DIAPASON (D1-A)
NORAD 2016
Payload
MEO
1966-013A
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MEO · NORAD 2016
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
497 km
Apogee
2293 km
Inclination
34.1°
Period
113.7 min
Mean Motion
12.66803321 rev/day
TLE Epoch
2026-10-21 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,395 km
Orbital Velocity25,791 km/h
Velocity7.16 km/s
Orbital Period114 minutes
Orbits / Day12.67
Eccentricity0.1156
Semi-Major Axis7,766 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇫🇷 CNES (France)
Launch Date
1966-02-17
Launch Site
Hammaguir, Algeria
Int'l Designator
1966-013A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
DIAPASON (D1-A) is an active satellite operated by CNES (France), launched on 1966-02-17 from Hammaguir, Algeria on the Diapason D-1A launch. After more than 60 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Medium Earth Orbit (MEO) at altitudes between 497 km and 2,293 km with an inclination of 34.1°. It travels at approximately 25,791 km/h (7.16 km/s), completing one full orbit every 114 minutes — that’s roughly 12.67 orbits per day. Its orbital eccentricity of 0.1156 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. Orbital Radar tracks DIAPASON (D1-A) in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
DIAPASON (D1-A) orbits at an average altitude of 1,395 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 DIAPASON (D1-A)’s average altitude, there are currently 295 active payloads and 265 tracked debris or rocket body fragments. With an inclination of 34.1°, DIAPASON (D1-A) passes over latitudes between 34.1°N and 34.1°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.
❓ Frequently Asked Questions
DIAPASON (D1-A) orbits in Medium Earth Orbit (MEO) at altitudes between 497 km (perigee) and 2,293 km (apogee), with an average altitude of approximately 1,395 km. It completes one orbit every 114 minutes, travelling at approximately 25,791 km/h (16,026 mph).
DIAPASON (D1-A) is operated by CNES (France). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 2016. You can track DIAPASON (D1-A) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
DIAPASON (D1-A) was launched on 1966-02-17 from Hammaguir, Algeria. At its current altitude, the estimated remaining orbital lifetime is: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks DIAPASON (D1-A) (NORAD ID 2016) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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.
DIAPASON (D1-A) travels at approximately 25,791 km/h (16,026 mph) — roughly 7.16 km/s. It completes 12.67 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 25 sunrises and sunsets every 24 hours.