[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 6th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 10763 91 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 124 9 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 730 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
226/10:19:30
000 0
0 0
0 0
0
N/A 0
0 0
0 219
8
000/00:00:00
000 0
0 0
0 212
7
Coasting Arc #1 (Orbit 3571)
---------------------------------------
Vector Time (GMT): 2015/217/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -822797
74 A = 6775970
43 meter
Y = -4438635
82 meter E =
0005550
Z = 5049315
02 I = 51
51299
XDOT = 7418
175658 Wp = 111
07975
YDOT = 709
253354 meter/sec RA = 196
71244 deg
ZDOT = 1828
703177 TA = 321
17383
MA = 321
21369
Ha = 219
894 n
mi
Hp = 213
073
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2699467
65 X = -797630
11
Y = -14562453
48 feet Y = -4447696
10 meter
Z = 16565994
18 Z = 5045379
26
XDOT = 24337
846648 XDOT = 7400
810221
YDOT = 2326
946698 feet/sec YDOT = 792
111193 meter/sec
ZDOT = 5999
682339 ZDOT = 1864
696668
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8760843
26 X = -2670305
03
Y = 11963976
16 feet Y = 3646619
93 meter
Z = 16549780
65 Z = 5044373
14
XDOT = -13957
347605 XDOT = -4254
199550
YDOT = -18750
353379 feet/sec YDOT = -5715
107710 meter/sec
ZDOT = 6154
526650 ZDOT = 1875
899723
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 15217
55146384
00016717 00000-0 10270-3 0 9009
2 25544 51
6401 197
5570 0001331 25
5903 334
5316 15
55001750 35726
Satellite: ISS
Catalog Number: 25544
Epoch time: 15217
55146384 = yrday
fracday
Element set: 900
Inclination: 51
6401 deg
RA of node: 197
5570 deg
Eccentricity:
0001331
Arg of perigee: 25
5903 deg
Mean anomaly: 334
5316 deg
Mean motion: 15
55001750 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3572
Checksum: 279
Coasting Arc #2 (Orbit 3586)
---------------------------------------
Vector Time (GMT): 2015/218/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1321214
17 A = 6774853
82 meter
Y = 4025514
70 meter E =
0015520
Z = -5300026
75 I = 51
54021
XDOT = -7412
761678 Wp = 88
93350
YDOT = -1877
669110 meter/sec RA = 191
69533 deg
ZDOT = 423
101230 TA = 185
10428
MA = 185
12012
Ha = 219
928 n
mi
Hp = 212
948
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4334692
17 X = -1340384
93
Y = 13207069
23 feet Y = 4010632
82 meter
Z = -17388539
20 Z = -5306491
46
XDOT = -24320
084245 XDOT = -7393
269447
YDOT = -6160
331726 feet/sec YDOT = -1960
454491 meter/sec
ZDOT = 1388
127395 ZDOT = 387
139122
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12447424
54 X = 3793975
00
Y = -6106225
61 feet Y = -1861177
57 meter
Z = -17417036
50 Z = -5308712
72
XDOT = 11972
993790 XDOT = 3649
368507
YDOT = 20900
757701 feet/sec YDOT = 6370
550947 meter/sec
ZDOT = 1233
593967 ZDOT = 375
999441
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 15218
51544565
00016717 00000-0 10270-3 0 9010
2 25544 51
6402 192
7446 0001371 31
8972 328
2264 15
55004942 35870
Satellite: ISS
Catalog Number: 25544
Epoch time: 15218
51544565 = yrday
fracday
Element set: 901
Inclination: 51
6402 deg
RA of node: 192
7446 deg
Eccentricity:
0001371
Arg of perigee: 31
8972 deg
Mean anomaly: 328
2264 deg
Mean motion: 15
55004942 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3587
Checksum: 304
Coasting Arc #3 (Orbit 3602)
---------------------------------------
Vector Time (GMT): 2015/219/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3385347
27 A = 6776914
04 meter
Y = -3414144
45 meter E =
0008592
Z = 4771711
22 I = 51
57877
XDOT = 6611
659752 Wp = 56
69438
YDOT = 2872
781552 meter/sec RA = 186
68245 deg
ZDOT = -2627
213805 TA = 59
26383
MA = 59
17923
Ha = 219
773 n
mi
Hp = 212
964
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11106782
37 X = 3400094
45
Y = -11201261
33 feet Y = -3376204
89 meter
Z = 15655220
54 Z = 4788192
22
XDOT = 21691
797086 XDOT = 6591
806140
YDOT = 9425
136324 feet/sec YDOT = 2946
606500 meter/sec
ZDOT = -8619
467863 ZDOT = -2595
144090
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15702699
48 X = -4786182
80
Y = 96277
32 feet Y = 29345
33 meter
Z = 15726753
00 Z = 4793514
31
XDOT = -8649
388874 XDOT = -2636
333729
YDOT = -20918
200700 feet/sec YDOT = -6375
867573 meter/sec
ZDOT = -8481
841223 ZDOT = -2585
265205
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 15219
54368098
00016717 00000-0 10270-3 0 9020
2 25544 51
6400 187
6116 0001383 29
8782 330
2450 15
55039451 36036
Satellite: ISS
Catalog Number: 25544
Epoch time: 15219
54368098 = yrday
fracday
Element set: 902
Inclination: 51
6400 deg
RA of node: 187
6116 deg
Eccentricity:
0001383
Arg of perigee: 29
8782 deg
Mean anomaly: 330
2450 deg
Mean motion: 15
55039451 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3603
Checksum: 300
Coasting Arc #4 (Orbit 3617)
---------------------------------------
Vector Time (GMT): 2015/220/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5099323
02 A = 6781160
74 meter
Y = 2685221
90 meter E =
0006165
Z = -3578532
20 I = 51
62474
XDOT = -5048
565663 Wp = 86
18531
YDOT = -3670
966486 meter/sec RA = 181
68261 deg
ZDOT = 4446
518923 TA = 231
52471
MA = 231
58003
Ha = 219
878 n
mi
Hp = 212
850
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16730062
39 X = -5111587
82
Y = 8809783
12 feet Y = 2628129
43 meter
Z = -11740591
21 Z = -3603333
21
XDOT = -16563
535640 XDOT = -5028
740124
YDOT = -12043
853299 feet/sec YDOT = -3727
312122 meter/sec
ZDOT = 14588
316677 ZDOT = 4422
042270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18084732
49 X = 5512226
46
Y = 5283913
98 feet Y = 1610536
98 meter
Z = -11847845
88 Z = -3611223
42
XDOT = 3944
392011 XDOT = 1202
250685
YDOT = 18924
390072 feet/sec YDOT = 5768
154094 meter/sec
ZDOT = 14483
505175 ZDOT = 4414
572377
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 15220
50764084
00016717 00000-0 10270-3 0 9034
2 25544 51
6401 182
7993 0001454 33
6703 326
4543 15
55035267 36188
Satellite: ISS
Catalog Number: 25544
Epoch time: 15220
50764084 = yrday
fracday
Element set: 903
Inclination: 51
6401 deg
RA of node: 182
7993 deg
Eccentricity:
0001454
Arg of perigee: 33
6703 deg
Mean anomaly: 326
4543 deg
Mean motion: 15
55035267 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3618
Checksum: 296
Coasting Arc #5 (Orbit 3633)
---------------------------------------
Vector Time (GMT): 2015/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6270507
31 A = 6785102
71 meter
Y = -1811867
29 meter E =
0014332
Z = 1831256
05 I = 51
67050
XDOT = 2902
527460 Wp = 108
22800
YDOT = 4304
874679 meter/sec RA = 176
69877 deg
ZDOT = -5647
530428 TA = 51
62938
MA = 51
50070
Ha = 219
837 n
mi
Hp = 212
826
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20572530
56 X = 6281406
57
Y = -5944446
48 feet Y = -1741685
47 meter
Z = 6008057
90 Z = 1861742
99
XDOT = 9522
727888 XDOT = 2881
606833
YDOT = 14123
604590 feet/sec YDOT = 4337
215846 meter/sec
ZDOT = -18528
643135 ZDOT = -5633
481370
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19041491
32 X = -5803846
56
Y = -9715359
48 feet Y = -2961241
57 meter
Z = 6139675
53 Z = 1871373
10
XDOT = 1923
714360 XDOT = 586
348137
YDOT = -15506
528211 feet/sec YDOT = -4726
389799 meter/sec
ZDOT = -18468
837167 ZDOT = -5629
301569
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 15221
53585293
00016717 00000-0 10270-3 0 9042
2 25544 51
6405 177
6657 0001445 35
5455 324
5795 15
55072604 36349
Satellite: ISS
Catalog Number: 25544
Epoch time: 15221
53585293 = yrday
fracday
Element set: 904
Inclination: 51
6405 deg
RA of node: 177
6657 deg
Eccentricity:
0001445
Arg of perigee: 35
5455 deg
Mean anomaly: 324
5795 deg
Mean motion: 15
55072604 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3634
Checksum: 315
Coasting Arc #6 (Orbit 3649)
---------------------------------------
Vector Time (GMT): 2015/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6723977
43 A = 6786505
13 meter
Y = 855200
20 meter E =
0013705
Z = 153576
80 I = 51
70709
XDOT = -457
344338 Wp = 46
31887
YDOT = -4735
128085 meter/sec RA = 171
72662 deg
ZDOT = 6018
174110 TA = 315
33498
MA = 315
44530
Ha = 219
816 n
mi
Hp = 212
827
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22060293
41 X = -6733786
75
Y = 2805774
94 feet Y = 779953
42 meter
Z = 503860
91 Z = 120889
75
XDOT = -1500
473550 XDOT = -433
594571
YDOT = -15535
197128 feet/sec YDOT = -4740
109793 meter/sec
ZDOT = 19744
665716 ZDOT = 6016
010002
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18231347
62 X = 5556914
75
Y = 12738487
31 feet Y = 3882690
93 meter
Z = 362903
84 Z = 110613
09
XDOT = -8298
181205 XDOT = -2529
285631
YDOT = 11271
816919 feet/sec YDOT = 3435
649797 meter/sec
ZDOT = 19736
122274 ZDOT = 6015
570069
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 15222
56405204
00016717 00000-0 10270-3 0 9050
2 25544 51
6406 172
5325 0001387 39
7560 320
3694 15
55099698 36506
Satellite: ISS
Catalog Number: 25544
Epoch time: 15222
56405204 = yrday
fracday
Element set: 905
Inclination: 51
6406 deg
RA of node: 172
5325 deg
Eccentricity:
0001387
Arg of perigee: 39
7560 deg
Mean anomaly: 320
3694 deg
Mean motion: 15
55099698 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3650
Checksum: 310
Coasting Arc #7 (Orbit 3664)
---------------------------------------
Vector Time (GMT): 2015/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6426021
67 A = 6784552
01 meter
Y = 238307
51 meter E =
0006299
Z = -2160452
76 I = 51
73316
XDOT = -2028
183805 Wp = 125
88440
YDOT = 4936
723385 meter/sec RA = 166
75570 deg
ZDOT = -5502
891914 TA = 78
04657
MA = 77
97596
Ha = 219
849 n
mi
Hp = 212
822
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21082748
25 X = 6433373
73
Y = 781848
79 feet Y = 310208
66 meter
Z = -7088099
59 Z = -2129219
12
XDOT = -6654
146341 XDOT = -2056
506219
YDOT = 16196
599033 feet/sec YDOT = 4913
884660 meter/sec
ZDOT = -18054
107330 ZDOT = -5512
812936
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15380968
23 X = -4688119
12
Y = -14505463
40 feet Y = -4421265
24 meter
Z = -6953564
92 Z = -2119446
59
XDOT = 14530
229031 XDOT = 4428
813809
YDOT = -6755
427745 feet/sec YDOT = -2059
054377 meter/sec
ZDOT = -18097
665401 ZDOT = -5516
168414
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 15223
52797805
00016717 00000-0 10270-3 0 9069
2 25544 51
6418 167
7198 0001446 38
9177 321
2080 15
55115167 36659
Satellite: ISS
Catalog Number: 25544
Epoch time: 15223
52797805 = yrday
fracday
Element set: 906
Inclination: 51
6418 deg
RA of node: 167
7198 deg
Eccentricity:
0001446
Arg of perigee: 38
9177 deg
Mean anomaly: 321
2080 deg
Mean motion: 15
55115167 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3665
Checksum: 322
Coasting Arc #8 (Orbit 3680)
---------------------------------------
Vector Time (GMT): 2015/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5419372
28 A = 6780291
03 meter
Y = -1387062
80 meter E =
0012371
Z = 3821055
75 I = 51
75036
XDOT = 4206
865030 Wp = 92
40383
YDOT = -4862
048187 meter/sec RA = 161
77681 deg
ZDOT = 4189
416788 TA = 313
50399
MA = 313
60675
Ha = 219
887 n
mi
Hp = 212
744
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17780092
78 X = -5422019
90
Y = -4550730
96 feet Y = -1447680
61 meter
Z = 12536272
15 Z = 3794723
61
XDOT = 13802
050624 XDOT = 4240
570777
YDOT = -15951
601663 feet/sec YDOT = -4814
815833 meter/sec
ZDOT = 13744
805734 ZDOT = 4209
934317
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10699661
33 X = 3261256
77
Y = 15006150
38 feet Y = 4573874
64 meter
Z = 12423029
79 Z = 3786539
48
XDOT = -19676
871089 XDOT = -5997
510308
YDOT = 2543
874394 feet/sec YDOT = 775
372915 meter/sec
ZDOT = 13834
018748 ZDOT = 4216
608914
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 15224
55615309
00016717 00000-0 10270-3 0 9072
2 25544 51
6422 162
5869 0001354 44
1091 316
0170 15
55142379 36819
Satellite: ISS
Catalog Number: 25544
Epoch time: 15224
55615309 = yrday
fracday
Element set: 907
Inclination: 51
6422 deg
RA of node: 162
5869 deg
Eccentricity:
0001354
Arg of perigee: 44
1091 deg
Mean anomaly: 316
0170 deg
Mean motion: 15
55142379 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3681
Checksum: 295
Coasting Arc #9 (Orbit 3695)
---------------------------------------
Vector Time (GMT): 2015/225/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 906095
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3851110
55 A = 6776068
69 meter
Y = 2590995
83 meter E =
0013505
Z = -4949217
73 I = 51
76697
XDOT = -5842
908495 Wp = 70
94537
YDOT = 4420
445073 meter/sec RA = 156
78448 deg
ZDOT = -2233
014967 TA = 177
27168
MA = 177
26430
Ha = 219
793 n
mi
Hp = 212
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12634877
14 X = 3845892
11
Y = 8500642
48 feet Y = 2634032
26 meter
Z = -16237590
97 Z = -4930522
89
XDOT = -19169
647293 XDOT = -5881
057812
YDOT = 14502
772550 feet/sec YDOT = 4354
892508 meter/sec
ZDOT = -7326
164591 ZDOT = -2261
490753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4491183
96 X = -1368912
87
Y = -14639896
85 feet Y = -4462240
56 meter
Z = -16157446
89 Z = -4924789
81
XDOT = 22916
591194 XDOT = 6984
976996
YDOT = 1189
085399 feet/sec YDOT = 362
433230 meter/sec
ZDOT = -7449
612883 ZDOT = -2270
642007
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 15225
52005683
00016717 00000-0 10270-3 0 9089
2 25544 51
6428 157
7740 0001460 45
1455 314
9817 15
55157710 36968
Satellite: ISS
Catalog Number: 25544
Epoch time: 15225
52005683 = yrday
fracday
Element set: 908
Inclination: 51
6428 deg
RA of node: 157
7740 deg
Eccentricity:
0001460
Arg of perigee: 45
1455 deg
Mean anomaly: 314
9817 deg
Mean motion: 15
55157710 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3696
Checksum: 311
Coasting Arc #10 (Orbit 3710)
---------------------------------------
Vector Time (GMT): 2015/226/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4731750
53 A = 6777406
30 meter
Y = -1578522
74 meter E =
0009271
Z = 4581938
08 I = 51
79815
XDOT = 4716
786811 Wp = 106
62279
YDOT = -5219
629845 meter/sec RA = 152
15493 deg
ZDOT = 3065
081315 TA = 312
78926
MA = 312
86719
Ha = 219
803 n
mi
Hp = 212
651
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15524115
92 X = -4736004
29
Y = -5178880
39 feet Y = -1631459
96 meter
Z = 15032605
25 Z = 4558942
37
XDOT = 15475
022346 XDOT = 4759
914720
YDOT = -17124
769834 feet/sec YDOT = -5166
642417 meter/sec
ZDOT = 10056
041060 ZDOT = 3088
098930
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2352593
87 X = 717070
61
Y = 16286394
08 feet Y = 4964092
91 meter
Z = 14933749
29 Z = 4551806
78
XDOT = -21019
534608 XDOT = -6406
754148
YDOT = -6299
659539 feet/sec YDOT = -1920
136228 meter/sec
ZDOT = 10156
106996 ZDOT = 3095
581412
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 15226
48394760
00016717 00000-0 10270-3 0 9093
2 25544 51
6422 152
9616 0001250 47
7096 312
4163 15
55199688 37112
Satellite: ISS
Catalog Number: 25544
Epoch time: 15226
48394760 = yrday
fracday
Element set: 909
Inclination: 51
6422 deg
RA of node: 152
9616 deg
Eccentricity:
0001250
Arg of perigee: 47
7096 deg
Mean anomaly: 312
4163 deg
Mean motion: 15
55199688 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3711
Checksum: 319
Coasting Arc #11 (Orbit 3725)
---------------------------------------
Vector Time (GMT): 2015/227/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3064372
20 A = 6774570
03 meter
Y = 2963370
90 meter E =
0015628
Z = -5278862
47 I = 51
81643
XDOT = -6002
810020 Wp = 80
60443
YDOT = 4678
026027 meter/sec RA = 147
15867 deg
ZDOT = -858
218616 TA = 181
19751
MA = 181
20126
Ha = 219
754 n
mi
Hp = 212
717
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10053714
57 X = 3056649
54
Y = 9722345
46 feet Y = 2997595
32 meter
Z = -17319102
60 Z = -5263995
53
XDOT = -19694
258596 XDOT = -6050
505877
YDOT = 15347
854420 feet/sec YDOT = 4610
631942 meter/sec
ZDOT = -2815
677874 ZDOT = -887
494544
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3918802
20 X = 1194450
91
Y = -13507148
13 feet Y = -4116978
75 meter
Z = -17255504
38 Z = -5259477
73
XDOT = 21721
832443 XDOT = 6620
814528
YDOT = 10062
718503 feet/sec YDOT = 3067
116600 meter/sec
ZDOT = -2942
641701 ZDOT = -896
917191
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 15227
44783009
00016717 00000-0 10270-3 0 9100
2 25544 51
6424 148
1484 0001383 48
7425 311
3848 15
55178014 37262
Satellite: ISS
Catalog Number: 25544
Epoch time: 15227
44783009 = yrday
fracday
Element set: 910
Inclination: 51
6424 deg
RA of node: 148
1484 deg
Eccentricity:
0001383
Arg of perigee: 48
7425 deg
Mean anomaly: 311
3848 deg
Mean motion: 15
55178014 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3726
Checksum: 306
Coasting Arc #12 (Orbit 3741)
---------------------------------------
Vector Time (GMT): 2015/228/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1172772
61 A = 6774904
40 meter
Y = -4224222
73 meter E =
0005957
Z = 5161841
19 I = 51
84458
XDOT = 6588
328000 Wp = 54
37960
YDOT = -3644
312011 meter/sec RA = 142
16134 deg
ZDOT = -1480
890104 TA = 49
85378
MA = 49
80162
Ha = 219
775 n
mi
Hp = 212
574
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3847679
17 X = -1150523
01
Y = -13858998
47 feet Y = -4237212
76 meter
Z = 16935174
52 Z = 5156198
47
XDOT = 21615
249345 XDOT = 6635
783401
YDOT = -11956
404237 feet/sec YDOT = -3570
371740 meter/sec
ZDOT = -4858
563333 ZDOT = -1448
770402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10285457
43 X = -3135007
43
Y = 10093841
80 feet Y = 3076602
98 meter
Z = 16911544
36 Z = 5154638
72
XDOT = -20107
231788 XDOT = -6128
684249
YDOT = -12556
512129 feet/sec YDOT = -3827
224897 meter/sec
ZDOT = -4719
498267 ZDOT = -1438
503072
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 15228
47595774
00016717 00000-0 10270-3 0 9115
2 25544 51
6429 143
0156 0001400 51
1898 308
9381 15
55203001 37426
Satellite: ISS
Catalog Number: 25544
Epoch time: 15228
47595774 = yrday
fracday
Element set: 911
Inclination: 51
6429 deg
RA of node: 143
0156 deg
Eccentricity:
0001400
Arg of perigee: 51
1898 deg
Mean anomaly: 308
9381 deg
Mean motion: 15
55203001 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3742
Checksum: 295
Coasting Arc #13 (Orbit 3756)
---------------------------------------
Vector Time (GMT): 2015/229/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -679654
35 A = 6778356
75 meter
Y = 5215009
98 meter E =
0009203
Z = -4285514
55 I = 51
88074
XDOT = -6428
123278 Wp = 103
42385
YDOT = 2112
605310 meter/sec RA = 137
17132 deg
ZDOT = 3594
665930 TA = 203
16370
MA = 203
20521
Ha = 219
703 n
mi
Hp = 212
538
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -2229837
10 X = -717102
22
Y = 17109612
81 feet Y = 5207199
99 meter
Z = -14060087
11 Z = -4288907
42
XDOT = -21089
643300 XDOT = -6468
730471
YDOT = 6931
119782 feet/sec YDOT = 2040
494991 meter/sec
ZDOT = 11793
523394 ZDOT = 3563
341059
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15942405
32 X = 4859245
14
Y = -6566197
00 feet Y = -2001376
85 meter
Z = -14075576
12 Z = -4290235
60
XDOT = 15980
562834 XDOT = 4870
875552
YDOT = 13840
050180 feet/sec YDOT = 4218
447295 meter/sec
ZDOT = 11658
125676 ZDOT = 3553
396706
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 15229
43981547
00016717 00000-0 10270-3 0 9120
2 25544 51
6427 138
2025 0001373 52
6424 307
4854 15
55219169 37572
Satellite: ISS
Catalog Number: 25544
Epoch time: 15229
43981547 = yrday
fracday
Element set: 912
Inclination: 51
6427 deg
RA of node: 138
2025 deg
Eccentricity:
0001373
Arg of perigee: 52
6424 deg
Mean anomaly: 307
4854 deg
Mean motion: 15
55219169 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3757
Checksum: 316
Coasting Arc #14 (Orbit 3772)
---------------------------------------
Vector Time (GMT): 2015/230/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2331702
55 A = 6782904
66 meter
Y = -5750198
09 meter E =
0014492
Z = 2724663
26 I = 51
91923
XDOT = 5649
435784 Wp = 97
39771
YDOT = -178
081009 meter/sec RA = 132
19747 deg
ZDOT = -5188
739748 TA = 51
88654
MA = 51
75597
Ha = 219
672 n
mi
Hp = 212
480
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7649942
76 X = 2382594
12
Y = -18865479
31 feet Y = -5723838
73 meter
Z = 8939183
92 Z = 2736114
09
XDOT = 18534
894303 XDOT = 5676
211914
YDOT = -584
255280 feet/sec YDOT = -114
755944 meter/sec
ZDOT = -17023
424369 ZDOT = -5161
231159
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20107908
25 X = -6128890
43
Y = 3032768
20 feet Y = 924387
75 meter
Z = 8989509
78 Z = 2740002
58
XDOT = -9745
964294 XDOT = -2970
569917
YDOT = -14299
660331 feet/sec YDOT = -4358
536469 meter/sec
ZDOT = -16904
791180 ZDOT = -5152
580352
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 15230
46791824
00016717 00000-0 10270-3 0 9133
2 25544 51
6431 133
0687 0001390 55
6816 304
4469 15
55243325 37739
Satellite: ISS
Catalog Number: 25544
Epoch time: 15230
46791824 = yrday
fracday
Element set: 913
Inclination: 51
6431 deg
RA of node: 133
0687 deg
Eccentricity:
0001390
Arg of perigee: 55
6816 deg
Mean anomaly: 304
4469 deg
Mean motion: 15
55243325 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3773
Checksum: 306
Coasting Arc #15 (Orbit 3787)
---------------------------------------
Vector Time (GMT): 2015/231/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3576710
25 A = 6785806
16 meter
Y = 5708314
18 meter E =
0011619
Z = -775136
56 I = 51
94919
XDOT = -4393
950524 Wp = 41
79818
YDOT = -1949
709951 meter/sec RA = 127
23780 deg
ZDOT = 5976
605812 TA = 309
85483
MA = 309
95699
Ha = 219
664 n
mi
Hp = 212
496
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11734613
67 X = -3636510
88
Y = 18728064
90 feet Y = 5667982
64 meter
Z = -2543098
97 Z = -792657
01
XDOT = -14415
848176 XDOT = -4400
853695
YDOT = -6396
686191 feet/sec YDOT = -1998
884188 meter/sec
ZDOT = 19608
286785 ZDOT = 5955
244402
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 22090767
40 X = 6733265
90
Y = 211240
65 feet Y = 64386
15 meter
Z = -2619598
95 Z = -798453
76
XDOT = 2156
641688 XDOT = 657
344387
YDOT = 14128
881232 feet/sec YDOT = 4306
482999 meter/sec
ZDOT = 19516
507592 ZDOT = 5948
631514
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 15231
43175294
00016717 00000-0 10270-3 0 9149
2 25544 51
6426 128
2557 0001373 55
8498 304
2785 15
55247081 37882
Satellite: ISS
Catalog Number: 25544
Epoch time: 15231
43175294 = yrday
fracday
Element set: 914
Inclination: 51
6426 deg
RA of node: 128
2557 deg
Eccentricity:
0001373
Arg of perigee: 55
8498 deg
Mean anomaly: 304
2785 deg
Mean motion: 15
55247081 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3788
Checksum: 325
Coasting Arc #16 (Orbit 3803)
---------------------------------------
Vector Time (GMT): 2015/232/10:19:30
000
Vector Time (MET): N/A
Weight (LBS) : 890969
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4392336
33 A = 6785292
25 meter
Y = -4991216
80 meter E =
0009168
Z = -1339101
78 I = 51
96693
XDOT = 2843
831569 Wp = 134
41838
YDOT = 4063
333935 meter/sec RA = 122
28377 deg
ZDOT = -5848
122538 TA = 60
09896
MA = 60
00791
Ha = 219
674 n
mi
Hp = 212
476
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14410552
25 X = 4454327
69
Y = -16375383
22 feet Y = -4941752
28 meter
Z = -4393378
55 Z = -1317613
91
XDOT = 9330
156066 XDOT = 2826
590847
YDOT = 13331
148080 feet/sec YDOT = 4095
038764 meter/sec
ZDOT = -19186
753733 ZDOT = -5834
349970
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21567235
16 X = -6573693
28
Y = -3388860
68 feet Y = -1032924
74 meter
Z = -4299878
77 Z = -1310603
05
XDOT = 5923
363743 XDOT = 1805
441269
YDOT = -13558
240324 feet/sec YDOT = -4132
551651 meter/sec
ZDOT = -19128
052422 ZDOT = -5830
230378
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 15232
45983123
00016717 00000-0 10270-3 0 9151
2 25544 51
6434 123
1213 0001316 61
9129 298
2157 15
55265841 38048
Satellite: ISS
Catalog Number: 25544
Epoch time: 15232
45983123 = yrday
fracday
Element set: 915
Inclination: 51
6434 deg
RA of node: 123
1213 deg
Eccentricity:
0001316
Arg of perigee: 61
9129 deg
Mean anomaly: 298
2157 deg
Mean motion: 15
55265841 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3804
Checksum: 293
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