ERS 2 DEB
NORAD 35393
Debris
LEO
1995-021G
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LEO · NORAD 35393
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
703 km
Apogee
707 km
Inclination
98.5°
Period
98.9 min
Mean Motion
14.56347034 rev/day
TLE Epoch
2026-06-20 10:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude705 km
Orbital Velocity27,020 km/h
Velocity7.51 km/s
Orbital Period99 minutes
Orbits / Day14.56
Eccentricity0.0003
Semi-Major Axis7,076 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
ESA (European Space Agency)
Launch Date
1995-04-21
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1995-021G
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
ERS 2 DEB is a tracked piece of space debris attributed to ESA (European Space Agency), launched on 1995-04-21 from Guiana Space Centre, Kourou on the ERS-2 launch. With over 31 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 703 km and 707 km with an inclination of 98.5°. It travels at approximately 27,020 km/h (7.51 km/s), completing one full orbit every 99 minutes — that’s roughly 14.56 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 ~25–100 years. As orbital debris, ERS 2 DEB poses a potential collision risk to operational satellites in nearby orbits and is continuously monitored by the U.S. Space Surveillance Network and other tracking systems.
🌍 Orbit Context
ERS 2 DEB orbits at an average altitude of 705 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of ERS 2 DEB’s average altitude, there are currently 251 active payloads and 1,494 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, LANDSAT 9. With an inclination of 98.5°, ERS 2 DEB passes over latitudes between 98.5°N and 98.5°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. ESA (European Space Agency) operates approximately 93 active satellites in total, of which 8 share a similar altitude band with ERS 2 DEB.
🔗 Tracked Space Debris
This is a tracked piece of orbital debris — a fragment from a collision, explosion, or separation event that no longer serves any useful purpose. Space surveillance networks catalogue objects larger than approximately 10 cm in LEO. Even small debris can be catastrophic at orbital velocities (7–8 km/s in LEO), carrying kinetic energy comparable to a hand grenade per centimetre-sized fragment. The growing debris population is one of the most pressing challenges for long-term space sustainability.
❓ Frequently Asked Questions
ERS 2 DEB is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 705 km altitude. Its 98.5° 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 99 minutes, travelling at 27,020 km/h.
ERS 2 DEB (NORAD ID 35393) is a piece of tracked orbital debris attributed to ESA (European Space Agency). It was likely created by a fragmentation event, collision, or mission-related separation. Even small debris objects at orbital velocities carry enormous kinetic energy, so they are tracked by the U.S. Space Surveillance Network to enable collision avoidance for operational satellites.
ERS 2 DEB was launched on 1995-04-21 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. View the full satellite launch log.
Yes — Orbital Radar tracks ERS 2 DEB (NORAD ID 35393) 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. You can also browse the satellite directory to find other tracked objects.
ERS 2 DEB travels at approximately 27,020 km/h (16,789 mph) — roughly 7.51 km/s. It completes 14.56 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.
All tracked debris poses a potential collision risk to operational satellites. At orbital velocities, even a small object carries enormous kinetic energy — a 1 cm fragment at 7.51 km/s has the energy equivalent of a hand grenade. Space agencies perform routine conjunction assessments and may manoeuvre operational satellites to avoid tracked objects like ERS 2 DEB. Read more about debris statistics and the Kessler syndrome.