[list_settings.list_name] Current ISS TLEs @ 06:30 UTC
Date:
December 22nd 2015
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 19116 7 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 1671)
---------------------------------------
Vector Time (GMT): 2015/352/12:05:57
727
Vector Time (MET): N/A
Weight (LBS) : 920943
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1251627
56 A = 6785252
17 meter
Y = 6311099
26 meter E =
0003651
Z = -2149115
78 I = 51
32612
XDOT = -5310
252086 Wp = 247
40402
YDOT = -811
564870 meter/sec RA = 243
27570 deg
ZDOT = -5469
815597 TA = 316
53749
MA = 316
56627
Ha = 218
921 n
mi
Hp = 216
364
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4106389
62 X = 1191401
85
Y = 20705706
22 feet Y = 6324759
11 meter
Z = -7050904
79 Z = -2143181
71
XDOT = -17422
086896 XDOT = -5274
212049
YDOT = -2662
614402 feet/sec YDOT = -870
745927 meter/sec
ZDOT = -17945
589229 ZDOT = -5495
524198
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -20870133
88 X = -6361216
81
Y = 3220395
65 feet Y = 981576
60 meter
Z = -7026416
42 Z = -2141651
72
XDOT = 3671
265025 XDOT = 1119
001580
YDOT = -15648
284991 feet/sec YDOT = -4769
597265 meter/sec
ZDOT = -18056
560636 ZDOT = -5503
639682
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
53204125
00016717 00000-0 10270-3 0 9005
2 25544 51
6431 244
0899 0008255 293
5867 66
4419 15
54861409 16727
Satellite: ISS
Catalog Number: 25544
Epoch time: 15352
53204125 = yrday
fracday
Element set: 900
Inclination: 51
6431 deg
RA of node: 244
0899 deg
Eccentricity:
0008255
Arg of perigee: 293
5867 deg
Mean anomaly: 66
4419 deg
Mean motion: 15
54861409 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1672
Checksum: 316
Coasting Arc #2 (Orbit 1687)
---------------------------------------
Vector Time (GMT): 2015/353/12:05:57
727
Vector Time (MET): N/A
Weight (LBS) : 920943
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 58139
63 A = 6781056
97 meter
Y = -5635485
59 meter E =
0005027
Z = 3765062
02 I = 51
32771
XDOT = 5735
022096 Wp = 58
75454
YDOT = 2871
337915 meter/sec RA = 238
26824 deg
ZDOT = 4207
606462 TA = 346
60387
MA = 346
61721
Ha = 219
060 n
mi
Hp = 216
029
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 190746
81 X = 102863
41
Y = -18489125
95 feet Y = -5634585
50 meter
Z = 12352565
67 Z = 3765452
89
XDOT = 18815
689292 XDOT = 5682
048860
YDOT = 9420
399985 feet/sec YDOT = 2935
174391 meter/sec
ZDOT = 13804
483143 ZDOT = 4235
337538
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 18477847
97 X = 5632048
06
Y = 621413
73 feet Y = 189406
90 meter
Z = 12355283
12 Z = 3765890
29
XDOT = -9889
244393 XDOT = -3014
241691
YDOT = 17112
513495 feet/sec YDOT = 5215
894113 meter/sec
ZDOT = 13923
829768 ZDOT = 4243
983313
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
56036302
00016717 00000-0 10270-3 0 9010
2 25544 51
6432 238
9567 0008217 298
9091 61
1238 15
54902569 16889
Satellite: ISS
Catalog Number: 25544
Epoch time: 15353
56036302 = yrday
fracday
Element set: 901
Inclination: 51
6432 deg
RA of node: 238
9567 deg
Eccentricity:
0008217
Arg of perigee: 298
9091 deg
Mean anomaly: 61
1238 deg
Mean motion: 15
54902569 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1688
Checksum: 323
Coasting Arc #3 (Orbit 1702)
---------------------------------------
Vector Time (GMT): 2015/354/12:05:57
727
Vector Time (MET): N/A
Weight (LBS) : 920943
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1521999
31 A = 6776824
02 meter
Y = 4470854
58 meter E =
0009054
Z = -4866765
88 I = 51
33176
XDOT = -5725
269440 Wp = 28
31674
YDOT = -4518
208185 meter/sec RA = 233
24877 deg
ZDOT = -2354
149269 TA = 218
48335
MA = 218
54795
Ha = 219
197 n
mi
Hp = 215
671
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -4993436
05 X = -1548239
38
Y = 14668158
07 feet Y = 4453688
07 meter
Z = -15967079
67 Z = -4874223
02
XDOT = -18783
692388 XDOT = -5662
884598
YDOT = -14823
517668 feet/sec YDOT = -4581
883013 meter/sec
ZDOT = -7723
586842 ZDOT = -2381
810284
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -14615094
85 X = -4454680
91
Y = -5042999
38 feet Y = -1537106
21 meter
Z = -16000126
80 Z = -4876838
65
XDOT = 14650
136259 XDOT = 4465
361532
YDOT = -17513
232017 feet/sec YDOT = -5338
033119 meter/sec
ZDOT = -7842
344457 ZDOT = -2390
346590
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
52439534
00016717 00000-0 10270-3 0 9022
2 25544 51
6432 234
1451 0008400 302
1598 57
8739 15
54962074 17036
Satellite: ISS
Catalog Number: 25544
Epoch time: 15354
52439534 = yrday
fracday
Element set: 902
Inclination: 51
6432 deg
RA of node: 234
1451 deg
Eccentricity:
0008400
Arg of perigee: 302
1598 deg
Mean anomaly: 57
8739 deg
Mean motion: 15
54962074 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1703
Checksum: 302
Coasting Arc #4 (Orbit 1718)
---------------------------------------
Vector Time (GMT): 2015/355/12:05:57
727
Vector Time (MET): N/A
Weight (LBS) : 920943
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 3037792
38 A = 6774875
64 meter
Y = -2951908
99 meter E =
0006257
Z = 5291113
22 I = 51
34553
XDOT = 5201
648883 Wp = 315
87428
YDOT = 5630
520320 meter/sec RA = 228
22006 deg
ZDOT = 159
359493 TA = 132
62698
MA = 132
57421
Ha = 219
248 n
mi
Hp = 215
516
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 9966510
45 X = 3044873
22
Y = -9684740
78 feet Y = -2917899
12 meter
Z = 17359295
36 Z = 5305887
32
XDOT = 17065
777176 XDOT = 5137
526312
YDOT = 18472
835697 feet/sec YDOT = 5688
330054 meter/sec
ZDOT = 522
832981 ZDOT = 184
472804
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9750115
48 X = 2971835
20
Y = 9788797
14 feet Y = 2983625
37 meter
Z = 17423701
34 Z = 5310744
17
XDOT = -17642
220609 XDOT = -5377
348842
YDOT = 16476
753052 feet/sec YDOT = 5022
114330 meter/sec
ZDOT = 630
390083 ZDOT = 192
142897
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
55267911
00016717 00000-0 10270-3 0 9035
2 25544 51
6433 229
0122 0008361 305
6520 54
3854 15
54982506 17193
Satellite: ISS
Catalog Number: 25544
Epoch time: 15355
55267911 = yrday
fracday
Element set: 903
Inclination: 51
6433 deg
RA of node: 229
0122 deg
Eccentricity:
0008361
Arg of perigee: 305
6520 deg
Mean anomaly: 54
3854 deg
Mean motion: 15
54982506 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1719
Checksum: 302
Coasting Arc #5 (Orbit 1733)
---------------------------------------
Vector Time (GMT): 2015/356/12:05:57
727
Vector Time (MET): N/A
Weight (LBS) : 920943
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4418001
28 A = 6776131
87 meter
Y = 1304168
16 meter E =
0006077
Z = -4973875
75 I = 51
37127
XDOT = -4122
190497 Wp = 70
60244
YDOT = -6126
726494 meter/sec RA = 223
19138 deg
ZDOT = 2059
089116 TA = 219
48534
MA = 219
52964
Ha = 219
374 n
mi
Hp = 215
155
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -14494754
85 X = -4408095
14
Y = 4278766
94 feet Y = 1254818
94 meter
Z = -16318490
01 Z = -4995313
46
XDOT = -13524
247038 XDOT = -4063
375885
YDOT = -20100
808706 feet/sec YDOT = -6172
494863 meter/sec
ZDOT = 6755
541720 ZDOT = 2039
206609
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -4621677
44 X = -1408687
29
Y = -14283009
54 feet Y = -4353461
31 meter
Z = -16411417
27 Z = -5002199
98
XDOT = 18726
899291 XDOT = 5707
958904
YDOT = -13709
201075 feet/sec YDOT = -4178
564488 meter/sec
ZDOT = 6670
675077 ZDOT = 2033
221764
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
51667752
00016717 00000-0 10270-3 0 9040
2 25544 51
6425 224
1997 0008491 309
1595 50
8803 15
55015687 17345
Satellite: ISS
Catalog Number: 25544
Epoch time: 15356
51667752 = yrday
fracday
Element set: 904
Inclination: 51
6425 deg
RA of node: 224
1997 deg
Eccentricity:
0008491
Arg of perigee: 309
1595 deg
Mean anomaly: 50
8803 deg
Mean motion: 15
55015687 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1734
Checksum: 329
Coasting Arc #6 (Orbit 1749)
---------------------------------------
Vector Time (GMT): 2015/357/12:05:57
727
Vector Time (MET): N/A
Weight (LBS) : 920943
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5510734
09 A = 6779893
01 meter
Y = 335272
78 meter E =
0009096
Z = 3937506
83 I = 51
40828
XDOT = 2504
254850 Wp = 29
81553
YDOT = 6036
632940 meter/sec RA = 218
17388 deg
ZDOT = -4007
098424 TA = 102
20624
MA = 102
10435
Ha = 219
573 n
mi
Hp = 214
866
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18079836
26 X = 5487448
48
Y = 1099976
33 feet Y = 396766
88 meter
Z = 12918329
49 Z = 3964220
40
XDOT = 8216
059220 XDOT = 2456
030611
YDOT = 19805
226182 feet/sec YDOT = 6064
367918 meter/sec
ZDOT = -13146
648373 ZDOT = -3995
049784
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -358513
00 X = -109274
76
Y = 18026798
65 feet Y = 5494568
23 meter
Z = 13033789
27 Z = 3972698
97
XDOT = -18130
510692 XDOT = -5526
179659
YDOT = 9135
464062 feet/sec YDOT = 2784
489446 meter/sec
ZDOT = -13095
627174 ZDOT = -3991
547163
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
54492329
00016717 00000-0 10270-3 0 9051
2 25544 51
6424 219
0670 0008648 313
2497 46
7933 15
55072585 17502
Satellite: ISS
Catalog Number: 25544
Epoch time: 15357
54492329 = yrday
fracday
Element set: 905
Inclination: 51
6424 deg
RA of node: 219
0670 deg
Eccentricity:
0008648
Arg of perigee: 313
2497 deg
Mean anomaly: 46
7933 deg
Mean motion: 15
55072585 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1750
Checksum: 327
Coasting Arc #7 (Orbit 1764)
---------------------------------------
Vector Time (GMT): 2015/358/12:05:57
727
Vector Time (MET): N/A
Weight (LBS) : 920943
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6110484
64 A = 6784253
25 meter
Y = -1765090
92 meter E =
0010333
Z = -2341169
27 I = 51
44676
XDOT = -487
598921 Wp = 349
67077
YDOT = -5444
813407 meter/sec RA = 213
17072 deg
ZDOT = 5383
954385 TA = 344
11604
MA = 344
14842
Ha = 219
680 n
mi
Hp = 214
782
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -20047521
78 X = -6078920
33
Y = -5790980
70 feet Y = -1833245
66 meter
Z = -7681001
55 Z = -2370776
24
XDOT = -1599
733993 XDOT = -452
830578
YDOT = -17863
561047 feet/sec YDOT = -5450
072232 meter/sec
ZDOT = 17663
892339 ZDOT = 5381
669601
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 4614013
20 X = 1406351
22
Y = -20301991
90 feet Y = -6188047
13 meter
Z = -7808737
35 Z = -2380103
15
XDOT = 16250
923542 XDOT = 4953
281496
YDOT = -3089
499804 feet/sec YDOT = -941
679540 meter/sec
ZDOT = 17654
982434 ZDOT = 5381
238646
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
50888836
00016717 00000-0 10270-3 0 9061
2 25544 51
6408 214
2538 0008665 316
3183 43
7284 15
55046843 17659
Satellite: ISS
Catalog Number: 25544
Epoch time: 15358
50888836 = yrday
fracday
Element set: 906
Inclination: 51
6408 deg
RA of node: 214
2538 deg
Eccentricity:
0008665
Arg of perigee: 316
3183 deg
Mean anomaly: 43
7284 deg
Mean motion: 15
55046843 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1765
Checksum: 334
Coasting Arc #8 (Orbit 1780)
---------------------------------------
Vector Time (GMT): 2015/359/12:05:57
727
Vector Time (MET): N/A
Weight (LBS) : 920943
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6108902
44 A = 6786500
05 meter
Y = 2927882
90 meter E =
0004636
Z = 382268
69 I = 51
48126
XDOT = -1759
289293 Wp = 112
67029
YDOT = 4459
013242 meter/sec RA = 208
18189 deg
ZDOT = -5981
724252 TA = 63
20037
MA = 63
15296
Ha = 219
888 n
mi
Hp = 214
510
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20042330
84 X = 6073851
21
Y = 9605915
04 feet Y = 2996000
66 meter
Z = 1254162
37 Z = 411859
49
XDOT = -5771
946498 XDOT = -1779
963591
YDOT = 14629
308538 feet/sec YDOT = 4439
224766 meter/sec
ZDOT = -19625
079567 ZDOT = -5990
320194
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -8064807
65 X = -2458153
37
Y = 20702451
36 feet Y = 6310107
17 meter
Z = 1381643
16 Z = 421124
84
XDOT = -13502
593489 XDOT = -4115
590495
YDOT = -3936
581960 feet/sec YDOT = -1199
870181 meter/sec
ZDOT = -19663
054908 ZDOT = -5993
299136
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
53709923
00016717 00000-0 10270-3 0 9075
2 25544 51
6404 209
1208 0008561 320
2670 39
7855 15
55074852 17810
Satellite: ISS
Catalog Number: 25544
Epoch time: 15359
53709923 = yrday
fracday
Element set: 907
Inclination: 51
6404 deg
RA of node: 209
1208 deg
Eccentricity:
0008561
Arg of perigee: 320
2670 deg
Mean anomaly: 39
7855 deg
Mean motion: 15
55074852 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1781
Checksum: 319
Coasting Arc #9 (Orbit 1796)
---------------------------------------
Vector Time (GMT): 2015/360/12:05:57
727
Vector Time (MET): N/A
Weight (LBS) : 920943
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5416073
29 A = 6785347
24 meter
Y = -3730476
55 meter E =
0015070
Z = 1629295
61 I = 51
50518
XDOT = 3960
330592 Wp = 29
10892
YDOT = -3249
028124 meter/sec RA = 203
19498 deg
ZDOT = 5716
455870 TA = 348
78478
MA = 348
81834
Ha = 219
966 n
mi
Hp = 214
296
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -17769269
32 X = -5381870
06
Y = -12239096
31 feet Y = -3790851
59 meter
Z = 5345458
05 Z = 1603068
40
XDOT = 12993
210603 XDOT = 3968
599639
YDOT = -10659
541088 feet/sec YDOT = -3204
695451 meter/sec
ZDOT = 18754
776476 ZDOT = 5735
713890
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10535512
23 X = 3211224
13
Y = -18861036
79 feet Y = -5748844
01 meter
Z = 5232648
05 Z = 1594911
12
XDOT = 10429
813843 XDOT = 3179
007259
YDOT = 11061
077257 feet/sec YDOT = 3371
416348 meter/sec
ZDOT = 18838
667369 ZDOT = 5742
025814
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
56528962
00016717 00000-0 10270-3 0 9083
2 25544 51
6392 203
9857 0008623 323
3611 36
6952 15
55129030 17976
Satellite: ISS
Catalog Number: 25544
Epoch time: 15360
56528962 = yrday
fracday
Element set: 908
Inclination: 51
6392 deg
RA of node: 203
9857 deg
Eccentricity:
0008623
Arg of perigee: 323
3611 deg
Mean anomaly: 36
6952 deg
Mean motion: 15
55129030 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1797
Checksum: 323
Coasting Arc #10 (Orbit 1811)
---------------------------------------
Vector Time (GMT): 2015/361/12:05:57
727
Vector Time (MET): N/A
Weight (LBS) : 920943
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 4084005
21 A = 6781508
17 meter
Y = 4203774
05 meter E =
0007251
Z = -3419119
78 I = 51
52120
XDOT = -5827
092894 Wp = 1
77218
YDOT = 1923
260156 meter/sec RA = 198
20292 deg
ZDOT = -4588
768770 TA = 218
29447
MA = 218
34598
Ha = 220
128 n
mi
Hp = 214
080
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 13398967
23 X = 4053302
58
Y = 13791909
60 feet Y = 4249272
73 meter
Z = -11217584
57 Z = -3399354
98
XDOT = -19117
758838 XDOT = -5825
876019
YDOT = 6309
908647 feet/sec YDOT = 1858
104971 meter/sec
ZDOT = -15055
015648 ZDOT = -4617
072077
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -12228167
07 X = -3727145
32
Y = 14903556
89 feet Y = 4542604
14 meter
Z = -11132799
26 Z = -3393277
21
XDOT = -7272
312754 XDOT = -2216
600927
YDOT = -17321
390119 feet/sec YDOT = -5279
559708 meter/sec
ZDOT = -15177
821906 ZDOT = -4626
200117
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
52920329
00016717 00000-0 10270-3 0 9094
2 25544 51
6382 199
1727 0008679 327
6258 32
4362 15
55140364 18122
Satellite: ISS
Catalog Number: 25544
Epoch time: 15361
52920329 = yrday
fracday
Element set: 909
Inclination: 51
6382 deg
RA of node: 199
1727 deg
Eccentricity:
0008679
Arg of perigee: 327
6258 deg
Mean anomaly: 32
4362 deg
Mean motion: 15
55140364 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1812
Checksum: 320
Coasting Arc #11 (Orbit 1827)
---------------------------------------
Vector Time (GMT): 2015/362/12:05:57
727
Vector Time (MET): N/A
Weight (LBS) : 920943
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -2201070
69 A = 6777059
85 meter
Y = -4352031
40 meter E =
0005076
Z = 4701249
85 I = 51
53700
XDOT = 7124
972187 Wp = 36
41349
YDOT = -599
916824 meter/sec RA = 193
19708 deg
ZDOT = 2782
934832 TA = 26
00403
MA = 25
97854
Ha = 220
327 n
mi
Hp = 213
805
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -7221360
53 X = -2175078
12
Y = -14278318
25 feet Y = -4376500
23 meter
Z = 15424048
08 Z = 4690620
49
XDOT = 23375
893001 XDOT = 7117
632847
YDOT = -1968
231049 feet/sec YDOT = -520
281911 meter/sec
ZDOT = 9130
363623 ZDOT = 2817
528088
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13232553
91 X = 4033282
43
Y = -9072568
85 feet Y = -2765318
99 meter
Z = 15378806
54 Z = 4687460
23
XDOT = 4248
694596 XDOT = 1295
002113
YDOT = 21913
820898 feet/sec YDOT = 6679
332610 meter/sec
ZDOT = 9280
174893 ZDOT = 2828
597307
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
55736019
00016717 00000-0 10270-3 0 9101
2 25544 51
6382 194
0375 0008733 331
6435 28
4242 15
55135432 18287
Satellite: ISS
Catalog Number: 25544
Epoch time: 15362
55736019 = yrday
fracday
Element set: 910
Inclination: 51
6382 deg
RA of node: 194
0375 deg
Eccentricity:
0008733
Arg of perigee: 331
6435 deg
Mean anomaly: 28
4242 deg
Mean motion: 15
55135432 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1828
Checksum: 302
Coasting Arc #12 (Orbit 1842)
---------------------------------------
Vector Time (GMT): 2015/363/12:05:57
727
Vector Time (MET): N/A
Weight (LBS) : 920943
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 27260
59 A = 6774379
35 meter
Y = 4245454
83 meter E =
0014246
Z = -5289309
40 I = 51
55939
XDOT = -7613
782706 Wp = 51
28914
YDOT = -650
633501 meter/sec RA = 188
18184 deg
ZDOT = -553
762677 TA = 213
37116
MA = 213
46104
Ha = 220
321 n
mi
Hp = 213
482
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 89437
62 X = 5477
87
Y = 13928657
57 feet Y = 4245638
15 meter
Z = -17353377
30 Z = -5289229
66
XDOT = -24979
602054 XDOT = -7603
251368
YDOT = -2134
624348 feet/sec YDOT = -735
716939 meter/sec
ZDOT = -1816
806684 ZDOT = -590
722759
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13753100
50 X = -4191945
03
Y = 2203219
25 feet Y = 671541
23 meter
Z = -17353767
77 Z = -5289428
42
XDOT = -1320
570118 XDOT = -402
509772
YDOT = -24011
837302 feet/sec YDOT = -7318
808010 meter/sec
ZDOT = -1976
664277 ZDOT = -602
487272
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 15363
52123851
00016717 00000-0 10270-3 0 9114
2 25544 51
6376 189
2238 0008588 335
2833 24
7907 15
55193595 18432
Satellite: ISS
Catalog Number: 25544
Epoch time: 15363
52123851 = yrday
fracday
Element set: 911
Inclination: 51
6376 deg
RA of node: 189
2238 deg
Eccentricity:
0008588
Arg of perigee: 335
2833 deg
Mean anomaly: 24
7907 deg
Mean motion: 15
55193595 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1843
Checksum: 330
Coasting Arc #13 (Orbit 1858)
---------------------------------------
Vector Time (GMT): 2015/364/12:05:57
727
Vector Time (MET): N/A
Weight (LBS) : 920943
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 2237304
96 A = 6775252
69 meter
Y = -3901116
19 meter E =
0011088
Z = 5069375
93 I = 51
59460
XDOT = 7233
777817 Wp = 6
64574
YDOT = 1816
248399 meter/sec RA = 183
16571 deg
ZDOT = -1783
678039 TA = 100
68309
MA = 100
55820
Ha = 220
386 n
mi
Hp = 213
314
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 7340239
36 X = 2256137
19
Y = -12798937
63 feet Y = -3875992
06 meter
Z = 16631810
78 Z = 5080289
74
XDOT = 23732
866855 XDOT = 7221
594751
YDOT = 5958
820208 feet/sec YDOT = 1897
073231 meter/sec
ZDOT = -5851
962071 ZDOT = -1748
567849
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 13794697
31 X = 4204623
74
Y = 5079576
41 feet Y = 1548254
89 meter
Z = 16679726
55 Z = 5083980
65
XDOT = -1684
655101 XDOT = -513
482875
YDOT = 23413
029238 feet/sec YDOT = 7136
291312 meter/sec
ZDOT = -5700
293360 ZDOT = -1737
449416
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 15364
54935840
00016717 00000-0 10270-3 0 9127
2 25544 51
6379 184
0893 0008607 338
7685 21
3109 15
55195794 18597
Satellite: ISS
Catalog Number: 25544
Epoch time: 15364
54935840 = yrday
fracday
Element set: 912
Inclination: 51
6379 deg
RA of node: 184
0893 deg
Eccentricity:
0008607
Arg of perigee: 338
7685 deg
Mean anomaly: 21
3109 deg
Mean motion: 15
55195794 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1859
Checksum: 348
Coasting Arc #14 (Orbit 1873)
---------------------------------------
Vector Time (GMT): 2015/365/12:05:57
727
Vector Time (MET): N/A
Weight (LBS) : 920943
6
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -4221479
46 A = 6778869
40 meter
Y = 3375417
70 meter E =
0007317
Z = -4091244
95 I = 51
63938
XDOT = -5993
179795 Wp = 39
33078
YDOT = -2849
854790 meter/sec RA = 178
15964 deg
ZDOT = 3842
025723 TA = 270
34286
MA = 270
42671
Ha = 220
426 n
mi
Hp = 212
947
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -13849998
22 X = -4239037
01
Y = 11074205
05 feet Y = 3328112
27 meter
Z = -13422719
65 Z = -4111794
33
XDOT = -19662
663371 XDOT = -5979
529449
YDOT = -9349
917289 feet/sec YDOT = -2916
798276 meter/sec
ZDOT = 12605
071271 ZDOT = 3812
945506
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13344788
20 X = -4067491
44
Y = -11574335
70 feet Y = -3527857
52 meter
Z = -13512263
03 Z = -4118537
77
XDOT = 4843
435129 XDOT = 1476
279027
YDOT = -20118
111522 feet/sec YDOT = -6132
000392 meter/sec
ZDOT = 12479
667281 ZDOT = 3803
802587
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 15365
51320319
00016717 00000-0 10270-3 0 9135
2 25544 51
6380 179
2751 0008540 342
9097 17
1768 15
55248207 18747
Satellite: ISS
Catalog Number: 25544
Epoch time: 15365
51320319 = yrday
fracday
Element set: 913
Inclination: 51
6380 deg
RA of node: 179
2751 deg
Eccentricity:
0008540
Arg of perigee: 342
9097 deg
Mean anomaly: 17
1768 deg
Mean motion: 15
55248207 rev/day
Decay rate: 1
67170E-04 rev/day^2
Epoch rev: 1874
Checksum: 316
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