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PD0RDD > NASA     04.11.98 18:48l 80 Lines 3064 Bytes #-9820 (0) @ WW
BID : 36526_PI8WNO
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Subj: Nasa Information 236
Path: DB0AAB<DB0KFB<DB0CZ<DB0LJ<DB0ZDF<DB0SRS<DB0SIF<DB0HSK<PI8DRS<PI8DAZ<
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Sent: 981104/1203Z @:PI8WNO.#UTR.NLD.EU #:36526 [DeMeern] FBB5.15c $:36526_PI8W
From: PD0RDD@PI8WNO.#UTR.NLD.EU
To  : NASA@WW


Onderwerp: STS-95 Orbital Data (Rev 2)
STS-95
1 25519U 98064A   98302.91811343  .00000064  00000-0  46092-5 0    22
2 25519  28.4666 157.5897 0006551  39.2226 289.6558 15.03348307    28

Launch time for STS-95: 29 OCT 98 @ 19:19:34 UTC

Earth-Fixed Greenwich State Vector:

Vector format = 117
Satellite Name:         STS-95
Catalog Number:         25519  98064A
Epoch Date/Time:        98302.91811342600
                        10/29/1998  22:02:05.000 UTC
EFG E:                   -11339957.000000 ft
    F:                   18900144.0000000 ft
    G:                   -5620597.0000000 ft
    Edot:                -19301.799999999 ft/s
    Fdot:                -8590.2199999999 ft/s
    Gdot:                10153.8500000000 ft/s
ndot/2 (drag):              0.00000064280 rev/day^2
nddt/6:                       0.00000E+00 rev/day^3
Bstar:                        4.60919E-06 1/Earth Radii
Elset #:                                2
Rev @ Epoch:                2.91359271518

Keplerian Elements (Amsat format):

Satellite: STS-95
Catalog number: 25519
Epoch time:      98302.91811343
Element set:       2
Inclination:       28.4666 deg
RA of node:       157.5897 deg
Eccentricity:    0.0006551
Arg of perigee:    39.2226 deg
Mean anomaly:     289.6558 deg
Mean motion:   15.03348307 rev/day
Decay rate:    6.42800e-07 rev/day^2
Epoch rev:               2
Checksum:              315


SPACE SHUTTLE ORBITAL DATA:

These 2-line elements have been generated using Ken Ernandes' program
VEC2TLE using real time state vector data supplied by DOD C-Band Radar
Network courtesy Dave Simonson. Note that the epoch of the 2-line
elements is the same as the state vector time.

Drag and B-Star parameters are internally calculated by VEC2TLE using
a drag factor of 0.1. Rev numbers use NASA orbit numbering convention.

                                   Dave Ransom
                                   RPV Astronomy BBS
                                   http://www.dransom.com
                                   http://tie.jpl.nasa.gov/dransom/


----------
David H. Ransom, Jr.   Email:rans7500@spacelink.nasa.gov

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