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Home Library Satellite Directory ARIANE 44L DEB (SPELDA)

ARIANE 44L DEB (SPELDA)

NORAD 21818 Debris MEO 1991-084D
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
286 km
Apogee
19320 km
Inclination
3.8°
Period
341.4 min
Mean Motion
4.21772332 rev/day
TLE Epoch
2026-06-19 19:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude9,803 km
Orbital Velocity17,872 km/h
Velocity4.96 km/s
Orbital Period5 hours 41 minutes
Orbits / Day4.22
Eccentricity0.5884
Semi-Major Axis16,174 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇫🇷 France
Launch Date
1991-12-16
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1991-084D
Object Type
Debris
RCS Size
Large (>1 m²)
📖 About This Object
ARIANE 44L DEB (SPELDA) is a tracked piece of space debris attributed to France, launched on 1991-12-16 from Guiana Space Centre, Kourou on the Telecom 2A launch. With over 35 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 286 km and 19,320 km with an inclination of 3.8°. It travels at approximately 17,872 km/h (4.96 km/s), completing one full orbit every 5 hours 41 minutes — that’s roughly 4.22 orbits per day. Its orbital eccentricity of 0.5884 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. As orbital debris, ARIANE 44L DEB (SPELDA) 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
ARIANE 44L DEB (SPELDA) orbits at an average altitude of 9,803 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of ARIANE 44L DEB (SPELDA)’s average altitude, there are currently 0 active payloads and 15 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 3.8°, ARIANE 44L DEB (SPELDA) passes over latitudes between 3.8°N and 3.8°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. France operates approximately 115 active satellites in total.
🔗 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
ARIANE 44L DEB (SPELDA) orbits in Medium Earth Orbit (MEO) at altitudes between 286 km (perigee) and 19,320 km (apogee), with an average altitude of approximately 9,803 km. It completes one orbit every 5 hours 41 minutes, travelling at approximately 17,872 km/h (11,105 mph).
ARIANE 44L DEB (SPELDA) (NORAD ID 21818) is a piece of tracked orbital debris attributed to France. 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.
ARIANE 44L DEB (SPELDA) was launched on 1991-12-16 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: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks ARIANE 44L DEB (SPELDA) (NORAD ID 21818) 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.
ARIANE 44L DEB (SPELDA) travels at approximately 17,872 km/h (11,105 mph) — roughly 4.96 km/s. It completes 4.22 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 8 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 4.96 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 ARIANE 44L DEB (SPELDA). Read more about debris statistics and the Kessler syndrome.