Molniya orbit

E529484

A Molniya orbit is a highly elliptical, high-inclination Earth orbit designed to provide long-duration coverage over high latitudes, particularly useful for communications and observation of polar regions.

All labels observed (1)

Label Occurrences
Molniya orbit canonical 4

How this entity was disambiguated

Statements (49)

Predicate Object
instanceOf Earth orbit ⓘ
communications orbit ⓘ
highly elliptical orbit ⓘ
satellite orbit ⓘ
advantageOver geostationary orbit for high-latitude coverage ⓘ
apoapsisLocation high northern latitudes above Earth ⓘ
appliesTo artificial Earth satellites ⓘ
benefit high elevation angles over target region ⓘ
improved link budget for communications ⓘ
long visibility periods from ground stations in high latitudes ⓘ
reduced atmospheric attenuation at high latitudes ⓘ
designedFor communications in high-latitude regions ⓘ
long-duration coverage over high latitudes ⓘ
meteorological observation of high latitudes ⓘ
military communications ⓘ
observation of polar regions ⓘ
television broadcasting to high latitudes ⓘ
developedBy Soviet Union ⓘ
hasCharacteristic argument of perigee near 270 degrees ⓘ
frozen argument of perigee at critical inclination ⓘ
ground track concentrated over high latitudes ⓘ
high eccentricity ⓘ
high inclination ⓘ
long dwell time over northern hemisphere ⓘ
short time near perigee over southern hemisphere ⓘ
limitationOf geostationary satellites at high latitudes ⓘ
namedAfter Soviet Molniya communications satellite program ⓘ
periapsisLocation southern hemisphere above Earth ⓘ
providesCoverage Arctic regions ⓘ
linked to: Arctic region

Russian territory at high latitudes ⓘ
northern high-latitude regions ⓘ
relatedTo Tundra orbit ⓘ
geosynchronous orbit ⓘ
requiresConstellationSize sometimes 2 satellites for partial coverage ⓘ
typically 3 satellites for continuous coverage ⓘ
requiresStationKeeping to maintain orbital parameters over time ⓘ
stabilityProperty argument of perigee remains nearly fixed at critical inclination ⓘ
typicalApogeeAltitude about 39,000 kilometers ⓘ
typicalEccentricity high eccentricity ⓘ
typicalInclination 63.3 degrees ⓘ
63.4 degrees ⓘ
typicalOrbitalPeriod about 12 hours ⓘ
half a sidereal day ⓘ
typicalPerigeeAltitude about 500 to 1,000 kilometers ⓘ
usedBy Russian communications satellites ⓘ
Soviet communications satellites ⓘ
communications satellites for northern Canada ⓘ
military early-warning satellites ⓘ
usesResonance 2:1 resonance with Earth rotation ⓘ

How these facts were elicited

Referenced by (4)

Full triples — surface form annotated when it differs from this entity's canonical label.

Molniya-M → typicalOrbit → Molniya orbit ⓘ
subject linked to: Molniya-M rocket
Blok-L → orbitTypeTargeted → Molniya orbit ⓘ
Earth orbit → hasType → Molniya orbit ⓘ