[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 4th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 17276 08 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 131 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 219 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 1174)
---------------------------------------
Vector Time (GMT): 2015/063/12:01:00
251
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4504613
91 A = 6776493
69 meter
Y = 160993
84 meter E =
0013846
Z = 5050932
74 I = 51
29003
XDOT = 1712
168335 Wp = 63
00949
YDOT = 7276
526686 meter/sec RA = 245
95130 deg
ZDOT = -1749
018932 TA = 44
02085
MA = 43
91068
Ha = 222
948 n
mi
Hp = 210
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14778917
04 X = 4477943
76
Y = 528195
02 feet Y = 211218
96 meter
Z = 16571301
63 Z = 5072750
07
XDOT = 5617
350180 XDOT = 1639
169166
YDOT = 23873
119048 feet/sec YDOT = 7295
264864 meter/sec
ZDOT = -5738
251089 ZDOT = -1740
880022
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13733611
27 X = 4186004
72
Y = 5194411
10 feet Y = 1583256
50 meter
Z = 16664616
15 Z = 5079375
00
XDOT = -1898
893570 XDOT = -578
782760
YDOT = 23425
510989 feet/sec YDOT = 7140
095749 meter/sec
ZDOT = -5704
622418 ZDOT = -1738
768913
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 15063
54595058
00016717 00000-0 10270-3 0 9003
2 25544 51
6406 246
6885 0008652 67
6435 292
5635 15
54765446 11758
Satellite: ISS
Catalog Number: 25544
Epoch time: 15063
54595058 = yrday
fracday
Element set: 900
Inclination: 51
6406 deg
RA of node: 246
6885 deg
Eccentricity:
0008652
Arg of perigee: 67
6435 deg
Mean anomaly: 292
5635 deg
Mean motion: 15
54765446 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1175
Checksum: 335
Coasting Arc #2 (Orbit 1189)
---------------------------------------
Vector Time (GMT): 2015/064/12:01:00
251
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4952132
45 A = 6779790
40 meter
Y = -2012304
87 meter E =
0015787
Z = -4184166
59 I = 51
31536
XDOT = -366
160059 Wp = 90
05959
YDOT = -6710
054276 meter/sec RA = 240
92651 deg
ZDOT = 3672
487460 TA = 217
78937
MA = 217
90032
Ha = 223
017 n
mi
Hp = 210
368
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16247153
70 X = -4908937
53
Y = -6602050
09 feet Y = -2067441
96 meter
Z = -13727580
69 Z = -4208117
50
XDOT = -1201
312530 XDOT = -308
938725
YDOT = -22014
613767 feet/sec YDOT = -6713
828423 meter/sec
ZDOT = 12048
843372 ZDOT = 3670
848743
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13394037
17 X = -4082502
53
Y = -11195620
74 feet Y = -3412425
20 meter
Z = -13829728
31 Z = -4215301
19
XDOT = 4646
230276 XDOT = 1416
170988
YDOT = -20386
550196 feet/sec YDOT = -6213
820500 meter/sec
ZDOT = 12042
917751 ZDOT = 3670
681331
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 15064
51006132
00016717 00000-0 10270-3 0 9012
2 25544 51
6406 241
8762 0008730 71
5871 288
6231 15
54821439 11904
Satellite: ISS
Catalog Number: 25544
Epoch time: 15064
51006132 = yrday
fracday
Element set: 901
Inclination: 51
6406 deg
RA of node: 241
8762 deg
Eccentricity:
0008730
Arg of perigee: 71
5871 deg
Mean anomaly: 288
6231 deg
Mean motion: 15
54821439 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1190
Checksum: 290
Coasting Arc #3 (Orbit 1205)
---------------------------------------
Vector Time (GMT): 2015/065/12:01:00
251
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5054069
51 A = 6784034
36 meter
Y = 3619131
20 meter E =
0021510
Z = 2697656
07 I = 51
34611
XDOT = -1212
520799 Wp = 90
96830
YDOT = 5558
357087 meter/sec RA = 235
91591 deg
ZDOT = -5150
068709 TA = 58
38305
MA = 58
17333
Ha = 222
895 n
mi
Hp = 210
405
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16581592
87 X = 5000119
85
Y = 11873790
04 feet Y = 3675347
88 meter
Z = 8850577
66 Z = 2722075
85
XDOT = -3978
086610 XDOT = -1249
568740
YDOT = 18236
079682 feet/sec YDOT = 5544
589935 meter/sec
ZDOT = -16896
550881 ZDOT = -5156
049681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12421659
44 X = 3786121
80
Y = 16117954
62 feet Y = 4912752
57 meter
Z = 8954482
25 Z = 2729326
19
XDOT = -7766
316393 XDOT = -2367
173237
YDOT = 15450
573876 feet/sec YDOT = 4709
334917 meter/sec
ZDOT = -16923
030727 ZDOT = -5158
139766
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 15065
53842182
00016717 00000-0 10270-3 0 9029
2 25544 51
6406 236
7433 0008596 74
3141 285
8960 15
54864009 12069
Satellite: ISS
Catalog Number: 25544
Epoch time: 15065
53842182 = yrday
fracday
Element set: 902
Inclination: 51
6406 deg
RA of node: 236
7433 deg
Eccentricity:
0008596
Arg of perigee: 74
3141 deg
Mean anomaly: 285
8960 deg
Mean motion: 15
54864009 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1206
Checksum: 312
Coasting Arc #4 (Orbit 1220)
---------------------------------------
Vector Time (GMT): 2015/066/12:01:00
251
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4769635
46 A = 6786733
07 meter
Y = -4737726
10 meter E =
0017606
Z = -895617
34 I = 51
37474
XDOT = 2854
048075 Wp = 57
82385
YDOT = -3972
018354 meter/sec RA = 230
91816 deg
ZDOT = 5906
702258 TA = 292
44464
MA = 292
63101
Ha = 222
944 n
mi
Hp = 210
282
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15648410
29 X = -4711952
06
Y = -15543720
79 feet Y = -4790740
89 meter
Z = -2938377
09 Z = -918646
25
XDOT = 9363
674787 XDOT = 2869
559695
YDOT = -13031
556281 feet/sec YDOT = -3940
014866 meter/sec
ZDOT = 19378
944416 ZDOT = 5920
604851
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10842216
41 X = -3304707
56
Y = -19192241
06 feet Y = -5849795
07 meter
Z = -3036163
22 Z = -925422
55
XDOT = 11021
157963 XDOT = 3359
248947
YDOT = -9253
924159 feet/sec YDOT = -2820
596084 meter/sec
ZDOT = 19439
061095 ZDOT = 5925
025822
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 15066
50248945
00016717 00000-0 10270-3 0 9035
2 25544 51
6415 231
9315 0008761 78
7438 281
4699 15
54895385 12215
Satellite: ISS
Catalog Number: 25544
Epoch time: 15066
50248945 = yrday
fracday
Element set: 903
Inclination: 51
6415 deg
RA of node: 231
9315 deg
Eccentricity:
0008761
Arg of perigee: 78
7438 deg
Mean anomaly: 281
4699 deg
Mean motion: 15
54895385 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1221
Checksum: 334
Coasting Arc #5 (Orbit 1236)
---------------------------------------
Vector Time (GMT): 2015/067/12:01:00
251
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3977863
40 A = 6786395
45 meter
Y = 5382626
78 meter E =
0015771
Z = -1109887
10 I = 51
39496
XDOT = -4469
734117 Wp = 112
80717
YDOT = 2109
859012 meter/sec RA = 225
92642 deg
ZDOT = -5860
032868 TA = 79
27668
MA = 79
09916
Ha = 222
902 n
mi
Hp = 210
160
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13050732
94 X = 3922769
34
Y = 17659536
67 feet Y = 5426801
62 meter
Z = -3641361
87 Z = -1090698
15
XDOT = -14664
482012 XDOT = -4464
529154
YDOT = 6922
109618 feet/sec YDOT = 2059
903736 meter/sec
ZDOT = -19225
829621 ZDOT = -5881
733535
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8161535
53 X = 2487636
03
Y = 20399887
83 feet Y = 6217885
81 meter
Z = -3560097
84 Z = -1085117
82
XDOT = -14335
254555 XDOT = -4369
385588
YDOT = 2406
253421 feet/sec YDOT = 733
426043 meter/sec
ZDOT = -19319
020339 ZDOT = -5888
437399
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 15067
53080217
00016717 00000-0 10270-3 0 9046
2 25544 51
6415 226
7984 0008792 80
7360 279
4787 15
54964212 12378
Satellite: ISS
Catalog Number: 25544
Epoch time: 15067
53080217 = yrday
fracday
Element set: 904
Inclination: 51
6415 deg
RA of node: 226
7984 deg
Eccentricity:
0008792
Arg of perigee: 80
7360 deg
Mean anomaly: 279
4787 deg
Mean motion: 15
54964212 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1237
Checksum: 328
Coasting Arc #6 (Orbit 1252)
---------------------------------------
Vector Time (GMT): 2015/068/12:01:00
251
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2758699
09 A = 6783307
47 meter
Y = -5461649
90 meter E =
0022012
Z = 2905716
80 I = 51
40804
XDOT = 5810
645463 Wp = 83
41590
YDOT = -253
463075 meter/sec RA = 220
93075 deg
ZDOT = 5010
045350 TA = 309
87083
MA = 310
06422
Ha = 222
867 n
mi
Hp = 210
147
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9050850
03 X = -2711535
45
Y = -17918798
89 feet Y = -5492235
35 meter
Z = 9533191
59 Z = 2892430
94
XDOT = 19063
797451 XDOT = 5788
711019
YDOT = -831
571768 feet/sec YDOT = -188
606571 meter/sec
ZDOT = 16437
156660 ZDOT = 5038
219025
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4600510
72 X = -1402235
67
Y = -19567859
59 feet Y = -5964283
60 meter
Z = 9477191
24 Z = 2888647
89
XDOT = 17188
036929 XDOT = 5238
913656
YDOT = 4026
580553 feet/sec YDOT = 1227
301753 meter/sec
ZDOT = 16557
761304 ZDOT = 5046
805645
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 15068
55909097
00016717 00000-0 10270-3 0 9056
2 25544 51
6422 221
6659 0008725 85
9211 274
2939 15
54982764 12539
Satellite: ISS
Catalog Number: 25544
Epoch time: 15068
55909097 = yrday
fracday
Element set: 905
Inclination: 51
6422 deg
RA of node: 221
6659 deg
Eccentricity:
0008725
Arg of perigee: 85
9211 deg
Mean anomaly: 274
2939 deg
Mean motion: 15
54982764 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1253
Checksum: 339
Coasting Arc #7 (Orbit 1267)
---------------------------------------
Vector Time (GMT): 2015/069/12:01:00
251
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1091797
16 A = 6778740
44 meter
Y = 5087568
04 meter E =
0017280
Z = -4361314
19 I = 51
41836
XDOT = -6690
182144 Wp = 79
29458
YDOT = -1483
813738 meter/sec RA = 215
92427 deg
ZDOT = -3414
101395 TA = 155
96437
MA = 155
88362
Ha = 222
829 n
mi
Hp = 210
066
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3582011
67 X = 1056011
24
Y = 16691496
18 feet Y = 5099576
56 meter
Z = -14308773
59 Z = -4356098
04
XDOT = -21949
416482 XDOT = -6656
508145
YDOT = -4868
155308 feet/sec YDOT = -1558
439884 meter/sec
ZDOT = -11201
120063 ZDOT = -3446
518984
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -97515
75 X = -29722
80
Y = 17089266
82 feet Y = 5208808
53 meter
Z = -14287242
71 Z = -4354751
58
XDOT = -19019
896411 XDOT = -5797
264426
YDOT = -9565
787643 feet/sec YDOT = -2915
652074 meter/sec
ZDOT = -11339
625883 ZDOT = -3456
317969
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 15069
52308854
00016717 00000-0 10270-3 0 9069
2 25544 51
6430 216
8545 0008788 88
3868 271
8292 15
55010769 12681
Satellite: ISS
Catalog Number: 25544
Epoch time: 15069
52308854 = yrday
fracday
Element set: 906
Inclination: 51
6430 deg
RA of node: 216
8545 deg
Eccentricity:
0008788
Arg of perigee: 88
3868 deg
Mean anomaly: 271
8292 deg
Mean motion: 15
55010769 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1268
Checksum: 344
Coasting Arc #8 (Orbit 1283)
---------------------------------------
Vector Time (GMT): 2015/070/12:01:00
251
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 797980
52 A = 6775265
92 meter
Y = -4312217
96 meter E =
0012613
Z = 5154461
81 I = 51
43350
XDOT = 6973
411817 Wp = 103
25946
YDOT = 2915
907037 meter/sec RA = 210
90519 deg
ZDOT = 1354
233291 TA = 333
67297
MA = 333
73702
Ha = 222
664 n
mi
Hp = 210
033
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2618046
32 X = 821103
02
Y = -14147696
72 feet Y = -4303164
53 meter
Z = 16910963
93 Z = 5158394
90
XDOT = 22878
647694 XDOT = 6933
708822
YDOT = 9566
624136 feet/sec YDOT = 2993
666445 meter/sec
ZDOT = 4443
022608 ZDOT = 1388
011965
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5339243
41 X = 1627401
39
Y = -13338352
86 feet Y = -4065529
95 meter
Z = 16928467
52 Z = 5159796
90
XDOT = 19449
975268 XDOT = 5928
352462
YDOT = 13630
920953 feet/sec YDOT = 4154
704706 meter/sec
ZDOT = 4587
145223 ZDOT = 1398
161864
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 15070
55132657
00016717 00000-0 10270-3 0 9071
2 25544 51
6429 211
7211 0008642 91
8197 268
3946 15
55063815 12841
Satellite: ISS
Catalog Number: 25544
Epoch time: 15070
55132657 = yrday
fracday
Element set: 907
Inclination: 51
6429 deg
RA of node: 211
7211 deg
Eccentricity:
0008642
Arg of perigee: 91
8197 deg
Mean anomaly: 268
3946 deg
Mean motion: 15
55063815 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1284
Checksum: 316
Coasting Arc #9 (Orbit 1298)
---------------------------------------
Vector Time (GMT): 2015/071/12:01:00
251
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2773421
43 A = 6774802
84 meter
Y = 3299857
57 meter E =
0023256
Z = -5246958
53 I = 51
46045
XDOT = -6477
843735 Wp = 96
56294
YDOT = -3966
749290 meter/sec RA = 205
88307 deg
ZDOT = 930
271741 TA = 182
37239
MA = 182
38344
Ha = 222
686 n
mi
Hp = 209
818
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9099151
69 X = -2784627
39
Y = 10826304
35 feet Y = 3268780
15 meter
Z = -17214430
86 Z = -5260458
80
XDOT = -21252
768161 XDOT = -6437
524062
YDOT = -13014
269324 feet/sec YDOT = -4038
963228 meter/sec
ZDOT = 3052
072641 ZDOT = 898
902053
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10853602
34 X = -3308177
99
Y = 8955007
60 feet Y = 2729486
32 meter
Z = -17272730
31 Z = -5264728
20
XDOT = -17813
335849 XDOT = -5429
504767
YDOT = -15966
928635 feet/sec YDOT = -4866
719848 meter/sec
ZDOT = 2918
407703 ZDOT = 889
530668
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 15071
51527711
00016717 00000-0 10270-3 0 9088
2 25544 51
6435 206
9103 0008788 95
0205 265
1952 15
55098231 12999
Satellite: ISS
Catalog Number: 25544
Epoch time: 15071
51527711 = yrday
fracday
Element set: 908
Inclination: 51
6435 deg
RA of node: 206
9103 deg
Eccentricity:
0008788
Arg of perigee: 95
0205 deg
Mean anomaly: 265
1952 deg
Mean motion: 15
55098231 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1299
Checksum: 311
Coasting Arc #10 (Orbit 1314)
---------------------------------------
Vector Time (GMT): 2015/072/12:01:00
251
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4556386
14 A = 6777670
70 meter
Y = -2122412
89 meter E =
0016763
Z = 4533250
15 I = 51
49897
XDOT = 5265
138611 Wp = 83
03043
YDOT = 4648
900039 meter/sec RA = 200
86464 deg
ZDOT = -3103
601507 TA = 38
12302
MA = 38
00455
Ha = 222
591 n
mi
Hp = 209
940
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14948773
42 X = 4557760
09
Y = -6963296
87 feet Y = -2071452
28 meter
Z = 14872867
94 Z = 4555387
63
XDOT = 17274
076807 XDOT = 5227
838261
YDOT = 15252
296717 feet/sec YDOT = 4707
569397 meter/sec
ZDOT = -10182
419642 ZDOT = -3078
115652
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15820909
37 X = 4822213
18
Y = -4337546
72 feet Y = -1322084
24 meter
Z = 14967967
33 Z = 4562236
44
XDOT = 14179
283517 XDOT = 4321
845616
YDOT = 16821
302081 feet/sec YDOT = 5127
132874 meter/sec
ZDOT = -10074
031095 ZDOT = -3070
564678
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 15072
54346597
00016717 00000-0 10270-3 0 9094
2 25544 51
6434 201
7762 0008818 98
5587 261
6565 15
55090233 13151
Satellite: ISS
Catalog Number: 25544
Epoch time: 15072
54346597 = yrday
fracday
Element set: 909
Inclination: 51
6434 deg
RA of node: 201
7762 deg
Eccentricity:
0008818
Arg of perigee: 98
5587 deg
Mean anomaly: 261
6565 deg
Mean motion: 15
55090233 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1315
Checksum: 329
Coasting Arc #11 (Orbit 1329)
---------------------------------------
Vector Time (GMT): 2015/073/12:01:00
251
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5917266
22 A = 6781972
13 meter
Y = 949939
10 meter E =
0013031
Z = -3187083
94 I = 51
54431
XDOT = -3369
283222 Wp = 94
28224
YDOT = -4923
632484 meter/sec RA = 195
86217 deg
ZDOT = 4804
039226 TA = 228
87720
MA = 228
98976
Ha = 222
518 n
mi
Hp = 209
869
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19413603
07 X = -5911967
33
Y = 3116598
11 feet Y = 883797
70 meter
Z = -10456312
15 Z = -3215815
87
XDOT = -11054
078811 XDOT = -3337
311636
YDOT = -16153
649883 feet/sec YDOT = -4961
130797 meter/sec
ZDOT = 15761
283550 ZDOT = 4787
750141
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19595806
83 X = -5972801
92
Y = 121052
26 feet Y = 36896
73 meter
Z = -10579476
98 Z = -3224624
58
XDOT = -8544
287132 XDOT = -2604
298718
YDOT = -16238
737865 feet/sec YDOT = -4949
567301 meter/sec
ZDOT = 15692
297603 ZDOT = 4783
012309
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 15073
50736664
00016717 00000-0 10270-3 0 9101
2 25544 51
6440 196
9642 0008624 100
7010 259
5114 15
55141930 13306
Satellite: ISS
Catalog Number: 25544
Epoch time: 15073
50736664 = yrday
fracday
Element set: 910
Inclination: 51
6440 deg
RA of node: 196
9642 deg
Eccentricity:
0008624
Arg of perigee: 100
7010 deg
Mean anomaly: 259
5114 deg
Mean motion: 15
55141930 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1330
Checksum: 281
Coasting Arc #12 (Orbit 1345)
---------------------------------------
Vector Time (GMT): 2015/074/12:01:00
251
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6646669
93 A = 6785492
90 meter
Y = 229388
74 meter E =
0022306
Z = 1297352
63 I = 51
58718
XDOT = 982
389227 Wp = 114
67616
YDOT = 4895
423240 meter/sec RA = 190
87503 deg
ZDOT = -5829
036861 TA = 51
18028
MA = 50
98134
Ha = 222
450 n
mi
Hp = 209
859
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21806659
88 X = 6637308
87
Y = 752587
74 feet Y = 303663
93 meter
Z = 4256406
26 Z = 1329617
76
XDOT = 3223
061770 XDOT = 955
889419
YDOT = 16061
099870 feet/sec YDOT = 4906
260223 meter/sec
ZDOT = -19124
136682 ZDOT = -5824
329495
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21474957
97 X = 6545567
19
Y = 3705136
18 feet Y = 1129325
51 meter
Z = 4394535
68 Z = 1339454
47
XDOT = 1401
445190 XDOT = 427
160494
YDOT = 14798
899774 feet/sec YDOT = 4510
704651 meter/sec
ZDOT = -19104
728713 ZDOT = -5823
121312
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 15074
53550331
00016717 00000-0 10270-3 0 9111
2 25544 51
6441 191
8302 0008679 104
8657 255
3458 15
55189143 13466
Satellite: ISS
Catalog Number: 25544
Epoch time: 15074
53550331 = yrday
fracday
Element set: 911
Inclination: 51
6441 deg
RA of node: 191
8302 deg
Eccentricity:
0008679
Arg of perigee: 104
8657 deg
Mean anomaly: 255
3458 deg
Mean motion: 15
55189143 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1346
Checksum: 311
Coasting Arc #13 (Orbit 1361)
---------------------------------------
Vector Time (GMT): 2015/075/12:01:00
251
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6619215
38 A = 6785914
91 meter
Y = -1271351
33 meter E =
0019595
Z = 738053
69 I = 51
62107
XDOT = 1557
346728 Wp = 74
01425
YDOT = -4579
076610 meter/sec RA = 185
89726 deg
ZDOT = 5953
158725 TA = 293
96720
MA = 294
17226
Ha = 222
390 n
mi
Hp = 209
879
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21716585
90 X = -6608092
02
Y = -4171100
16 feet Y = -1345309
44 meter
Z = 2421436
00 Z = 705926
39
XDOT = 5109
405276 XDOT = 1579
517447
YDOT = -15023
217223 feet/sec YDOT = -4561
536729 meter/sec
ZDOT = 19531
360645 ZDOT = 5960
778266
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21082049
23 X = -6425808
61
Y = -6723236
02 feet Y = -2049242
34 meter
Z = 2284037
97 Z = 696174
77
XDOT = 6244
542237 XDOT = 1903
336474
YDOT = -12785
464577 feet/sec YDOT = -3897
009603 meter/sec
ZDOT = 19564
690538 ZDOT = 5963
317676
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 15075
56361318
00016717 00000-0 10270-3 0 9121
2 25544 51
6450 186
6968 0008672 107
0869 253
1235 15
55233997 13623
Satellite: ISS
Catalog Number: 25544
Epoch time: 15075
56361318 = yrday
fracday
Element set: 912
Inclination: 51
6450 deg
RA of node: 186
6968 deg
Eccentricity:
0008672
Arg of perigee: 107
0869 deg
Mean anomaly: 253
1235 deg
Mean motion: 15
55233997 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1362
Checksum: 328
Coasting Arc #14 (Orbit 1376)
---------------------------------------
Vector Time (GMT): 2015/076/12:01:00
251
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5779265
78 A = 6782889
09 meter
Y = 2261009
73 meter E =
0013420
Z = -2739760
10 I = 51
64311
XDOT = -4003
841926 Wp = 115
91630
YDOT = 4016
817456 meter/sec RA = 180
91775 deg
ZDOT = -5156
188078 TA = 95
08391
MA = 94
93071
Ha = 222
328 n
mi
Hp = 209
901
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18960845
73 X = 5766861
66
Y = 7418010
92 feet Y = 2325567
55 meter
Z = -8988714
23 Z = -2711716
34
XDOT = -13135
964325 XDOT = -4023
414856
YDOT = 13178
534960 feet/sec YDOT = 3971
933785 meter/sec
ZDOT = -16916
627554 ZDOT = -5175
685757
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18164429
56 X = 5536518
13
Y = 9313052
35 feet Y = 2838618
36 meter
Z = -8868939
89 Z = -2703252
88
XDOT = -13621
985574 XDOT = -4151
981203
YDOT = 10459
001943 feet/sec YDOT = 3187
903792 meter/sec
ZDOT = -17000
748759 ZDOT = -5181
828222
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 15076
52744211
00016717 00000-0 10270-3 0 9136
2 25544 51
6452 181
8841 0008622 110
8137 249
3941 15
55275622 13775
Satellite: ISS
Catalog Number: 25544
Epoch time: 15076
52744211 = yrday
fracday
Element set: 913
Inclination: 51
6452 deg
RA of node: 181
8841 deg
Eccentricity:
0008622
Arg of perigee: 110
8137 deg
Mean anomaly: 249
3941 deg
Mean motion: 15
55275622 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1377
Checksum: 305
Coasting Arc #15 (Orbit 1392)
---------------------------------------
Vector Time (GMT): 2015/077/12:01:00
251
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4261459
62 A = 6778155
27 meter
Y = -3079616
56 meter E =
0018574
Z = 4266799
98 I = 51
66009
XDOT = 5957
640457 Wp = 110
21451
YDOT = -3260
939009 meter/sec RA = 175
92665 deg
ZDOT = 3577
654163 TA = 303
24072
MA = 303
41860
Ha = 222
237 n
mi
Hp = 209
818
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13981166
74 X = -4247432
17
Y = -10103728
88 feet Y = -3127191
93 meter
Z = 13998687
60 Z = 4246133
41
XDOT = 19546
064492 XDOT = 5976
283565
YDOT = -10698
618795 feet/sec YDOT = -3194
212014 meter/sec
ZDOT = 11737
710508 ZDOT = 3606
640640
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13164733
83 X = -4012610
87
Y = -11256372
68 feet Y = -3430942
39 meter
Z = 13910624
45 Z = 4239958
33
XDOT = 19485
469303 XDOT = 5939
171044
YDOT = -8052
304753 feet/sec YDOT = -2454
342489 meter/sec
ZDOT = 11862
369933 ZDOT = 3615
650356
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 15077
55549991
00016717 00000-0 10270-3 0 9149
2 25544 51
6458 176
7503 0008590 114
0292 246
1761 15
55342746 13936
Satellite: ISS
Catalog Number: 25544
Epoch time: 15077
55549991 = yrday
fracday
Element set: 914
Inclination: 51
6458 deg
RA of node: 176
7503 deg
Eccentricity:
0008590
Arg of perigee: 114
0292 deg
Mean anomaly: 246
1761 deg
Mean motion: 15
55342746 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1393
Checksum: 329
- This mailing list is a public mailing list - anyone may join or leave, at any time.
-
This mailing list is announce-only.
ISS TLE list
Privacy Policy:
Private list