[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
May 15th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14800 38 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 202 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
137/02:03:18
758 -2
8 4
8 4
9
N/A -3
4 -0
5 225
4
000/00:14:33
516 -2
1 0
2 223
4
Coasting Arc #1 (Orbit 2931)
---------------------------------------
Vector Time (GMT): 2013/133/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905021
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 590685
66 A = 6798030
18 meter
Y = -6732104
63 meter E =
0010966
Z = -669271
51 I = 51
31753
XDOT = 4846
934440 Wp = 12
84053
YDOT = -161
943570 meter/sec RA = 279
56224 deg
ZDOT = 5936
045496 TA = 339
90661
MA = 339
94974
Ha = 224
720 n
mi
Hp = 221
108
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1937945
07 X = 669172
78
Y = -22086957
46 feet Y = -6725060
32 meter
Z = -2195772
66 Z = -666211
79
XDOT = 15902
015878 XDOT = 4819
549013
YDOT = -531
310925 feet/sec YDOT = -107
895623 meter/sec
ZDOT = 19475
214882 ZDOT = 5959
525246
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15827037
45 X = -4824081
02
Y = -15529137
60 feet Y = -4733281
14 meter
Z = -2182088
30 Z = -665100
51
XDOT = 8476
534839 XDOT = 2583
647819
YDOT = -11375
896027 feet/sec YDOT = -3467
373109 meter/sec
ZDOT = 19573
126207 ZDOT = 5965
888868
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 13133
50128645
00016717 00000-0 10270-3 0 9009
2 25544 51
6466 280
3239 0005150 300
5488 59
5154 15
51075895 29327
Satellite: ISS
Catalog Number: 25544
Epoch time: 13133
50128645 = yrday
fracday
Element set: 900
Inclination: 51
6466 deg
RA of node: 280
3239 deg
Eccentricity:
0005150
Arg of perigee: 300
5488 deg
Mean anomaly: 59
5154 deg
Mean motion: 15
51075895 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2932
Checksum: 300
Coasting Arc #2 (Orbit 2947)
---------------------------------------
Vector Time (GMT): 2013/134/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 880554
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -579031
77 A = 6798106
39 meter
Y = 6769591
87 meter E =
0006827
Z = -45337
36 I = 51
31329
XDOT = -4768
402698 Wp = 142
21962
YDOT = -444
661872 meter/sec RA = 274
58269 deg
ZDOT = -5980
099403 TA = 38
27017
MA = 38
22174
Ha = 224
881 n
mi
Hp = 220
988
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1899710
53 X = -654467
53
Y = 22209947
08 feet Y = 6762694
99 meter
Z = -148744
61 Z = -48333
05
XDOT = -15644
365806 XDOT = -4734
025986
YDOT = -1458
864410 feet/sec YDOT = -497
792549 meter/sec
ZDOT = -19619
748698 ZDOT = -6003
180647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16220797
99 X = 4944099
23
Y = 15289610
56 feet Y = 4660273
30 meter
Z = -162159
28 Z = -49426
15
XDOT = -9675
623754 XDOT = -2949
130120
YDOT = 10071
284374 feet/sec YDOT = 3069
727477 meter/sec
ZDOT = -19715
920646 ZDOT = -6009
412613
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 13134
53213902
00016717 00000-0 10270-3 0 9015
2 25544 51
6459 275
2086 0005294 305
3493 54
7163 15
51112641 29485
Satellite: ISS
Catalog Number: 25544
Epoch time: 13134
53213902 = yrday
fracday
Element set: 901
Inclination: 51
6459 deg
RA of node: 275
2086 deg
Eccentricity:
0005294
Arg of perigee: 305
3493 deg
Mean anomaly: 54
7163 deg
Mean motion: 15
51112641 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2948
Checksum: 294
Coasting Arc #3 (Orbit 2963)
---------------------------------------
Vector Time (GMT): 2013/135/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 880554
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 552152
86 A = 6797837
78 meter
Y = -6725733
95 meter E =
0012995
Z = 747667
56 I = 51
31237
XDOT = 4751
380061 Wp = 30
22514
YDOT = 1052
399497 meter/sec RA = 269
60310 deg
ZDOT = 5924
070622 TA = 337
88494
MA = 337
94095
Ha = 224
940 n
mi
Hp = 220
847
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1811525
13 X = 623688
43
Y = -22066056
28 feet Y = -6719159
50 meter
Z = 2452977
57 Z = 750523
25
XDOT = 15588
517262 XDOT = 4710
480996
YDOT = 3452
754254 feet/sec YDOT = 1105
303392 meter/sec
ZDOT = 19435
927237 ZDOT = 5947
053314
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16429264
32 X = -5007639
77
Y = -14839430
56 feet Y = -4523058
43 meter
Z = 2465793
28 Z = 751573
79
XDOT = 11063
225807 XDOT = 3372
071226
YDOT = -8984
573734 feet/sec YDOT = -2738
498074 meter/sec
ZDOT = 19531
612008 ZDOT = 5953
235340
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 13135
56297827
00016717 00000-0 10270-3 0 9028
2 25544 51
6473 270
0937 0005207 309
0276 51
0411 15
51125616 29643
Satellite: ISS
Catalog Number: 25544
Epoch time: 13135
56297827 = yrday
fracday
Element set: 902
Inclination: 51
6473 deg
RA of node: 270
0937 deg
Eccentricity:
0005207
Arg of perigee: 309
0276 deg
Mean anomaly: 51
0411 deg
Mean motion: 15
51125616 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2964
Checksum: 295
Coasting Arc #4 (Orbit 2978)
---------------------------------------
Vector Time (GMT): 2013/136/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 880554
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -552597
90 A = 6797095
31 meter
Y = 6613444
92 meter E =
0003236
Z = -1460874
30 I = 51
31075
XDOT = -4780
492848 Wp = 157
28311
YDOT = -1667
535806 meter/sec RA = 264
62276 deg
ZDOT = -5747
924087 TA = 38
70410
MA = 38
68092
Ha = 225
126 n
mi
Hp = 220
698
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1812985
22 X = -619413
21
Y = 21697653
93 feet Y = 6606891
91 meter
Z = -4792894
68 Z = -1463720
75
XDOT = -15684
031652 XDOT = -4733
568743
YDOT = -5470
917998 feet/sec YDOT = -1720
731638 meter/sec
ZDOT = -18858
018657 ZDOT = -5771
033566
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16393337
02 X = 4996689
12
Y = 14325194
62 feet Y = 4366319
32 meter
Z = -4805646
81 Z = -1464761
15
XDOT = -12605
969772 XDOT = -3842
299586
YDOT = 8075
300963 feet/sec YDOT = 2461
351734 meter/sec
ZDOT = -18954
156662 ZDOT = -5777
226951
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 13136
52937730
00016717 00000-0 10270-3 0 9030
2 25544 51
6467 265
2982 0005322 313
4276 46
6432 15
51148610 29797
Satellite: ISS
Catalog Number: 25544
Epoch time: 13136
52937730 = yrday
fracday
Element set: 903
Inclination: 51
6467 deg
RA of node: 265
2982 deg
Eccentricity:
0005322
Arg of perigee: 313
4276 deg
Mean anomaly: 46
6432 deg
Mean motion: 15
51148610 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2979
Checksum: 311
Coasting Arc #5 (Orbit 2987)
---------------------------------------
Vector Time (GMT): 2013/137/02:10:35
516
Vector Time (MET): N/A
Weight (LBS) : 880039
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3863111
57 A = 6789507
34 meter
Y = 2156805
87 meter E =
0008112
Z = -5156834
31 I = 51
27850
XDOT = -2175
199991 Wp = 58
15830
YDOT = -7209
264529 meter/sec RA = 261
67874 deg
ZDOT = -1383
132586 TA = 198
43865
MA = 198
46807
Ha = 225
435 n
mi
Hp = 223
403
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12674250
54 X = -3861891
63
Y = 7076134
75 feet Y = 2113613
17 meter
Z = -16918747
74 Z = -5175598
04
XDOT = -7136
482909 XDOT = -2087
703846
YDOT = -23652
442680 feet/sec YDOT = -7233
099709 meter/sec
ZDOT = -4537
836569 ZDOT = -1393
487372
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6357766
27 X = -1937847
16
Y = -12946959
09 feet Y = -3946233
13 meter
Z = -16997276
06 Z = -5180769
74
XDOT = 23070
562471 XDOT = 7031
907441
YDOT = -5305
101397 feet/sec YDOT = -1616
994906 meter/sec
ZDOT = -4580
058935 ZDOT = -1396
001963
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 13137
10921950
00016717 00000-0 10270-3 0 9043
2 25544 51
6473 262
4245 0006929 284
5555 75
4827 15
50184075 29889
Satellite: ISS
Catalog Number: 25544
Epoch time: 13137
10921950 = yrday
fracday
Element set: 904
Inclination: 51
6473 deg
RA of node: 262
4245 deg
Eccentricity:
0006929
Arg of perigee: 284
5555 deg
Mean anomaly: 75
4827 deg
Mean motion: 15
50184075 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2988
Checksum: 326
Coasting Arc #6 (Orbit 3003)
---------------------------------------
Vector Time (GMT): 2013/138/02:10:35
516
Vector Time (MET): N/A
Weight (LBS) : 880039
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3838525
56 A = 6789081
61 meter
Y = -1999664
00 meter E =
0003745
Z = 5233752
50 I = 51
28235
XDOT = 2470
848962 Wp = 275
21191
YDOT = 7189
497137 meter/sec RA = 256
69570 deg
ZDOT = 935
647404 TA = 165
78611
MA = 165
77557
Ha = 225
573 n
mi
Hp = 223
574
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12593587
81 X = 3835176
59
Y = -6560577
42 feet Y = -1956758
07 meter
Z = 17171104
00 Z = 5252391
66
XDOT = 8106
459848 XDOT = 2385
725660
YDOT = 23587
589033 feet/sec YDOT = 7216
651747 meter/sec
ZDOT = 3069
709330 ZDOT = 947
444128
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6067551
53 X = 1849389
71
Y = 12733423
29 feet Y = 3881147
42 meter
Z = 17249092
50 Z = 5257523
39
XDOT = -22956
597512 XDOT = -6997
170922
YDOT = 6719
312741 feet/sec YDOT = 2048
046523 meter/sec
ZDOT = 3117
960740 ZDOT = 950
354433
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 13138
14067701
00016717 00000-0 10270-3 0 9054
2 25544 51
6469 257
3132 0007066 288
0208 72
0173 15
50209696 30043
Satellite: ISS
Catalog Number: 25544
Epoch time: 13138
14067701 = yrday
fracday
Element set: 905
Inclination: 51
6469 deg
RA of node: 257
3132 deg
Eccentricity:
0007066
Arg of perigee: 288
0208 deg
Mean anomaly: 72
0173 deg
Mean motion: 15
50209696 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3004
Checksum: 291
Coasting Arc #7 (Orbit 3018)
---------------------------------------
Vector Time (GMT): 2013/139/02:10:35
516
Vector Time (MET): N/A
Weight (LBS) : 880039
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3849824
94 A = 6788825
83 meter
Y = 1848371
86 meter E =
0008991
Z = -5284751
89 I = 51
29015
XDOT = -2759
217780 Wp = 65
74586
YDOT = -7125
447816 meter/sec RA = 251
71261 deg
ZDOT = -479
160031 TA = 199
63646
MA = 199
67110
Ha = 225
851 n
mi
Hp = 223
203
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12630659
25 X = -3844535
55
Y = 6064212
13 feet Y = 1805350
38 meter
Z = -17338424
83 Z = -5303441
29
XDOT = -9052
551772 XDOT = -2677
006763
YDOT = -23377
453464 feet/sec YDOT = -7155
843451 meter/sec
ZDOT = -1572
047347 ZDOT = -492
364670
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5788640
52 X = -1764377
63
Y = -12652381
34 feet Y = -3856445
83 meter
Z = -17416603
70 Z = -5308580
81
XDOT = 22646
394543 XDOT = 6902
621057
YDOT = -8109
129440 feet/sec YDOT = -2471
662653 meter/sec
ZDOT = -1626
190967 ZDOT = -495
663007
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 13139
10765793
00016717 00000-0 10270-3 0 9068
2 25544 51
6475 252
5212 0007046 292
8032 67
2374 15
50224009 30192
Satellite: ISS
Catalog Number: 25544
Epoch time: 13139
10765793 = yrday
fracday
Element set: 906
Inclination: 51
6475 deg
RA of node: 252
5212 deg
Eccentricity:
0007046
Arg of perigee: 292
8032 deg
Mean anomaly: 67
2374 deg
Mean motion: 15
50224009 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3019
Checksum: 294
Coasting Arc #8 (Orbit 3034)
---------------------------------------
Vector Time (GMT): 2013/140/02:10:35
516
Vector Time (MET): N/A
Weight (LBS) : 880039
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3898433
42 A = 6788661
02 meter
Y = -1683067
61 meter E =
0005089
Z = 5300225
53 I = 51
30034
XDOT = 3031
306580 Wp = 307
92720
YDOT = 7034
181033 meter/sec RA = 246
72979 deg
ZDOT = 7
160414 TA = 142
02212
MA = 141
98622
Ha = 225
989 n
mi
Hp = 223
253
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12790135
89 X = 3891216
70
Y = -5521875
35 feet Y = -1639513
31 meter
Z = 17389191
38 Z = 5319146
46
XDOT = 9945
231561 XDOT = 2952
388774
YDOT = 23078
021762 feet/sec YDOT = 7067
637761 meter/sec
ZDOT = 23
492172 ZDOT = 21
694861
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5462356
27 X = 1664926
19
Y = 12707606
81 feet Y = 3873278
56 meter
Z = 17468315
70 Z = 5324342
62
XDOT = -22196
722470 XDOT = -6765
561009
YDOT = 9440
674585 feet/sec YDOT = 2877
517613 meter/sec
ZDOT = 83
204300 ZDOT = 25
360671
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 13140
13909015
00016717 00000-0 10270-3 0 9071
2 25544 51
6474 247
4095 0007172 296
3661 63
6753 15
50251497 30350
Satellite: ISS
Catalog Number: 25544
Epoch time: 13140
13909015 = yrday
fracday
Element set: 907
Inclination: 51
6474 deg
RA of node: 247
4095 deg
Eccentricity:
0007172
Arg of perigee: 296
3661 deg
Mean anomaly: 63
6753 deg
Mean motion: 15
50251497 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3035
Checksum: 305
Coasting Arc #9 (Orbit 3049)
---------------------------------------
Vector Time (GMT): 2013/141/02:10:35
516
Vector Time (MET): N/A
Weight (LBS) : 880039
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3978532
98 A = 6788698
40 meter
Y = 1541146
19 meter E =
0008976
Z = -5287634
12 I = 51
31391
XDOT = -3285
554086 Wp = 72
02204
YDOT = -6899
810897 meter/sec RA = 241
74764 deg
ZDOT = 464
458729 TA = 202
41565
MA = 202
45490
Ha = 226
212 n
mi
Hp = 222
886
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13052929
71 X = -3969784
38
Y = 5056253
90 feet Y = 1496704
76 meter
Z = -17347880
99 Z = -5306940
52
XDOT = -10779
376921 XDOT = -3210
410976
YDOT = -22637
174860 feet/sec YDOT = -6936
131897 meter/sec
ZDOT = 1523
814728 ZDOT = 448
679903
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5217871
09 X = -1590407
11
Y = -12880662
95 feet Y = -3926026
07 meter
Z = -17428597
06 Z = -5312236
38
XDOT = 21559
864042 XDOT = 6571
446560
YDOT = -10692
860250 feet/sec YDOT = -3259
183804 meter/sec
ZDOT = 1458
886703 ZDOT = 444
668667
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 13141
10604758
00016717 00000-0 10270-3 0 9086
2 25544 51
6478 242
6172 0007207 300
8119 59
2322 15
50261512 30504
Satellite: ISS
Catalog Number: 25544
Epoch time: 13141
10604758 = yrday
fracday
Element set: 908
Inclination: 51
6478 deg
RA of node: 242
6172 deg
Eccentricity:
0007207
Arg of perigee: 300
8119 deg
Mean anomaly: 59
2322 deg
Mean motion: 15
50261512 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3050
Checksum: 274
Coasting Arc #10 (Orbit 3065)
---------------------------------------
Vector Time (GMT): 2013/142/02:10:35
516
Vector Time (MET): N/A
Weight (LBS) : 880039
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4097056
29 A = 6788828
16 meter
Y = -1391109
87 meter E =
0006665
Z = 5234835
56 I = 51
33024
XDOT = 3509
030072 Wp = 332
83868
YDOT = 6741
899935 meter/sec RA = 236
76654 deg
ZDOT = -949
414371 TA = 126
32696
MA = 126
26541
Ha = 226
347 n
mi
Hp = 222
841
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13441785
73 X = 4086877
54
Y = -4564008
77 feet Y = -1345351
11 meter
Z = 17174657
34 Z = 5254714
32
XDOT = 11512
565853 XDOT = 3437
991986
YDOT = 22119
094275 feet/sec YDOT = 6780
742960 meter/sec
ZDOT = -3114
876544 ZDOT = -932
539778
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4958272
17 X = 1511281
36
Y = 13193422
40 feet Y = 4021355
15 meter
Z = 17257745
41 Z = 5260160
80
XDOT = -20803
127682 XDOT = -6340
793318
YDOT = 11824
394213 feet/sec YDOT = 3604
075356 meter/sec
ZDOT = -3045
351017 ZDOT = -928
222990
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 13142
13745521
00016717 00000-0 10270-3 0 9095
2 25544 51
6480 237
5056 0007313 304
4760 55
5700 15
50292647 30660
Satellite: ISS
Catalog Number: 25544
Epoch time: 13142
13745521 = yrday
fracday
Element set: 909
Inclination: 51
6480 deg
RA of node: 237
5056 deg
Eccentricity:
0007313
Arg of perigee: 304
4760 deg
Mean anomaly: 55
5700 deg
Mean motion: 15
50292647 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3066
Checksum: 289
Coasting Arc #11 (Orbit 3080)
---------------------------------------
Vector Time (GMT): 2013/143/02:10:35
516
Vector Time (MET): N/A
Weight (LBS) : 880039
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4237634
84 A = 6789178
88 meter
Y = 1280618
71 meter E =
0008084
Z = -5153758
84 I = 51
34880
XDOT = -3705
584978 Wp = 75
75277
YDOT = -6547
432318 meter/sec RA = 231
78644 deg
ZDOT = 1423
797689 TA = 208
00016
MA = 208
04367
Ha = 226
534 n
mi
Hp = 222
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13903001
44 X = -4226603
91
Y = 4201504
96 feet Y = 1233292
79 meter
Z = -16908657
61 Z = -5174318
48
XDOT = -12157
431030 XDOT = -3639
011349
YDOT = -21481
077158 feet/sec YDOT = -6588
498357 meter/sec
ZDOT = 4671
252261 ZDOT = 1405
957201
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4844151
13 X = -1476497
26
Y = -13585555
77 feet Y = -4140877
40 meter
Z = -16994577
65 Z = -5179947
27
XDOT = 19893
503500 XDOT = 6063
539867
YDOT = -12829
056803 feet/sec YDOT = -3910
296514 meter/sec
ZDOT = 4597
666808 ZDOT = 1401
368843
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 13143
10439000
00016717 00000-0 10270-3 0 9107
2 25544 51
6478 232
7131 0007369 308
5282 51
5208 15
50296265 30819
Satellite: ISS
Catalog Number: 25544
Epoch time: 13143
10439000 = yrday
fracday
Element set: 910
Inclination: 51
6478 deg
RA of node: 232
7131 deg
Eccentricity:
0007369
Arg of perigee: 308
5282 deg
Mean anomaly: 51
5208 deg
Mean motion: 15
50296265 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3081
Checksum: 280
Coasting Arc #12 (Orbit 3096)
---------------------------------------
Vector Time (GMT): 2013/144/02:10:35
516
Vector Time (MET): N/A
Weight (LBS) : 880039
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4414714
37 A = 6789610
49 meter
Y = -1167597
04 meter E =
0008214
Z = 5027649
64 I = 51
37037
XDOT = 3857
308337 Wp = 354
07148
YDOT = 6336
314111 meter/sec RA = 226
80830 deg
ZDOT = -1907
805152 TA = 114
56420
MA = 114
47857
Ha = 226
674 n
mi
Hp = 222
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14483971
02 X = 4403019
07
Y = -3830698
96 feet Y = -1118294
76 meter
Z = 16494913
52 Z = 5049067
90
XDOT = 12655
211079 XDOT = 3795
435429
YDOT = 20788
432123 feet/sec YDOT = 6379
103182 meter/sec
ZDOT = -6259
203256 ZDOT = -1889
216006
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4744558
40 X = 1446141
40
Y = 14106323
96 feet Y = 4299607
54 meter
Z = 16584409
34 Z = 5054927
97
XDOT = -18901
768898 XDOT = -5761
259160
YDOT = 13655
682220 feet/sec YDOT = 4162
251941 meter/sec
ZDOT = -6182
460883 ZDOT = -1884
414077
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 13144
13577371
00016717 00000-0 10270-3 0 9116
2 25544 51
6479 227
6017 0007471 312
2426 47
8091 15
50331105 30970
Satellite: ISS
Catalog Number: 25544
Epoch time: 13144
13577371 = yrday
fracday
Element set: 911
Inclination: 51
6479 deg
RA of node: 227
6017 deg
Eccentricity:
0007471
Arg of perigee: 312
2426 deg
Mean anomaly: 47
8091 deg
Mean motion: 15
50331105 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3097
Checksum: 290
Coasting Arc #13 (Orbit 3111)
---------------------------------------
Vector Time (GMT): 2013/145/02:10:35
516
Vector Time (MET): N/A
Weight (LBS) : 880039
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4600083
54 A = 6790255
66 meter
Y = 1107005
50 meter E =
0006546
Z = -4875218
25 I = 51
39300
XDOT = -3976
200358 Wp = 73
57472
YDOT = -6100
023786 meter/sec RA = 221
83109 deg
ZDOT = 2371
151130 TA = 219
74437
MA = 219
79235
Ha = 226
825 n
mi
Hp = 222
110
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15092137
58 X = -4588437
47
Y = 3631907
80 feet Y = 1055630
14 meter
Z = -15994810
53 Z = -4897537
06
XDOT = -13045
276765 XDOT = -3919
211687
YDOT = -20013
201399 feet/sec YDOT = -6144
169795 meter/sec
ZDOT = 7779
367223 ZDOT = 2351
972459
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4838120
85 X = -1474659
23
Y = -14648004
37 feet Y = -4464711
73 meter
Z = -16088066
69 Z = -4903642
73
XDOT = 17813
202254 XDOT = 5429
464047
YDOT = -14324
686561 feet/sec YDOT = -4366
164464 meter/sec
ZDOT = 7700
126046 ZDOT = 2346
998419
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 13145
10268649
00016717 00000-0 10270-3 0 9120
2 25544 51
6467 222
8088 0007491 316
0065 44
0488 15
50328394 31128
Satellite: ISS
Catalog Number: 25544
Epoch time: 13145
10268649 = yrday
fracday
Element set: 912
Inclination: 51
6467 deg
RA of node: 222
8088 deg
Eccentricity:
0007491
Arg of perigee: 316
0065 deg
Mean anomaly: 44
0488 deg
Mean motion: 15
50328394 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3112
Checksum: 302
Coasting Arc #14 (Orbit 3127)
---------------------------------------
Vector Time (GMT): 2013/146/02:10:35
516
Vector Time (MET): N/A
Weight (LBS) : 880039
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4816972
86 A = 6790960
28 meter
Y = -1048143
99 meter E =
0009586
Z = 4673091
33 I = 51
41897
XDOT = 4038
082609 Wp = 13
57414
YDOT = 5857
007987 meter/sec RA = 216
85655 deg
ZDOT = -2838
401295 TA = 104
77628
MA = 104
67004
Ha = 226
975 n
mi
Hp = 221
954
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15803716
73 X = 4805634
49
Y = -3438792
62 feet Y = -994341
57 meter
Z = 15331664
48 Z = 4696464
41
XDOT = 13248
302524 XDOT = 3986
076540
YDOT = 19215
905469 feet/sec YDOT = 5901
873962 meter/sec
ZDOT = -9312
340206 ZDOT = -2818
909929
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4967710
61 X = 1514158
19
Y = 15293804
94 feet Y = 4661551
75 meter
Z = 15429325
15 Z = 4702858
31
XDOT = -16696
378707 XDOT = -5089
056230
YDOT = 14770
797651 feet/sec YDOT = 4502
139124 meter/sec
ZDOT = -9231
751110 ZDOT = -2813
837738
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 13146
13404677
00016717 00000-0 10270-3 0 9138
2 25544 51
6465 217
6972 0007607 319
6686 40
3900 15
50365815 31281
Satellite: ISS
Catalog Number: 25544
Epoch time: 13146
13404677 = yrday
fracday
Element set: 913
Inclination: 51
6465 deg
RA of node: 217
6972 deg
Eccentricity:
0007607
Arg of perigee: 319
6686 deg
Mean anomaly: 40
3900 deg
Mean motion: 15
50365815 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3128
Checksum: 313
Coasting Arc #15 (Orbit 3142)
---------------------------------------
Vector Time (GMT): 2013/147/02:10:35
516
Vector Time (MET): N/A
Weight (LBS) : 880039
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5025372
06 A = 6791840
75 meter
Y = 1049793
49 meter E =
0005116
Z = -4448848
28 I = 51
44516
XDOT = -4065
784693 Wp = 57
66102
YDOT = -5603
728380 meter/sec RA = 211
88282 deg
ZDOT = 3275
802113 TA = 245
46804
MA = 245
52139
Ha = 227
086 n
mi
Hp = 221
704
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16487441
13 X = -5015126
10
Y = 3444204
36 feet Y = 993654
50 meter
Z = -14595958
93 Z = -4473236
26
XDOT = -13339
188624 XDOT = -4018
733501
YDOT = -18384
935629 feet/sec YDOT = -5648
931910 meter/sec
ZDOT = 10747
382262 ZDOT = 3256
164266
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5315022
01 X = -1620018
71
Y = -15889098
51 feet Y = -4842997
22 meter
Z = -14697869
42 Z = -4479910
60
XDOT = 15552
983234 XDOT = 4740
549290
YDOT = -15052
658041 feet/sec YDOT = -4588
050171 meter/sec
ZDOT = 10666
134802 ZDOT = 3251
037888
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 13147
10093803
00016717 00000-0 10270-3 0 9142
2 25544 51
6448 212
9036 0007548 323
3790 36
6844 15
50358402 31439
Satellite: ISS
Catalog Number: 25544
Epoch time: 13147
10093803 = yrday
fracday
Element set: 914
Inclination: 51
6448 deg
RA of node: 212
9036 deg
Eccentricity:
0007548
Arg of perigee: 323
3790 deg
Mean anomaly: 36
6844 deg
Mean motion: 15
50358402 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3143
Checksum: 295
Coasting Arc #16 (Orbit 3158)
---------------------------------------
Vector Time (GMT): 2013/148/02:10:35
516
Vector Time (MET): N/A
Weight (LBS) : 880039
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5257627
06 A = 6792746
42 meter
Y = -1055133
71 meter E =
0010682
Z = 4170850
72 I = 51
47506
XDOT = 4027
746879 Wp = 32
10251
YDOT = 5356
057952 meter/sec RA = 206
91240 deg
ZDOT = -3709
020142 TA = 96
19919
MA = 96
07749
Ha = 227
245 n
mi
Hp = 221
519
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17249432
60 X = 5248774
10
Y = -3461724
79 feet Y = -996389
64 meter
Z = 13683893
44 Z = 4196370
25
XDOT = 13214
392646 XDOT = 3985
572404
YDOT = 17572
368609 feet/sec YDOT = 5400
863411 meter/sec
ZDOT = -12168
701252 ZDOT = -3689
555412
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5706800
70 X = 1739432
85
Y = 16553814
82 feet Y = 5045602
76 meter
Z = 13790541
83 Z = 4203357
15
XDOT = -14446
336594 XDOT = -4403
243394
YDOT = 15086
496512 feet/sec YDOT = 4598
364137 meter/sec
ZDOT = -12088
128776 ZDOT = -3684
461651
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 13148
13227536
00016717 00000-0 10270-3 0 9159
2 25544 51
6448 207
7915 0007688 326
8356 33
2312 15
50397353 31596
Satellite: ISS
Catalog Number: 25544
Epoch time: 13148
13227536 = yrday
fracday
Element set: 915
Inclination: 51
6448 deg
RA of node: 207
7915 deg
Eccentricity:
0007688
Arg of perigee: 326
8356 deg
Mean anomaly: 33
2312 deg
Mean motion: 15
50397353 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3159
Checksum: 319
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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