Date:
December 31st 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 73 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 95 ET - UTC (sec) : 66 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 3579)
---------------------------------------
Vector Time (GMT): 2009/357/14:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5241824
13 A = 6719680
35 meter
Y = 2807084
52 meter E =
0011922
Z = -3141423
74 I = 51
91789
XDOT = -269
031704 Wp = 94
80325
YDOT = 5945
658278 meter/sec RA = 52
62520 deg
ZDOT = 4878
745142 TA = 228
79375
MA = 228
89660
Ha = 188
428 n
mi
Hp = 176
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17197585
73 X = 5225305
70
Y = 9209594
89 feet Y = 2865609
58 meter
Z = -10306508
33 Z = -3115998
86
XDOT = -882
649949 XDOT = -359
197167
YDOT = 19506
752881 feet/sec YDOT = 5942
145294 meter/sec
ZDOT = 16006
381698 ZDOT = 4877
219626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1155725
01 X = 352264
98
Y = 19526989
46 feet Y = 5951826
39 meter
Z = -10205816
45 Z = -3110732
85
XDOT = -15723
185240 XDOT = -4792
426861
YDOT = 9267
651459 feet/sec YDOT = 2824
780165 meter/sec
ZDOT = 16000
455985 ZDOT = 4876
938984
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 09357
58970970
00016717 00000-0 10270-3 0 9006
2 25544 51
6443 53
2256 0007768 105
9060 254
2962 15
76911312 35809
Satellite: ISS
Catalog Number: 25544
Epoch time: 09357
58970970 = yrday
fracday
Element set: 900
Inclination: 51
6443 deg
RA of node: 53
2256 deg
Eccentricity:
0007768
Arg of perigee: 105
9060 deg
Mean anomaly: 254
2962 deg
Mean motion: 15
76911312 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3580
Checksum: 319
Coasting Arc #2 (Orbit 3595)
---------------------------------------
Vector Time (GMT): 2009/358/14:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 805310
42 A = 6714014
41 meter
Y = -4668214
41 meter E =
0018279
Z = -4773917
96 I = 51
87955
XDOT = 6196
892241 Wp = 86
29971
YDOT = 3733
487127 meter/sec RA = 47
53074 deg
ZDOT = -2612
850832 TA = 158
15915
MA = 158
08112
Ha = 188
358 n
mi
Hp = 176
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2642094
56 X = 880642
27
Y = -15315664
08 feet Y = -4658787
40 meter
Z = -15662460
50 Z = -4769823
11
XDOT = 20331
011290 XDOT = 6167
375964
YDOT = 12248
973514 feet/sec YDOT = 3802
619595 meter/sec
ZDOT = -8572
345248 ZDOT = -2582
817642
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14390547
68 X = 4386238
93
Y = -5913306
73 feet Y = -1802375
89 meter
Z = -15646336
30 Z = -4769003
30
XDOT = 171
853776 XDOT = 52
381031
YDOT = 22721
380500 feet/sec YDOT = 6925
476777 meter/sec
ZDOT = -8453
399526 ZDOT = -2576
596176
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 09358
60367376
00016717 00000-0 10270-3 0 9011
2 25544 51
6443 47
9959 0007665 109
5801 250
6192 15
76909417 35963
Satellite: ISS
Catalog Number: 25544
Epoch time: 09358
60367376 = yrday
fracday
Element set: 901
Inclination: 51
6443 deg
RA of node: 47
9959 deg
Eccentricity:
0007665
Arg of perigee: 109
5801 deg
Mean anomaly: 250
6192 deg
Mean motion: 15
76909417 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3596
Checksum: 348
Coasting Arc #3 (Orbit 3611)
---------------------------------------
Vector Time (GMT): 2009/359/14:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5507189
92 A = 6723071
47 meter
Y = -3597178
08 meter E =
0021681
Z = 1341472
54 I = 51
88793
XDOT = 1644
115059 Wp = 117
29852
YDOT = -4727
714113 meter/sec RA = 42
35720 deg
ZDOT = -5865
721952 TA = 47
98905
MA = 47
80466
Ha = 188
334 n
mi
Hp = 176
617
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18068208
40 X = -5473073
01
Y = -11801765
35 feet Y = -3658572
08 meter
Z = 4401156
61 Z = 1314801
01
XDOT = 5394
078277 XDOT = 1725
353803
YDOT = -15510
873075 feet/sec YDOT = -4708
873955 meter/sec
ZDOT = -19244
494593 ZDOT = -5857
537829
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -124393
08 X = -37915
01
Y = -21601967
28 feet Y = -6584279
63 meter
Z = 4295525
08 Z = 1309276
04
XDOT = 14402
659881 XDOT = 4389
930732
YDOT = -3944
747735 feet/sec YDOT = -1202
359110 meter/sec
ZDOT = -19212
179974 ZDOT = -5855
872456
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 09359
61761869
00016717 00000-0 10270-3 0 9029
2 25544 51
6432 42
7662 0007737 112
4198 247
7787 15
76943761 36123
Satellite: ISS
Catalog Number: 25544
Epoch time: 09359
61761869 = yrday
fracday
Element set: 902
Inclination: 51
6432 deg
RA of node: 42
7662 deg
Eccentricity:
0007737
Arg of perigee: 112
4198 deg
Mean anomaly: 247
7787 deg
Mean motion: 15
76943761 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3612
Checksum: 346
Coasting Arc #4 (Orbit 3627)
---------------------------------------
Vector Time (GMT): 2009/360/14:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2121452
77 A = 6711671
33 meter
Y = 3579904
19 meter E =
0010221
Z = 5258197
97 I = 51
82640
XDOT = -6329
858933 Wp = 113
49274
YDOT = -4387
063368 meter/sec RA = 37
23094 deg
ZDOT = 428
345101 TA = 332
42947
MA = 332
48365
Ha = 188
279 n
mi
Hp = 176
626
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6960146
89 X = -2186869
83
Y = 11745092
48 feet Y = 3555814
60 meter
Z = 17251305
68 Z = 5247733
29
XDOT = -20767
253717 XDOT = -6282
412410
YDOT = -14393
252519 feet/sec YDOT = -4457
582342 meter/sec
ZDOT = 1405
331697 ZDOT = 397
709201
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13680247
51 X = -4169739
44
Y = 816806
68 feet Y = 248962
68 meter
Z = 17209940
29 Z = 5245589
80
XDOT = 185
078165 XDOT = 56
411825
YDOT = -24276
025154 feet/sec YDOT = -7399
332467 meter/sec
ZDOT = 1284
001882 ZDOT = 391
363774
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 09360
63154398
00016717 00000-0 10270-3 0 9037
2 25544 51
6429 37
5366 0007647 116
0060 244
1893 15
76974330 36282
Satellite: ISS
Catalog Number: 25544
Epoch time: 09360
63154398 = yrday
fracday
Element set: 903
Inclination: 51
6429 deg
RA of node: 37
5366 deg
Eccentricity:
0007647
Arg of perigee: 116
0060 deg
Mean anomaly: 244
1893 deg
Mean motion: 15
76974330 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3628
Checksum: 323
Coasting Arc #5 (Orbit 3643)
---------------------------------------
Vector Time (GMT): 2009/361/14:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5393347
35 A = 6723353
97 meter
Y = 3958532
19 meter E =
0017654
Z = 621653
20 I = 51
84202
XDOT = -3289
561494 Wp = 75
20205
YDOT = 3515
828292 meter/sec RA = 32
09044 deg
ZDOT = 6015
063997 TA = 291
55538
MA = 291
74344
Ha = 188
065 n
mi
Hp = 176
587
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17694709
15 X = 5345661
59
Y = 12987310
32 feet Y = 4018577
09 meter
Z = 2039544
62 Z = 647738
97
XDOT = -10792
524586 XDOT = -3357
852001
YDOT = 11534
869723 feet/sec YDOT = 3478
659951 meter/sec
ZDOT = 19734
461931 ZDOT = 5998
917666
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -337245
63 X = -102792
47
Y = 21936890
22 feet Y = 6686364
14 meter
Z = 2142852
37 Z = 653141
40
XDOT = -14122
513529 XDOT = -4304
542124
YDOT = -2180
267336 feet/sec YDOT = -664
545484 meter/sec
ZDOT = 19670
601005 ZDOT = 5995
599186
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 09361
64544895
00016717 00000-0 10270-3 0 9045
2 25544 51
6432 32
3080 0007629 120
5937 239
5981 15
77041037 36449
Satellite: ISS
Catalog Number: 25544
Epoch time: 09361
64544895 = yrday
fracday
Element set: 904
Inclination: 51
6432 deg
RA of node: 32
3080 deg
Eccentricity:
0007629
Arg of perigee: 120
5937 deg
Mean anomaly: 239
5981 deg
Mean motion: 15
77041037 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3644
Checksum: 318
Coasting Arc #6 (Orbit 3658)
---------------------------------------
Vector Time (GMT): 2009/362/14:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3646443
30 A = 6712758
60 meter
Y = -2587032
08 meter E =
0020416
Z = -5025519
53 I = 51
77895
XDOT = 5854
913260 Wp = 110
52717
YDOT = 4622
749411 meter/sec RA = 26
92199 deg
ZDOT = 1867
620641 TA = 177
48466
MA = 177
47437
Ha = 188
040 n
mi
Hp = 176
840
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11963396
65 X = 3699514
21
Y = -8487638
06 feet Y = -2545957
96 meter
Z = -16487924
97 Z = -5007676
40
XDOT = 19209
033005 XDOT = 5793
713069
YDOT = 15166
500692 feet/sec YDOT = 4687
880058 meter/sec
ZDOT = 6127
364308 ZDOT = 1895
916056
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13988600
51 X = 4263725
44
Y = 4669569
17 feet Y = 1423284
68 meter
Z = -16417329
52 Z = -5004002
04
XDOT = -488
987607 XDOT = -149
043423
YDOT = 23412
205093 feet/sec YDOT = 7136
040112 meter/sec
ZDOT = 6239
423355 ZDOT = 1901
776239
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 09362
59597054
00016717 00000-0 10270-3 0 9056
2 25544 51
6426 27
4046 0007485 122
7800 237
4087 15
77002982 36598
Satellite: ISS
Catalog Number: 25544
Epoch time: 09362
59597054 = yrday
fracday
Element set: 905
Inclination: 51
6426 deg
RA of node: 27
4046 deg
Eccentricity:
0007485
Arg of perigee: 122
7800 deg
Mean anomaly: 237
4087 deg
Mean motion: 15
77002982 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3659
Checksum: 328
Coasting Arc #7 (Orbit 3674)
---------------------------------------
Vector Time (GMT): 2009/363/14:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4679937
00 A = 6720522
96 meter
Y = -4068378
07 meter E =
0012569
Z = -2588222
77 I = 51
77761
XDOT = 5042
605569 Wp = 125
87424
YDOT = -2458
945530 meter/sec RA = 21
81061 deg
ZDOT = -5277
667572 TA = 83
48528
MA = 83
34220
Ha = 187
918 n
mi
Hp = 176
692
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15354124
01 X = -4621522
68
Y = -13347697
08 feet Y = -4120384
85 meter
Z = -8491544
51 Z = -2610816
79
XDOT = 16543
981524 XDOT = 5095
365223
YDOT = -8067
406594 feet/sec YDOT = -2402
260277 meter/sec
ZDOT = -17315
182322 ZDOT = -5253
042722
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1313071
72 X = 400224
26
Y = -20264705
17 feet Y = -6176682
14 meter
Z = -8581027
71 Z = -2615497
25
XDOT = 15039
456103 XDOT = 4584
026220
YDOT = 8230
968142 feet/sec YDOT = 2508
799090 meter/sec
ZDOT = -17217
734270 ZDOT = -5247
965405
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 09363
60984046
00016717 00000-0 10270-3 0 9061
2 25544 51
6419 22
1739 0007540 126
0690 234
1174 15
77048733 36750
Satellite: ISS
Catalog Number: 25544
Epoch time: 09363
60984046 = yrday
fracday
Element set: 906
Inclination: 51
6419 deg
RA of node: 22
1739 deg
Eccentricity:
0007540
Arg of perigee: 126
0690 deg
Mean anomaly: 234
1174 deg
Mean motion: 15
77048733 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3675
Checksum: 315
Coasting Arc #8 (Orbit 3690)
---------------------------------------
Vector Time (GMT): 2009/364/14:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5081883
61 A = 6716479
41 meter
Y = 1776608
03 meter E =
0016573
Z = 4000360
50 I = 51
73519
XDOT = -4732
576015 Wp = 98
24264
YDOT = -4650
920509 meter/sec RA = 16
61193 deg
ZDOT = -3935
082847 TA = 32
32456
MA = 32
22312
Ha = 187
874 n
mi
Hp = 176
812
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16672846
49 X = -5120805
25
Y = 5828766
49 feet Y = 1719561
07 meter
Z = 13124542
32 Z = 3975578
52
XDOT = -15526
824195 XDOT = -4661
100980
YDOT = -15258
925553 feet/sec YDOT = -4703
442633 meter/sec
ZDOT = -12910
376793 ZDOT = -3957
900879
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14967566
42 X = -4562114
24
Y = -9512901
42 feet Y = -2899532
35 meter
Z = 13026457
77 Z = 3970464
33
XDOT = 1677
955595 XDOT = 511
440865
YDOT = -20494
436093 feet/sec YDOT = -6246
704121 meter/sec
ZDOT = -13000
754752 ZDOT = -3962
630048
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 09364
62369027
00016717 00000-0 10270-3 0 9071
2 25544 51
6414 16
9437 0007329 129
7917 230
3894 15
77096504 36912
Satellite: ISS
Catalog Number: 25544
Epoch time: 09364
62369027 = yrday
fracday
Element set: 907
Inclination: 51
6414 deg
RA of node: 16
9437 deg
Eccentricity:
0007329
Arg of perigee: 129
7917 deg
Mean anomaly: 230
3894 deg
Mean motion: 15
77096504 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3691
Checksum: 337
Coasting Arc #9 (Orbit 3706)
---------------------------------------
Vector Time (GMT): 2009/365/14:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 751809
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3421234
65 A = 6715704
75 meter
Y = 4028916
85 meter E =
0017082
Z = 4135059
96 I = 51
70401
XDOT = -6527
814257 Wp = 116
87907
YDOT = 1684
655526 meter/sec RA = 11
51029 deg
ZDOT = 3740
141179 TA = 294
85225
MA = 295
02977
Ha = 187
573 n
mi
Hp = 176
829
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11224523
15 X = 3355841
14
Y = 13218231
12 feet Y = 4066808
76 meter
Z = 13566469
67 Z = 4151522
03
XDOT = -21416
713443 XDOT = -6564
335973
YDOT = 5527
085060 feet/sec YDOT = 1611
452800 meter/sec
ZDOT = 12270
804394 ZDOT = 3708
340920
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3152911
74 X = -961007
50
Y = 16999912
16 feet Y = 5181573
23 meter
Z = 13631683
22 Z = 4154937
05
XDOT = -16661
233899 XDOT = -5078
344092
YDOT = -12879
467879 feet/sec YDOT = -3925
661810 meter/sec
ZDOT = 12144
927935 ZDOT = 3701
774035
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 09365
63752101
00016717 00000-0 10270-3 0 9083
2 25544 51
6414 11
7138 0007307 134
4911 225
6852 15
77142810 37077
Satellite: ISS
Catalog Number: 25544
Epoch time: 09365
63752101 = yrday
fracday
Element set: 908
Inclination: 51
6414 deg
RA of node: 11
7138 deg
Eccentricity:
0007307
Arg of perigee: 134
4911 deg
Mean anomaly: 225
6852 deg
Mean motion: 15
77142810 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3707
Checksum: 294
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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