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OV2-3

NORAD 13912 Payload MEO 1965-108V ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
267 km
Apogee
14635 km
Inclination
26.6°
Period
269.7 min
Mean Motion
5.33896841 rev/day
TLE Epoch
2026-09-17 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude7,451 km
Orbital Velocity19,332 km/h
Velocity5.37 km/s
Orbital Period4 hours 30 minutes
Orbits / Day5.34
Eccentricity0.5198
Semi-Major Axis13,822 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 USAF SSD (United States)
Launch Date
1965-12-21
Launch Site
Cape Canaveral Space Force Station, United States
Int'l Designator
1965-108V
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
OV2-3 is an active satellite operated by USAF SSD (United States), launched on 1965-12-21 from Cape Canaveral Space Force Station, United States on the LES 4 launch. After more than 61 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 267 km and 14,635 km with an inclination of 26.6°. It travels at approximately 19,332 km/h (5.37 km/s), completing one full orbit every 4 hours 30 minutes — that’s roughly 5.34 orbits per day. Its orbital eccentricity of 0.5198 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks OV2-3 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
OV2-3 orbits at an average altitude of 7,451 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 OV2-3’s average altitude, there are currently 3 active payloads and 14 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 26.6°, OV2-3 passes over latitudes between 26.6°N and 26.6°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. United States operates approximately 13,204 active satellites in total.
❓ Frequently Asked Questions
OV2-3 orbits in Medium Earth Orbit (MEO) at altitudes between 267 km (perigee) and 14,635 km (apogee), with an average altitude of approximately 7,451 km. It completes one orbit every 4 hours 30 minutes, travelling at approximately 19,332 km/h (12,013 mph).
OV2-3 is operated by USAF SSD (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 13912. You can track OV2-3 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
OV2-3 was launched on 1965-12-21 from Cape Canaveral Space Force Station, United States, one of the busiest launch facilities in the world, operated by NASA and the U.S. Space Force on Florida’s Atlantic coast. 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 OV2-3 (NORAD ID 13912) 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.
OV2-3 travels at approximately 19,332 km/h (12,013 mph) — roughly 5.37 km/s. It completes 5.34 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 11 sunrises and sunsets every 24 hours.