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HELIOS 1B

Helios 1B was a French-led military Earth-observation satellite launched in 1999, part of Europe's early optical reconnaissance capability.

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Object identity

NORAD ID
25977
COSPAR ID
1999-064A
Operator
Not listed
Country
Not listed
Launch date
Not listed

Immediate discovery

Why this satellite matters

Optical reconnaissance from orbit depends on the same geometry as civilian imaging: altitude, focal length, aperture, detector sampling and atmospheric conditions all affect what can be resolved.

Understanding the mission

Science and engineering ideas

Optical reconnaissance from orbit depends on the same geometry as civilian imaging: altitude, focal length, aperture, detector sampling and atmospheric conditions all affect what can be resolved.

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.

  • Optical reconnaissance from orbit depends on the same geometry as civilian imaging: altitude, focal length, aperture, detector sampling and atmospheric conditions all affect what can be resolved.

Design

Engineering

Optical reconnaissance from orbit depends on the same geometry as civilian imaging: altitude, focal length, aperture, detector sampling and atmospheric conditions all affect what can be resolved.

Real orbital values

The mathematics

The current two-line element set reports approximately 14.882 revolutions per day. Dividing 1,440 minutes by that value gives an estimated orbital period of 96.8 minutes.

Period

96.8 min

Representative speed

27,201 km/h

Representative altitude

611 km

Inclination

98.15°

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

Helios 1B launched on 3 December 1999 aboard an Ariane 4 from Kourou.

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

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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 17, 2026, 8:52 AM UTC

Story review

1970-01-01T00:00:00.000Z