OV2-3
NORAD 13912
Payload
MEO
1965-108V
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MEO · NORAD 13912
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
253 km
Apogee
14712 km
Inclination
26.6°
Period
270.7 min
Mean Motion
5.32055885 rev/day
TLE Epoch
2026-06-18 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude7,483 km
Orbital Velocity19,310 km/h
Velocity5.36 km/s
Orbital Period4 hours 31 minutes
Orbits / Day5.32
Eccentricity0.5219
Semi-Major Axis13,854 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1965-12-21
Launch Site
Cape Canaveral, Florida
Int'l Designator
1965-108V
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
OV2-3 is an active satellite operated by United States, launched on 1965-12-21 from Cape Canaveral, Florida. 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 253 km and 14,712 km with an inclination of 26.6°. It travels at approximately 19,310 km/h (5.36 km/s), completing one full orbit every 4 hours 31 minutes — that’s roughly 5.32 orbits per day. Its orbital eccentricity of 0.5219 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 7,483 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 13 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 12,339 active satellites in total.
❓ Frequently Asked Questions
OV2-3 orbits in Medium Earth Orbit (MEO) at altitudes between 253 km (perigee) and 14,712 km (apogee), with an average altitude of approximately 7,483 km. It completes one orbit every 4 hours 31 minutes, travelling at approximately 19,310 km/h (11,999 mph).
OV2-3 is operated by 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, Florida, 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 19,310 km/h (11,999 mph) — roughly 5.36 km/s. It completes 5.32 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 11 sunrises and sunsets every 24 hours.