Date:
January 3rd 2007
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 6243 07 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 15 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 2446)
---------------------------------------
Vector Time (GMT): 2007/001/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -170260
07 A = 6719820
41 meter
Y = 5813737
54 meter E =
0027100
Z = -3401309
05 I = 51
35073
XDOT = -5476
765859 Wp = 50
10498
YDOT = -2835
224389 meter/sec RA = 243
79493 deg
ZDOT = -4579
060138 TA = 170
16430
MA = 170
11115
Ha = 194
254 n
mi
Hp = 172
398
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -558596
01 X = -218734
56
Y = 19073942
07 feet Y = 5811563
19 meter
Z = -11159150
43 Z = -3402252
86
XDOT = -17968
391925 XDOT = -5422
410767
YDOT = -9301
917287 feet/sec YDOT = -2896
163880 meter/sec
ZDOT = -15023
163183 ZDOT = -4605
534672
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13220469
02 X = -4029598
96
Y = 13758029
53 feet Y = 4193447
40 meter
Z = -11161978
16 Z = -3402170
94
XDOT = -5942
598107 XDOT = -1811
303903
YDOT = -17960
688793 feet/sec YDOT = -5474
417944 meter/sec
ZDOT = -15122
617943 ZDOT = -4609
373949
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 07001
62886652
00020000 00000-0 20000-3 0 9000
2 25544 51
6324 244
4839 0023520 42
4205 317
8773 15
76579276 24474
Satellite: ISS
Catalog Number: 25544
Epoch time: 07001
62886652 = yrday
fracday
Element set: 900
Inclination: 51
6324 deg
RA of node: 244
4839 deg
Eccentricity:
0023520
Arg of perigee: 42
4205 deg
Mean anomaly: 317
8773 deg
Mean motion: 15
76579276 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2447
Checksum: 296
Coasting Arc #2 (Orbit 2462)
---------------------------------------
Vector Time (GMT): 2007/002/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4981012
21 A = 6719661
36 meter
Y = 2998063
43 meter E =
0033586
Z = 3361108
83 I = 51
36484
XDOT = -558
018210 Wp = 60
97765
YDOT = 6151
326785 meter/sec RA = 238
56654 deg
ZDOT = -4609
178887 TA = 79
17482
MA = 78
79697
Ha = 194
130 n
mi
Hp = 172
157
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16341903
58 X = 4930789
74
Y = 9836166
11 feet Y = 3053482
45 meter
Z = 11027259
95 Z = 3385184
93
XDOT = -1830
768404 XDOT = -604
371399
YDOT = 20181
518322 feet/sec YDOT = 6144
828395 meter/sec
ZDOT = -15121
977977 ZDOT = -4612
001166
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5713404
55 X = 1741445
71
Y = 18142785
16 feet Y = 5529920
92 meter
Z = 11117769
26 Z = 3388696
07
XDOT = -13329
094549 XDOT = -4062
708019
YDOT = 13571
392652 feet/sec YDOT = 4136
560480 meter/sec
ZDOT = -15131
795221 ZDOT = -4612
171183
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 07002
64302810
00020000 00000-0 20000-3 0 9013
2 25544 51
6326 239
2538 0023421 45
8268 314
4816 15
76645318 24630
Satellite: ISS
Catalog Number: 25544
Epoch time: 07002
64302810 = yrday
fracday
Element set: 901
Inclination: 51
6326 deg
RA of node: 239
2538 deg
Eccentricity:
0023421
Arg of perigee: 45
8268 deg
Mean anomaly: 314
4816 deg
Mean motion: 15
76645318 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2463
Checksum: 275
Coasting Arc #3 (Orbit 2478)
---------------------------------------
Vector Time (GMT): 2007/003/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 866989
74 A = 6715808
45 meter
Y = -4877453
74 meter E =
0028391
Z = 4506308
86 I = 51
36581
XDOT = 5931
762323 Wp = 66
10877
YDOT = 3888
181062 meter/sec RA = 233
43959 deg
ZDOT = 3063
422634 TA = 353
36783
MA = 353
40532
Ha = 194
264 n
mi
Hp = 172
068
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2844454
51 X = 899575
18
Y = -16002144
81 feet Y = -4867577
18 meter
Z = 14784477
90 Z = 4510598
92
XDOT = 19461
162477 XDOT = 5872
961952
YDOT = 12756
499546 feet/sec YDOT = 3954
184014 meter/sec
ZDOT = 10050
599193 ZDOT = 3092
096562
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12474236
08 X = 3802147
16
Y = -10396896
12 feet Y = -3168973
94 meter
Z = 14799943
65 Z = 4511022
82
XDOT = 5753
604112 XDOT = 1753
698533
YDOT = 21381
227452 feet/sec YDOT = 6516
998127 meter/sec
ZDOT = 10158
449811 ZDOT = 3096
295502
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 07003
65717517
00020000 00000-0 20000-3 0 9020
2 25544 51
6309 234
0242 0023454 50
0752 310
2469 15
76615133 24795
Satellite: ISS
Catalog Number: 25544
Epoch time: 07003
65717517 = yrday
fracday
Element set: 902
Inclination: 51
6309 deg
RA of node: 234
0242 deg
Eccentricity:
0023454
Arg of perigee: 50
0752 deg
Mean anomaly: 310
2469 deg
Mean motion: 15
76615133 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2479
Checksum: 267
Coasting Arc #4 (Orbit 2493)
---------------------------------------
Vector Time (GMT): 2007/004/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5298470
61 A = 6723021
85 meter
Y = -3671903
96 meter E =
0030215
Z = -1885932
14 I = 51
40804
XDOT = 1518
776847 Wp = 50
83481
YDOT = -5041
760391 meter/sec RA = 228
22420 deg
ZDOT = 5628
085000 TA = 288
11169
MA = 288
44053
Ha = 194
201 n
mi
Hp = 171
846
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17383433
76 X = -5247855
73
Y = -12046928
99 feet Y = -3730871
10 meter
Z = -6187441
39 Z = -1911549
24
XDOT = 4982
863670 XDOT = 1547
701970
YDOT = -16541
208631 feet/sec YDOT = -5024
615748 meter/sec
ZDOT = 18464
845801 ZDOT = 5635
532532
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5755971
34 X = -1754420
06
Y = -20321882
41 feet Y = -6194109
76 meter
Z = -6283835
42 Z = -1915313
04
XDOT = 12790
282187 XDOT = 3898
478011
YDOT = -9262
095757 feet/sec YDOT = -2823
086787 meter/sec
ZDOT = 18492
112114 ZDOT = 5636
395772
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 07004
60791902
00020000 00000-0 20000-3 0 9037
2 25544 51
6302 229
1210 0023370 54
0408 306
2919 15
76654774 24943
Satellite: ISS
Catalog Number: 25544
Epoch time: 07004
60791902 = yrday
fracday
Element set: 903
Inclination: 51
6302 deg
RA of node: 229
1210 deg
Eccentricity:
0023370
Arg of perigee: 54
0408 deg
Mean anomaly: 306
2919 deg
Mean motion: 15
76654774 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2494
Checksum: 272
Coasting Arc #5 (Orbit 2509)
---------------------------------------
Vector Time (GMT): 2007/005/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1889082
23 A = 6712936
11 meter
Y = 3885130
91 meter E =
0037075
Z = -5169909
67 I = 51
39365
XDOT = -6123
842289 Wp = 67
05929
YDOT = -4491
250552 meter/sec RA = 223
07812 deg
ZDOT = -1129
709161 TA = 192
04324
MA = 192
13213
Ha = 194
295 n
mi
Hp = 171
566
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6197776
34 X = -1907271
99
Y = 12746492
47 feet Y = 3863905
13 meter
Z = -16961645
89 Z = -5179130
29
XDOT = -20091
346093 XDOT = -6067
677557
YDOT = -14735
073989 feet/sec YDOT = -4559
416577 meter/sec
ZDOT = -3706
394886 ZDOT = -1159
322314
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12703489
96 X = -3872023
74
Y = 6192789
91 feet Y = 1887562
37 meter
Z = -16995694
43 Z = -5180287
66
XDOT = -6114
665754 XDOT = -1863
750122
YDOT = -23090
935135 feet/sec YDOT = -7038
117029 meter/sec
ZDOT = -3817
874752 ZDOT = -1163
688224
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 07005
62202929
00020000 00000-0 20000-3 0 9047
2 25544 51
6297 223
8909 0023440 58
1733 302
1709 15
76684860 25106
Satellite: ISS
Catalog Number: 25544
Epoch time: 07005
62202929 = yrday
fracday
Element set: 904
Inclination: 51
6297 deg
RA of node: 223
8909 deg
Eccentricity:
0023440
Arg of perigee: 58
1733 deg
Mean anomaly: 302
1709 deg
Mean motion: 15
76684860 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2510
Checksum: 285
Coasting Arc #6 (Orbit 2525)
---------------------------------------
Vector Time (GMT): 2007/006/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5329334
67 A = 6724306
93 meter
Y = 4102709
84 meter E =
0029622
Z = 44842
38 I = 51
45485
XDOT = -2876
186737 Wp = 85
11609
YDOT = 3839
182024 meter/sec RA = 217
89471 deg
ZDOT = -6019
961503 TA = 94
39548
MA = 94
05698
Ha = 194
223 n
mi
Hp = 171
424
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17484693
80 X = 5282843
67
Y = 13460334
13 feet Y = 4162045
48 meter
Z = 147120
66 Z = 70619
23
XDOT = -9436
308192 XDOT = -2889
660022
YDOT = 12595
741549 feet/sec YDOT = 3806
944227 meter/sec
ZDOT = -19750
529865 ZDOT = -6033
966014
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5699344
49 X = 1737160
20
Y = 21316064
28 feet Y = 6497136
39 meter
Z = 244197
77 Z = 74431
48
XDOT = -13508
141110 XDOT = -4117
281410
YDOT = 3915
802403 feet/sec YDOT = 1193
536573 meter/sec
ZDOT = -19802
501722 ZDOT = -6035
802525
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 07006
63611950
00020000 00000-0 20000-3 0 9058
2 25544 51
6298 218
6599 0023469 61
2728 299
0791 15
76766994 25265
Satellite: ISS
Catalog Number: 25544
Epoch time: 07006
63611950 = yrday
fracday
Element set: 905
Inclination: 51
6298 deg
RA of node: 218
6599 deg
Eccentricity:
0023469
Arg of perigee: 61
2728 deg
Mean anomaly: 299
0791 deg
Mean motion: 15
76766994 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2526
Checksum: 335
Coasting Arc #7 (Orbit 2541)
---------------------------------------
Vector Time (GMT): 2007/007/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3148682
94 A = 6712692
20 meter
Y = -2872716
96 meter E =
0026932
Z = 5166524
99 I = 51
43800
XDOT = 5989
672885 Wp = 65
14808
YDOT = 4775
918609 meter/sec RA = 212
71605 deg
ZDOT = -979
660006 TA = 34
27468
MA = 34
10117
Ha = 194
279 n
mi
Hp = 171
408
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10330324
62 X = 3155474
53
Y = -9424924
41 feet Y = -2837469
11 meter
Z = 16950541
32 Z = 5181837
23
XDOT = 19651
157758 XDOT = 5940
581639
YDOT = 15669
024307 feet/sec YDOT = 4842
624066 meter/sec
ZDOT = -3214
107632 ZDOT = -950
681600
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13833378
58 X = 4216413
79
Y = -1499012
69 feet Y = -456899
07 meter
Z = 17007535
27 Z = 5183896
75
XDOT = 6401
071184 XDOT = 1951
046497
YDOT = 23280
986762 feet/sec YDOT = 7096
044765 meter/sec
ZDOT = -3104
937949 ZDOT = -946
385087
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 07007
65019634
00020000 00000-0 20000-3 0 9063
2 25544 51
6294 213
4294 0023467 66
0108 294
3510 15
76703091 25423
Satellite: ISS
Catalog Number: 25544
Epoch time: 07007
65019634 = yrday
fracday
Element set: 906
Inclination: 51
6294 deg
RA of node: 213
4294 deg
Eccentricity:
0023467
Arg of perigee: 66
0108 deg
Mean anomaly: 294
3510 deg
Mean motion: 15
76703091 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2542
Checksum: 278
Coasting Arc #8 (Orbit 2557)
---------------------------------------
Vector Time (GMT): 2007/008/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4983743
47 A = 6723062
30 meter
Y = -4145190
67 meter E =
0037491
Z = 1719344
11 I = 51
49908
XDOT = 4359
060712 Wp = 68
05019
YDOT = -2840
629314 meter/sec RA = 207
57162 deg
ZDOT = 5701
905083 TA = 311
07241
MA = 311
39569
Ha = 194
257 n
mi
Hp = 171
257
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16350864
41 X = -4945373
08
Y = -13599706
92 feet Y = -4200707
25 meter
Z = 5640892
74 Z = 1695226
41
XDOT = 14301
380288 XDOT = 4362
802721
YDOT = -9319
649980 feet/sec YDOT = -2791
863355 meter/sec
ZDOT = 18707
037673 ZDOT = 5723
089916
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5451028
76 X = -1661473
57
Y = -20581696
29 feet Y = -6273301
03 meter
Z = 5550002
64 Z = 1691640
80
XDOT = 15469
845033 XDOT = 4715
208766
YDOT = 1044
958489 feet/sec YDOT = 318
503347 meter/sec
ZDOT = 18786
037890 ZDOT = 5725
984349
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 07008
66425144
00020000 00000-0 20000-3 0 9073
2 25544 51
6303 208
1995 0023384 69
9566 290
4113 15
76775742 25586
Satellite: ISS
Catalog Number: 25544
Epoch time: 07008
66425144 = yrday
fracday
Element set: 907
Inclination: 51
6303 deg
RA of node: 208
1995 deg
Eccentricity:
0023384
Arg of perigee: 69
9566 deg
Mean anomaly: 290
4113 deg
Mean motion: 15
76775742 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2558
Checksum: 311
Coasting Arc #9 (Orbit 2572)
---------------------------------------
Vector Time (GMT): 2007/009/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4452196
60 A = 6715022
72 meter
Y = 2113838
35 meter E =
0032545
Z = -4587274
53 I = 51
49919
XDOT = -5281
155445 Wp = 84
98422
YDOT = -4726
498597 meter/sec RA = 202
36622 deg
ZDOT = 2968
492202 TA = 214
49033
MA = 214
70194
Ha = 194
247 n
mi
Hp = 171
012
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14606944
21 X = -4453219
10
Y = 6935165
20 feet Y = 2064045
99 meter
Z = -15050113
28 Z = -4608905
35
XDOT = -17326
625476 XDOT = -5242
330764
YDOT = -15506
885160 feet/sec YDOT = -4785
338527 meter/sec
ZDOT = 9739
147644 ZDOT = 2942
930702
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15897930
63 X = -4845689
26
Y = -2505486
09 feet Y = -763672
16 meter
Z = -15130881
87 Z = -4611892
79
XDOT = -5730
258435 XDOT = -1746
582771
YDOT = -21462
997994 feet/sec YDOT = -6541
921789 meter/sec
ZDOT = 9642
764321 ZDOT = 2939
114565
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 07009
61491325
00020000 00000-0 20000-3 0 9084
2 25544 51
6312 203
2964 0023431 73
5436 286
8301 15
76787089 25730
Satellite: ISS
Catalog Number: 25544
Epoch time: 07009
61491325 = yrday
fracday
Element set: 908
Inclination: 51
6312 deg
RA of node: 203
2964 deg
Eccentricity:
0023431
Arg of perigee: 73
5436 deg
Mean anomaly: 286
8301 deg
Mean motion: 15
76787089 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2573
Checksum: 296
Coasting Arc #10 (Orbit 2588)
---------------------------------------
Vector Time (GMT): 2007/010/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4101253
02 A = 6719135
08 meter
Y = 4109871
81 meter E =
0028219
Z = -3410615
21 I = 51
54037
XDOT = -5820
052283 Wp = 79
69385
YDOT = 2015
952002 meter/sec RA = 197
24791 deg
ZDOT = -4596
555881 TA = 140
60882
MA = 140
40327
Ha = 194
236 n
mi
Hp = 171
057
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13455554
54 X = 4071559
03
Y = 13483831
41 feet Y = 4155568
50 meter
Z = -11189682
43 Z = -3390763
37
XDOT = -19094
659722 XDOT = -5819
833373
YDOT = 6614
015755 feet/sec YDOT = 1950
870463 meter/sec
ZDOT = -15080
563914 ZDOT = -4624
828750
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3830944
71 X = 1167671
95
Y = 18704558
35 feet Y = 5701149
39 meter
Z = -11114765
39 Z = -3387780
49
XDOT = -18139
684089 XDOT = -5528
975710
YDOT = -5255
380443 feet/sec YDOT = -1601
839959 meter/sec
ZDOT = -15186
236528 ZDOT = -4628
764894
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 07010
62893426
00020000 00000-0 20000-3 0 9096
2 25544 51
6313 198
0654 0023443 77
2118 283
1664 15
76831803 25892
Satellite: ISS
Catalog Number: 25544
Epoch time: 07010
62893426 = yrday
fracday
Element set: 909
Inclination: 51
6313 deg
RA of node: 198
0654 deg
Eccentricity:
0023443
Arg of perigee: 77
2118 deg
Mean anomaly: 283
1664 deg
Mean motion: 15
76831803 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2589
Checksum: 300
Coasting Arc #11 (Orbit 2604)
---------------------------------------
Vector Time (GMT): 2007/011/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5635142
28 A = 6719233
31 meter
Y = -1489032
88 meter E =
0035910
Z = 3315800
74 I = 51
56831
XDOT = 4008
203577 Wp = 84
76862
YDOT = 4649
330204 meter/sec RA = 192
03252 deg
ZDOT = -4677
562886 TA = 56
09044
MA = 55
74944
Ha = 194
149 n
mi
Hp = 170
947
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18487999
62 X = 5635266
59
Y = -4885278
49 feet Y = -1426017
14 meter
Z = 10878611
35 Z = 3343176
27
XDOT = 13150
274202 XDOT = 3978
638810
YDOT = 15253
708017 feet/sec YDOT = 4693
987208 meter/sec
ZDOT = -15346
334928 ZDOT = -4658
162633
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18165290
32 X = 5536780
49
Y = 5784132
16 feet Y = 1763003
48 meter
Z = 10980997
38 Z = 3347008
00
XDOT = 3384
676098 XDOT = 1031
649275
YDOT = 18652
127636 feet/sec YDOT = 5685
168503 meter/sec
ZDOT = -15273
034879 ZDOT = -4655
221031
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 07011
64293790
00020000 00000-0 20000-3 0 9109
2 25544 51
6310 192
8346 0023391 81
2231 279
1582 15
76834604 26057
Satellite: ISS
Catalog Number: 25544
Epoch time: 07011
64293790 = yrday
fracday
Element set: 910
Inclination: 51
6310 deg
RA of node: 192
8346 deg
Eccentricity:
0023391
Arg of perigee: 81
2231 deg
Mean anomaly: 279
1582 deg
Mean motion: 15
76834604 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2605
Checksum: 278
Coasting Arc #12 (Orbit 2620)
---------------------------------------
Vector Time (GMT): 2007/012/14:30:00
000
Vector Time (MET): N/A
Weight (LBS) : 471443
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2791765
00 A = 6714725
75 meter
Y = -4002887
94 meter E =
0030782
Z = 4586461
04 I = 51
58285
XDOT = 6988
937640 Wp = 93
12150
YDOT = -1494
047063 meter/sec RA = 186
91908 deg
ZDOT = 2931
749823 TA = 327
81220
MA = 327
99973
Ha = 194
123 n
mi
Hp = 170
890
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9159334
00 X = -2769076
75
Y = -13132834
44 feet Y = -4033980
56 meter
Z = 15047444
36 Z = 4572953
47
XDOT = 22929
585433 XDOT = 6990
883012
YDOT = -4901
729210 feet/sec YDOT = -1415
882255 meter/sec
ZDOT = 9618
601783 ZDOT = 2965
706517
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1011743
26 X = -308379
35
Y = -16027398
25 feet Y = -4885150
99 meter
Z = 14996306
30 Z = 4570874
16
XDOT = 20893
916444 XDOT = 6368
465732
YDOT = 7856
568588 feet/sec YDOT = 2394
682105 meter/sec
ZDOT = 9745
658143 ZDOT = 2970
476602
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 07012
65692086
00020000 00000-0 20000-3 0 9113
2 25544 51
6320 187
6049 0023234 84
9804 275
4012 15
76914176 26210
Satellite: ISS
Catalog Number: 25544
Epoch time: 07012
65692086 = yrday
fracday
Element set: 911
Inclination: 51
6320 deg
RA of node: 187
6049 deg
Eccentricity:
0023234
Arg of perigee: 84
9804 deg
Mean anomaly: 275
4012 deg
Mean motion: 15
76914176 rev/day
Decay rate: 2
00000E-04 rev/day^2
Epoch rev: 2621
Checksum: 285
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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