[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
September 23rd 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 13993 08 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 127 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 423 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 2642)
---------------------------------------
Vector Time (GMT): 2014/265/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912103
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2507374
52 A = 6787936
67 meter
Y = 3477148
71 meter E =
0004938
Z = 5259492
20 I = 51
48895
XDOT = -6717
725295 Wp = 119
14800
YDOT = 3601
418461 meter/sec RA = 336
70683 deg
ZDOT = 818
659194 TA = 322
99104
MA = 323
02509
Ha = 227
096 n
mi
Hp = 219
718
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8226294
34 X = 2442756
95
Y = 11407968
20 feet Y = 3504827
26 meter
Z = 17255551
82 Z = 5271515
21
XDOT = -22039
781151 XDOT = -6761
474695
YDOT = 11815
677367 feet/sec YDOT = 3526
052010 meter/sec
ZDOT = 2685
889744 ZDOT = 785
918643
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8205363
58 X = -2500994
82
Y = -11346363
85 feet Y = -3458371
70 meter
Z = 17306061
41 Z = 5274887
52
XDOT = 21136
899002 XDOT = 6442
526816
YDOT = -11387
651746 feet/sec YDOT = -3470
956252 meter/sec
ZDOT = 2545
995554 ZDOT = 776
019445
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 14265
54968726
00016717 00000-0 10270-3 0 9002
2 25544 51
6472 337
0187 0001753 121
7667 238
3655 15
50565642 26438
Satellite: ISS
Catalog Number: 25544
Epoch time: 14265
54968726 = yrday
fracday
Element set: 900
Inclination: 51
6472 deg
RA of node: 337
0187 deg
Eccentricity:
0001753
Arg of perigee: 121
7667 deg
Mean anomaly: 238
3655 deg
Mean motion: 15
50565642 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2643
Checksum: 324
Coasting Arc #2 (Orbit 2657)
---------------------------------------
Vector Time (GMT): 2014/266/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912103
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2226754
07 A = 6787838
30 meter
Y = -3609169
82 meter E =
0016331
Z = -5314182
47 I = 51
45888
XDOT = 6649
742590 Wp = 91
39092
YDOT = -3776
650980 meter/sec RA = 331
73366 deg
ZDOT = -222
420597 TA = 176
48470
MA = 176
47321
Ha = 227
218 n
mi
Hp = 219
666
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7305623
59 X = -2160415
31
Y = -11841108
34 feet Y = -3633700
71 meter
Z = -17434981
87 Z = -5324838
09
XDOT = 21816
740780 XDOT = 6692
560200
YDOT = -12390
587204 feet/sec YDOT = -3702
049879 meter/sec
ZDOT = -729
726369 ZDOT = -190
012399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7488623
19 X = 2282532
35
Y = 11659539
60 feet Y = 3553827
67 meter
Z = -17479652
01 Z = -5327797
93
XDOT = -20655
024455 XDOT = -6295
651454
YDOT = 12384
657139 feet/sec YDOT = 3774
843496 meter/sec
ZDOT = -591
227448 ZDOT = -180
206126
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 14266
51644593
00016717 00000-0 10270-3 0 9014
2 25544 51
6461 332
2258 0001734 120
3721 239
7601 15
50539581 26582
Satellite: ISS
Catalog Number: 25544
Epoch time: 14266
51644593 = yrday
fracday
Element set: 901
Inclination: 51
6461 deg
RA of node: 332
2258 deg
Eccentricity:
0001734
Arg of perigee: 120
3721 deg
Mean anomaly: 239
7601 deg
Mean motion: 15
50539581 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2658
Checksum: 300
Coasting Arc #3 (Orbit 2673)
---------------------------------------
Vector Time (GMT): 2014/267/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912103
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1954233
58 A = 6787674
60 meter
Y = 3766614
46 meter E =
0003960
Z = 5294305
45 I = 51
43219
XDOT = -6564
943098 Wp = 90
89918
YDOT = 3940
527140 meter/sec RA = 326
75805 deg
ZDOT = -380
036821 TA = 2
73707
MA = 2
73490
Ha = 227
022 n
mi
Hp = 219
675
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6411527
48 X = 1886250
95
Y = 12357659
00 feet Y = 3788088
66 meter
Z = 17369768
53 Z = 5303633
21
XDOT = -21538
527224 XDOT = -6606
672949
YDOT = 12928
238649 feet/sec YDOT = 3866
880313 meter/sec
ZDOT = -1246
839964 ZDOT = -412
030579
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6816957
31 X = -2077808
59
Y = -12082728
24 feet Y = -3682815
57 meter
Z = 17408763
62 Z = 5306191
15
XDOT = 20085
517166 XDOT = 6122
065632
YDOT = -13326
405783 feet/sec YDOT = -4061
888483 meter/sec
ZDOT = -1383
592937 ZDOT = -421
719127
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 14267
54763907
00016717 00000-0 10270-3 0 9020
2 25544 51
6464 327
1129 0001710 123
1133 237
0182 15
50606921 26743
Satellite: ISS
Catalog Number: 25544
Epoch time: 14267
54763907 = yrday
fracday
Element set: 902
Inclination: 51
6464 deg
RA of node: 327
1129 deg
Eccentricity:
0001710
Arg of perigee: 123
1133 deg
Mean anomaly: 237
0182 deg
Mean motion: 15
50606921 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2674
Checksum: 287
Coasting Arc #4 (Orbit 2688)
---------------------------------------
Vector Time (GMT): 2014/268/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912103
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1708227
39 A = 6788052
92 meter
Y = -3979260
71 meter E =
0015923
Z = -5241369
81 I = 51
40674
XDOT = 6414
968559 Wp = 99
92170
YDOT = -4051
226452 meter/sec RA = 321
78004 deg
ZDOT = 984
861313 TA = 179
55871
MA = 179
55731
Ha = 227
154 n
mi
Hp = 219
612
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5604420
56 X = -1638142
24
Y = -13055317
30 feet Y = -3997972
12 meter
Z = -17196095
18 Z = -5249497
41
XDOT = 21046
484775 XDOT = 6455
009340
YDOT = -13291
425366 feet/sec YDOT = -3979
266094 meter/sec
ZDOT = 3231
172286 ZDOT = 1016
122510
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6260579
39 X = 1908224
60
Y = 12707892
23 feet Y = 3873365
55 meter
Z = -17229949
21 Z = -5251688
52
XDOT = -19273
872713 XDOT = -5874
676403
YDOT = 14058
046363 feet/sec YDOT = 4284
892532 meter/sec
ZDOT = 3364
818421 ZDOT = 1025
596655
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 14268
51437224
00016717 00000-0 10270-3 0 9039
2 25544 51
6456 322
3191 0001741 120
4182 239
7141 15
50581731 26899
Satellite: ISS
Catalog Number: 25544
Epoch time: 14268
51437224 = yrday
fracday
Element set: 903
Inclination: 51
6456 deg
RA of node: 322
3191 deg
Eccentricity:
0001741
Arg of perigee: 120
4182 deg
Mean anomaly: 239
7141 deg
Mean motion: 15
50581731 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2689
Checksum: 292
Coasting Arc #5 (Orbit 2704)
---------------------------------------
Vector Time (GMT): 2014/269/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912103
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1477037
23 A = 6788376
80 meter
Y = 4212159
92 meter E =
0005883
Z = 5110155
56 I = 51
38442
XDOT = -6258
457850 Wp = 70
49541
YDOT = 4131
425157 meter/sec RA = 316
80082 deg
ZDOT = -1593
049097 TA = 34
94684
MA = 34
90825
Ha = 226
976 n
mi
Hp = 219
601
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4845922
67 X = 1405002
27
Y = 13819422
31 feet Y = 4228275
03 meter
Z = 16765602
23 Z = 5117155
35
XDOT = -20532
998195 XDOT = -6296
452628
YDOT = 13554
544478 feet/sec YDOT = 4061
226372 meter/sec
ZDOT = -5226
539033 ZDOT = -1623
545062
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5783109
13 X = -1762691
66
Y = -13417943
24 feet Y = -4089789
10 meter
Z = 16794620
14 Z = 5119000
22
XDOT = 18424
824222 XDOT = 5615
886423
YDOT = -14660
149467 feet/sec YDOT = -4468
413557 meter/sec
ZDOT = -5356
936023 ZDOT = -1632
794100
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 14269
54553802
00016717 00000-0 10270-3 0 9045
2 25544 51
6454 317
2059 0001731 123
1115 237
0202 15
50649237 27052
Satellite: ISS
Catalog Number: 25544
Epoch time: 14269
54553802 = yrday
fracday
Element set: 904
Inclination: 51
6454 deg
RA of node: 317
2059 deg
Eccentricity:
0001731
Arg of perigee: 123
1115 deg
Mean anomaly: 237
0202 deg
Mean motion: 15
50649237 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2705
Checksum: 281
Coasting Arc #6 (Orbit 2719)
---------------------------------------
Vector Time (GMT): 2014/270/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912103
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1291883
81 A = 6789195
91 meter
Y = -4483547
37 meter E =
0014020
Z = -4944804
91 I = 51
36494
XDOT = 6049
261524 Wp = 107
75285
YDOT = -4147
039415 meter/sec RA = 311
81951 deg
ZDOT = 2180
701216 TA = 183
64048
MA = 183
65069
Ha = 227
090 n
mi
Hp = 219
545
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4238463
95 X = -1217631
09
Y = -14709801
08 feet Y = -4497579
48 meter
Z = -16223113
24 Z = -4950899
90
XDOT = 19846
658543 XDOT = 6084
591769
YDOT = -13605
772358 feet/sec YDOT = -4079
194850 meter/sec
ZDOT = 7154
531550 ZDOT = 2210
174442
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5495018
04 X = 1674881
50
Y = 14259445
51 feet Y = 4346278
99 meter
Z = -16248237
38 Z = -4952462
75
XDOT = -17400
976835 XDOT = -5303
817739
YDOT = 14998
148534 feet/sec YDOT = 4571
435673 meter/sec
ZDOT = 7280
575404 ZDOT = 2219
119383
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 14270
51224540
00016717 00000-0 10270-3 0 9059
2 25544 51
6456 312
4115 0001782 120
9611 239
1715 15
50628919 27209
Satellite: ISS
Catalog Number: 25544
Epoch time: 14270
51224540 = yrday
fracday
Element set: 905
Inclination: 51
6456 deg
RA of node: 312
4115 deg
Eccentricity:
0001782
Arg of perigee: 120
9611 deg
Mean anomaly: 239
1715 deg
Mean motion: 15
50628919 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2720
Checksum: 282
Coasting Arc #7 (Orbit 2735)
---------------------------------------
Vector Time (GMT): 2014/271/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912103
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1125259
12 A = 6789977
11 meter
Y = 4765113
19 meter E =
0008968
Z = 4698115
95 I = 51
34740
XDOT = -5847
352423 Wp = 73
04119
YDOT = 4115
201070 meter/sec RA = 306
83790 deg
ZDOT = -2766
411933 TA = 44
51382
MA = 44
44181
Ha = 226
943 n
mi
Hp = 219
514
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3691795
03 X = 1049068
59
Y = 15633573
47 feet Y = 4777271
05 meter
Z = 15413766
25 Z = 4703396
83
XDOT = -19184
227108 XDOT = -5879
496406
YDOT = 13501
315846 feet/sec YDOT = 4049
632174 meter/sec
ZDOT = -9076
154636 ZDOT = -2794
896500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5303520
79 X = -1616513
14
Y = -15140799
85 feet Y = -4614915
79 meter
Z = 15435381
67 Z = 4704704
33
XDOT = 16410
302915 XDOT = 5001
860328
YDOT = -15148
382729 feet/sec YDOT = -4617
227056 meter/sec
ZDOT = -9197
984096 ZDOT = -2803
545552
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 14271
54338387
00016717 00000-0 10270-3 0 9069
2 25544 51
6450 307
2980 0001795 123
1905 236
9418 15
50691468 27361
Satellite: ISS
Catalog Number: 25544
Epoch time: 14271
54338387 = yrday
fracday
Element set: 906
Inclination: 51
6450 deg
RA of node: 307
2980 deg
Eccentricity:
0001795
Arg of perigee: 123
1905 deg
Mean anomaly: 236
9418 deg
Mean motion: 15
50691468 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2736
Checksum: 324
Coasting Arc #8 (Orbit 2750)
---------------------------------------
Vector Time (GMT): 2014/272/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912103
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1018086
63 A = 6791117
41 meter
Y = -5063604
66 meter E =
0010876
Z = -4420533
94 I = 51
33413
XDOT = 5612
279595 Wp = 112
36317
YDOT = -4015
115862 meter/sec RA = 301
85530 deg
ZDOT = 3309
153450 TA = 191
25166
MA = 191
27600
Ha = 227
015 n
mi
Hp = 219
477
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3340179
24 X = -939914
72
Y = -16612876
17 feet Y = -5074552
87 meter
Z = -14503064
09 Z = -4425289
40
XDOT = 18412
990798 XDOT = 5640
685388
YDOT = -13172
952302 feet/sec YDOT = -3952
196598 meter/sec
ZDOT = 10856
802656 ZDOT = 3336
486865
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5345277
36 X = 1629240
54
Y = 16062730
73 feet Y = 4895920
33 meter
Z = -14522396
89 Z = -4426426
57
XDOT = -15339
214913 XDOT = -4675
392705
YDOT = 15018
495965 feet/sec YDOT = 4577
637570 meter/sec
ZDOT = 10973
716583 ZDOT = 3344
788814
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 14272
51006506
00016717 00000-0 10270-3 0 9073
2 25544 51
6460 302
5036 0001831 123
0098 237
1229 15
50680084 27517
Satellite: ISS
Catalog Number: 25544
Epoch time: 14272
51006506 = yrday
fracday
Element set: 907
Inclination: 51
6460 deg
RA of node: 302
5036 deg
Eccentricity:
0001831
Arg of perigee: 123
0098 deg
Mean anomaly: 237
1229 deg
Mean motion: 15
50680084 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2751
Checksum: 274
Coasting Arc #9 (Orbit 2766)
---------------------------------------
Vector Time (GMT): 2014/273/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912103
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 928606
75 A = 6792231
85 meter
Y = 5358221
13 meter E =
0011983
Z = 4060155
54 I = 51
32153
XDOT = -5400
664374 Wp = 83
87653
YDOT = 3854
959678 meter/sec RA = 296
87265 deg
ZDOT = -3841
169965 TA = 46
09631
MA = 45
99743
Ha = 226
892 n
mi
Hp = 219
444
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3046610
07 X = 848897
70
Y = 17579465
65 feet Y = 5368160
05 meter
Z = 13320720
29 Z = 4064472
61
XDOT = -17718
715138 XDOT = -5424
710638
YDOT = 12647
505506 feet/sec YDOT = 3794
431202 meter/sec
ZDOT = -12602
263665 ZDOT = -3867
464655
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5477666
31 X = -1669592
69
Y = -16966146
96 feet Y = -5171281
59 meter
Z = 13338143
19 Z = 4065466
04
XDOT = 14384
150087 XDOT = 4384
288946
YDOT = -14668
363732 feet/sec YDOT = -4470
917265 meter/sec
ZDOT = -12714
730577 ZDOT = -3875
449880
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 14273
54117608
00016717 00000-0 10270-3 0 9084
2 25544 51
6448 297
3896 0001838 124
9298 235
2026 15
50732470 27675
Satellite: ISS
Catalog Number: 25544
Epoch time: 14273
54117608 = yrday
fracday
Element set: 908
Inclination: 51
6448 deg
RA of node: 297
3896 deg
Eccentricity:
0001838
Arg of perigee: 124
9298 deg
Mean anomaly: 235
2026 deg
Mean motion: 15
50732470 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2767
Checksum: 333
Coasting Arc #10 (Orbit 2781)
---------------------------------------
Vector Time (GMT): 2014/274/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912103
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -903902
99 A = 6793501
12 meter
Y = -5646114
41 meter E =
0007309
Z = -3676225
43 I = 51
31356
XDOT = 5179
327850 Wp = 106
47141
YDOT = -3632
381839 meter/sec RA = 291
89039 deg
ZDOT = 4310
420162 TA = 209
67535
MA = 209
71684
Ha = 226
921 n
mi
Hp = 219
420
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2965561
00 X = -822841
58
Y = -18523997
42 feet Y = -5655769
48 meter
Z = -12061107
05 Z = -3680419
18
XDOT = 16992
545441 XDOT = 5198
622226
YDOT = -11917
263250 feet/sec YDOT = -3574
355036 meter/sec
ZDOT = 14141
798431 ZDOT = 4335
627959
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5849383
63 X = 1782892
13
Y = 17813221
09 feet Y = 5429469
79 meter
Z = -12077963
47 Z = -3681363
26
XDOT = -13452
922379 XDOT = -4100
450741
YDOT = 14067
903056 feet/sec YDOT = 4287
896852 meter/sec
ZDOT = 14249
603019 ZDOT = 4343
279000
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 14274
50783063
00016717 00000-0 10270-3 0 9096
2 25544 51
6459 292
5957 0001865 126
8623 233
2699 15
50733072 27825
Satellite: ISS
Catalog Number: 25544
Epoch time: 14274
50783063 = yrday
fracday
Element set: 909
Inclination: 51
6459 deg
RA of node: 292
5957 deg
Eccentricity:
0001865
Arg of perigee: 126
8623 deg
Mean anomaly: 233
2699 deg
Mean motion: 15
50733072 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2782
Checksum: 335
Coasting Arc #11 (Orbit 2797)
---------------------------------------
Vector Time (GMT): 2014/275/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912103
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 890253
07 A = 6794734
55 meter
Y = 5913906
77 meter E =
0014296
Z = 3210699
87 I = 51
30577
XDOT = -4998
099622 Wp = 97
44723
YDOT = 3343
495016 meter/sec RA = 286
90778 deg
ZDOT = -4756
209585 TA = 45
24960
MA = 45
13335
Ha = 226
805 n
mi
Hp = 219
411
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2920777
80 X = 808459
60
Y = 19402581
26 feet Y = 5923405
08 meter
Z = 10533792
24 Z = 3214825
46
XDOT = -16397
964639 XDOT = -5012
011623
YDOT = 10969
471837 feet/sec YDOT = 3287
524854 meter/sec
ZDOT = -15604
362154 ZDOT = -4780
523840
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6277386
17 X = -1913347
30
Y = -18580554
07 feet Y = -5663352
88 meter
Z = 10550322
97 Z = 3215738
44
XDOT = 12720
872182 XDOT = 3877
321841
YDOT = -13247
708917 feet/sec YDOT = -4037
901678 meter/sec
ZDOT = -15708
314961 ZDOT = -4787
894400
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 14275
53891359
00016717 00000-0 10270-3 0 9100
2 25544 51
6444 287
4814 0001810 128
6500 231
4813 15
50772482 27981
Satellite: ISS
Catalog Number: 25544
Epoch time: 14275
53891359 = yrday
fracday
Element set: 910
Inclination: 51
6444 deg
RA of node: 287
4814 deg
Eccentricity:
0001810
Arg of perigee: 128
6500 deg
Mean anomaly: 231
4813 deg
Mean motion: 15
50772482 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2798
Checksum: 315
Coasting Arc #12 (Orbit 2812)
---------------------------------------
Vector Time (GMT): 2014/276/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912103
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -937869
47 A = 6795891
21 meter
Y = -6152456
23 meter E =
0005620
Z = -2732594
71 I = 51
30194
XDOT = 4830
533714 Wp = 76
11263
YDOT = -3007
574366 meter/sec RA = 281
92648 deg
ZDOT = 5123
890633 TA = 252
88168
MA = 252
94323
Ha = 226
808 n
mi
Hp = 219
376
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3076999
56 X = -855727
46
Y = -20185223
85 feet Y = -6162485
07 meter
Z = -8965205
76 Z = -2736950
65
XDOT = 15848
207724 XDOT = 4838
915795
YDOT = -9867
369967 feet/sec YDOT = -2953
508847 meter/sec
ZDOT = 16810
664808 ZDOT = 5147
377408
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6912078
43 X = 2106801
51
Y = 19204702
48 feet Y = 5853593
32 meter
Z = -8982687
60 Z = -2737923
18
XDOT = -12106
628105 XDOT = -3690
100246
YDOT = 12251
562552 feet/sec YDOT = 3734
276266 meter/sec
ZDOT = 16911
038541 ZDOT = 5154
484547
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 14276
50554093
00016717 00000-0 10270-3 0 9110
2 25544 51
6447 282
6876 0001880 132
1042 228
0269 15
50787388 28133
Satellite: ISS
Catalog Number: 25544
Epoch time: 14276
50554093 = yrday
fracday
Element set: 911
Inclination: 51
6447 deg
RA of node: 282
6876 deg
Eccentricity:
0001880
Arg of perigee: 132
1042 deg
Mean anomaly: 228
0269 deg
Mean motion: 15
50787388 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2813
Checksum: 317
Coasting Arc #13 (Orbit 2828)
---------------------------------------
Vector Time (GMT): 2014/277/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912103
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 983589
71 A = 6796975
87 meter
Y = 6355022
01 meter E =
0015449
Z = 2177693
15 I = 51
29880
XDOT = -4717
659695 Wp = 111
76006
YDOT = 2607
100244 meter/sec RA = 276
94441 deg
ZDOT = -5451
717307 TA = 43
97252
MA = 43
84971
Ha = 226
690 n
mi
Hp = 219
405
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3227000
36 X = 901874
71
Y = 20849809
76 feet Y = 6365564
51 meter
Z = 7144662
57 Z = 2182272
08
XDOT = -15477
886137 XDOT = -4719
979496
YDOT = 8553
478490 feet/sec YDOT = 2554
330712 meter/sec
ZDOT = -17886
211638 ZDOT = -5474
641033
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7540386
98 X = -2298309
95
Y = -19697899
97 feet Y = -6003919
91 meter
Z = 7163072
12 Z = 2183304
38
XDOT = 11760
019927 XDOT = 3584
454074
YDOT = -11072
091879 feet/sec YDOT = -3374
773605 meter/sec
ZDOT = -17984
120014 ZDOT = -5481
559780
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 14277
53659484
00016717 00000-0 10270-3 0 9125
2 25544 51
6433 277
5726 0001723 133
5545 226
5750 15
50812452 28290
Satellite: ISS
Catalog Number: 25544
Epoch time: 14277
53659484 = yrday
fracday
Element set: 912
Inclination: 51
6433 deg
RA of node: 277
5726 deg
Eccentricity:
0001723
Arg of perigee: 133
5545 deg
Mean anomaly: 226
5750 deg
Mean motion: 15
50812452 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2829
Checksum: 319
Coasting Arc #14 (Orbit 2843)
---------------------------------------
Vector Time (GMT): 2014/278/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912103
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1078879
02 A = 6797765
89 meter
Y = -6510165
19 meter E =
0007759
Z = -1624271
87 I = 51
29859
XDOT = 4637
701340 Wp = 51
68942
YDOT = -2182
835455 meter/sec RA = 271
96395 deg
ZDOT = 5691
736533 TA = 290
47682
MA = 290
56010
Ha = 226
675 n
mi
Hp = 219
345
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3539629
33 X = -998110
43
Y = -21358809
67 feet Y = -6521778
53 meter
Z = -5328975
96 Z = -1629315
88
XDOT = 15215
555576 XDOT = 4634
116865
YDOT = -7161
533646 feet/sec YDOT = -2130
992952 meter/sec
ZDOT = 18673
676291 ZDOT = 5714
257521
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8310207
70 X = 2532951
31
Y = 19986260
38 feet Y = 6091812
16 meter
Z = -5349350
91 Z = -1630482
16
XDOT = -11596
144269 XDOT = -3534
504773
YDOT = 9825
021514 feet/sec YDOT = 2994
666557 meter/sec
ZDOT = 18769
797897 ZDOT = 5721
034399
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 14278
50319417
00016717 00000-0 10270-3 0 9133
2 25544 51
6430 272
7785 0001882 138
4720 221
6574 15
50843949 28446
Satellite: ISS
Catalog Number: 25544
Epoch time: 14278
50319417 = yrday
fracday
Element set: 913
Inclination: 51
6430 deg
RA of node: 272
7785 deg
Eccentricity:
0001882
Arg of perigee: 138
4720 deg
Mean anomaly: 221
6574 deg
Mean motion: 15
50843949 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2844
Checksum: 323
Coasting Arc #15 (Orbit 2859)
---------------------------------------
Vector Time (GMT): 2014/279/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 912103
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1153652
73 A = 6798442
37 meter
Y = 6616640
29 meter E =
0015106
Z = 1003254
45 I = 51
30013
XDOT = -4621
875982 Wp = 125
66121
YDOT = 1704
523870 meter/sec RA = 266
98257 deg
ZDOT = -5873
069629 TA = 43
42702
MA = 43
30812
Ha = 226
570 n
mi
Hp = 219
408
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3784949
91 X = 1074704
66
Y = 21708137
44 feet Y = 6629099
91 meter
Z = 3291517
22 Z = 1008666
06
XDOT = -15163
635113 XDOT = -4612
063124
YDOT = 5592
269916 feet/sec YDOT = 1652
893073 meter/sec
ZDOT = -19268
601144 ZDOT = -5895
498648
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8988883
80 X = -2739811
78
Y = -20115272
28 feet Y = -6131134
99 meter
Z = 3313450
10 Z = 1009939
59
XDOT = 11737
482099 XDOT = 3577
584544
YDOT = -8463
746795 feet/sec YDOT = -2579
750023 meter/sec
ZDOT = -19364
250128 ZDOT = -5902
223439
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 14279
53421800
00016717 00000-0 10270-3 0 9148
2 25544 51
6424 267
6627 0001624 139
2126 220
9147 15
50852144 28603
Satellite: ISS
Catalog Number: 25544
Epoch time: 14279
53421800 = yrday
fracday
Element set: 914
Inclination: 51
6424 deg
RA of node: 267
6627 deg
Eccentricity:
0001624
Arg of perigee: 139
2126 deg
Mean anomaly: 220
9147 deg
Mean motion: 15
50852144 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2860
Checksum: 295
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