DIAMANT B-P4 DEB
NORAD 7659
Debris
LEO
1975-010E
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LEO · NORAD 7659
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Longitude
🛰️ Orbital Parameters
Perigee
779 km
Apogee
1049 km
Inclination
49.8°
Period
103.3 min
Mean Motion
13.94131059 rev/day
TLE Epoch
2026-09-18 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude914 km
Orbital Velocity26,629 km/h
Velocity7.40 km/s
Orbital Period103 minutes
Orbits / Day13.94
Eccentricity0.0185
Semi-Major Axis7,285 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇫🇷 France
Launch Date
1975-02-06
Launch Site
Guiana Space Centre, French Guiana
Int'l Designator
1975-010E
Object Type
Debris
RCS Size
Medium (0.1–1 m²)
📖 About This Object
DIAMANT B-P4 DEB is a tracked piece of space debris attributed to France, launched on 1975-02-06 from Guiana Space Centre, French Guiana on the Starlette launch. After more than 51 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Low Earth Orbit (LEO) at altitudes between 779 km and 1,049 km with an inclination of 49.8°. It travels at approximately 26,629 km/h (7.40 km/s), completing one full orbit every 103 minutes — that’s roughly 13.94 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. As orbital debris, DIAMANT B-P4 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
DIAMANT B-P4 DEB orbits at an average altitude of 914 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of DIAMANT B-P4 DEB’s average altitude, there are currently 290 active payloads and 1,421 tracked debris or rocket body fragments. With an inclination of 49.8°, DIAMANT B-P4 DEB passes over latitudes between 49.8°N and 49.8°S, covering the tropical and temperate zones where most of the world’s population resides. Low-to-mid inclination orbits are efficient to reach from equatorial and mid-latitude launch sites. France operates approximately 124 active satellites in total, of which 2 share a similar altitude band with DIAMANT B-P4 DEB.
🔗 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
DIAMANT B-P4 DEB orbits in Low Earth Orbit (LEO) at altitudes between 779 km (perigee) and 1,049 km (apogee), with an average altitude of approximately 914 km. It completes one orbit every 103 minutes, travelling at approximately 26,629 km/h (16,547 mph).
DIAMANT B-P4 DEB (NORAD ID 7659) 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.
DIAMANT B-P4 DEB was launched on 1975-02-06 from Guiana Space Centre, French Guiana. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks DIAMANT B-P4 DEB (NORAD ID 7659) 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.
DIAMANT B-P4 DEB travels at approximately 26,629 km/h (16,547 mph) — roughly 7.40 km/s. It completes 13.94 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 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 7.40 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 DIAMANT B-P4 DEB. Read more about debris statistics and the Kessler syndrome.