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physical object > artifact > device > instrument > artificial satellite > geosynchronous satellite > GMS satellite > GMS-4 |
GMS-4 | ||||
subject | fact |
GMS-4 | has dimension 2.146 m diameter cylinder, height 0.3451 m | |
has constant longitude 140 deg east | ||
has attitude control spin stabilized | ||
has launch vehicle H-I rocket | ||
has launch location Tanegashima Space Center, Kagoshima, Japan | ||
has launch date 6 Sept 1989 | ||
has mass 325 kg | ||
is an instance of GMS satellite | ||
GMS satellite | has specification | |
geosynchronous satellite | is a part of Earth | |
has orbital inclination approximately zero degrees | ||
has orbital period 24 hours (one day) | ||
orbits Earth | ||
has location above the same position on the Earth | ||
NASDA satellite | has creator NASDA | |
artificial satellite | has ground communication station | |
can have orbit decay date | ||
instrument | has operator | |
satellite | has approximately elliptical orbit | |
physical object | has angular momentum | |
has velocity | ||
has momentum | ||
has temperature | ||
has volume | ||
has extent | ||
has material | ||
artifact | has creation date | |
has purpose | ||
has owner |
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