Z = -8003596
20 Z = -2411763
77
XDOT = -13096
234985 XDOT = -4008
395096
YDOT = 12603
727691 feet/sec YDOT = 3796
885864 meter/sec
ZDOT = -17558
741847 ZDOT = -5371
336072
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5537088
14 X = -1687704
46
Y = 19817696
26 feet Y = 6040433
82 meter
Z = -7897472
45 Z = -2407149
60
XDOT = -12914
400905 XDOT = -3936
309396
YDOT = -10622
302920 feet/sec YDOT = -3237
677930 meter/sec
ZDOT = -17632
479389 ZDOT = -5374
379718
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 07361
53663386
00020000 00000-0 20000-3 0 9084
2 25544 51
6346 186
8736 0001690 358
1759 1
9400 15
78140080 41283
Satellite: ISS
Catalog Number: 25544
Epoch time: 07361
53663386 = yrday
fracday
Element set: 908
Inclination: 51
6346 deg
RA of node: 186
8736 deg
Eccentricity:
0001690
Arg of perigee: 358
1759 deg
Mean anomaly: 1
9400 deg
Mean motion: 15
78140080 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4128
Checksum: 299
Coasting Arc #10 (Orbit 4143)
---------------------------------------
Vector Time (GMT): 2007/362/12:14:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4602923
33 A = 6713752
01 meter
Y = -2990268
55 meter E =
0011551
Z = 3859231
53 I = 51
62740
XDOT = 5614
258292 Wp = 72
84052
YDOT = 3329
427466 meter/sec RA = 180
81937 deg
ZDOT = -4102
997667 TA = 59
96801
MA = 59
85347
Ha = 183
701 n
mi
Hp = 177
369
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15101454
51 X = 4617271
67
Y = -9810592
36 feet Y = -2938716
20 meter
Z = 12661520
78 Z = 3881626
81
XDOT = 18419
482584 XDOT = 5596
542223
YDOT = 10923
318458 feet/sec YDOT = 3392
110633 meter/sec
ZDOT = -13461
278434 ZDOT = -4075
766660
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12121150
91 X = 3694526
80
Y = 13236913
69 feet Y = 4034611
29 meter
Z = 12746669
21 Z = 3885184
78
XDOT = -6809
449577 XDOT = -2075
520231
YDOT = 19139
788803 feet/sec YDOT = 5833
807627 meter/sec
ZDOT = -13356
969305 ZDOT = -4071
204244
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 07362
54979305
00020000 00000-0 20000-3 0 9098
2 25544 51
6347 181
6370 0001594 357
5278 2
5880 15
78164879 41442
Satellite: ISS
Catalog Number: 25544
Epoch time: 07362
54979305 = yrday
fracday
Element set: 909
Inclination: 51
6347 deg
RA of node: 181
6370 deg
Eccentricity:
0001594
Arg of perigee: 357
5278 deg
Mean anomaly: 2
5880 deg
Mean motion: 15
78164879 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4144
Checksum: 322
Coasting Arc #11 (Orbit 4155)
---------------------------------------
Vector Time (GMT): 2007/363/07:07:25
377
Vector Time (MET): N/A
Weight (LBS) : 538460
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1801528
90 A = 6715606
02 meter
Y = 4082559
49 meter E =
0003900
Z = -5021667
55 I = 51
63965
XDOT = -7411
256012 Wp = 77
95788
YDOT = -1028
086389 meter/sec RA = 176
76723 deg
ZDOT = 1824
960204 TA = 209
62067
MA = 209
64277
Ha = 186
444 n
mi
Hp = 183
548
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5910527
87 X = -1822652
71
Y = 13394224
05 feet Y = 4062296
09 meter
Z = -16475287
25 Z = -5030470
25
XDOT = -24315
144397 XDOT = -7408
074207
YDOT = -3372
986841 feet/sec YDOT = -1110
945626 meter/sec
ZDOT = 5987
402245 ZDOT = 1788
964339
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -408
81 X = -124
61
Y = -14602955
61 feet Y = -4450980
87 meter
Z = -16508432
85 Z = -5031770
33
XDOT = 22611
811704 XDOT = 6892
080207
YDOT = -6606
491790 feet/sec YDOT = -2013
658698 meter/sec
ZDOT = 5849
885202 ZDOT = 1783
045010
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 07363
30964631
00020000 00000-0 20000-3 0 9101
2 25544 51
6390 177
7143 0010047 293
1615 66
8491 15
75945283 41564
Satellite: ISS
Catalog Number: 25544
Epoch time: 07363
30964631 = yrday
fracday
Element set: 910
Inclination: 51
6390 deg
RA of node: 177
7143 deg
Eccentricity:
0010047
Arg of perigee: 293
1615 deg
Mean anomaly: 66
8491 deg
Mean motion: 15
75945283 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4156
Checksum: 297
Coasting Arc #12 (Orbit 4171)
---------------------------------------
Vector Time (GMT): 2007/364/07:07:25
377
Vector Time (MET): N/A
Weight (LBS) : 538460
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6290892
26 A = 6724587
67 meter
Y = 845859
02 meter E =
0004937
Z = -2215856
96 I = 51
69885
XDOT = -2574
354806 Wp = 269
31040
YDOT = 4754
648583 meter/sec RA = 171
65378 deg
ZDOT = -5483
280601 TA = 295
52298
MA = 295
57403
Ha = 186
677 n
mi
Hp = 183
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20639410
29 X = 6291730
34
Y = 2775128
03 feet Y = 916212
21 meter
Z = -7269871
91 Z = -2185293
91
XDOT = -8446
045951 XDOT = -2600
694076
YDOT = 15599
240759 feet/sec YDOT = 4725
713845 meter/sec
ZDOT = -17989
765750 ZDOT = -5495
850338
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19972852
92 X = -6087725
57
Y = 6037869
86 feet Y = 1840342
73 meter
Z = -7153104
51 Z = -2180266
25
XDOT = 1575
635550 XDOT = 480
253716
YDOT = -16197
831164 feet/sec YDOT = -4937
098939 meter/sec
ZDOT = -18037
218509 ZDOT = -5497
744202
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 07364
32422105
00020000 00000-0 20000-3 0 9110
2 25544 51
6392 172
4889 0010140 296
4363 63
5760 15
75941316 41729
Satellite: ISS
Catalog Number: 25544
Epoch time: 07364
32422105 = yrday
fracday
Element set: 911
Inclination: 51
6392 deg
RA of node: 172
4889 deg
Eccentricity:
0010140
Arg of perigee: 296
4363 deg
Mean anomaly: 63
5760 deg
Mean motion: 15
75941316 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4172
Checksum: 281
Coasting Arc #13 (Orbit 4187)
---------------------------------------
Vector Time (GMT): 2007/365/07:07:25
377
Vector Time (MET): N/A
Weight (LBS) : 538460
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2668927
00 A = 6717639
50 meter
Y = -4263189
83 meter E =
0008833
Z = 4458053
76 I = 51
70525
XDOT = 6925
300942 Wp = 357
45914
YDOT = 953
013805 meter/sec RA = 166
46406 deg
ZDOT = -3226
232343 TA = 124
85315
MA = 124
77006
Ha = 186
809 n
mi
Hp = 182
887
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8756322
17 X = 2694743
93
Y = -13986843
27 feet Y = -4233200
38 meter
Z = 14626160
65 Z = 4471081
74
XDOT = 22720
803614 XDOT = 6929
801896
YDOT = 3126
685713 feet/sec YDOT = 1030
481880 meter/sec
ZDOT = -10584
751782 ZDOT = -3192
578324
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1821687
67 X = -555250
40
Y = 16356740
84 feet Y = 4985534
61 meter
Z = 14675422
34 Z = 4473068
73
XDOT = -20720
674618 XDOT = -6315
661624
YDOT = 7098
355140 feet/sec YDOT = 2163
578647 meter/sec
ZDOT = -10456
163771 ZDOT = -3187
038717
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 07365
33877018
00020000 00000-0 20000-3 0 9120
2 25544 51
6392 167
2628 0010286 301
7961 58
2201 15
76049910 41885
Satellite: ISS
Catalog Number: 25544
Epoch time: 07365
33877018 = yrday
fracday
Element set: 912
Inclination: 51
6392 deg
RA of node: 167
2628 deg
Eccentricity:
0010286
Arg of perigee: 301
7961 deg
Mean anomaly: 58
2201 deg
Mean motion: 15
76049910 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4188
Checksum: 297
INTERNATIONAL SPACE STATION ORBITAL DATA:
The 2-Line Elements (TLEs) and vectors are obtained from various sources at different times depending upon availability These sources include:
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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