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  2. Molniya (satellite) - Wikipedia

    en.wikipedia.org/wiki/Molniya_(satellite)

    Download as PDF; Printable version; ... (and the upgrade Molniya 1T) ... and the orbital period needed to be approximately half a sidereal day. These two factors ...

  3. Molniya orbit - Wikipedia

    en.wikipedia.org/wiki/Molniya_orbit

    Download as PDF; Printable version; ... is the orbital inclination, is the ... The exact height of a satellite in a Molniya orbit varies between missions, but a ...

  4. List of orbits - Wikipedia

    en.wikipedia.org/wiki/List_of_orbits

    Molniya orbit: A semi-synchronous variation of a Tundra orbit. For Earth this means an orbital period of just under 12 hours. Such a satellite spends most of its time over two designated areas of the planet. An inclination of 63.4° is normally used to keep the perigee shift small. [15]

  5. Highly elliptical orbit - Wikipedia

    en.wikipedia.org/wiki/Highly_elliptical_orbit

    A highly elliptical orbit (HEO) is an elliptic orbit with high eccentricity, usually referring to one around Earth.Examples of inclined HEO orbits include Molniya orbits, named after the Molniya Soviet communication satellites which used them, and Tundra orbits.

  6. Comparison of retired orbital launch systems - Wikipedia

    en.wikipedia.org/wiki/Comparison_of_retired...

    This comparison of retired orbital launch systems lists the attributes of all retired individual rocket configurations designed to reach orbit. For a list of proposed rocket configurations or individual configurations currently being launched check out Comparison of Orbital Launch Systems .

  7. IRS-1A - Wikipedia

    en.wikipedia.org/wiki/IRS-1A

    Toggle the table of contents. ... Download as PDF; Printable version; ... (570 mi), an inclination of 99.01°, and an orbital period of 102.7 minutes. [2] Mission

  8. Kosmos 1675 - Wikipedia

    en.wikipedia.org/wiki/Kosmos_1675

    A Molniya-M carrier rocket with a 2BL upper stage was used to perform the launch, which took place at 15:09 UTC on 12 August 1985. [3] The launch successfully placed the satellite into a molniya orbit. It subsequently received its Kosmos designation, and the international designator 1985-071A. [4]

  9. Molniya 1 - Wikipedia

    en.wikipedia.org/wiki/Molniya_1

    A total of 7 Molniya-1 satellites were launched, 5 of them successfully. In 1966, due to the heavy workload of OKB-1, the production of the Molniya-1 satellite was transferred to Branch No. 2 of OKB-1, nowadays Information Satellite Systems Reshetnev, and all subsequent satellites of the Molniya series were manufactured at this enterprise.