DIAMANT B-P4 R/B
NORAD 7647
Rocket Body
LEO
1975-010B
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LEO · NORAD 7647
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🛰️ Orbital Parameters
Perigee
796 km
Apogee
1115 km
Inclination
49.8°
Period
104.2 min
Mean Motion
13.82361540 rev/day
TLE Epoch
2026-09-16 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude956 km
Orbital Velocity26,554 km/h
Velocity7.38 km/s
Orbital Period104 minutes
Orbits / Day13.82
Eccentricity0.0218
Semi-Major Axis7,327 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
1975-010B
Object Type
Rocket Body
RCS Size
Large (>1 m²)
📖 About This Object
DIAMANT B-P4 R/B is a spent rocket body associated with 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 796 km and 1,115 km with an inclination of 49.8°. It travels at approximately 26,554 km/h (7.38 km/s), completing one full orbit every 104 minutes — that’s roughly 13.82 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. Spent rocket bodies like DIAMANT B-P4 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
DIAMANT B-P4 R/B orbits at an average altitude of 956 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 R/B’s average altitude, there are currently 393 active payloads and 1,281 tracked debris or rocket body fragments. With an inclination of 49.8°, DIAMANT B-P4 R/B 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.
🔗 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
DIAMANT B-P4 R/B orbits in Low Earth Orbit (LEO) at altitudes between 796 km (perigee) and 1,115 km (apogee), with an average altitude of approximately 956 km. It completes one orbit every 104 minutes, travelling at approximately 26,554 km/h (16,500 mph).
DIAMANT B-P4 R/B (NORAD ID 7647) 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.
DIAMANT B-P4 R/B 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 R/B (NORAD ID 7647) 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 R/B travels at approximately 26,554 km/h (16,500 mph) — roughly 7.38 km/s. It completes 13.82 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.