ARIANE 44P+3 R/B
NORAD 23716
Rocket Body
HEO
1995-062B
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HEO · NORAD 23716
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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
758 km
Apogee
73902 km
Inclination
5.7°
Period
1515.7 min
Mean Motion
0.95008248 rev/day
TLE Epoch
2026-06-25 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude37,330 km
Orbital Velocity10,872 km/h
Velocity3.02 km/s
Orbital Period25.3 hours
Orbits / Day0.95
Eccentricity0.8369
Semi-Major Axis43,701 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇫🇷 France
Launch Date
1995-11-17
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1995-062B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
ARIANE 44P+3 R/B is a spent rocket body associated with France, launched on 1995-11-17 from Guiana Space Centre, Kourou on the ISO launch. With over 31 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Highly Elliptical Orbit (HEO) at altitudes between 758 km and 73,902 km with an inclination of 5.7°. It travels at approximately 10,872 km/h (3.02 km/s), completing one full orbit every 25.3 hours — that’s roughly 0.95 orbits per day. Its orbital eccentricity of 0.8369 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Spent rocket bodies like ARIANE 44P+3 R/B are among the largest pieces of uncontrolled space debris and are priority targets for collision avoidance manoeuvres and future active debris removal efforts.
🌍 Orbit Context
ARIANE 44P+3 R/B follows a Highly Elliptical Orbit, sweeping between 758 km (perigee) and 73,902 km (apogee). It spends most of its 25.3 hours orbital period near apogee, effectively loitering over a region of interest before rapidly sweeping through perigee — a profile used for high-latitude communications (Molniya orbits), early-warning systems and magnetospheric science. Within ±50 km of ARIANE 44P+3 R/B’s average altitude, there are currently 4 active payloads and 4 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 5.7°, ARIANE 44P+3 R/B passes over latitudes between 5.7°N and 5.7°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.
🔗 Spent Rocket Body
This is a spent rocket body — the upper stage of a launch vehicle that remains in orbit after delivering its payload. Rocket bodies are a significant contributor to the space debris population. Older stages often retained residual propellant that could later explode, creating debris fields. Modern guidelines require upper stages to either deorbit (controlled re-entry) or passivate (vent residual fuel) to reduce fragmentation risk. The FCC's 5-year deorbit rule and UN debris mitigation guidelines are increasingly enforced to address this growing problem.
❓ Frequently Asked Questions
ARIANE 44P+3 R/B follows a Highly Elliptical Orbit, swinging between 758 km (perigee) and 73,902 km (apogee). It spends most of its 25.3 hours orbital period near apogee, moving slowly at high altitude — effectively loitering over a region of interest before rapidly sweeping through perigee.
ARIANE 44P+3 R/B (NORAD ID 23716) is a spent rocket body — the upper stage of a launch vehicle attributed to France. It no longer serves a functional purpose but continues to orbit Earth as tracked debris. Spent upper stages are among the largest uncontrolled objects in orbit and are closely monitored for collision risk.
ARIANE 44P+3 R/B was launched on 1995-11-17 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: permanent — geostationary orbit, no atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks ARIANE 44P+3 R/B (NORAD ID 23716) 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 44P+3 R/B’s speed varies dramatically throughout its orbit. At perigee it moves at its fastest, and at apogee it slows to a fraction of that — this is Kepler’s second law in action. Its average orbital velocity is approximately 10,872 km/h (3.02 km/s), completing one revolution every 25.3 hours. Learn more about highly elliptical orbits.