[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
February 11th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 25833 39 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 849)
---------------------------------------
Vector Time (GMT): 2015/042/14:55:03
523
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5573825
64 A = 6785298
86 meter
Y = 2942098
27 meter E =
0012776
Z = 2506759
87 I = 51
60256
XDOT = -4263
957854 Wp = 78
06768
YDOT = -3544
528079 meter/sec RA = 350
54644 deg
ZDOT = -5295
451500 TA = 73
79667
MA = 73
65612
Ha = 221
140 n
mi
Hp = 213
849
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18286829
51 X = -5618487
40
Y = 9652553
36 feet Y = 2879518
55 meter
Z = 8224277
78 Z = 2479574
90
XDOT = -13989
363037 XDOT = -4198
282116
YDOT = -11629
029132 feet/sec YDOT = -3591
843547 meter/sec
ZDOT = -17373
528543 ZDOT = -5316
005049
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17566177
64 X = -5354170
95
Y = 10996277
38 feet Y = 3351665
35 meter
Z = 8107401
05 Z = 2471135
84
XDOT = -13907
234057 XDOT = -4238
924941
YDOT = -9280
321474 feet/sec YDOT = -2828
641985 meter/sec
ZDOT = -17460
762832 ZDOT = -5322
040511
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 15042
65869246
00016717 00000-0 10270-3 0 9005
2 25544 51
6467 350
9323 0006155 353
2581 6
8488 15
54624958 8506
Satellite: ISS
Catalog Number: 25544
Epoch time: 15042
65869246 = yrday
fracday
Element set: 900
Inclination: 51
6467 deg
RA of node: 350
9323 deg
Eccentricity:
0006155
Arg of perigee: 353
2581 deg
Mean anomaly: 6
8488 deg
Mean motion: 15
54624958 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 850
Checksum: 325
Coasting Arc #2 (Orbit 864)
---------------------------------------
Vector Time (GMT): 2015/043/14:55:03
523
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6359956
11 A = 6787495
78 meter
Y = -2230127
15 meter E =
0015652
Z = -724346
67 I = 51
58012
XDOT = 2185
127365 Wp = 23
68746
YDOT = 4316
009955 meter/sec RA = 345
56683 deg
ZDOT = 5956
508747 TA = 328
47339
MA = 328
56709
Ha = 221
132 n
mi
Hp = 213
570
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20865997
72 X = 6387939
80
Y = -7316690
13 feet Y = -2158849
55 meter
Z = -2376465
47 Z = -693383
48
XDOT = 7169
053034 XDOT = 2107
768125
YDOT = 14160
137648 feet/sec YDOT = 4340
013228 meter/sec
ZDOT = 19542
351533 ZDOT = 5966
935453
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20120343
38 X = 6132680
66
Y = -9203780
66 feet Y = -2805312
35 meter
Z = -2243570
26 Z = -683840
21
XDOT = 7644
896300 XDOT = 2330
164392
YDOT = 11987
763314 feet/sec YDOT = 3653
870258 meter/sec
ZDOT = 19586
109669 ZDOT = 5969
846227
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 15043
62288985
00016717 00000-0 10270-3 0 9019
2 25544 51
6472 346
1217 0006227 355
8933 4
2167 15
54691721 8654
Satellite: ISS
Catalog Number: 25544
Epoch time: 15043
62288985 = yrday
fracday
Element set: 901
Inclination: 51
6472 deg
RA of node: 346
1217 deg
Eccentricity:
0006227
Arg of perigee: 355
8933 deg
Mean anomaly: 4
2167 deg
Mean motion: 15
54691721 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 865
Checksum: 317
Coasting Arc #3 (Orbit 880)
---------------------------------------
Vector Time (GMT): 2015/044/14:55:03
523
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6552736
75 A = 6786978
85 meter
Y = 1299911
63 meter E =
0005548
Z = -1198613
97 I = 51
54855
XDOT = 82
803370 Wp = 101
06941
YDOT = -4952
378546 meter/sec RA = 340
58869 deg
ZDOT = -5847
657318 TA = 91
96322
MA = 91
89968
Ha = 221
102 n
mi
Hp = 213
437
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21498480
17 X = -6560963
31
Y = 4264801
94 feet Y = 1226588
62 meter
Z = -3932460
52 Z = -1230465
53
XDOT = 271
664599 XDOT = 166
581258
YDOT = -16247
961109 feet/sec YDOT = -4950
984382 meter/sec
ZDOT = -19185
227420 ZDOT = -5847
051402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20880621
52 X = -6364413
44
Y = 6578796
35 feet Y = 2005217
13 meter
Z = -4068969
68 Z = -1240221
96
XDOT = -899
991294 XDOT = -274
317346
YDOT = -14673
133515 feet/sec YDOT = -4472
371095 meter/sec
ZDOT = -19181
665896 ZDOT = -5846
571765
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 15044
65133574
00016717 00000-0 10270-3 0 9027
2 25544 51
6474 340
9903 0006052 358
9278 1
1861 15
54710654 8814
Satellite: ISS
Catalog Number: 25544
Epoch time: 15044
65133574 = yrday
fracday
Element set: 902
Inclination: 51
6474 deg
RA of node: 340
9903 deg
Eccentricity:
0006052
Arg of perigee: 358
9278 deg
Mean anomaly: 1
1861 deg
Mean motion: 15
54710654 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 881
Checksum: 305
Coasting Arc #4 (Orbit 896)
---------------------------------------
Vector Time (GMT): 2015/045/14:55:03
523
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6095934
97 A = 6783668
70 meter
Y = -190684
76 meter E =
0015548
Z = 2948247
91 I = 51
50862
XDOT = -2251
486754 Wp = 59
18937
YDOT = 5379
613221 meter/sec RA = 335
60189 deg
ZDOT = 4991
468981 TA = 334
59368
MA = 334
67004
Ha = 221
073 n
mi
Hp = 213
147
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19999786
65 X = 6083292
93
Y = -625606
18 feet Y = -122586
64 meter
Z = 9672729
36 Z = 2977829
61
XDOT = -7386
767566 XDOT = -2335
721830
YDOT = 17649
649674 feet/sec YDOT = 5353
964807 meter/sec
ZDOT = 16376
210569 ZDOT = 4980
327096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19700340
81 X = 6004663
88
Y = -3132834
12 feet Y = -954887
84 meter
Z = 9799309
41 Z = 2986829
51
XDOT = -5434
263954 XDOT = -1656
363653
YDOT = 17017
886401 feet/sec YDOT = 5187
051775 meter/sec
ZDOT = 16327
498990 ZDOT = 4976
621692
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 15045
67974791
00016717 00000-0 10270-3 0 9035
2 25544 51
6474 335
8584 0006251 3
4257 356
6938 15
54772816 8970
Satellite: ISS
Catalog Number: 25544
Epoch time: 15045
67974791 = yrday
fracday
Element set: 903
Inclination: 51
6474 deg
RA of node: 335
8584 deg
Eccentricity:
0006251
Arg of perigee: 3
4257 deg
Mean anomaly: 356
6938 deg
Mean motion: 15
54772816 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 897
Checksum: 349
Coasting Arc #5 (Orbit 911)
---------------------------------------
Vector Time (GMT): 2015/046/14:55:03
523
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5099223
49 A = 6779159
36 meter
Y = -1097358
80 meter E =
0012775
Z = -4343470
67 I = 51
46586
XDOT = 4112
668598 Wp = 43
10764
YDOT = -5465
731009 meter/sec RA = 330
60120 deg
ZDOT = -3444
243609 TA = 191
78243
MA = 191
81235
Ha = 221
090 n
mi
Hp = 212
879
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16729735
85 X = -5065475
04
Y = -3600258
52 feet Y = -1154193
09 meter
Z = -14250231
86 Z = -4368159
22
XDOT = 13493
007211 XDOT = 4190
212549
YDOT = -17932
188351 feet/sec YDOT = -5419
307017 meter/sec
ZDOT = -11300
011842 ZDOT = -3424
076920
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16983228
38 X = -5176488
01
Y = -1183591
91 feet Y = -360758
81 meter
Z = -14355629
39 Z = -4375595
84
XDOT = 10772
386692 XDOT = 3283
423464
YDOT = -18451
137533 feet/sec YDOT = -5623
906720 meter/sec
ZDOT = -11212
684440 ZDOT = -3417
626217
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 15046
64385248
00016717 00000-0 10270-3 0 9047
2 25544 51
6474 331
0475 0006179 4
8030 355
3181 15
54839714 9125
Satellite: ISS
Catalog Number: 25544
Epoch time: 15046
64385248 = yrday
fracday
Element set: 904
Inclination: 51
6474 deg
RA of node: 331
0475 deg
Eccentricity:
0006179
Arg of perigee: 4
8030 deg
Mean anomaly: 355
3181 deg
Mean motion: 15
54839714 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 912
Checksum: 306
Coasting Arc #6 (Orbit 927)
---------------------------------------
Vector Time (GMT): 2015/047/14:55:03
523
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3652326
28 A = 6775789
78 meter
Y = 2467824
53 meter E =
0005820
Z = 5141266
07 I = 51
42812
XDOT = -5500
239296 Wp = 52
85490
YDOT = 5155
392435 meter/sec RA = 325
58548 deg
ZDOT = 1435
061136 TA = 23
31969
MA = 23
29330
Ha = 221
023 n
mi
Hp = 212
780
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11982697
78 X = 3599485
27
Y = 8096537
18 feet Y = 2508372
02 meter
Z = 16867670
82 Z = 5158879
48
XDOT = -18045
404516 XDOT = -5564
450151
YDOT = 16914
017175 feet/sec YDOT = 5093
526220 meter/sec
ZDOT = 4708
205827 ZDOT = 1408
186458
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13018841
45 X = 3968142
87
Y = 6092402
48 feet Y = 1856964
28 meter
Z = 16942540
50 Z = 5164086
34
XDOT = -14689
596451 XDOT = -4477
388998
YDOT = 18640
578507 feet/sec YDOT = 5681
648329 meter/sec
ZDOT = 4592
252666 ZDOT = 1399
718613
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 15047
67220028
00016717 00000-0 10270-3 0 9056
2 25544 51
6476 325
9155 0006129 9
6627 350
4643 15
54883450 9286
Satellite: ISS
Catalog Number: 25544
Epoch time: 15047
67220028 = yrday
fracday
Element set: 905
Inclination: 51
6476 deg
RA of node: 325
9155 deg
Eccentricity:
0006129
Arg of perigee: 9
6627 deg
Mean anomaly: 350
4643 deg
Mean motion: 15
54883450 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 928
Checksum: 316
Coasting Arc #7 (Orbit 942)
---------------------------------------
Vector Time (GMT): 2015/048/14:55:03
523
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1984414
63 A = 6775179
94 meter
Y = -3802373
08 meter E =
0016289
Z = -5257788
42 I = 51
40032
XDOT = 6261
016536 Wp = 73
98980
YDOT = -4340
972264 meter/sec RA = 320
56092 deg
ZDOT = 782
711237 TA = 203
48688
MA = 203
56136
Ha = 221
038 n
mi
Hp = 212
520
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6510546
69 X = -1916208
40
Y = -12474977
30 feet Y = -3824183
10 meter
Z = -17249962
02 Z = -5267262
15
XDOT = 20541
392835 XDOT = 6305
290961
YDOT = -14242
034987 feet/sec YDOT = -4270
709890 meter/sec
ZDOT = 2567
950254 ZDOT = 813
233099
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8508932
01 X = -2593522
48
Y = -11146104
70 feet Y = -3397332
71 meter
Z = -17289762
66 Z = -5269919
66
XDOT = 16866
177497 XDOT = 5140
810901
YDOT = -17030
200025 feet/sec YDOT = -5190
804968 meter/sec
ZDOT = 2699
337995 ZDOT = 822
758221
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 15048
63624497
00016717 00000-0 10270-3 0 9062
2 25544 51
6469 321
1036 0006124 11
6884 348
4410 15
54952039 9433
Satellite: ISS
Catalog Number: 25544
Epoch time: 15048
63624497 = yrday
fracday
Element set: 906
Inclination: 51
6469 deg
RA of node: 321
1036 deg
Eccentricity:
0006124
Arg of perigee: 11
6884 deg
Mean anomaly: 348
4410 deg
Mean motion: 15
54952039 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 943
Checksum: 309
Coasting Arc #8 (Orbit 958)
---------------------------------------
Vector Time (GMT): 2015/049/14:55:03
523
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 218295
74 A = 6777665
77 meter
Y = 4953353
26 meter E =
0013083
Z = 4617758
72 I = 51
38560
XDOT = -6415
362563 Wp = 43
51235
YDOT = 3022
758104 meter/sec RA = 315
53841 deg
ZDOT = -2924
892511 TA = 75
76711
MA = 75
62182
Ha = 220
998 n
mi
Hp = 212
403
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 716193
37 X = 140459
17
Y = 16251158
98 feet Y = 4955359
61 meter
Z = 15150127
03 Z = 4618629
61
XDOT = -21047
777439 XDOT = -6434
479285
YDOT = 9917
185381 feet/sec YDOT = 2950
910173 meter/sec
ZDOT = -9596
104040 ZDOT = -2956
103020
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3760603
35 X = 1146231
90
Y = 15823601
24 feet Y = 4823033
66 meter
Z = 15152919
07 Z = 4618609
73
XDOT = -17510
858596 XDOT = -5337
309700
YDOT = 13524
181419 feet/sec YDOT = 4122
170497 meter/sec
ZDOT = -9730
176554 ZDOT = -2965
757814
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 15049
66452691
00016717 00000-0 10270-3 0 9072
2 25544 51
6470 315
9716 0006110 14
0929 346
0394 15
55023900 9592
Satellite: ISS
Catalog Number: 25544
Epoch time: 15049
66452691 = yrday
fracday
Element set: 907
Inclination: 51
6470 deg
RA of node: 315
9716 deg
Eccentricity:
0006110
Arg of perigee: 14
0929 deg
Mean anomaly: 346
0394 deg
Mean motion: 15
55023900 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 959
Checksum: 308
Coasting Arc #9 (Orbit 973)
---------------------------------------
Vector Time (GMT): 2015/050/14:55:03
523
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1381550
93 A = 6781961
77 meter
Y = -5733206
79 meter E =
0008891
Z = -3348338
85 I = 51
37667
XDOT = 5966
103504 Wp = 47
14655
YDOT = -1267
323778 meter/sec RA = 310
52503 deg
ZDOT = 4645
417940 TA = 273
65746
MA = 273
75913
Ha = 221
029 n
mi
Hp = 212
298
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4532647
40 X = 1461822
93
Y = -18809733
56 feet Y = -5717308
95 meter
Z = -10985363
67 Z = -3341432
06
XDOT = 19573
830395 XDOT = 5957
266417
YDOT = -4157
886410 feet/sec YDOT = -1200
655787 meter/sec
ZDOT = 15240
872507 ZDOT = 4674
378134
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 533497
16 X = 162609
93
Y = -19358149
63 feet Y = -5900364
01 meter
Z = -10954752
74 Z = -3339008
63
XDOT = 16751
389754 XDOT = 5105
823597
YDOT = -8207
717870 feet/sec YDOT = -2501
712407 meter/sec
ZDOT = 15364
981184 ZDOT = 4683
246265
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 15050
62851325
00016717 00000-0 10270-3 0 9088
2 25544 51
6455 311
1593 0006020 17
6129 342
5232 15
55033936 9746
Satellite: ISS
Catalog Number: 25544
Epoch time: 15050
62851325 = yrday
fracday
Element set: 908
Inclination: 51
6455 deg
RA of node: 311
1593 deg
Eccentricity:
0006020
Arg of perigee: 17
6129 deg
Mean anomaly: 342
5232 deg
Mean motion: 15
55033936 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 974
Checksum: 288
Coasting Arc #10 (Orbit 989)
---------------------------------------
Vector Time (GMT): 2015/051/14:55:03
523
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2762729
69 A = 6785514
80 meter
Y = 5997596
08 meter E =
0014531
Z = 1547124
18 I = 51
36914
XDOT = -5031
740512 Wp = 92
95670
YDOT = -828
710814 meter/sec RA = 305
52453 deg
ZDOT = -5726
792748 TA = 70
06468
MA = 69
90820
Ha = 221
029 n
mi
Hp = 212
064
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9064073
78 X = -2837106
10
Y = 19677152
50 feet Y = 5966285
77 meter
Z = 5075866
73 Z = 1533522
20
XDOT = -16508
335013 XDOT = -4994
281598
YDOT = -2718
867501 feet/sec YDOT = -884
770311 meter/sec
ZDOT = -18788
690117 ZDOT = -5751
144424
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4379103
84 X = -1334750
85
Y = 21231333
80 feet Y = 6471310
54 meter
Z = 5016582
67 Z = 1529054
40
XDOT = -15029
800216 XDOT = -4581
083106
YDOT = 1400
006673 feet/sec YDOT = 426
722034 meter/sec
ZDOT = -18892
692918 ZDOT = -5758
492802
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 15051
65673221
00016717 00000-0 10270-3 0 9090
2 25544 51
6453 306
0266 0006090 21
4276 338
7132 15
55100318 9900
Satellite: ISS
Catalog Number: 25544
Epoch time: 15051
65673221 = yrday
fracday
Element set: 909
Inclination: 51
6453 deg
RA of node: 306
0266 deg
Eccentricity:
0006090
Arg of perigee: 21
4276 deg
Mean anomaly: 338
7132 deg
Mean motion: 15
55100318 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 990
Checksum: 284
Coasting Arc #11 (Orbit 1005)
---------------------------------------
Vector Time (GMT): 2015/052/14:55:03
523
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3739839
38 A = 6786338
27 meter
Y = -5632889
53 meter E =
0018472
Z = 450282
30 I = 51
35296
XDOT = 3777
471184 Wp = 41
93976
YDOT = 2995
635851 meter/sec RA = 300
52873 deg
ZDOT = 5972
117512 TA = 322
94095
MA = 323
06837
Ha = 220
971 n
mi
Hp = 211
923
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12269814
24 X = 3800362
46
Y = -18480608
69 feet Y = -5590729
74 meter
Z = 1477304
14 Z = 468597
19
XDOT = 12393
278162 XDOT = 3714
682619
YDOT = 9828
201611 feet/sec YDOT = 3037
527696 meter/sec
ZDOT = 19593
561391 ZDOT = 5990
314584
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7373976
76 X = 2247588
12
Y = -20915662
13 feet Y = -6375093
82 meter
Z = 1556666
67 Z = 474472
00
XDOT = 12773
353616 XDOT = 3893
318182
YDOT = 5997
115149 feet/sec YDOT = 1827
920697 meter/sec
ZDOT = 19670
841722 ZDOT = 5995
672557
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 15052
68491879
00016717 00000-0 10270-3 0 9103
2 25544 51
6437 300
8922 0005943 24
9075 335
2364 15
55127535 10062
Satellite: ISS
Catalog Number: 25544
Epoch time: 15052
68491879 = yrday
fracday
Element set: 910
Inclination: 51
6437 deg
RA of node: 300
8922 deg
Eccentricity:
0005943
Arg of perigee: 24
9075 deg
Mean anomaly: 335
2364 deg
Mean motion: 15
55127535 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1006
Checksum: 309
Coasting Arc #12 (Orbit 1020)
---------------------------------------
Vector Time (GMT): 2015/053/14:55:03
523
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4357339
71 A = 6783707
56 meter
Y = 4597288
10 meter E =
0007026
Z = -2437140
61 I = 51
32864
XDOT = -2319
805652 Wp = 76
35296
YDOT = -5009
352254 meter/sec RA = 295
53013 deg
ZDOT = -5313
122629 TA = 131
03056
MA = 130
96980
Ha = 220
975 n
mi
Hp = 211
713
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14295733
95 X = -4396585
23
Y = 15082966
22 feet Y = 4548341
76 meter
Z = -7995868
16 Z = -2458403
37
XDOT = -7610
910933 XDOT = -2237
808593
YDOT = -16434
882723 feet/sec YDOT = -5034
835992 meter/sec
ZDOT = -17431
504687 ZDOT = -5324
191917
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9815658
24 X = -2991812
63
Y = 18276780
66 feet Y = 5570762
74 meter
Z = -8087640
49 Z = -2465112
82
XDOT = -10196
627286 XDOT = -3107
931997
YDOT = -13194
067915 feet/sec YDOT = -4021
551901 meter/sec
ZDOT = -17477
936499 ZDOT = -5327
275045
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 15053
64881383
00016717 00000-0 10270-3 0 9114
2 25544 51
6428 296
0794 0005928 28
2133 331
9340 15
55174608 10217
Satellite: ISS
Catalog Number: 25544
Epoch time: 15053
64881383 = yrday
fracday
Element set: 911
Inclination: 51
6428 deg
RA of node: 296
0794 deg
Eccentricity:
0005928
Arg of perigee: 28
2133 deg
Mean anomaly: 331
9340 deg
Mean motion: 15
55174608 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1021
Checksum: 305
Coasting Arc #13 (Orbit 1036)
---------------------------------------
Vector Time (GMT): 2015/054/14:55:03
523
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4559159
01 A = 6779130
95 meter
Y = -2967478
95 meter E =
0013688
Z = 4031685
37 I = 51
30059
XDOT = 849
912743 Wp = 78
47933
YDOT = 6575
565101 meter/sec RA = 290
51680 deg
ZDOT = 3870
286411 TA = 331
24570
MA = 331
32108
Ha = 220
796 n
mi
Hp = 211
628
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14957870
77 X = 4572418
97
Y = -9735823
33 feet Y = -2916420
90 meter
Z = 13227314
22 Z = 4053865
20
XDOT = 2788
427633 XDOT = 757
519821
YDOT = 21573
376316 feet/sec YDOT = 6584
553182 meter/sec
ZDOT = 12697
790063 ZDOT = 3874
189991
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11588093
31 X = 3532050
84
Y = -13479893
84 feet Y = -4108671
64 meter
Z = 13322708
09 Z = 4060761
43
XDOT = 7605
687762 XDOT = 2318
213630
YDOT = 19130
637572 feet/sec YDOT = 5831
018332 meter/sec
ZDOT = 12713
298369 ZDOT = 3875
013343
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 15054
67693701
00016717 00000-0 10270-3 0 9124
2 25544 51
6424 290
9444 0005834 31
2257 328
9242 15
55223571 10373
Satellite: ISS
Catalog Number: 25544
Epoch time: 15054
67693701 = yrday
fracday
Element set: 912
Inclination: 51
6424 deg
RA of node: 290
9444 deg
Eccentricity:
0005834
Arg of perigee: 31
2257 deg
Mean anomaly: 328
9242 deg
Mean motion: 15
55223571 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1037
Checksum: 301
Coasting Arc #14 (Orbit 1051)
---------------------------------------
Vector Time (GMT): 2015/055/14:55:03
523
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4448054
23 A = 6775106
36 meter
Y = 895873
89 meter E =
0018075
Z = -5047646
74 I = 51
27673
XDOT = 555
374501 Wp = 64
36505
YDOT = -7420
300751 meter/sec RA = 285
48812 deg
ZDOT = -1803
775285 TA = 188
04480
MA = 188
07382
Ha = 220
937 n
mi
Hp = 211
247
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14593353
79 X = -4433222
16
Y = 2939218
79 feet Y = 846215
33 meter
Z = -16560520
82 Z = -5069218
38
XDOT = 1822
094820 XDOT = 647
070764
YDOT = -24344
818737 feet/sec YDOT = -7413
577648 meter/sec
ZDOT = -5917
897917 ZDOT = -1800
854030
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12984156
94 X = -3957571
03
Y = 7067326
92 feet Y = 2154121
24 meter
Z = -16652939
39 Z = -5075815
93
XDOT = -4864
632044 XDOT = -1482
739847
YDOT = -22869
337937 feet/sec YDOT = -6970
574203 meter/sec
ZDOT = -5904
074231 ZDOT = -1799
561825
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 15055
64077343
00016717 00000-0 10270-3 0 9131
2 25544 51
6418 286
1308 0005851 36
6235 323
5317 15
55272489 10529
Satellite: ISS
Catalog Number: 25544
Epoch time: 15055
64077343 = yrday
fracday
Element set: 913
Inclination: 51
6418 deg
RA of node: 286
1308 deg
Eccentricity:
0005851
Arg of perigee: 36
6235 deg
Mean anomaly: 323
5317 deg
Mean motion: 15
55272489 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1052
Checksum: 304
Coasting Arc #15 (Orbit 1067)
---------------------------------------
Vector Time (GMT): 2015/056/14:55:03
523
Vector Time (MET): N/A
Weight (LBS) : 950073
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4034205
94 A = 6774094
14 meter
Y = 1381811
05 meter E =
0008454
Z = 5258403
52 I = 51
26590
XDOT = -1820
802452 Wp = 48
71215
YDOT = 7435
818641 meter/sec RA = 280
44941 deg
ZDOT = -551
023376 TA = 46
60364
MA = 46
53328
Ha = 220
838 n
mi
Hp = 211
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13235583
80 X = 3992911
29
Y = 4533500
83 feet Y = 1426693
69 meter
Z = 17251980
04 Z = 5277900
29
XDOT = -5973
761327 XDOT = -1901
139569
YDOT = 24395
730449 feet/sec YDOT = 7415
008007 meter/sec
ZDOT = -1807
819475 ZDOT = -560
064096
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13885302
37 X = 4232240
16
Y = 236859
50 feet Y = 72194
78 meter
Z = 17335120
40 Z = 5283744
70
XDOT = 1921
739621 XDOT = 585
746237
YDOT = 24028
719851 feet/sec YDOT = 7323
953811 meter/sec
ZDOT = -1847
808698 ZDOT = -563
212091
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 15056
66883453
00016717 00000-0 10270-3 0 9142
2 25544 51
6418 280
9960 0005816 40
3194 319
8390 15
55281236 10688
Satellite: ISS
Catalog Number: 25544
Epoch time: 15056
66883453 = yrday
fracday
Element set: 914
Inclination: 51
6418 deg
RA of node: 280
9960 deg
Eccentricity:
0005816
Arg of perigee: 40
3194 deg
Mean anomaly: 319
8390 deg
Mean motion: 15
55281236 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1068
Checksum: 324
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