[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
January 23rd 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 21527 82 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 2872)
---------------------------------------
Vector Time (GMT): 2014/022/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4251083
18 A = 6790019
62 meter
Y = 230244
66 meter E =
0005670
Z = 5284706
15 I = 51
98008
XDOT = 725
206891 Wp = 90
96585
YDOT = -7576
998166 meter/sec RA = 100
84568 deg
ZDOT = 912
544635 TA = 350
33803
MA = 350
34893
Ha = 228
906 n
mi
Hp = 220
338
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13947123
30 X = -4279013
07
Y = 755395
86 feet Y = 182550
27 meter
Z = 17338274
77 Z = 5263987
32
XDOT = 2379
287699 XDOT = 805
447865
YDOT = -24858
917869 feet/sec YDOT = -7568
439769 meter/sec
ZDOT = 2993
912845 ZDOT = 916
262601
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -7875233
96 X = -2400371
31
Y = -11666168
12 feet Y = -3555848
04 meter
Z = 17250792
87 Z = 5258041
67
XDOT = 21684
559954 XDOT = 6609
453874
YDOT = -10181
522982 feet/sec YDOT = -3103
328205 meter/sec
ZDOT = 3010
781335 ZDOT = 917
686151
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
54995834
00016717 00000-0 10270-3 0 9003
2 25544 51
6485 101
4680 0003196 58
3461 301
8001 15
49879617 28737
Satellite: ISS
Catalog Number: 25544
Epoch time: 14022
54995834 = yrday
fracday
Element set: 900
Inclination: 51
6485 deg
RA of node: 101
4680 deg
Eccentricity:
0003196
Arg of perigee: 58
3461 deg
Mean anomaly: 301
8001 deg
Mean motion: 15
49879617 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2873
Checksum: 314
Coasting Arc #2 (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 = 4215111
46 A = 6789945
94 meter
Y = -222921
56 meter E =
0017702
Z = -5333814
50 I = 51
98352
XDOT = -333
010424 Wp = 80
98716
YDOT = 7619
023361 meter/sec RA = 95
91437 deg
ZDOT = -580
545873 TA = 183
47788
MA = 183
49021
Ha = 228
843 n
mi
Hp = 220
456
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13829105
83 X = 4243200
74
Y = -731369
95 feet Y = -175628
50 meter
Z = -17499391
41 Z = -5313269
98
XDOT = -1092
553883 XDOT = -415
363206
YDOT = 24996
795805 feet/sec YDOT = 7614
838958 meter/sec
ZDOT = -1904
678061 ZDOT = -582
363700
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7992489
37 X = 2436110
76
Y = 11442366
47 feet Y = 3487633
30 meter
Z = -17412642
90 Z = -5307373
56
XDOT = -20952
812800 XDOT = -6386
417341
YDOT = 11718
291536 feet/sec YDOT = 3571
735260 meter/sec
ZDOT = -1913
546727 ZDOT = -583
249042
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
51714582
00016717 00000-0 10270-3 0 9011
2 25544 51
6476 96
6781 0003295 60
3745 299
7734 15
49854077 28889
Satellite: ISS
Catalog Number: 25544
Epoch time: 14023
51714582 = yrday
fracday
Element set: 901
Inclination: 51
6476 deg
RA of node: 96
6781 deg
Eccentricity:
0003295
Arg of perigee: 60
3745 deg
Mean anomaly: 299
7734 deg
Mean motion: 15
49854077 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2888
Checksum: 344
Coasting Arc #3 (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 = -4179848
89 A = 6789635
95 meter
Y = 197008
62 meter E =
0005515
Z = 5342179
77 I = 51
98610
XDOT = -55
905932 Wp = 79
56702
YDOT = -7662
299105 meter/sec RA = 90
98249 deg
ZDOT = 239
590028 TA = 8
16408
MA = 8
15511
Ha = 228
919 n
mi
Hp = 220
180
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13713415
00 X = -4207691
69
Y = 646353
75 feet Y = 150111
20 meter
Z = 17526836
53 Z = 5321807
13
XDOT = -183
418411 XDOT = 28
615917
YDOT = -25138
776590 feet/sec YDOT = -7662
451692 meter/sec
ZDOT = 786
056523 ZDOT = 239
523742
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8053999
84 X = -2454859
15
Y = -11252405
19 feet Y = -3429733
10 meter
Z = 17440813
82 Z = 5315960
05
XDOT = 20181
662163 XDOT = 6151
370627
YDOT = -13229
271130 feet/sec YDOT = -4032
281840 meter/sec
ZDOT = 786
994194 ZDOT = 239
875830
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
54879511
00016717 00000-0 10270-3 0 9020
2 25544 51
6482 91
5680 0003326 63
7466 296
4026 15
49921872 29045
Satellite: ISS
Catalog Number: 25544
Epoch time: 14024
54879511 = yrday
fracday
Element set: 902
Inclination: 51
6482 deg
RA of node: 91
5680 deg
Eccentricity:
0003326
Arg of perigee: 63
7466 deg
Mean anomaly: 296
4026 deg
Mean motion: 15
49921872 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2904
Checksum: 319
Coasting Arc #4 (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 = 4186848
25 A = 6789709
02 meter
Y = -166792
96 meter E =
0018047
Z = -5358038
89 I = 51
98516
XDOT = 441
713289 Wp = 86
19828
YDOT = 7634
712740 meter/sec RA = 86
05056 deg
ZDOT = 108
974260 TA = 184
82925
MA = 184
84668
Ha = 228
871 n
mi
Hp = 220
277
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13736378
78 X = 4214429
67
Y = -547221
00 feet Y = -119818
65 meter
Z = -17578867
75 Z = -5337632
90
XDOT = 1449
190582 XDOT = 355
778039
YDOT = 25048
270144 feet/sec YDOT = 7639
171767 meter/sec
ZDOT = 357
527101 ZDOT = 110
911418
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8177074
73 X = 2492372
38
Y = 11186816
95 feet Y = 3409741
80 meter
Z = -17492704
76 Z = -5331776
41
XDOT = -19168
722613 XDOT = -5842
626652
YDOT = 14573
807456 feet/sec YDOT = 4442
096513 meter/sec
ZDOT = 364
475890 ZDOT = 111
092251
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
51595473
00016717 00000-0 10270-3 0 9031
2 25544 51
6477 86
7775 0003473 66
0954 294
0560 15
49897831 29191
Satellite: ISS
Catalog Number: 25544
Epoch time: 14025
51595473 = yrday
fracday
Element set: 903
Inclination: 51
6477 deg
RA of node: 86
7775 deg
Eccentricity:
0003473
Arg of perigee: 66
0954 deg
Mean anomaly: 294
0560 deg
Mean motion: 15
49897831 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2919
Checksum: 346
Coasting Arc #5 (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 = -4198433
76 A = 6789567
16 meter
Y = 119450
95 meter E =
0006243
Z = 5329630
21 I = 51
98283
XDOT = -816
761278 Wp = 69
46142
YDOT = -7608
284573 meter/sec RA = 81
11860 deg
ZDOT = -470
309023 TA = 25
01973
MA = 24
98949
Ha = 228
949 n
mi
Hp = 220
003
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13774388
99 X = -4225346
87
Y = 391899
44 feet Y = 72350
74 meter
Z = 17485663
43 Z = 5309169
62
XDOT = -2679
662984 XDOT = -729
338446
YDOT = -24961
563561 feet/sec YDOT = -7616
929296 meter/sec
ZDOT = -1543
008605 ZDOT = -474
064593
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8262279
69 X = -2518342
85
Y = -11164042
74 feet Y = -3402800
23 meter
Z = 17399272
59 Z = 5303298
29
XDOT = 18135
998399 XDOT = 5527
852312
YDOT = -15862
889909 feet/sec YDOT = -4835
008844 meter/sec
ZDOT = -1557
623809 ZDOT = -474
763737
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
54757433
00016717 00000-0 10270-3 0 9042
2 25544 51
6482 81
6678 0003518 69
5697 290
5831 15
49964578 29358
Satellite: ISS
Catalog Number: 25544
Epoch time: 14026
54757433 = yrday
fracday
Element set: 904
Inclination: 51
6482 deg
RA of node: 81
6678 deg
Eccentricity:
0003518
Arg of perigee: 69
5697 deg
Mean anomaly: 290
5831 deg
Mean motion: 15
49964578 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2935
Checksum: 354
Coasting Arc #6 (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 = 4253350
00 A = 6789800
72 meter
Y = -81715
51 meter E =
0017869
Z = -5307315
98 I = 51
97787
XDOT = 1178
199864 Wp = 91
50182
YDOT = 7511
306894 meter/sec RA = 76
18568 deg
ZDOT = 830
533329 TA = 186
40982
MA = 186
43271
Ha = 228
893 n
mi
Hp = 220
099
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13954560
36 X = 4279728
56
Y = -268095
51 feet Y = -34004
13 meter
Z = -17412454
00 Z = -5286589
99
XDOT = 3865
485118 XDOT = 1090
084773
YDOT = 24643
395323 feet/sec YDOT = 7523
989564 meter/sec
ZDOT = 2724
846880 ZDOT = 836
043071
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8458059
19 X = 2578016
44
Y = 11238449
67 feet Y = 3425479
46 meter
Z = -17324943
52 Z = -5280642
79
XDOT = -16896
343475 XDOT = -5150
005491
YDOT = 16940
749782 feet/sec YDOT = 5163
540534 meter/sec
ZDOT = 2746
871860 ZDOT = 837
246543
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
51470609
00016717 00000-0 10270-3 0 9058
2 25544 51
6484 76
8768 0003654 72
0596 288
0953 15
49944096 29501
Satellite: ISS
Catalog Number: 25544
Epoch time: 14027
51470609 = yrday
fracday
Element set: 905
Inclination: 51
6484 deg
RA of node: 76
8768 deg
Eccentricity:
0003654
Arg of perigee: 72
0596 deg
Mean anomaly: 288
0953 deg
Mean motion: 15
49944096 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2950
Checksum: 343
Coasting Arc #7 (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 = -4315277
90 A = 6789855
72 meter
Y = 29258
84 meter E =
0007690
Z = 5236655
82 I = 51
97003
XDOT = -1520
419611 Wp = 65
18640
YDOT = -7416
853627 meter/sec RA = 71
25273 deg
ZDOT = -1206
937484 TA = 36
36839
MA = 36
31616
Ha = 228
985 n
mi
Hp = 219
819
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14157735
91 X = -4340721
90
Y = 95993
58 feet Y = -19139
83 meter
Z = 17180629
34 Z = 5215631
38
XDOT = -4988
253316 XDOT = -1431
506886
YDOT = -24333
509274 feet/sec YDOT = -7433
358742 meter/sec
ZDOT = -3959
768649 ZDOT = -1214
107679
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8633385
73 X = -2631455
97
Y = -11355951
19 feet Y = -3461293
92 meter
Z = 17091862
06 Z = 5209599
56
XDOT = 15666
508261 XDOT = 4775
151718
YDOT = -17936
535145 feet/sec YDOT = -5467
055912 meter/sec
ZDOT = -3988
811370 ZDOT = -1215
789706
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
54629614
00016717 00000-0 10270-3 0 9065
2 25544 51
6480 71
7670 0003744 75
7213 284
4353 15
50008287 29665
Satellite: ISS
Catalog Number: 25544
Epoch time: 14028
54629614 = yrday
fracday
Element set: 906
Inclination: 51
6480 deg
RA of node: 71
7670 deg
Eccentricity:
0003744
Arg of perigee: 75
7213 deg
Mean anomaly: 284
4353 deg
Mean motion: 15
50008287 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2966
Checksum: 314
Coasting Arc #8 (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 = 4418033
80 A = 6790259
52 meter
Y = -227
79 meter E =
0017084
Z = -5171513
46 I = 51
96107
XDOT = 1838
588525 Wp = 96
64772
YDOT = 7255
982052 meter/sec RA = 66
31841 deg
ZDOT = 1572
926841 TA = 188
47347
MA = 188
50235
Ha = 228
895 n
mi
Hp = 219
941
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14494861
54 X = 4442828
96
Y = -747
35 feet Y = 49316
26 meter
Z = -16966907
68 Z = -5149991
54
XDOT = 6032
114584 XDOT = 1749
673268
YDOT = 23805
715394 feet/sec YDOT = 7276
045127 meter/sec
ZDOT = 5160
521132 ZDOT = 1581
642475
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8958195
76 X = 2730458
07
Y = 11529395
62 feet Y = 3514159
79 meter
Z = -16876040
20 Z = -5143817
05
XDOT = -14279
588230 XDOT = -4352
418492
YDOT = 18688
569562 feet/sec YDOT = 5696
276002 meter/sec
ZDOT = 5196
110895 ZDOT = 1583
774601
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
51339958
00016717 00000-0 10270-3 0 9073
2 25544 51
6487 66
9758 0003798 78
1795 281
9781 15
49991376 29818
Satellite: ISS
Catalog Number: 25544
Epoch time: 14029
51339958 = yrday
fracday
Element set: 907
Inclination: 51
6487 deg
RA of node: 66
9758 deg
Eccentricity:
0003798
Arg of perigee: 78
1795 deg
Mean anomaly: 281
9781 deg
Mean motion: 15
49991376 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2981
Checksum: 385
Coasting Arc #9 (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 = -4528305
80 A = 6790523
67 meter
Y = -40508
02 meter E =
0009517
Z = 5053663
88 I = 51
94802
XDOT = -2128
565721 Wp = 66
23527
YDOT = -7100
626495 meter/sec RA = 61
38334 deg
ZDOT = -1957
561782 TA = 42
72140
MA = 42
64745
Ha = 228
994 n
mi
Hp = 219
663
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14856646
32 X = -4552064
71
Y = -132900
34 feet Y = -91279
30 meter
Z = 16580262
06 Z = 5031608
88
XDOT = -6983
483338 XDOT = -2039
497776
YDOT = -23296
018686 feet/sec YDOT = -7123
931463 meter/sec
ZDOT = -6422
446791 ZDOT = -1967
685475
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9276340
14 X = -2827428
47
Y = -11737383
43 feet Y = -3577554
47 meter
Z = 16487147
61 Z = 5025282
59
XDOT = 12940
982149 XDOT = 3944
411359
YDOT = -19338
151571 feet/sec YDOT = -5894
268599 meter/sec
ZDOT = -6464
005178 ZDOT = -1970
228778
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
54495980
00016717 00000-0 10270-3 0 9087
2 25544 51
6474 61
8651 0003924 81
8886 278
2709 15
50052937 29972
Satellite: ISS
Catalog Number: 25544
Epoch time: 14030
54495980 = yrday
fracday
Element set: 908
Inclination: 51
6474 deg
RA of node: 61
8651 deg
Eccentricity:
0003924
Arg of perigee: 81
8886 deg
Mean anomaly: 278
2709 deg
Mean motion: 15
50052937 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2997
Checksum: 343
Coasting Arc #10 (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 = 4673367
66 A = 6791099
81 meter
Y = 45130
22 meter E =
0015667
Z = -4941492
72 I = 51
93511
XDOT = 2385
440075 Wp = 101
18445
YDOT = 6887
068850 meter/sec RA = 56
44731 deg
ZDOT = 2322
192597 TA = 191
47764
MA = 191
51341
Ha = 228
869 n
mi
Hp = 219
816
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15332571
07 X = 4696519
21
Y = 148065
04 feet Y = 97520
14 meter
Z = -16212246
46 Z = -4918734
54
XDOT = 7826
246965 XDOT = 2296
969880
YDOT = 22595
370242 feet/sec YDOT = 6913
249755 meter/sec
ZDOT = 7618
742116 ZDOT = 2333
565371
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9768420
21 X = 2977414
48
Y = 11949638
06 feet Y = 3642249
68 meter
Z = -16116163
03 Z = -4912206
49
XDOT = -11506
265941 XDOT = -3507
109859
YDOT = 19729
750521 feet/sec YDOT = 6013
627959 meter/sec
ZDOT = 7665
608087 ZDOT = 2336
477345
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
51203450
00016717 00000-0 10270-3 0 9095
2 25544 51
6484 57
0737 0003884 84
2965 275
8628 15
50037587 30121
Satellite: ISS
Catalog Number: 25544
Epoch time: 14031
51203450 = yrday
fracday
Element set: 909
Inclination: 51
6484 deg
RA of node: 57
0737 deg
Eccentricity:
0003884
Arg of perigee: 84
2965 deg
Mean anomaly: 275
8628 deg
Mean motion: 15
50037587 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3012
Checksum: 310
Coasting Arc #11 (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 = -4824224
66 A = 6791562
91 meter
Y = -58504
55 meter E =
0011456
Z = 4772338
04 I = 51
91798
XDOT = -2605
157181 Wp = 70
76847
YDOT = -6683
751377 meter/sec RA = 51
50968 deg
ZDOT = -2706
452163 TA = 45
92360
MA = 45
82934
Ha = 228
949 n
mi
Hp = 219
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15827508
73 X = -4846393
82
Y = -191944
06 feet Y = -112575
84 meter
Z = 15657277
02 Z = 4748849
37
XDOT = -8547
103611 XDOT = -2517
077608
YDOT = -21928
318167 feet/sec YDOT = -6712
391558 meter/sec
ZDOT = -8879
436231 ZDOT = -2718
893084
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10260369
43 X = -3127360
60
Y = -12180604
74 feet Y = -3712648
32 meter
Z = 15558113
20 Z = 4742112
90
XDOT = 10165
226523 XDOT = 3098
361044
YDOT = -20007
760013 feet/sec YDOT = -6098
365252 meter/sec
ZDOT = -8930
842742 ZDOT = -2722
120868
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
54356450
00016717 00000-0 10270-3 0 9100
2 25544 51
6470 51
9622 0003992 87
8931 272
2677 15
50098134 30281
Satellite: ISS
Catalog Number: 25544
Epoch time: 14032
54356450 = yrday
fracday
Element set: 910
Inclination: 51
6470 deg
RA of node: 51
9622 deg
Eccentricity:
0003992
Arg of perigee: 87
8931 deg
Mean anomaly: 272
2677 deg
Mean motion: 15
50098134 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3028
Checksum: 305
Coasting Arc #12 (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 = 5000617
60 A = 6792296
30 meter
Y = 25123
50 meter E =
0013707
Z = -4609768
51 I = 51
90117
XDOT = 2785
599070 Wp = 104
28679
YDOT = 6434
251046 meter/sec RA = 46
57194 deg
ZDOT = 3061
184723 TA = 196
25232
MA = 196
29633
Ha = 228
823 n
mi
Hp = 219
719
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16406225
71 X = 5022357
31
Y = 82426
17 feet Y = 81164
87 meter
Z = -15123912
42 Z = -4585423
92
XDOT = 9139
104559 XDOT = 2698
572863
YDOT = 21109
747525 feet/sec YDOT = 6464
914995 meter/sec
ZDOT = 10043
256964 ZDOT = 3074
504710
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10933368
92 X = 3332490
85
Y = 12358429
46 feet Y = 3766849
30 meter
Z = -15021132
74 Z = -4578441
26
XDOT = -8793
669657 XDOT = -2680
310511
YDOT = 20036
435722 feet/sec YDOT = 6107
105608 meter/sec
ZDOT = 10098
411124 ZDOT = 3077
995711
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
51061039
00016717 00000-0 10270-3 0 9115
2 25544 51
6478 47
1711 0003929 90
3805 269
7796 15
50082385 30435
Satellite: ISS
Catalog Number: 25544
Epoch time: 14033
51061039 = yrday
fracday
Element set: 911
Inclination: 51
6478 deg
RA of node: 47
1711 deg
Eccentricity:
0003929
Arg of perigee: 90
3805 deg
Mean anomaly: 269
7796 deg
Mean motion: 15
50082385 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3043
Checksum: 304
Coasting Arc #13 (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 = -5178903
61 A = 6792926
18 meter
Y = 1392
60 meter E =
0013338
Z = 4386239
51 I = 51
88092
XDOT = -2920
484066 Wp = 77
57721
YDOT = -6201
532488 meter/sec RA = 41
63196 deg
ZDOT = -3434
696235 TA = 47
18819
MA = 47
07614
Ha = 228
854 n
mi
Hp = 219
507
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16991153
57 X = -5199840
86
Y = 4568
89 feet Y = -56637
99 meter
Z = 14390549
58 Z = 4361030
70
XDOT = -9581
640636 XDOT = -2834
235717
YDOT = -20346
235197 feet/sec YDOT = -6233
709192 meter/sec
ZDOT = -11268
688435 ZDOT = -3448
673399
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11602207
35 X = -3536352
80
Y = -12535545
44 feet Y = -3820834
25 meter
Z = 14284121
35 Z = 4353800
19
XDOT = 7565
227898 XDOT = 2305
881463
YDOT = -19952
232132 feet/sec YDOT = -6081
440354 meter/sec
ZDOT = -11326
648499 ZDOT = -3452
362462
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
54210972
00016717 00000-0 10270-3 0 9122
2 25544 51
6468 42
0593 0003959 93
7938 266
3666 15
50143543 30593
Satellite: ISS
Catalog Number: 25544
Epoch time: 14034
54210972 = yrday
fracday
Element set: 912
Inclination: 51
6468 deg
RA of node: 42
0593 deg
Eccentricity:
0003959
Arg of perigee: 93
7938 deg
Mean anomaly: 266
3666 deg
Mean motion: 15
50143543 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3059
Checksum: 319
Coasting Arc #14 (Orbit 3073)
---------------------------------------
Vector Time (GMT): 2014/035/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5370927
30 A = 6793775
63 meter
Y = -82308
02 meter E =
0011426
Z = -4171076
74 I = 51
86027
XDOT = 3014
031284 Wp = 104
41382
YDOT = 5937
502449 meter/sec RA = 36
69220 deg
ZDOT = 3769
764015 TA = 204
34402
MA = 204
39803
Ha = 228
762 n
mi
Hp = 219
635
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17621152
56 X = 5391709
98
Y = -270039
44 feet Y = -22130
92 meter
Z = -13684634
97 Z = -4144935
41
XDOT = 9888
554083 XDOT = 2929
100743
YDOT = 19479
994913 feet/sec YDOT = 5970
732626 meter/sec
ZDOT = 12367
992175 ZDOT = 3784
198910
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12440447
75 X = 3791848
47
Y = 12602454
98 feet Y = 3841228
28 meter
Z = -13574260
99 Z = -4137434
75
XDOT = -6368
193728 XDOT = -1941
025448
YDOT = 19651
640173 feet/sec YDOT = 5989
819925 meter/sec
ZDOT = 12427
920337 ZDOT = 3788
030119
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 14035
50912662
00016717 00000-0 10270-3 0 9135
2 25544 51
6472 37
2683 0003958 96
4601 263
7001 15
50127807 30746
Satellite: ISS
Catalog Number: 25544
Epoch time: 14035
50912662 = yrday
fracday
Element set: 913
Inclination: 51
6472 deg
RA of node: 37
2683 deg
Eccentricity:
0003958
Arg of perigee: 96
4601 deg
Mean anomaly: 263
7001 deg
Mean motion: 15
50127807 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3074
Checksum: 295
Coasting Arc #15 (Orbit 3089)
---------------------------------------
Vector Time (GMT): 2014/036/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 911651
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5559115
41 A = 6794522
21 meter
Y = 156228
14 meter E =
0015047
Z = 3891397
40 I = 51
83735
XDOT = -3054
907789 Wp = 85
94314
YDOT = -5698
539226 meter/sec RA = 31
74987 deg
ZDOT = -4120
596433 TA = 47
24054
MA = 47
11404
Ha = 228
729 n
mi
Hp = 219
484
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18238567
63 X = -5579352
16
Y = 512559
52 feet Y = 93949
60 meter
Z = 12767051
84 Z = 3864343
16
XDOT = -10022
663351 XDOT = -2970
942106
YDOT = -18695
994836 feet/sec YDOT = -5732
231878 meter/sec
ZDOT = -13519
017169 ZDOT = -4135
232349
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13258136
30 X = -4041079
94
Y = -12650444
84 feet Y = -3855855
59 meter
Z = 12652815
75 Z = 3856578
24
XDOT = 5363
810711 XDOT = 1634
889505
YDOT = -19252
713085 feet/sec YDOT = -5868
226948 meter/sec
ZDOT = -13579
825609 ZDOT = -4139
130846
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 14036
54059456
00016717 00000-0 10270-3 0 9144
2 25544 51
6466 32
1565 0003882 99
6920 260
4669 15
50188926 30908
Satellite: ISS
Catalog Number: 25544
Epoch time: 14036
54059456 = yrday
fracday
Element set: 914
Inclination: 51
6466 deg
RA of node: 32
1565 deg
Eccentricity:
0003882
Arg of perigee: 99
6920 deg
Mean anomaly: 260
4669 deg
Mean motion: 15
50188926 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3090
Checksum: 326
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