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INTERCOSMOS 24

Intercosmos 24 was part of the Soviet Intercosmos scientific program, which involved international cooperation on space research. Missions in this family studied Earth's upper atmosphere, magnetosphere and related phenomena.

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Object identity

NORAD ID
20261
COSPAR ID
1989-080A
Operator
Not listed
Country
Not listed
Launch date
Not listed

Immediate discovery

Why this satellite matters

The magnetosphere is governed by charged-particle motion in magnetic and electric fields, linking satellite measurements to Lorentz-force equations.

Understanding the mission

Science and engineering ideas

The magnetosphere is governed by charged-particle motion in magnetic and electric fields, linking satellite measurements to Lorentz-force equations.

Mission

Mission and purpose

The current public orbital catalog identifies this object, but verified mission-specific information may be limited. TransitSatellite will expand this page when authoritative information is available.

  • The magnetosphere is governed by charged-particle motion in magnetic and electric fields, linking satellite measurements to Lorentz-force equations.

Design

Engineering

The magnetosphere is governed by charged-particle motion in magnetic and electric fields, linking satellite measurements to Lorentz-force equations.

Real orbital values

The mathematics

The current two-line element set reports approximately 12.5973 revolutions per day. Dividing 1,440 minutes by that value gives an estimated orbital period of 114.3 minutes.

Period

114.3 min

Representative speed

25,731 km/h

Representative altitude

1,431 km

Inclination

82.61°

These are representative calculations derived from current orbital elements, not fixed physical specifications. Altitude and speed change around an elliptical orbit, and predictions change as new orbital elements are published.

Launch record

Launch and deployment

The orbital catalog lists the launch designator as 1989-080A. A fully sourced launch story, launch vehicle, deployment sequence, historical weather, and documented delays have not yet been added to this page.

TransitSatellite does not estimate historical launch weather. Temperature, clouds, wind, holds, and scrub reasons will appear only when supported by traceable historical sources.

Orbit

LEO orbit explained

Low Earth orbit is the region closest to Earth used by most crewed spacecraft, many science missions, Earth-observation satellites, and large constellations. Objects move quickly and commonly complete an orbit in roughly 90 to 130 minutes.

LEO can provide detailed Earth views, lower communications delay, and easier access than higher orbits, but it covers less area per spacecraft and is more affected by atmospheric drag.

Live TransitSatellite experience

See INTERCOSMOS 24 moving now

Open the live tracker to view its current calculated position, trajectory, orbital information, visibility tools, and Save and Share controls.

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Learning

Questions to explore

  • What can an orbit tell us before the mission is fully identified?
  • Why are stable catalog identifiers important?

Evidence

Sources and data notes

Current identity and orbital elements come from CelesTrak’s public GP data. Calculated orbit values are derived from the current TLE and may change after catalog updates. Mission-history claims are added separately and require authoritative sources.

Catalog updated

Sep 19, 2026, 11:18 AM UTC

Story review

1970-01-01T00:00:00.000Z