ARIANE 1 DEB
NORAD 28556
Debris
HEO
1979-104V
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HEO · NORAD 28556
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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
875 km
Apogee
40369 km
Inclination
15.5°
Period
735.9 min
Mean Motion
1.95682123 rev/day
TLE Epoch
2026-06-20 10:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude20,622 km
Orbital Velocity13,834 km/h
Velocity3.84 km/s
Orbital Period12 hours 16 minutes
Orbits / Day1.96
Eccentricity0.7316
Semi-Major Axis26,993 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇫🇷 France
Launch Date
1979-12-24
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
1979-104V
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
ARIANE 1 DEB is a tracked piece of space debris attributed to France, launched on 1979-12-24 from Guiana Space Centre, Kourou on the CAT launch. With over 47 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Highly Elliptical Orbit (HEO) at altitudes between 875 km and 40,369 km with an inclination of 15.5°. It travels at approximately 13,834 km/h (3.84 km/s), completing one full orbit every 12 hours 16 minutes — that’s roughly 1.96 orbits per day. Its orbital eccentricity of 0.7316 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. As orbital debris, ARIANE 1 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
ARIANE 1 DEB follows a Highly Elliptical Orbit, sweeping between 875 km (perigee) and 40,369 km (apogee). It spends most of its 12 hours 16 minutes 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 1 DEB’s average altitude, there are currently 0 active payloads and 6 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 15.5°, ARIANE 1 DEB passes over latitudes between 15.5°N and 15.5°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 1 DEB follows a Highly Elliptical Orbit, swinging between 875 km (perigee) and 40,369 km (apogee). It spends most of its 12 hours 16 minutes orbital period near apogee, moving slowly at high altitude — effectively loitering over a region of interest before rapidly sweeping through perigee.
ARIANE 1 DEB (NORAD ID 28556) 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 1 DEB was launched on 1979-12-24 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 1 DEB (NORAD ID 28556) 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 1 DEB’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 13,834 km/h (3.84 km/s), completing one revolution every 12 hours 16 minutes. Learn more about highly elliptical orbits.
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 3.84 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 1 DEB. Read more about debris statistics and the Kessler syndrome.