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ERS-1

NORAD 21574 Payload LEO 1991-050A ● Active
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Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
737 km
Apogee
783 km
Inclination
98.8°
Period
100.0 min
Mean Motion
14.39455446 rev/day
TLE Epoch
2026-03-17 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude760 km
Orbital Velocity26,915 km/h
Velocity7.48 km/s
Orbital Period100 minutes
Orbits / Day14.39
Eccentricity0.0032
Semi-Major Axis7,131 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
ESA (European Space Agency)
Launch Date
1991-07-17
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1991-050A
Object Type
Payload
RCS Size
Large (>1 m²)
🔗 Constellation / Groups
visual
📖 About This Object
ERS-1 is an active satellite operated by ESA (European Space Agency), launched on 1991-07-17 from Guiana Space Centre, Kourou. With over 35 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 737 km and 783 km with an inclination of 98.8°. It travels at approximately 26,915 km/h (7.48 km/s), completing one full orbit every 100 minutes — that’s roughly 14.39 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. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. Orbital Radar tracks ERS-1 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
ERS-1 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
ERS-1 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 760 km altitude. Its 98.8° 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 100 minutes, travelling at 26,915 km/h.
ERS-1 is operated by ESA (European Space Agency). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 21574. You can track ERS-1 in real time on Orbital Radar’s live tracker.
ERS-1 was launched on 1991-07-17 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: ~25–100 years.
Yes — Orbital Radar tracks ERS-1 (NORAD ID 21574) 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.
ERS-1 travels at approximately 26,915 km/h (16,724 mph) — roughly 7.48 km/s. It completes 14.39 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.