| |
N2WWD > SAREX 29.09.97 12:21l 64 Lines 1828 Bytes #-10395 (0) @ AMSAT
BID : N6IYA15517
Read: GUEST OE7FMI
Subj: STS-86 Rev 1 Orbital Data
Path: DB0AAB<DB0KFB<DB0CZ<DB0GE<LX0PAC<ON5VL<ON1ANR<ON6AR<F6CNB<PP5BLU<
WB0TAX<KC6UFM<VE7ASS<VE7VBS<VE7DIE<N7MGZ<N7WE<KB7CNN<N7QDN<W0RLI<
N6IYA<W0RLI<KC7KVT<WA7SJN<KB7CNN<N7WE<VE7DIE<VE7SRY<VE7KIT<KA6EYH<
KO4KS<N4HHP<N4GAA<N2BQF<KC2FD
Sent: 970926/0436 @:KC2FD.#NLI.NY.USA.NOAM #:53641 $:53641_KC2FD
From: N2WWD@KC2FD.#NLI.NY.USA.NOAM
To : SAREX@AMSAT
Below is the current State Vector and Keplerian Elements for
STS-86. The vector data comes from NASA; the Keplerian Elements
were computed from the vector.
This file may be read by VEC2TLE version 9648 to update your
Keplerian Elements text file.
Vector format = 117
Satellite Name: STS-86
Catalog Number: 24964 97055A
Epoch Date/Time: 97269.13748726900
09/26/1997 03:17:58.900 UTC
EFG E: 6614698.00000000 ft
F: 20543550.0000000 ft
G: -3742877.0000000 ft
Edot: -14705.670000000 ft/s
Fdot: 1191.90000000000 ft/s
Gdot: -19385.459999999 ft/s
ndot/2 (drag): 0.00050150800 rev/day^2
nddt/6: 1.04870E-08 rev/day^3
Bstar: 9.46296E-05 1/Earth Radii
Elset #: 1
Rev @ Epoch: 1.53507853576
Launch occurred: 26-SEP-97 / 02:34:19.072 UTC
The following Keplerian elements were computed by VEC2TLE from this
vector, using a 1.0 drag multiplier:
STS-86
1 24964U 97055A 97269.13748727 .00050151 10487-7 94630-4 0 12
2 24964 51.6548 298.7294 0031237 351.0989 201.5193 15.99060847 19
Satellite: STS-86
Catalog number: 24964
Epoch time: 97269.13748727
Element set: 1
Inclination: 51.6548 deg
RA of node: 298.7294 deg
Eccentricity: 0.0031237
Arg of perigee: 351.0989 deg
Mean anomaly: 201.5193 deg
Mean motion: 15.99060847 rev/day
Decay rate: 5.01508e-04 rev/day^2
Epoch rev: 1
Checksum: 331
VEC2TLE may be downloaded from:
http://www.amsat.org/amsat/sarex/orbit.html
Ken Ernandes
n2wwd@amsat.org
http://www.mindspring.com/~n2wwd
Read previous mail | Read next mail
| |
