ARIANE 44L+ DEB (SPELDA)
NORAD 21942
Debris
MEO
1992-021D
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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
263 km
Apogee
19409 km
Inclination
4.4°
Period
342.4 min
Mean Motion
4.20497266 rev/day
TLE Epoch
2026-06-19 21:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude9,836 km
Orbital Velocity17,853 km/h
Velocity4.96 km/s
Orbital Period5 hours 42 minutes
Orbits / Day4.20
Eccentricity0.5907
Semi-Major Axis16,207 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇫🇷 France
Launch Date
1992-04-15
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1992-021D
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 1992-04-15 from Guiana Space Centre, Kourou on the Telecom 2B launch. With over 34 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 263 km and 19,409 km with an inclination of 4.4°. It travels at approximately 17,853 km/h (4.96 km/s), completing one full orbit every 5 hours 42 minutes — that’s roughly 4.20 orbits per day. Its orbital eccentricity of 0.5907 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 9,836 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 11 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 4.4°, ARIANE 44L+ DEB (SPELDA) passes over latitudes between 4.4°N and 4.4°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 263 km (perigee) and 19,409 km (apogee), with an average altitude of approximately 9,836 km. It completes one orbit every 5 hours 42 minutes, travelling at approximately 17,853 km/h (11,094 mph).
ARIANE 44L+ DEB (SPELDA) (NORAD ID 21942) 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 1992-04-15 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 21942) 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 17,853 km/h (11,094 mph) — roughly 4.96 km/s. It completes 4.20 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.