[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
March 20th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 26909 78 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 124 4 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 3 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
087/22:40:51
098 -1
0 2
7 2
7
N/A 2
3 -0
2 226
3
000/00:05:42
195 -0
9 -0
0 220
9
Coasting Arc #1 (Orbit 3741)
---------------------------------------
Vector Time (GMT): 2014/078/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5681671
57 A = 6796062
65 meter
Y = -2488831
06 meter E =
0012030
Z = 2760256
75 I = 51
63487
XDOT = 4188
877812 Wp = 65
54694
YDOT = -3850
761910 meter/sec RA = 183
03006 deg
ZDOT = 5137
446795 TA = 325
68632
MA = 325
76397
Ha = 225
861 n
mi
Hp = 220
837
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18640654
75 X = -5666827
13
Y = -8165456
22 feet Y = -2552283
77 meter
Z = 9055960
46 Z = 2732692
26
XDOT = 13743
037440 XDOT = 4206
670386
YDOT = -12633
733302 feet/sec YDOT = -3803
819004 meter/sec
ZDOT = 16855
140402 ZDOT = 5157
839609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18103782
29 X = -5518032
84
Y = -9406981
79 feet Y = -2867248
05 meter
Z = 8939847
04 Z = 2724865
38
XDOT = 13772
196418 XDOT = 4197
765468
YDOT = -10363
816880 feet/sec YDOT = -3158
891385 meter/sec
ZDOT = 16941
797011 ZDOT = 5163
859729
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 14078
55893889
00016717 00000-0 10270-3 0 9002
2 25544 51
6499 183
8210 0003344 316
8095 43
2794 15
50740152 37420
Satellite: ISS
Catalog Number: 25544
Epoch time: 14078
55893889 = yrday
fracday
Element set: 900
Inclination: 51
6499 deg
RA of node: 183
8210 deg
Eccentricity:
0003344
Arg of perigee: 316
8095 deg
Mean anomaly: 43
2794 deg
Mean motion: 15
50740152 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3742
Checksum: 326
Coasting Arc #2 (Orbit 3756)
---------------------------------------
Vector Time (GMT): 2014/079/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5461403
73 A = 6794736
28 meter
Y = 2395961
05 meter E =
0003025
Z = -3260069
51 I = 51
66129
XDOT = -4552
956437 Wp = 51
14949
YDOT = 3913
557099 meter/sec RA = 178
07328 deg
ZDOT = -4752
188851 TA = 166
55018
MA = 166
54211
Ha = 225
844 n
mi
Hp = 220
798
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 17917991
23 X = 5450042
11
Y = 7860764
61 feet Y = 2456970
05 meter
Z = -10695766
11 Z = -3233566
51
XDOT = -14937
521118 XDOT = -4573
295582
YDOT = 12839
754263 feet/sec YDOT = 3862
528729 meter/sec
ZDOT = -15591
170771 ZDOT = -4774
356469
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17566747
43 X = 5354344
62
Y = 8753932
32 feet Y = 2668198
57 meter
Z = -10584115
29 Z = -3226038
34
XDOT = -14827
903540 XDOT = -4519
544999
YDOT = 10795
373675 feet/sec YDOT = 3290
429896 meter/sec
ZDOT = -15685
344572 ZDOT = -4780
893025
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 14079
52557566
00016717 00000-0 10270-3 0 9010
2 25544 51
6495 179
0281 0003431 320
6520 39
4381 15
50763689 37579
Satellite: ISS
Catalog Number: 25544
Epoch time: 14079
52557566 = yrday
fracday
Element set: 901
Inclination: 51
6495 deg
RA of node: 179
0281 deg
Eccentricity:
0003431
Arg of perigee: 320
6520 deg
Mean anomaly: 39
4381 deg
Mean motion: 15
50763689 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3757
Checksum: 323
Coasting Arc #3 (Orbit 3772)
---------------------------------------
Vector Time (GMT): 2014/080/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5185978
41 A = 6793220
81 meter
Y = -2326573
00 meter E =
0009984
Z = 3710161
13 I = 51
68769
XDOT = 4896
700472 Wp = 79
42146
YDOT = -4023
785920 meter/sec RA = 173
11584 deg
ZDOT = 4313
176551 TA = 324
73540
MA = 324
80142
Ha = 225
966 n
mi
Hp = 220
536
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17014364
86 X = -5177599
58
Y = -7633113
51 feet Y = -2384518
71 meter
Z = 12172444
66 Z = 3684988
84
XDOT = 16065
290263 XDOT = 4920
379279
YDOT = -13201
397376 feet/sec YDOT = -3968
895039 meter/sec
ZDOT = 14150
841702 ZDOT = 4337
022080
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16828381
54 X = -5129290
69
Y = -8193234
32 feet Y = -2497297
82 meter
Z = 12066396
67 Z = 3677837
71
XDOT = 15806
869707 XDOT = 4817
933887
YDOT = -11437
428927 feet/sec YDOT = -3486
128337 meter/sec
ZDOT = 14252
133078 ZDOT = 4344
050162
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 14080
55662521
00016717 00000-0 10270-3 0 9024
2 25544 51
6493 173
9141 0003489 326
2341 33
8587 15
50829073 37735
Satellite: ISS
Catalog Number: 25544
Epoch time: 14080
55662521 = yrday
fracday
Element set: 902
Inclination: 51
6493 deg
RA of node: 173
9141 deg
Eccentricity:
0003489
Arg of perigee: 326
2341 deg
Mean anomaly: 33
8587 deg
Mean motion: 15
50829073 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3773
Checksum: 313
Coasting Arc #4 (Orbit 3787)
---------------------------------------
Vector Time (GMT): 2014/081/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4866970
98 A = 6791786
74 meter
Y = 2318392
77 meter E =
0007591
Z = -4139512
56 I = 51
71297
XDOT = -5199
902818 Wp = 44
00722
YDOT = 4146
926197 meter/sec RA = 168
16000 deg
ZDOT = -3790
020442 TA = 186
88090
MA = 186
89133
Ha = 225
949 n
mi
Hp = 220
528
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15967752
56 X = 4860792
95
Y = 7606275
49 feet Y = 2372783
45 meter
Z = -13581077
94 Z = -4115884
64
XDOT = -17060
048614 XDOT = -5227
477454
YDOT = 13605
400908 feet/sec YDOT = 4088
623037 meter/sec
ZDOT = -12434
450270 ZDOT = -3815
348251
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15929608
49 X = 4855344
67
Y = 7859120
49 feet Y = 2395459
93 meter
Z = -13481543
86 Z = -4109174
57
XDOT = -16622
721907 XDOT = -5066
605637
YDOT = 12171
394599 feet/sec YDOT = 3709
841074 meter/sec
ZDOT = -12542
037308 ZDOT = -3822
812971
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 14081
52320981
00016717 00000-0 10270-3 0 9034
2 25544 51
6486 169
1208 0003576 330
2927 29
8021 15
50840150 37883
Satellite: ISS
Catalog Number: 25544
Epoch time: 14081
52320981 = yrday
fracday
Element set: 903
Inclination: 51
6486 deg
RA of node: 169
1208 deg
Eccentricity:
0003576
Arg of perigee: 330
2927 deg
Mean anomaly: 29
8021 deg
Mean motion: 15
50840150 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3788
Checksum: 301
Coasting Arc #5 (Orbit 3803)
---------------------------------------
Vector Time (GMT): 2014/082/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4499766
17 A = 6790227
54 meter
Y = -2351280
32 meter E =
0006912
Z = 4503005
01 I = 51
73885
XDOT = 5470
489239 Wp = 90
23062
YDOT = -4301
018943 meter/sec RA = 163
20313 deg
ZDOT = 3216
448792 TA = 327
44887
MA = 327
49146
Ha = 226
069 n
mi
Hp = 220
219
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14763012
37 X = -4495013
33
Y = -7714174
28 feet Y = -2401572
65 meter
Z = 14773638
50 Z = 4481157
54
XDOT = 17947
799340 XDOT = 5502
553156
YDOT = -14110
954537 feet/sec YDOT = -4239
664885 meter/sec
ZDOT = 10552
653517 ZDOT = 3243
101866
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14865330
86 X = -4530952
85
Y = -7693329
77 feet Y = -2344926
91 meter
Z = 14681622
16 Z = 4474958
43
XDOT = 17301
754405 XDOT = 5273
574743
YDOT = -13049
715711 feet/sec YDOT = -3977
553349 meter/sec
ZDOT = 10665
878923 ZDOT = 3250
959896
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 14082
55420377
00016717 00000-0 10270-3 0 9049
2 25544 51
6488 164
0061 0003656 335
2458 24
8517 15
50911702 38045
Satellite: ISS
Catalog Number: 25544
Epoch time: 14082
55420377 = yrday
fracday
Element set: 904
Inclination: 51
6488 deg
RA of node: 164
0061 deg
Eccentricity:
0003656
Arg of perigee: 335
2458 deg
Mean anomaly: 24
8517 deg
Mean motion: 15
50911702 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3804
Checksum: 298
Coasting Arc #6 (Orbit 3818)
---------------------------------------
Vector Time (GMT): 2014/083/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4110655
38 A = 6788976
69 meter
Y = 2453244
89 meter E =
0011808
Z = -4825058
14 I = 51
76335
XDOT = -5674
495271 Wp = 53
59451
YDOT = 4445
728918 meter/sec RA = 158
24773 deg
ZDOT = -2571
498120 TA = 191
06714
MA = 191
09313
Ha = 226
073 n
mi
Hp = 220
204
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13486402
16 X = 4106355
61
Y = 8048703
69 feet Y = 2499188
43 meter
Z = -15830243
24 Z = -4805099
89
XDOT = -18617
110470 XDOT = -5711
295215
YDOT = 14585
724796 feet/sec YDOT = 4382
067099 meter/sec
ZDOT = -8436
673622 ZDOT = -2599
153647
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13731909
92 X = 4185486
14
Y = 7794397
09 feet Y = 2375732
23 meter
Z = -15746215
39 Z = -4799446
45
XDOT = -17722
240997 XDOT = -5401
739056
YDOT = 13925
041965 feet/sec YDOT = 4244
352791 meter/sec
ZDOT = -8554
172589 ZDOT = -2607
311805
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 14083
52073689
00016717 00000-0 10270-3 0 9058
2 25544 51
6480 159
2122 0003739 339
8879 20
2124 15
50916860 38190
Satellite: ISS
Catalog Number: 25544
Epoch time: 14083
52073689 = yrday
fracday
Element set: 905
Inclination: 51
6480 deg
RA of node: 159
2122 deg
Eccentricity:
0003739
Arg of perigee: 339
8879 deg
Mean anomaly: 20
2124 deg
Mean motion: 15
50916860 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3819
Checksum: 322
Coasting Arc #7 (Orbit 3834)
---------------------------------------
Vector Time (GMT): 2014/084/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3685971
52 A = 6787712
47 meter
Y = -2608559
04 meter E =
0003707
Z = 5064441
29 I = 51
78904
XDOT = 5839
429230 Wp = 82
93464
YDOT = -4596
343610 meter/sec RA = 153
29182 deg
ZDOT = 1881
828675 TA = 348
85621
MA = 348
86442
Ha = 226
168 n
mi
Hp = 219
877
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12093082
40 X = -3681129
32
Y = -8558264
56 feet Y = -2649750
38 meter
Z = 16615621
04 Z = 5046547
51
XDOT = 19158
232382 XDOT = 5881
251328
YDOT = -15079
867488 feet/sec YDOT = -4530
809348 meter/sec
ZDOT = 6173
978591 ZDOT = 1910
297605
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12494663
00 X = -3808373
28
Y = -8115800
06 feet Y = -2473695
86 meter
Z = 16540332
01 Z = 5041493
20
XDOT = 17976
598310 XDOT = 5479
267165
YDOT = -14841
523506 feet/sec YDOT = -4523
696365 meter/sec
ZDOT = 6294
952333 ZDOT = 1918
701471
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 14084
55167628
00016717 00000-0 10270-3 0 9060
2 25544 51
6487 154
0974 0003820 344
3720 15
7312 15
50990960 38351
Satellite: ISS
Catalog Number: 25544
Epoch time: 14084
55167628 = yrday
fracday
Element set: 906
Inclination: 51
6487 deg
RA of node: 154
0974 deg
Eccentricity:
0003820
Arg of perigee: 344
3720 deg
Mean anomaly: 15
7312 deg
Mean motion: 15
50990960 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3835
Checksum: 315
Coasting Arc #8 (Orbit 3849)
---------------------------------------
Vector Time (GMT): 2014/085/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3267807
37 A = 6786960
51 meter
Y = 2830824
02 meter E =
0014558
Z = -5244170
56 I = 51
81319
XDOT = -5922
085855 Wp = 65
75403
YDOT = 4709
904187 meter/sec RA = 148
33701 deg
ZDOT = -1144
496763 TA = 193
25811
MA = 193
29641
Ha = 226
204 n
mi
Hp = 219
829
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 10721152
78 X = 3261383
86
Y = 9287480
37 feet Y = 2867330
23 meter
Z = -17205283
98 Z = -5228312
07
XDOT = -19429
415535 XDOT = -5968
753372
YDOT = 15452
441558 feet/sec YDOT = 4643
418562 meter/sec
ZDOT = -3754
910641 ZDOT = -1173
379053
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11304699
58 X = 3445672
43
Y = 8700206
20 feet Y = 2651822
85 meter
Z = -17138622
61 Z = -5223852
17
XDOT = -17926
458930 XDOT = -5463
984682
YDOT = 15632
764380 feet/sec YDOT = 4764
866583 meter/sec
ZDOT = -3877
661575 ZDOT = -1181
911248
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 14085
51815866
00016717 00000-0 10270-3 0 9072
2 25544 51
6480 149
3028 0003908 349
5212 10
5857 15
50994650 38505
Satellite: ISS
Catalog Number: 25544
Epoch time: 14085
51815866 = yrday
fracday
Element set: 907
Inclination: 51
6480 deg
RA of node: 149
3028 deg
Eccentricity:
0003908
Arg of perigee: 349
5212 deg
Mean anomaly: 10
5857 deg
Mean motion: 15
50994650 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3850
Checksum: 321
Coasting Arc #9 (Orbit 3865)
---------------------------------------
Vector Time (GMT): 2014/086/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2829955
63 A = 6786311
57 meter
Y = -3110145
05 meter E =
0003763
Z = 5324587
17 I = 51
83818
XDOT = 5966
874006 Wp = 34
06205
YDOT = -4798
046039 meter/sec RA = 143
38279 deg
ZDOT = 371
648925 TA = 52
41988
MA = 52
38571
Ha = 226
260 n
mi
Hp = 219
502
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -9284631
32 X = -2820831
90
Y = -10203887
95 feet Y = -3141739
72 meter
Z = 17469118
03 Z = 5310862
32
XDOT = 19576
358286 XDOT = 6018
278029
YDOT = -15741
620863 feet/sec YDOT = -4731
033161 meter/sec
ZDOT = 1219
320620 ZDOT = 400
760417
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10085583
78 X = -3074085
94
Y = -9519142
26 feet Y = -2901434
56 meter
Z = 17411511
22 Z = 5307028
62
XDOT = 17723
036715 XDOT = 5401
981591
YDOT = -16338
583488 feet/sec YDOT = -4980
000247 meter/sec
ZDOT = 1343
065090 ZDOT = 409
366239
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 14086
54904405
00016717 00000-0 10270-3 0 9085
2 25544 51
6485 144
1881 0003970 353
9872 6
1231 15
51072220 38665
Satellite: ISS
Catalog Number: 25544
Epoch time: 14086
54904405 = yrday
fracday
Element set: 908
Inclination: 51
6485 deg
RA of node: 144
1881 deg
Eccentricity:
0003970
Arg of perigee: 353
9872 deg
Mean anomaly: 6
1231 deg
Mean motion: 15
51072220 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3866
Checksum: 304
Coasting Arc #10 (Orbit 3880)
---------------------------------------
Vector Time (GMT): 2014/087/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 886406
0
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2429258
02 A = 6786307
84 meter
Y = 3442086
02 meter E =
0015063
Z = -5332724
44 I = 51
86221
XDOT = -5928
340935 Wp = 77
60593
YDOT = 4821
657224 meter/sec RA = 138
42936 deg
ZDOT = 415
763003 TA = 196
33050
MA = 196
37909
Ha = 226
328 n
mi
Hp = 219
422
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7970006
62 X = 2416491
83
Y = 11292933
13 feet Y = 3469179
39 meter
Z = -17495815
08 Z = -5320955
01
XDOT = -19449
937450 XDOT = -5983
836819
YDOT = 15819
085380 feet/sec YDOT = 4755
052476 meter/sec
ZDOT = 1364
051848 ZDOT = 386
828602
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9033400
99 X = 2753380
62
Y = 10543789
36 feet Y = 3213747
00 meter
Z = -17446520
06 Z = -5317699
31
XDOT = -17235
288398 XDOT = -5253
315904
YDOT = 16797
345528 feet/sec YDOT = 5119
830917 meter/sec
ZDOT = 1241
041617 ZDOT = 378
269485
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 14087
51547591
00016717 00000-0 10270-3 0 9093
2 25544 51
6481 139
3927 0004076 359
0837 1
0306 15
51074862 38812
Satellite: ISS
Catalog Number: 25544
Epoch time: 14087
51547591 = yrday
fracday
Element set: 909
Inclination: 51
6481 deg
RA of node: 139
3927 deg
Eccentricity:
0004076
Arg of perigee: 359
0837 deg
Mean anomaly: 1
0306 deg
Mean motion: 15
51074862 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3881
Checksum: 319
Coasting Arc #11 (Orbit 3887)
---------------------------------------
Vector Time (GMT): 2014/087/22:43:42
195
Vector Time (MET): N/A
Weight (LBS) : 886141
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4294636
14 A = 6788769
31 meter
Y = 1404377
86 meter E =
0012558
Z = -5077817
73 I = 51
87754
XDOT = -4225
885431 Wp = 59
11001
YDOT = 6095
755624 meter/sec RA = 136
23753 deg
ZDOT = -1885
376784 TA = 192
62511
MA = 192
65660
Ha = 226
330 n
mi
Hp = 220
883
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14090013
58 X = 4303279
22
Y = 4607538
91 feet Y = 1452450
81 meter
Z = -16659506
99 Z = -5056934
27
XDOT = -13864
453514 XDOT = -4284
576936
YDOT = 19999
198241 feet/sec YDOT = 6048
170617 meter/sec
ZDOT = -6185
619371 ZDOT = -1906
048945
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12708817
57 X = -3873647
59
Y = -7821252
41 feet Y = -2383917
74 meter
Z = -16571392
13 Z = -5050960
32
XDOT = 17578
438968 XDOT = 5357
908198
YDOT = -15250
817919 feet/sec YDOT = -4648
449302 meter/sec
ZDOT = -6273
871959 ZDOT = -1912
276173
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 14087
96647124
00016717 00000-0 10270-3 0 9107
2 25544 51
6493 137
1553 0003781 331
4982 28
5961 15
50631499 38885
Satellite: ISS
Catalog Number: 25544
Epoch time: 14087
96647124 = yrday
fracday
Element set: 910
Inclination: 51
6493 deg
RA of node: 137
1553 deg
Eccentricity:
0003781
Arg of perigee: 331
4982 deg
Mean anomaly: 28
5961 deg
Mean motion: 15
50631499 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3888
Checksum: 336
Coasting Arc #12 (Orbit 3903)
---------------------------------------
Vector Time (GMT): 2014/088/22:43:42
195
Vector Time (MET): N/A
Weight (LBS) : 886141
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4028459
21 A = 6788053
07 meter
Y = -1613755
93 meter E =
0002195
Z = 5217789
73 I = 51
89689
XDOT = 4184
371141 Wp = 63
86571
YDOT = -6291
674260 meter/sec RA = 131
29171 deg
ZDOT = 1285
232263 TA = 13
83353
MA = 13
82752
Ha = 226
510 n
mi
Hp = 220
618
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13216729
71 X = -4035460
83
Y = -5294474
84 feet Y = -1658843
10 meter
Z = 17118732
71 Z = 5198203
25
XDOT = 13728
251776 XDOT = 4248
171811
YDOT = -20641
975919 feet/sec YDOT = -6244
525011 meter/sec
ZDOT = 4216
641283 ZDOT = 1305
715309
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11841829
53 X = 3609389
64
Y = 8081200
84 feet Y = 2463150
02 meter
Z = 17036128
78 Z = 5192612
05
XDOT = -17298
383962 XDOT = -5272
547432
YDOT = 16278
290880 feet/sec YDOT = 4961
623060 meter/sec
ZDOT = 4304
132767 ZDOT = 1311
899667
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 14088
99762803
00016717 00000-0 10270-3 0 9114
2 25544 51
6491 132
0420 0003738 335
7492 24
3482 15
50652335 39048
Satellite: ISS
Catalog Number: 25544
Epoch time: 14088
99762803 = yrday
fracday
Element set: 911
Inclination: 51
6491 deg
RA of node: 132
0420 deg
Eccentricity:
0003738
Arg of perigee: 335
7492 deg
Mean anomaly: 24
3482 deg
Mean motion: 15
50652335 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3904
Checksum: 306
Coasting Arc #13 (Orbit 3918)
---------------------------------------
Vector Time (GMT): 2014/089/22:43:42
195
Vector Time (MET): N/A
Weight (LBS) : 886141
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3797034
65 A = 6787479
81 meter
Y = 1871215
23 meter E =
0014036
Z = -5317562
59 I = 51
91452
XDOT = -4094
065346 Wp = 69
62339
YDOT = 6432
242411 meter/sec RA = 126
34597 deg
ZDOT = -656
576914 TA = 194
09916
MA = 194
13839
Ha = 226
398 n
mi
Hp = 220
581
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 12457462
76 X = 3801659
27
Y = 6139157
57 feet Y = 1913701
18 meter
Z = -17446071
47 Z = -5299106
05
XDOT = -13431
972919 XDOT = -4162
498389
YDOT = 21103
157515 feet/sec YDOT = 6386
077217 meter/sec
ZDOT = -2154
123732 ZDOT = -676
632596
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11066815
98 X = -3373165
51
Y = -8550522
91 feet Y = -2606199
38 meter
Z = -17368281
03 Z = -5293852
06
XDOT = 16782
359314 XDOT = 5115
263119
YDOT = -17149
054937 feet/sec YDOT = -5227
031945 meter/sec
ZDOT = -2239
841616 ZDOT = -682
703725
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 14089
96431182
00016717 00000-0 10270-3 0 9126
2 25544 51
6483 127
2478 0003869 338
6769 21
4221 15
50710896 39194
Satellite: ISS
Catalog Number: 25544
Epoch time: 14089
96431182 = yrday
fracday
Element set: 912
Inclination: 51
6483 deg
RA of node: 127
2478 deg
Eccentricity:
0003869
Arg of perigee: 338
6769 deg
Mean anomaly: 21
4221 deg
Mean motion: 15
50710896 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3919
Checksum: 334
Coasting Arc #14 (Orbit 3934)
---------------------------------------
Vector Time (GMT): 2014/090/22:43:42
195
Vector Time (MET): N/A
Weight (LBS) : 886141
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3570909
40 A = 6787237
54 meter
Y = -2181420
68 meter E =
0003806
Z = 5342744
50 I = 51
93158
XDOT = 3992
732432 Wp = 19
45506
YDOT = -6542
243450 meter/sec RA = 121
40117 deg
ZDOT =
929646 TA = 70
55667
MA = 70
51555
Ha = 226
532 n
mi
Hp = 220
325
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -11715582
02 X = -3572204
45
Y = -7156892
01 feet Y = -2221359
41 meter
Z = 17528689
31 Z = 5325394
51
XDOT = 13099
515854 XDOT = 4065
588008
YDOT = -21464
053313 feet/sec YDOT = -6497
186794 meter/sec
ZDOT = 3
050020 ZDOT = 20
503803
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10295250
36 X = 3137992
31
Y = 9221711
94 feet Y = 2810777
80 meter
Z = 17455622
68 Z = 5320473
79
XDOT = -16175
370720 XDOT = -4930
252996
YDOT = 17915
968267 feet/sec YDOT = 5460
787128 meter/sec
ZDOT = 86
763733 ZDOT = 26
445586
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 14090
99541541
00016717 00000-0 10270-3 0 9133
2 25544 51
6482 122
1341 0003824 342
5804 17
5215 15
50736916 39359
Satellite: ISS
Catalog Number: 25544
Epoch time: 14090
99541541 = yrday
fracday
Element set: 913
Inclination: 51
6482 deg
RA of node: 122
1341 deg
Eccentricity:
0003824
Arg of perigee: 342
5804 deg
Mean anomaly: 17
5215 deg
Mean motion: 15
50736916 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3935
Checksum: 296
Coasting Arc #15 (Orbit 3949)
---------------------------------------
Vector Time (GMT): 2014/091/22:43:42
195
Vector Time (MET): N/A
Weight (LBS) : 886141
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3396908
61 A = 6787236
30 meter
Y = 2520481
40 meter E =
0013848
Z = -5319503
87 I = 51
94638
XDOT = -3852
509844 Wp = 79
71671
YDOT = 6579
747412 meter/sec RA = 116
45611 deg
ZDOT = 661
352083 TA = 196
56108
MA = 196
60635
Ha = 226
457 n
mi
Hp = 220
272
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 11144713
29 X = 3394312
28
Y = 8269295
92 feet Y = 2558452
67 meter
Z = -17452440
51 Z = -5303008
58
XDOT = -12639
467993 XDOT = -3929
012407
YDOT = 21587
097809 feet/sec YDOT = 6536
238502 meter/sec
ZDOT = 2169
790297 ZDOT = 642
450341
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9701980
68 X = -2957163
71
Y = -10043660
27 feet Y = -3061307
65 meter
Z = -17383038
52 Z = -5298350
14
XDOT = 15372
506304 XDOT = 4685
539922
YDOT = -18442
862171 feet/sec YDOT = -5621
384390 meter/sec
ZDOT = 2088
896369 ZDOT = 636
695613
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 14091
96204970
00016717 00000-0 10270-3 0 9144
2 25544 51
6472 117
3389 0003900 345
6213 14
4826 15
50786461 39500
Satellite: ISS
Catalog Number: 25544
Epoch time: 14091
96204970 = yrday
fracday
Element set: 914
Inclination: 51
6472 deg
RA of node: 117
3389 deg
Eccentricity:
0003900
Arg of perigee: 345
6213 deg
Mean anomaly: 14
4826 deg
Mean motion: 15
50786461 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3950
Checksum: 308
Coasting Arc #16 (Orbit 3965)
---------------------------------------
Vector Time (GMT): 2014/092/22:43:42
195
Vector Time (MET): N/A
Weight (LBS) : 886141
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3237049
73 A = 6787569
23 meter
Y = -2903922
41 meter E =
0006826
Z = 5210325
46 I = 51
96118
XDOT = 3717
760335 Wp = 24
17968
YDOT = -6566
200723 meter/sec RA = 111
51291 deg
ZDOT = -1343
169024 TA = 78
71544
MA = 78
63874
Ha = 226
532 n
mi
Hp = 220
036
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -10620241
90 X = -3229647
19
Y = -9527304
51 feet Y = -2940079
29 meter
Z = 17094243
64 Z = 5194618
42
XDOT = 12197
376428 XDOT = 3797
433513
YDOT = -21542
653292 feet/sec YDOT = -6524
180993 meter/sec
ZDOT = -4406
722521 ZDOT = -1324
914321
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9162344
12 X = 2792682
49
Y = 11039155
57 feet Y = 3364734
62 meter
Z = 17028233
31 Z = 5190205
51
XDOT = -14538
265794 XDOT = -4431
263414
YDOT = 18777
419540 feet/sec YDOT = 5723
357476 meter/sec
ZDOT = -4328
547707 ZDOT = -1319
341341
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 14092
99309956
00016717 00000-0 10270-3 0 9159
2 25544 51
6475 112
2250 0003870 348
9183 11
1882 15
50822140 39660
Satellite: ISS
Catalog Number: 25544
Epoch time: 14092
99309956 = yrday
fracday
Element set: 915
Inclination: 51
6475 deg
RA of node: 112
2250 deg
Eccentricity:
0003870
Arg of perigee: 348
9183 deg
Mean anomaly: 11
1882 deg
Mean motion: 15
50822140 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 3966
Checksum: 313
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