[list_settings.list_name] Current ISS TLEs @ 18:30 UTC
Date:
December 15th 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 15607 67 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 110 8 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 964 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 1609)
---------------------------------------
Vector Time (GMT): 2015/348/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905771
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4274531
64 A = 6775572
28 meter
Y = 241096
93 meter E =
0006018
Z = 5256493
14 I = 51
25791
XDOT = 368
870032 Wp = 295
75456
YDOT = 7629
320960 meter/sec RA = 263
32946 deg
ZDOT = -647
902625 TA = 160
47794
MA = 160
45488
Ha = 218
235 n
mi
Hp = 217
214
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 14024053
95 X = 4245983
96
Y = 791000
44 feet Y = 288737
49 meter
Z = 17245712
39 Z = 5277188
60
XDOT = 1210
203516 XDOT = 286
676937
YDOT = 25030
580578 feet/sec YDOT = 7632
986396 meter/sec
ZDOT = -2125
664781 ZDOT = -646
309705
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2721985
41 X = -829661
15
Y = 13667467
80 feet Y = 4165844
19 meter
Z = 17335094
06 Z = 5283736
67
XDOT = -23960
341746 XDOT = -7303
112164
YDOT = -2074
445377 feet/sec YDOT = -632
290951 meter/sec
ZDOT = -2120
249761 ZDOT = -646
252127
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 15348
54710915
00016717 00000-0 10270-3 0 9000
2 25544 51
6427 263
9744 0008211 279
5037 80
5188 15
54787245 16103
Satellite: ISS
Catalog Number: 25544
Epoch time: 15348
54710915 = yrday
fracday
Element set: 900
Inclination: 51
6427 deg
RA of node: 263
9744 deg
Eccentricity:
0008211
Arg of perigee: 279
5037 deg
Mean anomaly: 80
5188 deg
Mean motion: 15
54787245 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1610
Checksum: 317
Coasting Arc #2 (Orbit 1624)
---------------------------------------
Vector Time (GMT): 2015/349/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905771
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4323623
86 A = 6777905
46 meter
Y = -2262669
85 meter E =
0003039
Z = -4706836
26 I = 51
27057
XDOT = 758
443437 Wp = 124
40236
YDOT = -7124
435182 meter/sec RA = 258
29830 deg
ZDOT = 2727
739332 TA = 172
73538
MA = 172
73097
Ha = 218
290 n
mi
Hp = 216
838
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14185117
66 X = -4275136
88
Y = -7423457
51 feet Y = -2310748
01 meter
Z = -15442376
19 Z = -4727721
87
XDOT = 2488
331485 XDOT = 824
803988
YDOT = -23374
131173 feet/sec YDOT = -7115
582922 meter/sec
ZDOT = 8949
276022 ZDOT = 2731
584342
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9090174
34 X = 2770685
14
Y = -13073319
71 feet Y = -3984747
85 meter
Z = -15532202
33 Z = -4734215
27
XDOT = 21947
889395 XDOT = 6689
716688
YDOT = 4605
374793 feet/sec YDOT = 1403
718237 meter/sec
ZDOT = 8967
247095 ZDOT = 2733
216914
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 15349
51124126
00016717 00000-0 10270-3 0 9012
2 25544 51
6429 259
1628 0008119 283
3180 76
7068 15
54786953 16257
Satellite: ISS
Catalog Number: 25544
Epoch time: 15349
51124126 = yrday
fracday
Element set: 901
Inclination: 51
6429 deg
RA of node: 259
1628 deg
Eccentricity:
0008119
Arg of perigee: 283
3180 deg
Mean anomaly: 76
7068 deg
Mean motion: 15
54786953 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1625
Checksum: 323
Coasting Arc #3 (Orbit 1640)
---------------------------------------
Vector Time (GMT): 2015/350/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905771
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4161176
43 A = 6782026
46 meter
Y = 4029938
64 meter E =
0005226
Z = 3526021
03 I = 51
29130
XDOT = -1951
793603 Wp = 56
87837
YDOT = 5923
583483 meter/sec RA = 253
27882 deg
ZDOT = -4459
151443 TA = 81
33849
MA = 81
27930
Ha = 218
632 n
mi
Hp = 216
728
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13652153
63 X = 4098675
42
Y = 13221583
47 feet Y = 4076122
00 meter
Z = 11568310
46 Z = 3546083
51
XDOT = -6403
522320 XDOT = -1996
226756
YDOT = 19434
329013 feet/sec YDOT = 5901
509051 meter/sec
ZDOT = -14629
761951 ZDOT = -4468
740404
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14576215
56 X = -4442830
50
Y = 12113198
24 feet Y = 3692102
82 meter
Z = 11654258
59 Z = 3552218
02
XDOT = -17779
037800 XDOT = -5419
050721
YDOT = -7253
824531 feet/sec YDOT = -2210
965717 meter/sec
ZDOT = -14672
316309 ZDOT = -4472
122011
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 15350
53963140
00016717 00000-0 10270-3 0 9024
2 25544 51
6423 254
0311 0008074 286
9249 73
1018 15
54799706 16413
Satellite: ISS
Catalog Number: 25544
Epoch time: 15350
53963140 = yrday
fracday
Element set: 902
Inclination: 51
6423 deg
RA of node: 254
0311 deg
Eccentricity:
0008074
Arg of perigee: 286
9249 deg
Mean anomaly: 73
1018 deg
Mean motion: 15
54799706 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1641
Checksum: 301
Coasting Arc #4 (Orbit 1655)
---------------------------------------
Vector Time (GMT): 2015/351/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905771
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -3739973
42 A = 6785720
16 meter
Y = -5335964
25 meter E =
0008934
Z = -1871855
79 I = 51
31471
XDOT = 3161
694130 Wp = 339
18415
YDOT = -4180
848134 meter/sec RA = 248
27176 deg
ZDOT = 5600
923836 TA =
10175
MA =
10157
Ha = 218
688 n
mi
Hp = 216
542
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -12270254
01 X = -3670934
67
Y = -17506444
38 feet Y = -5377401
00 meter
Z = -6141259
15 Z = -1889856
30
XDOT = 10373
012236 XDOT = 3181
003366
YDOT = -13716
693354 feet/sec YDOT = -4145
384251 meter/sec
ZDOT = 18375
734369 ZDOT = 5616
329380
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18514948
57 X = 5643356
33
Y = -10643407
13 feet Y = -3244110
49 meter
Z = -6218066
94 Z = -1895266
80
XDOT = 11983
659936 XDOT = 3652
619549
YDOT = 10071
545968 feet/sec YDOT = 3069
807211 meter/sec
ZDOT = 18443
094460 ZDOT = 5621
455192
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 15351
50373028
00016717 00000-0 10270-3 0 9033
2 25544 51
6429 249
2190 0008176 290
5202 69
5073 15
54845506 16569
Satellite: ISS
Catalog Number: 25544
Epoch time: 15351
50373028 = yrday
fracday
Element set: 903
Inclination: 51
6429 deg
RA of node: 249
2190 deg
Eccentricity:
0008176
Arg of perigee: 290
5202 deg
Mean anomaly: 69
5073 deg
Mean motion: 15
54845506 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1656
Checksum: 306
Coasting Arc #5 (Orbit 1671)
---------------------------------------
Vector Time (GMT): 2015/352/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905771
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3016082
17 A = 6787282
53 meter
Y = 6076182
20 meter E =
0005343
Z = -48248
45 I = 51
33255
XDOT = -4309
687409 Wp = 168
49037
YDOT = 2092
651076 meter/sec RA = 243
27511 deg
ZDOT = -5986
350426 TA = 12
03156
MA = 12
01880
Ha = 218
945 n
mi
Hp = 216
379
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9895282
72 X = 2948147
02
Y = 19934980
96 feet Y = 6109530
17 meter
Z = -158295
44 Z = -33761
75
XDOT = -14139
394387 XDOT = -4303
688265
YDOT = 6865
653135 feet/sec YDOT = 2044
491042 meter/sec
ZDOT = -19640
257303 ZDOT = -6007
271361
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20585664
44 X = -6274510
52
Y = 8459680
46 feet Y = 2578510
61 meter
Z = -96796
75 Z = -29503
65
XDOT = -5237
402071 XDOT = -1596
360151
YDOT = -12963
017060 feet/sec YDOT = -3951
127600 meter/sec
ZDOT = -19731
068944 ZDOT = -6014
029814
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 15352
53208739
00016717 00000-0 10270-3 0 9044
2 25544 51
6430 244
0868 0008158 293
5939 66
4357 15
54831905 16723
Satellite: ISS
Catalog Number: 25544
Epoch time: 15352
53208739 = yrday
fracday
Element set: 904
Inclination: 51
6430 deg
RA of node: 244
0868 deg
Eccentricity:
0008158
Arg of perigee: 293
5939 deg
Mean anomaly: 66
4357 deg
Mean motion: 15
54831905 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1672
Checksum: 331
Coasting Arc #6 (Orbit 1687)
---------------------------------------
Vector Time (GMT): 2015/353/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905771
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1971635
01 A = 6785550
35 meter
Y = -6180140
40 meter E =
0010864
Z = 1965620
97 I = 51
34240
XDOT = 5283
805295 Wp = 31
54850
YDOT = 85
080534 meter/sec RA = 238
27840 deg
ZDOT = 5562
612559 TA = 350
25066
MA = 350
27173
Ha = 219
147 n
mi
Hp = 216
081
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -6468618
80 X = -1911928
88
Y = -20276051
18 feet Y = -6201854
76 meter
Z = 6448887
68 Z = 1956187
95
XDOT = 17335
319210 XDOT = 5255
440091
YDOT = 279
135609 feet/sec YDOT = 144
008751 meter/sec
ZDOT = 18250
041203 ZDOT = 5588
211386
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 20595441
84 X = 6277490
67
Y = -5412841
60 feet Y = -1649834
12 meter
Z = 6409239
75 Z = 1953536
28
XDOT = -1598
760159 XDOT = -487
302096
YDOT = 15676
367885 feet/sec YDOT = 4778
156931 meter/sec
ZDOT = 18360
679093 ZDOT = 5596
334988
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 15353
56042707
00016717 00000-0 10270-3 0 9050
2 25544 51
6431 238
9537 0008282 298
9704 61
0618 15
54872285 16880
Satellite: ISS
Catalog Number: 25544
Epoch time: 15353
56042707 = yrday
fracday
Element set: 905
Inclination: 51
6431 deg
RA of node: 238
9537 deg
Eccentricity:
0008282
Arg of perigee: 298
9704 deg
Mean anomaly: 61
0618 deg
Mean motion: 15
54872285 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1688
Checksum: 334
Coasting Arc #7 (Orbit 1702)
---------------------------------------
Vector Time (GMT): 2015/354/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905771
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 636628
18 A = 6781539
60 meter
Y = 5699171
68 meter E =
0005479
Z = -3623070
28 I = 51
34701
XDOT = -5934
433884 Wp = 340
60342
YDOT = -2116
307086 meter/sec RA = 233
27437 deg
ZDOT = -4364
789926 TA = 242
54906
MA = 242
60479
Ha = 219
285 n
mi
Hp = 215
884
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 2088675
13 X = 590450
90
Y = 18698069
81 feet Y = 5706032
84 meter
Z = -11886713
52 Z = -3620089
56
XDOT = -19469
927440 XDOT = -5889
125172
YDOT = -6943
264719 feet/sec YDOT = -2182
416320 meter/sec
ZDOT = -14320
176922 ZDOT = -4393
508395
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -18763435
32 X = -5719095
09
Y = 1481723
14 feet Y = 451629
21 meter
Z = -11874861
18 Z = -3619457
69
XDOT = 7754
497333 XDOT = 2363
570787
YDOT = -17743
495299 feet/sec YDOT = -5408
217367 meter/sec
ZDOT = -14443
941131 ZDOT = -4402
513257
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 15354
52448001
00016717 00000-0 10270-3 0 9065
2 25544 51
6433 234
1425 0008433 301
3629 58
6698 15
54897548 17036
Satellite: ISS
Catalog Number: 25544
Epoch time: 15354
52448001 = yrday
fracday
Element set: 906
Inclination: 51
6433 deg
RA of node: 234
1425 deg
Eccentricity:
0008433
Arg of perigee: 301
3629 deg
Mean anomaly: 58
6698 deg
Mean motion: 15
54897548 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1703
Checksum: 315
Coasting Arc #8 (Orbit 1718)
---------------------------------------
Vector Time (GMT): 2015/355/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905771
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 925084
01 A = 6777278
65 meter
Y = -4709652
08 meter E =
0001348
Z = 4784516
42 I = 51
35289
XDOT = 6144
117600 Wp = 350
15057
YDOT = 3808
339443 meter/sec RA = 228
25717 deg
ZDOT = 2562
199047 TA = 74
53134
MA = 74
51645
Ha = 219
390 n
mi
Hp = 215
593
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 3035052
52 X = 954438
25
Y = -15451614
44 feet Y = -4699143
34 meter
Z = 15697232
35 Z = 4789081
33
XDOT = 20157
866143 XDOT = 6088
628911
YDOT = 12494
551979 feet/sec YDOT = 3876
736613 meter/sec
ZDOT = 8406
164853 ZDOT = 2591
911569
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 15390738
99 X = 4691097
24
Y = 3231468
85 feet Y = 984951
70 meter
Z = 15717817
86 Z = 4790790
88
XDOT = -12644
605768 XDOT = -3854
075838
YDOT = 18736
898316 feet/sec YDOT = 5711
006607 meter/sec
ZDOT = 8533
934574 ZDOT = 2601
143258
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 15355
55278923
00016717 00000-0 10270-3 0 9074
2 25544 51
6433 229
0095 0008330 306
2964 53
7419 15
54920864 17196
Satellite: ISS
Catalog Number: 25544
Epoch time: 15355
55278923 = yrday
fracday
Element set: 907
Inclination: 51
6433 deg
RA of node: 229
0095 deg
Eccentricity:
0008330
Arg of perigee: 306
2964 deg
Mean anomaly: 53
7419 deg
Mean motion: 15
54920864 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1719
Checksum: 324
Coasting Arc #9 (Orbit 1733)
---------------------------------------
Vector Time (GMT): 2015/356/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905771
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2560025
69 A = 6774942
71 meter
Y = 3390575
87 meter E =
0010331
Z = -5284832
54 I = 51
36683
XDOT = -5790
396457 Wp = 52
91713
YDOT = -5004
412246 meter/sec RA = 223
23067 deg
ZDOT = -400
171833 TA = 213
21765
MA = 213
28254
Ha = 219
510 n
mi
Hp = 215
200
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -8399034
42 X = -2572077
85
Y = 11123936
60 feet Y = 3361881
01 meter
Z = -17338689
42 Z = -5297297
69
XDOT = -18997
363703 XDOT = -5732
061643
YDOT = -16418
675347 feet/sec YDOT = -5068
838082 meter/sec
ZDOT = -1312
899716 ZDOT = -428
159267
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11105191
66 X = -3384862
42
Y = -8310676
26 feet Y = -2533094
12 meter
Z = -17393196
19 Z = -5301446
20
XDOT = 15851
858975 XDOT = 4831
646616
YDOT = -18144
905670 feet/sec YDOT = -5530
567248 meter/sec
ZDOT = -1433
012279 ZDOT = -436
782143
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 15356
51681297
00016717 00000-0 10270-3 0 9084
2 25544 51
6425 224
1974 0008493 309
5317 50
5085 15
54978442 17343
Satellite: ISS
Catalog Number: 25544
Epoch time: 15356
51681297 = yrday
fracday
Element set: 908
Inclination: 51
6425 deg
RA of node: 224
1974 deg
Eccentricity:
0008493
Arg of perigee: 309
5317 deg
Mean anomaly: 50
5085 deg
Mean motion: 15
54978442 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1734
Checksum: 331
Coasting Arc #10 (Orbit 1749)
---------------------------------------
Vector Time (GMT): 2015/357/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905771
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4126675
82 A = 6775883
94 meter
Y = -1874193
76 meter E =
0009082
Z = 5040936
82 I = 51
39419
XDOT = 4827
089540 Wp = 348
81258
YDOT = 5665
617720 meter/sec RA = 218
20397 deg
ZDOT = -1836
980547 TA = 119
08875
MA = 118
99777
Ha = 219
602 n
mi
Hp = 215
038
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13538962
68 X = 4122839
82
Y = -6148929
65 feet Y = -1828068
47 meter
Z = 16538506
64 Z = 5060973
93
XDOT = 15836
907939 XDOT = 4772
299820
YDOT = 18587
984645 feet/sec YDOT = 5719
291252 meter/sec
ZDOT = -6026
839066 ZDOT = -1813
664001
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 6350042
42 X = 1935492
93
Y = 13338105
82 feet Y = 4065454
65 meter
Z = 16625490
74 Z = 5067449
58
XDOT = -17372
275105 XDOT = -5295
069452
YDOT = 15691
775021 feet/sec YDOT = 4782
853026 meter/sec
ZDOT = -5927
024684 ZDOT = -1806
557124
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 15357
54509029
00016717 00000-0 10270-3 0 9091
2 25544 51
6424 219
0648 0008569 312
8609 47
1824 15
55006037 17502
Satellite: ISS
Catalog Number: 25544
Epoch time: 15357
54509029 = yrday
fracday
Element set: 909
Inclination: 51
6424 deg
RA of node: 219
0648 deg
Eccentricity:
0008569
Arg of perigee: 312
8609 deg
Mean anomaly: 47
1824 deg
Mean motion: 15
55006037 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1750
Checksum: 317
Coasting Arc #11 (Orbit 1764)
---------------------------------------
Vector Time (GMT): 2015/358/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905771
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5391736
66 A = 6779534
73 meter
Y = 372024
83 meter E =
0003920
Z = -4091424
60 I = 51
43073
XDOT = -3288
953984 Wp = 18
15214
YDOT = -5784
097970 meter/sec RA = 213
18586 deg
ZDOT = 3812
932587 TA = 291
31513
MA = 291
35697
Ha = 219
710 n
mi
Hp = 214
784
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17689424
72 X = -5375621
47
Y = 1220553
89 feet Y = 311821
41 meter
Z = -13423309
05 Z = -4117577
34
XDOT = -10790
531445 XDOT = -3242
552068
YDOT = -18976
699377 feet/sec YDOT = -5820
618183 meter/sec
ZDOT = 12509
621348 ZDOT = 3797
067632
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -1787895
97 X = -544950
69
Y = -17554420
58 feet Y = -5350587
39 meter
Z = -13536486
66 Z = -4125921
13
XDOT = 17333
957543 XDOT = 5283
390259
YDOT = -11348
052353 feet/sec YDOT = -3458
886357 meter/sec
ZDOT = 12442
037516 ZDOT = 3792
333035
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 15358
50908724
00016717 00000-0 10270-3 0 9105
2 25544 51
6409 214
2518 0008601 316
3364 43
7108 15
55010646 17656
Satellite: ISS
Catalog Number: 25544
Epoch time: 15358
50908724 = yrday
fracday
Element set: 910
Inclination: 51
6409 deg
RA of node: 214
2518 deg
Eccentricity:
0008601
Arg of perigee: 316
3364 deg
Mean anomaly: 43
7108 deg
Mean motion: 15
55010646 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1765
Checksum: 295
Coasting Arc #12 (Orbit 1780)
---------------------------------------
Vector Time (GMT): 2015/359/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905771
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6204751
81 A = 6783796
97 meter
Y = 1029743
74 meter E =
0008519
Z = 2540646
75 I = 51
47256
XDOT = 1260
919591 Wp = 65
51447
YDOT = 5429
518029 meter/sec RA = 208
18427 deg
ZDOT = -5262
645810 TA = 85
88097
MA = 85
78360
Ha = 219
968 n
mi
Hp = 214
446
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20356797
27 X = 6180434
41
Y = 3378424
33 feet Y = 1098993
12 meter
Z = 8335455
22 Z = 2570729
03
XDOT = 4136
875297 XDOT = 1225
675418
YDOT = 17813
379360 feet/sec YDOT = 5443
421979 meter/sec
ZDOT = -17265
898328 ZDOT = -5256
605567
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -2369542
99 X = -722236
70
Y = 20445416
22 feet Y = 6231762
86 meter
Z = 8465399
07 Z = 2580253
64
XDOT = -16088
613036 XDOT = -4903
809253
YDOT = 5297
158013 feet/sec YDOT = 1614
573762 meter/sec
ZDOT = -17240
734398 ZDOT = -5254
975845
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 15359
53733432
00016717 00000-0 10270-3 0 9112
2 25544 51
6408 209
1189 0008742 320
8012 39
2508 15
55060776 17819
Satellite: ISS
Catalog Number: 25544
Epoch time: 15359
53733432 = yrday
fracday
Element set: 911
Inclination: 51
6408 deg
RA of node: 209
1189 deg
Eccentricity:
0008742
Arg of perigee: 320
8012 deg
Mean anomaly: 39
2508 deg
Mean motion: 15
55060776 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1781
Checksum: 305
Coasting Arc #13 (Orbit 1795)
---------------------------------------
Vector Time (GMT): 2015/360/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905771
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6382619
01 A = 6786507
20 meter
Y = -2186561
52 meter E =
0015221
Z = -633821
25 I = 51
50829
XDOT = 1027
555855 Wp = 6
92420
YDOT = -4719
793468 meter/sec RA = 203
19471 deg
ZDOT = 5964
551754 TA = 346
21254
MA = 346
25406
Ha = 220
089 n
mi
Hp = 214
392
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20940351
08 X = -6354615
14
Y = -7173758
26 feet Y = -2257779
53 meter
Z = -2079466
05 Z = -664758
59
XDOT = 3371
246242 XDOT = 1051
284189
YDOT = -15484
886706 feet/sec YDOT = -4708
170607 meter/sec
ZDOT = 19568
739351 ZDOT = 5969
600500
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 5762195
71 X = 1756317
25
Y = -21358495
91 feet Y = -6510069
55 meter
Z = -2212926
33 Z = -674499
95
XDOT = 14107
548065 XDOT = 4299
980650
YDOT = 1785
653322 feet/sec YDOT = 544
267133 meter/sec
ZDOT = 19591
415328 ZDOT = 5971
463392
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 15360
50130313
00016717 00000-0 10270-3 0 9121
2 25544 51
6392 204
3052 0008716 323
8222 36
2340 15
55034459 17960
Satellite: ISS
Catalog Number: 25544
Epoch time: 15360
50130313 = yrday
fracday
Element set: 912
Inclination: 51
6392 deg
RA of node: 204
3052 deg
Eccentricity:
0008716
Arg of perigee: 323
8222 deg
Mean anomaly: 36
2340 deg
Mean motion: 15
55034459 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1796
Checksum: 275
Coasting Arc #14 (Orbit 1811)
---------------------------------------
Vector Time (GMT): 2015/361/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905771
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5877692
13 A = 6785835
93 meter
Y = 3094859
15 meter E =
0000768
Z = -1388222
19 I = 51
53555
XDOT = -3339
727050 Wp = 60
08259
YDOT = 3745
439006 meter/sec RA = 198
21211 deg
ZDOT = -5792
375513 TA = 135
06227
MA = 135
05605
Ha = 220
238 n
mi
Hp = 214
173
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 19283766
82 X = 5849391
17
Y = 10153737
36 feet Y = 3160429
27 meter
Z = -4554534
75 Z = -1359738
42
XDOT = -10957
109743 XDOT = -3353
224516
YDOT = 12288
185714 feet/sec YDOT = 3708
017025 meter/sec
ZDOT = -19003
856671 ZDOT = -5808
631447
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8498144
27 X = -2590234
37
Y = 20095926
91 feet Y = 6125238
52 meter
Z = -4431827
81 Z = -1350821
12
XDOT = -11686
236601 XDOT = -3561
964916
YDOT = -9146
997989 feet/sec YDOT = -2788
004987 meter/sec
ZDOT = -19074
853257 ZDOT = -5814
015273
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 15361
52952129
00016717 00000-0 10270-3 0 9132
2 25544 51
6388 199
1719 0008674 327
5185 32
5434 15
55062558 18121
Satellite: ISS
Catalog Number: 25544
Epoch time: 15361
52952129 = yrday
fracday
Element set: 913
Inclination: 51
6388 deg
RA of node: 199
1719 deg
Eccentricity:
0008674
Arg of perigee: 327
5185 deg
Mean anomaly: 32
5434 deg
Mean motion: 15
55062558 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1812
Checksum: 327
Coasting Arc #15 (Orbit 1827)
---------------------------------------
Vector Time (GMT): 2015/362/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 905771
4
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4674340
61 A = 6782196
66 meter
Y = -3711271
24 meter E =
0012014
Z = 3204056
41 I = 51
55390
XDOT = 5383
413243 Wp = 45
76344
YDOT = -2641
971711 meter/sec RA = 193
22251 deg
ZDOT = 4790
642867 TA = 351
38748
MA = 351
40808
Ha = 220
350 n
mi
Hp = 213
909
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -15335763
15 X = -4648056
69
Y = -12176086
75 feet Y = -3763396
07 meter
Z = 10511996
09 Z = 3181413
35
XDOT = 17662
116940 XDOT = 5389
285578
YDOT = -8667
886191 feet/sec YDOT = -2581
738333 meter/sec
ZDOT = 15717
332240 ZDOT = 4816
808060
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10557467
92 X = 3217916
22
Y = -16553539
63 feet Y = -5045518
88 meter
Z = 10414652
12 Z = 3174385
97
XDOT = 9188
313578 XDOT = 2800
597978
YDOT = 15826
254098 feet/sec YDOT = 4823
842249 meter/sec
ZDOT = 15831
025736 ZDOT = 4825
296644
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 15362
55772292
00016717 00000-0 10270-3 0 9148
2 25544 51
6383 194
0367 0008687 330
5873 29
4791 15
55109364 18286
Satellite: ISS
Catalog Number: 25544
Epoch time: 15362
55772292 = yrday
fracday
Element set: 914
Inclination: 51
6383 deg
RA of node: 194
0367 deg
Eccentricity:
0008687
Arg of perigee: 330
5873 deg
Mean anomaly: 29
4791 deg
Mean motion: 15
55109364 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1828
Checksum: 338
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