[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
July 20th 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
202/21:41:30
000 0
0 0
0 0
0
N/A 0
0 0
0 225
3
000/00:00:00
000 0
0 0
0 223
0
205/03:28:03
000 0
0 0
0 0
0
N/A 0
0 0
0 225
7
000/00:00:00
000 0
0 0
0 222
9
Coasting Arc #1 (Orbit 1618)
---------------------------------------
Vector Time (GMT): 2014/199/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1397009
04 A = 6791647
67 meter
Y = 4693041
67 meter E =
0003340
Z = 4706509
87 I = 51
33947
XDOT = -5605
539971 Wp = 25
50797
YDOT = 4435
594531 meter/sec RA = 303
68443 deg
ZDOT = -2755
347429 TA = 91
93714
MA = 91
89888
Ha = 225
256 n
mi
Hp = 223
050
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4583363
00 X = 1321564
03
Y = 15397118
33 feet Y = 4708241
85 meter
Z = 15441305
34 Z = 4713113
27
XDOT = -18390
879170 XDOT = -5641
338707
YDOT = 14552
475494 feet/sec YDOT = 4372
709746 meter/sec
ZDOT = -9039
853771 ZDOT = -2782
664862
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11987110
34 X = 3653671
23
Y = -10655913
73 feet Y = -3247922
51 meter
Z = 15468453
96 Z = 4714784
77
XDOT = 20230
590325 XDOT = 6166
283931
YDOT = 9448
429413 feet/sec YDOT = 2879
881285 meter/sec
ZDOT = -9156
551795 ZDOT = -2790
916987
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 14199
54340290
00016717 00000-0 10270-3 0 9008
2 25544 51
6481 304
1552 0005624 264
5850 95
4660 15
50112534 16198
Satellite: ISS
Catalog Number: 25544
Epoch time: 14199
54340290 = yrday
fracday
Element set: 900
Inclination: 51
6481 deg
RA of node: 304
1552 deg
Eccentricity:
0005624
Arg of perigee: 264
5850 deg
Mean anomaly: 95
4660 deg
Mean motion: 15
50112534 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1619
Checksum: 290
Coasting Arc #2 (Orbit 1633)
---------------------------------------
Vector Time (GMT): 2014/200/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1461916
63 A = 6792260
04 meter
Y = -4860373
59 meter E =
0004879
Z = -4518623
57 I = 51
32541
XDOT = 5331
361189 Wp = 136
10866
YDOT = -4516
414591 meter/sec RA = 298
70693 deg
ZDOT = 3131
726550 TA = 165
49178
MA = 165
47776
Ha = 225
166 n
mi
Hp = 222
960
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4796314
41 X = -1385508
29
Y = -15946107
59 feet Y = -4876294
19 meter
Z = -14824880
46 Z = -4525540
01
XDOT = 17491
342484 XDOT = 5366
255709
YDOT = -14817
633172 feet/sec YDOT = -4456
600959 meter/sec
ZDOT = 10274
693407 ZDOT = 3157
709870
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12197492
73 X = -3717795
78
Y = 11298663
22 feet Y = 3443832
55 meter
Z = -14853330
96 Z = -4527295
28
XDOT = -20192
528308 XDOT = -6154
682628
YDOT = -8139
624349 feet/sec YDOT = -2480
957502 meter/sec
ZDOT = 10385
741090 ZDOT = 3165
573884
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 14200
51042526
00016717 00000-0 10270-3 0 9010
2 25544 51
6481 299
3640 0005699 268
3610 91
6888 15
50156285 16347
Satellite: ISS
Catalog Number: 25544
Epoch time: 14200
51042526 = yrday
fracday
Element set: 901
Inclination: 51
6481 deg
RA of node: 299
3640 deg
Eccentricity:
0005699
Arg of perigee: 268
3610 deg
Mean anomaly: 91
6888 deg
Mean motion: 15
50156285 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1634
Checksum: 311
Coasting Arc #3 (Orbit 1649)
---------------------------------------
Vector Time (GMT): 2014/201/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1547665
89 A = 6793095
37 meter
Y = 5028243
46 meter E =
0004961
Z = 4296218
89 I = 51
31400
XDOT = -5066
025963 Wp = 48
65095
YDOT = 4556
481040 meter/sec RA = 293
72830 deg
ZDOT = -3502
011716 TA = 77
22353
MA = 77
16810
Ha = 225
184 n
mi
Hp = 222
994
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 5077644
01 X = 1470454
38
Y = 16496861
76 feet Y = 5045118
43 meter
Z = 14095206
33 Z = 4303550
02
XDOT = -16620
820087 XDOT = -5099
589516
YDOT = 14949
084776 feet/sec YDOT = 4499
642067 meter/sec
ZDOT = -11489
539750 ZDOT = -3526
702795
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12358996
24 X = 3767022
05
Y = -12013838
32 feet Y = -3661817
92 meter
Z = 14125390
57 Z = 4305419
05
XDOT = 20005
600440 XDOT = 6097
707014
YDOT = 6924
743828 feet/sec YDOT = 2110
661919 meter/sec
ZDOT = -11595
109032 ZDOT = -3534
189233
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 14201
54190730
00016717 00000-0 10270-3 0 9026
2 25544 51
6481 294
2529 0005627 273
6067 86
4440 15
50150731 16507
Satellite: ISS
Catalog Number: 25544
Epoch time: 14201
54190730 = yrday
fracday
Element set: 902
Inclination: 51
6481 deg
RA of node: 294
2529 deg
Eccentricity:
0005627
Arg of perigee: 273
6067 deg
Mean anomaly: 86
4440 deg
Mean motion: 15
50150731 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1650
Checksum: 287
Coasting Arc #4 (Orbit 1664)
---------------------------------------
Vector Time (GMT): 2014/202/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1669261
60 A = 6793854
30 meter
Y = -5190006
59 meter E =
0001958
Z = -4056043
67 I = 51
30502
XDOT = 4803
488650 Wp = 142
77163
YDOT = -4554
807704 meter/sec RA = 288
74964 deg
ZDOT = 3850
789271 TA = 167
34060
MA = 167
33568
Ha = 225
197 n
mi
Hp = 222
925
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5476580
04 X = -1591398
89
Y = -17027580
68 feet Y = -5208237
65 meter
Z = -13307229
90 Z = -4063963
97
XDOT = 15759
477197 XDOT = 4835
358791
YDOT = -14943
594831 feet/sec YDOT = -4500
914132 meter/sec
ZDOT = 12633
823069 ZDOT = 3874
200793
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12425744
63 X = -3787366
96
Y = 12832068
71 feet Y = 3911214
54 meter
Z = -13339890
68 Z = -4065998
68
XDOT = -19660
127572 XDOT = -5992
406884
YDOT = -5797
820691 feet/sec YDOT = -1767
175747 meter/sec
ZDOT = 12733
961236 ZDOT = 3881
311385
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 14202
50891197
00016717 00000-0 10270-3 0 9039
2 25544 51
6480 289
4617 0005698 277
1645 82
8857 15
50181454 16653
Satellite: ISS
Catalog Number: 25544
Epoch time: 14202
50891197 = yrday
fracday
Element set: 903
Inclination: 51
6480 deg
RA of node: 289
4617 deg
Eccentricity:
0005698
Arg of perigee: 277
1645 deg
Mean anomaly: 82
8857 deg
Mean motion: 15
50181454 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1665
Checksum: 336
Coasting Arc #5 (Orbit 1671)
---------------------------------------
Vector Time (GMT): 2014/202/21:41:30
000
Vector Time (MET): N/A
Weight (LBS) : 884340
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4266102
09 A = 6794781
52 meter
Y = -3715422
68 meter E =
0005876
Z = 3758578
00 I = 51
30275
XDOT = 1662
552340 Wp = 90
48280
YDOT = 6178
953967 meter/sec RA = 286
79108 deg
ZDOT = 4215
177048 TA = 314
67485
MA = 314
72272
Ha = 225
308 n
mi
Hp = 222
959
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13996397
93 X = 4289073
92
Y = -12189706
95 feet Y = -3667588
27 meter
Z = 12331292
66 Z = 3779357
42
XDOT = 5454
568046 XDOT = 1572
858498
YDOT = 20272
158685 feet/sec YDOT = 6197
043818 meter/sec
ZDOT = 13829
321022 ZDOT = 4223
036113
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10699174
26 X = 3261108
32
Y = 15093619
79 feet Y = 4600535
31 meter
Z = 12420112
75 Z = 3785650
37
XDOT = -19615
823765 XDOT = -5978
903083
YDOT = 2482
981492 feet/sec YDOT = 756
812759 meter/sec
ZDOT = 13861
546810 ZDOT = 4224
999468
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 14202
96017871
00016717 00000-0 10270-3 0 9049
2 25544 51
6465 287
2267 0005702 283
3131 76
7384 15
50180586 16728
Satellite: ISS
Catalog Number: 25544
Epoch time: 14202
96017871 = yrday
fracday
Element set: 904
Inclination: 51
6465 deg
RA of node: 287
2267 deg
Eccentricity:
0005702
Arg of perigee: 283
3131 deg
Mean anomaly: 76
7384 deg
Mean motion: 15
50180586 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1672
Checksum: 311
Coasting Arc #6 (Orbit 1686)
---------------------------------------
Vector Time (GMT): 2014/203/21:41:30
000
Vector Time (MET): N/A
Weight (LBS) : 884340
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4068011
16 A = 6793836
28 meter
Y = 3654965
78 meter E =
0004311
Z = -4035217
65 I = 51
29195
XDOT = -1847
882992 Wp = 18
93996
YDOT = -6339
356535 meter/sec RA = 281
81128 deg
ZDOT = -3876
246227 TA = 210
60022
MA = 210
62538
Ha = 225
657 n
mi
Hp = 222
823
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13346493
31 X = -4088977
91
Y = 11991357
54 feet Y = 3609357
80 meter
Z = -13238903
04 Z = -4055029
84
XDOT = -6062
608240 XDOT = -1758
028173
YDOT = -20798
413830 feet/sec YDOT = -6359
517983 meter/sec
ZDOT = -12717
343263 ZDOT = -3885
005226
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10815424
94 X = -3296541
52
Y = -14237210
42 feet Y = -4339501
74 meter
Z = -13323607
46 Z = -4061035
56
XDOT = 20195
767607 XDOT = 6155
669967
YDOT = -3398
274667 feet/sec YDOT = -1035
794118 meter/sec
ZDOT = -12753
368470 ZDOT = -3887
226710
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 14203
92717191
00016717 00000-0 10270-3 0 9059
2 25544 51
6468 282
4349 0005703 288
7269 71
3262 15
50194765 16877
Satellite: ISS
Catalog Number: 25544
Epoch time: 14203
92717191 = yrday
fracday
Element set: 905
Inclination: 51
6468 deg
RA of node: 282
4349 deg
Eccentricity:
0005703
Arg of perigee: 288
7269 deg
Mean anomaly: 71
3262 deg
Mean motion: 15
50194765 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1687
Checksum: 330
Coasting Arc #7 (Orbit 1702)
---------------------------------------
Vector Time (GMT): 2014/204/21:41:30
000
Vector Time (MET): N/A
Weight (LBS) : 884340
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3884932
94 A = 6792921
18 meter
Y = -3560302
54 meter E =
0004095
Z = 4283668
27 I = 51
28346
XDOT = 2062
696505 Wp = 101
50064
YDOT = 6487
248604 meter/sec RA = 276
83089 deg
ZDOT = 3517
408573 TA = 312
44276
MA = 312
47738
Ha = 225
631 n
mi
Hp = 222
871
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12745842
98 X = 3903647
94
Y = -11680782
62 feet Y = -3516754
48 meter
Z = 14054029
76 Z = 4302585
59
XDOT = 6767
376986 XDOT = 1972
915110
YDOT = 21283
624028 feet/sec YDOT = 6509
812682 meter/sec
ZDOT = 11540
054372 ZDOT = 3527
211250
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10790069
80 X = 3288813
27
Y = 13423539
18 feet Y = 4091494
74 meter
Z = 14134919
10 Z = 4308323
34
XDOT = -20712
436164 XDOT = -6313
150543
YDOT = 4442
203602 feet/sec YDOT = 1353
983658 meter/sec
ZDOT = 11580
493883 ZDOT = 3529
734536
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 14204
95862114
00016717 00000-0 10270-3 0 9060
2 25544 51
6468 277
3240 0005727 291
8776 68
1765 15
50205476 17037
Satellite: ISS
Catalog Number: 25544
Epoch time: 14204
95862114 = yrday
fracday
Element set: 906
Inclination: 51
6468 deg
RA of node: 277
3240 deg
Eccentricity:
0005727
Arg of perigee: 291
8776 deg
Mean anomaly: 68
1765 deg
Mean motion: 15
50205476 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1703
Checksum: 321
Coasting Arc #8 (Orbit 1705)
---------------------------------------
Vector Time (GMT): 2014/205/03:28:03
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2345999
13 A = 6795380
53 meter
Y = -5293302
16 meter E =
0001638
Z = -3555534
79 I = 51
28910
XDOT = 4036
436452 Wp = 351
39900
YDOT = -4766
483925 meter/sec RA = 275
58059 deg
ZDOT = 4434
120136 TA = 326
48535
MA = 326
49571
Ha = 225
701 n
mi
Hp = 222
882
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7696847
52 X = -2269362
47
Y = -17366476
91 feet Y = -5319107
81 meter
Z = -11665140
40 Z = -3566745
50
XDOT = 13242
901746 XDOT = 4067
897167
YDOT = -15638
070620 feet/sec YDOT = -4721
170391 meter/sec
ZDOT = 14547
638242 ZDOT = 4453
804261
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5439865
07 X = -1658070
87
Y = -18170135
84 feet Y = -5538257
41 meter
Z = -11711768
19 Z = -3569746
94
XDOT = 13641
537771 XDOT = 4157
940713
YDOT = -13512
501875 feet/sec YDOT = -4118
610571 meter/sec
ZDOT = 14631
993465 ZDOT = 4459
831608
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 14205
15201526
00016717 00000-0 10270-3 0 9078
2 25544 51
6452 276
3637 0005885 291
9008 68
1517 15
50204930 17065
Satellite: ISS
Catalog Number: 25544
Epoch time: 14205
15201526 = yrday
fracday
Element set: 907
Inclination: 51
6452 deg
RA of node: 276
3637 deg
Eccentricity:
0005885
Arg of perigee: 291
9008 deg
Mean anomaly: 68
1517 deg
Mean motion: 15
50204930 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1706
Checksum: 297
Coasting Arc #9 (Orbit 1721)
---------------------------------------
Vector Time (GMT): 2014/206/03:28:03
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2532768
39 A = 6796191
35 meter
Y = 5413670
65 meter E =
0007533
Z = 3231027
34 I = 51
29028
XDOT = -3845
052231 Wp = 74
29542
YDOT = 4632
677023 meter/sec RA = 270
60129 deg
ZDOT = -4736
814639 TA = 68
15648
MA = 68
07637
Ha = 225
922 n
mi
Hp = 222
843
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 8309607
57 X = 2456348
23
Y = 17761386
64 feet Y = 5441566
14 meter
Z = 10600483
39 Z = 3243145
79
XDOT = -12615
000759 XDOT = -3873
560602
YDOT = 15199
071599 feet/sec YDOT = 4589
520168 meter/sec
ZDOT = -15540
730442 ZDOT = -4755
561888
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6326016
42 X = 1928169
80
Y = 18531739
20 feet Y = 5648474
11 meter
Z = 10650954
89 Z = 3246411
05
XDOT = -12696
838455 XDOT = -3869
996361
YDOT = 13333
421062 feet/sec YDOT = 4064
026740 meter/sec
ZDOT = -15621
082655 ZDOT = -4761
305993
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 14206
18345227
00016717 00000-0 10270-3 0 9080
2 25544 51
6454 271
2526 0006082 296
3959 63
6567 15
50246819 17227
Satellite: ISS
Catalog Number: 25544
Epoch time: 14206
18345227 = yrday
fracday
Element set: 908
Inclination: 51
6454 deg
RA of node: 271
2526 deg
Eccentricity:
0006082
Arg of perigee: 296
3959 deg
Mean anomaly: 63
6567 deg
Mean motion: 15
50246819 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1722
Checksum: 321
Coasting Arc #10 (Orbit 1736)
---------------------------------------
Vector Time (GMT): 2014/207/03:28:03
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2749467
51 A = 6797105
34 meter
Y = -5495951
18 meter E =
0004859
Z = -2897255
63 I = 51
29222
XDOT = 3681
499294 Wp = 349
27868
YDOT = -4479
711710 meter/sec RA = 265
62080 deg
ZDOT = 5007
410704 TA = 337
59574
MA = 337
61695
Ha = 225
987 n
mi
Hp = 222
671
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9020562
69 X = -2673732
52
Y = -18031335
90 feet Y = -5526273
83 meter
Z = -9505431
86 Z = -2910428
33
XDOT = 12078
409758 XDOT = 3706
994931
YDOT = -14697
216897 feet/sec YDOT = -4438
400614 meter/sec
ZDOT = 16428
512808 ZDOT = 5025
356165
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7335072
46 X = -2235730
09
Y = -18752300
07 feet Y = -5715701
06 meter
Z = -9560377
31 Z = -2914003
01
XDOT = 11857
058986 XDOT = 3614
031579
YDOT = -13047
297065 feet/sec YDOT = -3976
816145 meter/sec
ZDOT = 16505
431178 ZDOT = 5030
855423
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 14207
15041877
00016717 00000-0 10270-3 0 9093
2 25544 51
6438 266
4594 0005813 299
3208 60
7361 15
50228036 17378
Satellite: ISS
Catalog Number: 25544
Epoch time: 14207
15041877 = yrday
fracday
Element set: 909
Inclination: 51
6438 deg
RA of node: 266
4594 deg
Eccentricity:
0005813
Arg of perigee: 299
3208 deg
Mean anomaly: 60
7361 deg
Mean motion: 15
50228036 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1737
Checksum: 315
Coasting Arc #11 (Orbit 1752)
---------------------------------------
Vector Time (GMT): 2014/208/03:28:03
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2968318
21 A = 6797834
65 meter
Y = 5566274
69 meter E =
0008204
Z = 2525906
98 I = 51
29828
XDOT = -3559
821602 Wp = 89
88720
YDOT = 4289
520509 meter/sec RA = 260
64233 deg
ZDOT = -5254
505980 TA = 61
66793
MA = 61
58521
Ha = 226
204 n
mi
Hp = 222
564
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9738576
81 X = 2893584
45
Y = 18262056
06 feet Y = 5599050
33 meter
Z = 8287096
39 Z = 2540145
14
XDOT = -11679
204731 XDOT = -3581
999261
YDOT = 14073
230016 feet/sec YDOT = 4249
588580 meter/sec
ZDOT = -17239
192848 ZDOT = -5271
852361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8363987
68 X = 2549343
45
Y = 18904948
26 feet Y = 5762228
23 meter
Z = 8346566
83 Z = 2544033
57
XDOT = -11162
714995 XDOT = -3402
395530
YDOT = 12603
990229 feet/sec YDOT = 3841
696222 meter/sec
ZDOT = -17313
530840 ZDOT = -5277
164200
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 14208
18183771
00016717 00000-0 10270-3 0 9109
2 25544 51
6438 261
3480 0006034 303
7025 56
3550 15
50271562 17530
Satellite: ISS
Catalog Number: 25544
Epoch time: 14208
18183771 = yrday
fracday
Element set: 910
Inclination: 51
6438 deg
RA of node: 261
3480 deg
Eccentricity:
0006034
Arg of perigee: 303
7025 deg
Mean anomaly: 56
3550 deg
Mean motion: 15
50271562 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1753
Checksum: 283
Coasting Arc #12 (Orbit 1767)
---------------------------------------
Vector Time (GMT): 2014/209/03:28:03
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3207242
90 A = 6798628
45 meter
Y = -5588941
42 meter E =
0008035
Z = -2151638
59 I = 51
30594
XDOT = 3473
039221 Wp = 357
48582
YDOT = -4094
938487 meter/sec RA = 255
66323 deg
ZDOT = 5466
884552 TA = 338
57345
MA = 338
60707
Ha = 226
257 n
mi
Hp = 222
392
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10522450
45 X = -3134055
95
Y = -18336421
99 feet Y = -5624397
58 meter
Z = -7059181
71 Z = -2167041
06
XDOT = 11394
485632 XDOT = 3492
015821
YDOT = -13434
837557 feet/sec YDOT = -4055
994836 meter/sec
ZDOT = 17935
972940 ZDOT = 5483
801669
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9474365
93 X = -2887786
73
Y = -18875089
88 feet Y = -5753127
40 meter
Z = -7123605
37 Z = -2171274
92
XDOT = 10612
652196 XDOT = 3234
736389
YDOT = -12114
850641 feet/sec YDOT = -3692
606475 meter/sec
ZDOT = 18008
450699 ZDOT = 5488
975773
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 14209
14878763
00016717 00000-0 10270-3 0 9119
2 25544 51
6430 256
5547 0005701 306
9637 53
0992 15
50252261 17681
Satellite: ISS
Catalog Number: 25544
Epoch time: 14209
14878763 = yrday
fracday
Element set: 911
Inclination: 51
6430 deg
RA of node: 256
5547 deg
Eccentricity:
0005701
Arg of perigee: 306
9637 deg
Mean anomaly: 53
0992 deg
Mean motion: 15
50252261 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1768
Checksum: 314
Coasting Arc #13 (Orbit 1783)
---------------------------------------
Vector Time (GMT): 2014/210/03:28:03
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3438508
35 A = 6799181
12 meter
Y = 5597683
64 meter E =
0008396
Z = 1740517
88 I = 51
31646
XDOT = -3434
248775 Wp = 103
62188
YDOT = 3872
056201 meter/sec RA = 250
68612 deg
ZDOT = -5647
237473 TA = 57
22558
MA = 57
14471
Ha = 226
464 n
mi
Hp = 222
228
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11281195
38 X = 3367203
50
Y = 18365103
81 feet Y = 5635736
53 meter
Z = 5710360
51 Z = 1757048
29
XDOT = -11267
220390 XDOT = -3449
859826
YDOT = 12703
596461 feet/sec YDOT = 3833
565064 meter/sec
ZDOT = -18527
681997 ZDOT = -5663
958071
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10563286
12 X = 3219689
61
Y = 18766033
23 feet Y = 5719886
93 meter
Z = 5779585
39 Z = 1761617
63
XDOT = -10240
810918 XDOT = -3121
399168
YDOT = 11513
790303 feet/sec YDOT = 3509
403284 meter/sec
ZDOT = -18599
283302 ZDOT = -5669
061550
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 14210
18018879
00016717 00000-0 10270-3 0 9120
2 25544 51
6426 251
4427 0005923 311
3097 48
7543 15
50296783 17841
Satellite: ISS
Catalog Number: 25544
Epoch time: 14210
18018879 = yrday
fracday
Element set: 912
Inclination: 51
6426 deg
RA of node: 251
4427 deg
Eccentricity:
0005923
Arg of perigee: 311
3097 deg
Mean anomaly: 48
7543 deg
Mean motion: 15
50296783 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1784
Checksum: 315
Coasting Arc #14 (Orbit 1798)
---------------------------------------
Vector Time (GMT): 2014/211/03:28:03
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3677421
32 A = 6799764
28 meter
Y = -5553477
55 meter E =
0010911
Z = -1333675
60 I = 51
32977
XDOT = 3433
474518 Wp = 7
37111
YDOT = -3660
759266 meter/sec RA = 245
70924 deg
ZDOT = 5792
121278 TA = 338
06454
MA = 338
11121
Ha = 226
512 n
mi
Hp = 222
077
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12065030
57 X = -3608569
29
Y = -18220070
70 feet Y = -5594215
86 meter
Z = -4375576
13 Z = -1351372
51
XDOT = 11264
680177 XDOT = 3446
019010
YDOT = -12010
365045 feet/sec YDOT = -3622
293856 meter/sec
ZDOT = 19003
022564 ZDOT = 5808
830757
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11679418
82 X = -3559886
86
Y = -18451891
28 feet Y = -5624136
46 meter
Z = -4449774
10 Z = -1356291
14
XDOT = 10031
638445 XDOT = 3057
643398
YDOT = -10937
247804 feet/sec YDOT = -3333
673131 meter/sec
ZDOT = 19074
537495 ZDOT = 5813
919029
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 14211
14712202
00016717 00000-0 10270-3 0 9139
2 25544 51
6430 246
6496 0005589 314
8629 45
2068 15
50279275 17992
Satellite: ISS
Catalog Number: 25544
Epoch time: 14211
14712202 = yrday
fracday
Element set: 913
Inclination: 51
6430 deg
RA of node: 246
6496 deg
Eccentricity:
0005589
Arg of perigee: 314
8629 deg
Mean anomaly: 45
2068 deg
Mean motion: 15
50279275 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1799
Checksum: 315
Coasting Arc #15 (Orbit 1814)
---------------------------------------
Vector Time (GMT): 2014/212/03:28:03
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3897993
68 A = 6800064
06 meter
Y = 5496251
47 meter E =
0007935
Z = 892053
71 I = 51
34431
XDOT = -3482
284109 Wp = 115
18738
YDOT = 3432
734813 meter/sec RA = 240
73409 deg
ZDOT = -5895
800678 TA = 55
13740
MA = 55
06282
Ha = 226
707 n
mi
Hp = 221
878
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12788693
18 X = 3831910
38
Y = 18032321
10 feet Y = 5539471
86 meter
Z = 2926685
39 Z = 910828
83
XDOT = -11424
816632 XDOT = -3491
771439
YDOT = 11262
253325 feet/sec YDOT = 3393
740620 meter/sec
ZDOT = -19343
178078 ZDOT = -5912
739922
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12728280
46 X = 3879579
88
Y = 18062079
45 feet Y = 5505321
81 meter
Z = 3005482
93 Z = 916071
20
XDOT = -10011
856117 XDOT = -3051
613744
YDOT = 10306
219096 feet/sec YDOT = 3141
335581 meter/sec
ZDOT = -19415
627995 ZDOT = -5917
883413
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 14212
17850571
00016717 00000-0 10270-3 0 9146
2 25544 51
6425 241
5372 0005793 319
1897 40
8819 15
50320905 18156
Satellite: ISS
Catalog Number: 25544
Epoch time: 14212
17850571 = yrday
fracday
Element set: 914
Inclination: 51
6425 deg
RA of node: 241
5372 deg
Eccentricity:
0005793
Arg of perigee: 319
1897 deg
Mean anomaly: 40
8819 deg
Mean motion: 15
50320905 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1815
Checksum: 306
Coasting Arc #16 (Orbit 1829)
---------------------------------------
Vector Time (GMT): 2014/213/03:28:03
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4112528
69 A = 6800354
29 meter
Y = -5385656
07 meter E =
0013257
Z = -462233
36 I = 51
36250
XDOT = 3568
258895 Wp = 17
81964
YDOT = -3231
744687 meter/sec RA = 235
76009 deg
ZDOT = 5965
023010 TA = 337
18208
MA = 337
24094
Ha = 226
752 n
mi
Hp = 221
751
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13492548
18 X = -4049754
04
Y = -17669475
30 feet Y = -5431294
03 meter
Z = -1516513
64 Z = -482058
72
XDOT = 11706
886137 XDOT = 3575
155969
YDOT = -10602
836898 feet/sec YDOT = -3191
803525 meter/sec
ZDOT = 19570
285467 ZDOT = 5982
373678
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13744315
65 X = -4189267
41
Y = -17466924
63 feet Y = -5323918
63 meter
Z = -1599799
63 Z = -487618
93
XDOT = 10150
753325 XDOT = 3093
949613
YDOT = -9770
155670 feet/sec YDOT = -2977
943448 meter/sec
ZDOT = 19644
447860 ZDOT = 5987
627708
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 14213
14542195
00016717 00000-0 10270-3 0 9155
2 25544 51
6438 236
7445 0005519 322
7926 37
2842 15
50309480 18304
Satellite: ISS
Catalog Number: 25544
Epoch time: 14213
14542195 = yrday
fracday
Element set: 915
Inclination: 51
6438 deg
RA of node: 236
7445 deg
Eccentricity:
0005519
Arg of perigee: 322
7926 deg
Mean anomaly: 37
2842 deg
Mean motion: 15
50309480 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1830
Checksum: 303
Coasting Arc #17 (Orbit 1845)
---------------------------------------
Vector Time (GMT): 2014/214/03:28:03
000
Vector Time (MET): N/A
Weight (LBS) : 898773
9
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4298435
77 A = 6800350
97 meter
Y = 5266299
27 meter E =
0006701
Z = 1389
22 I = 51
38054
XDOT = -3699
793698 Wp = 123
57695
YDOT = 3026
924396 meter/sec RA = 230
78749 deg
ZDOT = -5983
935760 TA = 56
40806
MA = 56
34412
Ha = 226
932 n
mi
Hp = 221
543
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14102479
55 X = 4239220
58
Y = 17277884
73 feet Y = 5314036
06 meter
Z = 4557
81 Z = 22126
40
XDOT = -12138
430767 XDOT = -3704
298690
YDOT = 9930
854316 feet/sec YDOT = 2985
525715 meter/sec
ZDOT = -19632
335169 ZDOT = -6001
919634
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14649277
15 X = 4465099
68
Y = 16816524
99 feet Y = 5125676
82 meter
Z = 91745
33 Z = 27963
98
XDOT = -10463
673760 XDOT = -3189
327762
YDOT = 9241
278087 feet/sec YDOT = 2816
741561 meter/sec
ZDOT = -19709
153152 ZDOT = -6007
349881
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 14214
17678823
00016717 00000-0 10270-3 0 9168
2 25544 51
6433 231
6321 0005693 327
0460 33
0335 15
50343092 18465
Satellite: ISS
Catalog Number: 25544
Epoch time: 14214
17678823 = yrday
fracday
Element set: 916
Inclination: 51
6433 deg
RA of node: 231
6321 deg
Eccentricity:
0005693
Arg of perigee: 327
0460 deg
Mean anomaly: 33
0335 deg
Mean motion: 15
50343092 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1846
Checksum: 287
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