ARIANE 44LP DEB (SPELDA)
NORAD 26471
Debris
MEO
2000-046C
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MEO · NORAD 26471
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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
556 km
Apogee
17532 km
Inclination
3.5°
Period
317.7 min
Mean Motion
4.53312444 rev/day
TLE Epoch
2026-06-20 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude9,044 km
Orbital Velocity18,306 km/h
Velocity5.09 km/s
Orbital Period5 hours 18 minutes
Orbits / Day4.53
Eccentricity0.5506
Semi-Major Axis15,415 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇫🇷 France
Launch Date
2000-08-17
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
2000-046C
Object Type
Debris
RCS Size
Large (>1 m²)
📖 About This Object
ARIANE 44LP DEB (SPELDA) is a tracked piece of space debris attributed to France, launched on 2000-08-17 from Guiana Space Centre, Kourou on the Brasilsat B4 launch. With over 26 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 556 km and 17,532 km with an inclination of 3.5°. It travels at approximately 18,306 km/h (5.09 km/s), completing one full orbit every 5 hours 18 minutes — that’s roughly 4.53 orbits per day. Its orbital eccentricity of 0.5506 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. As orbital debris, ARIANE 44LP 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 44LP DEB (SPELDA) orbits at an average altitude of 9,044 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 44LP DEB (SPELDA)’s average altitude, there are currently 2 active payloads and 8 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 3.5°, ARIANE 44LP DEB (SPELDA) passes over latitudes between 3.5°N and 3.5°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 44LP DEB (SPELDA) orbits in Medium Earth Orbit (MEO) at altitudes between 556 km (perigee) and 17,532 km (apogee), with an average altitude of approximately 9,044 km. It completes one orbit every 5 hours 18 minutes, travelling at approximately 18,306 km/h (11,375 mph).
ARIANE 44LP DEB (SPELDA) (NORAD ID 26471) 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 44LP DEB (SPELDA) was launched on 2000-08-17 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: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks ARIANE 44LP DEB (SPELDA) (NORAD ID 26471) 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 44LP DEB (SPELDA) travels at approximately 18,306 km/h (11,375 mph) — roughly 5.09 km/s. It completes 4.53 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 9 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 5.09 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 44LP DEB (SPELDA). Read more about debris statistics and the Kessler syndrome.