[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 28th 2014
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 22604 21 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 133 2 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 252 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 116)
---------------------------------------
Vector Time (GMT): 2014/360/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5570696
70 A = 6787762
32 meter
Y = -1470705
89 meter E =
0009533
Z = -3600727
17 I = 51
38708
XDOT = -1218
840146 Wp = 144
65090
YDOT = -6148
796981 meter/sec RA = 224
73134 deg
ZDOT = 4395
363421 TA = 172
64190
MA = 172
62790
Ha = 224
523 n
mi
Hp = 216
192
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18276563
98 X = -5536345
96
Y = -4825150
56 feet Y = -1532808
81 meter
Z = -11813409
35 Z = -3627705
09
XDOT = -3998
819377 XDOT = -1171
343245
YDOT = -20173
218441 feet/sec YDOT = -6162
161468 meter/sec
ZDOT = 14420
483665 ZDOT = 4389
557639
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 3520294
44 X = 1072985
75
Y = -18498516
97 feet Y = -5638347
97 meter
Z = -11928281
77 Z = -3635740
28
XDOT = 18481
233707 XDOT = 5633
080034
YDOT = -5770
069971 feet/sec YDOT = -1758
717327 meter/sec
ZDOT = 14396
767858 ZDOT = 4388
134843
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 14360
50771236
00016717 00000-0 10270-3 0 9002
2 25544 51
6449 225
7521 0006927 178
6316 181
4856 15
52747391 1177
Satellite: ISS
Catalog Number: 25544
Epoch time: 14360
50771236 = yrday
fracday
Element set: 900
Inclination: 51
6449 deg
RA of node: 225
7521 deg
Eccentricity:
0006927
Arg of perigee: 178
6316 deg
Mean anomaly: 181
4856 deg
Mean motion: 15
52747391 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 117
Checksum: 313
Coasting Arc #2 (Orbit 132)
---------------------------------------
Vector Time (GMT): 2014/361/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5870364
70 A = 6790326
44 meter
Y = 2217868
23 meter E =
0016381
Z = 2567077
17 I = 51
41932
XDOT = 185
325410 Wp = 127
59222
YDOT = 5596
717416 meter/sec RA = 219
74327 deg
ZDOT = -5245
990412 TA = 23
43897
MA = 23
36439
Ha = 224
225 n
mi
Hp = 216
358
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19259726
71 X = 5832657
79
Y = 7276470
57 feet Y = 2283303
54 meter
Z = 8422169
19 Z = 2595502
74
XDOT = 608
023000 XDOT = 148
210882
YDOT = 18361
933780 feet/sec YDOT = 5598
582499 meter/sec
ZDOT = -17211
254634 ZDOT = -5245
180101
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -5554393
99 X = -1692979
29
Y = 19773242
04 feet Y = 6026884
17 meter
Z = 8543104
69 Z = 2603938
31
XDOT = -16783
625369 XDOT = -5115
649013
YDOT = 2738
935573 feet/sec YDOT = 834
827563 meter/sec
ZDOT = -17208
752595 ZDOT = -5245
227791
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 14361
53745021
00016717 00000-0 10270-3 0 9010
2 25544 51
6451 220
6294 0006837 181
8780 178
2347 15
52798891 1330
Satellite: ISS
Catalog Number: 25544
Epoch time: 14361
53745021 = yrday
fracday
Element set: 901
Inclination: 51
6451 deg
RA of node: 220
6294 deg
Eccentricity:
0006837
Arg of perigee: 181
8780 deg
Mean anomaly: 178
2347 deg
Mean motion: 15
52798891 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 133
Checksum: 314
Coasting Arc #3 (Orbit 147)
---------------------------------------
Vector Time (GMT): 2014/362/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6019709
45 A = 6792286
71 meter
Y = -2819409
01 meter E =
0004364
Z = -1400272
06 I = 51
44977
XDOT = 969
581256 Wp = 91
44094
YDOT = -4932
664334 meter/sec RA = 214
76029 deg
ZDOT = 5779
128385 TA = 253
27689
MA = 253
32479
Ha = 224
167 n
mi
Hp = 216
542
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19749702
92 X = -5980932
74
Y = -9250029
57 feet Y = -2886508
46 meter
Z = -4594068
42 Z = -1429420
62
XDOT = 3181
040867 XDOT = 996
594481
YDOT = -16183
281936 feet/sec YDOT = -4921
670984 meter/sec
ZDOT = 18960
394963 ZDOT = 5783
903898
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7121507
29 X = 2170635
42
Y = -20585040
19 feet Y = -6274320
25 meter
Z = -4718000
80 Z = -1438046
64
XDOT = 14912
890293 XDOT = 4545
448961
YDOT = 820
066886 feet/sec YDOT = 249
956387 meter/sec
ZDOT = 18981
614959 ZDOT = 5785
596240
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 14362
50280745
00016717 00000-0 10270-3 0 9026
2 25544 51
6442 215
8256 0006837 186
8173 173
2888 15
52808510 1486
Satellite: ISS
Catalog Number: 25544
Epoch time: 14362
50280745 = yrday
fracday
Element set: 902
Inclination: 51
6442 deg
RA of node: 215
8256 deg
Eccentricity:
0006837
Arg of perigee: 186
8173 deg
Mean anomaly: 173
2888 deg
Mean motion: 15
52808510 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 148
Checksum: 316
Coasting Arc #4 (Orbit 163)
---------------------------------------
Vector Time (GMT): 2014/363/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5929895
09 A = 6793092
20 meter
Y = 3290441
77 meter E =
0017151
Z = 112706
36 I = 51
47890
XDOT = -2226
498102 Wp = 153
22328
YDOT = 4229
732940 meter/sec RA = 209
78350 deg
ZDOT = -6000
944368 TA = 25
55971
MA = 25
47502
Ha = 224
036 n
mi
Hp = 216
655
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19455036
37 X = 5892112
38
Y = 10795412
63 feet Y = 3356542
45 meter
Z = 369771
51 Z = 141421
15
XDOT = -7304
783799 XDOT = -2244
479983
YDOT = 13877
076574 feet/sec YDOT = 4204
734474 meter/sec
ZDOT = -19688
137691 ZDOT = -6011
803844
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8332541
69 X = -2539758
71
Y = 20627724
07 feet Y = 6287330
30 meter
Z = 491786
34 Z = 149896
48
XDOT = -13145
791555 XDOT = -4006
837266
YDOT = -4819
655793 feet/sec YDOT = -1469
031086 meter/sec
ZDOT = -19735
207209 ZDOT = -6015
291157
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 14363
53249952
00016717 00000-0 10270-3 0 9036
2 25544 51
6441 210
7027 0006915 190
2318 169
8695 15
52833611 1647
Satellite: ISS
Catalog Number: 25544
Epoch time: 14363
53249952 = yrday
fracday
Element set: 903
Inclination: 51
6441 deg
RA of node: 210
7027 deg
Eccentricity:
0006915
Arg of perigee: 190
2318 deg
Mean anomaly: 169
8695 deg
Mean motion: 15
52833611 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 164
Checksum: 307
Coasting Arc #5 (Orbit 179)
---------------------------------------
Vector Time (GMT): 2014/364/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5625949
32 A = 6792360
47 meter
Y = -3620091
11 meter E =
0009765
Z = 1163815
84 I = 51
50366
XDOT = 3481
739021 Wp = 86
37458
YDOT = -3516
652539 meter/sec RA = 204
80693 deg
ZDOT = 5850
345973 TA = 286
27490
MA = 286
38229
Ha = 223
809 n
mi
Hp = 216
804
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -18457838
98 X = -5590703
90
Y = -11876939
33 feet Y = -3682807
12 meter
Z = 3818293
43 Z = 1136571
29
XDOT = 11423
028285 XDOT = 3492
385288
YDOT = -11537
573948 feet/sec YDOT = -3477
658241 meter/sec
ZDOT = 19194
048468 ZDOT = 5867
285391
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9182459
05 X = 2798813
52
Y = -19957607
48 feet Y = -6083078
76 meter
Z = 3702596
61 Z = 1128551
45
XDOT = 11544
139614 XDOT = 3518
653754
YDOT = 8912
200488 feet/sec YDOT = 2716
438709 meter/sec
ZDOT = 19266
956567 ZDOT = 5872
568362
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 14364
56216564
00016717 00000-0 10270-3 0 9044
2 25544 51
6430 205
5781 0006908 194
8969 165
1981 15
52900769 1802
Satellite: ISS
Catalog Number: 25544
Epoch time: 14364
56216564 = yrday
fracday
Element set: 904
Inclination: 51
6430 deg
RA of node: 205
5781 deg
Eccentricity:
0006908
Arg of perigee: 194
8969 deg
Mean anomaly: 165
1981 deg
Mean motion: 15
52900769 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 180
Checksum: 330
Coasting Arc #6 (Orbit 194)
---------------------------------------
Vector Time (GMT): 2014/365/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 929709
2
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5035937
23 A = 6790457
19 meter
Y = 3854000
57 meter E =
0010519
Z = -2412217
83 I = 51
52550
XDOT = -4714
180457 Wp = 170
05813
YDOT = 2819
774784 meter/sec RA = 199
83109 deg
ZDOT = -5350
169527 TA = 36
95115
MA = 36
87874
Ha = 223
679 n
mi
Hp = 216
956
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 16522103
77 X = 5004184
34
Y = 12644358
83 feet Y = 3910138
31 meter
Z = -7914100
50 Z = -2387830
92
XDOT = -15466
471315 XDOT = -4719
372167
YDOT = 9251
229607 feet/sec YDOT = 2767
029080 meter/sec
ZDOT = -17553
049628 ZDOT = -5373
082690
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9894281
91 X = -3015777
13
Y = 18346388
29 feet Y = 5591979
15 meter
Z = -7810629
44 Z = -2380679
85
XDOT = -10200
926673 XDOT = -3109
242450
YDOT = -12996
847215 feet/sec YDOT = -3961
439031 meter/sec
ZDOT = -17651
353706 ZDOT = -5380
132610
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 14365
52745761
00016717 00000-0 10270-3 0 9058
2 25544 51
6421 200
7750 0006816 198
6864 161
4039 15
52914682 1957
Satellite: ISS
Catalog Number: 25544
Epoch time: 14365
52745761 = yrday
fracday
Element set: 905
Inclination: 51
6421 deg
RA of node: 200
7750 deg
Eccentricity:
0006816
Arg of perigee: 198
6864 deg
Mean anomaly: 161
4039 deg
Mean motion: 15
52914682 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 195
Checksum: 319
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