[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
July 12th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 18298 65 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
196/11:13:24
000 0
0 0
0 0
0
N/A 0
0 0
0 225
3
000/00:00:00
000 0
0 0
0 221
4
198/01:00:41
354 2
4 4
2 4
2
N/A -3
4 -0
4 225
2
000/00:01:22
709 0
2 0
1 223
6
Coasting Arc #1 (Orbit 1478)
---------------------------------------
Vector Time (GMT): 2014/190/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2171436
25 A = 6788329
60 meter
Y = -3779603
40 meter E =
0011211
Z = -5213678
55 I = 51
55902
XDOT = 7152
177757 Wp = 89
11741
YDOT = -2444
169697 meter/sec RA = 348
42716 deg
ZDOT = -1209
009060 TA = 169
26050
MA = 169
23654
Ha = 225
914 n
mi
Hp = 221
264
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7124134
69 X = -2103684
14
Y = -12400273
63 feet Y = -3803506
30 meter
Z = -17105244
57 Z = -5224062
99
XDOT = 23465
150122 XDOT = 7184
850423
YDOT = -8018
929451 feet/sec YDOT = -2364
006603 meter/sec
ZDOT = -3966
565157 ZDOT = -1174
185790
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9894372
53 X = -3015804
75
Y = 10253665
60 feet Y = 3125317
28 meter
Z = -17148562
83 Z = -5226881
95
XDOT = -13620
462031 XDOT = -4151
516827
YDOT = -19517
710017 feet/sec YDOT = -5948
998013 meter/sec
ZDOT = -3818
351644 ZDOT = -1163
833581
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 14190
51813357
00016717 00000-0 10270-3 0 9005
2 25544 51
6457 348
8738 0003478 232
7330 127
3500 15
50519584 14795
Satellite: ISS
Catalog Number: 25544
Epoch time: 14190
51813357 = yrday
fracday
Element set: 900
Inclination: 51
6457 deg
RA of node: 348
8738 deg
Eccentricity:
0003478
Arg of perigee: 232
7330 deg
Mean anomaly: 127
3500 deg
Mean motion: 15
50519584 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1479
Checksum: 314
Coasting Arc #2 (Orbit 1494)
---------------------------------------
Vector Time (GMT): 2014/191/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1889214
22 A = 6788029
15 meter
Y = 3819521
95 meter E =
0003006
Z = 5284421
39 I = 51
52713
XDOT = -7159
471217 Wp = 185
66353
YDOT = 2655
059440 meter/sec RA = 343
45761 deg
ZDOT = 637
612005 TA = 258
21832
MA = 258
25204
Ha = 225
746 n
mi
Hp = 221
445
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 6198209
39 X = 1820693
17
Y = 12531239
99 feet Y = 3840264
49 meter
Z = 17337340
52 Z = 5293432
98
XDOT = -23489
078796 XDOT = -7191
725886
YDOT = 8710
824933 feet/sec YDOT = 2574
817191 meter/sec
ZDOT = 2091
902904 ZDOT = 602
754523
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10120433
94 X = 3084708
27
Y = -9577334
66 feet Y = -2919171
60 meter
Z = 17374827
46 Z = 5295847
41
XDOT = 14679
138467 XDOT = 4474
201405
YDOT = 19054
574548 feet/sec YDOT = 5807
834322 meter/sec
ZDOT = 1943
502930 ZDOT = 592
379693
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 14191
54936479
00016717 00000-0 10270-3 0 9011
2 25544 51
6452 343
7596 0003472 238
6843 121
3969 15
50506927 14952
Satellite: ISS
Catalog Number: 25544
Epoch time: 14191
54936479 = yrday
fracday
Element set: 901
Inclination: 51
6452 deg
RA of node: 343
7596 deg
Eccentricity:
0003472
Arg of perigee: 238
6843 deg
Mean anomaly: 121
3969 deg
Mean motion: 15
50506927 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1495
Checksum: 337
Coasting Arc #3 (Orbit 1509)
---------------------------------------
Vector Time (GMT): 2014/192/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1596608
74 A = 6787730
14 meter
Y = -3917952
60 meter E =
0011936
Z = -5318154
16 I = 51
49835
XDOT = 7107
900395 Wp = 97
54000
YDOT = -2839
163753 meter/sec RA = 338
48774 deg
ZDOT = -43
892061 TA = 172
04963
MA = 172
03069
Ha = 225
659 n
mi
Hp = 221
301
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5238217
64 X = -1526845
04
Y = -12854175
19 feet Y = -3935416
09 meter
Z = -17448012
35 Z = -5325741
28
XDOT = 23319
883187 XDOT = 7139
333510
YDOT = -9314
841708 feet/sec YDOT = -2759
502879 meter/sec
ZDOT = -144
002824 ZDOT = -9
287307
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10565179
00 X = -3220266
56
Y = 8941367
92 feet Y = 2725328
94 meter
Z = -17479439
68 Z = -5327733
21
XDOT = -15578
811277 XDOT = -4748
421677
YDOT = -18391
105110 feet/sec YDOT = -5605
608838 meter/sec
ZDOT = 3
360840 ZDOT = 1
024384
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 14192
51612675
00016717 00000-0 10270-3 0 9029
2 25544 51
6465 338
9673 0003450 241
4443 118
6361 15
50571677 15109
Satellite: ISS
Catalog Number: 25544
Epoch time: 14192
51612675 = yrday
fracday
Element set: 902
Inclination: 51
6465 deg
RA of node: 338
9673 deg
Eccentricity:
0003450
Arg of perigee: 241
4443 deg
Mean anomaly: 118
6361 deg
Mean motion: 15
50571677 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1510
Checksum: 302
Coasting Arc #4 (Orbit 1525)
---------------------------------------
Vector Time (GMT): 2014/193/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1314857
42 A = 6787896
92 meter
Y = 4048913
47 meter E =
0000522
Z = 5287477
96 I = 51
47016
XDOT = -7026
161371 Wp = 252
25571
YDOT = 3006
843519 meter/sec RA = 333
51356 deg
ZDOT = -555
484698 TA = 203
06020
MA = 203
06254
Ha = 225
535 n
mi
Hp = 221
446
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4313836
68 X = 1243799
37
Y = 13283836
85 feet Y = 4063219
08 meter
Z = 17347368
62 Z = 5293693
16
XDOT = -23051
710536 XDOT = -7056
564062
YDOT = 9864
972175 feet/sec YDOT = 2928
102541 meter/sec
ZDOT = -1822
456359 ZDOT = -589
689716
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11122898
33 X = 3390259
41
Y = -8394180
76 feet Y = -2558546
29 meter
Z = 17372955
09 Z = 5295276
71
XDOT = 16370
851903 XDOT = 4989
835660
YDOT = 17620
553223 feet/sec YDOT = 5370
744622 meter/sec
ZDOT = -1968
154997 ZDOT = -599
893643
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 14193
54732504
00016717 00000-0 10270-3 0 9038
2 25544 51
6466 333
8531 0003417 247
0646 113
0145 15
50552631 15262
Satellite: ISS
Catalog Number: 25544
Epoch time: 14193
54732504 = yrday
fracday
Element set: 903
Inclination: 51
6466 deg
RA of node: 333
8531 deg
Eccentricity:
0003417
Arg of perigee: 247
0646 deg
Mean anomaly: 113
0145 deg
Mean motion: 15
50552631 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1526
Checksum: 284
Coasting Arc #5 (Orbit 1540)
---------------------------------------
Vector Time (GMT): 2014/194/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1045355
36 A = 6788062
97 meter
Y = -4231669
95 meter E =
0011174
Z = -5213488
04 I = 51
44479
XDOT = 6887
848876 Wp = 107
21944
YDOT = -3131
162393 meter/sec RA = 328
53977 deg
ZDOT = 1159
236819 TA = 173
95396
MA = 173
94047
Ha = 225
411 n
mi
Hp = 221
332
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3429643
57 X = -972633
22
Y = -13883431
58 feet Y = -4242952
63 meter
Z = -17104619
56 Z = -5218389
94
XDOT = 22597
929384 XDOT = 6916
719243
YDOT = -10272
842496 feet/sec YDOT = -3053
976731 meter/sec
ZDOT = 3803
270402 ZDOT = 1192
766164
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11847190
30 X = -3611023
60
Y = 7966938
32 feet Y = 2428322
80 meter
Z = -17124605
50 Z = -5219579
76
XDOT = -16935
506706 XDOT = -5161
942444
YDOT = -16693
541950 feet/sec YDOT = -5088
191586 meter/sec
ZDOT = 3946
121978 ZDOT = 1202
777979
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 14194
51405566
00016717 00000-0 10270-3 0 9042
2 25544 51
6475 329
0609 0003454 251
0627 109
0150 15
50621715 15418
Satellite: ISS
Catalog Number: 25544
Epoch time: 14194
51405566 = yrday
fracday
Element set: 904
Inclination: 51
6475 deg
RA of node: 329
0609 deg
Eccentricity:
0003454
Arg of perigee: 251
0627 deg
Mean anomaly: 109
0150 deg
Mean motion: 15
50621715 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1541
Checksum: 284
Coasting Arc #6 (Orbit 1556)
---------------------------------------
Vector Time (GMT): 2014/195/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 888286
5
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 795009
95 A = 6788713
69 meter
Y = 4441731
14 meter E =
0002547
Z = 5071640
68 I = 51
42104
XDOT = -6726
995944 Wp = 27
11157
YDOT = 3219
091926 meter/sec RA = 323
56253 deg
ZDOT = -1762
203851 TA = 80
01040
MA = 79
98166
Ha = 225
348 n
mi
Hp = 221
423
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2608300
36 X = 720646
51
Y = 14572608
72 feet Y = 4450205
26 meter
Z = 16639241
07 Z = 5075322
38
XDOT = -22070
196666 XDOT = -6753
932556
YDOT = 10561
325215 feet/sec YDOT = 3143
715854 meter/sec
ZDOT = -5781
508697 ZDOT = -1794
947163
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12649078
10 X = 3855439
00
Y = -7659831
54 feet Y = -2334716
65 meter
Z = 16654017
62 Z = 5076144
57
XDOT = 17328
132521 XDOT = 5281
614792
YDOT = 15722
988070 feet/sec YDOT = 4792
366764 meter/sec
ZDOT = -5921
034963 ZDOT = -1804
731457
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 14195
54522104
00016717 00000-0 10270-3 0 9055
2 25544 51
6478 323
9472 0003390 256
2504 103
8269 15
50601767 15577
Satellite: ISS
Catalog Number: 25544
Epoch time: 14195
54522104 = yrday
fracday
Element set: 905
Inclination: 51
6478 deg
RA of node: 323
9472 deg
Eccentricity:
0003390
Arg of perigee: 256
2504 deg
Mean anomaly: 103
8269 deg
Mean motion: 15
50601767 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1557
Checksum: 306
Coasting Arc #7 (Orbit 1571)
---------------------------------------
Vector Time (GMT): 2014/196/11:13:24
000
Vector Time (MET): N/A
Weight (LBS) : 898831
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 638194
63 A = 6789374
34 meter
Y = 4649214
00 meter E =
0003794
Z = 4905385
84 I = 51
39893
XDOT = -6527
305315 Wp = 39
51356
YDOT = 3304
856401 meter/sec RA = 318
74584 deg
ZDOT = -2279
215643 TA = 72
87698
MA = 72
83543
Ha = 225
308 n
mi
Hp = 221
397
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2093814
42 X = 562330
28
Y = 15253326
77 feet Y = 4655926
23 meter
Z = 16093785
58 Z = 4908302
05
XDOT = -21415
043685 XDOT = -6552
704361
YDOT = 10842
704729 feet/sec YDOT = 3231
721990 meter/sec
ZDOT = -7477
741612 ZDOT = -2310
985288
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14615053
31 X = 4454668
25
Y = -4803962
34 feet Y = -1464247
72 meter
Z = 16105282
78 Z = 4908890
19
XDOT = 14288
235251 XDOT = 4355
054105
YDOT = 17903
649208 feet/sec YDOT = 5457
032278 meter/sec
ZDOT = -7613
144336 ZDOT = -2320
486394
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 14196
51192228
00016717 00000-0 10270-3 0 9064
2 25544 51
6471 319
1534 0003339 260
2836 99
7938 15
50617288 15720
Satellite: ISS
Catalog Number: 25544
Epoch time: 14196
51192228 = yrday
fracday
Element set: 906
Inclination: 51
6471 deg
RA of node: 319
1534 deg
Eccentricity:
0003339
Arg of perigee: 260
2836 deg
Mean anomaly: 99
7938 deg
Mean motion: 15
50617288 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1572
Checksum: 328
Coasting Arc #8 (Orbit 1586)
---------------------------------------
Vector Time (GMT): 2014/197/11:13:24
000
Vector Time (MET): N/A
Weight (LBS) : 898831
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -452087
78 A = 6790186
61 meter
Y = -4918117
14 meter E =
0007467
Z = -4667251
25 I = 51
37982
XDOT = 6300
457986 Wp = 119
99745
YDOT = -3284
947701 meter/sec RA = 313
76760 deg
ZDOT = 2851
005437 TA = 178
46884
MA = 178
46655
Ha = 225
162 n
mi
Hp = 221
340
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -1483227
63 X = -374387
01
Y = -16135554
92 feet Y = -4922738
01 meter
Z = -15312504
10 Z = -4669258
89
XDOT = 20670
793916 XDOT = 6322
873701
YDOT = -10777
387472 feet/sec YDOT = -3214
366720 meter/sec
ZDOT = 9353
692377 ZDOT = 2881
666007
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15517189
70 X = -4729639
42
Y = 4641133
68 feet Y = 1414617
55 meter
Z = -15320103
80 Z = -4669567
64
XDOT = -14406
310612 XDOT = -4391
043474
YDOT = -16856
364268 feet/sec YDOT = -5137
819829 meter/sec
ZDOT = 9484
376517 ZDOT = 2890
837962
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 14197
47860720
00016717 00000-0 10270-3 0 9070
2 25544 51
6476 314
3607 0003474 266
0658 94
0096 15
50677336 15878
Satellite: ISS
Catalog Number: 25544
Epoch time: 14197
47860720 = yrday
fracday
Element set: 907
Inclination: 51
6476 deg
RA of node: 314
3607 deg
Eccentricity:
0003474
Arg of perigee: 266
0658 deg
Mean anomaly: 94
0096 deg
Mean motion: 15
50677336 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1587
Checksum: 332
Coasting Arc #9 (Orbit 1595)
---------------------------------------
Vector Time (GMT): 2014/198/01:01:22
709
Vector Time (MET): N/A
Weight (LBS) : 898418
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3170610
02 A = 6789603
78 meter
Y = -2820144
57 meter E =
0008143
Z = -5307331
37 I = 51
35900
XDOT = 5043
974208 Wp = 87
90108
YDOT = -5759
179291 meter/sec RA = 310
92924 deg
ZDOT = 47
317456 TA = 182
55023
MA = 182
55438
Ha = 225
198 n
mi
Hp = 223
639
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10402263
85 X = -3113057
90
Y = -9252442
82 feet Y = -2855278
35 meter
Z = -17412504
49 Z = -5322593
88
XDOT = 16548
471812 XDOT = 5107
769940
YDOT = -18894
945181 feet/sec YDOT = -5702
417623 meter/sec
ZDOT = 155
240997 ZDOT = 71
974760
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 641811
26 X = 195624
07
Y = -13826140
83 feet Y = -4214207
72 meter
Z = -17476727
73 Z = -5326906
61
XDOT = 24094
101770 XDOT = 7343
882220
YDOT = 790
117689 feet/sec YDOT = 240
827872 meter/sec
ZDOT = 260
912238 ZDOT = 79
526050
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 14198
05861346
00016717 00000-0 10270-3 0 9081
2 25544 51
6481 311
4869 0006716 273
5929 86
4454 15
49930432 15968
Satellite: ISS
Catalog Number: 25544
Epoch time: 14198
05861346 = yrday
fracday
Element set: 908
Inclination: 51
6481 deg
RA of node: 311
4869 deg
Eccentricity:
0006716
Arg of perigee: 273
5929 deg
Mean anomaly: 86
4454 deg
Mean motion: 15
49930432 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1596
Checksum: 343
Coasting Arc #10 (Orbit 1611)
---------------------------------------
Vector Time (GMT): 2014/199/01:01:22
709
Vector Time (MET): N/A
Weight (LBS) : 898418
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3151571
18 A = 6789521
72 meter
Y = 2864869
67 meter E =
0004631
Z = 5291334
04 I = 51
33914
XDOT = -4752
717893 Wp = 292
49447
YDOT = 5991
559614 meter/sec RA = 305
95385 deg
ZDOT = -411
776187 TA = 161
46215
MA = 161
44528
Ha = 225
278 n
mi
Hp = 223
873
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10339800
47 X = 3093597
97
Y = 9399178
70 feet Y = 2899788
18 meter
Z = 17360019
81 Z = 5306503
10
XDOT = -15592
906473 XDOT = -4817
363394
YDOT = 19657
347815 feet/sec YDOT = 5938
050226 meter/sec
ZDOT = -1350
971742 ZDOT = -435
020746
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -555995
07 X = -169467
30
Y = 13882614
74 feet Y = 4231420
97 meter
Z = 17423839
97 Z = 5310786
42
XDOT = -24059
442888 XDOT = -7333
318192
YDOT = 863
095147 feet/sec YDOT = 263
071401 meter/sec
ZDOT = -1450
682635 ZDOT = -442
168067
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
09023098
00016717 00000-0 10270-3 0 9091
2 25544 51
6477 306
3771 0006871 277
7896 82
2474 15
49979423 16127
Satellite: ISS
Catalog Number: 25544
Epoch time: 14199
09023098 = yrday
fracday
Element set: 909
Inclination: 51
6477 deg
RA of node: 306
3771 deg
Eccentricity:
0006871
Arg of perigee: 277
7896 deg
Mean anomaly: 82
2474 deg
Mean motion: 15
49979423 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1612
Checksum: 352
Coasting Arc #11 (Orbit 1626)
---------------------------------------
Vector Time (GMT): 2014/200/01:01:22
709
Vector Time (MET): N/A
Weight (LBS) : 898418
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3153223
18 A = 6789677
37 meter
Y = -2927167
28 meter E =
0007803
Z = -5259286
40 I = 51
32263
XDOT = 4442
434890 Wp = 90
97098
YDOT = -6186
388384 meter/sec RA = 300
97614 deg
ZDOT = 780
566589 TA = 186
52798
MA = 186
53815
Ha = 225
551 n
mi
Hp = 223
671
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10345220
42 X = -3094708
84
Y = -9603567
19 feet Y = -2962101
19 meter
Z = -17254876
65 Z = -5274462
24
XDOT = 14574
917619 XDOT = 4507
490614
YDOT = -20296
549815 feet/sec YDOT = -6136
346511 meter/sec
ZDOT = 2560
914007 ZDOT = 802
304835
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 466714
31 X = 142254
52
Y = -14029508
46 feet Y = -4276194
18 meter
Z = -17318716
08 Z = -5278744
66
XDOT = 23834
708258 XDOT = 7264
819077
YDOT = -2480
109073 feet/sec YDOT = -755
937246 meter/sec
ZDOT = 2654
262664 ZDOT = 809
019260
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
05736034
00016717 00000-0 10270-3 0 9103
2 25544 51
6483 301
5859 0006770 282
0911 77
9481 15
49978418 16271
Satellite: ISS
Catalog Number: 25544
Epoch time: 14200
05736034 = yrday
fracday
Element set: 910
Inclination: 51
6483 deg
RA of node: 301
5859 deg
Eccentricity:
0006770
Arg of perigee: 282
0911 deg
Mean anomaly: 77
9481 deg
Mean motion: 15
49978418 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1627
Checksum: 318
Coasting Arc #12 (Orbit 1642)
---------------------------------------
Vector Time (GMT): 2014/201/01:01:22
709
Vector Time (MET): N/A
Weight (LBS) : 898418
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3165606
75 A = 6789783
10 meter
Y = 3011643
48 meter E =
0005324
Z = 5200747
99 I = 51
30801
XDOT = -4127
813707 Wp = 321
03649
YDOT = 6346
312827 meter/sec RA = 295
99761 deg
ZDOT = -1159
073274 TA = 140
16318
MA = 140
12409
Ha = 225
801 n
mi
Hp = 223
825
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10385848
93 X = 3106431
18
Y = 9880720
08 feet Y = 3046712
11 meter
Z = 17062821
48 Z = 5215982
44
XDOT = -13542
695888 XDOT = -4192
842469
YDOT = 20821
236308 feet/sec YDOT = 6299
789437 meter/sec
ZDOT = -3802
733838 ZDOT = -1179
283012
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -402307
49 X = -122623
32
Y = 14252786
11 feet Y = 4344249
21 meter
Z = 17126897
00 Z = 5220278
21
XDOT = -23461
562224 XDOT = -7151
084166
YDOT = 4025
137683 feet/sec YDOT = 1226
861966 meter/sec
ZDOT = -3889
621280 ZDOT = -1185
556566
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
08894784
00016717 00000-0 10270-3 0 9115
2 25544 51
6481 296
4755 0006926 286
2880 73
7508 15
50027538 16432
Satellite: ISS
Catalog Number: 25544
Epoch time: 14201
08894784 = yrday
fracday
Element set: 911
Inclination: 51
6481 deg
RA of node: 296
4755 deg
Eccentricity:
0006926
Arg of perigee: 286
2880 deg
Mean anomaly: 73
7508 deg
Mean motion: 15
50027538 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1643
Checksum: 331
Coasting Arc #13 (Orbit 1657)
---------------------------------------
Vector Time (GMT): 2014/202/01:01:22
709
Vector Time (MET): N/A
Weight (LBS) : 898418
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3207211
16 A = 6790128
97 meter
Y = -3101363
84 meter E =
0006858
Z = -5124753
42 I = 51
29688
XDOT = 3802
109038 Wp = 93
02738
YDOT = -6466
185699 meter/sec RA = 291
01776 deg
ZDOT = 1535
129511 TA = 191
85169
MA = 191
86784
Ha = 225
976 n
mi
Hp = 223
559
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10522346
33 X = -3147398
40
Y = -10175078
21 feet Y = -3136894
10 meter
Z = -16813495
48 Z = -5140188
47
XDOT = 12474
111017 XDOT = 3866
675709
YDOT = -21214
520009 feet/sec YDOT = -6423
307177 meter/sec
ZDOT = 5036
514144 ZDOT = 1553
755809
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 276910
64 X = 84402
36
Y = -14559815
18 feet Y = -4437831
67 meter
Z = -16878409
93 Z = -5144539
35
XDOT = 22915
843696 XDOT = 6984
749159
YDOT = -5490
262552 feet/sec YDOT = -1673
432026 meter/sec
ZDOT = 5116
700745 ZDOT = 1559
570387
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
05604929
00016717 00000-0 10270-3 0 9124
2 25544 51
6486 291
6842 0006883 290
4179 69
6232 15
50024758 16586
Satellite: ISS
Catalog Number: 25544
Epoch time: 14202
05604929 = yrday
fracday
Element set: 912
Inclination: 51
6486 deg
RA of node: 291
6842 deg
Eccentricity:
0006883
Arg of perigee: 290
4179 deg
Mean anomaly: 69
6232 deg
Mean motion: 15
50024758 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1658
Checksum: 324
Coasting Arc #14 (Orbit 1673)
---------------------------------------
Vector Time (GMT): 2014/203/01:01:22
709
Vector Time (MET): N/A
Weight (LBS) : 898418
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3262014
91 A = 6790429
53 meter
Y = 3211750
69 meter E =
0006334
Z = 5018581
99 I = 51
28808
XDOT = -3482
615018 Wp = 345
15337
YDOT = 6545
589589 meter/sec RA = 286
03742 deg
ZDOT = -1919
866886 TA = 123
61530
MA = 123
55485
Ha = 226
212 n
mi
Hp = 223
536
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10702148
64 X = 3201479
49
Y = 10537239
80 feet Y = 3247889
72 meter
Z = 16465164
02 Z = 5034281
52
XDOT = -11425
902289 XDOT = -3546
224449
YDOT = 21475
031459 feet/sec YDOT = 6506
289256 meter/sec
ZDOT = -6298
775874 ZDOT = -1936
938709
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -158974
26 X = -48455
35
Y = 14945421
89 feet Y = 4555364
59 meter
Z = 16531186
47 Z = 5038705
64
XDOT = -22240
005429 XDOT = -6778
753655
YDOT = 6831
713159 feet/sec YDOT = 2082
306171 meter/sec
ZDOT = -6372
376868 ZDOT = -1942
300469
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
08760766
00016717 00000-0 10270-3 0 9131
2 25544 51
6486 286
5738 0007024 294
6554 65
3865 15
50075362 16744
Satellite: ISS
Catalog Number: 25544
Epoch time: 14203
08760766 = yrday
fracday
Element set: 913
Inclination: 51
6486 deg
RA of node: 286
5738 deg
Eccentricity:
0007024
Arg of perigee: 294
6554 deg
Mean anomaly: 65
3865 deg
Mean motion: 15
50075362 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1674
Checksum: 329
Coasting Arc #15 (Orbit 1688)
---------------------------------------
Vector Time (GMT): 2014/204/01:01:22
709
Vector Time (MET): N/A
Weight (LBS) : 898418
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3350864
84 A = 6790967
64 meter
Y = -3312966
13 meter E =
0005380
Z = -4894841
15 I = 51
28216
XDOT = 3161
630600 Wp = 91
37986
YDOT = -6585
825561 meter/sec RA = 281
05631 deg
ZDOT = 2295
181067 TA = 201
20024
MA = 201
22254
Ha = 226
345 n
mi
Hp = 223
288
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10993651
05 X = -3289792
17
Y = -10869311
44 feet Y = -3350095
72 meter
Z = -16059190
13 Z = -4910970
96
XDOT = 10372
803807 XDOT = 3223
890709
YDOT = -21607
039241 feet/sec YDOT = -6550
122270 meter/sec
ZDOT = 7530
121611 ZDOT = 2310
690252
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -72920
65 X = -22226
22
Y = -15388747
36 feet Y = -4690490
19 meter
Z = -16127027
61 Z = -4915518
02
XDOT = 21426
914257 XDOT = 6530
923465
YDOT = -8056
016968 feet/sec YDOT = -2455
473972 meter/sec
ZDOT = 7597
094117 ZDOT = 2315
594287
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
05468208
00016717 00000-0 10270-3 0 9146
2 25544 51
6487 281
7825 0007025 298
4748 61
5695 15
50068968 16896
Satellite: ISS
Catalog Number: 25544
Epoch time: 14204
05468208 = yrday
fracday
Element set: 914
Inclination: 51
6487 deg
RA of node: 281
7825 deg
Eccentricity:
0007025
Arg of perigee: 298
4748 deg
Mean anomaly: 61
5695 deg
Mean motion: 15
50068968 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1689
Checksum: 346
Coasting Arc #16 (Orbit 1704)
---------------------------------------
Vector Time (GMT): 2014/205/01:01:22
709
Vector Time (MET): N/A
Weight (LBS) : 898418
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3454018
06 A = 6791455
20 meter
Y = 3432078
32 meter E =
0007457
Z = 4736979
47 I = 51
27925
XDOT = -2858
730262 Wp = 5
73875
YDOT = 6582
023735 meter/sec RA = 276
07529 deg
ZDOT = -2676
740007 TA = 110
91317
MA = 110
83333
Ha = 226
560 n
mi
Hp = 223
142
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11332080
26 X = 3392372
69
Y = 11260099
48 feet Y = 3470358
26 meter
Z = 15541271
23 Z = 4753608
94
XDOT = -9379
036292 XDOT = -2919
116942
YDOT = 21594
566060 feet/sec YDOT = 6549
718177 meter/sec
ZDOT = -8781
955403 ZDOT = -2690
773180
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 313772
05 X = 95637
72
Y = 15903724
41 feet Y = 4847455
20 meter
Z = 15611216
85 Z = 4758298
90
XDOT = -20515
721299 XDOT = -6253
191852
YDOT = 9109
320295 feet/sec YDOT = 2776
520826 meter/sec
ZDOT = -8842
657289 ZDOT = -2695
241942
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
08621207
00016717 00000-0 10270-3 0 9151
2 25544 51
6487 276
6720 0007151 302
7653 57
2808 15
50121194 17055
Satellite: ISS
Catalog Number: 25544
Epoch time: 14205
08621207 = yrday
fracday
Element set: 915
Inclination: 51
6487 deg
RA of node: 276
6720 deg
Eccentricity:
0007151
Arg of perigee: 302
7653 deg
Mean anomaly: 57
2808 deg
Mean motion: 15
50121194 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1705
Checksum: 290
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