Lesson 2 of 7 · Raduga and geostationary links
Raduga: hold a direction in the sky
8 minute lesson · 3 checks along the way
Your goal for this lessonExplain the advantages and limits of a geostationary communications link.
In this lesson 3 sections · 3 checks
Using archive links & definitions
Follow a linked name to explore its archive card. “Back to your lesson” brings you to the same part of the reading.
Words with a dotted underline open a short definition right here in the lesson.
Read & understand
A different orbital solution
The Raduga communications family began with a launch on December 22, 1975. Manufacturer and ITU records connect the original system to telephone and television transmission and the Orbita ground network. Its offered a different operating arrangement from the strongly elliptical Molniya paths: a ground antenna could point toward approximately the same direction throughout the day.
This did not mean the spacecraft was parked without moving. In an ideal geostationary orbit, a satellite circles Earth over the equator in the same direction and at the same angular rate as Earth’s rotation. From a fixed ground site, those motions match. Operators still maintain the orbit and spacecraft attitude; a useful signal depends on the antenna beam reaching the intended receivers.
Check 1 of 3
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Read & understand
One location in the sky is not universal access
A stable direction can simplify a fixed ground installation, but geography remains important. At high latitudes an equatorial geostationary satellite appears low in the sky, and some locations cannot see it at all. Mountains, buildings and the curvature of Earth impose limits. Geostationary service and northern elliptical-orbit service therefore answer different combinations of requirements.
For a simplified teaching estimate, suppose a signal travels 36,000 kilometres up and 36,000 kilometres down. At 300,000 kilometres per second, that 72,000-kilometre path takes about 0.24 seconds one way. A reply over the same path needs about 0.48 seconds of propagation for the round trip, before processing. Real paths are often longer; these rounded distances are not measured Raduga performance.
Count the radio journey
Original teaching diagram. One-way path. 36,000 up + 36,000 down. 72,000 km / 300,000 km/s. Simplified result. 0.24 s one way. 0.48 s for a reply. Rounded teaching distances; processing and longer real paths add delay.
Open full-size diagram in a new tab: Count the radio journeyCheck 2 of 3
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Read & understand
Keep generations and physical evidence separate
Later Raduga-1 and Raduga-1M names represent developments in the lineage. The photograph documents an identified Raduga-1M display at Patriot Park, not the original 1975 spacecraft. Its visible panels and antennas illustrate the physical functions of power collection and radio communication. They do not establish undisclosed payload specifications or the operating status of a particular satellite.
The archive example Raduga-1M — S32373 records a 2007 launch. That flight card and the museum image answer different questions: one identifies a mission, while the other shows a displayed design. Neither should be silently used to claim that the displayed article flew on that mission. Keeping those distinctions preserves useful history while avoiding a misleading appearance of precision.
Raduga-1M display at Patriot Park, identified by photographer Vitaly V. Kuzmin. This illustrates the later lineage; it is not identified as the linked 2007 flight article. Display copy resized and converted to WebP.
Look closely
What kind of evidence does this photograph provide?
See what to notice
The display shows visible hardware form, solar panels and antennas. It does not establish the flight provenance, undisclosed payload details or current operational status of an individual satellite.
Check 3 of 3
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Put it together
Your lesson progress
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Explore further · Optional
Go to the source
Explore the evidence behind this lesson. These optional readings and videos open in a new tab.
- Read: Reshetnev: RadugaManufacturer specifies geostationary orbit and first launch on December 22, 1975. Specifications apply to this design, not every later Raduga variant.
- Read: ITU: satellites launched in 1975Contemporaneous registry, printed page 16, distinguishes elliptical Molniya systems and geostationary Raduga with Orbita ground-network connections.
- Read: Reshetnev: company historyFollow the manufacturer’s account of the Orbita network, Raduga links and Gorizont’s Olympic broadcasting requirement.