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OV3-3

NORAD 2389 Payload LEO 1966-070A ● Active
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🛰️ Orbital Parameters
Perigee
334 km
Apogee
1827 km
Inclination
81.3°
Period
106.8 min
Mean Motion
13.47811273 rev/day
TLE Epoch
2026-10-21 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,081 km
Orbital Velocity26,330 km/h
Velocity7.31 km/s
Orbital Period107 minutes
Orbits / Day13.48
Eccentricity0.1002
Semi-Major Axis7,452 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇺🇸 USAF OAR (United States)
Launch Date
1966-08-04
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1966-070A
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
OV3-3 is an active satellite operated by USAF OAR (United States), launched on 1966-08-04 from Vandenberg Space Force Base, United States on the OV3-3 launch. After more than 60 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 334 km and 1,827 km with an inclination of 81.3°. It travels at approximately 26,330 km/h (7.31 km/s), completing one full orbit every 107 minutes — that’s roughly 13.48 orbits per day. Its orbital eccentricity of 0.1002 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 ~500–1,000 years. Orbital Radar tracks OV3-3 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
OV3-3 orbits at an average altitude of 1,081 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 OV3-3’s average altitude, there are currently 308 active payloads and 543 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0041. With an inclination of 81.3°, OV3-3 passes over latitudes between 81.3°N and 81.3°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. United States operates approximately 13,279 active satellites in total, of which 42 share a similar altitude band with OV3-3.
❓ Frequently Asked Questions
OV3-3 orbits in Low Earth Orbit (LEO) at altitudes between 334 km (perigee) and 1,827 km (apogee), with an average altitude of approximately 1,081 km. It completes one orbit every 107 minutes, travelling at approximately 26,330 km/h (16,361 mph).
OV3-3 is operated by USAF OAR (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 2389. You can track OV3-3 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
OV3-3 was launched on 1966-08-04 from Vandenberg Space Force Base, United States, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. At its current altitude, the estimated remaining orbital lifetime is: ~500–1,000 years. View the full satellite launch log.
Yes — Orbital Radar tracks OV3-3 (NORAD ID 2389) 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.
OV3-3 travels at approximately 26,330 km/h (16,361 mph) — roughly 7.31 km/s. It completes 13.48 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 sunrises and sunsets every 24 hours.