[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 1st 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 40902 86 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 121 7 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 169 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
072/03:59:49
040 -1
0 1
6 1
6
N/A -1
2 -0
0 224
0
000/00:03:38
080 0
5 0
0 220
6
Coasting Arc #1 (Orbit 3445)
---------------------------------------
Vector Time (GMT): 2014/059/10:21:16
157
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3712466
26 A = 6792517
60 meter
Y = -4166260
52 meter E =
0011499
Z = 3867605
16 I = 51
29307
XDOT = 2464
198065 Wp = 114
91459
YDOT = 5999
264242 meter/sec RA = 277
96545 deg
ZDOT = 4082
831597 TA = 291
96952
MA = 292
09168
Ha = 226
244 n
mi
Hp = 219
984
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12180007
43 X = 3739991
24
Y = -13668833
72 feet Y = -4124590
97 meter
Z = 12688993
30 Z = 3885706
75
XDOT = 8084
639321 XDOT = 2377
097160
YDOT = 19682
625467 feet/sec YDOT = 6026
333967 meter/sec
ZDOT = 13395
116787 ZDOT = 4094
589773
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18250967
87 X = 5562895
01
Y = -362282
94 feet Y = -110423
84 meter
Z = 12766012
30 Z = 3891080
55
XDOT = -9081
124762 XDOT = -2767
926827
YDOT = 17890
788341 feet/sec YDOT = 5453
112286 meter/sec
ZDOT = 13443
808389 ZDOT = 4097
672797
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 14059
48747252
00016717 00000-0 10270-3 0 9005
2 25544 51
6486 278
4410 0003203 192
0179 168
0896 15
50838095 34464
Satellite: ISS
Catalog Number: 25544
Epoch time: 14059
48747252 = yrday
fracday
Element set: 900
Inclination: 51
6486 deg
RA of node: 278
4410 deg
Eccentricity:
0003203
Arg of perigee: 192
0179 deg
Mean anomaly: 168
0896 deg
Mean motion: 15
50838095 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3446
Checksum: 323
Coasting Arc #2 (Orbit 3460)
---------------------------------------
Vector Time (GMT): 2014/060/10:21:16
157
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3638785
29 A = 6790897
43 meter
Y = 3815265
39 meter E =
0006767
Z = -4285928
36 I = 51
28433
XDOT = -2495
062698 Wp = 90
85075
YDOT = -6326
714763 meter/sec RA = 272
97882 deg
ZDOT = -3518
549637 TA = 143
09234
MA = 143
04575
Ha = 225
977 n
mi
Hp = 220
007
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11938271
94 X = -3660358
73
Y = 12517274
91 feet Y = 3774452
94 meter
Z = -14061444
76 Z = -4303657
66
XDOT = -8185
901241 XDOT = -2407
038851
YDOT = -20756
938198 feet/sec YDOT = -6354
124472 meter/sec
ZDOT = -11543
798022 ZDOT = -3530
455391
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17235859
36 X = -5253489
93
Y = 62489
48 feet Y = 19046
79 meter
Z = -14136830
77 Z = -4308906
02
XDOT = 9426
745851 XDOT = 2873
272135
YDOT = -18940
707472 feet/sec YDOT = -5773
127637 meter/sec
ZDOT = -11593
075914 ZDOT = -3533
569538
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 14060
45402484
00016717 00000-0 10270-3 0 9010
2 25544 51
6480 273
6461 0003252 200
8803 159
2215 15
50899666 34612
Satellite: ISS
Catalog Number: 25544
Epoch time: 14060
45402484 = yrday
fracday
Element set: 901
Inclination: 51
6480 deg
RA of node: 273
6461 deg
Eccentricity:
0003252
Arg of perigee: 200
8803 deg
Mean anomaly: 159
2215 deg
Mean motion: 15
50899666 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3461
Checksum: 296
Coasting Arc #3 (Orbit 3476)
---------------------------------------
Vector Time (GMT): 2014/061/10:21:16
157
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3590641
01 A = 6789499
05 meter
Y = -3432750
46 meter E =
0008939
Z = 4625922
95 I = 51
27916
XDOT = 2563
822087 Wp = 135
67863
YDOT = 6611
696356 meter/sec RA = 267
99008 deg
ZDOT = 2906
592423 TA = 285
18748
MA = 285
28632
Ha = 225
845 n
mi
Hp = 220
063
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11780318
27 X = 3606289
00
Y = -11262304
66 feet Y = -3392509
43 meter
Z = 15176912
55 Z = 4643404
04
XDOT = 8411
489787 XDOT = 2475
578970
YDOT = 21691
917180 feet/sec YDOT = 6639
873694 meter/sec
ZDOT = 9536
064381 ZDOT = 2918
831619
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 16223164
87 X = 4944820
65
Y = 405339
14 feet Y = 123547
37 meter
Z = 15251186
89 Z = 4648561
76
XDOT = -9541
817718 XDOT = -2908
346040
YDOT = 19999
824551 feet/sec YDOT = 6095
946523 meter/sec
ZDOT = 9586
718285 ZDOT = 2922
031733
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 14061
48498313
00016717 00000-0 10270-3 0 9021
2 25544 51
6479 268
5310 0003120 202
8940 157
2073 15
50934269 34770
Satellite: ISS
Catalog Number: 25544
Epoch time: 14061
48498313 = yrday
fracday
Element set: 902
Inclination: 51
6479 deg
RA of node: 268
5310 deg
Eccentricity:
0003120
Arg of perigee: 202
8940 deg
Mean anomaly: 157
2073 deg
Mean motion: 15
50934269 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3477
Checksum: 305
Coasting Arc #4 (Orbit 3491)
---------------------------------------
Vector Time (GMT): 2014/062/10:21:16
157
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3611637
24 A = 6788091
35 meter
Y = 2980102
33 meter E =
0010164
Z = -4923671
96 I = 51
27634
XDOT = -2629
218040 Wp = 85
89943
YDOT = -6840
240100 meter/sec RA = 262
99899 deg
ZDOT = -2214
785637 TA = 162
35185
MA = 162
31652
Ha = 225
591 n
mi
Hp = 220
005
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11849203
55 X = -3620775
60
Y = 9777238
61 feet Y = 2939662
87 meter
Z = -16153779
39 Z = -4941239
24
XDOT = -8626
043439 XDOT = -2541
774914
YDOT = -22441
732613 feet/sec YDOT = -6869
153105 meter/sec
ZDOT = -7266
357077 ZDOT = -2227
344486
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15233742
04 X = -4643244
58
Y = -1231466
49 feet Y = -375350
99 meter
Z = -16228345
62 Z = -4946399
74
XDOT = 9476
686229 XDOT = 2888
493963
YDOT = -20929
197717 feet/sec YDOT = -6379
219464 meter/sec
ZDOT = -7318
336052 ZDOT = -2230
628829
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 14062
45147257
00016717 00000-0 10270-3 0 9038
2 25544 51
6470 263
7351 0003165 211
3575 148
7388 15
51010490 34924
Satellite: ISS
Catalog Number: 25544
Epoch time: 14062
45147257 = yrday
fracday
Element set: 903
Inclination: 51
6470 deg
RA of node: 263
7351 deg
Eccentricity:
0003165
Arg of perigee: 211
3575 deg
Mean anomaly: 148
7388 deg
Mean motion: 15
51010490 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3492
Checksum: 296
Coasting Arc #5 (Orbit 3507)
---------------------------------------
Vector Time (GMT): 2014/063/10:21:16
157
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3670808
37 A = 6787117
15 meter
Y = -2507042
42 meter E =
0005684
Z = 5128166
76 I = 51
27835
XDOT = 2707
494154 Wp = 158
18973
YDOT = 7014
328057 meter/sec RA = 258
00738 deg
ZDOT = 1485
366534 TA = 277
39441
MA = 277
45900
Ha = 225
429 n
mi
Hp = 220
127
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12043334
55 X = 3673659
03
Y = -8225204
77 feet Y = -2465976
44 meter
Z = 16824694
10 Z = 5146006
18
XDOT = 8882
854835 XDOT = 2621
641746
YDOT = 23012
887327 feet/sec YDOT = 7044
125167 meter/sec
ZDOT = 4873
249782 ZDOT = 1498
309585
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14324223
66 X = 4366023
37
Y = 2227433
64 feet Y = 678921
77 meter
Z = 16900336
93 Z = 5151222
70
XDOT = -9218
376950 XDOT = -2809
761294
YDOT = 21758
388234 feet/sec YDOT = 6631
956734 meter/sec
ZDOT = 4926
833493 ZDOT = 1501
698849
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 14063
48236325
00016717 00000-0 10270-3 0 9048
2 25544 51
6473 258
6199 0003100 214
1923 145
9029 15
51035334 35080
Satellite: ISS
Catalog Number: 25544
Epoch time: 14063
48236325 = yrday
fracday
Element set: 904
Inclination: 51
6473 deg
RA of node: 258
6199 deg
Eccentricity:
0003100
Arg of perigee: 214
1923 deg
Mean anomaly: 145
9029 deg
Mean motion: 15
51035334 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3508
Checksum: 292
Coasting Arc #6 (Orbit 3522)
---------------------------------------
Vector Time (GMT): 2014/064/10:21:16
157
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3804972
27 A = 6786300
34 meter
Y = 1991697
85 meter E =
0012509
Z = -5265196
11 I = 51
28261
XDOT = -2756
530513 Wp = 94
47695
YDOT = -7106
723926 meter/sec RA = 253
01355 deg
ZDOT = -698
654945 TA = 168
81907
MA = 168
79125
Ha = 225
234 n
mi
Hp = 219
978
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12483504
83 X = -3801384
58
Y = 6534441
78 feet Y = 1949167
64 meter
Z = -17274265
45 Z = -5283671
56
XDOT = -9043
735278 XDOT = -2673
462833
YDOT = -23316
023379 feet/sec YDOT = -7137
084843 meter/sec
ZDOT = -2292
175017 ZDOT = -711
843092
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13542851
52 X = -4127861
14
Y = -3523973
76 feet Y = -1074107
20 meter
Z = -17352517
13 Z = -5289047
22
XDOT = 8803
842191 XDOT = 2683
411100
YDOT = -22316
396116 feet/sec YDOT = -6802
037536 meter/sec
ZDOT = -2346
788554 ZDOT = -715
301151
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 14064
44878870
00016717 00000-0 10270-3 0 9053
2 25544 51
6461 253
8231 0003121 221
0985 138
9931 15
51118857 35232
Satellite: ISS
Catalog Number: 25544
Epoch time: 14064
44878870 = yrday
fracday
Element set: 905
Inclination: 51
6461 deg
RA of node: 253
8231 deg
Eccentricity:
0003121
Arg of perigee: 221
0985 deg
Mean anomaly: 138
9931 deg
Mean motion: 15
51118857 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3523
Checksum: 309
Coasting Arc #7 (Orbit 3538)
---------------------------------------
Vector Time (GMT): 2014/065/10:21:16
157
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3981119
56 A = 6786051
74 meter
Y = -1472320
90 meter E =
0002027
Z = 5294467
80 I = 51
29243
XDOT = 2785
415646 Wp = 174
70788
YDOT = 7139
326360 meter/sec RA = 248
02109 deg
ZDOT = -111
091753 TA = 276
34489
MA = 276
36798
Ha = 225
001 n
mi
Hp = 220
158
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13061415
89 X = 3971568
80
Y = -4830449
14 feet Y = -1427854
32 meter
Z = 17370301
19 Z = 5313784
38
XDOT = 9138
502776 XDOT = 2705
914722
YDOT = 23422
986746 feet/sec YDOT = 7170
030136 meter/sec
ZDOT = -364
474254 ZDOT = -97
754511
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12906757
05 X = 3933979
55
Y = 4950099
18 feet Y = 1508790
23 meter
Z = 17452029
34 Z = 5319378
54
XDOT = -8284
776038 XDOT = -2525
199736
YDOT = 22668
925856 feet/sec YDOT = 6909
488601 meter/sec
ZDOT = -309
226406 ZDOT = -94
252209
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 14065
47960946
00016717 00000-0 10270-3 0 9064
2 25544 51
6465 248
7079 0003130 225
3871 134
7026 15
51144140 35390
Satellite: ISS
Catalog Number: 25544
Epoch time: 14065
47960946 = yrday
fracday
Element set: 906
Inclination: 51
6465 deg
RA of node: 248
7079 deg
Eccentricity:
0003130
Arg of perigee: 225
3871 deg
Mean anomaly: 134
7026 deg
Mean motion: 15
51144140 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3539
Checksum: 308
Coasting Arc #8 (Orbit 3553)
---------------------------------------
Vector Time (GMT): 2014/066/10:21:16
157
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4225362
41 A = 6786111
27 meter
Y = 945023
84 meter E =
0012499
Z = -5236258
89 I = 51
30447
XDOT = -2754
797090 Wp = 107
79857
YDOT = -7079
104034 meter/sec RA = 243
02701 deg
ZDOT = 943
468946 TA = 171
29862
MA = 171
27693
Ha = 224
901 n
mi
Hp = 219
937
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13862737
58 X = -4210179
94
Y = 3100471
90 feet Y = 897857
54 meter
Z = -17179327
07 Z = -5256748
18
XDOT = -9038
048194 XDOT = -2680
015254
YDOT = -23225
406935 feet/sec YDOT = -7109
491724 meter/sec
ZDOT = 3095
370558 ZDOT = 930
268907
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12478482
61 X = -3803441
50
Y = -6564506
06 feet Y = -2000861
45 meter
Z = -17265932
63 Z = -5262656
27
XDOT = 7694
782923 XDOT = 2345
369835
YDOT = -22640
760270 feet/sec YDOT = -6900
903730 meter/sec
ZDOT = 3040
681830 ZDOT = 926
799822
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 14066
44596924
00016717 00000-0 10270-3 0 9074
2 25544 51
6451 243
9105 0003100 230
2166 129
8713 15
51223712 35549
Satellite: ISS
Catalog Number: 25544
Epoch time: 14066
44596924 = yrday
fracday
Element set: 907
Inclination: 51
6451 deg
RA of node: 243
9105 deg
Eccentricity:
0003100
Arg of perigee: 230
2166 deg
Mean anomaly: 129
8713 deg
Mean motion: 15
51223712 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3554
Checksum: 287
Coasting Arc #9 (Orbit 3569)
---------------------------------------
Vector Time (GMT): 2014/067/10:21:16
157
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4502945
05 A = 6786743
45 meter
Y = -432353
58 meter E =
0002160
Z = 5058092
78 I = 51
32210
XDOT = 2667
186847 Wp = 54
89137
YDOT = 6962
333400 meter/sec RA = 238
03598 deg
ZDOT = -1777
568760 TA = 52
40029
MA = 52
38068
Ha = 224
593 n
mi
Hp = 220
131
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14773441
77 X = 4482874
68
Y = -1418482
89 feet Y = -382110
55 meter
Z = 16594792
60 Z = 5079918
55
XDOT = 8750
613015 XDOT = 2597
769022
YDOT = 22842
301181 feet/sec YDOT = 6991
771302 meter/sec
ZDOT = -5831
918505 ZDOT = -1764
781266
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12226587
63 X = 3726663
91
Y = 8228569
04 feet Y = 2508067
84 meter
Z = 16686971
65 Z = 5086188
96
XDOT = -7132
216721 XDOT = -2173
899657
YDOT = 22328
485925 feet/sec YDOT = 6805
722510 meter/sec
ZDOT = -5778
941614 ZDOT = -1761
421404
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 14067
47671752
00016717 00000-0 10270-3 0 9082
2 25544 51
6453 238
7950 0003158 235
8993 124
1859 15
51258347 35702
Satellite: ISS
Catalog Number: 25544
Epoch time: 14067
47671752 = yrday
fracday
Element set: 908
Inclination: 51
6453 deg
RA of node: 238
7950 deg
Eccentricity:
0003158
Arg of perigee: 235
8993 deg
Mean anomaly: 124
1859 deg
Mean motion: 15
51258347 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3570
Checksum: 338
Coasting Arc #10 (Orbit 3584)
---------------------------------------
Vector Time (GMT): 2014/068/10:21:16
157
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4826562
29 A = 6787714
26 meter
Y = -53127
51 meter E =
0009691
Z = -4781555
74 I = 51
34206
XDOT = -2492
629113 Wp = 122
33862
YDOT = -6759
419510 meter/sec RA = 233
04468 deg
ZDOT = 2589
970735 TA = 173
34040
MA = 173
32752
Ha = 224
585 n
mi
Hp = 219
881
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15835178
10 X = -4802382
48
Y = -174302
86 feet Y = -106966
45 meter
Z = -15687518
84 Z = -4804943
50
XDOT = -8177
917036 XDOT = -2429
439613
YDOT = -22176
573197 feet/sec YDOT = -6786
940147 meter/sec
ZDOT = 8497
279314 ZDOT = 2578
016104
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12211076
29 X = -3721936
05
Y = -9928043
73 feet Y = -3026067
73 meter
Z = -15786230
01 Z = -4811642
91
XDOT = 6628
717054 XDOT = 2020
432958
YDOT = -21591
895071 feet/sec YDOT = -6581
209617 meter/sec
ZDOT = 8447
775376 ZDOT = 2574
881934
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 14068
44300934
00016717 00000-0 10270-3 0 9092
2 25544 51
6441 233
9971 0003065 239
0247 121
0604 15
51329129 35851
Satellite: ISS
Catalog Number: 25544
Epoch time: 14068
44300934 = yrday
fracday
Element set: 909
Inclination: 51
6441 deg
RA of node: 233
9971 deg
Eccentricity:
0003065
Arg of perigee: 239
0247 deg
Mean anomaly: 121
0604 deg
Mean motion: 15
51329129 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3585
Checksum: 297
Coasting Arc #11 (Orbit 3600)
---------------------------------------
Vector Time (GMT): 2014/069/10:21:16
157
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5160408
55 A = 6789123
82 meter
Y = 507376
36 meter E =
0006239
Z = 4378241
81 I = 51
36665
XDOT = 2227
010426 Wp = 72
99289
YDOT = 6512
704422 meter/sec RA = 228
05761 deg
ZDOT = -3373
807452 TA = 51
32928
MA = 51
27347
Ha = 224
256 n
mi
Hp = 220
031
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16930474
24 X = 5133083
61
Y = 1664620
62 feet Y = 564930
99 meter
Z = 14364310
39 Z = 4403243
59
XDOT = 7306
464651 XDOT = 2170
407042
YDOT = 21367
140493 feet/sec YDOT = 6537
291473 meter/sec
ZDOT = -11068
922086 ZDOT = -3363
127193
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12348770
53 X = 3763905
26
Y = 11570594
18 feet Y = 3526717
11 meter
Z = 14469780
57 Z = 4410389
12
XDOT = -6307
096280 XDOT = -1922
402946
YDOT = 20542
008446 feet/sec YDOT = 6261
204174 meter/sec
ZDOT = -11024
748878 ZDOT = -3360
343458
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 14069
47368284
00016717 00000-0 10270-3 0 9100
2 25544 51
6441 228
8808 0003135 245
4259 114
6566 15
51373221 36011
Satellite: ISS
Catalog Number: 25544
Epoch time: 14069
47368284 = yrday
fracday
Element set: 910
Inclination: 51
6441 deg
RA of node: 228
8808 deg
Eccentricity:
0003135
Arg of perigee: 245
4259 deg
Mean anomaly: 114
6566 deg
Mean motion: 15
51373221 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3601
Checksum: 305
Coasting Arc #12 (Orbit 3615)
---------------------------------------
Vector Time (GMT): 2014/070/10:21:16
157
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5503780
40 A = 6790691
27 meter
Y = -905836
92 meter E =
0004545
Z = -3878559
06 I = 51
39358
XDOT = -1858
450559 Wp = 130
22621
YDOT = -6204
168241 meter/sec RA = 223
07213 deg
ZDOT = 4086
476521 TA = 182
84015
MA = 182
84273
Ha = 224
283 n
mi
Hp = 219
798
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18057022
31 X = -5474401
55
Y = -2971905
92 feet Y = -967219
87 meter
Z = -12724931
29 Z = -3905223
80
XDOT = -6097
278737 XDOT = -1808
786534
YDOT = -20354
882680 feet/sec YDOT = -6224
672508 meter/sec
ZDOT = 13407
075200 ZDOT = 4077
569844
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12682199
11 X = -3865534
29
Y = -13083414
05 feet Y = -3987824
60 meter
Z = -12837377
40 Z = -3912832
63
XDOT = 6184
841909 XDOT = 1885
139814
YDOT = -19113
114377 feet/sec YDOT = -5825
677262 meter/sec
ZDOT = 13370
332860 ZDOT = 4075
277456
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 14070
43990420
00016717 00000-0 10270-3 0 9112
2 25544 51
6437 224
0827 0002990 247
8885 112
1948 15
51440103 36161
Satellite: ISS
Catalog Number: 25544
Epoch time: 14070
43990420 = yrday
fracday
Element set: 911
Inclination: 51
6437 deg
RA of node: 224
0827 deg
Eccentricity:
0002990
Arg of perigee: 247
8885 deg
Mean anomaly: 112
1948 deg
Mean motion: 15
51440103 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3616
Checksum: 297
Coasting Arc #13 (Orbit 3631)
---------------------------------------
Vector Time (GMT): 2014/071/10:21:16
157
Vector Time (MET): N/A
Weight (LBS) : 901736
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5820685
06 A = 6792421
56 meter
Y = 1263713
73 meter E =
0009758
Z = 3255013
26 I = 51
42302
XDOT = 1376
353408 Wp = 97
92975
YDOT = 5873
101101 meter/sec RA = 218
09136 deg
ZDOT = -4730
501450 TA = 44
23361
MA = 44
15565
Ha = 224
001 n
mi
Hp = 219
868
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19096735
75 X = 5790309
75
Y = 4146042
42 feet Y = 1328634
91 meter
Z = 10679177
36 Z = 3283214
97
XDOT = 4515
595172 XDOT = 1333
555694
YDOT = 19268
704398 feet/sec YDOT = 5888
252512 meter/sec
ZDOT = -15520
017880 ZDOT = -4723
920065
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13080048
50 X = 3986798
78
Y = 14430305
52 feet Y = 4398357
12 meter
Z = 10798075
16 Z = 3291253
31
XDOT = -6386
421812 XDOT = -1946
581368
YDOT = 17408
545707 feet/sec YDOT = 5306
124731 meter/sec
ZDOT = -15493
034996 ZDOT = -4722
277067
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 14071
47050079
00016717 00000-0 10270-3 0 9125
2 25544 51
6436 218
9655 0003073 254
7299 105
3513 15
51493202 36328
Satellite: ISS
Catalog Number: 25544
Epoch time: 14071
47050079 = yrday
fracday
Element set: 912
Inclination: 51
6436 deg
RA of node: 218
9655 deg
Eccentricity:
0003073
Arg of perigee: 254
7299 deg
Mean anomaly: 105
3513 deg
Mean motion: 15
51493202 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3632
Checksum: 297
Coasting Arc #14 (Orbit 3642)
---------------------------------------
Vector Time (GMT): 2014/072/04:01:38
080
Vector Time (MET): N/A
Weight (LBS) : 901568
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4729513
40 A = 6788292
89 meter
Y = 1301356
35 meter E =
0007052
Z = -4699372
63 I = 51
42912
XDOT = -4330
695441 Wp = 118
80993
YDOT = -5665
738968 meter/sec RA = 214
43194 deg
ZDOT = 2789
366078 TA = 178
96025
MA = 178
95879
Ha = 224
025 n
mi
Hp = 220
574
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15516776
26 X = -4720886
24
Y = 4269541
83 feet Y = 1248515
53 meter
Z = -15417889
19 Z = -4722326
81
XDOT = -14208
318375 XDOT = -4280
567656
YDOT = -18588
382442 feet/sec YDOT = -5713
886942 meter/sec
ZDOT = 9151
463512 ZDOT = 2768
450963
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6565585
03 X = 2001190
32
Y = -14590712
84 feet Y = -4447249
27 meter
Z = -15514987
34 Z = -4728968
14
XDOT = 22349
572150 XDOT = 6812
149591
YDOT = 418
362880 feet/sec YDOT = 127
517006 meter/sec
ZDOT = 9063
921878 ZDOT = 2762
683388
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 14072
17901392
00016717 00000-0 10270-3 0 9137
2 25544 51
6477 215
4515 0004103 272
9179 87
1502 15
51243118 36430
Satellite: ISS
Catalog Number: 25544
Epoch time: 14072
17901392 = yrday
fracday
Element set: 913
Inclination: 51
6477 deg
RA of node: 215
4515 deg
Eccentricity:
0004103
Arg of perigee: 272
9179 deg
Mean anomaly: 87
1502 deg
Mean motion: 15
51243118 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3643
Checksum: 291
Coasting Arc #15 (Orbit 3658)
---------------------------------------
Vector Time (GMT): 2014/073/04:01:38
080
Vector Time (MET): N/A
Weight (LBS) : 901568
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5164273
51 A = 6789630
58 meter
Y = -1007363
83 meter E =
0006314
Z = 4288951
46 I = 51
46040
XDOT = 4009
994737 Wp = 55
63555
YDOT = 5494
176361 meter/sec RA = 209
45206 deg
ZDOT = -3530
728480 TA = 70
48518
MA = 70
41700
Ha = 223
859 n
mi
Hp = 220
576
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16943154
55 X = 5154320
18
Y = -3304999
44 feet Y = -949668
65 meter
Z = 14071363
07 Z = 4314014
41
XDOT = 13156
150711 XDOT = 3965
410513
YDOT = 18025
512996 feet/sec YDOT = 5538
768904 meter/sec
ZDOT = -11583
754857 ZDOT = -3511
357825
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7963507
89 X = -2427277
20
Y = 15217836
77 feet Y = 4638396
65 meter
Z = 14177332
35 Z = 4321250
90
XDOT = -21227
933610 XDOT = -6470
274164
YDOT = -370
492360 feet/sec YDOT = -112
926071 meter/sec
ZDOT = -11502
697152 ZDOT = -3506
022092
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 14073
20974390
00016717 00000-0 10270-3 0 9141
2 25544 51
6477 210
3356 0004127 278
9016 81
1668 15
51314057 36594
Satellite: ISS
Catalog Number: 25544
Epoch time: 14073
20974390 = yrday
fracday
Element set: 914
Inclination: 51
6477 deg
RA of node: 210
3356 deg
Eccentricity:
0004127
Arg of perigee: 278
9016 deg
Mean anomaly: 81
1668 deg
Mean motion: 15
51314057 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3659
Checksum: 309
Coasting Arc #16 (Orbit 3673)
---------------------------------------
Vector Time (GMT): 2014/074/04:01:38
080
Vector Time (MET): N/A
Weight (LBS) : 901568
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5584789
68 A = 6791212
63 meter
Y = 769603
10 meter E =
0001898
Z = -3788622
24 I = 51
49442
XDOT = -3582
786855 Wp = 105
15684
YDOT = -5306
420415 meter/sec RA = 204
47504 deg
ZDOT = 4204
726083 TA = 209
38215
MA = 209
39282
Ha = 223
883 n
mi
Hp = 220
430
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18322800
78 X = -5574576
76
Y = 2524944
55 feet Y = 707206
91 meter
Z = -12429863
00 Z = -3815727
39
XDOT = -11754
550048 XDOT = -3543
607986
YDOT = -17409
515796 feet/sec YDOT = -5346
265721 meter/sec
ZDOT = 13795
033082 ZDOT = 4187
417579
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9167910
61 X = 2794379
15
Y = -15974621
16 feet Y = -4869064
53 meter
Z = -12544431
49 Z = -3823542
72
XDOT = 19849
280249 XDOT = 6050
060620
YDOT = 618
843035 feet/sec YDOT = 188
623357 meter/sec
ZDOT = 13722
646471 ZDOT = 4182
662644
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 14074
17601672
00016717 00000-0 10270-3 0 9159
2 25544 51
6485 205
5386 0004241 283
7561 76
3118 15
51360203 36745
Satellite: ISS
Catalog Number: 25544
Epoch time: 14074
17601672 = yrday
fracday
Element set: 915
Inclination: 51
6485 deg
RA of node: 205
5386 deg
Eccentricity:
0004241
Arg of perigee: 283
7561 deg
Mean anomaly: 76
3118 deg
Mean motion: 15
51360203 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3674
Checksum: 298
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