[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 15th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15069 47 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 126 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 347 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
017/02:16:52
660 -1
2 1
5 1
5
N/A 0
2 -0
1 228
5
000/00:03:45
321 1
0 0
1 215
5
Coasting Arc #1 (Orbit 1083)
---------------------------------------
Vector Time (GMT): 2013/014/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6192638
45 A = 6792679
22 meter
Y = -1224252
24 meter E =
0020572
Z = -2487740
36 I = 51
82477
XDOT = -1061
648618 Wp = 150
96935
YDOT = 5403
255778 meter/sec RA = 150
76701 deg
ZDOT = -5337
717710 TA = 56
83184
MA = 56
63468
Ha = 229
131 n
mi
Hp = 214
065
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20317055
27 X = 6217952
58
Y = -4016575
58 feet Y = -1154860
67 meter
Z = -8161877
81 Z = -2457596
20
XDOT = -3483
099140 XDOT = -1096
061376
YDOT = 17727
217121 feet/sec YDOT = 5391
191486 meter/sec
ZDOT = -17512
197210 ZDOT = -5342
958447
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11747255
42 X = 3580563
45
Y = 17115777
55 feet Y = 5216889
00 meter
Z = -8036417
91 Z = -2449500
18
XDOT = -16366
927638 XDOT = -4988
639544
YDOT = 3056
519091 feet/sec YDOT = 931
627019 meter/sec
ZDOT = -17534
574334 ZDOT = -5344
538257
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 13014
52736292
00016717 00000-0 10270-3 0 9002
2 25544 51
6453 151
6624 0015508 157
1126 203
0720 15
52102819 10844
Satellite: ISS
Catalog Number: 25544
Epoch time: 13014
52736292 = yrday
fracday
Element set: 900
Inclination: 51
6453 deg
RA of node: 151
6624 deg
Eccentricity:
0015508
Arg of perigee: 157
1126 deg
Mean anomaly: 203
0720 deg
Mean motion: 15
52102819 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1084
Checksum: 270
Coasting Arc #2 (Orbit 1099)
---------------------------------------
Vector Time (GMT): 2013/015/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5859417
03 A = 6790465
64 meter
Y = 813175
20 meter E =
0022697
Z = 3334323
91 I = 51
84517
XDOT = 1895
282567 Wp = 129
13071
YDOT = -5748
363809 meter/sec RA = 145
81426 deg
ZDOT = 4697
083120 TA = 269
51024
MA = 269
77033
Ha = 228
905 n
mi
Hp = 214
232
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19223809
15 X = -5884271
62
Y = 2667897
64 feet Y = 747512
52 meter
Z = 10939382
89 Z = 3305799
49
XDOT = 6218
118657 XDOT = 1936
604340
YDOT = -18859
461316 feet/sec YDOT = -5726
938574 meter/sec
ZDOT = 15410
377689 ZDOT = 4706
390392
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10368144
36 X = -3160210
40
Y = -16485048
76 feet Y = -5024642
86 meter
Z = 10820691
46 Z = 3298146
76
XDOT = 18505
561374 XDOT = 5640
495107
YDOT = -1420
732016 feet/sec YDOT = -433
039118 meter/sec
ZDOT = 15449
703864 ZDOT = 4709
069738
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 13015
55752830
00016717 00000-0 10270-3 0 9013
2 25544 51
6464 146
5432 0015507 161
1518 199
0211 15
52160620 11007
Satellite: ISS
Catalog Number: 25544
Epoch time: 13015
55752830 = yrday
fracday
Element set: 901
Inclination: 51
6464 deg
RA of node: 146
5432 deg
Eccentricity:
0015507
Arg of perigee: 161
1518 deg
Mean anomaly: 199
0211 deg
Mean motion: 15
52160620 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1100
Checksum: 264
Coasting Arc #3 (Orbit 1114)
---------------------------------------
Vector Time (GMT): 2013/016/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 903313
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5392093
23 A = 6788055
34 meter
Y = -219439
50 meter E =
0016658
Z = -4118146
63 I = 51
86171
XDOT = -2672
567511 Wp = 138
78570
YDOT = 6066
263179 meter/sec RA = 140
85866 deg
ZDOT = -3843
604358 TA = 91
68537
MA = 91
49456
Ha = 228
830 n
mi
Hp = 214
495
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17690594
58 X = 5414150
88
Y = -719945
86 feet Y = -159018
39 meter
Z = -13510979
77 Z = -4091899
10
XDOT = -8768
266112 XDOT = -2721
532171
YDOT = 19902
438251 feet/sec YDOT = 6036
103087 meter/sec
ZDOT = -12610
250518 ZDOT = -3856
706195
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8240995
47 X = 2511855
42
Y = 15763865
99 feet Y = 4804826
35 meter
Z = -13401811
65 Z = -4084872
19
XDOT = -20557
320190 XDOT = -6265
871194
YDOT = 38
432193 feet/sec YDOT = 11
714132 meter/sec
ZDOT = -12665
396862 ZDOT = -3860
412964
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 13016
52329576
00016717 00000-0 10270-3 0 9029
2 25544 51
6464 141
7434 0015371 164
5450 195
6175 15
52138826 11157
Satellite: ISS
Catalog Number: 25544
Epoch time: 13016
52329576 = yrday
fracday
Element set: 902
Inclination: 51
6464 deg
RA of node: 141
7434 deg
Eccentricity:
0015371
Arg of perigee: 164
5450 deg
Mean anomaly: 195
6175 deg
Mean motion: 15
52138826 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1115
Checksum: 300
Coasting Arc #4 (Orbit 1123)
---------------------------------------
Vector Time (GMT): 2013/017/02:18:45
321
Vector Time (MET): N/A
Weight (LBS) : 903159
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2493130
38 A = 6791765
96 meter
Y = 5523187
50 meter E =
0014194
Z = -3088258
00 I = 51
88686
XDOT = -5861
237077 Wp = 149
71562
YDOT = 103
684080 meter/sec RA = 137
85911 deg
ZDOT = 4915
099869 TA = 175
03705
MA = 175
02297
Ha = 228
451 n
mi
Hp = 215
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8179561
60 X = -2539704
78
Y = 18120693
91 feet Y = 5495047
35 meter
Z = -10132080
06 Z = -3100482
38
XDOT = -19229
780437 XDOT = -5885
836831
YDOT = 340
170865 feet/sec YDOT = 38
002492 meter/sec
ZDOT = 16125
655739 ZDOT = 4886
567077
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15976429
13 X = 4869615
60
Y = -11788697
32 feet Y = -3593194
94 meter
Z = -10183523
44 Z = -3103937
94
XDOT = 16139
825447 XDOT = 4919
418796
YDOT = 8039
932104 feet/sec YDOT = 2450
571305 meter/sec
ZDOT = 16006
992233 ZDOT = 4878
931233
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 13017
10274829
00016717 00000-0 10270-3 0 9035
2 25544 51
6474 138
8676 0013734 167
9037 192
2447 15
51894326 11240
Satellite: ISS
Catalog Number: 25544
Epoch time: 13017
10274829 = yrday
fracday
Element set: 903
Inclination: 51
6474 deg
RA of node: 138
8676 deg
Eccentricity:
0013734
Arg of perigee: 167
9037 deg
Mean anomaly: 192
2447 deg
Mean motion: 15
51894326 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1124
Checksum: 319
Coasting Arc #5 (Orbit 1139)
---------------------------------------
Vector Time (GMT): 2013/018/02:18:45
321
Vector Time (MET): N/A
Weight (LBS) : 903159
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2913052
48 A = 6793743
04 meter
Y = -5699846
74 meter E =
0023493
Z = 2229759
73 I = 51
91499
XDOT = 5337
480074 Wp = 140
01054
YDOT = 575
311141 meter/sec RA = 132
91251 deg
ZDOT = -5488
043434 TA = 15
28531
MA = 15
21446
Ha = 228
359 n
mi
Hp = 215
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9557258
79 X = 2965741
39
Y = -18700284
58 feet Y = -5666976
58 meter
Z = 7315484
68 Z = 2244038
87
XDOT = 17511
417567 XDOT = 5357
309326
YDOT = 1887
503744 feet/sec YDOT = 635
109117 meter/sec
ZDOT = -18005
391844 ZDOT = -5462
066494
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17273994
91 X = -5265113
65
Y = 11906687
45 feet Y = 3629158
33 meter
Z = 7375503
31 Z = 2248053
41
XDOT = -13725
004789 XDOT = -4183
381460
YDOT = -8796
487521 feet/sec YDOT = -2681
169396 meter/sec
ZDOT = -17897
424166 ZDOT = -5455
134886
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 13018
13306445
00016717 00000-0 10270-3 0 9040
2 25544 51
6471 133
7490 0013736 171
5455 188
5930 15
51878569 11406
Satellite: ISS
Catalog Number: 25544
Epoch time: 13018
13306445 = yrday
fracday
Element set: 904
Inclination: 51
6471 deg
RA of node: 133
7490 deg
Eccentricity:
0013736
Arg of perigee: 171
5455 deg
Mean anomaly: 188
5930 deg
Mean motion: 15
51878569 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1140
Checksum: 310
Coasting Arc #6 (Orbit 1154)
---------------------------------------
Vector Time (GMT): 2013/019/02:18:45
321
Vector Time (MET): N/A
Weight (LBS) : 903159
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3241329
48 A = 6794914
16 meter
Y = 5831008
76 meter E =
0009215
Z = -1318274
24 I = 51
94018
XDOT = -4762
412917 Wp = 135
97053
YDOT = -1330
899955 meter/sec RA = 127
96907 deg
ZDOT = 5840
890673 TA = 209
77640
MA = 209
82888
Ha = 228
078 n
mi
Hp = 215
902
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10634283
08 X = -3299888
38
Y = 19130606
16 feet Y = 5794434
79 meter
Z = -4325046
71 Z = -1334162
32
XDOT = -15624
714295 XDOT = -4775
549814
YDOT = -4366
469667 feet/sec YDOT = -1384
229823 meter/sec
ZDOT = 19163
027143 ZDOT = 5817
723533
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18237117
45 X = 5558673
40
Y = -12078653
63 feet Y = -3681573
63 meter
Z = -4391784
54 Z = -1338615
93
XDOT = 11072
066665 XDOT = 3374
765920
YDOT = 9805
874754 feet/sec YDOT = 2988
830625 meter/sec
ZDOT = 19066
823281 ZDOT = 5811
567736
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 13019
09896902
00016717 00000-0 10270-3 0 9059
2 25544 51
6476 128
9497 0013569 175
4816 184
6461 15
51945330 11555
Satellite: ISS
Catalog Number: 25544
Epoch time: 13019
09896902 = yrday
fracday
Element set: 905
Inclination: 51
6476 deg
RA of node: 128
9497 deg
Eccentricity:
0013569
Arg of perigee: 175
4816 deg
Mean anomaly: 184
6461 deg
Mean motion: 15
51945330 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1155
Checksum: 338
Coasting Arc #7 (Orbit 1170)
---------------------------------------
Vector Time (GMT): 2013/020/02:18:45
321
Vector Time (MET): N/A
Weight (LBS) : 903159
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3478424
47 A = 6795744
84 meter
Y = -5811292
36 meter E =
0024073
Z = 321126
40 I = 51
96064
XDOT = 4213
235851 Wp = 156
32726
YDOT = 2181
004298 meter/sec RA = 123
02914 deg
ZDOT = -6034
233963 TA = 20
22522
MA = 20
13001
Ha = 228
054 n
mi
Hp = 216
116
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11412153
76 X = 3541589
11
Y = -19065919
82 feet Y = -5772041
28 meter
Z = 1053564
29 Z = 338177
36
XDOT = 13822
952266 XDOT = 4217
846721
YDOT = 7155
525911 feet/sec YDOT = 2228
145335 meter/sec
ZDOT = -19797
355522 ZDOT = -6013
755317
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18712113
88 X = -5703452
31
Y = 11976951
97 feet Y = 3650574
96 meter
Z = 1125151
36 Z = 342946
13
XDOT = -8416
189438 XDOT = -2565
254541
YDOT = -11258
293989 feet/sec YDOT = -3431
528008 meter/sec
ZDOT = -19712
425545 ZDOT = -6008
347306
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 13020
12925371
00016717 00000-0 10270-3 0 9069
2 25544 51
6477 123
8308 0013646 179
2711 180
8463 15
51910923 11711
Satellite: ISS
Catalog Number: 25544
Epoch time: 13020
12925371 = yrday
fracday
Element set: 906
Inclination: 51
6477 deg
RA of node: 123
8308 deg
Eccentricity:
0013646
Arg of perigee: 179
2711 deg
Mean anomaly: 180
8463 deg
Mean motion: 15
51910923 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1171
Checksum: 294
Coasting Arc #8 (Orbit 1186)
---------------------------------------
Vector Time (GMT): 2013/021/02:18:45
321
Vector Time (MET): N/A
Weight (LBS) : 903159
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3632092
76 A = 6795374
67 meter
Y = 5708443
96 meter E =
0010916
Z = 660402
90 I = 51
97616
XDOT = -3679
926062 Wp = 118
94146
YDOT = -3042
941214 meter/sec RA = 118
08994 deg
ZDOT = 5984
041758 TA = 248
14221
MA = 248
25834
Ha = 227
680 n
mi
Hp = 216
374
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11916314
82 X = -3698863
87
Y = 18728490
69 feet Y = 5667454
26 meter
Z = 2166676
19 Z = 642596
75
XDOT = -12073
248235 XDOT = -3674
694355
YDOT = -9983
402934 feet/sec YDOT = -3084
063478 meter/sec
ZDOT = 19632
682932 ZDOT = 5966
177727
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18831048
97 X = 5739703
72
Y = -11767105
52 feet Y = -3586613
76 meter
Z = 2091944
22 Z = 637624
60
XDOT = 5849
545281 XDOT = 1782
941402
YDOT = 12886
483481 feet/sec YDOT = 3927
800165 meter/sec
ZDOT = 19558
725122 ZDOT = 5961
499417
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 13021
15951953
00016717 00000-0 10270-3 0 9079
2 25544 51
6478 118
7113 0013373 183
4472 176
6589 15
51989621 11877
Satellite: ISS
Catalog Number: 25544
Epoch time: 13021
15951953 = yrday
fracday
Element set: 907
Inclination: 51
6478 deg
RA of node: 118
7113 deg
Eccentricity:
0013373
Arg of perigee: 183
4472 deg
Mean anomaly: 176
6589 deg
Mean motion: 15
51989621 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1187
Checksum: 330
Coasting Arc #9 (Orbit 1201)
---------------------------------------
Vector Time (GMT): 2013/022/02:18:45
321
Vector Time (MET): N/A
Weight (LBS) : 903159
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3729206
20 A = 6794501
60 meter
Y = -5415849
50 meter E =
0019802
Z = -1662547
29 I = 51
98667
XDOT = 3194
337624 Wp = 171
09068
YDOT = 3955
057713 meter/sec RA = 113
15172 deg
ZDOT = -5746
852307 TA = 27
03616
MA = 26
93315
Ha = 227
667 n
mi
Hp = 216
575
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12234928
48 X = 3797566
33
Y = -17768535
10 feet Y = -5373764
86 meter
Z = -5454551
47 Z = -1644265
58
XDOT = 10480
110316 XDOT = 3177
790275
YDOT = 12975
911133 feet/sec YDOT = 3990
686585 meter/sec
ZDOT = -18854
502319 ZDOT = -5731
374648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18535873
40 X = -5649734
21
Y = 11075489
38 feet Y = 3375809
16 meter
Z = -5377860
04 Z = -1639171
74
XDOT = -3448
593665 XDOT = -1051
131349
YDOT = -14850
131058 feet/sec YDOT = -4526
319947 meter/sec
ZDOT = -18790
577231 ZDOT = -5727
367940
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 13022
12538190
00016717 00000-0 10270-3 0 9082
2 25544 51
6480 113
9124 0013469 187
3440 172
7516 15
51961321 12025
Satellite: ISS
Catalog Number: 25544
Epoch time: 13022
12538190 = yrday
fracday
Element set: 908
Inclination: 51
6480 deg
RA of node: 113
9124 deg
Eccentricity:
0013469
Arg of perigee: 187
3440 deg
Mean anomaly: 172
7516 deg
Mean motion: 15
51961321 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1202
Checksum: 281
Coasting Arc #10 (Orbit 1217)
---------------------------------------
Vector Time (GMT): 2013/023/02:18:45
321
Vector Time (MET): N/A
Weight (LBS) : 903159
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3774181
87 A = 6792714
86 meter
Y = 5028768
08 meter E =
0014442
Z = 2576514
10 I = 51
99219
XDOT = -2768
780550 Wp = 132
03321
YDOT = -4800
401042 meter/sec RA = 108
21105 deg
ZDOT = 5285
069637 TA = 256
73310
MA = 256
89421
Ha = 227
282 n
mi
Hp = 216
868
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12382486
44 X = -3842649
95
Y = 16498582
93 feet Y = 4986179
84 meter
Z = 8453130
24 Z = 2558013
69
XDOT = -9083
925689 XDOT = -2740
568757
YDOT = -15749
347250 feet/sec YDOT = -4831
205840 meter/sec
ZDOT = 17339
467313 ZDOT = 5271
687584
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17987851
53 X = 5482697
14
Y = -10162273
61 feet Y = -3097461
00 meter
Z = 8375560
42 Z = 2552870
82
XDOT = 1397
257554 XDOT = 425
884102
YDOT = 16796
184482 feet/sec YDOT = 5119
477030 meter/sec
ZDOT = 17284
361174 ZDOT = 5268
273286
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 13023
15561823
00016717 00000-0 10270-3 0 9096
2 25544 51
6478 108
7927 0013163 191
1590 168
9272 15
52019979 12182
Satellite: ISS
Catalog Number: 25544
Epoch time: 13023
15561823 = yrday
fracday
Element set: 909
Inclination: 51
6478 deg
RA of node: 108
7927 deg
Eccentricity:
0013163
Arg of perigee: 191
1590 deg
Mean anomaly: 168
9272 deg
Mean motion: 15
52019979 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1218
Checksum: 322
Coasting Arc #11 (Orbit 1232)
---------------------------------------
Vector Time (GMT): 2013/024/02:18:45
321
Vector Time (MET): N/A
Weight (LBS) : 903159
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3807104
53 A = 6790508
83 meter
Y = -4440615
64 meter E =
0012862
Z = -3437429
50 I = 51
99319
XDOT = 2391
938288 Wp = 173
70540
YDOT = 5624
629362 meter/sec RA = 103
26867 deg
ZDOT = -4631
019708 TA = 46
31215
MA = 46
20565
Ha = 227
214 n
mi
Hp = 217
030
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12490500
43 X = 3873175
30
Y = -14568948
97 feet Y = -4397672
61 meter
Z = -11277655
83 Z = -3418775
00
XDOT = 7847
566563 XDOT = 2351
360581
YDOT = 18453
508406 feet/sec YDOT = 5651
150886 meter/sec
ZDOT = -15193
634211 ZDOT = -4619
498333
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17186371
89 X = -5238406
15
Y = 8640148
07 feet Y = 2633517
13 meter
Z = -11199502
60 Z = -3413608
39
XDOT = 371
568705 XDOT = 113
254141
YDOT = -18833
647600 feet/sec YDOT = -5740
495788 meter/sec
ZDOT = -15146
370038 ZDOT = -4616
613588
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 13024
12145085
00016717 00000-0 10270-3 0 9104
2 25544 51
6474 103
9935 0013244 195
1534 164
9222 15
52026257 12331
Satellite: ISS
Catalog Number: 25544
Epoch time: 13024
12145085 = yrday
fracday
Element set: 910
Inclination: 51
6474 deg
RA of node: 103
9935 deg
Eccentricity:
0013244
Arg of perigee: 195
1534 deg
Mean anomaly: 164
9222 deg
Mean motion: 15
52026257 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1233
Checksum: 279
Coasting Arc #12 (Orbit 1248)
---------------------------------------
Vector Time (GMT): 2013/025/02:18:45
321
Vector Time (MET): N/A
Weight (LBS) : 903159
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3827794
67 A = 6788227
40 meter
Y = 3778511
38 meter E =
0015993
Z = 4146499
34 I = 51
99164
XDOT = -2084
141255 Wp = 157
67277
YDOT = -6310
681402 meter/sec RA = 98
32236 deg
ZDOT = 3807
469813 TA = 253
12260
MA = 253
29804
Ha = 226
913 n
mi
Hp = 217
331
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12558381
45 X = -3889904
46
Y = 12396690
88 feet Y = 3735359
11 meter
Z = 13604000
46 Z = 4127753
94
XDOT = -6837
733777 XDOT = -2031
914272
YDOT = -20704
335307 feet/sec YDOT = -6333
695734 meter/sec
ZDOT = 12491
698861 ZDOT = 3797
472006
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16313412
29 X = 4972328
07
Y = -6884192
64 feet Y = -2098301
92 meter
Z = 13525538
40 Z = 4122584
10
XDOT = -1679
907979 XDOT = -512
035952
YDOT = 20606
170155 feet/sec YDOT = 6280
760663 meter/sec
ZDOT = 12450
859465 ZDOT = 3795
021965
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 13025
15165858
00016717 00000-0 10270-3 0 9119
2 25544 51
6473 98
8736 0013004 198
5874 161
4804 15
52042049 12491
Satellite: ISS
Catalog Number: 25544
Epoch time: 13025
15165858 = yrday
fracday
Element set: 911
Inclination: 51
6473 deg
RA of node: 98
8736 deg
Eccentricity:
0013004
Arg of perigee: 198
5874 deg
Mean anomaly: 161
4804 deg
Mean motion: 15
52042049 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1249
Checksum: 314
Coasting Arc #13 (Orbit 1263)
---------------------------------------
Vector Time (GMT): 2013/026/02:18:45
321
Vector Time (MET): N/A
Weight (LBS) : 903159
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3877388
04 A = 6785899
59 meter
Y = -2939538
13 meter E =
0010001
Z = -4730638
27 I = 51
98661
XDOT = 1801
140568 Wp = 148
72641
YDOT = 6894
990060 meter/sec RA = 93
37227 deg
ZDOT = -2819
130565 TA = 93
49759
MA = 93
38319
Ha = 226
764 n
mi
Hp = 217
454
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12721089
37 X = 3932950
05
Y = -9644153
98 feet Y = -2895867
94 meter
Z = -15520466
78 Z = -4711667
83
XDOT = 5909
253832 XDOT = 1737
599732
YDOT = 22621
358465 feet/sec YDOT = 6914
776355 meter/sec
ZDOT = -9249
116026 ZDOT = -2810
535100
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15388626
37 X = -4690453
32
Y = 4525638
73 feet Y = 1379414
68 meter
Z = -15441161
95 Z = -4706466
16
XDOT = 2694
566991 XDOT = 821
304019
YDOT = -22152
270718 feet/sec YDOT = -6752
012115 meter/sec
ZDOT = -9214
186033 ZDOT = -2808
483903
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 13026
11746212
00016717 00000-0 10270-3 0 9126
2 25544 51
6461 94
0736 0013098 202
4955 157
5624 15
52085383 12645
Satellite: ISS
Catalog Number: 25544
Epoch time: 13026
11746212 = yrday
fracday
Element set: 912
Inclination: 51
6461 deg
RA of node: 94
0736 deg
Eccentricity:
0013098
Arg of perigee: 202
4955 deg
Mean anomaly: 157
5624 deg
Mean motion: 15
52085383 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1264
Checksum: 295
Coasting Arc #14 (Orbit 1279)
---------------------------------------
Vector Time (GMT): 2013/027/02:18:45
321
Vector Time (MET): N/A
Weight (LBS) : 903159
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3945963
32 A = 6784337
95 meter
Y = 2075198
51 meter E =
0014762
Z = 5118648
89 I = 51
98216
XDOT = -1561
878359 Wp = 185
01158
YDOT = -7295
390176 meter/sec RA = 88
41964 deg
ZDOT = 1739
712418 TA = 248
15650
MA = 248
31357
Ha = 226
561 n
mi
Hp = 217
715
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12946073
88 X = -3993739
78
Y = 6808394
05 feet Y = 2030805
08 meter
Z = 16793467
50 Z = 5099364
19
XDOT = -5124
272833 XDOT = -1488
634532
YDOT = -23935
007140 feet/sec YDOT = -7312
446570 meter/sec
ZDOT = 5707
717907 ZDOT = 1732
302953
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14577064
69 X = 4443089
32
Y = -2040084
80 feet Y = -621817
85 meter
Z = 16712954
49 Z = 5094108
53
XDOT = -3313
226645 XDOT = -1009
871481
YDOT = 23216
023458 feet/sec YDOT = 7076
243950 meter/sec
ZDOT = 5677
775610 ZDOT = 1730
586006
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 13027
14764060
00016717 00000-0 10270-3 0 9132
2 25544 51
6462 88
9538 0012982 205
8198 154
2307 15
52075646 12806
Satellite: ISS
Catalog Number: 25544
Epoch time: 13027
14764060 = yrday
fracday
Element set: 913
Inclination: 51
6462 deg
RA of node: 88
9538 deg
Eccentricity:
0012982
Arg of perigee: 205
8198 deg
Mean anomaly: 154
2307 deg
Mean motion: 15
52075646 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1280
Checksum: 312
Coasting Arc #15 (Orbit 1294)
---------------------------------------
Vector Time (GMT): 2013/028/02:18:45
321
Vector Time (MET): N/A
Weight (LBS) : 903159
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4066068
53 A = 6783248
51 meter
Y = -1091720
09 meter E =
0013188
Z = -5324931
12 I = 51
97576
XDOT = 1302
803999 Wp = 141
07467
YDOT = 7527
729530 meter/sec RA = 83
46284 deg
ZDOT = -559
255043 TA = 123
67043
MA = 123
54459
Ha = 226
320 n
mi
Hp = 217
841
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13340119
84 X = 4103840
64
Y = -3581758
83 feet Y = -1046039
62 meter
Z = -17470246
46 Z = -5305087
24
XDOT = 4274
291336 XDOT = 1221
247152
YDOT = 24697
275361 feet/sec YDOT = 7541
842286 meter/sec
ZDOT = -1834
826257 ZDOT = -553
124459
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13887808
66 X = -4233004
08
Y = -894491
01 feet Y = -272640
86 meter
Z = -17387523
16 Z = -5299717
06
XDOT = 3752
562111 XDOT = 1143
780932
YDOT = -23761
042971 feet/sec YDOT = -7242
365898 meter/sec
ZDOT = -1810
238667 ZDOT = -551
760746
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 13028
11341633
00016717 00000-0 10270-3 0 9148
2 25544 51
6446 84
1526 0013030 209
4407 150
6012 15
52138600 12950
Satellite: ISS
Catalog Number: 25544
Epoch time: 13028
11341633 = yrday
fracday
Element set: 914
Inclination: 51
6446 deg
RA of node: 84
1526 deg
Eccentricity:
0013030
Arg of perigee: 209
4407 deg
Mean anomaly: 150
6012 deg
Mean motion: 15
52138600 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1295
Checksum: 262
Coasting Arc #16 (Orbit 1310)
---------------------------------------
Vector Time (GMT): 2013/029/02:18:45
321
Vector Time (MET): N/A
Weight (LBS) : 903159
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4213396
01 A = 6783304
73 meter
Y = 147526
99 meter E =
0010665
Z = 5316948
09 I = 51
97156
XDOT = -1040
227601 Wp = 204
45915
YDOT = -7566
400683 meter/sec RA = 78
50691 deg
ZDOT = -624
272528 TA = 251
41912
MA = 251
53499
Ha = 226
174 n
mi
Hp = 218
041
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13823477
72 X = -4240560
27
Y = 484012
43 feet Y = 100258
42 meter
Z = 17444055
42 Z = 5296414
26
XDOT = -3412
820212 XDOT = -952
508714
YDOT = -24824
149223 feet/sec YDOT = -7577
542715 meter/sec
ZDOT = -2048
138214 ZDOT = -629
112465
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13424008
80 X = 4091637
88
Y = 3754160
92 feet Y = 1144268
25 meter
Z = 17358575
32 Z = 5290893
76
XDOT = -3999
642257 XDOT = -1219
090960
YDOT = 23710
065602 feet/sec YDOT = 7226
827996 meter/sec
ZDOT = -2067
344670 ZDOT = -630
126655
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 13029
14356469
00016717 00000-0 10270-3 0 9156
2 25544 51
6448 79
0329 0013037 213
1368 146
8969 15
52129074 13113
Satellite: ISS
Catalog Number: 25544
Epoch time: 13029
14356469 = yrday
fracday
Element set: 915
Inclination: 51
6448 deg
RA of node: 79
0329 deg
Eccentricity:
0013037
Arg of perigee: 213
1368 deg
Mean anomaly: 146
8969 deg
Mean motion: 15
52129074 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1311
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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