Date:
October 6th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 88 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 34 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 66)
---------------------------------------
Vector Time (GMT): 2010/277/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2649213
89 A = 6726902
63 meter
Y = 3239412
65 meter E =
0009773
Z = 5259790
53 I = 51
80059
XDOT = -6367
547676 Wp = 61
70143
YDOT = -4301
166933 meter/sec RA = 30
79287 deg
ZDOT = -552
832224 TA = 33
56864
MA = 33
50675
Ha = 196
203 n
mi
Hp = 185
111
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8691646
60 X = -2710791
90
Y = 10627994
25 feet Y = 3209443
73 meter
Z = 17256530
61 Z = 5246770
73
XDOT = -20890
904449 XDOT = -6316
292410
YDOT = -14111
440068 feet/sec YDOT = -4372
086144 meter/sec
ZDOT = -1813
754015 ZDOT = -583
640980
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6329862
29 X = 1929342
03
Y = -12256902
95 feet Y = -3735904
02 meter
Z = 17204301
92 Z = 5243871
23
XDOT = 22511
346407 XDOT = 6861
458385
YDOT = 8881
815906 feet/sec YDOT = 2707
177488 meter/sec
ZDOT = -1937
260469 ZDOT = -590
476991
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 10277
54673488
00016717 00000-0 10270-3 0 9009
2 25544 51
6453 31
1070 0006920 60
8349 299
3505 15
71652633 670
Satellite: ISS
Catalog Number: 25544
Epoch time: 10277
54673488 = yrday
fracday
Element set: 900
Inclination: 51
6453 deg
RA of node: 31
1070 deg
Eccentricity:
0006920
Arg of perigee: 60
8349 deg
Mean anomaly: 299
3505 deg
Mean motion: 15
71652633 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 67
Checksum: 303
Coasting Arc #2 (Orbit 81)
---------------------------------------
Vector Time (GMT): 2010/278/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6158767
18 A = 6738869
10 meter
Y = 2700502
51 meter E =
0018423
Z = -300377
47 I = 51
81470
XDOT = -1676
582868 Wp = 50
53149
YDOT = 4467
226678 meter/sec RA = 25
68981 deg
ZDOT = 6042
483243 TA = 306
21405
MA = 306
38424
Ha = 196
213 n
mi
Hp = 185
034
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20205929
08 X = 6129571
12
Y = 8859916
37 feet Y = 2769210
27 meter
Z = -985490
37 Z = -270529
17
XDOT = -5500
599960 XDOT = -1755
765130
YDOT = 14656
255504 feet/sec YDOT = 4448
036055 meter/sec
ZDOT = 19824
420090 ZDOT = 6034
145516
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21705892
62 X = -6615956
07
Y = -3981638
26 feet Y = -1213603
34 meter
Z = -865830
12 Z = -263905
02
XDOT = 1811
779680 XDOT = 552
230446
YDOT = -13972
538201 feet/sec YDOT = -4258
829644 meter/sec
ZDOT = 19790
957494 ZDOT = 6032
283844
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 10278
50050882
00016717 00000-0 10270-3 0 9014
2 25544 51
6460 26
2269 0007018 64
0485 296
1400 15
71640394 826
Satellite: ISS
Catalog Number: 25544
Epoch time: 10278
50050882 = yrday
fracday
Element set: 901
Inclination: 51
6460 deg
RA of node: 26
2269 deg
Eccentricity:
0007018
Arg of perigee: 64
0485 deg
Mean anomaly: 296
1400 deg
Mean motion: 15
71640394 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 82
Checksum: 284
Coasting Arc #3 (Orbit 97)
---------------------------------------
Vector Time (GMT): 2010/279/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 203088
23 A = 6727203
11 meter
Y = -4295929
13 meter E =
0021128
Z = -5191366
51 I = 51
74819
XDOT = 7378
766743 Wp = 76
36162
YDOT = 1777
688764 meter/sec RA = 20
59526 deg
ZDOT = -1181
540999 TA = 182
33757
MA = 182
34746
Ha = 196
133 n
mi
Hp = 184
996
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 666299
97 X = 276330
07
Y = -14094255
69 feet Y = -4293249
16 meter
Z = -17032042
37 Z = -5190201
50
XDOT = 24208
552305 XDOT = 7364
079676
YDOT = 5832
312218 feet/sec YDOT = 1860
120313 meter/sec
ZDOT = -3876
446848 ZDOT = -1145
730362
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2728573
53 X = 831669
21
Y = 13849443
67 feet Y = 4221310
43 meter
Z = -17027338
69 Z = -5189932
83
XDOT = -23911
194629 XDOT = -7288
132123
YDOT = 118
001439 feet/sec YDOT = 35
966839 meter/sec
ZDOT = -3732
883015 ZDOT = -1137
782743
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 10279
51785357
00016717 00000-0 10270-3 0 9029
2 25544 51
6463 21
0215 0006907 67
4987 292
6906 15
71664210 985
Satellite: ISS
Catalog Number: 25544
Epoch time: 10279
51785357 = yrday
fracday
Element set: 902
Inclination: 51
6463 deg
RA of node: 21
0215 deg
Eccentricity:
0006907
Arg of perigee: 67
4987 deg
Mean anomaly: 292
6906 deg
Mean motion: 15
71664210 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 98
Checksum: 318
Coasting Arc #4 (Orbit 113)
---------------------------------------
Vector Time (GMT): 2010/280/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6490644
08 A = 6737528
23 meter
Y = -369570
03 meter E =
0019802
Z = 1743181
01 I = 51
75395
XDOT = -1260
349222 Wp = 100
91166
YDOT = -5014
292071 meter/sec RA = 15
46031 deg
ZDOT = -5705
073075 TA = 59
83371
MA = 59
63767
Ha = 196
213 n
mi
Hp = 184
915
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21294764
03 X = -6494497
29
Y = -1212500
10 feet Y = -442173
68 meter
Z = 5719097
80 Z = 1711639
54
XDOT = -4135
004009 XDOT = -1176
470059
YDOT = -16451
089473 feet/sec YDOT = -5027
917658 meter/sec
ZDOT = -18717
431349 ZDOT = -5710
991696
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20896382
35 X = 6369217
34
Y = -4439448
63 feet Y = -1353143
94 meter
Z = 5592648
05 Z = 1704639
13
XDOT = 7885
064175 XDOT = 2403
367561
YDOT = 13290
565724 feet/sec YDOT = 4050
964433 meter/sec
ZDOT = -18741
116784 ZDOT = -5712
292396
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 10280
53518503
00016717 00000-0 10270-3 0 9031
2 25544 51
6461 15
8159 0007047 72
0336 288
1594 15
71681399 1146
Satellite: ISS
Catalog Number: 25544
Epoch time: 10280
53518503 = yrday
fracday
Element set: 903
Inclination: 51
6461 deg
RA of node: 15
8159 deg
Eccentricity:
0007047
Arg of perigee: 72
0336 deg
Mean anomaly: 288
1594 deg
Mean motion: 15
71681399 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 114
Checksum: 301
Coasting Arc #5 (Orbit 129)
---------------------------------------
Vector Time (GMT): 2010/281/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2393538
17 A = 6729036
64 meter
Y = 4193331
21 meter E =
0013808
Z = 4675881
64 I = 51
69726
XDOT = -7119
287134 Wp = 96
96778
YDOT = 938
654818 meter/sec RA = 10
38544 deg
ZDOT = 2793
847979 TA = 325
46813
MA = 325
55775
Ha = 196
042 n
mi
Hp = 184
762
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7852815
52 X = 2323754
55
Y = 13757648
33 feet Y = 4219707
40 meter
Z = 15340819
04 Z = 4687339
87
XDOT = -23357
241253 XDOT = -7142
826546
YDOT = 3079
576175 feet/sec YDOT = 858
911287 meter/sec
ZDOT = 9166
167911 ZDOT = 2759
204420
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11298209
43 X = -3443694
23
Y = -11039921
21 feet Y = -3364967
99 meter
Z = 15386712
81 Z = 4689870
06
XDOT = 20811
883686 XDOT = 6343
462148
YDOT = -8677
693511 feet/sec YDOT = -2644
960982 meter/sec
ZDOT = 9027
276469 ZDOT = 2751
513868
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 10281
55250011
00016717 00000-0 10270-3 0 9042
2 25544 51
6467 10
6097 0007004 74
8677 285
3259 15
71744242 1309
Satellite: ISS
Catalog Number: 25544
Epoch time: 10281
55250011 = yrday
fracday
Element set: 904
Inclination: 51
6467 deg
RA of node: 10
6097 deg
Eccentricity:
0007004
Arg of perigee: 74
8677 deg
Mean anomaly: 285
3259 deg
Mean motion: 15
71744242 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 130
Checksum: 285
Coasting Arc #6 (Orbit 144)
---------------------------------------
Vector Time (GMT): 2010/282/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5675959
00 A = 6734627
21 meter
Y = -1923314
75 meter E =
0011524
Z = -3078319
04 I = 51
68529
XDOT = 4099
497443 Wp = 74
87688
YDOT = 4270
193739 meter/sec RA = 5
22685 deg
ZDOT = 4909
043936 TA = 249
50868
MA = 249
63241
Ha = 196
161 n
mi
Hp = 184
834
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18621912
71 X = 5711998
29
Y = -6310087
77 feet Y = -1859641
43 meter
Z = -10099471
92 Z = -3050656
90
XDOT = 13449
794760 XDOT = 4027
594816
YDOT = 14009
821977 feet/sec YDOT = 4315
635027 meter/sec
ZDOT = 16105
787192 ZDOT = 4928
784893
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15976257
82 X = -4869563
38
Y = 11557682
79 feet Y = 3522781
71 meter
Z = -9988559
87 Z = -3044513
05
XDOT = -16059
997569 XDOT = -4895
087259
YDOT = -8264
399195 feet/sec YDOT = -2518
988875 meter/sec
ZDOT = 16184
876230 ZDOT = 4933
150275
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 10282
50622257
00016717 00000-0 10270-3 0 9054
2 25544 51
6464 5
7301 0007011 77
0898 283
1046 15
71728062 1455
Satellite: ISS
Catalog Number: 25544
Epoch time: 10282
50622257 = yrday
fracday
Element set: 905
Inclination: 51
6464 deg
RA of node: 5
7301 deg
Eccentricity:
0007011
Arg of perigee: 77
0898 deg
Mean anomaly: 283
1046 deg
Mean motion: 15
71728062 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 145
Checksum: 283
Coasting Arc #7 (Orbit 160)
---------------------------------------
Vector Time (GMT): 2010/283/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4610720
94 A = 6732096
20 meter
Y = -3058504
35 meter E =
0013571
Z = -3848884
72 I = 51
64598
XDOT = 5602
336817 Wp = 77
24914
YDOT = -3255
267256 meter/sec RA =
16068 deg
ZDOT = -4133
742063 TA = 149
48718
MA = 149
40816
Ha = 196
118 n
mi
Hp = 184
610
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15127037
19 X = -4557479
86
Y = -10034463
08 feet Y = -3109766
63 meter
Z = -12627574
54 Z = -3871154
70
XDOT = 18380
370136 XDOT = 5658
402880
YDOT = -10680
010684 feet/sec YDOT = -3192
305210 meter/sec
ZDOT = -13562
145876 ZDOT = -4106
388982
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17433410
22 X = 5313703
44
Y = 4830350
42 feet Y = 1472290
81 meter
Z = -12716810
33 Z = -3876083
79
XDOT = -13847
704363 XDOT = -4220
780290
YDOT = 14641
799597 feet/sec YDOT = 4462
820517 meter/sec
ZDOT = -13452
455590 ZDOT = -4100
308464
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 10283
52351211
00016717 00000-0 10270-3 0 9067
2 25544 51
6455
5238 0007076 81
2101 278
9862 15
71745956 1619
Satellite: ISS
Catalog Number: 25544
Epoch time: 10283
52351211 = yrday
fracday
Element set: 906
Inclination: 51
6455 deg
RA of node:
5238 deg
Eccentricity:
0007076
Arg of perigee: 81
2101 deg
Mean anomaly: 278
9862 deg
Mean motion: 15
71745956 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 161
Checksum: 290
Coasting Arc #8 (Orbit 176)
---------------------------------------
Vector Time (GMT): 2010/284/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3927458
62 A = 6731196
76 meter
Y = 3603480
54 meter E =
0017669
Z = 4098355
17 I = 51
61336
XDOT = -6236
816969 Wp = 78
70428
YDOT = -2467
399344 meter/sec RA = 354
99042 deg
ZDOT = -3790
137132 TA = 50
25006
MA = 50
09453
Ha = 196
119 n
mi
Hp = 184
594
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12885362
92 X = -3987370
97
Y = 11822442
70 feet Y = 3559226
41 meter
Z = 13446047
13 Z = 4079129
60
XDOT = -20461
997929 XDOT = -6190
350339
YDOT = -8095
142206 feet/sec YDOT = -2536
883426 meter/sec
ZDOT = -12434
833111 ZDOT = -3820
323295
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8358365
64 X = 2547629
85
Y = -15427519
03 feet Y = -4702307
80 meter
Z = 13368930
13 Z = 4074849
90
XDOT = 20790
980039 XDOT = 6337
090716
YDOT = 334
748399 feet/sec YDOT = 102
031312 meter/sec
ZDOT = -12555
807528 ZDOT = -3827
010135
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 10284
54078600
00016717 00000-0 10270-3 0 9079
2 25544 51
6459 355
3171 0007088 83
1519 277
0449 15
71811890 1776
Satellite: ISS
Catalog Number: 25544
Epoch time: 10284
54078600 = yrday
fracday
Element set: 907
Inclination: 51
6459 deg
RA of node: 355
3171 deg
Eccentricity:
0007088
Arg of perigee: 83
1519 deg
Mean anomaly: 277
0449 deg
Mean motion: 15
71811890 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 177
Checksum: 319
Coasting Arc #9 (Orbit 192)
---------------------------------------
Vector Time (GMT): 2010/285/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6056872
30 A = 6735161
41 meter
Y = 1104114
20 meter E =
0020737
Z = 2708938
29 I = 51
59619
XDOT = -3190
208052 Wp = 81
63987
YDOT = 4732
495876 meter/sec RA = 349
91794 deg
ZDOT = 5173
396551 TA = 309
28574
MA = 309
46948
Ha = 196
032 n
mi
Hp = 184
503
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19871628
27 X = 6030915
98
Y = 3622421
92 feet Y = 1171700
68 meter
Z = 8887592
80 Z = 2738299
99
XDOT = -10466
561849 XDOT = -3268
022425
YDOT = 15526
561272 feet/sec YDOT = 4696
386011 meter/sec
ZDOT = 16973
085796 ZDOT = 5157
709217
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19851931
44 X = -6050868
70
Y = 3434907
86 feet Y = 1046959
92 meter
Z = 9005280
80 Z = 2744809
59
XDOT = 4813
965496 XDOT = 1467
296683
YDOT = -16771
336363 feet/sec YDOT = -5111
903323 meter/sec
ZDOT = 16910
134873 ZDOT = 5154
209109
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 10285
55804727
00016717 00000-0 10270-3 0 9089
2 25544 51
6453 350
1108 0007194 87
4278 272
7708 15
71807045 1935
Satellite: ISS
Catalog Number: 25544
Epoch time: 10285
55804727 = yrday
fracday
Element set: 908
Inclination: 51
6453 deg
RA of node: 350
1108 deg
Eccentricity:
0007194
Arg of perigee: 87
4278 deg
Mean anomaly: 272
7708 deg
Mean motion: 15
71807045 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 193
Checksum: 318
Coasting Arc #10 (Orbit 207)
---------------------------------------
Vector Time (GMT): 2010/286/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1567677
61 A = 6728276
93 meter
Y = -4416063
65 meter E =
0018970
Z = -4845403
27 I = 51
54262
XDOT = 7301
853239 Wp = 100
31398
YDOT = -23
909360 meter/sec RA = 344
75242 deg
ZDOT = 2388
815024 TA = 193
05654
MA = 193
10572
Ha = 196
092 n
mi
Hp = 184
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5143299
24 X = 1640480
72
Y = -14488397
80 feet Y = -4398125
92 meter
Z = -15896992
35 Z = -4837610
51
XDOT = 23956
211413 XDOT = 7289
973327
YDOT = -78
442782 feet/sec YDOT = 57
677949 meter/sec
ZDOT = 7837
319632 ZDOT = 2424
259008
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 345971
40 X = 105452
08
Y = 15402651
06 feet Y = 4694728
04 meter
Z = -15865692
80 Z = -4835863
16
XDOT = -21145
637421 XDOT = -6445
190286
YDOT = 8678
717770 feet/sec YDOT = 2645
273176 meter/sec
ZDOT = 7979
406465 ZDOT = 2432
123091
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 10286
51171662
00016717 00000-0 10270-3 0 9092
2 25544 51
6447 345
2295 0007250 89
5671 270
6322 15
71821859 2088
Satellite: ISS
Catalog Number: 25544
Epoch time: 10286
51171662 = yrday
fracday
Element set: 909
Inclination: 51
6447 deg
RA of node: 345
2295 deg
Eccentricity:
0007250
Arg of perigee: 89
5671 deg
Mean anomaly: 270
6322 deg
Mean motion: 15
71821859 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 208
Checksum: 314
Coasting Arc #11 (Orbit 223)
---------------------------------------
Vector Time (GMT): 2010/287/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6471615
25 A = 6737314
29 meter
Y = 1165241
27 meter E =
0014246
Z = -1456865
84 I = 51
54509
XDOT = 383
944899 Wp = 119
07648
YDOT = -5049
010149 meter/sec RA = 339
65924 deg
ZDOT = -5793
228622 TA = 76
95833
MA = 76
79934
Ha = 196
038 n
mi
Hp = 184
384
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21232333
51 X = -6477086
95
Y = 3822970
06 feet Y = 1092841
16 meter
Z = -4779743
56 Z = -1488318
55
XDOT = 1259
661741 XDOT = 468
518051
YDOT = -16564
993928 feet/sec YDOT = -5044
243888 meter/sec
ZDOT = -19006
655583 ZDOT = -5791
157870
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18198094
37 X = 5546779
16
Y = -11534083
06 feet Y = -3515588
52 meter
Z = -4905845
92 Z = -1495301
84
XDOT = 4132
601623 XDOT = 1259
616975
YDOT = 14533
815913 feet/sec YDOT = 4429
907090 meter/sec
ZDOT = -18998
287471 ZDOT = -5790
678021
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 10287
52895007
00016717 00000-0 10270-3 0 9102
2 25544 51
6452 340
0223 0007349 92
9729 267
2274 15
71854403 2246
Satellite: ISS
Catalog Number: 25544
Epoch time: 10287
52895007 = yrday
fracday
Element set: 910
Inclination: 51
6452 deg
RA of node: 340
0223 deg
Eccentricity:
0007349
Arg of perigee: 92
9729 deg
Mean anomaly: 267
2274 deg
Mean motion: 15
71854403 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 224
Checksum: 302
Coasting Arc #12 (Orbit 239)
---------------------------------------
Vector Time (GMT): 2010/288/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 895848
78 A = 6726387
63 meter
Y = 4159444
05 meter E =
0010166
Z = 5201123
44 I = 51
48018
XDOT = -7182
314306 Wp = 84
05646
YDOT = 2649
127855 meter/sec RA = 334
51011 deg
ZDOT = -878
965076 TA = 14
34124
MA = 14
31241
Ha = 195
947 n
mi
Hp = 184
401
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2939136
42 X = 824004
21
Y = 13646469
97 feet Y = 4169060
44 meter
Z = 17064053
28 Z = 5205300
85
XDOT = -23564
023314 XDOT = -7207
133648
YDOT = 8691
364353 feet/sec YDOT = 2568
672098 meter/sec
ZDOT = -2883
743688 ZDOT = -913
917405
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7970934
75 X = -2429540
91
Y = -11434983
61 feet Y = -3485383
00 meter
Z = 17080747
32 Z = 5206211
78
XDOT = 17405
080034 XDOT = 5305
068394
YDOT = -16661
615866 feet/sec YDOT = -5078
460516 meter/sec
ZDOT = -3023
892257 ZDOT = -921
682360
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 10288
54616780
00016717 00000-0 10270-3 0 9115
2 25544 51
6449 334
8158 0007238 96
6854 263
5132 15
71890230 2405
Satellite: ISS
Catalog Number: 25544
Epoch time: 10288
54616780 = yrday
fracday
Element set: 911
Inclination: 51
6449 deg
RA of node: 334
8158 deg
Eccentricity:
0007238
Arg of perigee: 96
6854 deg
Mean anomaly: 263
5132 deg
Mean motion: 15
71890230 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 240
Checksum: 314
Coasting Arc #13 (Orbit 255)
---------------------------------------
Vector Time (GMT): 2010/289/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5823243
05 A = 6738299
50 meter
Y = -3378973
69 meter E =
0017992
Z = 71888
99 I = 51
49296
XDOT = 2338
991647 Wp = 64
75854
YDOT = 4183
874925 meter/sec RA = 329
38851 deg
ZDOT = 6022
670919 TA = 296
02325
MA = 296
20841
Ha = 196
096 n
mi
Hp = 184
396
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19105128
11 X = 5860245
33
Y = -11085871
67 feet Y = -3313647
79 meter
Z = 235856
27 Z = 100268
58
XDOT = 7673
857109 XDOT = 2262
775665
YDOT = 13726
623770 feet/sec YDOT = 4209
605095 meter/sec
ZDOT = 19759
419027 ZDOT = 6033
848486
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12905921
46 X = -3933724
86
Y = 17924090
71 feet Y = 5463262
85 meter
Z = 349660
69 Z = 106576
58
XDOT = -11198
918352 XDOT = -3413
430314
YDOT = -8500
196136 feet/sec YDOT = -2590
859782 meter/sec
ZDOT = 19804
177494 ZDOT = 6036
313300
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 10289
56337512
00016717 00000-0 10270-3 0 9122
2 25544 51
6448 329
6087 0007383 98
2628 261
9371 15
71850112 2564
Satellite: ISS
Catalog Number: 25544
Epoch time: 10289
56337512 = yrday
fracday
Element set: 912
Inclination: 51
6448 deg
RA of node: 329
6087 deg
Eccentricity:
0007383
Arg of perigee: 98
2628 deg
Mean anomaly: 261
9371 deg
Mean motion: 15
71850112 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 256
Checksum: 320
Coasting Arc #14 (Orbit 270)
---------------------------------------
Vector Time (GMT): 2010/290/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3042885
60 A = 6726250
64 meter
Y = -2956807
29 meter E =
0021946
Z = -5238116
81 I = 51
42807
XDOT = 5887
651775 Wp = 90
72800
YDOT = -4888
597325 meter/sec RA = 324
26071 deg
ZDOT = -663
367523 TA = 172
94561
MA = 172
91467
Ha = 195
992 n
mi
Hp = 184
269
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9983220
46 X = -2984149
80
Y = -9700811
33 feet Y = -2990506
61 meter
Z = -17185422
60 Z = -5252756
42
XDOT = 19316
442831 XDOT = 5945
101939
YDOT = -16038
705135 feet/sec YDOT = -4822
436886 meter/sec
ZDOT = -2176
402635 ZDOT = -634
625171
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13063533
45 X = 3981765
00
Y = 4592946
14 feet Y = 1399929
98 meter
Z = -17244074
95 Z = -5255994
04
XDOT = -10363
790972 XDOT = -3158
883488
YDOT = 21771
630308 feet/sec YDOT = 6635
992918 meter/sec
ZDOT = -2061
133992 ZDOT = -628
233641
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 10290
51698978
00016717 00000-0 10270-3 0 9136
2 25544 51
6456 324
7268 0007357 103
2143 256
9840 15
71892872 2711
Satellite: ISS
Catalog Number: 25544
Epoch time: 10290
51698978 = yrday
fracday
Element set: 913
Inclination: 51
6456 deg
RA of node: 324
7268 deg
Eccentricity:
0007357
Arg of perigee: 103
2143 deg
Mean anomaly: 256
9840 deg
Mean motion: 15
71892872 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 271
Checksum: 331
Coasting Arc #15 (Orbit 286)
---------------------------------------
Vector Time (GMT): 2010/291/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 812637
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4309727
46 A = 6737424
48 meter
Y = 5020356
21 meter E =
0021155
Z = 1221883
78 I = 51
44127
XDOT = -4417
005357 Wp = 116
00914
YDOT = -2349
714842 meter/sec RA = 319
10944 deg
ZDOT = -5855
818602 TA = 50
56205
MA = 50
37502
Ha = 195
942 n
mi
Hp = 184
313
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14139525
77 X = -4371481
46
Y = 16470984
93 feet Y = 4971817
05 meter
Z = 4008805
05 Z = 1200796
47
XDOT = -14491
487393 XDOT = -4361
955256
YDOT = -7709
038196 feet/sec YDOT = -2398
801103 meter/sec
ZDOT = -19212
003286 ZDOT = -5877
142782
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5476522
48 X = 1669244
05
Y = -21021374
49 feet Y = -6407314
94 meter
Z = 3924228
29 Z = 1196104
78
XDOT = 14769
854224 XDOT = 4501
851567
YDOT = 202
159995 feet/sec YDOT = 61
618366 meter/sec
ZDOT = -19297
456825 ZDOT = -5881
864840
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 10291
53416597
00016717 00000-0 10270-3 0 9145
2 25544 51
6447 319
5195 0007468 106
0566 254
1419 15
71942389 2873
Satellite: ISS
Catalog Number: 25544
Epoch time: 10291
53416597 = yrday
fracday
Element set: 914
Inclination: 51
6447 deg
RA of node: 319
5195 deg
Eccentricity:
0007468
Arg of perigee: 106
0566 deg
Mean anomaly: 254
1419 deg
Mean motion: 15
71942389 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 287
Checksum: 332
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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