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HELIOS 1B

NORAD 25977 Payload LEO 1999-064A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
603 km
Apogee
607 km
Inclination
98.2°
Period
96.8 min
Mean Motion
14.87730442 rev/day
TLE Epoch
2026-03-17 15:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude605 km
Orbital Velocity27,212 km/h
Velocity7.56 km/s
Orbital Period97 minutes
Orbits / Day14.88
Eccentricity0.0003
Semi-Major Axis6,976 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇫🇷 France
Launch Date
1999-12-03
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1999-064A
Object Type
Payload
RCS Size
Large (>1 m²)
🔗 Constellation / Groups
visual
📖 About This Object
HELIOS 1B is an active satellite operated by France, launched on 1999-12-03 from Guiana Space Centre, Kourou. With over 27 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 603 km and 607 km with an inclination of 98.2°. It travels at approximately 27,212 km/h (7.56 km/s), completing one full orbit every 97 minutes — that’s roughly 14.88 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~10–25 years. Orbital Radar tracks HELIOS 1B in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
HELIOS 1B operates in a sun-synchronous orbit (SSO), a special subset of LEO where the orbital plane precesses to keep a constant angle relative to the Sun. This means the satellite crosses any given latitude at approximately the same local solar time on every pass, providing consistent lighting conditions — essential for Earth observation, weather monitoring and environmental science. SSO orbits typically sit between 600 and 800 km altitude with inclinations near 97–99°.
❓ Frequently Asked Questions
HELIOS 1B is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 605 km altitude. Its 98.2° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 97 minutes, travelling at 27,212 km/h.
HELIOS 1B is operated by France. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 25977. You can track HELIOS 1B in real time on Orbital Radar’s live tracker.
HELIOS 1B was launched on 1999-12-03 from Guiana Space Centre, Kourou, the European spaceport in French Guiana, chosen for its equatorial location which provides an energy-efficient boost for orbital insertions. At its current altitude, the estimated remaining orbital lifetime is: ~10–25 years.
Yes — Orbital Radar tracks HELIOS 1B (NORAD ID 25977) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. Open the live tracker to see its current position, altitude, speed and orbital path updated in real time.
HELIOS 1B travels at approximately 27,212 km/h (16,909 mph) — roughly 7.56 km/s. It completes 14.88 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.