Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:orbit_type
|
| gptkbp:advantage |
long dwell time over northern hemisphere
|
| gptkbp:apogee_altitude |
~39,700 km
|
| gptkbp:argument_of_perigee |
270 degrees
|
| gptkbp:eccentricity |
high
|
| gptkbp:inclination |
63.4 degrees
|
| gptkbp:introducedIn |
1965
|
| gptkbp:namedAfter |
gptkb:Molniya_satellite
|
| gptkbp:orbital_shape |
elliptical
|
| gptkbp:orbitType |
~12 hours
|
| gptkbp:perigee_altitude |
~600 km
|
| gptkbp:provides_coverage |
high latitudes
|
| gptkbp:used_in |
gptkb:Russia
gptkb:Soviet_Union |
| gptkbp:usedFor |
communications satellites
early warning satellites |
| gptkbp:bfsParent |
gptkb:Molniya
gptkb:Highly_Elliptical_Orbit_(HEO) gptkb:NROL-34 gptkb:Oko_early-warning_satellite_system gptkb:Meridian_Two |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Molniya orbit
|