Date:
November 6th 2010
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14262 18 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 90 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 45 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 538)
---------------------------------------
Vector Time (GMT): 2010/307/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1470534
10 A = 6727536
77 meter
Y = -4598580
06 meter E =
0014631
Z = 4681345
38 I = 51
34578
XDOT = 5573
946877 Wp = 137
64797
YDOT = 4565
071625 meter/sec RA = 236
87858 deg
ZDOT = 2717
840736 TA = 285
40164
MA = 285
56323
Ha = 194
834 n
mi
Hp = 184
909
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4824586
95 X = 1499105
27
Y = -15087204
91 feet Y = -4581975
70 meter
Z = 15358744
68 Z = 4688559
02
XDOT = 18287
227287 XDOT = 5509
282003
YDOT = 14977
269112 feet/sec YDOT = 4627
041411 meter/sec
ZDOT = 8916
800314 ZDOT = 2744
762392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6542042
70 X = 1994014
61
Y = 14394887
68 feet Y = 4387561
77 meter
Z = 15387667
63 Z = 4690161
09
XDOT = -22525
282251 XDOT = -6865
706030
YDOT = 535
282424 feet/sec YDOT = 163
154083 meter/sec
ZDOT = 9024
764560 ZDOT = 2750
748238
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 10307
55247034
00016717 00000-0 10270-3 0 9008
2 25544 51
6442 237
5145 0007727 157
8011 202
3488 15
72274503 5397
Satellite: ISS
Catalog Number: 25544
Epoch time: 10307
55247034 = yrday
fracday
Element set: 900
Inclination: 51
6442 deg
RA of node: 237
5145 deg
Eccentricity:
0007727
Arg of perigee: 157
8011 deg
Mean anomaly: 202
3488 deg
Mean motion: 15
72274503 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 539
Checksum: 289
Coasting Arc #2 (Orbit 553)
---------------------------------------
Vector Time (GMT): 2010/308/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5299523
99 A = 6733446
28 meter
Y = -3028128
09 meter E =
0008459
Z = -2856124
46 I = 51
38371
XDOT = 579
466099 Wp = 128
41430
YDOT = -5769
965861 meter/sec RA = 231
69163 deg
ZDOT = 5047
185091 TA = 198
73594
MA = 198
76709
Ha = 194
735 n
mi
Hp = 184
975
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17386889
74 X = -5251394
07
Y = -9934803
43 feet Y = -3087121
51 meter
Z = -9370487
08 Z = -2881753
34
XDOT = 1901
135494 XDOT = 619
424804
YDOT = -18930
334189 feet/sec YDOT = -5763
262377 meter/sec
ZDOT = 16559
006204 ZDOT = 5050
097427
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19463054
37 X = 5932338
97
Y = -4500771
43 feet Y = -1371835
13 meter
Z = -9473270
47 Z = -2887452
84
XDOT = 11222
496491 XDOT = 3420
616931
YDOT = 13685
913192 feet/sec YDOT = 4171
466341 meter/sec
ZDOT = 16570
679635 ZDOT = 5050
743153
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 10308
50586330
00016717 00000-0 10270-3 0 9010
2 25544 51
6444 232
6310 0007621 160
8998 199
2451 15
72284280 5544
Satellite: ISS
Catalog Number: 25544
Epoch time: 10308
50586330 = yrday
fracday
Element set: 901
Inclination: 51
6444 deg
RA of node: 232
6310 deg
Eccentricity:
0007621
Arg of perigee: 160
8998 deg
Mean anomaly: 199
2451 deg
Mean motion: 15
72284280 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 554
Checksum: 298
Coasting Arc #3 (Orbit 569)
---------------------------------------
Vector Time (GMT): 2010/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 492043
62 A = 6729553
94 meter
Y = 5304509
63 meter E =
0010458
Z = -4116518
53 I = 51
39170
XDOT = -6307
158953 Wp = 117
28421
YDOT = -2314
044517 meter/sec RA = 226
60009 deg
ZDOT = -3747
752083 TA = 114
20311
MA = 114
09377
Ha = 194
553 n
mi
Hp = 185
094
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1614316
34 X = 452688
99
Y = 17403246
80 feet Y = 5309791
92 meter
Z = -13505638
23 Z = -4114223
69
XDOT = -20692
778718 XDOT = -6262
607613
YDOT = -7592
009571 feet/sec YDOT = -2384
325853 meter/sec
ZDOT = -12295
774549 ZDOT = -3778
285045
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13274247
76 X = -4045990
72
Y = -11380772
26 feet Y = -3468859
38 meter
Z = -13496430
99 Z = -4113712
17
XDOT = 19302
763955 XDOT = 5883
482454
YDOT = -7834
252244 feet/sec YDOT = -2387
880084 meter/sec
ZDOT = -12418
231635 ZDOT = -3785
077002
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 10309
52278861
00016717 00000-0 10270-3 0 9021
2 25544 51
6453 227
4220 0007606 164
2898 195
8502 15
72342924 5703
Satellite: ISS
Catalog Number: 25544
Epoch time: 10309
52278861 = yrday
fracday
Element set: 902
Inclination: 51
6453 deg
RA of node: 227
4220 deg
Eccentricity:
0007606
Arg of perigee: 164
2898 deg
Mean anomaly: 195
8502 deg
Mean motion: 15
72342924 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 570
Checksum: 308
Coasting Arc #4 (Orbit 585)
---------------------------------------
Vector Time (GMT): 2010/310/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5544128
65 A = 6730885
35 meter
Y = 985230
70 meter E =
0014652
Z = 3670440
81 I = 51
41780
XDOT = 1765
849880 Wp = 115
62125
YDOT = 6140
240785 meter/sec RA = 221
41003 deg
ZDOT = -4308
377954 TA = 20
06813
MA = 20
01057
Ha = 194
331 n
mi
Hp = 185
219
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18189398
44 X = 5514868
65
Y = 3232384
19 feet Y = 1047064
77 meter
Z = 12042128
65 Z = 3697304
01
XDOT = 5793
470736 XDOT = 1717
987315
YDOT = 20145
146931 feet/sec YDOT = 6159
720094 meter/sec
ZDOT = -14135
098275 ZDOT = -4299
915260
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15130735
63 X = -4611848
22
Y = 10476484
57 feet Y = 3193232
50 meter
Z = 12149876
38 Z = 3703282
32
XDOT = -17603
842025 XDOT = -5365
651049
YDOT = -9044
243458 feet/sec YDOT = -2756
685406 meter/sec
ZDOT = -14101
153573 ZDOT = -4298
031609
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 10310
53968776
00016717 00000-0 10270-3 0 9036
2 25544 51
6448 222
2136 0007644 168
4602 191
6737 15
72359136 5861
Satellite: ISS
Catalog Number: 25544
Epoch time: 10310
53968776 = yrday
fracday
Element set: 903
Inclination: 51
6448 deg
RA of node: 222
2136 deg
Eccentricity:
0007644
Arg of perigee: 168
4602 deg
Mean anomaly: 191
6737 deg
Mean motion: 15
72359136 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 586
Checksum: 321
Coasting Arc #5 (Orbit 601)
---------------------------------------
Vector Time (GMT): 2010/311/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2561727
22 A = 6731818
47 meter
Y = -5225957
04 meter E =
0015494
Z = 3378956
23 I = 51
44484
XDOT = 6164
759816 Wp = 118
96128
YDOT = -26
883483 meter/sec RA = 216
32345 deg
ZDOT = 4608
871139 TA = 280
98348
MA = 281
15774
Ha = 194
288 n
mi
Hp = 185
356
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8404616
86 X = -2519514
04
Y = -17145528
36 feet Y = -5254367
97 meter
Z = 11085814
41 Z = 3366613
27
XDOT = 20225
589946 XDOT = 6142
212534
YDOT = -88
200402 feet/sec YDOT = 41
928258 meter/sec
ZDOT = 15120
968305 ZDOT = 4638
765643
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18196894
32 X = 5546413
39
Y = 5880056
57 feet Y = 1792241
24 meter
Z = 11036302
84 Z = 3363865
11
XDOT = -13545
714524 XDOT = -4128
733787
YDOT = 13169
777358 feet/sec YDOT = 4014
148139 meter/sec
ZDOT = 15240
888068 ZDOT = 4645
422683
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 10311
55655944
00016717 00000-0 10270-3 0 9040
2 25544 51
6450 217
0042 0007569 172
5572 187
5704 15
72403753 6022
Satellite: ISS
Catalog Number: 25544
Epoch time: 10311
55655944 = yrday
fracday
Element set: 904
Inclination: 51
6450 deg
RA of node: 217
0042 deg
Eccentricity:
0007569
Arg of perigee: 172
5572 deg
Mean anomaly: 187
5704 deg
Mean motion: 15
72403753 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 602
Checksum: 296
Coasting Arc #6 (Orbit 616)
---------------------------------------
Vector Time (GMT): 2010/312/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5067865
56 A = 6728345
07 meter
Y = 970191
23 meter E =
0013898
Z = -4332103
62 I = 51
45929
XDOT = -4000
792752 Wp = 140
70098
YDOT = -5601
088917 meter/sec RA = 211
13696 deg
ZDOT = 3421
315883 TA = 164
00585
MA = 163
96192
Ha = 194
048 n
mi
Hp = 185
330
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16626855
52 X = -5057292
67
Y = 3183042
10 feet Y = 913578
72 meter
Z = -14212938
39 Z = -4356698
17
XDOT = -13125
960472 XDOT = -3954
483524
YDOT = -18376
275975 feet/sec YDOT = -5645
569485 meter/sec
ZDOT = 11224
789642 ZDOT = 3401
991670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9007116
24 X = 2745369
03
Y = -14235214
91 feet Y = -4338893
51 meter
Z = -14311611
12 Z = -4362179
07
XDOT = 21387
552319 XDOT = 6518
925947
YDOT = 2310
545518 feet/sec YDOT = 704
254274 meter/sec
ZDOT = 11147
264397 ZDOT = 3397
686188
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 10312
50985192
00016717 00000-0 10270-3 0 9058
2 25544 51
6452 212
1204 0007518 176
8087 183
3124 15
72453485 6175
Satellite: ISS
Catalog Number: 25544
Epoch time: 10312
50985192 = yrday
fracday
Element set: 905
Inclination: 51
6452 deg
RA of node: 212
1204 deg
Eccentricity:
0007518
Arg of perigee: 176
8087 deg
Mean anomaly: 183
3124 deg
Mean motion: 15
72453485 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 617
Checksum: 297
Coasting Arc #7 (Orbit 632)
---------------------------------------
Vector Time (GMT): 2010/313/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4353328
23 A = 6733663
91 meter
Y = 4425520
80 meter E =
0011430
Z = -2595544
23 I = 51
50374
XDOT = -5236
501466 Wp = 160
99594
YDOT = 2084
420956 meter/sec RA = 206
04841 deg
ZDOT = -5245
875893 TA = 48
53396
MA = 48
43587
Ha = 193
952 n
mi
Hp = 185
664
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14282572
95 X = 4316126
62
Y = 14519425
19 feet Y = 4473994
51 meter
Z = -8515565
04 Z = -2574485
39
XDOT = -17180
122920 XDOT = -5233
936638
YDOT = 6838
651432 feet/sec YDOT = 2025
877961 meter/sec
ZDOT = -17210
878913 ZDOT = -5271
308942
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20383960
96 X = -6213031
30
Y = 855377
34 feet Y = 260719
01 meter
Z = -8431068
19 Z = -2569789
59
XDOT = 6476
309953 XDOT = 1973
979274
YDOT = -15754
866526 feet/sec YDOT = -4802
083317 meter/sec
ZDOT = -17312
929933 ZDOT = -5276
981044
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 10313
52667213
00016717 00000-0 10270-3 0 9063
2 25544 51
6452 206
9108 0007603 181
8520 178
2616 15
72469730 6339
Satellite: ISS
Catalog Number: 25544
Epoch time: 10313
52667213 = yrday
fracday
Element set: 906
Inclination: 51
6452 deg
RA of node: 206
9108 deg
Eccentricity:
0007603
Arg of perigee: 181
8520 deg
Mean anomaly: 178
2616 deg
Mean motion: 15
72469730 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 633
Checksum: 296
Coasting Arc #8 (Orbit 648)
---------------------------------------
Vector Time (GMT): 2010/314/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3938834
32 A = 6726133
64 meter
Y = -2580554
84 meter E =
0006491
Z = 4796844
05 I = 51
50700
XDOT = 5860
111006 Wp = 126
00478
YDOT = 4342
844343 meter/sec RA = 200
87357 deg
ZDOT = -2477
024572 TA = 348
24579
MA = 348
26093
Ha = 193
489 n
mi
Hp = 185
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12922684
78 X = 3944095
26
Y = -8466387
26 feet Y = -2536479
32 meter
Z = 15737677
33 Z = 4815991
82
XDOT = 19226
085977 XDOT = 5823
146097
YDOT = 14248
176977 feet/sec YDOT = 4408
169106 meter/sec
ZDOT = -8126
721038 ZDOT = -2448
645214
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2091574
50 X = -637511
91
Y = 15227485
20 feet Y = 4641337
49 meter
Z = 15814518
44 Z = 4820265
22
XDOT = -22309
246770 XDOT = -6799
858416
YDOT = 5252
607750 feet/sec YDOT = 1600
994842 meter/sec
ZDOT = -8012
833753 ZDOT = -2442
311728
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 10314
54346459
00016717 00000-0 10270-3 0 9073
2 25544 51
6447 201
7011 0007413 186
0552 174
0522 15
72571996 6495
Satellite: ISS
Catalog Number: 25544
Epoch time: 10314
54346459 = yrday
fracday
Element set: 907
Inclination: 51
6447 deg
RA of node: 201
7011 deg
Eccentricity:
0007413
Arg of perigee: 186
0552 deg
Mean anomaly: 174
0522 deg
Mean motion: 15
72571996 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 649
Checksum: 302
Coasting Arc #9 (Orbit 664)
---------------------------------------
Vector Time (GMT): 2010/315/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5746082
86 A = 6735007
42 meter
Y = -3052356
36 meter E =
0011536
Z = 1732780
84 I = 51
56541
XDOT = 3668
587034 Wp = 96
29614
YDOT = -3656
427000 meter/sec RA = 195
77656 deg
ZDOT = 5690
871311 TA = 282
88364
MA = 283
01249
Ha = 193
476 n
mi
Hp = 185
929
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18851977
90 X = -5719941
42
Y = -10014292
50 feet Y = -3116466
43 meter
Z = 5684976
53 Z = 1704929
36
XDOT = 12036
046701 XDOT = 3681
555645
YDOT = -11996
151576 feet/sec YDOT = -3615
330441 meter/sec
ZDOT = 18670
837635 ZDOT = 5708
724845
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19846259
84 X = 6049140
00
Y = -7941510
26 feet Y = -2420572
33 meter
Z = 5573191
92 Z = 1698708
90
XDOT = 869
478482 XDOT = 265
017041
YDOT = 15404
934389 feet/sec YDOT = 4695
424002 meter/sec
ZDOT = 18742
492295 ZDOT = 5712
711652
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 10315
56023314
00016717 00000-0 10270-3 0 9089
2 25544 51
6447 196
4905 0007387 189
8877 170
2141 15
72567244 6652
Satellite: ISS
Catalog Number: 25544
Epoch time: 10315
56023314 = yrday
fracday
Element set: 908
Inclination: 51
6447 deg
RA of node: 196
4905 deg
Eccentricity:
0007387
Arg of perigee: 189
8877 deg
Mean anomaly: 170
2141 deg
Mean motion: 15
72567244 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 665
Checksum: 325
Coasting Arc #10 (Orbit 679)
---------------------------------------
Vector Time (GMT): 2010/316/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2405499
78 A = 6724734
12 meter
Y = 3672483
94 meter E =
0015401
Z = -5106267
20 I = 51
56106
XDOT = -7096
626207 Wp = 130
28767
YDOT = -2545
920154 meter/sec RA = 190
61773 deg
ZDOT = 1505
280109 TA = 154
22608
MA = 154
14926
Ha = 193
209 n
mi
Hp = 185
934
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7892059
65 X = -2421581
79
Y = 12048831
84 feet Y = 3645494
46 meter
Z = -16752845
15 Z = -5117992
19
XDOT = -23282
894379 XDOT = -7074
942276
YDOT = -8352
756410 feet/sec YDOT = -2625
157708 meter/sec
ZDOT = 4938
583036 ZDOT = 1470
856878
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4394899
99 X = -1339565
52
Y = -13658871
85 feet Y = -4163224
14 meter
Z = -16799906
20 Z = -5120611
41
XDOT = 20226
252670 XDOT = 6164
961814
YDOT = -12439
712223 feet/sec YDOT = -3791
624285 meter/sec
ZDOT = 4800
405392 ZDOT = 1463
163563
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 10316
51342816
00016717 00000-0 10270-3 0 9097
2 25544 51
6446 191
6055 0007409 194
3748 165
7204 15
72626332 6807
Satellite: ISS
Catalog Number: 25544
Epoch time: 10316
51342816 = yrday
fracday
Element set: 909
Inclination: 51
6446 deg
RA of node: 191
6055 deg
Eccentricity:
0007409
Arg of perigee: 194
3748 deg
Mean anomaly: 165
7204 deg
Mean motion: 15
72626332 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 680
Checksum: 308
Coasting Arc #11 (Orbit 695)
---------------------------------------
Vector Time (GMT): 2010/317/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6528668
79 A = 6735820
02 meter
Y = 1345189
00 meter E =
0015687
Z = -899199
17 I = 51
62830
XDOT = -1755
247467 Wp = 165
50213
YDOT = 4565
123907 meter/sec RA = 185
51104 deg
ZDOT = -5951
847487 TA = 24
31582
MA = 24
24188
Ha = 193
209 n
mi
Hp = 186
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21419517
02 X = 6517509
60
Y = 4413349
74 feet Y = 1418134
13 meter
Z = -2950128
51 Z = -867509
59
XDOT = -5758
685915 XDOT = -1777
251725
YDOT = 14977
440640 feet/sec YDOT = 4545
372758 meter/sec
ZDOT = -19527
058686 ZDOT = -5960
427943
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16745702
94 X = -5104090
26
Y = 14092169
04 feet Y = 4295293
12 meter
Z = -2822911
29 Z = -860423
36
XDOT = -7232
261056 XDOT = -2204
393170
YDOT = -12487
071641 feet/sec YDOT = -3806
059436 meter/sec
ZDOT = -19561
498334 ZDOT = -5962
344692
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 10317
53014612
00016717 00000-0 10270-3 0 9102
2 25544 51
6447 186
3956 0007593 198
4150 161
6739 15
72609094 6966
Satellite: ISS
Catalog Number: 25544
Epoch time: 10317
53014612 = yrday
fracday
Element set: 910
Inclination: 51
6447 deg
RA of node: 186
3956 deg
Eccentricity:
0007593
Arg of perigee: 198
4150 deg
Mean anomaly: 161
6739 deg
Mean motion: 15
72609094 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 696
Checksum: 322
Coasting Arc #12 (Orbit 711)
---------------------------------------
Vector Time (GMT): 2010/318/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 624169
58 A = 6723880
92 meter
Y = -4154221
26 meter E =
0005841
Z = 5249958
95 I = 51
61935
XDOT = 7665
787911 Wp = 183
64987
YDOT = 477
109207 meter/sec RA = 180
37148 deg
ZDOT = -539
616569 TA = 271
44600
MA = 271
51292
Ha = 192
839 n
mi
Hp = 186
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2047800
44 X = 645072
75
Y = -13629334
85 feet Y = -4147124
59 meter
Z = 17224274
77 Z = 5253041
95
XDOT = 25150
222804 XDOT = 7662
504440
YDOT = 1565
318922 feet/sec YDOT = 562
814304 meter/sec
ZDOT = -1770
395566 ZDOT = -502
383613
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9662516
00 X = 2945134
88
Y = 9806207
68 feet Y = 2988932
10 meter
Z = 17236646
20 Z = 5253729
76
XDOT = -15776
661399 XDOT = -4808
726394
YDOT = 18361
424044 feet/sec YDOT = 5596
562049 meter/sec
ZDOT = -1620
912327 ZDOT = -494
054077
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 10318
54683608
00016717 00000-0 10270-3 0 9112
2 25544 51
6446 181
1847 0007398 202
9172 157
1661 15
72699680 7128
Satellite: ISS
Catalog Number: 25544
Epoch time: 10318
54683608 = yrday
fracday
Element set: 911
Inclination: 51
6446 deg
RA of node: 181
1847 deg
Eccentricity:
0007398
Arg of perigee: 202
9172 deg
Mean anomaly: 157
1661 deg
Mean motion: 15
72699680 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 712
Checksum: 324
Coasting Arc #13 (Orbit 727)
---------------------------------------
Vector Time (GMT): 2010/319/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6714827
42 A = 6735748
11 meter
Y = 508714
10 meter E =
0005767
Z = 61969
43 I = 51
68933
XDOT = -300
820329 Wp = 69
68660
YDOT = -4760
935670 meter/sec RA = 175
25099 deg
ZDOT = 6036
917595 TA = 290
98534
MA = 291
04703
Ha = 192
599 n
mi
Hp = 186
483
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22030273
68 X = -6720317
93
Y = 1669009
52 feet Y = 433594
16 meter
Z = 203311
77 Z = 29334
90
XDOT = -986
943336 XDOT = -276
887065
YDOT = -15619
867685 feet/sec YDOT = -4764
165808 meter/sec
ZDOT = 19806
160088 ZDOT = 6035
514318
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11702071
17 X = 3566791
29
Y = -18740762
85 feet Y = -5712184
52 meter
Z = 72280
97 Z = 22031
24
XDOT = 11873
288658 XDOT = 3618
978383
YDOT = 7506
285694 feet/sec YDOT = 2287
915880 meter/sec
ZDOT = 19800
518999 ZDOT = 6035
198191
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 10319
56350090
00016717 00000-0 10270-3 0 9122
2 25544 51
6437 175
9731 0007389 207
5046 152
5727 15
72745027 7288
Satellite: ISS
Catalog Number: 25544
Epoch time: 10319
56350090 = yrday
fracday
Element set: 912
Inclination: 51
6437 deg
RA of node: 175
9731 deg
Eccentricity:
0007389
Arg of perigee: 207
5046 deg
Mean anomaly: 152
5727 deg
Mean motion: 15
72745027 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 728
Checksum: 314
Coasting Arc #14 (Orbit 742)
---------------------------------------
Vector Time (GMT): 2010/320/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1117432
78 A = 6723628
97 meter
Y = 4034104
68 meter E =
0012352
Z = -5270801
29 I = 51
67785
XDOT = -7512
969988 Wp = 116
43132
YDOT = 1604
561476 meter/sec RA = 170
13038 deg
ZDOT = -370
759334 TA = 150
08134
MA = 150
01069
Ha = 192
368 n
mi
Hp = 186
644
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3666118
05 X = 1097844
76
Y = 13235251
56 feet Y = 4046490
96 meter
Z = -17292655
14 Z = -5265420
27
XDOT = -24648
851668 XDOT = -7528
552987
YDOT = 5264
309305 feet/sec YDOT = 1520
459796 meter/sec
ZDOT = -1216
402014 ZDOT = -407
295958
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12976885
79 X = -3955354
79
Y = -4578176
07 feet Y = -1395428
07 meter
Z = -17271044
16 Z = -5264214
26
XDOT = 9620
235332 XDOT = 2932
247729
YDOT = -22201
424730 feet/sec YDOT = -6766
994258 meter/sec
ZDOT = -1363
110540 ZDOT = -415
476093
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 10320
51660159
00016717 00000-0 10270-3 0 9130
2 25544 51
6425 171
0870 0007335 211
5751 148
4973 15
72782157 7434
Satellite: ISS
Catalog Number: 25544
Epoch time: 10320
51660159 = yrday
fracday
Element set: 913
Inclination: 51
6425 deg
RA of node: 171
0870 deg
Eccentricity:
0007335
Arg of perigee: 211
5751 deg
Mean anomaly: 148
4973 deg
Mean motion: 15
72782157 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 743
Checksum: 298
Coasting Arc #15 (Orbit 758)
---------------------------------------
Vector Time (GMT): 2010/321/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 829939
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6294034
16 A = 6735329
35 meter
Y = -2262235
28 meter E =
0015476
Z = 705387
72 I = 51
74764
XDOT = 2220
609343 Wp = 155
77653
YDOT = 4298
662350 meter/sec RA = 164
99995 deg
ZDOT = -5995
568435 TA = 16
54799
MA = 16
49754
Ha = 192
150 n
mi
Hp = 186
752
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20649718
37 X = 6315436
37
Y = -7422031
77 feet Y = -2191731
94 meter
Z = 2314264
16 Z = 736016
86
XDOT = 7285
463725 XDOT = 2201
501962
YDOT = 14103
222933 feet/sec YDOT = 4323
387735 meter/sec
ZDOT = -19670
500114 ZDOT = -5984
826841
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5513174
99 X = -1680415
74
Y = 21225406
89 feet Y = 6469504
02 meter
Z = 2437262
12 Z = 742877
49
XDOT = -14272
278610 XDOT = -4350
190520
YDOT = -1441
812959 feet/sec YDOT = -439
464590 meter/sec
ZDOT = -19627
364008 ZDOT = -5982
420550
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 10321
53321732
00016717 00000-0 10270-3 0 9145
2 25544 51
6428 165
8767 0007315 215
7212 144
3462 15
72810719 7590
Satellite: ISS
Catalog Number: 25544
Epoch time: 10321
53321732 = yrday
fracday
Element set: 914
Inclination: 51
6428 deg
RA of node: 165
8767 deg
Eccentricity:
0007315
Arg of perigee: 215
7212 deg
Mean anomaly: 144
3462 deg
Mean motion: 15
72810719 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 759
Checksum: 299
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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