[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
November 24th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 23142 41 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 118 0 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 827 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 1925)
---------------------------------------
Vector Time (GMT): 2013/326/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5679086
76 A = 6798337
68 meter
Y = 3068711
39 meter E =
0006817
Z = -2127376
27 I = 51
91162
XDOT = -765
318749 Wp = 45
53463
YDOT = 5240
900661 meter/sec RA = 43
35404 deg
ZDOT = 5532
455667 TA = 291
03178
MA = 291
10469
Ha = 227
138 n
mi
Hp = 220
349
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18632174
41 X = 5654684
01
Y = 10067950
76 feet Y = 3132082
21 meter
Z = -6979580
93 Z = -2099846
58
XDOT = -2510
888285 XDOT = -850
742270
YDOT = 17194
555973 feet/sec YDOT = 5231
864503 meter/sec
ZDOT = 18151
101269 ZDOT = 5528
530513
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17895636
17 X = -5454589
90
Y = 11395780
49 feet Y = 3473433
89 meter
Z = -6864291
59 Z = -2092236
08
XDOT = -12902
862250 XDOT = -3932
792414
YDOT = -9370
690787 feet/sec YDOT = -2856
186552 meter/sec
ZDOT = 18133
705046 ZDOT = 5527
153298
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 13326
50414324
00016717 00000-0 10270-3 0 9005
2 25544 51
6499 43
9685 0000645 99
9547 260
1676 15
50399847 19266
Satellite: ISS
Catalog Number: 25544
Epoch time: 13326
50414324 = yrday
fracday
Element set: 900
Inclination: 51
6499 deg
RA of node: 43
9685 deg
Eccentricity:
0000645
Arg of perigee: 99
9547 deg
Mean anomaly: 260
1676 deg
Mean motion: 15
50399847 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1926
Checksum: 335
Coasting Arc #2 (Orbit 1941)
---------------------------------------
Vector Time (GMT): 2013/327/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5865716
89 A = 6798907
15 meter
Y = -3000801
87 meter E =
0014675
Z = 1649325
62 I = 51
89059
XDOT = 935
446588 Wp = 115
50520
YDOT = -4998
764678 meter/sec RA = 38
41690 deg
ZDOT = -5734
380083 TA = 46
51873
MA = 46
39680
Ha = 227
095 n
mi
Hp = 220
175
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19244477
98 X = -5839737
36
Y = -9845150
50 feet Y = -3066250
85 meter
Z = 5411173
28 Z = 1620893
19
XDOT = 3069
050484 XDOT = 1019
130717
YDOT = -16400
146581 feet/sec YDOT = -4987
835817 meter/sec
ZDOT = -18813
582948 ZDOT = -5729
632624
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17785426
20 X = 5420997
90
Y = -12338162
00 feet Y = -3760671
78 meter
Z = 5292078
13 Z = 1613025
41
XDOT = 12049
976299 XDOT = 3672
832776
YDOT = 9261
112676 feet/sec YDOT = 2822
787144 meter/sec
ZDOT = -18792
764171 ZDOT = -5728
034519
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 13327
53542423
00016717 00000-0 10270-3 0 9012
2 25544 51
6494 38
8564 0000818 100
1907 259
9337 15
50464058 19422
Satellite: ISS
Catalog Number: 25544
Epoch time: 13327
53542423 = yrday
fracday
Element set: 901
Inclination: 51
6494 deg
RA of node: 38
8564 deg
Eccentricity:
0000818
Arg of perigee: 100
1907 deg
Mean anomaly: 259
9337 deg
Mean motion: 15
50464058 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1942
Checksum: 308
Coasting Arc #3 (Orbit 1956)
---------------------------------------
Vector Time (GMT): 2013/328/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6040315
68 A = 6799486
43 meter
Y = 2879086
72 meter E =
0009799
Z = -1185332
49 I = 51
86752
XDOT = -1132
846295 Wp = 41
07143
YDOT = 4781
992242 meter/sec RA = 33
47805 deg
ZDOT = 5877
006753 TA = 306
11655
MA = 306
20722
Ha = 227
093 n
mi
Hp = 220
208
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19817308
66 X = 6013430
25
Y = 9445822
59 feet Y = 2946483
08 meter
Z = -3888886
11 Z = -1156054
11
XDOT = -3716
687318 XDOT = -1214
784598
YDOT = 15688
950926 feet/sec YDOT = 4768
865754 meter/sec
ZDOT = 19281
518219 ZDOT = 5871
304515
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17473152
84 X = -5325816
99
Y = 13325812
13 feet Y = 4061707
54 meter
Z = -3766215
99 Z = -1147942
63
XDOT = -11227
721278 XDOT = -3422
209446
YDOT = -9312
907554 feet/sec YDOT = -2838
574222 meter/sec
ZDOT = 19256
716787 ZDOT = 5869
447277
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 13328
50223076
00016717 00000-0 10270-3 0 9021
2 25544 51
6493 34
0636 0000730 88
0635 272
0599 15
50448800 19573
Satellite: ISS
Catalog Number: 25544
Epoch time: 13328
50223076 = yrday
fracday
Element set: 902
Inclination: 51
6493 deg
RA of node: 34
0636 deg
Eccentricity:
0000730
Arg of perigee: 88
0635 deg
Mean anomaly: 272
0599 deg
Mean motion: 15
50448800 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1957
Checksum: 298
Coasting Arc #4 (Orbit 1972)
---------------------------------------
Vector Time (GMT): 2013/329/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6170426
24 A = 6799645
59 meter
Y = -2763246
03 meter E =
0013814
Z = 662268
24 I = 51
84271
XDOT = 1402
784018 Wp = 125
70725
YDOT = -4584
474237 meter/sec RA = 28
53799 deg
ZDOT = -5978
788697 TA = 47
17079
MA = 47
05478
Ha = 226
988 n
mi
Hp = 220
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20244180
56 X = -6142285
56
Y = -9065767
83 feet Y = -2832090
33 meter
Z = 2172796
07 Z = 632360
85
XDOT = 4602
309770 XDOT = 1482
988028
YDOT = -15040
925974 feet/sec YDOT = -4568
338894 meter/sec
ZDOT = -19615
448480 ZDOT = -5971
779264
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17084461
94 X = 5207344
00
Y = -14165630
22 feet Y = -4317684
09 meter
Z = 2047465
88 Z = 624067
60
XDOT = 10373
209893 XDOT = 3161
754375
YDOT = 9639
778571 feet/sec YDOT = 2938
204509 meter/sec
ZDOT = -19585
179839 ZDOT = -5969
562815
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 13329
53347205
00016717 00000-0 10270-3 0 9037
2 25544 51
6494 28
9510 0000881 91
9150 268
2102 15
50530447 19733
Satellite: ISS
Catalog Number: 25544
Epoch time: 13329
53347205 = yrday
fracday
Element set: 903
Inclination: 51
6494 deg
RA of node: 28
9510 deg
Eccentricity:
0000881
Arg of perigee: 91
9150 deg
Mean anomaly: 268
2102 deg
Mean motion: 15
50530447 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1973
Checksum: 294
Coasting Arc #5 (Orbit 1987)
---------------------------------------
Vector Time (GMT): 2013/330/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6274593
85 A = 6799885
89 meter
Y = 2600779
95 meter E =
0012579
Z = -163126
20 I = 51
81545
XDOT = -1687
444566 Wp = 46
66696
YDOT = 4429
891541 meter/sec RA = 23
59601 deg
ZDOT = 6020
413411 TA = 311
58263
MA = 311
69038
Ha = 227
064 n
mi
Hp = 220
033
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20585937
84 X = 6245837
44
Y = 8532742
62 feet Y = 2670785
67 meter
Z = -535190
95 Z = -132714
23
XDOT = -5536
235454 XDOT = -1766
101101
YDOT = 14533
764897 feet/sec YDOT = 4410
581648 meter/sec
ZDOT = 19752
012503 ZDOT = 6012
024808
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16497638
42 X = -5028480
19
Y = 14984547
24 feet Y = 4567290
00 meter
Z = -407717
53 Z = -124272
30
XDOT = -9641
718277 XDOT = -2938
795731
YDOT = -10114
009840 feet/sec YDOT = -3082
750199 meter/sec
ZDOT = 19715
967500 ZDOT = 6009
426894
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 13330
50024219
00016717 00000-0 10270-3 0 9044
2 25544 51
6491 24
1580 0000918 81
9319 278
1936 15
50501134 19884
Satellite: ISS
Catalog Number: 25544
Epoch time: 13330
50024219 = yrday
fracday
Element set: 904
Inclination: 51
6491 deg
RA of node: 24
1580 deg
Eccentricity:
0000918
Arg of perigee: 81
9319 deg
Mean anomaly: 278
1936 deg
Mean motion: 15
50501134 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1988
Checksum: 292
Coasting Arc #6 (Orbit 2003)
---------------------------------------
Vector Time (GMT): 2013/331/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6323000
54 A = 6799560
53 meter
Y = -2456308
07 meter E =
0011874
Z = -387477
25 I = 51
78730
XDOT = 2032
300017 Wp = 133
80569
YDOT = -4303
624154 meter/sec RA = 18
65223 deg
ZDOT = -6004
921999 TA = 50
35659
MA = 50
25188
Ha = 226
920 n
mi
Hp = 219
881
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20744752
42 X = -6293181
32
Y = -8058753
52 feet Y = -2526849
16 meter
Z = -1271250
83 Z = -418121
87
XDOT = 6667
650975 XDOT = 2109
443795
YDOT = -14119
501817 feet/sec YDOT = -4280
466351 meter/sec
ZDOT = -19701
187661 ZDOT = -5994
861727
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15866051
53 X = 4835972
51
Y = -15595304
87 feet Y = -4753448
92 meter
Z = -1399719
48 Z = -426634
50
XDOT = 8947
913276 XDOT = 2727
323966
YDOT = 10834
796577 feet/sec YDOT = 3302
445997 meter/sec
ZDOT = -19658
131817 ZDOT = -5991
798578
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 13331
53144463
00016717 00000-0 10270-3 0 9053
2 25544 51
6498 19
0451 0001007 89
5973 270
5294 15
50588576 20049
Satellite: ISS
Catalog Number: 25544
Epoch time: 13331
53144463 = yrday
fracday
Element set: 905
Inclination: 51
6498 deg
RA of node: 19
0451 deg
Eccentricity:
0001007
Arg of perigee: 89
5973 deg
Mean anomaly: 270
5294 deg
Mean motion: 15
50588576 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2004
Checksum: 306
Coasting Arc #7 (Orbit 2019)
---------------------------------------
Vector Time (GMT): 2013/332/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6335309
22 A = 6799341
70 meter
Y = 2277744
73 meter E =
0014484
Z = 903068
01 I = 51
75625
XDOT = -2375
886783 Wp = 56
82774
YDOT = 4232
429310 meter/sec RA = 13
70630 deg
ZDOT = 5931
357698 TA = 312
91810
MA = 313
03955
Ha = 227
024 n
mi
Hp = 219
838
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20785135
25 X = 6304981
18
Y = 7472915
77 feet Y = 2348420
61 meter
Z = 2962821
56 Z = 933771
29
XDOT = -7794
904144 XDOT = -2451
851634
YDOT = 13885
922934 feet/sec YDOT = 4205
435868 meter/sec
ZDOT = 19459
834967 ZDOT = 5919
631132
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -15069181
60 X = -4593086
55
Y = 16124721
93 feet Y = 4914815
24 meter
Z = 3091559
08 Z = 942307
21
XDOT = -8454
764261 XDOT = -2577
012147
YDOT = -11659
528268 feet/sec YDOT = -3553
824216 meter/sec
ZDOT = 19409
781812 ZDOT = 5916
101496
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 13332
56262905
00016717 00000-0 10270-3 0 9060
2 25544 51
6492 13
9325 0001137 82
8147 277
3133 15
50563110 20201
Satellite: ISS
Catalog Number: 25544
Epoch time: 13332
56262905 = yrday
fracday
Element set: 906
Inclination: 51
6492 deg
RA of node: 13
9325 deg
Eccentricity:
0001137
Arg of perigee: 82
8147 deg
Mean anomaly: 277
3133 deg
Mean motion: 15
50563110 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2020
Checksum: 275
Coasting Arc #8 (Orbit 2034)
---------------------------------------
Vector Time (GMT): 2013/333/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6284908
65 A = 6798537
71 meter
Y = -2132909
26 meter E =
0009039
Z = -1458876
85 I = 51
72506
XDOT = 2759
931811 Wp = 136
33948
YDOT = -4194
029899 meter/sec RA = 8
75778 deg
ZDOT = -5785
938037 TA = 59
53126
MA = 59
44201
Ha = 226
868 n
mi
Hp = 219
730
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20619779
04 X = -6253503
89
Y = -6997733
80 feet Y = -2203015
49 meter
Z = -4786341
38 Z = -1489332
78
XDOT = 9054
894392 XDOT = 2834
732379
YDOT = -13759
940614 feet/sec YDOT = -4162
748251 meter/sec
ZDOT = -18982
736343 ZDOT = -5772
348630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14283024
90 X = 4353465
99
Y = -16398167
25 feet Y = -4998161
38 meter
Z = -4914055
39 Z = -1497804
08
XDOT = 8059
601763 XDOT = 2456
566617
YDOT = 12664
643066 feet/sec YDOT = 3860
183207 meter/sec
ZDOT = -18924
853605 ZDOT = -5768
295379
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 13333
52934300
00016717 00000-0 10270-3 0 9073
2 25544 51
6501 9
1391 0001123 91
9434 268
1845 15
50640070 20352
Satellite: ISS
Catalog Number: 25544
Epoch time: 13333
52934300 = yrday
fracday
Element set: 907
Inclination: 51
6501 deg
RA of node: 9
1391 deg
Eccentricity:
0001123
Arg of perigee: 91
9434 deg
Mean anomaly: 268
1845 deg
Mean motion: 15
50640070 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2035
Checksum: 269
Coasting Arc #9 (Orbit 2050)
---------------------------------------
Vector Time (GMT): 2013/334/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6193626
37 A = 6797814
14 meter
Y = 1970302
35 meter E =
0015136
Z = 1968034
99 I = 51
69088
XDOT = -3125
747359 Wp = 69
48338
YDOT = 4215
582168 meter/sec RA = 3
80659 deg
ZDOT = 5587
006433 TA = 312
19092
MA = 312
31932
Ha = 226
939 n
mi
Hp = 219
662
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20320296
49 X = 6161573
28
Y = 6464246
54 feet Y = 2039384
12 meter
Z = 6456807
72 Z = 1998045
99
XDOT = -10255
076637 XDOT = -3199
795406
YDOT = 13830
650157 feet/sec YDOT = 4180
213823 meter/sec
ZDOT = 18330
073600 ZDOT = 5571
641787
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13389364
55 X = -4081078
31
Y = 16546439
08 feet Y = 5043354
63 meter
Z = 6582671
92 Z = 2006398
40
XDOT = -7914
564190 XDOT = -2412
359165
YDOT = -13708
650013 feet/sec YDOT = -4178
396524 meter/sec
ZDOT = 18264
718957 ZDOT = 5567
086338
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 13334
56048892
00016717 00000-0 10270-3 0 9081
2 25544 51
6490 4
0262 0001287 87
2985 272
8313 15
50632882 20512
Satellite: ISS
Catalog Number: 25544
Epoch time: 13334
56048892 = yrday
fracday
Element set: 908
Inclination: 51
6490 deg
RA of node: 4
0262 deg
Eccentricity:
0001287
Arg of perigee: 87
2985 deg
Mean anomaly: 272
8313 deg
Mean motion: 15
50632882 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2051
Checksum: 307
Coasting Arc #10 (Orbit 2065)
---------------------------------------
Vector Time (GMT): 2013/335/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6039164
49 A = 6796614
57 meter
Y = -1858769
68 meter E =
0006248
Z = -2502488
21 I = 51
65722
XDOT = 3506
502769 Wp = 122
92370
YDOT = -4267
444576 meter/sec RA = 358
85209 deg
ZDOT = -5305
339740 TA = 85
07658
MA = 85
00525
Ha = 226
809 n
mi
Hp = 219
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19813531
78 X = -6005773
78
Y = -6098325
73 feet Y = -1926116
60 meter
Z = -8210263
16 Z = -2531745
61
XDOT = 11504
274175 XDOT = 3579
734150
YDOT = -14000
802416 feet/sec YDOT = -4227
822820 meter/sec
ZDOT = -17405
970276 ZDOT = -5288
127481
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 12580027
51 X = 3834392
38
Y = -16415800
55 feet Y = -5003536
01 meter
Z = -8332973
03 Z = -2539890
18
XDOT = 7903
196230 XDOT = 2408
894211
YDOT = 14833
739691 feet/sec YDOT = 4521
323858 meter/sec
ZDOT = -17332
833520 ZDOT = -5283
047657
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 13335
52716767
00016717 00000-0 10270-3 0 9092
2 25544 51
6496 359
2324 0001189 95
5011 264
6275 15
50690645 20668
Satellite: ISS
Catalog Number: 25544
Epoch time: 13335
52716767 = yrday
fracday
Element set: 909
Inclination: 51
6496 deg
RA of node: 359
2324 deg
Eccentricity:
0001189
Arg of perigee: 95
5011 deg
Mean anomaly: 264
6275 deg
Mean motion: 15
50690645 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2066
Checksum: 324
Coasting Arc #11 (Orbit 2081)
---------------------------------------
Vector Time (GMT): 2013/336/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5845168
44 A = 6795464
97 meter
Y = 1747322
27 meter E =
0014401
Z = 2978759
73 I = 51
62141
XDOT = -3853
921988 Wp = 83
67168
YDOT = 4375
970025 meter/sec RA = 353
89426 deg
ZDOT = 4976
412940 TA = 310
36265
MA = 310
48831
Ha = 226
803 n
mi
Hp = 219
542
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19177061
82 X = 5810724
78
Y = 5732684
61 feet Y = 1812493
81 meter
Z = 9772833
77 Z = 3007072
09
XDOT = -12644
101012 XDOT = -3926
743160
YDOT = 14356
857037 feet/sec YDOT = 4332
465406 meter/sec
ZDOT = 16326
814109 ZDOT = 4957
514072
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11737017
03 X = -3577442
79
Y = 16140959
95 feet Y = 4919764
59 meter
Z = 9891587
14 Z = 3014955
76
XDOT = -8153
727731 XDOT = -2485
256212
YDOT = -15923
393552 feet/sec YDOT = -4853
450355 meter/sec
ZDOT = 16246
561959 ZDOT = 4951
952085
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 13336
55827511
00016717 00000-0 10270-3 0 9108
2 25544 51
6484 354
1189 0001314 92
8615 267
2686 15
50704196 20828
Satellite: ISS
Catalog Number: 25544
Epoch time: 13336
55827511 = yrday
fracday
Element set: 910
Inclination: 51
6484 deg
RA of node: 354
1189 deg
Eccentricity:
0001314
Arg of perigee: 92
8615 deg
Mean anomaly: 267
2686 deg
Mean motion: 15
50704196 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2082
Checksum: 310
Coasting Arc #12 (Orbit 2096)
---------------------------------------
Vector Time (GMT): 2013/337/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5595526
99 A = 6794028
07 meter
Y = -1703024
83 meter E =
0006251
Z = -3462264
07 I = 51
58663
XDOT = 4188
100749 Wp = 88
46176
YDOT = -4503
821654 meter/sec RA = 348
93279 deg
ZDOT = -4560
213547 TA = 132
08794
MA = 132
03476
Ha = 226
742 n
mi
Hp = 219
464
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18358028
17 X = -5559248
52
Y = -5587351
81 feet Y = -1765394
37 meter
Z = -11359134
09 Z = -3489359
09
XDOT = 13740
488021 XDOT = 4260
304813
YDOT = -14776
317763 feet/sec YDOT = -4456
583459 meter/sec
ZDOT = -14961
330534 ZDOT = -4539
692913
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11058972
00 X = 3370774
66
Y = -15599364
16 feet Y = -4754686
20 meter
Z = -11472776
55 Z = -3496902
29
XDOT = 8536
179076 XDOT = 2601
827382
YDOT = 16974
418298 feet/sec YDOT = 5173
802697 meter/sec
ZDOT = -14874
232543 ZDOT = -4533
666079
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 13337
52491901
00016717 00000-0 10270-3 0 9117
2 25544 51
6485 349
3247 0001223 98
5536 261
5753 15
50743073 20979
Satellite: ISS
Catalog Number: 25544
Epoch time: 13337
52491901 = yrday
fracday
Element set: 911
Inclination: 51
6485 deg
RA of node: 349
3247 deg
Eccentricity:
0001223
Arg of perigee: 98
5536 deg
Mean anomaly: 261
5753 deg
Mean motion: 15
50743073 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2097
Checksum: 310
Coasting Arc #13 (Orbit 2112)
---------------------------------------
Vector Time (GMT): 2013/338/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5313597
65 A = 6792651
80 meter
Y = 1675542
80 meter E =
0012404
Z = 3876532
82 I = 51
55128
XDOT = -4478
301244 Wp = 98
62374
YDOT = 4677
051078 meter/sec RA = 343
96778 deg
ZDOT = 4103
824195 TA = 308
20095
MA = 308
31259
Ha = 226
644 n
mi
Hp = 219
474
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17433063
15 X = 5275635
13
Y = 5497187
68 feet Y = 1734750
17 meter
Z = 12718283
54 Z = 3902253
99
XDOT = -14692
589382 XDOT = -4550
203663
YDOT = 15344
655767 feet/sec YDOT = 4626
569402 meter/sec
ZDOT = 13463
990142 ZDOT = 4081
894662
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10424610
21 X = -3177421
19
Y = 14923228
08 feet Y = 4548599
92 meter
Z = 12826155
51 Z = 3909412
20
XDOT = -9151
015398 XDOT = -2789
229493
YDOT = -17920
988546 feet/sec YDOT = -5462
317309 meter/sec
ZDOT = 13370
934808 ZDOT = 4075
460929
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 13338
55598823
00016717 00000-0 10270-3 0 9123
2 25544 51
6477 344
2106 0001252 97
8783 262
2510 15
50769848 21132
Satellite: ISS
Catalog Number: 25544
Epoch time: 13338
55598823 = yrday
fracday
Element set: 912
Inclination: 51
6477 deg
RA of node: 344
2106 deg
Eccentricity:
0001252
Arg of perigee: 97
8783 deg
Mean anomaly: 262
2510 deg
Mean motion: 15
50769848 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2113
Checksum: 319
Coasting Arc #14 (Orbit 2127)
---------------------------------------
Vector Time (GMT): 2013/339/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4991831
43 A = 6791206
81 meter
Y = -1726675
28 meter E =
0009522
Z = -4278252
45 I = 51
51732
XDOT = 4728
883767 Wp = 73
17421
YDOT = -4850
127672 meter/sec RA = 338
99912 deg
ZDOT = -3564
042749 TA = 160
34412
MA = 160
30739
Ha = 226
675 n
mi
Hp = 219
346
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16377399
71 X = -4951369
70
Y = -5664945
13 feet Y = -1782270
47 meter
Z = -14036261
31 Z = -4302404
28
XDOT = 15514
710523 XDOT = 4800
080719
YDOT = -15912
492362 feet/sec YDOT = -4796
847860 meter/sec
ZDOT = -11693
053638 ZDOT = -3540
897702
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10027586
35 X = 3056408
32
Y = -14032294
71 feet Y = -4277043
43 meter
Z = -14137527
14 Z = -4309118
27
XDOT = 9851
883399 XDOT = 3002
854060
YDOT = 18709
247668 feet/sec YDOT = 5702
578689 meter/sec
ZDOT = -11594
856778 ZDOT = -3534
112346
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 13339
52259739
00016717 00000-0 10270-3 0 9132
2 25544 51
6477 339
4161 0001247 101
3459 258
7832 15
50796026 21285
Satellite: ISS
Catalog Number: 25544
Epoch time: 13339
52259739 = yrday
fracday
Element set: 913
Inclination: 51
6477 deg
RA of node: 339
4161 deg
Eccentricity:
0001247
Arg of perigee: 101
3459 deg
Mean anomaly: 258
7832 deg
Mean motion: 15
50796026 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2128
Checksum: 321
Coasting Arc #15 (Orbit 2143)
---------------------------------------
Vector Time (GMT): 2013/340/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886492
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4649719
64 A = 6789878
96 meter
Y = 1807528
06 meter E =
0009477
Z = 4600269
64 I = 51
48425
XDOT = -4931
267474 Wp = 112
79748
YDOT = 5050
453570 meter/sec RA = 334
02730 deg
ZDOT = 2991
335476 TA = 307
24612
MA = 307
33253
Ha = 226
500 n
mi
Hp = 219
426
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15254985
69 X = 4606815
02
Y = 5930210
17 feet Y = 1859283
94 meter
Z = 15092748
17 Z = 4622753
49
XDOT = -16178
699062 XDOT = -5001
907359
YDOT = 16569
729560 feet/sec YDOT = 4994
913796 meter/sec
ZDOT = 9814
092770 ZDOT = 2967
208628
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9741053
50 X = -2969073
11
Y = 13043784
84 feet Y = 3975745
62 meter
Z = 15186987
26 Z = 4628993
72
XDOT = -10717
243959 XDOT = -3266
615959
YDOT = -19343
424331 feet/sec YDOT = -5895
875736 meter/sec
ZDOT = 9711
735609 ZDOT = 2960
137014
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 13340
55362862
00016717 00000-0 10270-3 0 9140
2 25544 51
6472 334
3020 0001174 101
8108 258
3174 15
50828119 21445
Satellite: ISS
Catalog Number: 25544
Epoch time: 13340
55362862 = yrday
fracday
Element set: 914
Inclination: 51
6472 deg
RA of node: 334
3020 deg
Eccentricity:
0001174
Arg of perigee: 101
8108 deg
Mean anomaly: 258
3174 deg
Mean motion: 15
50828119 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2144
Checksum: 279
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