[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
August 10th 2014
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) : 128 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 453 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
224/13:30:14
000 0
0 0
0 0
0
N/A 0
0 0
0 227
8
000/00:00:00
000 0
0 0
0 219
6
226/17:17:06
146 -2
6 3
8 3
8
N/A 2
0 0
2 228
0
000/00:08:12
292 -2
1 -0
3 221
6
227/10:40:00
000 0
0 0
0 0
0
N/A 0
0 0
0 228
1
000/00:00:00
000 0
0 0
0 221
3
Coasting Arc #1 (Orbit 1944)
---------------------------------------
Vector Time (GMT): 2014/220/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3353149
15 A = 6793164
19 meter
Y = -4439697
57 meter E =
0010593
Z = 3885614
44 I = 51
51686
XDOT = 6368
111541 Wp = 61
63887
YDOT = -1225
345239 meter/sec RA = 199
21381 deg
ZDOT = 4091
799898 TA = 345
36955
MA = 345
40019
Ha = 227
401 n
mi
Hp = 220
353
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11001145
52 X = -3322128
95
Y = -14565936
90 feet Y = -4477021
37 meter
Z = 12748078
86 Z = 3869400
75
XDOT = 20892
754400 XDOT = 6361
464054
YDOT = -4020
161545 feet/sec YDOT = -1154
170259 meter/sec
ZDOT = 13424
540349 ZDOT = 4122
718529
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2117855
43 X = -645522
33
Y = 18178018
94 feet Y = 5540660
17 meter
Z = 12679887
65 Z = 3864829
76
XDOT = -16452
385820 XDOT = -5014
687198
YDOT = -11380
936299 feet/sec YDOT = -3468
909384 meter/sec
ZDOT = 13556
065542 ZDOT = 4131
888777
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 14220
55612399
00016717 00000-0 10270-3 0 9006
2 25544 51
6421 200
0062 0006998 344
6628 15
4309 15
50642818 19457
Satellite: ISS
Catalog Number: 25544
Epoch time: 14220
55612399 = yrday
fracday
Element set: 900
Inclination: 51
6421 deg
RA of node: 200
0062 deg
Eccentricity:
0006998
Arg of perigee: 344
6628 deg
Mean anomaly: 15
4309 deg
Mean motion: 15
50642818 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1945
Checksum: 297
Coasting Arc #2 (Orbit 1959)
---------------------------------------
Vector Time (GMT): 2014/221/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3140096
65 A = 6791993
36 meter
Y = 4279348
30 meter E =
0011535
Z = -4249522
45 I = 51
54279
XDOT = -6626
735797 Wp = 33
34561
YDOT = 1274
456033 meter/sec RA = 194
24562 deg
ZDOT = -3608
544019 TA = 199
60550
MA = 199
64989
Ha = 227
571 n
mi
Hp = 220
185
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10302154
37 X = 3112652
98
Y = 14039856
63 feet Y = 4314309
54 meter
Z = -13942002
80 Z = -4234335
19
XDOT = -21741
259176 XDOT = -6622
965784
YDOT = 4181
286199 feet/sec YDOT = 1200
372768 meter/sec
ZDOT = -11839
055180 ZDOT = -3640
725874
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 1952836
80 X = 595224
66
Y = -17355554
34 feet Y = -5289972
96 meter
Z = -13878132
55 Z = -4230054
80
XDOT = 17446
591530 XDOT = 5317
721098
YDOT = 11552
006393 feet/sec YDOT = 3521
051549 meter/sec
ZDOT = -11975
971495 ZDOT = -3650
276112
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 14221
52283775
00016717 00000-0 10270-3 0 9017
2 25544 51
6423 195
2114 0007071 349
7947 10
3057 15
50626642 19603
Satellite: ISS
Catalog Number: 25544
Epoch time: 14221
52283775 = yrday
fracday
Element set: 901
Inclination: 51
6423 deg
RA of node: 195
2114 deg
Eccentricity:
0007071
Arg of perigee: 349
7947 deg
Mean anomaly: 10
3057 deg
Mean motion: 15
50626642 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1960
Checksum: 294
Coasting Arc #3 (Orbit 1975)
---------------------------------------
Vector Time (GMT): 2014/222/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2866497
84 A = 6790673
17 meter
Y = -4131203
37 meter E =
0007932
Z = 4555948
15 I = 51
56989
XDOT = 6882
093136 Wp = 63
23716
YDOT = -1362
740895 meter/sec RA = 189
27974 deg
ZDOT = 3093
690890 TA = 355
75819
MA = 355
76491
Ha = 227
603 n
mi
Hp = 219
968
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9404520
48 X = -2842219
54
Y = -13553816
82 feet Y = -4163122
64 meter
Z = 14947336
44 Z = 4542082
41
XDOT = 22579
045723 XDOT = 6881
792328
YDOT = -4470
934694 feet/sec YDOT = -1285
782565 meter/sec
ZDOT = 10149
904494 ZDOT = 3127
121609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1992110
91 X = -607195
40
Y = 16429292
54 feet Y = 5007648
37 meter
Z = 14889045
07 Z = 4538180
94
XDOT = -18537
296315 XDOT = -5650
167917
YDOT = -11576
978032 feet/sec YDOT = -3528
662904 meter/sec
ZDOT = 10292
156229 ZDOT = 3137
049219
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 14222
55398626
00016717 00000-0 10270-3 0 9024
2 25544 51
6429 190
0982 0007094 351
7808 8
3225 15
50675123 19768
Satellite: ISS
Catalog Number: 25544
Epoch time: 14222
55398626 = yrday
fracday
Element set: 902
Inclination: 51
6429 deg
RA of node: 190
0982 deg
Eccentricity:
0007094
Arg of perigee: 351
7808 deg
Mean anomaly: 8
3225 deg
Mean motion: 15
50675123 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1976
Checksum: 316
Coasting Arc #4 (Orbit 1990)
---------------------------------------
Vector Time (GMT): 2014/223/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2577267
34 A = 6789684
85 meter
Y = 4033086
40 meter E =
0014916
Z = -4829143
16 I = 51
59803
XDOT = -7067
483466 Wp = 44
51530
YDOT = 1478
872677 meter/sec RA = 184
31378 deg
ZDOT = -2531
127511 TA = 200
48585
MA = 200
54574
Ha = 227
754 n
mi
Hp = 219
817
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8455601
50 X = 2555434
79
Y = 13231910
75 feet Y = 4061784
86 meter
Z = -15843645
55 Z = -4816676
59
XDOT = -23187
281712 XDOT = -7071
200164
YDOT = 4851
944478 feet/sec YDOT = 1399
818664 meter/sec
ZDOT = -8304
224118 ZDOT = -2565
468643
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 2210565
81 X = 673780
46
Y = -15599706
17 feet Y = -4754790
44 meter
Z = -15791273
84 Z = -4813180
27
XDOT = 19514
473154 XDOT = 5948
011417
YDOT = 11338
223963 feet/sec YDOT = 3455
890664 meter/sec
ZDOT = -8450
375976 ZDOT = -2575
674598
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 14223
52068079
00016717 00000-0 10270-3 0 9039
2 25544 51
6435 185
3036 0007170 356
4994 3
6106 15
50658449 19910
Satellite: ISS
Catalog Number: 25544
Epoch time: 14223
52068079 = yrday
fracday
Element set: 903
Inclination: 51
6435 deg
RA of node: 185
3036 deg
Eccentricity:
0007170
Arg of perigee: 356
4994 deg
Mean anomaly: 3
6106 deg
Mean motion: 15
50658449 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1991
Checksum: 313
Coasting Arc #5 (Orbit 2006)
---------------------------------------
Vector Time (GMT): 2014/224/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 900447
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2232043
92 A = 6788624
90 meter
Y = -3961958
90 meter E =
0006124
Z = 5035223
22 I = 51
62697
XDOT = 7239
391149 Wp = 50
56280
YDOT = -1617
334426 meter/sec RA = 179
35037 deg
ZDOT = 1938
751397 TA = 20
63280
MA = 20
60809
Ha = 227
778 n
mi
Hp = 219
595
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7322978
73 X = -2212033
52
Y = -12998552
83 feet Y = -3986806
94 meter
Z = 16519761
22 Z = 5024429
26
XDOT = 23751
283298 XDOT = 7247
520856
YDOT = -5306
215308 feet/sec YDOT = -1536
333336 meter/sec
ZDOT = 6360
732929 ZDOT = 1973
938487
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2656745
11 X = -809775
91
Y = 14731739
56 feet Y = 4490234
22 meter
Z = 16474479
01 Z = 5021421
20
XDOT = -20506
045868 XDOT = -6250
242780
YDOT = -10970
590527 feet/sec YDOT = -3343
835993 meter/sec
ZDOT = 6510
513145 ZDOT = 1984
404407
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
55180881
00016717 00000-0 10270-3 0 9040
2 25544 51
6443 180
1907 0007182 358
8529 1
2604 15
50706665 20072
Satellite: ISS
Catalog Number: 25544
Epoch time: 14224
55180881 = yrday
fracday
Element set: 904
Inclination: 51
6443 deg
RA of node: 180
1907 deg
Eccentricity:
0007182
Arg of perigee: 358
8529 deg
Mean anomaly: 1
2604 deg
Mean motion: 15
50706665 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2007
Checksum: 296
Coasting Arc #6 (Orbit 2007)
---------------------------------------
Vector Time (GMT): 2014/224/13:30:14
000
Vector Time (MET): N/A
Weight (LBS) : 941131
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3328462
38 A = 6790183
78 meter
Y = -3635546
56 meter E =
0008228
Z = 4662081
59 I = 51
63514
XDOT = 6681
280868 Wp = 64
26961
YDOT = -2403
485962 meter/sec RA = 179
04587 deg
ZDOT = 2895
299856 TA = 356
94047
MA = 356
94550
Ha = 227
815 n
mi
Hp = 219
578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10920152
16 X = -3310207
95
Y = -11927646
18 feet Y = -3672665
29 meter
Z = 15295543
28 Z = 4645957
20
XDOT = 21920
212821 XDOT = 6693
596462
YDOT = -7885
452631 feet/sec YDOT = -2328
702570 meter/sec
ZDOT = 9499
015274 ZDOT = 2927
785991
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6959139
98 X = 2121145
86
Y = 14668467
66 feet Y = 4470948
94 meter
Z = 15227558
51 Z = 4641359
83
XDOT = -22146
964840 XDOT = -6750
394883
YDOT = 500
710582 feet/sec YDOT = 152
616585 meter/sec
ZDOT = 9637
434673 ZDOT = 2937
490088
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
61625416
00016717 00000-0 10270-3 0 9056
2 25544 51
6454 179
8714 0007144 359
4374
6768 15
50704740 20085
Satellite: ISS
Catalog Number: 25544
Epoch time: 14224
61625416 = yrday
fracday
Element set: 905
Inclination: 51
6454 deg
RA of node: 179
8714 deg
Eccentricity:
0007144
Arg of perigee: 359
4374 deg
Mean anomaly:
6768 deg
Mean motion: 15
50704740 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2008
Checksum: 305
Coasting Arc #7 (Orbit 2022)
---------------------------------------
Vector Time (GMT): 2014/225/13:30:14
000
Vector Time (MET): N/A
Weight (LBS) : 941131
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3008692
48 A = 6789176
28 meter
Y = 3600580
61 meter E =
0016060
Z = -4921034
16 I = 51
66345
XDOT = -6834
784890 Wp = 48
32978
YDOT = 2545
370830 meter/sec RA = 174
08428 deg
ZDOT = -2310
840022 TA = 198
99202
MA = 199
05198
Ha = 227
915 n
mi
Hp = 219
422
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9871038
33 X = 2992110
81
Y = 11812928
51 feet Y = 3634132
77 meter
Z = -16145125
19 Z = -4906459
03
XDOT = -22423
834940 XDOT = -6851
514678
YDOT = 8350
954167 feet/sec YDOT = 2468
846188 meter/sec
ZDOT = -7581
496134 ZDOT = -2344
082735
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6241286
12 X = -1902344
01
Y = -14142427
91 feet Y = -4310612
03 meter
Z = -16083713
05 Z = -4902315
74
XDOT = 22790
518745 XDOT = 6946
550114
YDOT = -1253
808729 feet/sec YDOT = -382
160901 meter/sec
ZDOT = -7723
163358 ZDOT = -2354
020191
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
58292840
00016717 00000-0 10270-3 0 9065
2 25544 51
6459 175
0773 0007285 3
8223 356
2982 15
50708463 20233
Satellite: ISS
Catalog Number: 25544
Epoch time: 14225
58292840 = yrday
fracday
Element set: 906
Inclination: 51
6459 deg
RA of node: 175
0773 deg
Eccentricity:
0007285
Arg of perigee: 3
8223 deg
Mean anomaly: 356
2982 deg
Mean motion: 15
50708463 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2023
Checksum: 312
Coasting Arc #8 (Orbit 2038)
---------------------------------------
Vector Time (GMT): 2014/226/13:30:14
000
Vector Time (MET): N/A
Weight (LBS) : 941131
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2639005
49 A = 6788226
91 meter
Y = -3601712
67 meter E =
0006577
Z = 5107567
16 I = 51
69150
XDOT = 6971
060200 Wp = 51
39412
YDOT = -2704
608343 meter/sec RA = 169
12438 deg
ZDOT = 1697
164808 TA = 22
23570
MA = 22
20719
Ha = 227
953 n
mi
Hp = 219
220
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8658154
50 X = -2623344
84
Y = -11816642
62 feet Y = -3631135
92 meter
Z = 16757110
12 Z = 5094785
60
XDOT = 22870
932415 XDOT = 6992
541452
YDOT = -8873
386953 feet/sec YDOT = -2626
533256 meter/sec
ZDOT = 5568
126010 ZDOT = 1731
081189
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5316927
31 X = 1620599
44
Y = 13715935
91 feet Y = 4180617
26 meter
Z = 16703317
27 Z = 5091171
10
XDOT = -23370
569363 XDOT = -7123
349542
YDOT = 2112
722785 feet/sec YDOT = 643
957905 meter/sec
ZDOT = 5712
693077 ZDOT = 1741
228850
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
61403508
00016717 00000-0 10270-3 0 9076
2 25544 51
6458 169
9640 0007190 6
4773 353
6469 15
50739925 20396
Satellite: ISS
Catalog Number: 25544
Epoch time: 14226
61403508 = yrday
fracday
Element set: 907
Inclination: 51
6458 deg
RA of node: 169
9640 deg
Eccentricity:
0007190
Arg of perigee: 6
4773 deg
Mean anomaly: 353
6469 deg
Mean motion: 15
50739925 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2039
Checksum: 326
Coasting Arc #9 (Orbit 2040)
---------------------------------------
Vector Time (GMT): 2014/226/17:21:12
292
Vector Time (MET): N/A
Weight (LBS) : 940777
3
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3123273
38 A = 6790936
35 meter
Y = 3387631
28 meter E =
0013529
Z = -5000374
81 I = 51
69865
XDOT = -6688
827416 Wp = 50
25230
YDOT = 3069
622030 meter/sec RA = 168
33277 deg
ZDOT = -2093
638373 TA = 199
31606
MA = 199
36739
Ha = 227
974 n
mi
Hp = 221
591
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10246959
91 X = 3109449
95
Y = 11114275
86 feet Y = 3422480
21 meter
Z = -16405429
17 Z = -4985236
28
XDOT = -21944
971838 XDOT = -6712
485385
YDOT = 10070
938418 feet/sec YDOT = 2994
690864 meter/sec
ZDOT = -6868
892301 ZDOT = -2126
189039
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15139076
15 X = -4614390
41
Y = -1194313
53 feet Y = -364026
76 meter
Z = -16341585
30 Z = -4980915
20
XDOT = 9247
142946 XDOT = 2818
529170
YDOT = -21121
057266 feet/sec YDOT = -6437
698255 meter/sec
ZDOT = -7007
710819 ZDOT = -2135
950258
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
74292807
00016717 00000-0 10270-3 0 9089
2 25544 51
6463 169
3252 0005609 342
7883 17
3077 15
49994215 20411
Satellite: ISS
Catalog Number: 25544
Epoch time: 14226
74292807 = yrday
fracday
Element set: 908
Inclination: 51
6463 deg
RA of node: 169
3252 deg
Eccentricity:
0005609
Arg of perigee: 342
7883 deg
Mean anomaly: 17
3077 deg
Mean motion: 15
49994215 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2041
Checksum: 324
Coasting Arc #10 (Orbit 2051)
---------------------------------------
Vector Time (GMT): 2014/227/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 930232
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4081133
42 A = 6795860
65 meter
Y = 4063947
06 meter E =
0006189
Z = -3606624
62 I = 51
73485
XDOT = -5912
480544 Wp = 42
82510
YDOT = -2010
334812 meter/sec RA = 164
72026 deg
ZDOT = 4434
016028 TA = 274
64579
MA = 274
71647
Ha = 228
050 n
mi
Hp = 221
316
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13389545
34 X = -4108754
41
Y = 13333159
64 feet Y = 4018154
61 meter
Z = -11832757
94 Z = -3626517
28
XDOT = -19397
902048 XDOT = -5911
099940
YDOT = -6595
586654 feet/sec YDOT = -2076
444089 meter/sec
ZDOT = 14547
296679 ZDOT = 4405
297700
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18428580
50 X = 5617031
34
Y = 3926532
59 feet Y = 1196807
13 meter
Z = -11917927
40 Z = -3632584
27
XDOT = 5347
649110 XDOT = 1629
963449
YDOT = 18598
375108 feet/sec YDOT = 5668
784733 meter/sec
ZDOT = 14425
517410 ZDOT = 4396
897707
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
45214249
00016717 00000-0 10270-3 0 9093
2 25544 51
6440 165
8111 0005509 347
3547 12
7464 15
49975205 20527
Satellite: ISS
Catalog Number: 25544
Epoch time: 14227
45214249 = yrday
fracday
Element set: 909
Inclination: 51
6440 deg
RA of node: 165
8111 deg
Eccentricity:
0005509
Arg of perigee: 347
3547 deg
Mean anomaly: 12
7464 deg
Mean motion: 15
49975205 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2052
Checksum: 304
Coasting Arc #11 (Orbit 2067)
---------------------------------------
Vector Time (GMT): 2014/228/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 930232
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4073418
33 A = 6796552
49 meter
Y = -4297919
62 meter E =
0012737
Z = 3331409
75 I = 51
76773
XDOT = 5773
120680 Wp = 66
07016
YDOT = 1816
215057 meter/sec RA = 159
77384 deg
ZDOT = -4696
594829 TA = 75
30575
MA = 75
16460
Ha = 228
103 n
mi
Hp = 221
159
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13364233
36 X = 4104993
10
Y = -14100786
14 feet Y = -4252191
39 meter
Z = 10929822
02 Z = 3351274
51
XDOT = 18940
684647 XDOT = 5775
196664
YDOT = 5958
710817 feet/sec YDOT = 1880
785298 meter/sec
ZDOT = -15408
775685 ZDOT = -4668
545026
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -19119491
10 X = -5827620
89
Y = -3164255
38 feet Y = -964465
04 meter
Z = 11014919
91 Z = 3357347
59
XDOT = -5910
783844 XDOT = -1801
606916
YDOT = -17727
638852 feet/sec YDOT = -5403
384322 meter/sec
ZDOT = -15289
798759 ZDOT = -4660
330662
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
48371589
00016717 00000-0 10270-3 0 9100
2 25544 51
6444 160
7005 0005558 350
7355 9
3692 15
50018269 20688
Satellite: ISS
Catalog Number: 25544
Epoch time: 14228
48371589 = yrday
fracday
Element set: 910
Inclination: 51
6444 deg
RA of node: 160
7005 deg
Eccentricity:
0005558
Arg of perigee: 350
7355 deg
Mean anomaly: 9
3692 deg
Mean motion: 15
50018269 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2068
Checksum: 312
Coasting Arc #12 (Orbit 2082)
---------------------------------------
Vector Time (GMT): 2014/229/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 930232
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4003982
75 A = 6797283
37 meter
Y = 4551224
05 meter E =
0007754
Z = -3070251
75 I = 51
79890
XDOT = -5631
595679 Wp = 29
21692
YDOT = -1638
234794 meter/sec RA = 154
82976 deg
ZDOT = 4927
674301 TA = 295
68529
MA = 295
76535
Ha = 228
202 n
mi
Hp = 221
042
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13136426
35 X = -4039663
81
Y = 14931837
44 feet Y = 4506249
38 meter
Z = -10073004
43 Z = -3089789
13
XDOT = -18476
363777 XDOT = -5636
794891
YDOT = -5374
786071 feet/sec YDOT = -1701
239925 meter/sec
ZDOT = 16166
910436 ZDOT = 4900
304401
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 19725418
31 X = 6012307
50
Y = 2176911
39 feet Y = 663522
59 meter
Z = -10156761
99 Z = -3095781
05
XDOT = 6382
831829 XDOT = 1945
487141
YDOT = 16871
878882 feet/sec YDOT = 5142
548683 meter/sec
ZDOT = 16050
786054 ZDOT = 4892
279589
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
45080645
00016717 00000-0 10270-3 0 9119
2 25544 51
6443 155
9094 0005596 353
7784 6
3296 15
50009013 20833
Satellite: ISS
Catalog Number: 25544
Epoch time: 14229
45080645 = yrday
fracday
Element set: 911
Inclination: 51
6443 deg
RA of node: 155
9094 deg
Eccentricity:
0005596
Arg of perigee: 353
7784 deg
Mean anomaly: 6
3296 deg
Mean motion: 15
50009013 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2083
Checksum: 306
Coasting Arc #13 (Orbit 2098)
---------------------------------------
Vector Time (GMT): 2014/230/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 930232
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3947189
64 A = 6797955
12 meter
Y = -4794895
93 meter E =
0013326
Z = 2757405
85 I = 51
83010
XDOT = 5460
261580 Wp = 76
61842
YDOT = 1517
033155 meter/sec RA = 149
88786 deg
ZDOT = -5154
341034 TA = 72
30721
MA = 72
16177
Ha = 228
268 n
mi
Hp = 220
859
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12950097
24 X = 3987119
43
Y = -15731285
86 feet Y = -4750532
63 meter
Z = 9046607
11 Z = 2776677
59
XDOT = 17914
244029 XDOT = 5467
929854
YDOT = 4977
142898 feet/sec YDOT = 1578
136160 meter/sec
ZDOT = -16910
567697 ZDOT = -5127
797479
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20302223
42 X = -6188117
70
Y = -1222837
61 feet Y = -372720
90 meter
Z = 9129286
17 Z = 2782606
42
XDOT = -6622
702777 XDOT = -2018
599807
YDOT = -16035
302976 feet/sec YDOT = -4887
560347 meter/sec
ZDOT = -16797
926772 ZDOT = -5120
008080
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
48235971
00016717 00000-0 10270-3 0 9129
2 25544 51
6451 150
7985 0005609 357
6914 2
4209 15
50047657 20991
Satellite: ISS
Catalog Number: 25544
Epoch time: 14230
48235971 = yrday
fracday
Element set: 912
Inclination: 51
6451 deg
RA of node: 150
7985 deg
Eccentricity:
0005609
Arg of perigee: 357
6914 deg
Mean anomaly: 2
4209 deg
Mean motion: 15
50047657 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2099
Checksum: 314
Coasting Arc #14 (Orbit 2113)
---------------------------------------
Vector Time (GMT): 2014/231/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 930232
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3824218
45 A = 6798615
69 meter
Y = 5046544
66 meter E =
0010026
Z = -2464065
33 I = 51
85863
XDOT = -5300
244748 Wp = 24
38499
YDOT = -1412
753900 meter/sec RA = 144
94813 deg
ZDOT = 5349
201428 TA = 308
15599
MA = 308
24629
Ha = 228
346 n
mi
Hp = 220
763
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12546648
47 X = -3868396
35
Y = 16556905
06 feet Y = 5003532
76 meter
Z = -8084203
85 Z = -2482749
96
XDOT = -17389
254423 XDOT = -5310
037484
YDOT = -4635
019358 feet/sec YDOT = -1472
079384 meter/sec
ZDOT = 17549
873453 ZDOT = 5323
430106
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20742280
09 X = 6322246
97
Y = 60046
43 feet Y = 18302
15 meter
Z = -8164438
50 Z = -2488520
86
XDOT = 6799
332085 XDOT = 2072
436420
YDOT = 15266
173518 feet/sec YDOT = 4653
129688 meter/sec
ZDOT = 17440
488675 ZDOT = 5315
860948
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
44943132
00016717 00000-0 10270-3 0 9132
2 25544 51
6450 146
0073 0005651
4023 359
7131 15
50042504 21143
Satellite: ISS
Catalog Number: 25544
Epoch time: 14231
44943132 = yrday
fracday
Element set: 913
Inclination: 51
6450 deg
RA of node: 146
0073 deg
Eccentricity:
0005651
Arg of perigee:
4023 deg
Mean anomaly: 359
7131 deg
Mean motion: 15
50042504 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2114
Checksum: 249
Coasting Arc #15 (Orbit 2129)
---------------------------------------
Vector Time (GMT): 2014/232/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 930232
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3714370
40 A = 6799212
38 meter
Y = -5282937
13 meter E =
0013528
Z = 2116793
38 I = 51
88690
XDOT = 5118
895111 Wp = 86
47717
YDOT = 1370
081195 meter/sec RA = 140
01052 deg
ZDOT = -5531
569180 TA = 70
20224
MA = 70
05644
Ha = 228
418 n
mi
Hp = 220
578
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12186254
61 X = 3762886
81
Y = -17332470
90 feet Y = -5241129
35 meter
Z = 6944860
17 Z = 2134954
90
XDOT = 16794
275300 XDOT = 5130
064302
YDOT = 4495
017044 feet/sec YDOT = 1427
386387 meter/sec
ZDOT = -18148
192849 ZDOT = -5506
675549
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21135821
79 X = -6442198
48
Y = 1051699
55 feet Y = 320558
02 meter
Z = 7022919
42 Z = 2140585
84
XDOT = -6753
582781 XDOT = -2058
492032
YDOT = -14565
411311 feet/sec YDOT = -4439
537368 meter/sec
ZDOT = -18042
522935 ZDOT = -5499
360991
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
48096459
00016717 00000-0 10270-3 0 9149
2 25544 51
6460 140
8963 0005635 4
6613 355
4589 15
50073335 21301
Satellite: ISS
Catalog Number: 25544
Epoch time: 14232
48096459 = yrday
fracday
Element set: 914
Inclination: 51
6460 deg
RA of node: 140
8963 deg
Eccentricity:
0005635
Arg of perigee: 4
6613 deg
Mean anomaly: 355
4589 deg
Mean motion: 15
50073335 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2130
Checksum: 304
Coasting Arc #16 (Orbit 2144)
---------------------------------------
Vector Time (GMT): 2014/233/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 930232
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3537613
07 A = 6799738
79 meter
Y = 5515272
69 meter E =
0012506
Z = -1794893
41 I = 51
91194
XDOT = -4962
331158 Wp = 25
34917
YDOT = -1341
730299 meter/sec RA = 135
07480 deg
ZDOT = 5683
216760 TA = 315
03713
MA = 315
13833
Ha = 228
483 n
mi
Hp = 220
481
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11606342
10 X = -3590304
33
Y = 18094726
66 feet Y = 5475418
17 meter
Z = -5888757
92 Z = -1812206
43
XDOT = -16280
614034 XDOT = -4974
565592
YDOT = -4402
002292 feet/sec YDOT = -1397
290597 meter/sec
ZDOT = 18645
724278 ZDOT = 5659
081163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21348744
65 X = 6507097
37
Y = -2339756
90 feet Y = -713157
90 meter
Z = -5963255
77 Z = -1817600
36
XDOT = 6687
947986 XDOT = 2038
486546
YDOT = 13974
048943 feet/sec YDOT = 4259
290118 meter/sec
ZDOT = 18543
263831 ZDOT = 5651
986816
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
44801745
00016717 00000-0 10270-3 0 9159
2 25544 51
6460 136
1052 0005685 7
3146 352
8087 15
50075683 21452
Satellite: ISS
Catalog Number: 25544
Epoch time: 14233
44801745 = yrday
fracday
Element set: 915
Inclination: 51
6460 deg
RA of node: 136
1052 deg
Eccentricity:
0005685
Arg of perigee: 7
3146 deg
Mean anomaly: 352
8087 deg
Mean motion: 15
50075683 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2145
Checksum: 295
Coasting Arc #17 (Orbit 2160)
---------------------------------------
Vector Time (GMT): 2014/234/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 930232
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3376428
32 A = 6800205
69 meter
Y = -5726136
17 meter E =
0013272
Z = 1417876
12 I = 51
93589
XDOT = 4794
224751 Wp = 95
33592
YDOT = 1376
222230 meter/sec RA = 130
14096 deg
ZDOT = -5813
139816 TA = 69
29993
MA = 69
15771
Ha = 228
553 n
mi
Hp = 220
319
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11077520
75 X = 3433320
89
Y = -18786535
99 feet Y = -5688060
62 meter
Z = 4651824
56 Z = 1434416
40
XDOT = 15729
083829 XDOT = 4806
717056
YDOT = 4515
164796 feet/sec YDOT = 1429
904019 meter/sec
ZDOT = -19071
981024 ZDOT = -5789
820270
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -21502912
06 X = -6554087
60
Y = 3549954
39 feet Y = 1082026
10 meter
Z = 4723078
32 Z = 1439594
27
XDOT = -6427
400717 XDOT = -1959
071739
YDOT = -13493
549720 feet/sec YDOT = -4112
833955 meter/sec
ZDOT = -18972
988255 ZDOT = -5782
966820
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
47953096
00016717 00000-0 10270-3 0 9161
2 25544 51
6468 130
9942 0005639 11
6393 348
4887 15
50095045 21612
Satellite: ISS
Catalog Number: 25544
Epoch time: 14234
47953096 = yrday
fracday
Element set: 916
Inclination: 51
6468 deg
RA of node: 130
9942 deg
Eccentricity:
0005639
Arg of perigee: 11
6393 deg
Mean anomaly: 348
4887 deg
Mean motion: 15
50095045 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2161
Checksum: 327
Coasting Arc #18 (Orbit 2175)
---------------------------------------
Vector Time (GMT): 2014/235/10:40:00
000
Vector Time (MET): N/A
Weight (LBS) : 930232
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3151519
24 A = 6800534
08 meter
Y = 5921318
64 meter E =
0014870
Z = -1072174
23 I = 51
95658
XDOT = -4663
095400 Wp = 29
57406
YDOT = -1419
440761 meter/sec RA = 125
20854 deg
ZDOT = 5914
846770 TA = 318
86459
MA = 318
97659
Ha = 228
608 n
mi
Hp = 220
206
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10339630
04 X = -3212290
38
Y = 19426898
41 feet Y = 5885736
47 meter
Z = -3517631
98 Z = -1087631
45
XDOT = -15298
869424 XDOT = -4675
608209
YDOT = -4656
957876 feet/sec YDOT = -1471
656199 meter/sec
ZDOT = 19405
665255 ZDOT = 5892
164203
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 21445679
89 X = 6536643
23
Y = -4890965
93 feet Y = -1490766
41 meter
Z = -3584317
59 Z = -1092500
00
XDOT = 6200
575318 XDOT = 1889
935357
YDOT = 13149
178373 feet/sec YDOT = 4007
869568 meter/sec
ZDOT = 19309
381682 ZDOT = 5885
499537
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
44656506
00016717 00000-0 10270-3 0 9176
2 25544 51
6469 126
2029 0005718 14
1902 345
9409 15
50109004 21768
Satellite: ISS
Catalog Number: 25544
Epoch time: 14235
44656506 = yrday
fracday
Element set: 917
Inclination: 51
6469 deg
RA of node: 126
2029 deg
Eccentricity:
0005718
Arg of perigee: 14
1902 deg
Mean anomaly: 345
9409 deg
Mean motion: 15
50109004 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2176
Checksum: 298
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