[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
October 24th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 26737 55 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 130 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 252 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 3107)
---------------------------------------
Vector Time (GMT): 2014/295/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 437965
24 A = 6787489
18 meter
Y = 4270841
74 meter E =
0011897
Z = -5267571
25 I = 51
57539
XDOT = -7599
106761 Wp = 76
26493
YDOT = -293
336492 meter/sec RA = 187
40883 deg
ZDOT = -868
542032 TA = 185
40055
MA = 185
41340
Ha = 225
383 n
mi
Hp = 220
992
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1436893
82 X = 415763
91
Y = 14011947
95 feet Y = 4275614
62 meter
Z = -17282057
89 Z = -5265498
03
XDOT = -24931
452629 XDOT = -7591
042620
YDOT = -962
390064 feet/sec YDOT = -378
269637 meter/sec
ZDOT = -2849
547350 ZDOT = -905
438654
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8346150
41 X = -2543906
64
Y = -11358875
00 feet Y = -3462185
10 meter
Z = -17273870
63 Z = -5265075
77
XDOT = 21226
042923 XDOT = 6469
697883
YDOT = -11018
504846 feet/sec YDOT = -3358
440277 meter/sec
ZDOT = -3006
573406 ZDOT = -916
403574
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 14295
51769800
00016717 00000-0 10270-3 0 9004
2 25544 51
6469 188
4270 0002996 292
4814 67
6020 15
50749512 31081
Satellite: ISS
Catalog Number: 25544
Epoch time: 14295
51769800 = yrday
fracday
Element set: 900
Inclination: 51
6469 deg
RA of node: 188
4270 deg
Eccentricity:
0002996
Arg of perigee: 292
4814 deg
Mean anomaly: 67
6020 deg
Mean motion: 15
50749512 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3108
Checksum: 319
Coasting Arc #2 (Orbit 3123)
---------------------------------------
Vector Time (GMT): 2014/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -47242
40 A = 6787085
31 meter
Y = -4218903
92 meter E =
0000856
Z = 5316596
13 I = 51
60542
XDOT = 7658
788020 Wp = 335
33809
YDOT = 166
891943 meter/sec RA = 182
44126 deg
ZDOT = 201
261838 TA = 112
74611
MA = 112
73706
Ha = 225
297 n
mi
Hp = 220
937
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -154994
75 X = -25889
11
Y = -13841548
30 feet Y = -4219312
30 meter
Z = 17442900
68 Z = 5316418
91
XDOT = 25127
257284 XDOT = 7655
374880
YDOT = 547
545746 feet/sec YDOT = 252
518410 meter/sec
ZDOT = 660
307869 ZDOT = 238
459807
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7354592
98 X = 2241679
94
Y = 11727177
24 feet Y = 3574443
62 meter
Z = 17442779
11 Z = 5316559
07
XDOT = -20961
852441 XDOT = -6389
172624
YDOT = 11932
162221 feet/sec YDOT = 3636
923045 meter/sec
ZDOT = 818
649498 ZDOT = 249
524367
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 14296
54877239
00016717 00000-0 10270-3 0 9015
2 25544 51
6467 183
3132 0003089 294
5696 65
5133 15
50796593 31246
Satellite: ISS
Catalog Number: 25544
Epoch time: 14296
54877239 = yrday
fracday
Element set: 901
Inclination: 51
6467 deg
RA of node: 183
3132 deg
Eccentricity:
0003089
Arg of perigee: 294
5696 deg
Mean anomaly: 65
5133 deg
Mean motion: 15
50796593 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3124
Checksum: 335
Coasting Arc #3 (Orbit 3138)
---------------------------------------
Vector Time (GMT): 2014/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -361150
08 A = 6787012
92 meter
Y = 4223678
51 meter E =
0011970
Z = -5310658
86 I = 51
63653
XDOT = -7638
995031 Wp = 87
29644
YDOT = -46
567338 meter/sec RA = 177
47493 deg
ZDOT = 483
947500 TA = 187
31983
MA = 187
33732
Ha = 225
301 n
mi
Hp = 220
829
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1184875
58 X = -382555
20
Y = 13857212
96 feet Y = 4219519
79 meter
Z = -17423421
44 Z = -5312465
65
XDOT = -25062
319656 XDOT = -7640
257477
YDOT = -152
779980 feet/sec YDOT = -131
998551 meter/sec
ZDOT = 1587
754264 ZDOT = 446
834252
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6426950
85 X = -1958934
62
Y = -12321941
24 feet Y = -3755727
69 meter
Z = -17431751
56 Z = -5313197
88
XDOT = 20448
525829 XDOT = 6232
710673
YDOT = -12681
366612 feet/sec YDOT = -3865
280543 meter/sec
ZDOT = 1429
739834 ZDOT = 435
784701
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 14297
51537704
00016717 00000-0 10270-3 0 9024
2 25544 51
6463 178
5186 0003169 298
9037 61
1796 15
50838535 31399
Satellite: ISS
Catalog Number: 25544
Epoch time: 14297
51537704 = yrday
fracday
Element set: 902
Inclination: 51
6463 deg
RA of node: 178
5186 deg
Eccentricity:
0003169
Arg of perigee: 298
9037 deg
Mean anomaly: 61
1796 deg
Mean motion: 15
50838535 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3139
Checksum: 337
Coasting Arc #4 (Orbit 3154)
---------------------------------------
Vector Time (GMT): 2014/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 791762
43 A = 6787205
47 meter
Y = -4266199
54 meter E =
0003885
Z = 5219329
60 I = 51
66872
XDOT = 7570
809929 Wp = 7
22490
YDOT = -49
951954 meter/sec RA = 172
51071 deg
ZDOT = -1185
445831 TA = 94
17070
MA = 94
12630
Ha = 225
202 n
mi
Hp = 220
768
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2597645
76 X = 814054
68
Y = -13996717
64 feet Y = -4257220
58 meter
Z = 17123784
77 Z = 5223230
38
XDOT = 24838
615254 XDOT = 7576
564494
YDOT = -163
884364 feet/sec YDOT = 34
741853 meter/sec
ZDOT = -3889
257975 ZDOT = -1148
652895
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5527042
87 X = 1684642
67
Y = 13096423
31 feet Y = 3991789
83 meter
Z = 17141043
33 Z = 5224590
01
XDOT = -19814
758987 XDOT = -6039
538539
YDOT = 13264
248335 feet/sec YDOT = 4042
942892 meter/sec
ZDOT = -3732
575502 ZDOT = -1137
689013
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 14298
54639081
00016717 00000-0 10270-3 0 9030
2 25544 51
6460 173
4043 0003271 301
6218 58
4613 15
50895912 31556
Satellite: ISS
Catalog Number: 25544
Epoch time: 14298
54639081 = yrday
fracday
Element set: 903
Inclination: 51
6460 deg
RA of node: 173
4043 deg
Eccentricity:
0003271
Arg of perigee: 301
6218 deg
Mean anomaly: 58
4613 deg
Mean motion: 15
50895912 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3155
Checksum: 300
Coasting Arc #5 (Orbit 3169)
---------------------------------------
Vector Time (GMT): 2014/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1210558
01 A = 6787807
94 meter
Y = 4363844
52 meter E =
0010082
Z = -5065271
44 I = 51
70100
XDOT = -7420
541039 Wp = 97
18307
YDOT = 119
471637 meter/sec RA = 167
54787 deg
ZDOT = 1878
357203 TA = 191
02459
MA = 191
04670
Ha = 225
252 n
mi
Hp = 220
652
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3971647
01 X = -1234659
44
Y = 14317075
20 feet Y = 4350172
30 meter
Z = -16618344
63 Z = -5071211
05
XDOT = -24345
607082 XDOT = -7430
450182
YDOT = 391
967314 feet/sec YDOT = 36
435014 meter/sec
ZDOT = 6162
589248 ZDOT = 1842
284220
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4788112
61 X = -1459416
72
Y = -14034350
48 feet Y = -4277670
03 meter
Z = -16644307
87 Z = -5073185
04
XDOT = 18983
646911 XDOT = 5786
215578
YDOT = -13595
391431 feet/sec YDOT = -4143
875308 meter/sec
ZDOT = 6008
943040 ZDOT = 1831
525839
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 14299
51293941
00016717 00000-0 10270-3 0 9040
2 25544 51
6451 168
6087 0003336 305
2478 54
8360 15
50924357 31702
Satellite: ISS
Catalog Number: 25544
Epoch time: 14299
51293941 = yrday
fracday
Element set: 904
Inclination: 51
6451 deg
RA of node: 168
6087 deg
Eccentricity:
0003336
Arg of perigee: 305
2478 deg
Mean anomaly: 54
8360 deg
Mean motion: 15
50924357 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3170
Checksum: 316
Coasting Arc #6 (Orbit 3185)
---------------------------------------
Vector Time (GMT): 2014/300/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1635446
21 A = 6788615
59 meter
Y = -4494636
48 meter E =
0006731
Z = 4816751
27 I = 51
73473
XDOT = 7217
559480 Wp = 32
49687
YDOT = -137
552151 meter/sec RA = 162
58824 deg
ZDOT = -2571
741508 TA = 82
84556
MA = 82
76904
Ha = 225
158 n
mi
Hp = 220
579
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5365637
16 X = 1662185
93
Y = -14746182
68 feet Y = -4476198
21 meter
Z = 15802989
74 Z = 4824761
31
XDOT = 23679
657085 XDOT = 7231
054186
YDOT = -451
286586 feet/sec YDOT = -56
765348 meter/sec
ZDOT = -8437
472139 ZDOT = -2536
645989
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4127681
12 X = 1258117
20
Y = 15103006
05 feet Y = 4603396
24 meter
Z = 15837799
95 Z = 4827361
42
XDOT = -18094
657780 XDOT = -5515
251691
YDOT = 13661
256729 feet/sec YDOT = 4163
951051 meter/sec
ZDOT = -8287
966092 ZDOT = -2526
172065
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 14300
54389323
00016717 00000-0 10270-3 0 9057
2 25544 51
6451 163
4940 0003465 308
5033 51
5807 15
50991614 31866
Satellite: ISS
Catalog Number: 25544
Epoch time: 14300
54389323 = yrday
fracday
Element set: 905
Inclination: 51
6451 deg
RA of node: 163
4940 deg
Eccentricity:
0003465
Arg of perigee: 308
5033 deg
Mean anomaly: 51
5807 deg
Mean motion: 15
50991614 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3186
Checksum: 297
Coasting Arc #7 (Orbit 3200)
---------------------------------------
Vector Time (GMT): 2014/301/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2018946
37 A = 6789800
88 meter
Y = 4668283
83 meter E =
0006510
Z = -4504195
55 I = 51
76734
XDOT = -6943
271041 Wp = 99
77108
YDOT = 108
100848 meter/sec RA = 157
63033 deg
ZDOT = 3227
167594 TA = 202
66222
MA = 202
69098
Ha = 225
231 n
mi
Hp = 220
455
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6623839
80 X = -2049117
76
Y = 15315891
82 feet Y = 4645537
86 meter
Z = -14777544
47 Z = -4514076
90
XDOT = -22779
760634 XDOT = -6959
640673
YDOT = 354
661575 feet/sec YDOT = 30
365237 meter/sec
ZDOT = 10587
820191 ZDOT = 3193
397702
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3697087
80 X = -1126872
36
Y = -16233176
54 feet Y = -4947872
21 meter
Z = -14820362
27 Z = -4517246
42
XDOT = 17108
087147 XDOT = 5214
544963
YDOT = -13422
672469 feet/sec YDOT = -4091
230569 meter/sec
ZDOT = 10443
945226 ZDOT = 3183
314505
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 14301
51038638
00016717 00000-0 10270-3 0 9066
2 25544 51
6440 158
6976 0003463 311
5322 48
5532 15
51009445 32014
Satellite: ISS
Catalog Number: 25544
Epoch time: 14301
51038638 = yrday
fracday
Element set: 906
Inclination: 51
6440 deg
RA of node: 158
6976 deg
Eccentricity:
0003463
Arg of perigee: 311
5322 deg
Mean anomaly: 48
5532 deg
Mean motion: 15
51009445 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3201
Checksum: 284
Coasting Arc #8 (Orbit 3216)
---------------------------------------
Vector Time (GMT): 2014/302/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2392231
82 A = 6791067
08 meter
Y = -4860463
52 meter E =
0009139
Z = 4092224
93 I = 51
80127
XDOT = 6620
062842 Wp = 57
41144
YDOT = -1
203980 meter/sec RA = 152
67659 deg
ZDOT = -3860
306165 TA = 72
50415
MA = 72
40429
Ha = 225
162 n
mi
Hp = 220
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7848529
58 X = 2426525
80
Y = -15946402
64 feet Y = -4833520
20 meter
Z = 13425934
80 Z = 4103929
66
XDOT = 21719
366279 XDOT = 6638
336725
YDOT = -3
950066 feet/sec YDOT = 72
927937 meter/sec
ZDOT = -12665
046472 ZDOT = -3828
101907
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3368484
79 X = 1026714
16
Y = 17412022
43 feet Y = 5307184
44 meter
Z = 13476560
55 Z = 4107655
66
XDOT = -16157
035924 XDOT = -4924
664550
YDOT = 12850
023764 feet/sec YDOT = 3916
687243 meter/sec
ZDOT = -12527
839116 ZDOT = -3818
485363
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 14302
54128085
00016717 00000-0 10270-3 0 9077
2 25544 51
6444 153
5824 0003644 315
0837 45
0019 15
51083622 32173
Satellite: ISS
Catalog Number: 25544
Epoch time: 14302
54128085 = yrday
fracday
Element set: 907
Inclination: 51
6444 deg
RA of node: 153
5824 deg
Eccentricity:
0003644
Arg of perigee: 315
0837 deg
Mean anomaly: 45
0019 deg
Mean motion: 15
51083622 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3217
Checksum: 284
Coasting Arc #9 (Orbit 3231)
---------------------------------------
Vector Time (GMT): 2014/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2699766
49 A = 6792567
36 meter
Y = 5072837
73 meter E =
0003516
Z = -3622643
25 I = 51
83251
XDOT = -6249
104400 Wp = 59
75928
YDOT = -168
263538 meter/sec RA = 147
72483 deg
ZDOT = 4426
439773 TA = 257
52982
MA = 257
56916
Ha = 225
233 n
mi
Hp = 220
239
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8857501
61 X = -2738693
61
Y = 16643168
42 feet Y = 5042429
42 meter
Z = -11885312
51 Z = -3635853
23
XDOT = -20502
311023 XDOT = -6268
260904
YDOT = -552
045727 feet/sec YDOT = -238
252037 meter/sec
ZDOT = 14522
440200 ZDOT = 4396
035565
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3291701
10 X = -1003310
49
Y = -18527140
87 feet Y = -5647072
54 meter
Z = -11942395
01 Z = -3640042
00
XDOT = 15238
143339 XDOT = 4644
586090
YDOT = -11974
485503 feet/sec YDOT = -3649
823181 meter/sec
ZDOT = 14392
912280 ZDOT = 4386
959663
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 14303
50771891
00016717 00000-0 10270-3 0 9084
2 25544 51
6432 148
7856 0003544 317
8591 42
2287 15
51094021 32325
Satellite: ISS
Catalog Number: 25544
Epoch time: 14303
50771891 = yrday
fracday
Element set: 908
Inclination: 51
6432 deg
RA of node: 148
7856 deg
Eccentricity:
0003544
Arg of perigee: 317
8591 deg
Mean anomaly: 42
2287 deg
Mean motion: 15
51094021 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3232
Checksum: 303
Coasting Arc #10 (Orbit 3247)
---------------------------------------
Vector Time (GMT): 2014/304/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2984541
15 A = 6793936
97 meter
Y = -5279417
61 meter E =
0010725
Z = 3055121
54 I = 51
86432
XDOT = 5841
728125 Wp = 81
49817
YDOT = 433
750570 meter/sec RA = 142
77770 deg
ZDOT = -4940
869320 TA = 63
61278
MA = 63
50273
Ha = 225
198 n
mi
Hp = 220
111
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9791801
69 X = 3028514
03
Y = -17320923
91 feet Y = -5245796
52 meter
Z = 10023364
65 Z = 3069727
27
XDOT = 19165
774689 XDOT = 5860
445104
YDOT = 1423
066175 feet/sec YDOT = 499
180972 meter/sec
ZDOT = -16210
201180 ZDOT = -4912
445238
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3299021
41 X = 1005541
73
Y = 19589330
50 feet Y = 5970827
94 meter
Z = 10086437
07 Z = 3074346
02
XDOT = -14462
676152 XDOT = -4408
223691
YDOT = 10747
312409 feet/sec YDOT = 3275
780822 meter/sec
ZDOT = -16089
139186 ZDOT = -4903
969624
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 14304
53855409
00016717 00000-0 10270-3 0 9097
2 25544 51
6437 143
6701 0003786 321
6851 38
4030 15
51175222 32486
Satellite: ISS
Catalog Number: 25544
Epoch time: 14304
53855409 = yrday
fracday
Element set: 909
Inclination: 51
6437 deg
RA of node: 143
6701 deg
Eccentricity:
0003786
Arg of perigee: 321
6851 deg
Mean anomaly: 38
4030 deg
Mean motion: 15
51175222 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3248
Checksum: 297
Coasting Arc #11 (Orbit 3262)
---------------------------------------
Vector Time (GMT): 2014/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3189366
21 A = 6795350
04 meter
Y = 5475690
05 meter E =
0006807
Z = -2444708
48 I = 51
89195
XDOT = -5419
196702 Wp = 17
15333
YDOT = -766
682227 meter/sec RA = 137
83223 deg
ZDOT = 5362
787689 TA = 315
62453
MA = 315
67906
Ha = 225
263 n
mi
Hp = 220
000
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10463799
91 X = -3238483
85
Y = 17964862
38 feet Y = 5439749
70 meter
Z = -8020697
12 Z = -2460321
83
XDOT = -17779
516739 XDOT = -5436
271755
YDOT = -2515
361636 feet/sec YDOT = -827
378320 meter/sec
ZDOT = 17594
447800 ZDOT = 5336
420229
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -3522919
14 X = -1073785
75
Y = -20462907
28 feet Y = -6237094
14 meter
Z = -8088104
70 Z = -2465254
31
XDOT = 13850
440439 XDOT = 4221
614246
YDOT = -9281
439231 feet/sec YDOT = -2828
982677 meter/sec
ZDOT = 17482
192743 ZDOT = 5328
572348
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 14305
50493682
00016717 00000-0 10270-3 0 9108
2 25544 51
6422 138
8729 0003586 324
6654 35
4259 15
51177473 32635
Satellite: ISS
Catalog Number: 25544
Epoch time: 14305
50493682 = yrday
fracday
Element set: 910
Inclination: 51
6422 deg
RA of node: 138
8729 deg
Eccentricity:
0003586
Arg of perigee: 324
6654 deg
Mean anomaly: 35
4259 deg
Mean motion: 15
51177473 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3263
Checksum: 317
Coasting Arc #12 (Orbit 3278)
---------------------------------------
Vector Time (GMT): 2014/306/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3366621
93 A = 6796333
24 meter
Y = -5634796
08 meter E =
0010936
Z = 1746535
01 I = 51
91887
XDOT = 4979
908173 Wp = 103
66579
YDOT = 1200
424319 meter/sec RA = 132
89109 deg
ZDOT = -5698
979519 TA = 57
26744
MA = 57
16207
Ha = 225
257 n
mi
Hp = 219
810
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11045347
54 X = 3420897
07
Y = -18486863
77 feet Y = -5596844
72 meter
Z = 5730101
74 Z = 1763022
10
XDOT = 16338
281409 XDOT = 4993
798879
YDOT = 3938
399998 feet/sec YDOT = 1256
190114 meter/sec
ZDOT = -18697
439366 ZDOT = -5674
753798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3765174
91 X = 1147625
31
Y = 21184112
75 feet Y = 6456917
57 meter
Z = 5801269
25 Z = 1768226
87
XDOT = -13477
427285 XDOT = -4107
919836
YDOT = 7511
805996 feet/sec YDOT = 2289
598468 meter/sec
ZDOT = -18594
374295 ZDOT = -5667
565285
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 14306
53571214
00016717 00000-0 10270-3 0 9111
2 25544 51
6425 133
7569 0003872 329
0267 31
0655 15
51269427 32791
Satellite: ISS
Catalog Number: 25544
Epoch time: 14306
53571214 = yrday
fracday
Element set: 911
Inclination: 51
6425 deg
RA of node: 133
7569 deg
Eccentricity:
0003872
Arg of perigee: 329
0267 deg
Mean anomaly: 31
0655 deg
Mean motion: 15
51269427 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3279
Checksum: 306
Coasting Arc #13 (Orbit 3293)
---------------------------------------
Vector Time (GMT): 2014/307/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3463287
36 A = 6797202
57 meter
Y = 5749873
85 meter E =
0011528
Z = -1028351
17 I = 51
94106
XDOT = -4560
742178 Wp = 22
18945
YDOT = -1693
371806 meter/sec RA = 127
95076 deg
ZDOT = 5923
442948 TA = 326
72175
MA = 326
79418
Ha = 225
325 n
mi
Hp = 219
718
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11362491
34 X = -3522330
88
Y = 18864415
50 feet Y = 5710814
91 meter
Z = -3373855
56 Z = -1045319
53
XDOT = -14963
064888 XDOT = -4570
242284
YDOT = -5555
681778 feet/sec YDOT = -1744
425638 meter/sec
ZDOT = 19433
867938 ZDOT = 5901
264127
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4133643
08 X = -1259934
41
Y = -21619105
99 feet Y = -6589503
51 meter
Z = -3447105
15 Z = -1050677
65
XDOT = 13367
192498 XDOT = 4074
320273
YDOT = -5623
118148 feet/sec YDOT = -1713
926412 meter/sec
ZDOT = 19339
602201 ZDOT = 5894
710751
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 14307
50203860
00016717 00000-0 10270-3 0 9129
2 25544 51
6412 128
9591 0003599 332
3934 27
7025 15
51263465 32948
Satellite: ISS
Catalog Number: 25544
Epoch time: 14307
50203860 = yrday
fracday
Element set: 912
Inclination: 51
6412 deg
RA of node: 128
9591 deg
Eccentricity:
0003599
Arg of perigee: 332
3934 deg
Mean anomaly: 27
7025 deg
Mean motion: 15
51263465 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3294
Checksum: 301
Coasting Arc #14 (Orbit 3309)
---------------------------------------
Vector Time (GMT): 2014/308/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3538129
22 A = 6797351
30 meter
Y = -5794690
88 meter E =
0009209
Z = 243235
31 I = 51
96097
XDOT = 4147
554193 Wp = 121
71373
YDOT = 2272
568193 meter/sec RA = 123
01362 deg
ZDOT = -6027
835778 TA = 55
68082
MA = 55
59369
Ha = 225
333 n
mi
Hp = 219
472
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11608035
49 X = 3601482
25
Y = -19011453
03 feet Y = -5754770
98 meter
Z = 798016
12 Z = 260577
74
XDOT = 13607
461262 XDOT = 4151
115533
YDOT = 7455
932392 feet/sec YDOT = 2318
968323 meter/sec
ZDOT = -19776
364101 ZDOT = -6007
678578
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4413007
34 X = 1345084
64
Y = 21830760
57 feet Y = 6654015
82 meter
Z = 872882
07 Z = 266054
45
XDOT = -13546
656390 XDOT = -4129
020868
YDOT = 3545
234919 feet/sec YDOT = 1080
587603 meter/sec
ZDOT = -19690
807840 ZDOT = -6001
758230
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 14308
53275327
00016717 00000-0 10270-3 0 9131
2 25544 51
6412 123
8423 0003888 337
5169 22
5812 15
51361804 33106
Satellite: ISS
Catalog Number: 25544
Epoch time: 14308
53275327 = yrday
fracday
Element set: 913
Inclination: 51
6412 deg
RA of node: 123
8423 deg
Eccentricity:
0003888
Arg of perigee: 337
5169 deg
Mean anomaly: 22
5812 deg
Mean motion: 15
51361804 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3310
Checksum: 291
Coasting Arc #15 (Orbit 3325)
---------------------------------------
Vector Time (GMT): 2014/309/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 946559
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3546182
27 A = 6797286
11 meter
Y = 5764565
40 meter E =
0014588
Z = 531730
20 I = 51
97651
XDOT = -3784
628183 Wp = 37
35635
YDOT = -2889
419135 meter/sec RA = 118
07642 deg
ZDOT = 6009
566527 TA = 328
34980
MA = 328
43744
Ha = 225
397 n
mi
Hp = 219
387
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11634456
26 X = -3612962
46
Y = 18912616
14 feet Y = 5724536
33 meter
Z = 1744521
64 Z = 514340
36
XDOT = -12416
759131 XDOT = -3781
230067
YDOT = -9479
721573 feet/sec YDOT = -2931
721970 meter/sec
ZDOT = 19716
425613 ZDOT = 5991
189259
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4688968
52 X = -1429197
60
Y = -21709848
38 feet Y = -6617161
79 meter
Z = 1669441
60 Z = 508845
80
XDOT = 14028
200297 XDOT = 4275
795451
YDOT = -1499
964387 feet/sec YDOT = -457
189145 meter/sec
ZDOT = 19638
558780 ZDOT = 5985
832716
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 14309
56343903
00016717 00000-0 10270-3 0 9142
2 25544 51
6407 118
7244 0003597 341
0355 19
0662 15
51359300 33267
Satellite: ISS
Catalog Number: 25544
Epoch time: 14309
56343903 = yrday
fracday
Element set: 914
Inclination: 51
6407 deg
RA of node: 118
7244 deg
Eccentricity:
0003597
Arg of perigee: 341
0355 deg
Mean anomaly: 19
0662 deg
Mean motion: 15
51359300 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3326
Checksum: 293
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