Date:
December 13th 2008
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 5381 96 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) : 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
352/04:03:34
300 1
5 1
7 1
7
N/A -0
8 0
2 196
5
000/00:09:28
600 0
0 0
2 184
8
Coasting Arc #1 (Orbit 1627)
---------------------------------------
Vector Time (GMT): 2008/347/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1125242
84 A = 6726540
28 meter
Y = 4110125
29 meter E =
0020730
Z = -5222462
25 I = 51
60676
XDOT = -7572
349909 Wp = 93
68079
YDOT = -919
869175 meter/sec RA = 181
50546 deg
ZDOT = 909
402897 TA = 184
99607
MA = 185
01679
Ha = 195
679 n
mi
Hp = 184
813
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3691741
59 X = -1145749
17
Y = 13484663
02 feet Y = 4097428
51 meter
Z = -17134062
50 Z = -5227977
78
XDOT = -24843
667679 XDOT = -7565
918759
YDOT = -3017
943487 feet/sec YDOT = -1004
511785 meter/sec
ZDOT = 2983
605304 ZDOT = 872
631350
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12736620
47 X = -3882121
92
Y = -5702645
23 feet Y = -1738166
26 meter
Z = -17155160
35 Z = -5228892
88
XDOT = 6537
592582 XDOT = 1992
658219
YDOT = -23129
446601 feet/sec YDOT = -7049
855324 meter/sec
ZDOT = 2840
720886 ZDOT = 865
851726
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 08347
51446436
00010596 00000-0 82463-4 0 9005
2 25544 51
6363 182
4550 0006179 85
1784 275
0083 15
71833360 16286
Satellite: ISS
Catalog Number: 25544
Epoch time: 08347
51446436 = yrday
fracday
Element set: 900
Inclination: 51
6363 deg
RA of node: 182
4550 deg
Eccentricity:
0006179
Arg of perigee: 85
1784 deg
Mean anomaly: 275
0083 deg
Mean motion: 15
71833360 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1628
Checksum: 311
Coasting Arc #2 (Orbit 1643)
---------------------------------------
Vector Time (GMT): 2008/348/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6723674
32 A = 6738256
92 meter
Y = -329310
44 meter E =
0016832
Z = -119002
47 I = 51
67631
XDOT = 138
274143 Wp = 120
04753
YDOT = 4772
916452 meter/sec RA = 176
39540 deg
ZDOT = -6037
478715 TA = 61
24345
MA = 61
07445
Ha = 195
639 n
mi
Hp = 184
814
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22059298
96 X = 6727435
10
Y = -1080414
84 feet Y = -254101
38 meter
Z = -390428
06 Z = -86329
61
XDOT = 453
655325 XDOT = 114
221470
YDOT = 15659
174711 feet/sec YDOT = 4774
329396 meter/sec
ZDOT = -19808
001034 ZDOT = -6036
864477
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2082377
38 X = -634708
62
Y = 21989239
49 feet Y = 6702320
20 meter
Z = -263537
82 Z = -80326
33
XDOT = -13975
934500 XDOT = -4259
864836
YDOT = -1523
476362 feet/sec YDOT = -464
355595 meter/sec
ZDOT = -19805
240914 ZDOT = -6036
637431
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 08348
53169697
00010596 00000-0 82463-4 0 9010
2 25544 51
6366 177
2477 0006145 87
5031 272
6834 15
71864668 16443
Satellite: ISS
Catalog Number: 25544
Epoch time: 08348
53169697 = yrday
fracday
Element set: 901
Inclination: 51
6366 deg
RA of node: 177
2477 deg
Eccentricity:
0006145
Arg of perigee: 87
5031 deg
Mean anomaly: 272
6834 deg
Mean motion: 15
71864668 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1644
Checksum: 343
Coasting Arc #3 (Orbit 1659)
---------------------------------------
Vector Time (GMT): 2008/349/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1373356
29 A = 6726510
32 meter
Y = -3980056
86 meter E =
0009120
Z = 5238351
01 I = 51
66480
XDOT = 7486
652430 Wp = 101
11529
YDOT = -1689
246597 meter/sec RA = 171
28245 deg
ZDOT = 676
607668 TA = 342
44083
MA = 342
47234
Ha = 195
794 n
mi
Hp = 184
873
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4505762
09 X = -1354195
48
Y = -13057929
32 feet Y = -3995308
31 meter
Z = 17186190
99 Z = 5231725
10
XDOT = 24562
507973 XDOT = 7501
698605
YDOT = -5542
147628 feet/sec YDOT = -1605
442512 meter/sec
ZDOT = 2219
841432 ZDOT = 713
014020
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13533301
02 X = 4124950
15
Y = -2925076
33 feet Y = -891563
26 meter
Z = 17160135
86 Z = 5230409
41
XDOT = 2196
073184 XDOT = 669
363106
YDOT = 24064
678581 feet/sec YDOT = 7334
914031 meter/sec
ZDOT = 2361
151218 ZDOT = 719
678891
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 08349
54892357
00010596 00000-0 82463-4 0 9029
2 25544 51
6359 172
0390 0006251 92
5727 267
6151 15
71810047 16604
Satellite: ISS
Catalog Number: 25544
Epoch time: 08349
54892357 = yrday
fracday
Element set: 902
Inclination: 51
6359 deg
RA of node: 172
0390 deg
Eccentricity:
0006251
Arg of perigee: 92
5727 deg
Mean anomaly: 267
6151 deg
Mean motion: 15
71810047 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1660
Checksum: 313
Coasting Arc #4 (Orbit 1674)
---------------------------------------
Vector Time (GMT): 2008/350/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6100317
69 A = 6737494
59 meter
Y = 2548967
16 meter E =
0013165
Z = -1285852
45 I = 51
73139
XDOT = -2914
262985 Wp = 61
80311
YDOT = -4043
693673 meter/sec RA = 166
14827 deg
ZDOT = 5861
346243 TA = 284
12353
MA = 284
26979
Ha = 195
612 n
mi
Hp = 184
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20014165
66 X = -6122120
87
Y = 8362753
15 feet Y = 2480628
16 meter
Z = -4218676
01 Z = -1315540
20
XDOT = -9561
230267 XDOT = -2897
302336
YDOT = -13266
711524 feet/sec YDOT = -4076
188685 meter/sec
ZDOT = 19230
138592 ZDOT = 5847
229431
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6139594
96 X = -1871348
54
Y = -20780350
59 feet Y = -6333850
86 meter
Z = -4333831
77 Z = -1320951
92
XDOT = 12724
148649 XDOT = 3878
320508
YDOT = -7724
137288 feet/sec YDOT = -2354
317045 meter/sec
ZDOT = 19174
965230 ZDOT = 5844
529402
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 08350
50256269
00010596 00000-0 82463-4 0 9034
2 25544 51
6360 167
1560 0006210 97
0749 263
1119 15
71865210 16752
Satellite: ISS
Catalog Number: 25544
Epoch time: 08350
50256269 = yrday
fracday
Element set: 903
Inclination: 51
6360 deg
RA of node: 167
1560 deg
Eccentricity:
0006210
Arg of perigee: 97
0749 deg
Mean anomaly: 263
1119 deg
Mean motion: 15
71865210 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1675
Checksum: 296
Coasting Arc #5 (Orbit 1690)
---------------------------------------
Vector Time (GMT): 2008/351/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 640390
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3578103
26 A = 6727774
28 meter
Y = 2884408
38 meter E =
0018359
Z = -4929651
38 I = 51
72736
XDOT = -6208
286679 Wp = 83
02843
YDOT = 3959
811328 meter/sec RA = 161
06545 deg
ZDOT = -2194
019872 TA = 165
66868
MA = 165
61653
Ha = 195
661 n
mi
Hp = 184
812
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11739183
94 X = 3569530
60
Y = 9463282
09 feet Y = 2924373
46 meter
Z = -16173396
92 Z = -4912289
55
XDOT = -20368
394617 XDOT = -6241
446444
YDOT = 12991
506981 feet/sec YDOT = 3890
201528 meter/sec
ZDOT = -7198
227925 ZDOT = -2224
259608
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10507331
58 X = -3202634
67
Y = 10915284
94 feet Y = 3326978
85 meter
Z = -16105696
30 Z = -4909016
23
XDOT = -10278
553800 XDOT = -3132
903198
YDOT = -20665
195116 feet/sec YDOT = -6298
751471 meter/sec
ZDOT = -7315
429256 ZDOT = -2229
742837
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 08351
51977119
00010596 00000-0 82463-4 0 9041
2 25544 51
6364 161
9484 0006380 100
3673 259
8208 15
71889180 16916
Satellite: ISS
Catalog Number: 25544
Epoch time: 08351
51977119 = yrday
fracday
Element set: 904
Inclination: 51
6364 deg
RA of node: 161
9484 deg
Eccentricity:
0006380
Arg of perigee: 100
3673 deg
Mean anomaly: 259
8208 deg
Mean motion: 15
71889180 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1691
Checksum: 327
Coasting Arc #6 (Orbit 1701)
---------------------------------------
Vector Time (GMT): 2008/352/04:08:18
600
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -886275
00 A = 6727099
25 meter
Y = -4107613
25 meter E =
0009988
Z = 5244665
41 I = 51
74350
XDOT = 7281
713448 Wp = 87
94099
YDOT = -2428
542574 meter/sec RA = 157
60879 deg
ZDOT = -670
079388 TA = 8
42583
MA = 8
40907
Ha = 196
538 n
mi
Hp = 184
810
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2907726
39 X = -865754
62
Y = -13476421
43 feet Y = -4117409
89 meter
Z = 17206907
51 Z = 5240409
33
XDOT = 23890
135985 XDOT = 7311
583722
YDOT = -7967
659364 feet/sec YDOT = -2346
947158 meter/sec
ZDOT = -2198
423189 ZDOT = -634
632708
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4708693
08 X = -1435209
65
Y = 12979879
06 feet Y = 3956267
14 meter
Z = 17190038
47 Z = 5239523
73
XDOT = -23491
839337 XDOT = -7160
312630
YDOT = -5786
508030 feet/sec YDOT = -1763
727647 meter/sec
ZDOT = -2060
856049 ZDOT = -628
148924
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 08352
21910950
00010596 00000-0 82463-4 0 9050
2 25544 51
6390 158
3717 0007392 96
6179 263
5824 15
71588741 17024
Satellite: ISS
Catalog Number: 25544
Epoch time: 08352
21910950 = yrday
fracday
Element set: 905
Inclination: 51
6390 deg
RA of node: 158
3717 deg
Eccentricity:
0007392
Arg of perigee: 96
6179 deg
Mean anomaly: 263
5824 deg
Mean motion: 15
71588741 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1702
Checksum: 324
Coasting Arc #7 (Orbit 1716)
---------------------------------------
Vector Time (GMT): 2008/353/04:08:18
600
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5888854
72 A = 6739086
08 meter
Y = 3260129
65 meter E =
0017011
Z = -220076
49 I = 51
81040
XDOT = -2468
070471 Wp = 64
93321
YDOT = -4075
082690 meter/sec RA = 152
50442 deg
ZDOT = 6043
828174 TA = 292
68391
MA = 292
86368
Ha = 196
534 n
mi
Hp = 184
858
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19320389
49 X = -5923803
26
Y = 10695963
43 feet Y = 3194081
68 meter
Z = -722035
74 Z = -248769
09
XDOT = -8097
344066 XDOT = -2451
678548
YDOT = -13369
693864 feet/sec YDOT = -4102
590947 meter/sec
ZDOT = 19828
832591 ZDOT = 6031
877783
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22057620
16 X = 6723162
62
Y = 984596
12 feet Y = 300104
90 meter
Z = -833296
41 Z = -253988
74
XDOT = 79
106244 XDOT = 24
111583
YDOT = 14081
287840 feet/sec YDOT = 4291
976534 meter/sec
ZDOT = 19782
058402 ZDOT = 6029
571401
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 08353
17292756
00010596 00000-0 82463-4 0 9064
2 25544 51
6391 153
4907 0007448 99
5795 260
6208 15
71563933 17176
Satellite: ISS
Catalog Number: 25544
Epoch time: 08353
17292756 = yrday
fracday
Element set: 906
Inclination: 51
6391 deg
RA of node: 153
4907 deg
Eccentricity:
0007448
Arg of perigee: 99
5795 deg
Mean anomaly: 260
6208 deg
Mean motion: 15
71563933 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1717
Checksum: 340
Coasting Arc #8 (Orbit 1732)
---------------------------------------
Vector Time (GMT): 2008/354/04:08:18
600
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3257797
42 A = 6727396
97 meter
Y = 2780381
78 meter E =
0021463
Z = -5206323
44 I = 51
79764
XDOT = -5885
307068 Wp = 89
02197
YDOT = 4807
430699 meter/sec RA = 147
41037 deg
ZDOT = -1118
904962 TA = 170
31611
MA = 170
27467
Ha = 196
495 n
mi
Hp = 184
876
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10688311
75 X = 3251756
02
Y = 9121987
46 feet Y = 2816778
99 meter
Z = -17081113
65 Z = -5190511
49
XDOT = -19308
750223 XDOT = -5933
191690
YDOT = 15772
410430 feet/sec YDOT = 4741
350140 meter/sec
ZDOT = -3670
948037 ZDOT = -1147
611756
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4653702
97 X = -1418448
67
Y = -13337808
51 feet Y = -4065364
03 meter
Z = -17019430
66 Z = -5187522
46
XDOT = 23653
972965 XDOT = 7209
730960
YDOT = -3442
109215 feet/sec YDOT = -1049
154889 meter/sec
ZDOT = -3782
150000 ZDOT = -1152
799320
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 08354
19032411
00010596 00000-0 82463-4 0 9078
2 25544 51
6400 148
2841 0007489 103
2504 256
9494 15
71600107 17330
Satellite: ISS
Catalog Number: 25544
Epoch time: 08354
19032411 = yrday
fracday
Element set: 907
Inclination: 51
6400 deg
RA of node: 148
2841 deg
Eccentricity:
0007489
Arg of perigee: 103
2504 deg
Mean anomaly: 256
9494 deg
Mean motion: 15
71600107 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1733
Checksum: 288
Coasting Arc #9 (Orbit 1748)
---------------------------------------
Vector Time (GMT): 2008/355/04:08:18
600
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4203810
43 A = 6737734
47 meter
Y = -4962352
34 meter E =
0021526
Z = 1723426
87 I = 51
85633
XDOT = 4744
000463 Wp = 112
59176
YDOT = 2014
005654 meter/sec RA = 142
28086 deg
ZDOT = -5724
275907 TA = 48
40005
MA = 48
21579
Ha = 196
478 n
mi
Hp = 184
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13792028
97 X = 4250615
69
Y = -16280683
53 feet Y = -4915081
34 meter
Z = 5654287
63 Z = 1743962
37
XDOT = 15564
305980 XDOT = 4748
934577
YDOT = 6607
630100 feet/sec YDOT = 2067
083879 meter/sec
ZDOT = -18780
432766 ZDOT = -5701
217278
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20000096
63 X = -6096029
45
Y = 7373752
49 feet Y = 2247519
76 meter
Z = 5733724
55 Z = 1747639
24
XDOT = -9834
940844 XDOT = -2997
689969
YDOT = -12020
493142 feet/sec YDOT = -3663
846310 meter/sec
ZDOT = -18690
638019 ZDOT = -5696
906468
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 08355
20771237
00010596 00000-0 82463-4 0 9088
2 25544 51
6397 143
0778 0007471 107
2501 252
9479 15
71586904 17493
Satellite: ISS
Catalog Number: 25544
Epoch time: 08355
20771237 = yrday
fracday
Element set: 908
Inclination: 51
6397 deg
RA of node: 143
0778 deg
Eccentricity:
0007471
Arg of perigee: 107
2501 deg
Mean anomaly: 252
9479 deg
Mean motion: 15
71586904 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1749
Checksum: 331
Coasting Arc #10 (Orbit 1764)
---------------------------------------
Vector Time (GMT): 2008/356/04:08:18
600
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4792100
65 A = 6729557
32 meter
Y = -574075
64 meter E =
0015440
Z = 4680407
29 I = 51
85157
XDOT = 3508
278973 Wp = 113
89060
YDOT = -6255
685450 meter/sec RA = 137
21588 deg
ZDOT = 2811
330769 TA = 308
39112
MA = 308
52970
Ha = 196
531 n
mi
Hp = 184
879
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15722114
98 X = -4808061
83
Y = -1883450
27 feet Y = -627753
37 meter
Z = 15355666
95 Z = 4657088
24
XDOT = 11510
101616 XDOT = 3564
313281
YDOT = -20523
902395 feet/sec YDOT = -6216
140805 meter/sec
ZDOT = 9223
526145 ZDOT = 2828
509646
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12983772
33 X = 3957453
81
Y = 9215813
21 feet Y = 2808979
87 meter
Z = 15264967
57 Z = 4652762
12
XDOT = -19205
760528 XDOT = -5853
915809
YDOT = 11597
495076 feet/sec YDOT = 3534
916499 meter/sec
ZDOT = 9289
825030 ZDOT = 2831
538669
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 08356
22509077
00010596 00000-0 82463-4 0 9093
2 25544 51
6399 137
8715 0007418 110
4466 249
7493 15
71617028 17654
Satellite: ISS
Catalog Number: 25544
Epoch time: 08356
22509077 = yrday
fracday
Element set: 909
Inclination: 51
6399 deg
RA of node: 137
8715 deg
Eccentricity:
0007418
Arg of perigee: 110
4466 deg
Mean anomaly: 249
7493 deg
Mean motion: 15
71617028 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1765
Checksum: 337
Coasting Arc #11 (Orbit 1779)
---------------------------------------
Vector Time (GMT): 2008/357/04:08:18
600
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1830887
77 A = 6734644
75 meter
Y = 5685135
12 meter E =
0011313
Z = -3123532
13 I = 51
89037
XDOT = -5878
001618 Wp = 100
02008
YDOT = 786
959207 meter/sec RA = 132
06863 deg
ZDOT = 4890
810744 TA = 223
89570
MA = 223
98564
Ha = 196
313 n
mi
Hp = 184
894
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6006849
63 X = -1879150
11
Y = 18652018
10 feet Y = 5664391
57 meter
Z = -10247808
82 Z = -3132543
27
XDOT = -19284
782210 XDOT = -5910
123557
YDOT = 2581
887163 feet/sec YDOT = 721
047844 meter/sec
ZDOT = 16045
967009 ZDOT = 4862
177197
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13909498
46 X = 4239615
13
Y = -13776628
86 feet Y = -4199116
48 meter
Z = -10282410
06 Z = -3134078
59
XDOT = 17364
797238 XDOT = 5292
790198
YDOT = 5670
928941 feet/sec YDOT = 1728
499141 meter/sec
ZDOT = 15934
702594 ZDOT = 4856
897351
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 08357
17887519
00010596 00000-0 82463-4 0 9100
2 25544 51
6404 132
9903 0007330 113
4857 246
7075 15
71639363 17802
Satellite: ISS
Catalog Number: 25544
Epoch time: 08357
17887519 = yrday
fracday
Element set: 910
Inclination: 51
6404 deg
RA of node: 132
9903 deg
Eccentricity:
0007330
Arg of perigee: 113
4857 deg
Mean anomaly: 246
7075 deg
Mean motion: 15
71639363 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1780
Checksum: 322
Coasting Arc #12 (Orbit 1795)
---------------------------------------
Vector Time (GMT): 2008/358/04:08:18
600
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5207398
43 A = 6732733
28 meter
Y = -1952592
28 meter E =
0012421
Z = -3803664
27 I = 51
90284
XDOT = -675
924454 Wp = 98
78811
YDOT = 6391
442383 meter/sec RA = 127
01910 deg
ZDOT = -4219
900042 TA = 127
04793
MA = 126
93427
Ha = 196
270 n
mi
Hp = 185
103
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17084640
51 X = 5247323
29
Y = -6406142
64 feet Y = -1894136
41 meter
Z = -12479213
47 Z = -3778269
76
XDOT = -2217
599914 XDOT = -726
844672
YDOT = 20969
299157 feet/sec YDOT = 6383
599642 meter/sec
ZDOT = -13844
816411 ZDOT = -4223
306572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18208640
28 X = -5549993
56
Y = -1954498
32 feet Y = -595731
09 meter
Z = -12380619
09 Z = -3773612
70
XDOT = 11159
056127 XDOT = 3401
280307
YDOT = -16464
052145 feet/sec YDOT = -5018
243094 meter/sec
ZDOT = -13857
584679 ZDOT = -4223
791810
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 08358
19623648
00010596 00000-0 82463-4 0 9115
2 25544 51
6407 127
7836 0007167 117
4379 242
7512 15
71639352 17960
Satellite: ISS
Catalog Number: 25544
Epoch time: 08358
19623648 = yrday
fracday
Element set: 911
Inclination: 51
6407 deg
RA of node: 127
7836 deg
Eccentricity:
0007167
Arg of perigee: 117
4379 deg
Mean anomaly: 242
7512 deg
Mean motion: 15
71639352 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1796
Checksum: 335
Coasting Arc #13 (Orbit 1811)
---------------------------------------
Vector Time (GMT): 2008/359/04:08:18
600
Vector Time (MET): N/A
Weight (LBS) : 640263
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -633223
50 A = 6731118
88 meter
Y = -5212150
79 meter E =
0015974
Z = 4197780
64 I = 51
91474
XDOT = 5684
231248 Wp = 92
87599
YDOT = -3669
476849 meter/sec RA = 121
86986 deg
ZDOT = -3687
550857 TA = 34
62212
MA = 34
51823
Ha = 196
163 n
mi
Hp = 184
993
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2077504
92 X = -595285
52
Y = -17100232
25 feet Y = -5219020
36 meter
Z = 13772246
18 Z = 4194795
80
XDOT = 18649
052651 XDOT = 5742
755062
YDOT = -12038
966041 feet/sec YDOT = -3605
584722 meter/sec
ZDOT = -12098
263965 ZDOT = -3659
795031
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5448577
82 X = -1660726
52
Y = 16351667
52 feet Y = 4983988
26 meter
Z = 13760258
13 Z = 4194126
68
XDOT = -20891
204082 XDOT = -6367
639004
YDOT = 3160
029116 feet/sec YDOT = 963
176875 meter/sec
ZDOT = -11990
599881 ZDOT = -3654
734844
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 08359
21358883
00010596 00000-0 82463-4 0 9126
2 25544 51
6407 122
5771 0007132 119
9650 240
2221 15
71686887 18126
Satellite: ISS
Catalog Number: 25544
Epoch time: 08359
21358883 = yrday
fracday
Element set: 912
Inclination: 51
6407 deg
RA of node: 122
5771 deg
Eccentricity:
0007132
Arg of perigee: 119
9650 deg
Mean anomaly: 240
2221 deg
Mean motion: 15
71686887 rev/day
Decay rate: 1
05960E-04 rev/day^2
Epoch rev: 1812
Checksum: 312
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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