[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
August 14th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 8611 13 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
226/17:01:54
736 1
2 3
3 3
4
N/A 2
1 -0
4 228
4
000/00:07:49
472 -2
3 -0
5 220
5
227/10:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
5
000/00:00:00
000 0
0 0
0 220
3
Coasting Arc #1 (Orbit 2008)
---------------------------------------
Vector Time (GMT): 2014/224/16:06:15
470
Vector Time (MET): N/A
Weight (LBS) : 938342
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3921676
85 A = 6791510
98 meter
Y = 3507669
58 meter E =
0009005
Z = -4298504
23 I = 51
64521
XDOT = -6247
834921 Wp = 61
79464
YDOT = -2644
446038 meter/sec RA = 178
46608 deg
ZDOT = 3552
031988 TA = 244
42110
MA = 244
51420
Ha = 227
792 n
mi
Hp = 219
523
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12866393
88 X = -3939728
58
Y = 11508102
29 feet Y = 3463713
72 meter
Z = -14102704
18 Z = -4317598
85
XDOT = -20498
146067 XDOT = -6235
054081
YDOT = -8676
004062 feet/sec YDOT = -2714
241728 meter/sec
ZDOT = 11653
648255 ZDOT = 3521
712615
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7599586
15 X = 2316353
86
Y = -15424542
92 feet Y = -4701400
68 meter
Z = -14184376
65 Z = -4323398
00
XDOT = 21196
536087 XDOT = 6460
704199
YDOT = -125
619739 feet/sec YDOT = -38
288896 meter/sec
ZDOT = 11525
187750 ZDOT = 3512
877226
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 14224
68072293
00016717 00000-0 10270-3 0 9007
2 25544 51
6477 179
5552 0007290 359
3131
8008 15
50670418 20093
Satellite: ISS
Catalog Number: 25544
Epoch time: 14224
68072293 = yrday
fracday
Element set: 900
Inclination: 51
6477 deg
RA of node: 179
5552 deg
Eccentricity:
0007290
Arg of perigee: 359
3131 deg
Mean anomaly:
8008 deg
Mean motion: 15
50670418 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2009
Checksum: 294
Coasting Arc #2 (Orbit 2024)
---------------------------------------
Vector Time (GMT): 2014/225/16:06:15
470
Vector Time (MET): N/A
Weight (LBS) : 938342
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4215848
86 A = 6792740
92 meter
Y = -3599955
50 meter E =
0014585
Z = 3922777
41 I = 51
68068
XDOT = 5975
175936 Wp = 51
08925
YDOT = 2550
676831 meter/sec RA = 173
50753 deg
ZDOT = -4061
681354 TA = 81
49959
MA = 81
33431
Ha = 227
879 n
mi
Hp = 219
355
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13831525
12 X = 4236735
73
Y = -11810877
64 feet Y = -3552694
17 meter
Z = 12870004
62 Z = 3943308
05
XDOT = 19603
595589 XDOT = 5965
939663
YDOT = 8368
362308 feet/sec YDOT = 2617
443246 meter/sec
ZDOT = -13325
726228 ZDOT = -4032
677767
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8113175
56 X = -2472895
91
Y = 16208538
76 feet Y = 4940362
61 meter
Z = 12957800
37 Z = 3949537
55
XDOT = -20209
177074 XDOT = -6159
757172
YDOT = 489
052824 feet/sec YDOT = 149
063301 meter/sec
ZDOT = -13202
832649 ZDOT = -4024
223391
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 14225
71185090
00016717 00000-0 10270-3 0 9013
2 25544 51
6477 174
4419 0007353 3
2997 356
8202 15
50696828 20255
Satellite: ISS
Catalog Number: 25544
Epoch time: 14225
71185090 = yrday
fracday
Element set: 901
Inclination: 51
6477 deg
RA of node: 174
4419 deg
Eccentricity:
0007353
Arg of perigee: 3
2997 deg
Mean anomaly: 356
8202 deg
Mean motion: 15
50696828 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2025
Checksum: 312
Coasting Arc #3 (Orbit 2039)
---------------------------------------
Vector Time (GMT): 2014/226/16:06:15
470
Vector Time (MET): N/A
Weight (LBS) : 938342
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4431134
19 A = 6793977
17 meter
Y = 3744060
27 meter E =
0009005
Z = -3534867
18 I = 51
71584
XDOT = -5677
962912 Wp = 41
68733
YDOT = -2478
574207 meter/sec RA = 168
55194 deg
ZDOT = 4505
518954 TA = 276
79045
MA = 276
89290
Ha = 227
952 n
mi
Hp = 219
227
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14537841
84 X = -4455500
73
Y = 12283662
30 feet Y = 3694372
06 meter
Z = -11597333
26 Z = -3556452
15
XDOT = -18628
487244 XDOT = -5671
711070
YDOT = -8131
805142 feet/sec YDOT = -2542
033680 meter/sec
ZDOT = 14781
886333 ZDOT = 4477
951796
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8296690
61 X = 2528831
30
Y = -17066123
57 feet Y = -5201754
46 meter
Z = -11689640
50 Z = -3563002
42
XDOT = 19165
755162 XDOT = 5841
722173
YDOT = -698
245092 feet/sec YDOT = -212
825104 meter/sec
ZDOT = 14665
077763 ZDOT = 4469
915702
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 14226
67852614
00016717 00000-0 10270-3 0 9023
2 25544 51
6479 169
6480 0007360 5
7236 354
3997 15
50690638 20406
Satellite: ISS
Catalog Number: 25544
Epoch time: 14226
67852614 = yrday
fracday
Element set: 902
Inclination: 51
6479 deg
RA of node: 169
6480 deg
Eccentricity:
0007360
Arg of perigee: 5
7236 deg
Mean anomaly: 354
3997 deg
Mean motion: 15
50690638 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2040
Checksum: 323
Coasting Arc #4 (Orbit 2040)
---------------------------------------
Vector Time (GMT): 2014/226/17:05:49
472
Vector Time (MET): N/A
Weight (LBS) : 938004
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6707539
36 A = 6800925
25 meter
Y = -649550
52 meter E =
0008225
Z = -906001
23 I = 51
73233
XDOT = -325
580850 Wp = 113
99015
YDOT = 4838
992379 meter/sec RA = 168
38091 deg
ZDOT = -5925
510742 TA = 75
78085
MA = 75
68950
Ha = 228
423 n
mi
Hp = 220
522
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 22006362
74 X = 6718705
29
Y = -2131071
27 feet Y = -574480
10 meter
Z = -2972444
98 Z = -873390
12
XDOT = -1068
178642 XDOT = -350
883436
YDOT = 15875
959249 feet/sec YDOT = 4835
209765 meter/sec
ZDOT = -19440
652041 ZDOT = -5927
154042
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15864349
42 X = -4835453
70
Y = 15425604
88 feet Y = 4701724
37 meter
Z = -2833730
15 Z = -863720
95
XDOT = -8055
331739 XDOT = -2455
265114
YDOT = -11828
207425 feet/sec YDOT = -3605
237623 meter/sec
ZDOT = -19448
357804 ZDOT = -5927
859459
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 14226
74298585
00016717 00000-0 10270-3 0 9033
2 25544 51
6465 169
3288 0004659 14
2578 345
8712 15
50038101 20418
Satellite: ISS
Catalog Number: 25544
Epoch time: 14226
74298585 = yrday
fracday
Element set: 903
Inclination: 51
6465 deg
RA of node: 169
3288 deg
Eccentricity:
0004659
Arg of perigee: 14
2578 deg
Mean anomaly: 345
8712 deg
Mean motion: 15
50038101 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2041
Checksum: 315
Coasting Arc #5 (Orbit 2051)
---------------------------------------
Vector Time (GMT): 2014/227/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 927460
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4074222
11 A = 6795599
22 meter
Y = 4067333
98 meter E =
0007903
Z = -3613267
43 I = 51
73417
XDOT = -5917
319851 Wp = 61
72317
YDOT = -2003
963785 meter/sec RA = 164
72278 deg
ZDOT = 4427
445058 TA = 255
66128
MA = 255
74903
Ha = 228
479 n
mi
Hp = 220
263
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13366870
44 X = -4101849
22
Y = 13344271
58 feet Y = 4021618
78 meter
Z = -11854551
92 Z = -3633126
53
XDOT = -19413
779040 XDOT = -5915
978210
YDOT = -6574
684335 feet/sec YDOT = -2070
127397 meter/sec
ZDOT = 14525
738378 ZDOT = 4398
703126
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18425502
78 X = 5616093
25
Y = 3901346
68 feet Y = 1189130
47 meter
Z = -11939579
22 Z = -3639183
75
XDOT = 5371
912205 XDOT = 1637
358840
YDOT = 18600
447584 feet/sec YDOT = 5669
416424 meter/sec
ZDOT = 14403
857827 ZDOT = 4390
295866
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 14227
45216014
00016717 00000-0 10270-3 0 9040
2 25544 51
6434 165
8138 0004870 18
3981 341
7345 15
50058291 20528
Satellite: ISS
Catalog Number: 25544
Epoch time: 14227
45216014 = yrday
fracday
Element set: 904
Inclination: 51
6434 deg
RA of node: 165
8138 deg
Eccentricity:
0004870
Arg of perigee: 18
3981 deg
Mean anomaly: 341
7345 deg
Mean motion: 15
50058291 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2052
Checksum: 292
Coasting Arc #6 (Orbit 2067)
---------------------------------------
Vector Time (GMT): 2014/228/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 927460
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4093891
64 A = 6796372
16 meter
Y = -4289829
36 meter E =
0014951
Z = 3312953
33 I = 51
76729
XDOT = 5755
936336 Wp = 73
85310
YDOT = 1836
518868 meter/sec RA = 159
77568 deg
ZDOT = -4712
966599 TA = 67
76346
MA = 67
60495
Ha = 228
482 n
mi
Hp = 220
153
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13431403
02 X = 4125464
08
Y = -14074243
31 feet Y = -4243872
20 meter
Z = 10869269
44 Z = 3332917
54
XDOT = 18884
305564 XDOT = 5757
866084
YDOT = 6025
324369 feet/sec YDOT = 1900
896124 meter/sec
ZDOT = -15462
488842 ZDOT = -4685
000630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19135165
07 X = -5832398
31
Y = -3235117
85 feet Y = -986063
92 meter
Z = 10954788
91 Z = 3339019
66
XDOT = -5829
405683 XDOT = -1776
802852
YDOT = -17717
163596 feet/sec YDOT = -5400
191464 meter/sec
ZDOT = -15343
871380 ZDOT = -4676
811997
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 14228
48367945
00016717 00000-0 10270-3 0 9055
2 25544 51
6438 160
7026 0004898 21
5083 338
6273 15
50097172 20684
Satellite: ISS
Catalog Number: 25544
Epoch time: 14228
48367945 = yrday
fracday
Element set: 905
Inclination: 51
6438 deg
RA of node: 160
7026 deg
Eccentricity:
0004898
Arg of perigee: 21
5083 deg
Mean anomaly: 338
6273 deg
Mean motion: 15
50097172 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2068
Checksum: 323
Coasting Arc #7 (Orbit 2082)
---------------------------------------
Vector Time (GMT): 2014/229/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 927460
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4046960
00 A = 6797157
22 meter
Y = 4539650
23 meter E =
0008614
Z = -3033851
28 I = 51
79861
XDOT = -5591
333421 Wp = 47
64842
YDOT = -1682
083674 meter/sec RA = 154
83112 deg
ZDOT = 4956
160944 TA = 277
73759
MA = 277
83539
Ha = 228
561 n
mi
Hp = 220
077
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13277427
84 X = -4082685
27
Y = 14893865
57 feet Y = 4494194
71 meter
Z = -9953580
31 Z = -3053597
54
XDOT = -18344
269754 XDOT = -5596
183675
YDOT = -5518
647224 feet/sec YDOT = -1744
636615 meter/sec
ZDOT = 16260
370550 ZDOT = 4928
987479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19775400
27 X = 6027542
00
Y = 2314882
45 feet Y = 705576
17 meter
Z = -10038224
25 Z = -3059650
75
XDOT = 6199
669800 XDOT = 1889
659355
YDOT = 16842
706614 feet/sec YDOT = 5133
656976 meter/sec
ZDOT = 16145
088008 ZDOT = 4921
022825
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 14229
45072176
00016717 00000-0 10270-3 0 9063
2 25544 51
6437 155
9112 0004911 24
3388 335
7994 15
50084423 20830
Satellite: ISS
Catalog Number: 25544
Epoch time: 14229
45072176 = yrday
fracday
Element set: 906
Inclination: 51
6437 deg
RA of node: 155
9112 deg
Eccentricity:
0004911
Arg of perigee: 24
3388 deg
Mean anomaly: 335
7994 deg
Mean motion: 15
50084423 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2083
Checksum: 307
Coasting Arc #8 (Orbit 2098)
---------------------------------------
Vector Time (GMT): 2014/230/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 927460
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4011985
68 A = 6797895
85 meter
Y = -4774723
98 meter E =
0015620
Z = 2693954
11 I = 51
82999
XDOT = 5401
052228 Wp = 84
18510
YDOT = 1590
434491 meter/sec RA = 149
88872 deg
ZDOT = -5197
231950 TA = 65
52334
MA = 65
36051
Ha = 228
591 n
mi
Hp = 219
943
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13162682
68 X = 4051993
32
Y = -15665104
92 feet Y = -4729635
65 meter
Z = 8838432
10 Z = 2713540
80
XDOT = 17719
987625 XDOT = 5408
112461
YDOT = 5217
960928 feet/sec YDOT = 1650
871978 meter/sec
ZDOT = -17051
285926 ZDOT = -5170
977500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20374017
51 X = -6210000
54
Y = -1434905
16 feet Y = -437359
09 meter
Z = 8922447
39 Z = 2719561
96
XDOT = -6329
721507 XDOT = -1929
299115
YDOT = -16014
589026 feet/sec YDOT = -4881
246735 meter/sec
ZDOT = -16939
885538 ZDOT = -5163
277112
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 14230
48222623
00016717 00000-0 10270-3 0 9073
2 25544 51
6445 150
7999 0004934 28
1965 331
9452 15
50117942 20990
Satellite: ISS
Catalog Number: 25544
Epoch time: 14230
48222623 = yrday
fracday
Element set: 907
Inclination: 51
6445 deg
RA of node: 150
7999 deg
Eccentricity:
0004934
Arg of perigee: 28
1965 deg
Mean anomaly: 331
9452 deg
Mean motion: 15
50117942 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2099
Checksum: 317
Coasting Arc #9 (Orbit 2113)
---------------------------------------
Vector Time (GMT): 2014/231/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 927460
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3906223
67 A = 6798587
14 meter
Y = 5025006
69 meter E =
0010391
Z = -2381706
26 I = 51
85859
XDOT = -5222
638244 Wp = 39
64020
YDOT = -1512
142370 meter/sec RA = 144
94867 deg
ZDOT = 5396
006231 TA = 293
89708
MA = 294
00591
Ha = 228
639 n
mi
Hp = 219
894
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12815694
47 X = -3950554
71
Y = 16486242
43 feet Y = 4981076
90 meter
Z = -7813996
91 Z = -2400789
62
XDOT = -17134
639907 XDOT = -5231
552723
YDOT = -4961
097015 feet/sec YDOT = -1570
595097 meter/sec
ZDOT = 17703
432515 ZDOT = 5370
614039
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20848246
41 X = 6354545
51
Y = 319009
48 feet Y = 97234
09 meter
Z = -7895924
03 Z = -2406677
64
XDOT = 6405
177827 XDOT = 1952
298202
YDOT = 15251
223239 feet/sec YDOT = 4648
572843 meter/sec
ZDOT = 17595
675323 ZDOT = 5363
161838
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 14231
44925454
00016717 00000-0 10270-3 0 9083
2 25544 51
6444 146
0084 0004935 30
6544 329
4894 15
50109970 21146
Satellite: ISS
Catalog Number: 25544
Epoch time: 14231
44925454 = yrday
fracday
Element set: 908
Inclination: 51
6444 deg
RA of node: 146
0084 deg
Eccentricity:
0004935
Arg of perigee: 30
6544 deg
Mean anomaly: 329
4894 deg
Mean motion: 15
50109970 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2114
Checksum: 303
Coasting Arc #10 (Orbit 2129)
---------------------------------------
Vector Time (GMT): 2014/232/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 927460
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3812891
03 A = 6799224
45 meter
Y = -5253379
26 meter E =
0015816
Z = 2007246
35 I = 51
88696
XDOT = 5027
033470 Wp = 93
95323
YDOT = 1500
922476 meter/sec RA = 140
01071 deg
ZDOT = -5584
102239 TA = 63
99303
MA = 63
83023
Ha = 228
688 n
mi
Hp = 219
758
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12509485
02 X = 3861601
73
Y = -17235496
26 feet Y = -5210468
68 meter
Z = 6585453
91 Z = 2025886
93
XDOT = 16492
891961 XDOT = 5037
001575
YDOT = 4924
286340 feet/sec YDOT = 1557
193696 meter/sec
ZDOT = -18320
545403 ZDOT = -5559
657770
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21259061
05 X = -6479761
81
Y = 735232
61 feet Y = 224098
90 meter
Z = 6665546
22 Z = 2031658
49
XDOT = -6253
459700 XDOT = -1906
054517
YDOT = -14582
813595 feet/sec YDOT = -4444
841584 meter/sec
ZDOT = -18216
806046 ZDOT = -5552
482483
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 14232
48074434
00016717 00000-0 10270-3 0 9092
2 25544 51
6454 140
8970 0004947 35
0386 325
1089 15
50135052 21306
Satellite: ISS
Catalog Number: 25544
Epoch time: 14232
48074434 = yrday
fracday
Element set: 909
Inclination: 51
6454 deg
RA of node: 140
8970 deg
Eccentricity:
0004947
Arg of perigee: 35
0386 deg
Mean anomaly: 325
1089 deg
Mean motion: 15
50135052 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2130
Checksum: 292
Coasting Arc #11 (Orbit 2144)
---------------------------------------
Vector Time (GMT): 2014/233/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 927460
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3648639
45 A = 6799753
21 meter
Y = 5484522
69 meter E =
0012647
Z = -1667075
28 I = 51
91197
XDOT = -4857
986769 Wp = 38
15276
YDOT = -1499
574408 meter/sec RA = 135
07477 deg
ZDOT = 5731
800336 TA = 303
68464
MA = 303
80517
Ha = 228
716 n
mi
Hp = 219
714
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11970601
87 X = -3701599
49
Y = 17993840
84 feet Y = 5443425
10 meter
Z = -5469407
08 Z = -1684928
29
XDOT = -15938
276800 XDOT = -4868
699908
YDOT = -4919
863543 feet/sec YDOT = -1553
959353 meter/sec
ZDOT = 18805
119214 ZDOT = 5708
175319
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21500339
66 X = 6553303
53
Y = -1990759
26 feet Y = -606783
42 meter
Z = -5546197
20 Z = -1690480
91
XDOT = 6095
991979 XDOT = 1858
058355
YDOT = 14021
992392 feet/sec YDOT = 4273
903281 meter/sec
ZDOT = 18704
855047 ZDOT = 5701
239818
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 14233
44775885
00016717 00000-0 10270-3 0 9109
2 25544 51
6454 136
1056 0004955 37
3602 322
7893 15
50134842 21452
Satellite: ISS
Catalog Number: 25544
Epoch time: 14233
44775885 = yrday
fracday
Element set: 910
Inclination: 51
6454 deg
RA of node: 136
1056 deg
Eccentricity:
0004955
Arg of perigee: 37
3602 deg
Mean anomaly: 322
7893 deg
Mean motion: 15
50134842 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2145
Checksum: 305
Coasting Arc #12 (Orbit 2160)
---------------------------------------
Vector Time (GMT): 2014/234/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 927460
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3499727
52 A = 6800226
11 meter
Y = -5686120
66 meter E =
0015469
Z = 1264525
01 I = 51
93592
XDOT = 4681
487493 Wp = 102
82840
YDOT = 1565
727256 meter/sec RA = 130
14067 deg
ZDOT = -5859
109273 TA = 63
50048
MA = 63
34193
Ha = 228
771 n
mi
Hp = 219
600
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11482045
67 X = 3556908
38
Y = -18655251
50 feet Y = -5646664
69 meter
Z = 4148704
11 Z = 1281664
95
XDOT = 15359
210934 XDOT = 4692
092388
YDOT = 5136
900445 feet/sec YDOT = 1618
137790 meter/sec
ZDOT = -19222
799451 ZDOT = -5836
341968
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21663279
94 X = -6602967
72
Y = 3152824
13 feet Y = 960980
79 meter
Z = 4222502
74 Z = 1287018
84
XDOT = -5742
622145 XDOT = -1750
351230
YDOT = -13596
818112 feet/sec YDOT = -4144
310160 meter/sec
ZDOT = -19126
185421 ZDOT = -5829
661316
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 14234
47923416
00016717 00000-0 10270-3 0 9119
2 25544 51
6462 130
9942 0004942 41
9932 318
1597 15
50148513 21618
Satellite: ISS
Catalog Number: 25544
Epoch time: 14234
47923416 = yrday
fracday
Element set: 911
Inclination: 51
6462 deg
RA of node: 130
9942 deg
Eccentricity:
0004942
Arg of perigee: 41
9932 deg
Mean anomaly: 318
1597 deg
Mean motion: 15
50148513 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2161
Checksum: 301
Coasting Arc #13 (Orbit 2175)
---------------------------------------
Vector Time (GMT): 2014/235/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 927460
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3283820
54 A = 6800528
58 meter
Y = 5878903
96 meter E =
0014894
Z = -902705
62 I = 51
95645
XDOT = -4544
393953 Wp = 40
99416
YDOT = -1635
012096 meter/sec RA = 125
20807 deg
ZDOT = 5949
725414 TA = 309
29304
MA = 309
42503
Ha = 228
782 n
mi
Hp = 219
546
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10773689
42 X = -3344930
76
Y = 19287742
66 feet Y = 5841840
43 meter
Z = -2961632
62 Z = -918806
36
XDOT = -14909
428980 XDOT = -4554
674442
YDOT = -5364
212915 feet/sec YDOT = -1685
887656 meter/sec
ZDOT = 19520
096502 ZDOT = 5927
624903
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21626425
19 X = 6591734
40
Y = -4468908
23 feet Y = -1362123
23 meter
Z = -3031049
49 Z = -923863
88
XDOT = 5442
036276 XDOT = 1658
732657
YDOT = 13304
144306 feet/sec YDOT = 4055
103184 meter/sec
ZDOT = 19426
322885 ZDOT = 5921
143215
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 14235
44623485
00016717 00000-0 10270-3 0 9121
2 25544 51
6462 126
2028 0004972 44
0355 316
1191 15
50159641 21765
Satellite: ISS
Catalog Number: 25544
Epoch time: 14235
44623485 = yrday
fracday
Element set: 912
Inclination: 51
6462 deg
RA of node: 126
2028 deg
Eccentricity:
0004972
Arg of perigee: 44
0355 deg
Mean anomaly: 316
1191 deg
Mean motion: 15
50159641 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2176
Checksum: 290
Coasting Arc #14 (Orbit 2191)
---------------------------------------
Vector Time (GMT): 2014/236/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 927460
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3088766
18 A = 6800784
06 meter
Y = -6035058
45 meter E =
0014534
Z = 479931
58 I = 51
97492
XDOT = 4409
669789 Wp = 110
31139
YDOT = 1767
669089 meter/sec RA = 120
27694 deg
ZDOT = -6009
543460 TA = 64
54563
MA = 64
39532
Ha = 228
831 n
mi
Hp = 219
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10133747
30 X = 3153690
72
Y = -19800060
54 feet Y = -6000154
83 meter
Z = 1574578
69 Z = 495094
17
XDOT = 14467
420569 XDOT = 4418
767481
YDOT = 5799
439270 feet/sec YDOT = 1817
031365 meter/sec
ZDOT = -19716
349934 ZDOT = -5988
100302
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21507575
04 X = -6555508
87
Y = 5652346
83 feet Y = 1722835
31 meter
Z = 1640036
80 Z = 499883
22
XDOT = -4992
635127 XDOT = -1521
755187
YDOT = -13172
957422 feet/sec YDOT = -4015
117422 meter/sec
ZDOT = -19625
388509 ZDOT = -5981
818418
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 14236
47769572
00016717 00000-0 10270-3 0 9134
2 25544 51
6466 121
0913 0004912 48
8162 311
3412 15
50159783 21925
Satellite: ISS
Catalog Number: 25544
Epoch time: 14236
47769572 = yrday
fracday
Element set: 913
Inclination: 51
6466 deg
RA of node: 121
0913 deg
Eccentricity:
0004912
Arg of perigee: 48
8162 deg
Mean anomaly: 311
3412 deg
Mean motion: 15
50159783 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2192
Checksum: 303
Coasting Arc #15 (Orbit 2206)
---------------------------------------
Vector Time (GMT): 2014/237/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 927460
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2834251
21 A = 6800811
18 meter
Y = 6172712
86 meter E =
0016798
Z = -103752
97 I = 51
99014
XDOT = -4324
238315 Wp = 46
46809
YDOT = -1894
470502 meter/sec RA = 115
34664 deg
ZDOT = 6037
868685 TA = 312
42118
MA = 312
56316
Ha = 228
827 n
mi
Hp = 219
400
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9298724
43 X = -2902561
26
Y = 20251682
60 feet Y = 6140636
48 meter
Z = -340396
89 Z = -117687
53
XDOT = -14187
133579 XDOT = -4332
062078
YDOT = -6215
454404 feet/sec YDOT = -1942
870211 meter/sec
ZDOT = 19809
280462 ZDOT = 6016
843628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21176697
59 X = 6454657
43
Y = -6935398
00 feet Y = -2113909
31 meter
Z = -400659
35 Z = -122120
97
XDOT = 4656
556653 XDOT = 1419
318468
YDOT = 13179
290575 feet/sec YDOT = 4017
047767 meter/sec
ZDOT = 19720
114437 ZDOT = 6010
690880
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 14237
44468245
00016717 00000-0 10270-3 0 9146
2 25544 51
6466 116
2996 0004975 50
3172 309
8417 15
50185002 22077
Satellite: ISS
Catalog Number: 25544
Epoch time: 14237
44468245 = yrday
fracday
Element set: 914
Inclination: 51
6466 deg
RA of node: 116
2996 deg
Eccentricity:
0004975
Arg of perigee: 50
3172 deg
Mean anomaly: 309
8417 deg
Mean motion: 15
50185002 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2207
Checksum: 307
Coasting Arc #16 (Orbit 2222)
---------------------------------------
Vector Time (GMT): 2014/238/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 927460
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2608523
24 A = 6800809
01 meter
Y = -6268360
77 meter E =
0013038
Z = -330103
40 I = 52
00259
XDOT = 4249
639254 Wp = 115
52870
YDOT = 2075
699646 meter/sec RA = 110
41744 deg
ZDOT = -6024
968575 TA = 68
00438
MA = 67
86590
Ha = 228
860 n
mi
Hp = 219
383
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8558147
12 X = 2680027
14
Y = -20565488
10 feet Y = -6238790
81 meter
Z = -1083016
40 Z = -317257
49
XDOT = 13942
386005 XDOT = 4255
379431
YDOT = 6810
038209 feet/sec YDOT = 2123
253412 meter/sec
ZDOT = -19766
957266 ZDOT = -6004
310950
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20774778
86 X = -6332152
60
Y = 8044078
32 feet Y = 2451835
07 meter
Z = -1027363
15 Z = -313140
29
XDOT = -4229
382565 XDOT = -1289
115806
YDOT = -13352
081487 feet/sec YDOT = -4069
714437 meter/sec
ZDOT = -19679
381645 ZDOT = -5998
275525
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 14238
47612878
00016717 00000-0 10270-3 0 9154
2 25544 51
6467 111
1880 0004856 55
2236 304
9371 15
50172241 22231
Satellite: ISS
Catalog Number: 25544
Epoch time: 14238
47612878 = yrday
fracday
Element set: 915
Inclination: 51
6467 deg
RA of node: 111
1880 deg
Eccentricity:
0004856
Arg of perigee: 55
2236 deg
Mean anomaly: 304
9371 deg
Mean motion: 15
50172241 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2223
Checksum: 299
Coasting Arc #17 (Orbit 2238)
---------------------------------------
Vector Time (GMT): 2014/239/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 927460
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2333665
68 A = 6800538
83 meter
Y = 6338563
83 meter E =
0018131
Z = 712282
73 I = 52
01188
XDOT = -4230
562903 Wp = 53
64009
YDOT = -2241
012494 meter/sec RA = 105
48830 deg
ZDOT = 5986
764361 TA = 314
00649
MA = 314
15579
Ha = 228
846 n
mi
Hp = 219
278
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7656383
48 X = -2407831
53
Y = 20795813
08 feet Y = 6312052
66 meter
Z = 2336885
61 Z = 700765
46
XDOT = -13879
799550 XDOT = -4234
270445
YDOT = -7352
403196 feet/sec YDOT = -2288
341521 meter/sec
ZDOT = 19641
615359 ZDOT = 5966
204311
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20167532
00 X = 6147063
75
Y = -9197172
42 feet Y = -2803298
16 meter
Z = 2286866
14 Z = 697036
80
XDOT = 3970
584085 XDOT = 1210
234029
YDOT = 13648
247865 feet/sec YDOT = 4159
985949 meter/sec
ZDOT = 19554
481269 ZDOT = 5960
205891
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 14239
50756633
00016717 00000-0 10270-3 0 9168
2 25544 51
6465 106
0762 0004950 56
4263 303
7360 15
50211783 22396
Satellite: ISS
Catalog Number: 25544
Epoch time: 14239
50756633 = yrday
fracday
Element set: 916
Inclination: 51
6465 deg
RA of node: 106
0762 deg
Eccentricity:
0004950
Arg of perigee: 56
4263 deg
Mean anomaly: 303
7360 deg
Mean motion: 15
50211783 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2239
Checksum: 298
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