Date:
December 17th 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 12378 5 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
There are no maneuvers
Coasting Arc #1 (Orbit 3922)
---------------------------------------
Vector Time (GMT): 2007/348/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2446243
61 A = 6713314
71 meter
Y = -4354437
24 meter E =
0007893
Z = 4480895
40 I = 51
32003
XDOT = 4272
062879 Wp = 109
65661
YDOT = 5611
410900 meter/sec RA = 253
41648 deg
ZDOT = 3113
749277 TA = 309
15158
MA = 309
22169
Ha = 184
382 n
mi
Hp = 178
594
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8025733
62 X = 2472986
43
Y = -14286211
43 feet Y = -4326932
99 meter
Z = 14701100
38 Z = 4492843
65
XDOT = 14015
954329 XDOT = 4193
871714
YDOT = 18410
140748 feet/sec YDOT = 5658
745954 meter/sec
ZDOT = 10215
712851 ZDOT = 3134
313699
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13048311
04 X = 3977125
20
Y = 9844910
96 feet Y = 3000728
86 meter
Z = 14746182
45 Z = 4494636
41
XDOT = -19448
187818 XDOT = -5927
807647
YDOT = 10321
897506 feet/sec YDOT = 3146
114360 meter/sec
ZDOT = 10294
678993 ZDOT = 3137
818157
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 07348
55303019
00020000 00000-0 20000-3 0 9007
2 25544 51
6396 253
9353 0001092 320
3366 39
7719 15
77531681 39234
Satellite: ISS
Catalog Number: 25544
Epoch time: 07348
55303019 = yrday
fracday
Element set: 900
Inclination: 51
6396 deg
RA of node: 253
9353 deg
Eccentricity:
0001092
Arg of perigee: 320
3366 deg
Mean anomaly: 39
7719 deg
Mean motion: 15
77531681 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3923
Checksum: 293
Coasting Arc #2 (Orbit 3937)
---------------------------------------
Vector Time (GMT): 2007/349/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3584137
08 A = 6720785
42 meter
Y = -5440882
68 meter E =
0008215
Z = -1633982
22 I = 51
35575
XDOT = 3356
352638 Wp = 29
71081
YDOT = -3923
001331 meter/sec RA = 248
19288 deg
ZDOT = 5720
057813 TA = 312
14229
MA = 312
21206
Ha = 184
327 n
mi
Hp = 178
495
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11758979
94 X = -3515092
34
Y = -17850664
95 feet Y = -5480576
32 meter
Z = -5360834
07 Z = -1651226
80
XDOT = 11011
655636 XDOT = 3372
183801
YDOT = -12870
739275 feet/sec YDOT = -3885
380762 meter/sec
ZDOT = 18766
593876 ZDOT = 5736
401016
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19143054
04 X = 5834802
87
Y = -9473542
45 feet Y = -2887535
74 meter
Z = -5427141
59 Z = -1654192
76
XDOT = 10760
037682 XDOT = 3279
659485
YDOT = 10992
127523 feet/sec YDOT = 3350
400469 meter/sec
ZDOT = 18828
470443 ZDOT = 5738
917791
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 07349
50322444
00020000 00000-0 20000-3 0 9017
2 25544 51
6399 249
0296 0001162 321
0213 39
0868 15
77587907 39382
Satellite: ISS
Catalog Number: 25544
Epoch time: 07349
50322444 = yrday
fracday
Element set: 901
Inclination: 51
6399 deg
RA of node: 249
0296 deg
Eccentricity:
0001162
Arg of perigee: 321
0213 deg
Mean anomaly: 39
0868 deg
Mean motion: 15
77587907 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3938
Checksum: 301
Coasting Arc #3 (Orbit 3953)
---------------------------------------
Vector Time (GMT): 2007/350/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3473045
77 A = 6709810
19 meter
Y = 2399569
26 meter E =
0014364
Z = -5227886
31 I = 51
33150
XDOT = -3837
438080 Wp = 81
94081
YDOT = -6652
535377 meter/sec RA = 243
02841 deg
ZDOT = -503
339979 TA = 183
24970
MA = 183
25904
Ha = 184
286 n
mi
Hp = 178
281
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11394507
13 X = -3474223
82
Y = 7872602
55 feet Y = 2360725
55 meter
Z = -17151857
99 Z = -5244761
06
XDOT = -12590
019946 XDOT = -3760
318070
YDOT = -21825
903469 feet/sec YDOT = -6695
016544 meter/sec
ZDOT = -1651
377883 ZDOT = -521
795535
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6650509
85 X = -2027075
40
Y = -12057429
16 feet Y = -3675104
41 meter
Z = -17215923
35 Z = -5247413
44
XDOT = 22140
469491 XDOT = 6748
415101
YDOT = -9748
893094 feet/sec YDOT = -2971
462615 meter/sec
ZDOT = -1722
442057 ZDOT = -525
000339
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 07350
51673297
00020000 00000-0 20000-3 0 9026
2 25544 51
6402 243
7965 0001210 325
3618 34
7468 15
77649935 39547
Satellite: ISS
Catalog Number: 25544
Epoch time: 07350
51673297 = yrday
fracday
Element set: 902
Inclination: 51
6402 deg
RA of node: 243
7965 deg
Eccentricity:
0001210
Arg of perigee: 325
3618 deg
Mean anomaly: 34
7468 deg
Mean motion: 15
77649935 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3954
Checksum: 305
Coasting Arc #4 (Orbit 3969)
---------------------------------------
Vector Time (GMT): 2007/351/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2995496
53 A = 6721551
13 meter
Y = 5959585
67 meter E =
0009321
Z = -795551
45 I = 51
38559
XDOT = -4643
523036 Wp = 140
99710
YDOT = 1545
452183 meter/sec RA = 237
84785 deg
ZDOT = -5951
943477 TA = 47
72093
MA = 47
64193
Ha = 184
269 n
mi
Hp = 178
426
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9827744
52 X = 2932497
57
Y = 19552446
41 feet Y = 5992730
82 meter
Z = -2610076
95 Z = -781151
81
XDOT = -15234
655629 XDOT = -4631
545756
YDOT = 5070
381177 feet/sec YDOT = 1493
593100 meter/sec
ZDOT = -19527
373611 ZDOT = -5974
472641
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20336588
67 X = -6198592
23
Y = 8098932
82 feet Y = 2468554
72 meter
Z = -2554539
76 Z = -778623
72
XDOT = -3140
951027 XDOT = -957
361873
YDOT = -14025
877542 feet/sec YDOT = -4275
087475 meter/sec
ZDOT = -19613
087320 ZDOT = -5978
069015
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 07351
53021008
00020000 00000-0 20000-3 0 9037
2 25544 51
6402 238
5632 0001146 320
0846 40
0235 15
77648091 39705
Satellite: ISS
Catalog Number: 25544
Epoch time: 07351
53021008 = yrday
fracday
Element set: 903
Inclination: 51
6402 deg
RA of node: 238
5632 deg
Eccentricity:
0001146
Arg of perigee: 320
0846 deg
Mean anomaly: 40
0235 deg
Mean motion: 15
77648091 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3970
Checksum: 254
Coasting Arc #5 (Orbit 3985)
---------------------------------------
Vector Time (GMT): 2007/352/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4625208
91 A = 6711058
76 meter
Y = -328231
25 meter E =
0006709
Z = 4849124
95 I = 51
36819
XDOT = 2879
901792 Wp = 45
67092
YDOT = 6776
916558 meter/sec RA = 232
63874 deg
ZDOT = -2281
629631 TA = 66
62903
MA = 66
55847
Ha = 183
952 n
mi
Hp = 178
248
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15174569
90 X = 4604979
05
Y = -1076874
18 feet Y = -276623
04 meter
Z = 15909202
61 Z = 4871545
30
XDOT = 9448
496694 XDOT = 2814
991102
YDOT = 22233
978209 feet/sec YDOT = 6808
758505 meter/sec
ZDOT = -7485
661519 ZDOT = -2267
796036
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16849
65 X = 5135
77
Y = 15122871
28 feet Y = 4609451
16 meter
Z = 15994637
78 Z = 4875165
60
XDOT = -21741
771862 XDOT = -6626
892064
YDOT = 7907
510937 feet/sec YDOT = 2410
209334 meter/sec
ZDOT = -7432
188192 ZDOT = -2265
330961
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 07352
54365239
00020000 00000-0 20000-3 0 9047
2 25544 51
6403 233
3297 0001424 326
3000 33
8074 15
77775739 39864
Satellite: ISS
Catalog Number: 25544
Epoch time: 07352
54365239 = yrday
fracday
Element set: 904
Inclination: 51
6403 deg
RA of node: 233
3297 deg
Eccentricity:
0001424
Arg of perigee: 326
3000 deg
Mean anomaly: 33
8074 deg
Mean motion: 15
77775739 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 3986
Checksum: 293
Coasting Arc #6 (Orbit 4001)
---------------------------------------
Vector Time (GMT): 2007/353/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1858090
45 A = 6717378
59 meter
Y = -5665808
70 meter E =
0012721
Z = 3079815
25 I = 51
40779
XDOT = 5930
673377 Wp = 78
92747
YDOT = 713
043083 meter/sec RA = 227
49935 deg
ZDOT = 4875
248940 TA = 317
02688
MA = 317
12618
Ha = 184
169 n
mi
Hp = 178
221
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6096097
28 X = -1809557
82
Y = -18588611
21 feet Y = -5686315
86 meter
Z = 10104380
75 Z = 3070905
84
XDOT = 19457
589820 XDOT = 5898
575817
YDOT = 2339
380195 feet/sec YDOT = 779
183289 meter/sec
ZDOT = 15994
911221 ZDOT = 4903
982678
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18888220
28 X = 5757129
54
Y = -5160588
20 feet Y = -1572947
28 meter
Z = 10069798
57 Z = 3069274
60
XDOT = -3737
464604 XDOT = -1139
179211
YDOT = 17838
640899 feet/sec YDOT = 5437
217746 meter/sec
ZDOT = 16104
534475 ZDOT = 4908
662108
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
55706685
00020000 00000-0 20000-3 0 9054
2 25544 51
6402 228
0957 0001436 333
9079 26
2014 15
77763434 40029
Satellite: ISS
Catalog Number: 25544
Epoch time: 07353
55706685 = yrday
fracday
Element set: 905
Inclination: 51
6402 deg
RA of node: 228
0957 deg
Eccentricity:
0001436
Arg of perigee: 333
9079 deg
Mean anomaly: 26
2014 deg
Mean motion: 15
77763434 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4002
Checksum: 285
Coasting Arc #7 (Orbit 4016)
---------------------------------------
Vector Time (GMT): 2007/354/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5617462
29 A = 6716224
80 meter
Y = -1461655
77 meter E =
0004348
Z = -3381061
54 I = 51
42505
XDOT = -1195
296529 Wp = 74
37457
YDOT = -6054
217703 meter/sec RA = 222
26778 deg
ZDOT = 4609
261285 TA = 245
54890
MA = 245
59425
Ha = 183
974 n
mi
Hp = 178
081
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18429994
38 X = -5584275
48
Y = -4795458
57 feet Y = -1524287
43 meter
Z = -11092721
59 Z = -3408271
19
XDOT = -3921
576538 XDOT = -1149
899824
YDOT = -19862
918974 feet/sec YDOT = -6067
330950 meter/sec
ZDOT = 15122
248309 ZDOT = 4603
563936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5448882
95 X = 1660819
52
Y = -18183917
97 feet Y = -5542458
20 meter
Z = -11196624
05 Z = -3412731
01
XDOT = 18667
444173 XDOT = 5689
836984
YDOT = -3691
745828 feet/sec YDOT = -1125
244128 meter/sec
ZDOT = 15099
870518 ZDOT = 4602
440534
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
50711151
00020000 00000-0 20000-3 0 9065
2 25544 51
6398 223
1891 0001537 329
7324 30
3753 15
77824438 40178
Satellite: ISS
Catalog Number: 25544
Epoch time: 07354
50711151 = yrday
fracday
Element set: 906
Inclination: 51
6398 deg
RA of node: 223
1891 deg
Eccentricity:
0001537
Arg of perigee: 329
7324 deg
Mean anomaly: 30
3753 deg
Mean motion: 15
77824438 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4017
Checksum: 285
Coasting Arc #8 (Orbit 4032)
---------------------------------------
Vector Time (GMT): 2007/355/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 61035
71 A = 6711422
28 meter
Y = 4774433
48 meter E =
0011208
Z = -4727078
10 I = 51
43058
XDOT = -6786
173940 Wp = 63
52735
YDOT = -2512
705221 meter/sec RA = 217
13416 deg
ZDOT = -2625
369158 TA = 180
61000
MA = 180
61137
Ha = 183
951 n
mi
Hp = 178
062
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 200248
40 X = 30606
36
Y = 15664151
84 feet Y = 4774946
64 meter
Z = -15508786
40 Z = -4726854
73
XDOT = -22264
350197 XDOT = -6744
818369
YDOT = -8243
783532 feet/sec YDOT = -2588
360413 meter/sec
ZDOT = -8613
415872 ZDOT = -2658
236827
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15666783
30 X = -4775235
55
Y = -2732
21 feet Y = -832
78 meter
Z = -15507420
85 Z = -4726661
88
XDOT = 8654
196627 XDOT = 2637
799132
YDOT = -20916
190894 feet/sec YDOT = -6375
254985 meter/sec
ZDOT = -8739
017697 ZDOT = -2663
652594
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
52046303
00020000 00000-0 20000-3 0 9079
2 25544 51
6389 217
9549 0001592 331
5570 28
5508 15
77877606 40334
Satellite: ISS
Catalog Number: 25544
Epoch time: 07355
52046303 = yrday
fracday
Element set: 907
Inclination: 51
6389 deg
RA of node: 217
9549 deg
Eccentricity:
0001592
Arg of perigee: 331
5570 deg
Mean anomaly: 28
5508 deg
Mean motion: 15
77877606 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4033
Checksum: 305
Coasting Arc #9 (Orbit 4048)
---------------------------------------
Vector Time (GMT): 2007/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6025368
15 A = 6720571
16 meter
Y = 2773360
67 meter E =
0012633
Z = 1045963
71 I = 51
48578
XDOT = -1178
456540 Wp = 119
87000
YDOT = 4806
587031 meter/sec RA = 211
92516 deg
ZDOT = -5909
119131 TA = 48
64718
MA = 48
53858
Ha = 183
961 n
mi
Hp = 177
930
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19768268
22 X = 5988827
04
Y = 9098952
32 feet Y = 2840535
24 meter
Z = 3431639
46 Z = 1075146
99
XDOT = -3866
327231 XDOT = -1203
411238
YDOT = 15769
642489 feet/sec YDOT = 4793
270442 meter/sec
ZDOT = -19386
873791 ZDOT = -5914
903843
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9125522
81 X = -2781459
35
Y = 19736307
48 feet Y = 6015626
52 meter
Z = 3543234
64 Z = 1079977
92
XDOT = -14325
357859 XDOT = -4366
369076
YDOT = -3112
533768 feet/sec YDOT = -948
700292 meter/sec
ZDOT = -19408
420052 ZDOT = -5915
686432
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
53378466
00020000 00000-0 20000-3 0 9080
2 25544 51
6387 212
7211 0001488 337
8987 22
2113 15
77909064 40490
Satellite: ISS
Catalog Number: 25544
Epoch time: 07356
53378466 = yrday
fracday
Element set: 908
Inclination: 51
6387 deg
RA of node: 212
7211 deg
Eccentricity:
0001488
Arg of perigee: 337
8987 deg
Mean anomaly: 22
2113 deg
Mean motion: 15
77909064 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4049
Checksum: 312
Coasting Arc #10 (Orbit 4064)
---------------------------------------
Vector Time (GMT): 2007/357/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2182631
09 A = 6708842
35 meter
Y = -3572831
61 meter E =
0002724
Z = 5240608
06 I = 51
47105
XDOT = 6765
907300 Wp = 42
38132
YDOT = 3682
978210 meter/sec RA = 206
75524 deg
ZDOT = -304
916454 TA = 50
52872
MA = 50
50463
Ha = 183
812 n
mi
Hp = 177
886
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7160863
15 X = 2196962
83
Y = -11721888
50 feet Y = -3548345
12 meter
Z = 17193595
99 Z = 5251245
40
XDOT = 22197
858596 XDOT = 6725
702051
YDOT = 12083
261844 feet/sec YDOT = 3758
413683 meter/sec
ZDOT = -1000
382068 ZDOT = -272
144512
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11832393
84 X = 3606513
64
Y = 6876872
76 feet Y = 2096070
82 meter
Z = 17233788
06 Z = 5252858
60
XDOT = -11228
222384 XDOT = -3422
362183
YDOT = 21529
123030 feet/sec YDOT = 6562
076700 meter/sec
ZDOT = -874
983258 ZDOT = -266
694897
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
54707359
00020000 00000-0 20000-3 0 9090
2 25544 51
6377 207
4859 0001594 338
4583 21
6515 15
77964798 40657
Satellite: ISS
Catalog Number: 25544
Epoch time: 07357
54707359 = yrday
fracday
Element set: 909
Inclination: 51
6377 deg
RA of node: 207
4859 deg
Eccentricity:
0001594
Arg of perigee: 338
4583 deg
Mean anomaly: 21
6515 deg
Mean motion: 15
77964798 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4065
Checksum: 339
Coasting Arc #11 (Orbit 4080)
---------------------------------------
Vector Time (GMT): 2007/358/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5493852
47 A = 6719670
66 meter
Y = -3520130
16 meter E =
0014348
Z = 1574583
69 I = 51
53349
XDOT = 3837
880065 Wp = 56
28266
YDOT = -3400
893156 meter/sec RA = 201
59583 deg
ZDOT = 5758
115392 TA = 321
15157
MA = 321
25462
Ha = 183
776 n
mi
Hp = 177
803
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18024450
37 X = -5461730
53
Y = -11548983
48 feet Y = -3581386
24 meter
Z = 5165956
98 Z = 1547972
02
XDOT = 12591
470028 XDOT = 3847
652402
YDOT = -11157
785944 feet/sec YDOT = -3357
922297 meter/sec
ZDOT = 18891
454697 ZDOT = 5776
782785
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10945955
72 X = 3336327
30
Y = -18425209
45 feet Y = -5616003
84 meter
Z = 5064054
91 Z = 1543523
94
XDOT = 10220
726541 XDOT = 3115
277450
YDOT = 11310
730217 feet/sec YDOT = 3447
510570 meter/sec
ZDOT = 18962
305144 ZDOT = 5779
710608
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
56033089
00020000 00000-0 20000-3 0 9107
2 25544 51
6363 202
2501 0001625 337
6515 22
4579 15
78041662 40814
Satellite: ISS
Catalog Number: 25544
Epoch time: 07358
56033089 = yrday
fracday
Element set: 910
Inclination: 51
6363 deg
RA of node: 202
2501 deg
Eccentricity:
0001625
Arg of perigee: 337
6515 deg
Mean anomaly: 22
4579 deg
Mean motion: 15
78041662 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4081
Checksum: 273
Coasting Arc #12 (Orbit 4095)
---------------------------------------
Vector Time (GMT): 2007/359/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 539213
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4437937
44 A = 6711891
77 meter
Y = 2377785
77 meter E =
0008870
Z = -4446967
67 I = 51
53426
XDOT = -5522
931399 Wp = 102
40440
YDOT = -4290
805540 meter/sec RA = 196
38213 deg
ZDOT = 3220
940000 TA = 199
87162
MA = 199
90620
Ha = 183
750 n
mi
Hp = 177
575
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14560162
22 X = -4442594
06
Y = 7801134
43 feet Y = 2328132
99 meter
Z = -14589788
95 Z = -4468537
82
XDOT = -18119
853671 XDOT = -5490
187045
YDOT = -14077
445998 feet/sec YDOT = -4352
383579 meter/sec
ZDOT = 10567
388450 ZDOT = 3194
188675
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8518612
56 X = -2596473
11
Y = -14067283
98 feet Y = -4287708
16 meter
Z = -14671834
43 Z = -4471975
13
XDOT = 12120
533609 XDOT = 3694
338644
YDOT = -18242
376183 feet/sec YDOT = -5560
276261 meter/sec
ZDOT = 10464
851164 ZDOT = 3189
686635
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
51023347
00020000 00000-0 20000-3 0 9110
2 25544 51
6353 197
3411 0001660 343
2191 16
8919 15
78068929 40965
Satellite: ISS
Catalog Number: 25544
Epoch time: 07359
51023347 = yrday
fracday
Element set: 911
Inclination: 51
6353 deg
RA of node: 197
3411 deg
Eccentricity:
0001660
Arg of perigee: 343
2191 deg
Mean anomaly: 16
8919 deg
Mean motion: 15
78068929 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 4096
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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