[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
January 22nd 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 16145 87 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 120 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 031 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
There are no maneuvers
Coasting Arc #1 (Orbit 2841)
---------------------------------------
Vector Time (GMT): 2014/020/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4393799
29 A = 6790675
26 meter
Y = 187934
99 meter E =
0006482
Z = 5168858
07 I = 51
96480
XDOT = 1496
576033 Wp = 97
32425
YDOT = -7359
737621 meter/sec RA = 110
70835 deg
ZDOT = 1537
309134 TA = 337
91171
MA = 337
93963
Ha = 228
928 n
mi
Hp = 220
487
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14415352
02 X = -4420682
56
Y = 616584
61 feet Y = 138650
49 meter
Z = 16958195
76 Z = 5147448
61
XDOT = 4910
026356 XDOT = 1571
295386
YDOT = -24146
120804 feet/sec YDOT = -7342
584149 meter/sec
ZDOT = 5043
665139 ZDOT = 1544
760783
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7573429
90 X = -2308381
44
Y = -12404958
33 feet Y = -3781031
30 meter
Z = 16867813
19 Z = 5141309
46
XDOT = 22583
012828 XDOT = 6883
302310
YDOT = -6873
818862 feet/sec YDOT = -2095
139989 meter/sec
ZDOT = 5076
236204 ZDOT = 1547
236795
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 14020
55105750
00016717 00000-0 10270-3 0 9002
2 25544 51
6492 111
3668 0003171 52
1637 307
9800 15
49831395 28422
Satellite: ISS
Catalog Number: 25544
Epoch time: 14020
55105750 = yrday
fracday
Element set: 900
Inclination: 51
6492 deg
RA of node: 111
3668 deg
Eccentricity:
0003171
Arg of perigee: 52
1637 deg
Mean anomaly: 307
9800 deg
Mean motion: 15
49831395 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2842
Checksum: 288
Coasting Arc #2 (Orbit 2856)
---------------------------------------
Vector Time (GMT): 2014/021/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4324928
51 A = 6790495
32 meter
Y = -220311
32 meter E =
0016979
Z = -5245364
98 I = 51
97314
XDOT = -1111
014393 Wp = 75
79773
YDOT = 7467
011919 meter/sec RA = 105
77720 deg
ZDOT = -1228
966147 TA = 182
42840
MA = 182
43666
Ha = 228
853 n
mi
Hp = 220
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14189398
01 X = 4352550
65
Y = -722806
17 feet Y = -171792
87 meter
Z = -17209202
68 Z = -5224288
23
XDOT = -3645
060345 XDOT = -1188
459759
YDOT = 24498
070602 feet/sec YDOT = 7454
154800 meter/sec
ZDOT = -4032
041166 ZDOT = -1234
551496
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7765709
98 X = 2366988
40
Y = 12025393
96 feet Y = 3665340
08 meter
Z = -17120215
25 Z = -5218241
61
XDOT = -22156
065719 XDOT = -6753
168831
YDOT = 8528
999854 feet/sec YDOT = 2599
639155 meter/sec
ZDOT = -4056
762226 ZDOT = -1236
501127
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 14021
51827869
00016717 00000-0 10270-3 0 9012
2 25544 51
6484 106
5774 0003212 53
9914 306
1534 15
49800752 28574
Satellite: ISS
Catalog Number: 25544
Epoch time: 14021
51827869 = yrday
fracday
Element set: 901
Inclination: 51
6484 deg
RA of node: 106
5774 deg
Eccentricity:
0003212
Arg of perigee: 53
9914 deg
Mean anomaly: 306
1534 deg
Mean motion: 15
49800752 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2857
Checksum: 310
Coasting Arc #3 (Orbit 2872)
---------------------------------------
Vector Time (GMT): 2014/022/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4251621
36 A = 6790072
15 meter
Y = 235859
66 meter E =
0005709
Z = 5284050
96 I = 51
98013
XDOT = 721
127760 Wp = 90
30073
YDOT = -7576
790953 meter/sec RA = 100
84524 deg
ZDOT = 917
545173 TA = 350
95549
MA = 350
96577
Ha = 228
951 n
mi
Hp = 220
350
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13948888
99 X = -4279610
81
Y = 773817
79 feet Y = 188158
92 meter
Z = 17336125
19 Z = 5263329
37
XDOT = 2365
904724 XDOT = 801
342430
YDOT = -24858
238035 feet/sec YDOT = -7568
278318 meter/sec
ZDOT = 3010
318808 ZDOT = 921
243259
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7891935
44 X = -2405461
92
Y = -11658199
94 feet Y = -3553419
34 meter
Z = 17248630
77 Z = 5257382
66
XDOT = 21677
623676 XDOT = 6607
339696
YDOT = -10191
521285 feet/sec YDOT = -3106
375688 meter/sec
ZDOT = 3027
103363 ZDOT = 922
661105
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 14022
54996762
00016717 00000-0 10270-3 0 9026
2 25544 51
6486 101
4675 0003264 57
5469 302
5996 15
49862664 28732
Satellite: ISS
Catalog Number: 25544
Epoch time: 14022
54996762 = yrday
fracday
Element set: 902
Inclination: 51
6486 deg
RA of node: 101
4675 deg
Eccentricity:
0003264
Arg of perigee: 57
5469 deg
Mean anomaly: 302
5996 deg
Mean motion: 15
49862664 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2873
Checksum: 342
Coasting Arc #4 (Orbit 2887)
---------------------------------------
Vector Time (GMT): 2014/023/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4215774
47 A = 6790016
97 meter
Y = -237144
71 meter E =
0017741
Z = -5332798
33 I = 51
98358
XDOT = -323
066993 Wp = 80
70666
YDOT = 7618
418779 meter/sec RA = 95
91414 deg
ZDOT = -593
080384 TA = 183
63828
MA = 183
65120
Ha = 228
896 n
mi
Hp = 220
477
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13831281
05 X = 4244017
80
Y = -778033
81 feet Y = -189843
37 meter
Z = -17496057
50 Z = -5312250
21
XDOT = -1059
931080 XDOT = -405
352865
YDOT = 24994
812266 feet/sec YDOT = 7614
345943 meter/sec
ZDOT = -1945
801785 ZDOT = -594
849745
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8033234
07 X = 2448529
74
Y = 11419519
12 feet Y = 3480669
43 meter
Z = -17409291
59 Z = -5306352
08
XDOT = -20935
405956 XDOT = -6381
111735
YDOT = 11742
175496 feet/sec YDOT = 3579
015091 meter/sec
ZDOT = -1954
465793 ZDOT = -595
721174
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 14023
51716757
00016717 00000-0 10270-3 0 9039
2 25544 51
6477 96
6776 0003359 59
6548 300
4934 15
49831471 28882
Satellite: ISS
Catalog Number: 25544
Epoch time: 14023
51716757 = yrday
fracday
Element set: 903
Inclination: 51
6477 deg
RA of node: 96
6776 deg
Eccentricity:
0003359
Arg of perigee: 59
6548 deg
Mean anomaly: 300
4934 deg
Mean motion: 15
49831471 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2888
Checksum: 345
Coasting Arc #5 (Orbit 2903)
---------------------------------------
Vector Time (GMT): 2014/024/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4179668
56 A = 6789722
34 meter
Y = 221979
75 meter E =
0005560
Z = 5341412
21 I = 51
98615
XDOT = -73
285366 Wp = 79
44501
YDOT = -7661
411477 meter/sec RA = 90
98253 deg
ZDOT = 261
809121 TA = 8
07513
MA = 8
06618
Ha = 228
980 n
mi
Hp = 220
210
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13712823
36 X = -4207786
87
Y = 728280
02 feet Y = 175082
81 meter
Z = 17524318
27 Z = 5321039
77
XDOT = -240
437552 XDOT = 11
119916
YDOT = -25135
864426 feet/sec YDOT = -7661
759064 meter/sec
ZDOT = 858
953808 ZDOT = 261
658125
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8122448
64 X = -2475722
35
Y = -11207382
87 feet Y = -3416010
30 meter
Z = 17438292
47 Z = 5315191
54
XDOT = 20151
268735 XDOT = 6142
106710
YDOT = -13270
944289 feet/sec YDOT = -4044
983819 meter/sec
ZDOT = 859
533785 ZDOT = 261
985898
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 14024
54883389
00016717 00000-0 10270-3 0 9040
2 25544 51
6483 91
5677 0003386 63
0395 297
1101 15
49893571 29048
Satellite: ISS
Catalog Number: 25544
Epoch time: 14024
54883389 = yrday
fracday
Element set: 904
Inclination: 51
6483 deg
RA of node: 91
5677 deg
Eccentricity:
0003386
Arg of perigee: 63
0395 deg
Mean anomaly: 297
1101 deg
Mean motion: 15
49893571 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2904
Checksum: 332
Coasting Arc #6 (Orbit 2918)
---------------------------------------
Vector Time (GMT): 2014/025/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4184639
93 A = 6789805
79 meter
Y = -205025
65 meter E =
0018093
Z = -5358598
24 I = 51
98521
XDOT = 468
166345 Wp = 85
80761
YDOT = 7633
457174 meter/sec RA = 86
05094 deg
ZDOT = 75
038765 TA = 184
89707
MA = 184
91479
Ha = 228
941 n
mi
Hp = 220
317
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13729133
63 X = 4212651
76
Y = -672656
33 feet Y = -158073
63 meter
Z = -17580702
89 Z = -5338201
93
XDOT = 1535
978823 XDOT = 382
408016
YDOT = 25044
150834 feet/sec YDOT = 7638
213006 meter/sec
ZDOT = 246
190175 ZDOT = 77
104857
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8277158
75 X = 2522877
99
Y = 11110859
23 feet Y = 3386589
89 meter
Z = -17494574
62 Z = -5332346
34
XDOT = -19122
047335 XDOT = -5828
400028
YDOT = 14636
821254 feet/sec YDOT = 4461
303118 meter/sec
ZDOT = 253
683414 ZDOT = 77
322705
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 14025
51601297
00016717 00000-0 10270-3 0 9055
2 25544 51
6478 86
7773 0003528 65
4521 294
6997 15
49864039 29198
Satellite: ISS
Catalog Number: 25544
Epoch time: 14025
51601297 = yrday
fracday
Element set: 905
Inclination: 51
6478 deg
RA of node: 86
7773 deg
Eccentricity:
0003528
Arg of perigee: 65
4521 deg
Mean anomaly: 294
6997 deg
Mean motion: 15
49864039 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2919
Checksum: 347
Coasting Arc #7 (Orbit 2934)
---------------------------------------
Vector Time (GMT): 2014/026/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4192618
93 A = 6789668
80 meter
Y = 172895
20 meter E =
0006236
Z = 5332844
96 I = 51
98283
XDOT = -854
273949 Wp = 69
79842
YDOT = -7606
934748 meter/sec RA = 81
11936 deg
ZDOT = -422
502055 TA = 24
22752
MA = 24
19821
Ha = 229
027 n
mi
Hp = 220
052
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13755311
44 X = -4220145
71
Y = 567241
46 feet Y = 125856
58 meter
Z = 17496210
48 Z = 5312411
12
XDOT = -2802
736052 XDOT = -767
095652
YDOT = -24957
134999 feet/sec YDOT = -7616
000330 meter/sec
ZDOT = -1386
161597 ZDOT = -426
440449
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8395247
76 X = -2558871
52
Y = -11048171
86 feet Y = -3367482
78 meter
Z = 17409923
91 Z = 5306544
81
XDOT = 18069
862362 XDOT = 5507
694048
YDOT = -15952
416556 feet/sec YDOT = -4862
296566 meter/sec
ZDOT = -1401
548786 ZDOT = -427
192070
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 14026
54765705
00016717 00000-0 10270-3 0 9065
2 25544 51
6483 81
6677 0003570 68
9205 291
2327 15
49924926 29355
Satellite: ISS
Catalog Number: 25544
Epoch time: 14026
54765705 = yrday
fracday
Element set: 906
Inclination: 51
6483 deg
RA of node: 81
6677 deg
Eccentricity:
0003570
Arg of perigee: 68
9205 deg
Mean anomaly: 291
2327 deg
Mean motion: 15
49924926 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2935
Checksum: 334
Coasting Arc #8 (Orbit 2949)
---------------------------------------
Vector Time (GMT): 2014/027/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4242130
28 A = 6789898
73 meter
Y = -152275
73 meter E =
0017962
Z = -5314942
42 I = 51
97782
XDOT = 1228
545564 Wp = 90
96255
YDOT = 7509
831961 meter/sec RA = 76
18689 deg
ZDOT = 767
351187 TA = 186
34310
MA = 186
36587
Ha = 228
978 n
mi
Hp = 220
158
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13917750
26 X = 4269335
74
Y = -499592
30 feet Y = -104685
19 meter
Z = -17437475
12 Z = -5294268
93
XDOT = 4030
661298 XDOT = 1140
750139
YDOT = 24638
556301 feet/sec YDOT = 7523
079418 meter/sec
ZDOT = 2517
556388 ZDOT = 773
106274
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8624185
60 X = 2628651
77
Y = 11073110
00 feet Y = 3375083
93 meter
Z = -17350174
67 Z = -5288333
24
XDOT = -16806
930361 XDOT = -5122
752374
YDOT = 17060
692019 feet/sec YDOT = 5200
098927 meter/sec
ZDOT = 2540
617368 ZDOT = 774
380174
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 14027
51481522
00016717 00000-0 10270-3 0 9076
2 25544 51
6485 76
8769 0003699 71
4515 288
7037 15
49899147 29502
Satellite: ISS
Catalog Number: 25544
Epoch time: 14027
51481522 = yrday
fracday
Element set: 907
Inclination: 51
6485 deg
RA of node: 76
8769 deg
Eccentricity:
0003699
Arg of perigee: 71
4515 deg
Mean anomaly: 288
7037 deg
Mean motion: 15
49899147 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2950
Checksum: 352
Coasting Arc #9 (Orbit 2965)
---------------------------------------
Vector Time (GMT): 2014/028/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4296659
01 A = 6789942
38 meter
Y = 118507
71 meter E =
0007578
Z = 5250807
63 I = 51
96989
XDOT = -1586
327831 Wp = 65
45119
YDOT = -7415
666166 meter/sec RA = 71
25442 deg
ZDOT = -1126
362785 TA = 35
32353
MA = 35
27334
Ha = 229
080 n
mi
Hp = 219
887
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14096650
29 X = -4323171
13
Y = 388804
82 feet Y = 70311
28 meter
Z = 17227059
15 Z = 5229871
04
XDOT = -5204
487636 XDOT = -1497
814886
YDOT = -24329
613407 feet/sec YDOT = -7432
910548 meter/sec
ZDOT = -3695
415962 ZDOT = -1133
854118
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8831228
57 X = -2691758
47
Y = -11131685
96 feet Y = -3392937
88 meter
Z = 17138648
00 Z = 5223859
91
XDOT = 15549
050619 XDOT = 4739
350629
YDOT = -18094
102628 feet/sec YDOT = -5515
082481 meter/sec
ZDOT = -3725
814687 ZDOT = -1135
628317
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 14028
54643718
00016717 00000-0 10270-3 0 9088
2 25544 51
6481 71
7673 0003789 75
0950 285
0620 15
49957222 29663
Satellite: ISS
Catalog Number: 25544
Epoch time: 14028
54643718 = yrday
fracday
Element set: 908
Inclination: 51
6481 deg
RA of node: 71
7673 deg
Eccentricity:
0003789
Arg of perigee: 75
0950 deg
Mean anomaly: 285
0620 deg
Mean motion: 15
49957222 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2966
Checksum: 335
Coasting Arc #10 (Orbit 2980)
---------------------------------------
Vector Time (GMT): 2014/029/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4389875
28 A = 6790324
30 meter
Y = -109249
08 meter E =
0017277
Z = -5194554
22 I = 51
96081
XDOT = 1922
093023 Wp = 95
97070
YDOT = 7254
863706 meter/sec RA = 66
32061 deg
ZDOT = 1474
231168 TA = 188
18098
MA = 188
20919
Ha = 228
995 n
mi
Hp = 220
019
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14402477
94 X = 4416003
56
Y = -358428
75 feet Y = -60012
46 meter
Z = -17042500
73 Z = -5173165
86
XDOT = 6306
079472 XDOT = 1833
663486
YDOT = 23802
046281 feet/sec YDOT = 7275
863300 meter/sec
ZDOT = 4836
716431 ZDOT = 1483
353626
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9184297
34 X = 2799373
83
Y = 11237392
22 feet Y = 3425157
15 meter
Z = -16952178
97 Z = -5167024
15
XDOT = -14128
665481 XDOT = -4306
417239
YDOT = 18887
770214 feet/sec YDOT = 5756
992361 meter/sec
ZDOT = 4874
024030 ZDOT = 1485
602524
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 14029
51357401
00016717 00000-0 10270-3 0 9098
2 25544 51
6488 66
9763 0003835 77
5633 282
5947 15
49935181 29814
Satellite: ISS
Catalog Number: 25544
Epoch time: 14029
51357401 = yrday
fracday
Element set: 909
Inclination: 51
6488 deg
RA of node: 66
9763 deg
Eccentricity:
0003835
Arg of perigee: 77
5633 deg
Mean anomaly: 282
5947 deg
Mean motion: 15
49935181 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2981
Checksum: 346
Coasting Arc #11 (Orbit 2996)
---------------------------------------
Vector Time (GMT): 2014/030/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4488503
00 A = 6790557
15 meter
Y = 89361
31 meter E =
0009272
Z = 5088538
10 I = 51
94759
XDOT = -2233
445266 Wp = 66
01300
YDOT = -7100
003147 meter/sec RA = 61
38607 deg
ZDOT = -1839
085257 TA = 41
75788
MA = 41
68715
Ha = 229
106 n
mi
Hp = 219
749
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14726059
71 X = -4513886
49
Y = 293180
15 feet Y = 39026
05 meter
Z = 16694678
80 Z = 5066672
51
XDOT = -7327
576332 XDOT = -2144
952001
YDOT = -23293
973580 feet/sec YDOT = -7124
484158 meter/sec
ZDOT = -6033
744281 ZDOT = -1849
719823
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9526878
00 X = -2903792
41
Y = -11369077
04 feet Y = -3465294
68 meter
Z = 16602342
37 Z = 5060393
96
XDOT = 12748
981252 XDOT = 3885
889486
YDOT = -19588
540880 feet/sec YDOT = -5970
587260 meter/sec
ZDOT = -6077
459799 ZDOT = -1852
409747
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 14030
54517362
00016717 00000-0 10270-3 0 9109
2 25544 51
6475 61
8659 0003962 81
2453 278
9146 15
49990323 29977
Satellite: ISS
Catalog Number: 25544
Epoch time: 14030
54517362 = yrday
fracday
Element set: 910
Inclination: 51
6475 deg
RA of node: 61
8659 deg
Eccentricity:
0003962
Arg of perigee: 81
2453 deg
Mean anomaly: 278
9146 deg
Mean motion: 15
49990323 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2997
Checksum: 330
Coasting Arc #12 (Orbit 3011)
---------------------------------------
Vector Time (GMT): 2014/031/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4619789
50 A = 6791092
02 meter
Y = -105766
29 meter E =
0016018
Z = -4991045
66 I = 51
93450
XDOT = 2513
991690 Wp = 100
47935
YDOT = 6886
173147 meter/sec RA = 56
45059 deg
ZDOT = 2184
188192 TA = 190
76870
MA = 190
80304
Ha = 228
985 n
mi
Hp = 219
914
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15156789
70 X = 4644873
09
Y = -347002
28 feet Y = -53964
72 meter
Z = -16374821
72 Z = -4968543
05
XDOT = 8248
004232 XDOT = 2426
192320
YDOT = 22592
431585 feet/sec YDOT = 6913
795346 meter/sec
ZDOT = 7165
971757 ZDOT = 2196
187064
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10036840
62 X = 3059229
02
Y = 11498420
31 feet Y = 3504718
51 meter
Z = -16279792
13 Z = -4962080
64
XDOT = -11265
052842 XDOT = -3433
588106
YDOT = 20034
422295 feet/sec YDOT = 6106
491916 meter/sec
ZDOT = 7215
481436 ZDOT = 2199
278742
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 14031
51228873
00016717 00000-0 10270-3 0 9114
2 25544 51
6485 57
0748 0003913 83
6274 276
5322 15
49969925 30120
Satellite: ISS
Catalog Number: 25544
Epoch time: 14031
51228873 = yrday
fracday
Element set: 911
Inclination: 51
6485 deg
RA of node: 57
0748 deg
Eccentricity:
0003913
Arg of perigee: 83
6274 deg
Mean anomaly: 276
5322 deg
Mean motion: 15
49969925 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3012
Checksum: 318
Coasting Arc #13 (Orbit 3027)
---------------------------------------
Vector Time (GMT): 2014/032/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4755057
16 A = 6791503
97 meter
Y = 113982
26 meter E =
0011071
Z = 4840347
67 I = 51
91715
XDOT = -2762
421573 Wp = 69
82485
YDOT = -6682
800583 meter/sec RA = 51
51351 deg
ZDOT = -2547
939920 TA = 45
19399
MA = 45
10403
Ha = 229
079 n
mi
Hp = 219
664
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15600581
23 X = -4779490
60
Y = 373957
54 feet Y = 60671
78 meter
Z = 15880405
76 Z = 4817189
50
XDOT = -9063
062904 XDOT = -2675
110927
YDOT = -21925
198763 feet/sec YDOT = -6713
203687 meter/sec
ZDOT = -8359
382939 ZDOT = -2561
146657
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10541448
66 X = -3213033
55
Y = -11640120
21 feet Y = -3547908
64 meter
Z = 15782608
38 Z = 4810539
04
XDOT = 9863
024074 XDOT = 3006
249738
YDOT = -20378
256490 feet/sec YDOT = -6211
292578 meter/sec
ZDOT = -8414
023045 ZDOT = -2564
594224
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 14032
54386570
00016717 00000-0 10270-3 0 9128
2 25544 51
6471 51
9637 0004024 87
1898 272
9713 15
50023738 30286
Satellite: ISS
Catalog Number: 25544
Epoch time: 14032
54386570 = yrday
fracday
Element set: 912
Inclination: 51
6471 deg
RA of node: 51
9637 deg
Eccentricity:
0004024
Arg of perigee: 87
1898 deg
Mean anomaly: 272
9713 deg
Mean motion: 15
50023738 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3028
Checksum: 308
Coasting Arc #14 (Orbit 3042)
---------------------------------------
Vector Time (GMT): 2014/033/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4914115
47 A = 6792179
92 meter
Y = -168314
76 meter E =
0014259
Z = -4699379
38 I = 51
90009
XDOT = 2973
975992 Wp = 103
87830
YDOT = 6431
508594 meter/sec RA = 46
57629 deg
ZDOT = 2883
534220 TA = 194
71992
MA = 194
76148
Ha = 228
955 n
mi
Hp = 219
838
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16122426
09 X = 4938459
98
Y = -552213
77 feet Y = -113226
15 meter
Z = -15417911
36 Z = -4675448
66
XDOT = 9757
139082 XDOT = 2887
829403
YDOT = 21100
749980 feet/sec YDOT = 6464
284002 meter/sec
ZDOT = 9460
414109 ZDOT = 2897
771434
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11218774
92 X = 3419482
59
Y = 11725308
41 feet Y = 3573874
00 meter
Z = -15316846
47 Z = -4668574
80
XDOT = -8418
889269 XDOT = -2566
077449
YDOT = 20473
171292 feet/sec YDOT = 6240
222610 meter/sec
ZDOT = 9519
441310 ZDOT = 2901
525711
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 14033
51095916
00016717 00000-0 10270-3 0 9138
2 25544 51
6479 47
1728 0003950 89
6138 270
5465 15
50002908 30434
Satellite: ISS
Catalog Number: 25544
Epoch time: 14033
51095916 = yrday
fracday
Element set: 913
Inclination: 51
6479 deg
RA of node: 47
1728 deg
Eccentricity:
0003950
Arg of perigee: 89
6138 deg
Mean anomaly: 270
5465 deg
Mean motion: 15
50002908 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3043
Checksum: 306
Coasting Arc #15 (Orbit 3058)
---------------------------------------
Vector Time (GMT): 2014/034/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5074009
73 A = 6792744
52 meter
Y = 215961
49 meter E =
0012832
Z = 4501996
26 I = 51
87957
XDOT = -3146
327477 Wp = 75
78098
YDOT = -6196
728534 meter/sec RA = 41
63682 deg
ZDOT = -3238
043470 TA = 46
74061
MA = 46
63359
Ha = 229
003 n
mi
Hp = 219
631
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16647013
56 X = -5097916
44
Y = 708535
07 feet Y = 159087
29 meter
Z = 14770328
94 Z = 4477289
77
XDOT = -10322
596710 XDOT = -3061
071322
YDOT = -20330
474192 feet/sec YDOT = -6231
436298 meter/sec
ZDOT = -10623
502197 ZDOT = -3253
120141
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11886973
13 X = -3623149
41
Y = -11806627
34 feet Y = -3598660
01 meter
Z = 14665985
15 Z = 4470192
27
XDOT = 7100
928169 XDOT = 2164
362906
YDOT = -20467
634371 feet/sec YDOT = -6238
534956 meter/sec
ZDOT = -10686
105047 ZDOT = -3257
124818
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 14034
54251319
00016717 00000-0 10270-3 0 9144
2 25544 51
6469 42
0614 0003984 92
9916 267
1691 15
50057027 30591
Satellite: ISS
Catalog Number: 25544
Epoch time: 14034
54251319 = yrday
fracday
Element set: 914
Inclination: 51
6469 deg
RA of node: 42
0614 deg
Eccentricity:
0003984
Arg of perigee: 92
9916 deg
Mean anomaly: 267
1691 deg
Mean motion: 15
50057027 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3059
Checksum: 309
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