Date:
February 22nd 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 30138 95 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 74 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 0 74 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
051/21:28:00
838 4
1 8
8 8
9
N/A 6
0 -1
3 191
5
000/00:26:01
676 -5
1 -0
0 185
9
Coasting Arc #1 (Orbit 504)
---------------------------------------
Vector Time (GMT): 2010/051/05:08:18
792
Vector Time (MET): N/A
Weight (LBS) : 800608
7
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1529106
60 A = 6720543
90 meter
Y = 5109023
93 meter E =
0012154
Z = -4088039
48 I = 51
95428
XDOT = -4885
596697 Wp = 32
50263
YDOT = 4536
521474 meter/sec RA = 110
19987 deg
ZDOT = 3857
359848 TA = 276
91601
MA = 277
05426
Ha = 190
878 n
mi
Hp = 179
881
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5016753
93 X = 1491721
72
Y = 16761889
52 feet Y = 5125914
12 meter
Z = -13412203
03 Z = -4080702
16
XDOT = -16028
860553 XDOT = -4954
699965
YDOT = 14883
600638 feet/sec YDOT = 4481
501606 meter/sec
ZDOT = 12655
380080 ZDOT = 3833
457810
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15643778
36 X = -4768223
65
Y = -7885841
97 feet Y = -2403604
63 meter
Z = -13382886
29 Z = -4079103
74
XDOT = -225
193749 XDOT = -68
639055
YDOT = -20784
400362 feet/sec YDOT = -6335
085230 meter/sec
ZDOT = 12560
630110 ZDOT = 3828
480057
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 10051
22303558
00016717 00000-0 10270-3 0 9002
2 25544 51
6428 111
0426 0012782 357
1816 2
9274 15
75537700 5058
Satellite: ISS
Catalog Number: 25544
Epoch time: 10051
22303558 = yrday
fracday
Element set: 900
Inclination: 51
6428 deg
RA of node: 111
0426 deg
Eccentricity:
0012782
Arg of perigee: 357
1816 deg
Mean anomaly: 2
9274 deg
Mean motion: 15
75537700 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 505
Checksum: 274
Coasting Arc #2 (Orbit 515)
---------------------------------------
Vector Time (GMT): 2010/051/21:41:01
676
Vector Time (MET): N/A
Weight (LBS) : 799531
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4197874
38 A = 6722074
53 meter
Y = 311566
99 meter E =
0013059
Z = -5250681
19 I = 51
94568
XDOT = -1580
782234 Wp = 52
59627
YDOT = 7483
474718 meter/sec RA = 106
70289 deg
ZDOT = -813
388392 TA = 209
64876
MA = 209
72285
Ha = 191
460 n
mi
Hp = 185
920
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13772553
75 X = 4219585
02
Y = 1022201
40 feet Y = 358631
36 meter
Z = -17226644
31 Z = -5230235
37
XDOT = -5186
293418 XDOT = -1660
395031
YDOT = 24552
082409 feet/sec YDOT = 7465
352313 meter/sec
ZDOT = -2668
597088 ZDOT = -821
261339
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4981810
00 X = -1518455
69
Y = -12988485
24 feet Y = -3958890
30 meter
Z = -17145443
33 Z = -5225931
13
XDOT = 23470
010970 XDOT = 7153
659344
YDOT = -5410
706291 feet/sec YDOT = -1649
183278 meter/sec
ZDOT = -2699
603424 ZDOT = -822
839124
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 10051
92076042
00016717 00000-0 10270-3 0 9015
2 25544 51
6431 107
4551 0007616 326
1706 33
8970 15
73387021 5169
Satellite: ISS
Catalog Number: 25544
Epoch time: 10051
92076042 = yrday
fracday
Element set: 901
Inclination: 51
6431 deg
RA of node: 107
4551 deg
Eccentricity:
0007616
Arg of perigee: 326
1706 deg
Mean anomaly: 33
8970 deg
Mean motion: 15
73387021 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 516
Checksum: 278
Coasting Arc #3 (Orbit 531)
---------------------------------------
Vector Time (GMT): 2010/052/21:41:01
676
Vector Time (MET): N/A
Weight (LBS) : 799531
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 653095
02 A = 6733566
82 meter
Y = -6641086
01 meter E =
0007371
Z = 887074
53 I = 51
99204
XDOT = 4835
935242 Wp = 100
88601
YDOT = -328
271911 meter/sec RA = 101
57960 deg
ZDOT = -5977
681529 TA = 69
48656
MA = 69
40746
Ha = 191
526 n
mi
Hp = 185
641
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2142700
20 X = 722999
08
Y = -21788339
94 feet Y = -6633391
85 meter
Z = 2910349
52 Z = 890417
09
XDOT = 15865
929273 XDOT = 4868
284806
YDOT = -1077
007581 feet/sec YDOT = -274
012795 meter/sec
ZDOT = -19611
816040 ZDOT = -5954
110229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20490510
59 X = -6245507
63
Y = 7706213
48 feet Y = 2348853
87 meter
Z = 2923406
48 Z = 891054
29
XDOT = -7456
249391 XDOT = -2272
664814
YDOT = -12371
545779 feet/sec YDOT = -3770
847153 meter/sec
ZDOT = -19518
218539 ZDOT = -5949
153011
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 10052
93698822
00016717 00000-0 10270-3 0 9024
2 25544 51
6432 102
2411 0007570 329
6448 30
4276 15
73389579 5328
Satellite: ISS
Catalog Number: 25544
Epoch time: 10052
93698822 = yrday
fracday
Element set: 902
Inclination: 51
6432 deg
RA of node: 102
2411 deg
Eccentricity:
0007570
Arg of perigee: 329
6448 deg
Mean anomaly: 30
4276 deg
Mean motion: 15
73389579 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 532
Checksum: 306
Coasting Arc #4 (Orbit 547)
---------------------------------------
Vector Time (GMT): 2010/053/21:41:01
676
Vector Time (MET): N/A
Weight (LBS) : 799531
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4184260
83 A = 6722104
40 meter
Y = 873946
33 meter E =
0004556
Z = 5187253
81 I = 51
95940
XDOT = -90
064890 Wp = 358
62512
YDOT = -7604
408263 meter/sec RA = 96
49062 deg
ZDOT = 1213
012700 TA = 79
86381
MA = 79
81242
Ha = 191
701 n
mi
Hp = 185
306
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13727889
87 X = -4218920
86
Y = 2867277
99 feet Y = 826961
63 meter
Z = 17018549
23 Z = 5166842
77
XDOT = -295
488485 XDOT = -10
916865
YDOT = -24948
846006 feet/sec YDOT = -7604
972886 meter/sec
ZDOT = 3979
700460 ZDOT = 1212
767391
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8865043
15 X = 2702065
15
Y = 10992677
32 feet Y = 3350568
05 meter
Z = 16937512
11 Z = 5162553
69
XDOT = -21248
975343 XDOT = -6476
687685
YDOT = 11028
912127 feet/sec YDOT = 3361
612416 meter/sec
ZDOT = 3978
488414 ZDOT = 1212
643269
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 10053
95318894
00016717 00000-0 10270-3 0 9036
2 25544 51
6436 97
0269 0007672 333
5684 26
5086 15
73464052 5485
Satellite: ISS
Catalog Number: 25544
Epoch time: 10053
95318894 = yrday
fracday
Element set: 903
Inclination: 51
6436 deg
RA of node: 97
0269 deg
Eccentricity:
0007672
Arg of perigee: 333
5684 deg
Mean anomaly: 26
5086 deg
Mean motion: 15
73464052 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 548
Checksum: 325
Coasting Arc #5 (Orbit 562)
---------------------------------------
Vector Time (GMT): 2010/054/21:41:01
676
Vector Time (MET): N/A
Weight (LBS) : 799531
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 802461
08 A = 6732954
31 meter
Y = 6562246
97 meter E =
0014672
Z = -1226305
95 I = 51
99904
XDOT = -4656
327960 Wp = 10
24548
YDOT = 1668
656898 meter/sec RA = 91
36126 deg
ZDOT = 5907
203179 TA = 336
37226
MA = 336
43958
Ha = 191
727 n
mi
Hp = 185
045
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2632746
34 X = 734978
29
Y = 21529681
66 feet Y = 6570843
26 meter
Z = -4023313
50 Z = -1222571
53
XDOT = -15276
666537 XDOT = -4703
336693
YDOT = 5474
596121 feet/sec YDOT = 1616
324185 meter/sec
ZDOT = 19380
587859 ZDOT = 5884
468999
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17728942
15 X = 5403781
57
Y = -12500555
08 feet Y = -3810169
19 meter
Z = -4008282
70 Z = -1221724
57
XDOT = 11177
461530 XDOT = 3406
890274
YDOT = 9693
240970 feet/sec YDOT = 2954
499848 meter/sec
ZDOT = 19290
339250 ZDOT = 5879
695403
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 10054
90585537
00016717 00000-0 10270-3 0 9043
2 25544 51
6442 92
1387 0007748 337
3017 22
7802 15
73498873 5634
Satellite: ISS
Catalog Number: 25544
Epoch time: 10054
90585537 = yrday
fracday
Element set: 904
Inclination: 51
6442 deg
RA of node: 92
1387 deg
Eccentricity:
0007748
Arg of perigee: 337
3017 deg
Mean anomaly: 22
7802 deg
Mean motion: 15
73498873 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 563
Checksum: 321
Coasting Arc #6 (Orbit 578)
---------------------------------------
Vector Time (GMT): 2010/055/21:41:01
676
Vector Time (MET): N/A
Weight (LBS) : 799531
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3885535
09 A = 6722186
55 meter
Y = -1994739
65 meter E =
0015000
Z = -5121624
09 I = 51
96268
XDOT = 1700
273064 Wp = 46
92921
YDOT = 7335
864984 meter/sec RA = 86
27811 deg
ZDOT = -1560
060840 TA = 208
10447
MA = 208
18552
Ha = 191
800 n
mi
Hp = 184
889
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12747818
52 X = 3932431
16
Y = -6544421
41 feet Y = -1951027
07 meter
Z = -16803228
65 Z = -5102634
71
XDOT = 5578
323700 XDOT = 1625
694062
YDOT = 24067
798505 feet/sec YDOT = 7354
461455 meter/sec
ZDOT = -5118
309841 ZDOT = -1551
982250
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11971837
92 X = -3649016
20
Y = -8033600
42 feet Y = -2448641
41 meter
Z = -16727856
49 Z = -5098650
66
XDOT = 17704
924436 XDOT = 5396
460968
YDOT = -15744
911089 feet/sec YDOT = -4799
048900 meter/sec
ZDOT = -5086
003361 ZDOT = -1550
213824
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 10055
92200722
00016717 00000-0 10270-3 0 9057
2 25544 51
6442 86
9244 0007842 341
2152 18
8719 15
73549722 5796
Satellite: ISS
Catalog Number: 25544
Epoch time: 10055
92200722 = yrday
fracday
Element set: 905
Inclination: 51
6442 deg
RA of node: 86
9244 deg
Eccentricity:
0007842
Arg of perigee: 341
2152 deg
Mean anomaly: 18
8719 deg
Mean motion: 15
73549722 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 579
Checksum: 307
Coasting Arc #7 (Orbit 594)
---------------------------------------
Vector Time (GMT): 2010/056/21:41:01
676
Vector Time (MET): N/A
Weight (LBS) : 799531
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2140510
32 A = 6732546
66 meter
Y = -6206789
91 meter E =
0010406
Z = 1483598
22 I = 51
99414
XDOT = 4161
485150 Wp = 85
99894
YDOT = -2834
875063 meter/sec RA = 81
14322 deg
ZDOT = -5820
379150 TA = 77
75710
MA = 77
64059
Ha = 191
887 n
mi
Hp = 184
636
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7022671
64 X = -2078152
65
Y = -20363483
96 feet Y = -6230377
68 meter
Z = 4867448
22 Z = 1473351
50
XDOT = 13653
166503 XDOT = 4221
149491
YDOT = -9300
771205 feet/sec YDOT = -2788
005380 meter/sec
ZDOT = -19095
732118 ZDOT = -5800
018250
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14074061
43 X = -4289773
92
Y = 16318901
45 feet Y = 4974001
16 meter
Z = 4826561
75 Z = 1471136
02
XDOT = -13763
504633 XDOT = -4195
116212
YDOT = -6211
494199 feet/sec YDOT = -1893
263432 meter/sec
ZDOT = -19014
930283 ZDOT = -5795
750750
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 10056
93813501
00016717 00000-0 10270-3 0 9065
2 25544 51
6440 81
7099 0007680 345
3923 14
7017 15
73539454 5951
Satellite: ISS
Catalog Number: 25544
Epoch time: 10056
93813501 = yrday
fracday
Element set: 906
Inclination: 51
6440 deg
RA of node: 81
7099 deg
Eccentricity:
0007680
Arg of perigee: 345
3923 deg
Mean anomaly: 14
7017 deg
Mean motion: 15
73539454 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 595
Checksum: 310
Coasting Arc #8 (Orbit 610)
---------------------------------------
Vector Time (GMT): 2010/057/21:41:01
676
Vector Time (MET): N/A
Weight (LBS) : 799531
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3341739
66 A = 6722326
81 meter
Y = 2922672
91 meter E =
0005443
Z = 5044044
05 I = 51
95429
XDOT = -3163
230669 Wp = 33
06821
YDOT = -6779
886233 meter/sec RA = 76
06239 deg
ZDOT = 1836
333778 TA = 39
33229
MA = 39
29277
Ha = 192
081 n
mi
Hp = 184
301
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10963712
78 X = -3398675
46
Y = 9588821
88 feet Y = 2884985
50 meter
Z = 16548700
94 Z = 5027671
92
XDOT = -10378
053375 XDOT = -3096
101990
YDOT = -22243
721236 feet/sec YDOT = -6814
883928 meter/sec
ZDOT = 6024
717119 ZDOT = 1821
130654
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13925025
14 X = 4244347
66
Y = 4515291
06 feet Y = 1376260
71 meter
Z = 16483744
34 Z = 5024245
27
XDOT = -13334
615040 XDOT = -4064
390664
YDOT = 19393
199208 feet/sec YDOT = 5911
047118 meter/sec
ZDOT = 5964
122360 ZDOT = 1817
864495
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 10057
95423448
00016717 00000-0 10270-3 0 9076
2 25544 51
6438 76
4945 0007838 349
2302 10
8692 15
73597828 6112
Satellite: ISS
Catalog Number: 25544
Epoch time: 10057
95423448 = yrday
fracday
Element set: 907
Inclination: 51
6438 deg
RA of node: 76
4945 deg
Eccentricity:
0007838
Arg of perigee: 349
2302 deg
Mean anomaly: 10
8692 deg
Mean motion: 15
73597828 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 611
Checksum: 332
Coasting Arc #9 (Orbit 625)
---------------------------------------
Vector Time (GMT): 2010/058/21:41:01
676
Vector Time (MET): N/A
Weight (LBS) : 799531
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3347941
98 A = 6731944
95 meter
Y = 5572482
63 meter E =
0014429
Z = -1717052
02 I = 51
97787
XDOT = -3429
329297 Wp = 14
19155
YDOT = 3822
591168 meter/sec RA = 70
92124 deg
ZDOT = 5742
925503 TA = 326
89341
MA = 326
98363
Ha = 192
076 n
mi
Hp = 184
099
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10984061
60 X = 3293721
55
Y = 18282423
34 feet Y = 5609618
01 meter
Z = -5633372
78 Z = -1700920
33
XDOT = -11251
080372 XDOT = -3499
716630
YDOT = 12541
309607 feet/sec YDOT = 3783
849281 meter/sec
ZDOT = 18841
619103 ZDOT = 5726
095015
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9634193
91 X = 2936502
30
Y = -19047274
54 feet Y = -5805609
28 meter
Z = -5569123
95 Z = -1697468
98
XDOT = 15272
798794 XDOT = 4655
149072
YDOT = 2258
613929 feet/sec YDOT = 688
425526 meter/sec
ZDOT = 18774
866410 ZDOT = 5722
579282
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 10058
90680362
00016717 00000-0 10270-3 0 9083
2 25544 51
6431 71
6048 0007957 351
7208 8
3823 15
73640409 6269
Satellite: ISS
Catalog Number: 25544
Epoch time: 10058
90680362 = yrday
fracday
Element set: 908
Inclination: 51
6431 deg
RA of node: 71
6048 deg
Eccentricity:
0007957
Arg of perigee: 351
7208 deg
Mean anomaly: 8
3823 deg
Mean motion: 15
73640409 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 626
Checksum: 306
Coasting Arc #10 (Orbit 641)
---------------------------------------
Vector Time (GMT): 2010/059/21:41:01
676
Vector Time (MET): N/A
Weight (LBS) : 799531
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2624545
68 A = 6722347
88 meter
Y = -3686715
43 meter E =
0016284
Z = -4984416
42 I = 51
93408
XDOT = 4428
279524 Wp = 46
15719
YDOT = 5940
182965 meter/sec RA = 65
84192 deg
ZDOT = -2055
057063 TA = 203
95938
MA = 204
03525
Ha = 192
040 n
mi
Hp = 183
938
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8610714
18 X = 2689788
96
Y = -12095523
08 feet Y = -3657001
93 meter
Z = -16353072
23 Z = -4971507
82
XDOT = 14528
476128 XDOT = 4371
509087
YDOT = 19488
789254 feet/sec YDOT = 5989
384984 meter/sec
ZDOT = -6742
313198 ZDOT = -2033
683492
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14887482
23 X = -4537704
58
Y = -692906
04 feet Y = -211197
76 meter
Z = -16301895
68 Z = -4968817
80
XDOT = 8327
194437 XDOT = 2538
128865
YDOT = -21758
278422 feet/sec YDOT = -6631
923263 meter/sec
ZDOT = -6657
232311 ZDOT = -2029
124408
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 10059
92285202
00016717 00000-0 10270-3 0 9091
2 25544 51
6421 66
3887 0007919 355
2763 4
8324 15
73693530 6421
Satellite: ISS
Catalog Number: 25544
Epoch time: 10059
92285202 = yrday
fracday
Element set: 909
Inclination: 51
6421 deg
RA of node: 66
3887 deg
Eccentricity:
0007919
Arg of perigee: 355
2763 deg
Mean anomaly: 4
8324 deg
Mean motion: 15
73693530 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 642
Checksum: 316
Coasting Arc #11 (Orbit 657)
---------------------------------------
Vector Time (GMT): 2010/060/21:41:01
676
Vector Time (MET): N/A
Weight (LBS) : 799531
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4353997
42 A = 6731427
40 meter
Y = -4782396
22 meter E =
0013042
Z = 1860628
37 I = 51
95233
XDOT = 2544
456402 Wp = 79
88941
YDOT = -4537
453195 meter/sec RA = 60
69645 deg
ZDOT = -5672
771297 TA = 79
55720
MA = 79
41025
Ha = 192
093 n
mi
Hp = 183
614
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14284768
45 X = -4309234
66
Y = -15690276
31 feet Y = -4830834
72 meter
Z = 6104423
79 Z = 1839586
27
XDOT = 8347
954074 XDOT = 2622
562733
YDOT = -14886
657463 feet/sec YDOT = -4508
563482 meter/sec
ZDOT = -18611
454385 ZDOT = -5660
220322
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4975555
50 X = -1516549
32
Y = 20651837
66 feet Y = 6294680
12 meter
Z = 6020699
19 Z = 1835109
11
XDOT = -15563
652096 XDOT = -4743
801159
YDOT = 1696
299134 feet/sec YDOT = 517
031976 meter/sec
ZDOT = -18561
720580 ZDOT = -5657
612433
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 10060
93887378
00016717 00000-0 10270-3 0 9108
2 25544 51
6427 61
1731 0007949 359
6300
4856 15
73749481 6582
Satellite: ISS
Catalog Number: 25544
Epoch time: 10060
93887378 = yrday
fracday
Element set: 910
Inclination: 51
6427 deg
RA of node: 61
1731 deg
Eccentricity:
0007949
Arg of perigee: 359
6300 deg
Mean anomaly:
4856 deg
Mean motion: 15
73749481 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 658
Checksum: 324
Coasting Arc #12 (Orbit 673)
---------------------------------------
Vector Time (GMT): 2010/061/21:41:01
676
Vector Time (MET): N/A
Weight (LBS) : 799531
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1803972
49 A = 6722407
64 meter
Y = 4198786
49 meter E =
0007305
Z = 4923739
19 I = 51
90539
XDOT = -5482
049402 Wp = 52
60255
YDOT = -4943
931010 meter/sec RA = 55
61641 deg
ZDOT = 2209
598247 TA = 16
04080
MA = 16
01768
Ha = 192
285 n
mi
Hp = 183
403
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5918544
92 X = -1874708
36
Y = 13775546
21 feet Y = 4178218
39 meter
Z = 16153999
97 Z = 4914803
35
XDOT = -17985
726383 XDOT = -5437
091754
YDOT = -16220
246095 feet/sec YDOT = -5004
982945 meter/sec
ZDOT = 7249
338082 ZDOT = 2183
076468
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14730956
28 X = 4489995
48
Y = -2989275
33 feet Y = -911131
12 meter
Z = 16118614
16 Z = 4912953
60
XDOT = -3141
969507 XDOT = -957
672306
YDOT = 22999
674277 feet/sec YDOT = 7010
300720 meter/sec
ZDOT = 7143
849977 ZDOT = 2177
445473
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 10061
95486966
00016717 00000-0 10270-3 0 9110
2 25544 51
6420 55
9564 0007890 3
7641 356
3580 15
73735947 6747
Satellite: ISS
Catalog Number: 25544
Epoch time: 10061
95486966 = yrday
fracday
Element set: 911
Inclination: 51
6420 deg
RA of node: 55
9564 deg
Eccentricity:
0007890
Arg of perigee: 3
7641 deg
Mean anomaly: 356
3580 deg
Mean motion: 15
73735947 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 674
Checksum: 331
Coasting Arc #13 (Orbit 688)
---------------------------------------
Vector Time (GMT): 2010/062/21:41:01
676
Vector Time (MET): N/A
Weight (LBS) : 799531
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5168735
68 A = 6731059
94 meter
Y = 3813247
65 meter E =
0014064
Z = -1989500
17 I = 51
91642
XDOT = -1558
296488 Wp = 21
49034
YDOT = 5031
630692 meter/sec RA = 50
46549 deg
ZDOT = 5620
803356 TA = 316
42998
MA = 316
54098
Ha = 192
205 n
mi
Hp = 183
223
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16957794
24 X = 5135375
67
Y = 12510655
01 feet Y = 3870860
83 meter
Z = -6527231
53 Z = -1964472
01
XDOT = -5112
521287 XDOT = -1641
749895
YDOT = 16507
974711 feet/sec YDOT = 5013
738754 meter/sec
ZDOT = 18440
955893 ZDOT = 5613
030084
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 117063
88 X = 35681
07
Y = -21103525
77 feet Y = -6432354
65 meter
Z = -6427715
13 Z = -1959167
57
XDOT = 14881
717126 XDOT = 4535
947380
YDOT = -5499
248607 feet/sec YDOT = -1676
170976 meter/sec
ZDOT = 18410
203340 ZDOT = 5611
429978
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 10062
90733799
00016717 00000-0 10270-3 0 9126
2 25544 51
6414 51
0659 0007789 6
2375 353
8884 15
73804347 6897
Satellite: ISS
Catalog Number: 25544
Epoch time: 10062
90733799 = yrday
fracday
Element set: 912
Inclination: 51
6414 deg
RA of node: 51
0659 deg
Eccentricity:
0007789
Arg of perigee: 6
2375 deg
Mean anomaly: 353
8884 deg
Mean motion: 15
73804347 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 689
Checksum: 337
Coasting Arc #14 (Orbit 704)
---------------------------------------
Vector Time (GMT): 2010/063/21:41:01
676
Vector Time (MET): N/A
Weight (LBS) : 799531
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 934226
99 A = 6722224
05 meter
Y = -4526367
00 meter E =
0017339
Z = -4896617
14 I = 51
86647
XDOT = 6279
112757 Wp = 49
84655
YDOT = 3791
679504 meter/sec RA = 45
38501 deg
ZDOT = -2301
385503 TA = 197
75303
MA = 197
81369
Ha = 192
158 n
mi
Hp = 182
977
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3065049
19 X = 1008558
92
Y = -14850285
43 feet Y = -4515504
61 meter
Z = -16065016
87 Z = -4891897
87
XDOT = 20600
763638 XDOT = 6247
426482
YDOT = 12439
893387 feet/sec YDOT = 3861
718962 meter/sec
ZDOT = -7550
477373 ZDOT = -2270
958987
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13758946
88 X = -4193727
01
Y = 6419927
01 feet Y = 1956793
75 meter
Z = -16046376
19 Z = -4890935
46
XDOT = -2031
537257 XDOT = -619
212556
YDOT = -22969
705148 feet/sec YDOT = -7001
166129 meter/sec
ZDOT = -7429
524814 ZDOT = -2264
519163
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 10063
92327893
00016717 00000-0 10270-3 0 9134
2 25544 51
6408 45
8497 0007730 11
0242 349
1089 15
73854856 7058
Satellite: ISS
Catalog Number: 25544
Epoch time: 10063
92327893 = yrday
fracday
Element set: 913
Inclination: 51
6408 deg
RA of node: 45
8497 deg
Eccentricity:
0007730
Arg of perigee: 11
0242 deg
Mean anomaly: 349
1089 deg
Mean motion: 15
73854856 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 705
Checksum: 316
Coasting Arc #15 (Orbit 720)
---------------------------------------
Vector Time (GMT): 2010/064/21:41:01
676
Vector Time (MET): N/A
Weight (LBS) : 799531
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5771963
58 A = 6730609
91 meter
Y = -2805557
26 meter E =
0015080
Z = 2020797
36 I = 51
87437
XDOT = 583
501458 Wp = 80
48912
YDOT = -5256
640037 meter/sec RA = 40
23025 deg
ZDOT = -5593
708915 TA = 77
06602
MA = 76
89763
Ha = 192
125 n
mi
Hp = 182
740
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18936888
39 X = -5749978
95
Y = -9204584
20 feet Y = -2869979
78 meter
Z = 6629912
60 Z = 1992810
90
XDOT = 1914
374862 XDOT = 669
411787
YDOT = -17246
194346 feet/sec YDOT = -5249
634862 meter/sec
ZDOT = -18352
063370 ZDOT = -5590
665392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4432861
15 X = 1351136
08
Y = 20618981
74 feet Y = 6284665
63 meter
Z = 6518679
89 Z = 1986893
63
XDOT = -13330
426295 XDOT = -4063
113935
YDOT = 8703
837318 feet/sec YDOT = 2652
929614 meter/sec
ZDOT = -18340
088354 ZDOT = -5590
058930
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 10064
93918942
00016717 00000-0 10270-3 0 9148
2 25544 51
6417 40
6333 0007846 13
2784 346
8584 15
73948406 7210
Satellite: ISS
Catalog Number: 25544
Epoch time: 10064
93918942 = yrday
fracday
Element set: 914
Inclination: 51
6417 deg
RA of node: 40
6333 deg
Eccentricity:
0007846
Arg of perigee: 13
2784 deg
Mean anomaly: 346
8584 deg
Mean motion: 15
73948406 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 721
Checksum: 322
Coasting Arc #16 (Orbit 736)
---------------------------------------
Vector Time (GMT): 2010/065/21:41:01
676
Vector Time (MET): N/A
Weight (LBS) : 799531
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -89431
55 A = 6722071
80 meter
Y = 4622037
31 meter E =
0008945
Z = 4871785
73 I = 51
82068
XDOT = -6872
325786 Wp = 64
80733
YDOT = -2593
180352 meter/sec RA = 35
14590 deg
ZDOT = 2334
506765 TA = 2
53125
MA = 2
52673
Ha = 192
281 n
mi
Hp = 182
541
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -293410
60 X = -164775
35
Y = 15164164
41 feet Y = 4620616
10 meter
Z = 15983548
97 Z = 4871168
13
XDOT = -22547
000611 XDOT = -6854
158107
YDOT = -8507
809555 feet/sec YDOT = -2669
929132 meter/sec
ZDOT = 7659
142931 ZDOT = 2301
165567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12029580
01 X = 3666615
99
Y = -9241349
85 feet Y = -2816763
43 meter
Z = 15981191
05 Z = 4871067
03
XDOT = 6930
003683 XDOT = 2112
265122
YDOT = 22034
422381 feet/sec YDOT = 6716
091942 meter/sec
ZDOT = 7526
645799 ZDOT = 2294
121640
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 10065
95507556
00016717 00000-0 10270-3 0 9157
2 25544 51
6407 35
4162 0007703 18
9839 341
1609 15
73914451 7372
Satellite: ISS
Catalog Number: 25544
Epoch time: 10065
95507556 = yrday
fracday
Element set: 915
Inclination: 51
6407 deg
RA of node: 35
4162 deg
Eccentricity:
0007703
Arg of perigee: 18
9839 deg
Mean anomaly: 341
1609 deg
Mean motion: 15
73914451 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 737
Checksum: 313
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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