[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
April 6th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13185 79 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 122 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 ET - UTC (sec) : 67 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 2341)
---------------------------------------
Vector Time (GMT): 2013/095/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2315772
67 A = 6786733
02 meter
Y = 4450485
33 meter E =
0020384
Z = -4590671
12 I = 51
96980
XDOT = -4355
750622 Wp = 109
46426
YDOT = 5465
909763 meter/sec RA = 108
20919 deg
ZDOT = 3106
363827 TA = 191
55105
MA = 191
59789
Ha = 228
133 n
mi
Hp = 214
391
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7597679
38 X = 2288134
42
Y = 14601329
84 feet Y = 4476226
77 meter
Z = -15061256
97 Z = -4579488
93
XDOT = -14290
520412 XDOT = -4431
637674
YDOT = 17932
774812 feet/sec YDOT = 5416
777015 meter/sec
ZDOT = 10191
482372 ZDOT = 3085
019212
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10808256
80 X = 3294356
67
Y = 12469667
89 feet Y = 3800754
77 meter
Z = -15015125
51 Z = -4576610
25
XDOT = -8991
105787 XDOT = -2740
489044
YDOT = 19938
751047 feet/sec YDOT = 6077
331319 meter/sec
ZDOT = 10101
839682 ZDOT = 3079
040735
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 13095
51060533
00016717 00000-0 10270-3 0 9008
2 25544 51
6448 109
0796 0010440 108
5171 251
7116 15
51989879 23420
Satellite: ISS
Catalog Number: 25544
Epoch time: 13095
51060533 = yrday
fracday
Element set: 900
Inclination: 51
6448 deg
RA of node: 109
0796 deg
Eccentricity:
0010440
Arg of perigee: 108
5171 deg
Mean anomaly: 251
7116 deg
Mean motion: 15
51989879 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2342
Checksum: 302
Coasting Arc #2 (Orbit 2357)
---------------------------------------
Vector Time (GMT): 2013/096/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1969920
35 A = 6788758
98 meter
Y = -5135708
94 meter E =
0020636
Z = 3959598
96 I = 51
98438
XDOT = 4389
460773 Wp = 95
54274
YDOT = -4819
669882 meter/sec RA = 103
25920 deg
ZDOT = -4051
330987 TA = 36
59342
MA = 36
45262
Ha = 228
075 n
mi
Hp = 214
281
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6462993
28 X = -1931579
97
Y = -16849438
79 feet Y = -5157523
01 meter
Z = 12990810
24 Z = 3950123
00
XDOT = 14401
118022 XDOT = 4462
709350
YDOT = -15812
565230 feet/sec YDOT = -4770
175072 meter/sec
ZDOT = -13291
768329 ZDOT = -4029
828960
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10457102
64 X = -3187324
88
Y = -14742215
22 feet Y = -4493427
20 meter
Z = 12951876
90 Z = 3947732
08
XDOT = 9110
586751 XDOT = 2776
906842
YDOT = -18107
364631 feet/sec YDOT = -5519
124740 meter/sec
ZDOT = -13201
534133 ZDOT = -4023
827604
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 13096
54083594
00016717 00000-0 10270-3 0 9015
2 25544 51
6433 103
9591 0010441 111
9970 248
2292 15
52053534 23580
Satellite: ISS
Catalog Number: 25544
Epoch time: 13096
54083594 = yrday
fracday
Element set: 901
Inclination: 51
6433 deg
RA of node: 103
9591 deg
Eccentricity:
0010441
Arg of perigee: 111
9970 deg
Mean anomaly: 248
2292 deg
Mean motion: 15
52053534 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2358
Checksum: 299
Coasting Arc #3 (Orbit 2372)
---------------------------------------
Vector Time (GMT): 2013/097/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1713975
23 A = 6791009
92 meter
Y = 5731016
92 meter E =
0014482
Z = -3231238
01 I = 51
99791
XDOT = -4387
796139 Wp = 104
97535
YDOT = 4017
850504 meter/sec RA = 98
31457 deg
ZDOT = 4813
066725 TA = 217
92942
MA = 218
03151
Ha = 228
017 n
mi
Hp = 214
375
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5623278
31 X = 1665458
89
Y = 18802548
97 feet Y = 5749912
01 meter
Z = -10601174
58 Z = -3223030
20
XDOT = -14395
656623 XDOT = -4455
779112
YDOT = 13181
924225 feet/sec YDOT = 3968
403876 meter/sec
ZDOT = 15790
901330 ZDOT = 4791
585553
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10393458
76 X = 3167926
23
Y = 16668645
20 feet Y = 5080603
06 meter
Z = -10567605
75 Z = -3221006
23
XDOT = -9339
385846 XDOT = -2846
644806
YDOT = 15747
511980 feet/sec YDOT = 4799
841652 meter/sec
ZDOT = 15700
839149 ZDOT = 4785
615773
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 13097
50666530
00016717 00000-0 10270-3 0 9020
2 25544 51
6433 99
1600 0010489 115
3231 244
9008 15
52044675 23738
Satellite: ISS
Catalog Number: 25544
Epoch time: 13097
50666530 = yrday
fracday
Element set: 902
Inclination: 51
6433 deg
RA of node: 99
1600 deg
Eccentricity:
0010489
Arg of perigee: 115
3231 deg
Mean anomaly: 244
9008 deg
Mean motion: 15
52044675 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2373
Checksum: 292
Coasting Arc #4 (Orbit 2388)
---------------------------------------
Vector Time (GMT): 2013/098/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1449113
82 A = 6793001
70 meter
Y = -6204901
26 meter E =
0024051
Z = 2319327
62 I = 52
00756
XDOT = 4441
511357 Wp = 112
20684
YDOT = -3085
763622 meter/sec RA = 93
37197 deg
ZDOT = -5444
205359 TA = 42
07079
MA = 41
88636
Ha = 227
891 n
mi
Hp = 214
375
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4754310
44 X = -1390888
32
Y = -20357287
59 feet Y = -6220780
32 meter
Z = 7609342
58 Z = 2312430
10
XDOT = 14571
887654 XDOT = 4502
133563
YDOT = -10123
896399 feet/sec YDOT = -3035
757553 meter/sec
ZDOT = -17861
566137 ZDOT = -5422
481140
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10257157
82 X = -3126381
70
Y = -18227431
72 feet Y = -5555721
19 meter
Z = 7581303
75 Z = 2310781
38
XDOT = 9969
679707 XDOT = 3038
758375
YDOT = -13050
980580 feet/sec YDOT = -3977
938881 meter/sec
ZDOT = -17770
592826 ZDOT = -5416
476693
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 13098
53686856
00016717 00000-0 10270-3 0 9038
2 25544 51
6424 94
0387 0010351 118
7240 241
4953 15
52092065 23893
Satellite: ISS
Catalog Number: 25544
Epoch time: 13098
53686856 = yrday
fracday
Element set: 903
Inclination: 51
6424 deg
RA of node: 94
0387 deg
Eccentricity:
0010351
Arg of perigee: 118
7240 deg
Mean anomaly: 241
4953 deg
Mean motion: 15
52092065 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2389
Checksum: 315
Coasting Arc #5 (Orbit 2403)
---------------------------------------
Vector Time (GMT): 2013/099/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1254652
00 A = 6794377
73 meter
Y = 6535716
28 meter E =
0014213
Z = -1377299
35 I = 52
01304
XDOT = -4501
022763 Wp = 85
32796
YDOT = 2082
438660 meter/sec RA = 88
43389 deg
ZDOT = 5834
476384 TA = 259
77193
MA = 259
93224
Ha = 227
849 n
mi
Hp = 214
380
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4116312
33 X = 1188165
59
Y = 21442638
71 feet Y = 6549374
68 meter
Z = -4518698
66 Z = -1371366
56
XDOT = -14767
135050 XDOT = -4552
317107
YDOT = 6832
147834 feet/sec YDOT = 2031
819264 meter/sec
ZDOT = 19141
982887 ZDOT = 5812
485767
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10259995
09 X = 3127246
50
Y = 19278985
36 feet Y = 5876234
74 meter
Z = -4494735
14 Z = -1369995
27
XDOT = -10815
077774 XDOT = -3296
435705
YDOT = 10156
327563 feet/sec YDOT = 3095
648641 meter/sec
ZDOT = 19050
012488 ZDOT = 5806
443806
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 13099
50267172
00016717 00000-0 10270-3 0 9043
2 25544 51
6422 89
2394 0010539 122
7992 237
4176 15
52117479 24049
Satellite: ISS
Catalog Number: 25544
Epoch time: 13099
50267172 = yrday
fracday
Element set: 904
Inclination: 51
6422 deg
RA of node: 89
2394 deg
Eccentricity:
0010539
Arg of perigee: 122
7992 deg
Mean anomaly: 237
4176 deg
Mean motion: 15
52117479 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2404
Checksum: 316
Coasting Arc #6 (Orbit 2419)
---------------------------------------
Vector Time (GMT): 2013/100/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1006290
39 A = 6795140
26 meter
Y = -6702550
08 meter E =
0022902
Z = 308129
69 I = 52
01399
XDOT = 4630
943578 Wp = 128
88519
YDOT = -985
872843 meter/sec RA = 83
49615 deg
ZDOT = -6035
158343 TA = 47
81147
MA = 47
61725
Ha = 227
731 n
mi
Hp = 214
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3301477
66 X = -932763
08
Y = -21989993
69 feet Y = -6713391
90 meter
Z = 1010924
18 Z = 303420
46
XDOT = 15193
384442 XDOT = 4670
941192
YDOT = -3234
490954 feet/sec YDOT = -933
863707 meter/sec
ZDOT = -19800
388265 ZDOT = -6012
564085
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9964724
84 X = -3037248
13
Y = -19879676
67 feet Y = -6059325
45 meter
Z = 992098
46 Z = 302391
61
XDOT = 12106
778824 XDOT = 3690
146185
YDOT = -7099
721397 feet/sec YDOT = -2163
995082 meter/sec
ZDOT = -19706
029144 ZDOT = -6006
397683
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 13100
53284730
00016717 00000-0 10270-3 0 9059
2 25544 51
6424 84
1179 0010294 125
8187 234
3922 15
52120416 24202
Satellite: ISS
Catalog Number: 25544
Epoch time: 13100
53284730 = yrday
fracday
Element set: 905
Inclination: 51
6424 deg
RA of node: 84
1179 deg
Eccentricity:
0010294
Arg of perigee: 125
8187 deg
Mean anomaly: 234
3922 deg
Mean motion: 15
52120416 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2420
Checksum: 275
Coasting Arc #7 (Orbit 2435)
---------------------------------------
Vector Time (GMT): 2013/101/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 792135
81 A = 6794788
57 meter
Y = 6708488
43 meter E =
0018479
Z = 709529
45 I = 52
00890
XDOT = -4784
825216 Wp = 86
07980
YDOT = -81
926720 meter/sec RA = 78
56006 deg
ZDOT = 5983
744498 TA = 281
53703
MA = 281
74445
Ha = 227
618 n
mi
Hp = 214
511
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2598870
77 X = 713614
43
Y = 22009476
49 feet Y = 6716907
62 meter
Z = 2327852
52 Z = 713186
31
XDOT = -15698
245458 XDOT = -4812
621326
YDOT = -268
788452 feet/sec YDOT = -135
588538 meter/sec
ZDOT = 19631
707671 ZDOT = 5960
432389
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9628072
03 X = 2934636
36
Y = 19960061
84 feet Y = 6083826
85 meter
Z = 2342272
82 Z = 713924
76
XDOT = -13584
171331 XDOT = -4140
455422
YDOT = 4209
426042 feet/sec YDOT = 1283
033057 meter/sec
ZDOT = 19534
484318 ZDOT = 5954
110820
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 13101
56300644
00016717 00000-0 10270-3 0 9067
2 25544 51
6423 78
9984 0010428 130
8153 229
3905 15
52178152 24366
Satellite: ISS
Catalog Number: 25544
Epoch time: 13101
56300644 = yrday
fracday
Element set: 906
Inclination: 51
6423 deg
RA of node: 78
9984 deg
Eccentricity:
0010428
Arg of perigee: 130
8153 deg
Mean anomaly: 229
3905 deg
Mean motion: 15
52178152 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2436
Checksum: 297
Coasting Arc #8 (Orbit 2450)
---------------------------------------
Vector Time (GMT): 2013/102/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -473469
26 A = 6793718
89 meter
Y = -6534435
85 meter E =
0017568
Z = -1776943
25 I = 51
99910
XDOT = 4988
268975 Wp = 136
49891
YDOT = 1176
374911 meter/sec RA = 73
62140 deg
ZDOT = -5700
834548 TA = 62
90291
MA = 62
72380
Ha = 227
534 n
mi
Hp = 214
680
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1553376
84 X = -391732
56
Y = -21438437
84 feet Y = -6539273
60 meter
Z = -5829866
31 Z = -1779044
36
XDOT = 16365
711859 XDOT = 5002
437303
YDOT = 3859
497740 feet/sec YDOT = 1232
235698 meter/sec
ZDOT = -18703
525420 ZDOT = -5676
567277
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8771916
73 X = -2673680
22
Y = -19620918
85 feet Y = -5980456
07 meter
Z = -5837804
23 Z = -1779362
73
XDOT = 15374
300766 XDOT = 4686
086873
YDOT = -1383
213704 feet/sec YDOT = -421
603537 meter/sec
ZDOT = -18602
455757 ZDOT = -5670
028515
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 13102
52877055
00016717 00000-0 10270-3 0 9070
2 25544 51
6433 74
1973 0010193 133
1659 227
0347 15
52158268 24517
Satellite: ISS
Catalog Number: 25544
Epoch time: 13102
52877055 = yrday
fracday
Element set: 907
Inclination: 51
6433 deg
RA of node: 74
1973 deg
Eccentricity:
0010193
Arg of perigee: 133
1659 deg
Mean anomaly: 227
0347 deg
Mean motion: 15
52158268 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2451
Checksum: 301
Coasting Arc #9 (Orbit 2466)
---------------------------------------
Vector Time (GMT): 2013/103/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 151996
23 A = 6791797
56 meter
Y = 6220572
06 meter E =
0020679
Z = 2711841
26 I = 51
98396
XDOT = -5204
105467 Wp = 103
56963
YDOT = -2155
852816 meter/sec RA = 68
68111 deg
ZDOT = 5198
960572 TA = 286
90213
MA = 287
12876
Ha = 227
384 n
mi
Hp = 214
740
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 498675
30 X = 69251
58
Y = 20408701
00 feet Y = 6221809
27 meter
Z = 8897117
00 Z = 2712378
34
XDOT = -17073
836834 XDOT = -5204
866995
YDOT = -7073
007928 feet/sec YDOT = -2214
052385 meter/sec
ZDOT = 17056
957257 ZDOT = 5173
677387
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7736624
73 X = 2358123
22
Y = 18891340
89 feet Y = 5758080
70 meter
Z = 8898557
27 Z = 2712280
26
XDOT = -17194
682422 XDOT = -5240
939202
YDOT = -1001
782627 feet/sec YDOT = -305
343345 meter/sec
ZDOT = 16951
777381 ZDOT = 5166
901746
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 13103
55890114
00016717 00000-0 10270-3 0 9086
2 25544 51
6436 69
0781 0010234 138
1197 222
0740 15
52213045 24672
Satellite: ISS
Catalog Number: 25544
Epoch time: 13103
55890114 = yrday
fracday
Element set: 908
Inclination: 51
6436 deg
RA of node: 69
0781 deg
Eccentricity:
0010234
Arg of perigee: 138
1197 deg
Mean anomaly: 222
0740 deg
Mean motion: 15
52213045 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2467
Checksum: 282
Coasting Arc #10 (Orbit 2481)
---------------------------------------
Vector Time (GMT): 2013/104/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 311483
77 A = 6789423
57 meter
Y = -5745603
98 meter E =
0013699
Z = -3607266
80 I = 51
96468
XDOT = 5411
649151 Wp = 120
87288
YDOT = 3081
586461 meter/sec RA = 63
73502 deg
ZDOT = -4460
380332 TA = 101
53310
MA = 101
37925
Ha = 227
309 n
mi
Hp = 214
878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1021928
36 X = 393232
55
Y = -18850406
77 feet Y = -5741663
84 meter
Z = -11834864
84 Z = -3605554
82
XDOT = 17754
754433 XDOT = 5398
455587
YDOT = 10110
191802 feet/sec YDOT = 3142
028981 meter/sec
ZDOT = -14633
793740 ZDOT = -4434
122857
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6049941
88 X = -1844022
28
Y = -17887624
20 feet Y = -5452147
85 meter
Z = -11826973
52 Z = -3604861
53
XDOT = 19028
411500 XDOT = 5799
859825
YDOT = 3125
642387 feet/sec YDOT = 952
695800 meter/sec
ZDOT = -14524
673601 ZDOT = -4427
120514
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 13104
52463744
00016717 00000-0 10270-3 0 9090
2 25544 51
6443 64
2772 0010089 140
5706 219
6182 15
52206439 24826
Satellite: ISS
Catalog Number: 25544
Epoch time: 13104
52463744 = yrday
fracday
Element set: 909
Inclination: 51
6443 deg
RA of node: 64
2772 deg
Eccentricity:
0010089
Arg of perigee: 140
5706 deg
Mean anomaly: 219
6182 deg
Mean motion: 15
52206439 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2482
Checksum: 300
Coasting Arc #11 (Orbit 2497)
---------------------------------------
Vector Time (GMT): 2013/105/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -799019
24 A = 6786957
36 meter
Y = 5182161
08 meter E =
0018825
Z = 4303227
18 I = 51
94297
XDOT = -5594
576595 Wp = 126
39593
YDOT = -3843
125821 meter/sec RA = 58
78573 deg
ZDOT = 3567
574384 TA = 287
28128
MA = 287
48717
Ha = 227
148 n
mi
Hp = 214
973
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2621454
20 X = -877812
03
Y = 17001840
82 feet Y = 5172785
54 meter
Z = 14118199
40 Z = 4299154
01
XDOT = -18354
910087 XDOT = -5568
516633
YDOT = -12608
680515 feet/sec YDOT = -3905
542070 meter/sec
ZDOT = 11704
640366 ZDOT = 3540
459572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4149260
41 X = 1264694
57
Y = 16709788
87 feet Y = 5093143
65 meter
Z = 14100523
45 Z = 4297839
55
XDOT = -20669
455091 XDOT = -6300
049912
YDOT = -4709
621421 feet/sec YDOT = -1435
492609 meter/sec
ZDOT = 11592
048724 ZDOT = 3533
256451
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 13105
55473875
00016717 00000-0 10270-3 0 9102
2 25544 51
6448 59
1580 0010096 145
5626 214
6181 15
52256981 24983
Satellite: ISS
Catalog Number: 25544
Epoch time: 13105
55473875 = yrday
fracday
Element set: 910
Inclination: 51
6448 deg
RA of node: 59
1580 deg
Eccentricity:
0010096
Arg of perigee: 145
5626 deg
Mean anomaly: 214
6181 deg
Mean motion: 15
52256981 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2498
Checksum: 319
Coasting Arc #12 (Orbit 2512)
---------------------------------------
Vector Time (GMT): 2013/106/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1434802
74 A = 6784810
11 meter
Y = -4509198
94 meter E =
0017221
Z = -4874645
57 I = 51
91919
XDOT = 5687
168428 Wp = 106
48282
YDOT = 4481
512918 meter/sec RA = 53
82898 deg
ZDOT = -2483
589090 TA = 139
23949
MA = 139
11052
Ha = 227
079 n
mi
Hp = 215
134
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4707358
08 X = 1508798
84
Y = -14793959
77 feet Y = -4492740
50 meter
Z = -15992931
65 Z = -4867495
48
XDOT = 18658
689068 XDOT = 5648
697212
YDOT = 14703
126371 feet/sec YDOT = 4544
895230 meter/sec
ZDOT = -8148
258168 ZDOT = -2456
054699
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1622366
77 X = -494497
39
Y = -15471287
61 feet Y = -4715648
46 meter
Z = -15962503
39 Z = -4865371
03
XDOT = 21941
224248 XDOT = 6687
685151
YDOT = 5947
529070 feet/sec YDOT = 1812
806861 meter/sec
ZDOT = -8034
006297 ZDOT = -2448
765119
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 13106
52044725
00016717 00000-0 10270-3 0 9119
2 25544 51
6450 54
3568 0010010 148
2650 211
9107 15
52248052 25138
Satellite: ISS
Catalog Number: 25544
Epoch time: 13106
52044725 = yrday
fracday
Element set: 911
Inclination: 51
6450 deg
RA of node: 54
3568 deg
Eccentricity:
0010010
Arg of perigee: 148
2650 deg
Mean anomaly: 211
9107 deg
Mean motion: 15
52248052 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2513
Checksum: 261
Coasting Arc #13 (Orbit 2528)
---------------------------------------
Vector Time (GMT): 2013/107/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2088181
49 A = 6783224
95 meter
Y = 3811941
63 meter E =
0013830
Z = 5202958
99 I = 51
89593
XDOT = -5704
888749 Wp = 144
19205
YDOT = -4952
077753 meter/sec RA = 48
87002 deg
ZDOT = 1325
793259 TA = 293
04531
MA = 293
19109
Ha = 226
913 n
mi
Hp = 215
229
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6850989
15 X = -2155926
98
Y = 12506370
16 feet Y = 3788211
67 meter
Z = 17070075
44 Z = 5192650
04
XDOT = -18716
826603 XDOT = -5655
529939
YDOT = -16246
974254 feet/sec YDOT = -5015
597383 meter/sec
ZDOT = 4349
715418 ZDOT = 1298
199319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1026613
65 X = -312911
84
Y = 14274983
79 feet Y = 4351015
06 meter
Z = 17026559
39 Z = 5189695
30
XDOT = -22808
550659 XDOT = -6952
046241
YDOT = -6741
850549 feet/sec YDOT = -2054
916047 meter/sec
ZDOT = 4235
283738 ZDOT = 1290
914483
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 13107
55051882
00016717 00000-0 10270-3 0 9126
2 25544 51
6454 49
2374 0009954 153
0122 207
1549 15
52302001 25292
Satellite: ISS
Catalog Number: 25544
Epoch time: 13107
55051882 = yrday
fracday
Element set: 912
Inclination: 51
6454 deg
RA of node: 49
2374 deg
Eccentricity:
0009954
Arg of perigee: 153
0122 deg
Mean anomaly: 207
1549 deg
Mean motion: 15
52302001 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2529
Checksum: 282
Coasting Arc #14 (Orbit 2543)
---------------------------------------
Vector Time (GMT): 2013/108/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2854578
63 A = 6782731
06 meter
Y = -3075353
63 meter E =
0020936
Z = -5345335
93 I = 51
87323
XDOT = 5552
045151 Wp = 115
10538
YDOT = 5264
537992 meter/sec RA = 43
90508 deg
ZDOT = -72
762691 TA = 154
25417
MA = 154
14981
Ha = 226
824 n
mi
Hp = 215
450
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9365415
44 X = 2914722
06
Y = -10089742
88 feet Y = -3043095
89 meter
Z = -17537191
37 Z = -5331322
35
XDOT = 18215
371231 XDOT = 5493
116780
YDOT = 17272
106272 feet/sec YDOT = 5326
294969 meter/sec
ZDOT = -238
722738 ZDOT = -45
934588
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4101908
09 X = 1250261
58
Y = -13219292
71 feet Y = -4029240
42 meter
Z = -17478319
40 Z = -5327391
75
XDOT = 22974
335157 XDOT = 7002
577356
YDOT = 7258
917175 feet/sec YDOT = 2212
517955 meter/sec
ZDOT = -127
533643 ZDOT = -38
872254
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 13108
51619930
00016717 00000-0 10270-3 0 9138
2 25544 51
6455 44
4358 0009923 155
9930 204
1686 15
52285603 25440
Satellite: ISS
Catalog Number: 25544
Epoch time: 13108
51619930 = yrday
fracday
Element set: 913
Inclination: 51
6455 deg
RA of node: 44
4358 deg
Eccentricity:
0009923
Arg of perigee: 155
9930 deg
Mean anomaly: 204
1686 deg
Mean motion: 15
52285603 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2544
Checksum: 312
Coasting Arc #15 (Orbit 2559)
---------------------------------------
Vector Time (GMT): 2013/109/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 904217
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3600698
17 A = 6783062
18 meter
Y = 2371343
85 meter E =
0009731
Z = 5229530
96 I = 51
85225
XDOT = -5276
615705 Wp = 135
81971
YDOT = -5444
968546 meter/sec RA = 38
94069 deg
ZDOT = -1169
582920 TA = 325
32632
MA = 325
38972
Ha = 226
739 n
mi
Hp = 215
494
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11813314
19 X = -3652351
20
Y = 7779999
49 feet Y = 2330790
05 meter
Z = 17157253
81 Z = 5211913
41
XDOT = -17311
731314 XDOT = -5209
655182
YDOT = -17864
070034 feet/sec YDOT = -5503
600656 meter/sec
ZDOT = -3837
214304 ZDOT = -1195
053418
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7100478
24 X = -2164225
77
Y = 12336664
05 feet Y = 3760215
20 meter
Z = 17083444
36 Z = 5207033
84
XDOT = -22605
478672 XDOT = -6890
149899
YDOT = -7576
135882 feet/sec YDOT = -2309
206217 meter/sec
ZDOT = -3942
709623 ZDOT = -1201
737893
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 13109
54624194
00016717 00000-0 10270-3 0 9141
2 25544 51
6457 39
3160 0009878 159
9731 200
1810 15
52327634 25602
Satellite: ISS
Catalog Number: 25544
Epoch time: 13109
54624194 = yrday
fracday
Element set: 914
Inclination: 51
6457 deg
RA of node: 39
3160 deg
Eccentricity:
0009878
Arg of perigee: 159
9731 deg
Mean anomaly: 200
1810 deg
Mean motion: 15
52327634 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2560
Checksum: 307
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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