[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
March 12th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 11840 3 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 130 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 315 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
077/23:46:39
036 -2
3 2
3 2
3
N/A 0
1 0
0 222
3
000/00:05:14
073 0
2 -0
0 211
3
Coasting Arc #1 (Orbit 1283)
---------------------------------------
Vector Time (GMT): 2015/070/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905416
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 364651
78 A = 6775757
10 meter
Y = -4482194
72 meter E =
0013451
Z = 5057984
67 I = 51
43497
XDOT = 7019
286099 Wp = 104
97938
YDOT = 2566
925823 meter/sec RA = 210
91708 deg
ZDOT = 1761
330713 TA = 327
92039
MA = 328
00218
Ha = 222
677 n
mi
Hp = 210
095
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1196364
12 X = 390175
86
Y = -14705363
26 feet Y = -4477973
64 meter
Z = 16594437
90 Z = 5059818
60
XDOT = 23029
153868 XDOT = 6981
504559
YDOT = 8421
672646 feet/sec YDOT = 2645
209018 meter/sec
ZDOT = 5778
644072 ZDOT = 1795
336944
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4125167
61 X = 1257351
09
Y = -14155504
36 feet Y = -4314597
73 meter
Z = 16602983
27 Z = 5060589
30
XDOT = 19705
606572 XDOT = 6006
268883
YDOT = 12718
780161 feet/sec YDOT = 3876
684193 meter/sec
ZDOT = 5923
794804 ZDOT = 1805
572656
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 15070
55134688
00016717 00000-0 10270-3 0 9000
2 25544 51
6430 211
7266 0008558 92
2156 267
9977 15
55044264 12845
Satellite: ISS
Catalog Number: 25544
Epoch time: 15070
55134688 = yrday
fracday
Element set: 900
Inclination: 51
6430 deg
RA of node: 211
7266 deg
Eccentricity:
0008558
Arg of perigee: 92
2156 deg
Mean anomaly: 267
9977 deg
Mean motion: 15
55044264 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1284
Checksum: 319
Coasting Arc #2 (Orbit 1298)
---------------------------------------
Vector Time (GMT): 2015/071/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890325
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2354515
81 A = 6774716
62 meter
Y = 3543545
26 meter E =
0023498
Z = -5292662
75 I = 51
45982
XDOT = -6684
802230 Wp = 94
60798
YDOT = -3690
680743 meter/sec RA = 205
89567 deg
ZDOT = 502
928299 TA = 180
21140
MA = 180
21240
Ha = 222
721 n
mi
Hp = 209
908
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7724789
39 X = -2368255
85
Y = 11625804
65 feet Y = 3517138
14 meter
Z = -17364379
11 Z = -5304134
26
XDOT = -21931
765847 XDOT = -6645
478368
YDOT = -12108
532620 feet/sec YDOT = -3765
214638 meter/sec
ZDOT = 1650
027227 ZDOT = 470
550801
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9695693
81 X = -2955247
47
Y = 9954816
77 feet Y = 3034228
15 meter
Z = -17414032
03 Z = -5307796
96
XDOT = -18497
435984 XDOT = -5638
018488
YDOT = -15371
475533 feet/sec YDOT = -4685
225742 meter/sec
ZDOT = 1512
005607 ZDOT = 460
859309
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 15071
51531708
00016717 00000-0 10270-3 0 9012
2 25544 51
6436 206
9159 0008728 95
2937 264
9213 15
55062103 12995
Satellite: ISS
Catalog Number: 25544
Epoch time: 15071
51531708 = yrday
fracday
Element set: 901
Inclination: 51
6436 deg
RA of node: 206
9159 deg
Eccentricity:
0008728
Arg of perigee: 95
2937 deg
Mean anomaly: 264
9213 deg
Mean motion: 15
55062103 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1299
Checksum: 311
Coasting Arc #3 (Orbit 1314)
---------------------------------------
Vector Time (GMT): 2015/072/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890325
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4196204
16 A = 6777060
31 meter
Y = -2423162
56 meter E =
0015537
Z = 4725615
11 I = 51
49648
XDOT = 5635
942303 Wp = 82
10515
YDOT = 4456
525483 meter/sec RA = 200
87605 deg
ZDOT = -2709
639422 TA = 34
74730
MA = 34
64592
Ha = 222
653 n
mi
Hp = 210
042
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13767074
00 X = 4200033
50
Y = -7950008
39 feet Y = -2376216
00 meter
Z = 15503986
58 Z = 4746008
90
XDOT = 18490
624353 XDOT = 5598
851860
YDOT = 14621
146599 feet/sec YDOT = 4519
342622 meter/sec
ZDOT = -8889
893118 ZDOT = -2682
351755
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14844136
33 X = 4524492
75
Y = -5446106
80 feet Y = -1659973
35 meter
Z = 15591667
55 Z = 4752340
27
XDOT = 15319
109498 XDOT = 4669
264575
YDOT = 16545
141786 feet/sec YDOT = 5042
959216 meter/sec
ZDOT = -8773
761250 ZDOT = -2674
242429
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 15072
54353497
00016717 00000-0 10270-3 0 9024
2 25544 51
6435 201
7820 0008769 98
8843 261
3303 15
55040005 13159
Satellite: ISS
Catalog Number: 25544
Epoch time: 15072
54353497 = yrday
fracday
Element set: 902
Inclination: 51
6435 deg
RA of node: 201
7820 deg
Eccentricity:
0008769
Arg of perigee: 98
8843 deg
Mean anomaly: 261
3303 deg
Mean motion: 15
55040005 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1315
Checksum: 297
Coasting Arc #4 (Orbit 1329)
---------------------------------------
Vector Time (GMT): 2015/073/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890325
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5666668
44 A = 6781236
56 meter
Y = 1286775
05 meter E =
0013734
Z = -3509448
65 I = 51
54124
XDOT = -3879
528912 Wp = 99
56929
YDOT = -4825
304893 meter/sec RA = 195
87122 deg
ZDOT = 4507
835214 TA = 219
11565
MA = 219
21501
Ha = 222
594 n
mi
Hp = 209
984
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18591431
89 X = -5663588
84
Y = 4221702
93 feet Y = 1223423
56 meter
Z = -11513939
14 Z = -3536968
65
XDOT = -12728
113227 XDOT = -3847
180089
YDOT = -15831
052800 feet/sec YDOT = -4868
507025 meter/sec
ZDOT = 14789
485609 ZDOT = 4489
068380
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18951341
60 X = -5776368
92
Y = 1256546
88 feet Y = 382995
49 meter
Z = -11631966
79 Z = -3545423
48
XDOT = -10081
581522 XDOT = -3072
866048
YDOT = -16266
879952 feet/sec YDOT = -4958
145009 meter/sec
ZDOT = 14709
875829 ZDOT = 4483
570153
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 15073
50747039
00016717 00000-0 10270-3 0 9031
2 25544 51
6440 196
9703 0008558 101
3473 258
8642 15
55079587 13306
Satellite: ISS
Catalog Number: 25544
Epoch time: 15073
50747039 = yrday
fracday
Element set: 903
Inclination: 51
6440 deg
RA of node: 196
9703 deg
Eccentricity:
0008558
Arg of perigee: 101
3473 deg
Mean anomaly: 258
8642 deg
Mean motion: 15
55079587 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1330
Checksum: 321
Coasting Arc #5 (Orbit 1345)
---------------------------------------
Vector Time (GMT): 2015/074/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890325
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6552490
35 A = 6785163
31 meter
Y = -127738
75 meter E =
0022530
Z = 1718081
30 I = 51
58539
XDOT = 1600
306096 Wp = 111
72290
YDOT = 4900
271560 meter/sec RA = 190
88184 deg
ZDOT = -5687
280785 TA = 49
39384
MA = 49
19804
Ha = 222
539 n
mi
Hp = 209
999
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21497671
77 X = 6545086
06
Y = -419090
40 feet Y = -54505
76 meter
Z = 5636749
66 Z = 1749893
72
XDOT = 5250
348083 XDOT = 1573
017557
YDOT = 16077
006430 feet/sec YDOT = 4918
014096 meter/sec
ZDOT = -18659
057695 ZDOT = -5679
573647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21308153
58 X = 6494725
21
Y = 2594916
71 feet Y = 790930
61 meter
Z = 5772995
16 Z = 1759608
93
XDOT = 3250
636032 XDOT = 990
793863
YDOT = 15115
516618 feet/sec YDOT = 4607
209465 meter/sec
ZDOT = -18626
804969 ZDOT = -5677
450154
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 15074
53565254
00016717 00000-0 10270-3 0 9043
2 25544 51
6441 191
8367 0008642 105
5702 254
6406 15
55112264 13461
Satellite: ISS
Catalog Number: 25544
Epoch time: 15074
53565254 = yrday
fracday
Element set: 904
Inclination: 51
6441 deg
RA of node: 191
8367 deg
Eccentricity:
0008642
Arg of perigee: 105
5702 deg
Mean anomaly: 254
6406 deg
Mean motion: 15
55112264 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1346
Checksum: 298
Coasting Arc #6 (Orbit 1361)
---------------------------------------
Vector Time (GMT): 2015/075/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890325
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6714526
09 A = 6786355
64 meter
Y = -912910
63 meter E =
0018441
Z = 274535
49 I = 51
62175
XDOT = 896
065220 Wp = 72
00945
YDOT = -4687
207235 meter/sec RA = 185
90378 deg
ZDOT = 6003
383007 TA = 290
95053
MA = 291
14777
Ha = 222
496 n
mi
Hp = 210
042
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -22029285
07 X = -6705152
24
Y = -2995113
61 feet Y = -987944
40 meter
Z = 900706
99 Z = 241940
91
XDOT = 2939
846523 XDOT = 919
250261
YDOT = -15377
976492 feet/sec YDOT = -4677
056559 meter/sec
ZDOT = 19696
138473 ZDOT = 6007
792687
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21497877
48 X = -6552553
05
Y = -5686223
43 feet Y = -1733160
90 meter
Z = 761253
13 Z = 232029
95
XDOT = 4272
686561 XDOT = 1302
314864
YDOT = -13344
805222 feet/sec YDOT = -4067
496632 meter/sec
ZDOT = 19715
737952 ZDOT = 6009
356928
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 15075
56381635
00016717 00000-0 10270-3 0 9057
2 25544 51
6451 186
7036 0008612 107
8141 252
3953 15
55144393 13625
Satellite: ISS
Catalog Number: 25544
Epoch time: 15075
56381635 = yrday
fracday
Element set: 905
Inclination: 51
6451 deg
RA of node: 186
7036 deg
Eccentricity:
0008612
Arg of perigee: 107
8141 deg
Mean anomaly: 252
3953 deg
Mean motion: 15
55144393 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1362
Checksum: 306
Coasting Arc #7 (Orbit 1376)
---------------------------------------
Vector Time (GMT): 2015/076/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890325
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6084624
86 A = 6784099
87 meter
Y = 1920205
91 meter E =
0014216
Z = -2302032
08 I = 51
64621
XDOT = -3377
069178 Wp = 122
06149
YDOT = 4237
398100 meter/sec RA = 180
92670 deg
ZDOT = -5423
457990 TA = 83
58251
MA = 83
42064
Ha = 222
464 n
mi
Hp = 210
067
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19962680
00 X = 6073882
71
Y = 6299888
15 feet Y = 1988187
80 meter
Z = -7552598
69 Z = -2272500
89
XDOT = -11079
623286 XDOT = -3397
856995
YDOT = 13902
224737 feet/sec YDOT = 4199
516584 meter/sec
ZDOT = -17793
497344 ZDOT = -5439
913948
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19229040
04 X = 5861011
41
Y = 8386388
18 feet Y = 2556171
12 meter
Z = -7426401
74 Z = -2263567
25
XDOT = -11767
727783 XDOT = -3586
803428
YDOT = 11256
677614 feet/sec YDOT = 3431
035337 meter/sec
ZDOT = -17864
623665 ZDOT = -5445
137293
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 15076
52770350
00016717 00000-0 10270-3 0 9061
2 25544 51
6452 181
8912 0008584 111
6499 248
5569 15
55177716 13773
Satellite: ISS
Catalog Number: 25544
Epoch time: 15076
52770350 = yrday
fracday
Element set: 906
Inclination: 51
6452 deg
RA of node: 181
8912 deg
Eccentricity:
0008584
Arg of perigee: 111
6499 deg
Mean anomaly: 248
5569 deg
Mean motion: 15
55177716 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1377
Checksum: 338
Coasting Arc #8 (Orbit 1392)
---------------------------------------
Vector Time (GMT): 2015/077/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 890325
8
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4766917
62 A = 6779672
06 meter
Y = -2776492
54 meter E =
0019571
Z = 3929109
09 I = 51
66406
XDOT = 5444
721351 Wp = 106
41048
YDOT = -3592
920241 meter/sec RA = 175
94001 deg
ZDOT = 4044
674676 TA = 301
28697
MA = 301
47848
Ha = 222
395 n
mi
Hp = 210
027
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15639493
51 X = -4754601
85
Y = -9109227
50 feet Y = -2829729
89 meter
Z = 12890777
84 Z = 3905982
93
XDOT = 17863
259026 XDOT = 5464
846289
YDOT = -11787
796067 feet/sec YDOT = -3531
920688 meter/sec
ZDOT = 13269
930041 ZDOT = 4071
173170
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14848334
32 X = -4525772
30
Y = -10470541
43 feet Y = -3191421
03 meter
Z = 12792132
99 Z = 3899042
14
XDOT = 17993
277076 XDOT = 5484
350853
YDOT = -9075
522029 feet/sec YDOT = -2766
219114 meter/sec
ZDOT = 13383
981935 ZDOT = 4079
437694
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 15077
55583186
00016717 00000-0 10270-3 0 9075
2 25544 51
6458 176
7579 0008566 114
9977 245
2066 15
55228691 13931
Satellite: ISS
Catalog Number: 25544
Epoch time: 15077
55583186 = yrday
fracday
Element set: 907
Inclination: 51
6458 deg
RA of node: 176
7579 deg
Eccentricity:
0008566
Arg of perigee: 114
9977 deg
Mean anomaly: 245
2066 deg
Mean motion: 15
55228691 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1393
Checksum: 360
Coasting Arc #9 (Orbit 1399)
---------------------------------------
Vector Time (GMT): 2015/077/23:49:16
073
Vector Time (MET): N/A
Weight (LBS) : 890095
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1550319
43 A = 6776459
03 meter
Y = 4225006
71 meter E =
0019831
Z = -5084143
58 I = 51
66409
XDOT = -7420
582064 Wp = 108
13534
YDOT = -570
663536 meter/sec RA = 173
44454 deg
ZDOT = 1788
258634 TA = 179
19459
MA = 179
19139
Ha = 222
297 n
mi
Hp = 211
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5086349
84 X = -1572752
62
Y = 13861570
58 feet Y = 4207543
80 meter
Z = -16680261
09 Z = -5091729
80
XDOT = -24345
741680 XDOT = -7422
335859
YDOT = -1872
255694 feet/sec YDOT = -653
654857 meter/sec
ZDOT = 5866
990270 ZDOT = 1752
207095
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6701542
26 X = 2042630
08
Y = -13114760
14 feet Y = -3997378
89 meter
Z = -16713395
87 Z = -5094243
06
XDOT = 22990
528492 XDOT = 7007
513084
YDOT = 4466
630802 feet/sec YDOT = 1361
429068 meter/sec
ZDOT = 5712
638068 ZDOT = 1741
212083
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 15078
00563523
00016717 00000-0 10270-3 0 9080
2 25544 51
6452 174
5148 0006656 116
8863 243
2971 15
54783386 14004
Satellite: ISS
Catalog Number: 25544
Epoch time: 15078
00563523 = yrday
fracday
Element set: 908
Inclination: 51
6452 deg
RA of node: 174
5148 deg
Eccentricity:
0006656
Arg of perigee: 116
8863 deg
Mean anomaly: 243
2971 deg
Mean motion: 15
54783386 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1400
Checksum: 318
Coasting Arc #10 (Orbit 1415)
---------------------------------------
Vector Time (GMT): 2015/078/23:49:16
073
Vector Time (MET): N/A
Weight (LBS) : 890095
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3462870
84 A = 6779901
67 meter
Y = -4063874
12 meter E =
0015661
Z = 4164522
97 I = 51
70705
XDOT = 6489
721043 Wp = 92
94036
YDOT = 1686
734374 meter/sec RA = 168
44830 deg
ZDOT = -3739
014259 TA = 35
46593
MA = 35
36190
Ha = 222
178 n
mi
Hp = 211
393
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11361124
79 X = 3487827
09
Y = -13332920
33 feet Y = -4025009
80 meter
Z = 13663133
12 Z = 4181406
12
XDOT = 21291
735707 XDOT = 6488
539877
YDOT = 5533
905426 feet/sec YDOT = 1759
299443 meter/sec
ZDOT = -12267
107148 ZDOT = -3707
491798
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12672416
23 X = -3862552
47
Y = 12010546
43 feet Y = 3660814
55 meter
Z = 13736075
45 Z = 4186755
80
XDOT = -19754
928097 XDOT = -6021
302084
YDOT = -6925
951580 feet/sec YDOT = -2111
030042 meter/sec
ZDOT = -12132
313967 ZDOT = -3697
929297
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 15079
03402410
00016717 00000-0 10270-3 0 9092
2 25544 51
6450 169
3836 0006678 120
2092 239
9723 15
54806485 14165
Satellite: ISS
Catalog Number: 25544
Epoch time: 15079
03402410 = yrday
fracday
Element set: 909
Inclination: 51
6450 deg
RA of node: 169
3836 deg
Eccentricity:
0006678
Arg of perigee: 120
2092 deg
Mean anomaly: 239
9723 deg
Mean motion: 15
54806485 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1416
Checksum: 311
Coasting Arc #11 (Orbit 1430)
---------------------------------------
Vector Time (GMT): 2015/079/23:49:16
073
Vector Time (MET): N/A
Weight (LBS) : 890095
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4984085
85 A = 6784014
53 meter
Y = 3718147
28 meter E =
0009657
Z = -2722438
93 I = 51
75253
XDOT = -4906
519218 Wp = 97
18130
YDOT = -2798
622839 meter/sec RA = 163
46590 deg
ZDOT = 5174
945576 TA = 232
10915
MA = 232
19652
Ha = 222
110 n
mi
Hp = 211
367
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16351987
71 X = -5012068
05
Y = 12198645
94 feet Y = 3662255
07 meter
Z = -8931886
26 Z = -2746719
21
XDOT = -16097
503996 XDOT = -4899
997618
YDOT = -9181
833462 feet/sec YDOT = -2853
453413 meter/sec
ZDOT = 16978
167899 ZDOT = 5151
126994
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17357671
25 X = 5290618
20
Y = -10631387
40 feet Y = -3240446
88 meter
Z = -9036476
51 Z = -2754318
04
XDOT = 14506
721882 XDOT = 4421
648830
YDOT = 9380
267727 feet/sec YDOT = 2859
105603 meter/sec
ZDOT = 16876
540505 ZDOT = 5143
969546
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 15079
99812225
00016717 00000-0 10270-3 0 9108
2 25544 51
6455 164
5723 0006626 123
5996 236
5790 15
54848805 14310
Satellite: ISS
Catalog Number: 25544
Epoch time: 15079
99812225 = yrday
fracday
Element set: 910
Inclination: 51
6455 deg
RA of node: 164
5723 deg
Eccentricity:
0006626
Arg of perigee: 123
5996 deg
Mean anomaly: 236
5790 deg
Mean motion: 15
54848805 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1431
Checksum: 332
Coasting Arc #12 (Orbit 1446)
---------------------------------------
Vector Time (GMT): 2015/080/23:49:16
073
Vector Time (MET): N/A
Weight (LBS) : 890095
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5974777
54 A = 6786938
22 meter
Y = -3081062
57 meter E =
0020104
Z = 859563
79 I = 51
79185
XDOT = 2879
174814 Wp = 126
46842
YDOT = 3899
670536 meter/sec RA = 158
49740 deg
ZDOT = -5950
052379 TA = 44
24271
MA = 44
08215
Ha = 222
111 n
mi
Hp = 211
475
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19602288
52 X = 6004611
20
Y = -10108473
01 feet Y = -3014081
76 meter
Z = 2820091
16 Z = 888661
12
XDOT = 9446
111595 XDOT = 2864
257003
YDOT = 12794
194671 feet/sec YDOT = 3931
783016 meter/sec
ZDOT = -19521
169222 ZDOT = -5936
102707
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20293475
03 X = -6185451
19
Y = 8595598
26 feet Y = 2619938
35 meter
Z = 2945236
45 Z = 897708
07
XDOT = -7946
339581 XDOT = -2422
044304
YDOT = -12000
854444 feet/sec YDOT = -3657
860435 meter/sec
ZDOT = -19461
990433 ZDOT = -5932
014684
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 15081
02647805
00016717 00000-0 10270-3 0 9116
2 25544 51
6452 159
4402 0006649 127
6003 232
5754 15
54835824 14473
Satellite: ISS
Catalog Number: 25544
Epoch time: 15081
02647805 = yrday
fracday
Element set: 911
Inclination: 51
6452 deg
RA of node: 159
4402 deg
Eccentricity:
0006649
Arg of perigee: 127
6003 deg
Mean anomaly: 232
5754 deg
Mean motion: 15
54835824 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1447
Checksum: 303
Coasting Arc #13 (Orbit 1462)
---------------------------------------
Vector Time (GMT): 2015/081/23:49:16
073
Vector Time (MET): N/A
Weight (LBS) : 890095
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6323591
64 A = 6786695
18 meter
Y = 2203208
22 meter E =
0016622
Z = 1075622
74 I = 51
82027
XDOT = -673
104461 Wp = 78
51501
YDOT = -4849
579600 meter/sec RA = 153
53477 deg
ZDOT = 5902
386825 TA = 293
12453
MA = 293
29962
Ha = 221
960 n
mi
Hp = 211
582
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20746691
72 X = -6352983
45
Y = 7228373
44 feet Y = 2132329
50 meter
Z = 3528945
99 Z = 1044832
12
XDOT = -2208
347968 XDOT = -647
497015
YDOT = -15910
694225 feet/sec YDOT = -4856
962711 meter/sec
ZDOT = 19364
786172 ZDOT = 5899
179857
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21156511
82 X = 6448504
80
Y = -5999394
95 feet Y = -1828615
58 meter
Z = 3396664
21 Z = 1035303
25
XDOT = 957
502871 XDOT = 291
846875
YDOT = 14475
490684 feet/sec YDOT = 4412
129560 meter/sec
ZDOT = 19351
787634 ZDOT = 5898
424871
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 15082
05481568
00016717 00000-0 10270-3 0 9123
2 25544 51
6451 154
3079 0006455 129
9584 230
2137 15
54879347 14636
Satellite: ISS
Catalog Number: 25544
Epoch time: 15082
05481568 = yrday
fracday
Element set: 912
Inclination: 51
6451 deg
RA of node: 154
3079 deg
Eccentricity:
0006455
Arg of perigee: 129
9584 deg
Mean anomaly: 230
2137 deg
Mean motion: 15
54879347 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1463
Checksum: 323
Coasting Arc #14 (Orbit 1477)
---------------------------------------
Vector Time (GMT): 2015/082/23:49:16
073
Vector Time (MET): N/A
Weight (LBS) : 890095
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6037714
09 A = 6783571
86 meter
Y = -994221
05 meter E =
0010849
Z = -2926977
23 I = 51
83790
XDOT = -1517
659033 Wp = 127
35010
YDOT = 5571
428330 meter/sec RA = 148
56886 deg
ZDOT = -5042
298240 TA = 85
93561
MA = 85
81161
Ha = 221
910 n
mi
Hp = 211
722
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19808773
26 X = 6062601
20
Y = -3261880
10 feet Y = -926564
58 meter
Z = -9602943
66 Z = -2897586
48
XDOT = -4979
196301 XDOT = -1555
353550
YDOT = 18278
964337 feet/sec YDOT = 5554
245531 meter/sec
ZDOT = -16542
973229 ZDOT = -5049
762969
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19987346
24 X = -6092143
13
Y = 2437115
31 feet Y = 742832
75 meter
Z = -9476832
06 Z = -2888538
41
XDOT = 5804
596636 XDOT = 1769
241055
YDOT = -16602
485043 feet/sec YDOT = -5060
437441 meter/sec
ZDOT = -16575
827401 ZDOT = -5052
312192
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 15083
01886671
00016717 00000-0 10270-3 0 9135
2 25544 51
6452 149
4962 0006385 135
0035 225
1637 15
54889788 14788
Satellite: ISS
Catalog Number: 25544
Epoch time: 15083
01886671 = yrday
fracday
Element set: 913
Inclination: 51
6452 deg
RA of node: 149
4962 deg
Eccentricity:
0006385
Arg of perigee: 135
0035 deg
Mean anomaly: 225
1637 deg
Mean motion: 15
54889788 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1478
Checksum: 337
Coasting Arc #15 (Orbit 1493)
---------------------------------------
Vector Time (GMT): 2015/083/23:49:16
073
Vector Time (MET): N/A
Weight (LBS) : 890095
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5192476
24 A = 6779159
98 meter
Y = -399662
67 meter E =
0015705
Z = 4332875
57 I = 51
84981
XDOT = 3393
956764 Wp = 119
20565
YDOT = -5922
876594 meter/sec RA = 143
59212 deg
ZDOT = 3503
926001 TA = 295
21411
MA = 295
37685
Ha = 221
884 n
mi
Hp = 211
660
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17035683
22 X = -5208668
76
Y = -1311229
25 feet Y = -457818
44 meter
Z = 14215471
05 Z = 4307612
16
XDOT = 11135
028753 XDOT = 3442
914708
YDOT = -19432
009823 feet/sec YDOT = -5884
649066 meter/sec
ZDOT = 11495
820214 ZDOT = 3520
532740
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17088753
52 X = 5208652
07
Y = 1724346
25 feet Y = 525580
74 meter
Z = 14107252
57 Z = 4299890
58
XDOT = -11403
485938 XDOT = -3475
782514
YDOT = 17911
263541 feet/sec YDOT = 5459
353127 meter/sec
ZDOT = 11567
924813 ZDOT = 3525
903483
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 15084
04717254
00016717 00000-0 10270-3 0 9140
2 25544 51
6450 144
3636 0006393 136
5228 223
6430 15
54924942 14941
Satellite: ISS
Catalog Number: 25544
Epoch time: 15084
04717254 = yrday
fracday
Element set: 914
Inclination: 51
6450 deg
RA of node: 144
3636 deg
Eccentricity:
0006393
Arg of perigee: 136
5228 deg
Mean anomaly: 223
6430 deg
Mean motion: 15
54924942 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1494
Checksum: 305
Coasting Arc #16 (Orbit 1508)
---------------------------------------
Vector Time (GMT): 2015/084/23:49:16
073
Vector Time (MET): N/A
Weight (LBS) : 890095
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3909462
64 A = 6775598
55 meter
Y = 1978323
17 meter E =
0017576
Z = -5182822
37 I = 51
86315
XDOT = -4825
957896 Wp = 97
32513
YDOT = 5766
922655 meter/sec RA = 138
60347 deg
ZDOT = -1445
373227 TA = 158
82588
MA = 158
75304
Ha = 221
586 n
mi
Hp = 211
809
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12826321
01 X = 3912226
24
Y = 6490561
59 feet Y = 2022056
32 meter
Z = -17004010
40 Z = -5163824
41
XDOT = -15833
195198 XDOT = -4883
065227
YDOT = 18920
349917 feet/sec YDOT = 5712
636206 meter/sec
ZDOT = -4742
038147 ZDOT = -1468
956043
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12888055
64 X = -3928279
36
Y = -6579679
79 feet Y = -2005486
40 meter
Z = -16922887
04 Z = -5158095
97
XDOT = 15455
393623 XDOT = 4710
803976
YDOT = -17868
739577 feet/sec YDOT = -5446
391823 meter/sec
ZDOT = -4844
037919 ZDOT = -1476
462758
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 15085
01119255
00016717 00000-0 10270-3 0 9156
2 25544 51
6448 139
5513 0006225 140
6510 219
5097 15
54979420 15093
Satellite: ISS
Catalog Number: 25544
Epoch time: 15085
01119255 = yrday
fracday
Element set: 915
Inclination: 51
6448 deg
RA of node: 139
5513 deg
Eccentricity:
0006225
Arg of perigee: 140
6510 deg
Mean anomaly: 219
5097 deg
Mean motion: 15
54979420 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1509
Checksum: 303
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