[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 18th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 23680 6 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 124 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 3 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 3703)
---------------------------------------
Vector Time (GMT): 2014/076/02:12:55
216
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -122581
55 A = 6787829
07 meter
Y = 4296464
88 meter E =
0012414
Z = -5264262
62 I = 51
53333
XDOT = -7494
351572 Wp = 70
93142
YDOT = -1285
722825 meter/sec RA = 194
96574 deg
ZDOT = -872
564581 TA = 190
68302
MA = 190
70942
Ha = 225
856 n
mi
Hp = 221
069
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -402170
43 X = -145044
46
Y = 14096013
39 feet Y = 4294967
64 meter
Z = -17271202
82 Z = -5264913
36
XDOT = -24587
767624 XDOT = -7475
178707
YDOT = -4218
250738 feet/sec YDOT = -1369
422412 meter/sec
ZDOT = -2862
744688 ZDOT = -908
924182
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6134603
54 X = -1869827
16
Y = -12692967
47 feet Y = -3868816
48 meter
Z = -17274518
74 Z = -5265273
31
XDOT = 22882
298545 XDOT = 6974
524597
YDOT = -6944
192502 feet/sec YDOT = -2116
589875 meter/sec
ZDOT = -3016
142982 ZDOT = -919
320381
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 14076
11000926
00016717 00000-0 10270-3 0 9004
2 25544 51
6503 195
9663 0003515 312
3588 47
7265 15
50633737 37040
Satellite: ISS
Catalog Number: 25544
Epoch time: 14076
11000926 = yrday
fracday
Element set: 900
Inclination: 51
6503 deg
RA of node: 195
9663 deg
Eccentricity:
0003515
Arg of perigee: 312
3588 deg
Mean anomaly: 47
7265 deg
Mean motion: 15
50633737 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3704
Checksum: 298
Coasting Arc #2 (Orbit 3719)
---------------------------------------
Vector Time (GMT): 2014/077/02:12:55
216
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 457089
40 A = 6787426
28 meter
Y = -4200331
73 meter E =
0001985
Z = 5312027
91 I = 51
56261
XDOT = 7574
665039 Wp = 356
99887
YDOT = 1135
367469 meter/sec RA = 189
99665 deg
ZDOT = 247
917229 TA = 90
64540
MA = 90
62266
Ha = 225
795 n
mi
Hp = 221
006
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1499637
13 X = 478220
34
Y = -13780615
91 feet Y = -4195101
28 meter
Z = 17427913
09 Z = 5314300
37
XDOT = 24851
263252 XDOT = 7560
201834
YDOT = 3724
958889 feet/sec YDOT = 1219
991403 meter/sec
ZDOT = 813
376736 ZDOT = 284
678592
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5235734
78 X = 1595851
96
Y = 12821364
16 feet Y = 3907951
80 meter
Z = 17438065
93 Z = 5315122
50
XDOT = -22754
808954 XDOT = -6935
665769
YDOT = 7983
583601 feet/sec YDOT = 2433
396282 meter/sec
ZDOT = 968
503076 ZDOT = 295
199737
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 14077
14116152
00016717 00000-0 10270-3 0 9018
2 25544 51
6502 190
8535 0003646 315
0414 45
0441 15
50682188 37203
Satellite: ISS
Catalog Number: 25544
Epoch time: 14077
14116152 = yrday
fracday
Element set: 901
Inclination: 51
6502 deg
RA of node: 190
8535 deg
Eccentricity:
0003646
Arg of perigee: 315
0414 deg
Mean anomaly: 45
0441 deg
Mean motion: 15
50682188 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3720
Checksum: 275
Coasting Arc #3 (Orbit 3734)
---------------------------------------
Vector Time (GMT): 2014/078/02:12:55
216
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -806310
34 A = 6787369
28 meter
Y = 4158237
49 meter E =
0012620
Z = -5314183
97 I = 51
59376
XDOT = -7581
396446 Wp = 80
46278
YDOT = -976
680368 meter/sec RA = 185
02915 deg
ZDOT = 388
910056 TA = 193
23842
MA = 193
27156
Ha = 225
935 n
mi
Hp = 220
818
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2645375
13 X = -826934
06
Y = 13642511
45 feet Y = 4149104
73 meter
Z = -17434986
78 Z = -5318151
62
XDOT = -24873
347919 XDOT = -7571
800725
YDOT = -3204
331915 feet/sec YDOT = -1061
406697 meter/sec
ZDOT = 1275
951628 ZDOT = 352
104018
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4386231
07 X = -1336923
23
Y = -13163328
23 feet Y = -4012182
45 meter
Z = -17452296
68 Z = -5319460
03
XDOT = 22361
047688 XDOT = 6815
647335
YDOT = -8924
477678 feet/sec YDOT = -2720
180796 meter/sec
ZDOT = 1120
603542 ZDOT = 341
559960
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 14078
10784505
00016717 00000-0 10270-3 0 9029
2 25544 51
6506 186
0601 0003710 320
7650 39
3231 15
50707865 37354
Satellite: ISS
Catalog Number: 25544
Epoch time: 14078
10784505 = yrday
fracday
Element set: 902
Inclination: 51
6506 deg
RA of node: 186
0601 deg
Eccentricity:
0003710
Arg of perigee: 320
7650 deg
Mean anomaly: 39
3231 deg
Mean motion: 15
50707865 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3735
Checksum: 287
Coasting Arc #4 (Orbit 3750)
---------------------------------------
Vector Time (GMT): 2014/079/02:12:55
216
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1187415
94 A = 6787488
49 meter
Y = -4147906
01 meter E =
0005075
Z = 5239801
48 I = 51
62550
XDOT = 7545
727145 Wp = 9
27095
YDOT = 835
011402 meter/sec RA = 180
06348 deg
ZDOT = -1043
927580 TA = 90
76486
MA = 90
70671
Ha = 225
877 n
mi
Hp = 220
736
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3895721
60 X = 1208257
09
Y = -13608615
53 feet Y = -4134510
37 meter
Z = 17190949
75 Z = 5245620
96
XDOT = 24756
322653 XDOT = 7540
900135
YDOT = 2739
538722 feet/sec YDOT = 919
365441 meter/sec
ZDOT = -3424
959251 ZDOT = -1007
283133
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3510388
14 X = 1069966
30
Y = 13681498
43 feet Y = 4170120
72 meter
Z = 17216085
28 Z = 5247462
79
XDOT = -21838
933429 XDOT = -6656
506909
YDOT = 9739
309105 feet/sec YDOT = 2968
541415 meter/sec
ZDOT = -3270
261450 ZDOT = -996
775690
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 14079
13894750
00016717 00000-0 10270-3 0 9038
2 25544 51
6503 180
9469 0003847 323
8712 36
2179 15
50764562 37512
Satellite: ISS
Catalog Number: 25544
Epoch time: 14079
13894750 = yrday
fracday
Element set: 903
Inclination: 51
6503 deg
RA of node: 180
9469 deg
Eccentricity:
0003847
Arg of perigee: 323
8712 deg
Mean anomaly: 36
2179 deg
Mean motion: 15
50764562 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3751
Checksum: 324
Coasting Arc #5 (Orbit 3765)
---------------------------------------
Vector Time (GMT): 2014/080/02:12:55
216
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1556226
34 A = 6788010
00 meter
Y = 4193938
29 meter E =
0011108
Z = -5115018
63 I = 51
65811
XDOT = -7433
167273 Wp = 88
14074
YDOT = -703
135455 meter/sec RA = 175
09972 deg
ZDOT = 1688
522383 TA = 198
17343
MA = 198
21316
Ha = 226
021 n
mi
Hp = 220
550
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5105729
46 X = -1578160
98
Y = 13759640
07 feet Y = 4176412
37 meter
Z = -16781557
17 Z = -5122632
33
XDOT = -24387
031735 XDOT = -7432
954549
YDOT = -2306
874854 feet/sec YDOT = -786
256525 meter/sec
ZDOT = 5539
771598 ZDOT = 1652
413495
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2782771
78 X = -848188
84
Y = -14371945
83 feet Y = -4380569
09 meter
Z = -16814285
10 Z = -5124994
10
XDOT = 21085
369164 XDOT = 6426
820521
YDOT = -10371
960285 feet/sec YDOT = -3161
373495 meter/sec
ZDOT = 5387
303451 ZDOT = 1642
050092
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 14080
10558458
00016717 00000-0 10270-3 0 9040
2 25544 51
6500 176
1528 0003912 328
5329 31
5588 15
50779839 37662
Satellite: ISS
Catalog Number: 25544
Epoch time: 14080
10558458 = yrday
fracday
Element set: 904
Inclination: 51
6500 deg
RA of node: 176
1528 deg
Eccentricity:
0003912
Arg of perigee: 328
5329 deg
Mean anomaly: 31
5588 deg
Mean motion: 15
50779839 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3766
Checksum: 326
Coasting Arc #6 (Orbit 3781)
---------------------------------------
Vector Time (GMT): 2014/081/02:12:55
216
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1944172
96 A = 6788676
59 meter
Y = -4270918
31 meter E =
0007988
Z = 4904938
21 I = 51
69170
XDOT = 7271
329384 Wp = 28
48483
YDOT = 612
547947 meter/sec RA = 170
13848 deg
ZDOT = -2340
339914 TA = 84
46544
MA = 84
37433
Ha = 225
980 n
mi
Hp = 220
436
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6378520
21 X = 1967960
12
Y = -14012199
18 feet Y = -4249043
86 meter
Z = 16092316
97 Z = 4914440
94
XDOT = 23856
067534 XDOT = 7275
307979
YDOT = 2009
671741 feet/sec YDOT = 693
882641 meter/sec
ZDOT = -7678
280557 ZDOT = -2305
007074
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2079152
69 X = 633725
74
Y = 15211571
69 feet Y = 4636487
05 meter
Z = 16133044
42 Z = 4917351
94
XDOT = -20242
419947 XDOT = -6169
889600
YDOT = 10781
196241 feet/sec YDOT = 3286
108614 meter/sec
ZDOT = -7529
062150 ZDOT = -2294
858143
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 14081
13663761
00016717 00000-0 10270-3 0 9059
2 25544 51
6499 171
0392 0004053 332
1299 27
9634 15
50844104 37823
Satellite: ISS
Catalog Number: 25544
Epoch time: 14081
13663761 = yrday
fracday
Element set: 905
Inclination: 51
6499 deg
RA of node: 171
0392 deg
Eccentricity:
0004053
Arg of perigee: 332
1299 deg
Mean anomaly: 27
9634 deg
Mean motion: 15
50844104 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3782
Checksum: 306
Coasting Arc #7 (Orbit 3796)
---------------------------------------
Vector Time (GMT): 2014/082/02:12:55
216
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2291885
64 A = 6789717
60 meter
Y = 4397534
08 meter E =
0008196
Z = -4644827
22 I = 51
72493
XDOT = -7040
899740 Wp = 89
07427
YDOT = -550
791186 meter/sec RA = 165
17936 deg
ZDOT = 2957
351915 TA = 210
37459
MA = 210
42211
Ha = 226
108 n
mi
Hp = 220
266
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7519309
85 X = -2318326
42
Y = 14427605
24 feet Y = 4371756
52 meter
Z = -15238934
46 Z = -4656025
48
XDOT = -23100
064765 XDOT = -7048
583252
YDOT = -1807
057696 feet/sec YDOT = -629
569757 meter/sec
ZDOT = 9702
598147 ZDOT = 2923
129572
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1603957
27 X = -488886
18
Y = -16144980
58 feet Y = -4920990
08 meter
Z = -15286852
53 Z = -4659432
65
XDOT = 19248
900014 XDOT = 5867
064724
YDOT = -10947
961412 feet/sec YDOT = -3336
938638 meter/sec
ZDOT = 9558
045944 ZDOT = 2913
292404
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 14082
10322881
00016717 00000-0 10270-3 0 9063
2 25544 51
6492 166
2443 0004073 335
9876 24
1084 15
50850298 37978
Satellite: ISS
Catalog Number: 25544
Epoch time: 14082
10322881 = yrday
fracday
Element set: 906
Inclination: 51
6492 deg
RA of node: 166
2443 deg
Eccentricity:
0004073
Arg of perigee: 335
9876 deg
Mean anomaly: 24
1084 deg
Mean motion: 15
50850298 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3797
Checksum: 315
Coasting Arc #8 (Orbit 3812)
---------------------------------------
Vector Time (GMT): 2014/083/02:12:55
216
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2644480
40 A = 6790828
17 meter
Y = -4546290
51 meter E =
0010458
Z = 4293252
06 I = 51
75931
XDOT = 6760
810101 Wp = 49
07893
YDOT = 554
535084 meter/sec RA = 160
22369 deg
ZDOT = -3564
823949 TA = 77
29872
MA = 77
18184
Ha = 226
091 n
mi
Hp = 220
119
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8676116
79 X = 2674266
32
Y = -14915651
29 feet Y = -4516551
35 meter
Z = 14085472
63 Z = 4306171
25
XDOT = 22181
135503 XDOT = 6771
423405
YDOT = 1819
340826 feet/sec YDOT = 630
197850 meter/sec
ZDOT = -11695
616630 ZDOT = -3531
955252
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1187370
42 X = 361910
50
Y = 17169249
87 feet Y = 5233187
36 meter
Z = 14140693
25 Z = 4310083
30
XDOT = -18235
165780 XDOT = -5558
078530
YDOT = 10812
573992 feet/sec YDOT = 3295
672553 meter/sec
ZDOT = -11556
767720 ZDOT = -3522
502801
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 14083
13423323
00016717 00000-0 10270-3 0 9071
2 25544 51
6494 161
1303 0004231 339
7836 20
3147 15
50919177 38132
Satellite: ISS
Catalog Number: 25544
Epoch time: 14083
13423323 = yrday
fracday
Element set: 907
Inclination: 51
6494 deg
RA of node: 161
1303 deg
Eccentricity:
0004231
Arg of perigee: 339
7836 deg
Mean anomaly: 20
3147 deg
Mean motion: 15
50919177 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3813
Checksum: 287
Coasting Arc #9 (Orbit 3827)
---------------------------------------
Vector Time (GMT): 2014/084/02:12:55
216
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2932404
94 A = 6792198
89 meter
Y = 4728750
01 meter E =
0005526
Z = -3898019
13 I = 51
79181
XDOT = -6431
972434 Wp = 67
02817
YDOT = -602
901263 meter/sec RA = 155
27023 deg
ZDOT = 4114
004284 TA = 246
06867
MA = 246
12657
Ha = 226
191 n
mi
Hp = 219
976
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9620751
12 X = -2966129
74
Y = 15514271
70 feet Y = 4695769
07 meter
Z = -12788776
67 Z = -3912346
58
XDOT = -21102
271766 XDOT = -6444
737003
YDOT = -1978
022518 feet/sec YDOT = -674
898707 meter/sec
ZDOT = 13497
389382 ZDOT = 4082
727920
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1043260
90 X = -317985
92
Y = -18182238
96 feet Y = -5541946
43 meter
Z = -12849983
67 Z = -3916675
02
XDOT = 17185
752401 XDOT = 5238
217332
YDOT = -10416
188776 feet/sec YDOT = -3174
854339 meter/sec
ZDOT = 13365
260743 ZDOT = 4073
731474
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 14084
10077940
00016717 00000-0 10270-3 0 9080
2 25544 51
6485 156
3349 0004171 343
3259 16
7754 15
50918489 38285
Satellite: ISS
Catalog Number: 25544
Epoch time: 14084
10077940 = yrday
fracday
Element set: 908
Inclination: 51
6485 deg
RA of node: 156
3349 deg
Eccentricity:
0004171
Arg of perigee: 343
3259 deg
Mean anomaly: 16
7754 deg
Mean motion: 15
50918489 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3828
Checksum: 329
Coasting Arc #10 (Orbit 3843)
---------------------------------------
Vector Time (GMT): 2014/085/02:12:55
216
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3212492
53 A = 6793499
34 meter
Y = -4916209
95 meter E =
0012165
Z = 3409541
99 I = 51
82510
XDOT = 6060
799384 Wp = 69
71553
YDOT = 736
585728 meter/sec RA = 150
32094 deg
ZDOT = -4630
939085 TA = 70
59076
MA = 70
45932
Ha = 226
198 n
mi
Hp = 219
796
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10539673
67 X = 3250665
62
Y = -16129297
75 feet Y = -4880072
00 meter
Z = 11186161
37 Z = 3425240
92
XDOT = 19884
512415 XDOT = 6074
607693
YDOT = 2416
619841 feet/sec YDOT = 804
438193 meter/sec
ZDOT = -15193
369701 ZDOT = -4601
463364
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 963393
07 X = 293642
21
Y = 19204336
28 feet Y = 5853481
70 meter
Z = 11253200
21 Z = 3429975
42
XDOT = -16206
556428 XDOT = -4939
758399
YDOT = 9676
385026 feet/sec YDOT = 2949
362156 meter/sec
ZDOT = -15068
856760 ZDOT = -4592
987540
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 14085
13173607
00016717 00000-0 10270-3 0 9092
2 25544 51
6490 151
2207 0004355 347
0356 13
0682 15
50990750 38440
Satellite: ISS
Catalog Number: 25544
Epoch time: 14085
13173607 = yrday
fracday
Element set: 909
Inclination: 51
6490 deg
RA of node: 151
2207 deg
Eccentricity:
0004355
Arg of perigee: 347
0356 deg
Mean anomaly: 13
0682 deg
Mean motion: 15
50990750 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3844
Checksum: 296
Coasting Arc #11 (Orbit 3858)
---------------------------------------
Vector Time (GMT): 2014/086/02:12:55
216
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3411381
00 A = 6794902
44 meter
Y = 5113902
47 meter E =
0007021
Z = -2889928
94 I = 51
85487
XDOT = -5669
638867 Wp = 30
22530
YDOT = -923
536035 meter/sec RA = 145
37356 deg
ZDOT = 5069
662732 TA = 297
02508
MA = 297
09674
Ha = 226
274 n
mi
Hp = 219
684
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11192194
89 X = -3454274
04
Y = 16777895
24 feet Y = 5075514
03 meter
Z = -9481394
17 Z = -2906605
63
XDOT = -18601
177384 XDOT = -5683
516890
YDOT = -3029
973868 feet/sec YDOT = -987
014543 meter/sec
ZDOT = 16632
751745 ZDOT = 5042
087064
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1151919
39 X = -351105
03
Y = -20101758
96 feet Y = -6127016
13 meter
Z = -9552601
71 Z = -2911633
00
XDOT = 15318
843725 XDOT = 4669
183568
YDOT = -8709
154160 feet/sec YDOT = -2654
550188 meter/sec
ZDOT = 16516
285979 ZDOT = 5034
163966
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 14086
09823796
00016717 00000-0 10270-3 0 9101
2 25544 51
6476 146
4250 0004207 350
8743 9
2331 15
50983459 38598
Satellite: ISS
Catalog Number: 25544
Epoch time: 14086
09823796 = yrday
fracday
Element set: 910
Inclination: 51
6476 deg
RA of node: 146
4250 deg
Eccentricity:
0004207
Arg of perigee: 350
8743 deg
Mean anomaly: 9
2331 deg
Mean motion: 15
50983459 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3859
Checksum: 323
Coasting Arc #12 (Orbit 3874)
---------------------------------------
Vector Time (GMT): 2014/087/02:12:55
216
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3594708
60 A = 6796018
21 meter
Y = -5292465
96 meter E =
0012735
Z = 2281389
47 I = 51
88460
XDOT = 5250
795538 Wp = 89
28628
YDOT = 1206
282227 meter/sec RA = 140
43047 deg
ZDOT = -5448
705328 TA = 65
44261
MA = 65
30993
Ha = 226
293 n
mi
Hp = 219
466
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11793663
39 X = 3642540
79
Y = -17363733
46 feet Y = -5251999
86 meter
Z = 7484873
58 Z = 2298968
87
XDOT = 17227
019481 XDOT = 5263
384270
YDOT = 3957
618854 feet/sec YDOT = 1265
069616 meter/sec
ZDOT = -17876
329817 ZDOT = -5423
167454
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1372045
65 X = 418199
51
Y = 20918365
43 feet Y = 6375917
78 meter
Z = 7559930
35 Z = 2304266
77
XDOT = -14595
309367 XDOT = -4448
650295
YDOT = 7409
885646 feet/sec YDOT = 2258
533145 meter/sec
ZDOT = -17768
510755 ZDOT = -5415
842078
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 14087
12914733
00016717 00000-0 10270-3 0 9119
2 25544 51
6479 141
3104 0004414 354
4502 5
6599 15
51061860 38754
Satellite: ISS
Catalog Number: 25544
Epoch time: 14087
12914733 = yrday
fracday
Element set: 911
Inclination: 51
6479 deg
RA of node: 141
3104 deg
Eccentricity:
0004414
Arg of perigee: 354
4502 deg
Mean anomaly: 5
6599 deg
Mean motion: 15
51061860 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3875
Checksum: 297
Coasting Arc #13 (Orbit 3889)
---------------------------------------
Vector Time (GMT): 2014/088/02:12:55
216
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3691478
56 A = 6797100
10 meter
Y = 5453608
34 meter E =
0011289
Z = -1659930
73 I = 51
90973
XDOT = -4844
799304 Wp = 24
88088
YDOT = -1541
075129 meter/sec RA = 135
48846 deg
ZDOT = 5735
222621 TA = 317
02686
MA = 317
11498
Ha = 226
364 n
mi
Hp = 219
381
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12111150
12 X = -3744124
28
Y = 17892415
80 feet Y = 5412033
25 meter
Z = -5445966
95 Z = -1677992
06
XDOT = -15895
010841 XDOT = -4855
066393
YDOT = -5056
020765 feet/sec YDOT = -1595
309331 meter/sec
ZDOT = 18816
347181 ZDOT = 5711
662615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1805868
53 X = -550428
73
Y = -21510726
27 feet Y = -6556469
37 meter
Z = -5523092
49 Z = -1683438
59
XDOT = 14075
802888 XDOT = 4290
304720
YDOT = -5967
424261 feet/sec YDOT = -1818
870915 meter/sec
ZDOT = 18716
932388 ZDOT = 5704
920992
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 14088
09560514
00016717 00000-0 10270-3 0 9121
2 25544 51
6463 136
5142 0004196 359
0784 1
0358 15
51047460 38905
Satellite: ISS
Catalog Number: 25544
Epoch time: 14088
09560514 = yrday
fracday
Element set: 912
Inclination: 51
6463 deg
RA of node: 136
5142 deg
Eccentricity:
0004196
Arg of perigee: 359
0784 deg
Mean anomaly: 1
0358 deg
Mean motion: 15
51047460 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3890
Checksum: 300
Coasting Arc #14 (Orbit 3905)
---------------------------------------
Vector Time (GMT): 2014/089/02:12:55
216
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3772887
87 A = 6797637
11 meter
Y = -5567791
22 meter E =
0011801
Z = 961397
10 I = 51
93375
XDOT = 4430
690828 Wp = 106
05897
YDOT = 1968
097552 meter/sec RA = 130
55017 deg
ZDOT = -5932
572402 TA = 63
58668
MA = 63
46561
Ha = 226
379 n
mi
Hp = 219
127
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12378241
03 X = 3830197
58
Y = -18267031
55 feet Y = -5525279
78 meter
Z = 3154189
96 Z = 979865
35
XDOT = 14536
387230 XDOT = 4437
172428
YDOT = 6457
012966 feet/sec YDOT = 2017
679720 meter/sec
ZDOT = -19463
820218 ZDOT = -5911
033233
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2199340
66 X = 670359
03
Y = 21944575
96 feet Y = 6688706
75 meter
Z = 3233062
57 Z = 985437
47
XDOT = -13793
128861 XDOT = -4204
145677
YDOT = 4263
549857 feet/sec YDOT = 1299
529996 meter/sec
ZDOT = -19373
007547 ZDOT = -5904
892700
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 14089
12646720
00016717 00000-0 10270-3 0 9131
2 25544 51
6462 131
3990 0004418 2
7171 357
4003 15
51133982 39065
Satellite: ISS
Catalog Number: 25544
Epoch time: 14089
12646720 = yrday
fracday
Element set: 913
Inclination: 51
6462 deg
RA of node: 131
3990 deg
Eccentricity:
0004418
Arg of perigee: 2
7171 deg
Mean anomaly: 357
4003 deg
Mean motion: 15
51133982 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3906
Checksum: 290
Coasting Arc #15 (Orbit 3920)
---------------------------------------
Vector Time (GMT): 2014/090/02:12:55
216
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3774886
20 A = 6798063
84 meter
Y = 5637240
12 meter E =
0015070
Z = -272975
92 I = 51
95317
XDOT = -4060
260378 Wp = 34
30282
YDOT = -2435
309316 meter/sec RA = 125
61206 deg
ZDOT = 6029
839843 TA = 322
77089
MA = 322
87527
Ha = 226
453 n
mi
Hp = 219
055
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12384797
24 X = -3836316
49
Y = 18494882
28 feet Y = 5594683
40 meter
Z = -895590
27 Z = -291463
94
XDOT = -13321
064233 XDOT = -4062
017664
YDOT = -7989
859959 feet/sec YDOT = -2480
722700 meter/sec
ZDOT = 19782
939116 ZDOT = 6010
111622
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2709796
15 X = -825945
87
Y = -22089662
17 feet Y = -6732929
03 meter
Z = -974569
04 Z = -297048
64
XDOT = 13786
906375 XDOT = 4202
249063
YDOT = -2537
310049 feet/sec YDOT = -773
372103 meter/sec
ZDOT = 19699
849773 ZDOT = 6004
514211
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 14090
09288062
00016717 00000-0 10270-3 0 9141
2 25544 51
6449 126
6022 0004152 8
1868 351
9350 15
51116113 39219
Satellite: ISS
Catalog Number: 25544
Epoch time: 14090
09288062 = yrday
fracday
Element set: 914
Inclination: 51
6449 deg
RA of node: 126
6022 deg
Eccentricity:
0004152
Arg of perigee: 8
1868 deg
Mean anomaly: 351
9350 deg
Mean motion: 15
51116113 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3921
Checksum: 284
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