[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 26th 2013
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 29600 75 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 2406)
---------------------------------------
Vector Time (GMT): 2013/357/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4483681
45 A = 6795479
21 meter
Y = -3526777
98 meter E =
0002180
Z = -3692462
84 I = 51
31452
XDOT = 1343
013768 Wp = 38
20670
YDOT = -6198
912936 meter/sec RA = 249
40657 deg
ZDOT = 4293
011940 TA = 277
67647
MA = 277
70123
Ha = 226
446 n
mi
Hp = 222
633
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14710240
99 X = -4425974
15
Y = -11570793
90 feet Y = -3576594
54 meter
Z = -12114379
38 Z = -3714103
99
XDOT = 4406
213148 XDOT = 1391
377434
YDOT = -20337
640866 feet/sec YDOT = -6183
624273 meter/sec
ZDOT = 14084
684842 ZDOT = 4299
653332
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11218453
67 X = 3419384
68
Y = -14907037
63 feet Y = -4543665
07 meter
Z = -12204883
27 Z = -3720048
42
XDOT = 19346
891614 XDOT = 5896
932564
YDOT = 3012
570105 feet/sec YDOT = 918
231368 meter/sec
ZDOT = 14113
591217 ZDOT = 4301
822603
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 13357
50793206
00016717 00000-0 10270-3 0 9008
2 25544 51
6503 250
3085 0005137 303
5348 56
5311 15
50013412 24073
Satellite: ISS
Catalog Number: 25544
Epoch time: 13357
50793206 = yrday
fracday
Element set: 900
Inclination: 51
6503 deg
RA of node: 250
3085 deg
Eccentricity:
0005137
Arg of perigee: 303
5348 deg
Mean anomaly: 56
5311 deg
Mean motion: 15
50013412 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2407
Checksum: 265
Coasting Arc #2 (Orbit 2422)
---------------------------------------
Vector Time (GMT): 2013/358/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4711382
12 A = 6796215
57 meter
Y = 3499864
32 meter E =
0008889
Z = 3422818
01 I = 51
32863
XDOT = -1160
809408 Wp = 68
73871
YDOT = 6040
590878 meter/sec RA = 244
43037 deg
ZDOT = -4565
968980 TA = 71
07617
MA = 70
97984
Ha = 226
617 n
mi
Hp = 222
538
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 15457290
41 X = 4655268
66
Y = 11482494
50 feet Y = 3552236
13 meter
Z = 11229717
89 Z = 3445569
20
XDOT = -3808
429817 XDOT = -1206
090234
YDOT = 19818
211543 feet/sec YDOT = 6027
356954 meter/sec
ZDOT = -14980
213189 ZDOT = -4571
717824
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -10841134
47 X = -3304377
79
Y = 15846083
08 feet Y = 4829886
12 meter
Z = 11324907
29 Z = 3451831
74
XDOT = -18797
413851 XDOT = -5729
451742
YDOT = -2106
537742 feet/sec YDOT = -642
072704 meter/sec
ZDOT = -15005
331486 ZDOT = -4573
625037
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 13358
53949254
00016717 00000-0 10270-3 0 9019
2 25544 51
6499 245
1983 0005108 307
7762 52
2925 15
50040163 24235
Satellite: ISS
Catalog Number: 25544
Epoch time: 13358
53949254 = yrday
fracday
Element set: 901
Inclination: 51
6499 deg
RA of node: 245
1983 deg
Eccentricity:
0005108
Arg of perigee: 307
7762 deg
Mean anomaly: 52
2925 deg
Mean motion: 15
50040163 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2423
Checksum: 308
Coasting Arc #3 (Orbit 2437)
---------------------------------------
Vector Time (GMT): 2013/359/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4948365
63 A = 6796885
71 meter
Y = -3430776
99 meter E =
0004383
Z = -3148197
46 I = 51
34568
XDOT = 1008
949138 Wp = 5
91617
YDOT = -5870
674230 meter/sec RA = 239
45451 deg
ZDOT = 4816
622189 TA = 317
69160
MA = 317
72540
Ha = 226
621 n
mi
Hp = 222
417
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16234795
38 X = -4894341
09
Y = -11255830
01 feet Y = -3485810
59 meter
Z = -10328731
84 Z = -3172105
02
XDOT = 3310
200583 XDOT = 1051
123543
YDOT = -19260
742224 feet/sec YDOT = -5859
155872 meter/sec
ZDOT = 15802
566237 ZDOT = 4821
625799
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10294952
77 X = 3137901
61
Y = -16798776
85 feet Y = -5120267
19 meter
Z = -10428807
95 Z = -3178700
66
XDOT = 18188
891567 XDOT = 5543
974150
YDOT = 1332
727730 feet/sec YDOT = 406
215412 meter/sec
ZDOT = 15824
516324 ZDOT = 4823
312575
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 13359
50656034
00016717 00000-0 10270-3 0 9029
2 25544 51
6503 240
4067 0005297 310
6590 49
4099 15
50070424 24382
Satellite: ISS
Catalog Number: 25544
Epoch time: 13359
50656034 = yrday
fracday
Element set: 902
Inclination: 51
6503 deg
RA of node: 240
4067 deg
Eccentricity:
0005297
Arg of perigee: 310
6590 deg
Mean anomaly: 49
4099 deg
Mean motion: 15
50070424 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2438
Checksum: 295
Coasting Arc #4 (Orbit 2453)
---------------------------------------
Vector Time (GMT): 2013/360/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5181094
81 A = 6797603
10 meter
Y = 3363759
51 meter E =
0009565
Z = 2830927
06 I = 51
36479
XDOT = -914
177304 Wp = 80
79356
YDOT = 5679
262031 meter/sec RA = 234
48090 deg
ZDOT = -5058
918348 TA = 66
97467
MA = 66
87383
Ha = 226
801 n
mi
Hp = 222
249
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16998342
54 X = 5129343
55
Y = 11035956
39 feet Y = 3421408
34 meter
Z = 9287818
43 Z = 2855970
78
XDOT = -2999
269370 XDOT = -953
041271
YDOT = 18632
749446 feet/sec YDOT = 5668
822016 meter/sec
ZDOT = -16597
501142 ZDOT = -5063
453515
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9727032
04 X = -2964799
37
Y = 17724606
06 feet Y = 5402459
93 meter
Z = 9392696
19 Z = 2862893
80
XDOT = -17504
238777 XDOT = -5335
291979
YDOT = -772
295848 feet/sec YDOT = -235
395774 meter/sec
ZDOT = -16617
446510 ZDOT = -5064
997696
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 13360
53808077
00016717 00000-0 10270-3 0 9031
2 25544 51
6502 235
2964 0005232 315
1004 44
9723 15
50102214 24543
Satellite: ISS
Catalog Number: 25544
Epoch time: 13360
53808077 = yrday
fracday
Element set: 903
Inclination: 51
6502 deg
RA of node: 235
2964 deg
Eccentricity:
0005232
Arg of perigee: 315
1004 deg
Mean anomaly: 44
9723 deg
Mean motion: 15
50102214 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2454
Checksum: 268
Coasting Arc #5 (Orbit 2468)
---------------------------------------
Vector Time (GMT): 2013/361/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5412256
26 A = 6798256
83 meter
Y = -3249021
45 meter E =
0007339
Z = -2511907
37 I = 51
38564
XDOT = 851
708281 Wp = 3
05778
YDOT = -5491
132638 meter/sec RA = 229
50784 deg
ZDOT = 5275
265542 TA = 328
70140
MA = 328
74506
Ha = 226
808 n
mi
Hp = 222
168
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17756746
26 X = -5363320
54
Y = -10659519
19 feet Y = -3309271
00 meter
Z = -8241165
93 Z = -2538080
99
XDOT = 2794
318508 XDOT = 887
422186
YDOT = -18015
527029 feet/sec YDOT = -5481
408880 meter/sec
ZDOT = 17307
301648 ZDOT = 5279
489534
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 8974970
64 X = 2735571
05
Y = -18616062
77 feet Y = -5674175
93 meter
Z = -8350827
03 Z = -2545332
08
XDOT = 16827
916930 XDOT = 5129
149080
YDOT = 352
271265 feet/sec YDOT = 107
372282 meter/sec
ZDOT = 17325
906644 ZDOT = 5280
936345
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 13361
50511138
00016717 00000-0 10270-3 0 9049
2 25544 51
6500 230
5045 0005456 317
6013 42
4715 15
50124423 24690
Satellite: ISS
Catalog Number: 25544
Epoch time: 13361
50511138 = yrday
fracday
Element set: 904
Inclination: 51
6500 deg
RA of node: 230
5045 deg
Eccentricity:
0005456
Arg of perigee: 317
6013 deg
Mean anomaly: 42
4715 deg
Mean motion: 15
50124423 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2469
Checksum: 263
Coasting Arc #6 (Orbit 2484)
---------------------------------------
Vector Time (GMT): 2013/362/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5632755
64 A = 6798871
46 meter
Y = 3136873
61 meter E =
0009774
Z = 2148702
04 I = 51
40867
XDOT = -850
579972 Wp = 92
24411
YDOT = 5291
120102 meter/sec RA = 224
53761 deg
ZDOT = -5473
442282 TA = 63
89520
MA = 63
79467
Ha = 226
976 n
mi
Hp = 221
944
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18480169
43 X = 5586821
95
Y = 10291580
10 feet Y = 3199605
70 meter
Z = 7049547
39 Z = 2175954
18
XDOT = -2790
616705 XDOT = -883
094678
YDOT = 17359
317921 feet/sec YDOT = 5281
426965 meter/sec
ZDOT = -17957
487801 ZDOT = -5477
652932
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8207424
08 X = -2501622
86
Y = 19453737
11 feet Y = 5929499
07 meter
Z = 7163777
22 Z = 2183519
30
XDOT = -16128
302265 XDOT = -4915
906530
YDOT = -159
565001 feet/sec YDOT = -48
635412 meter/sec
ZDOT = -17976
005780 ZDOT = -5479
086562
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 13362
53659247
00016717 00000-0 10270-3 0 9058
2 25544 51
6499 225
3941 0005377 322
0489 38
0282 15
50162823 24857
Satellite: ISS
Catalog Number: 25544
Epoch time: 13362
53659247 = yrday
fracday
Element set: 905
Inclination: 51
6499 deg
RA of node: 225
3941 deg
Eccentricity:
0005377
Arg of perigee: 322
0489 deg
Mean anomaly: 38
0282 deg
Mean motion: 15
50162823 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2485
Checksum: 319
Coasting Arc #7 (Orbit 2499)
---------------------------------------
Vector Time (GMT): 2013/363/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5839219
70 A = 6799430
57 meter
Y = -2975616
40 meter E =
0010289
Z = -1788012
75 I = 51
43223
XDOT = 880
157004 Wp = 7
67677
YDOT = -5109
815644 meter/sec RA = 219
56774 deg
ZDOT = 5643
140481 TA = 332
65120
MA = 332
70533
Ha = 226
990 n
mi
Hp = 221
881
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19157544
95 X = -5796826
03
Y = -9762521
01 feet Y = -3040677
08 meter
Z = -5866183
55 Z = -1816276
47
XDOT = 2887
654211 XDOT = 909
817822
YDOT = -16764
487020 feet/sec YDOT = -5099
807849 meter/sec
ZDOT = 18514
240424 ZDOT = 5647
487777
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7259872
58 X = 2212809
16
Y = -20204156
56 feet Y = -6158226
92 meter
Z = -5984710
73 Z = -1824139
83
XDOT = 15505
806444 XDOT = 4726
169804
YDOT = 94
947844 feet/sec YDOT = 28
940103 meter/sec
ZDOT = 18533
306635 ZDOT = 5648
951862
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 13363
50358661
00016717 00000-0 10270-3 0 9063
2 25544 51
6488 220
6018 0005572 324
4063 35
6716 15
50178145 25006
Satellite: ISS
Catalog Number: 25544
Epoch time: 13363
50358661 = yrday
fracday
Element set: 906
Inclination: 51
6488 deg
RA of node: 220
6018 deg
Eccentricity:
0005572
Arg of perigee: 324
4063 deg
Mean anomaly: 35
6716 deg
Mean motion: 15
50178145 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2500
Checksum: 293
Coasting Arc #8 (Orbit 2515)
---------------------------------------
Vector Time (GMT): 2013/364/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 901192
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6027668
24 A = 6799848
95 meter
Y = 2819887
09 meter E =
0009402
Z = 1383007
12 I = 51
45808
XDOT = -971
012781 Wp = 102
78317
YDOT = 4927
416823 meter/sec RA = 214
60109 deg
ZDOT = -5783
455694 TA = 62
13783
MA = 62
04261
Ha = 227
137 n
mi
Hp = 221
627
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19775814
44 X = 5988969
40
Y = 9251598
07 feet Y = 2887075
79 meter
Z = 4537424
94 Z = 1412195
21
XDOT = -3185
737471 XDOT = -997
945722
YDOT = 16166
065693 feet/sec YDOT = 4916
408389 meter/sec
ZDOT = -18974
592171 ZDOT = -5788
237643
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -6315419
94 X = -1924940
00
Y = 20872567
43 feet Y = 6361958
55 meter
Z = 4659885
03 Z = 1420332
96
XDOT = -14915
512963 XDOT = -4546
248351
YDOT = -249
871536 feet/sec YDOT = -76
160844 meter/sec
ZDOT = -18995
461399 ZDOT = -5789
816635
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 13364
53502851
00016717 00000-0 10270-3 0 9070
2 25544 51
6484 215
4910 0005524 328
7414 31
3407 15
50224804 25160
Satellite: ISS
Catalog Number: 25544
Epoch time: 13364
53502851 = yrday
fracday
Element set: 907
Inclination: 51
6484 deg
RA of node: 215
4910 deg
Eccentricity:
0005524
Arg of perigee: 328
7414 deg
Mean anomaly: 31
3407 deg
Mean motion: 15
50224804 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 2516
Checksum: 284
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