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
249 km
Apogee
14761 km
Inclination
26.6°
Period
271.3 min
Mean Motion
5.30761162 rev/day
TLE Epoch
2026-05-08 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude7,505 km
Orbital Velocity19,295 km/h
Velocity5.36 km/s
Orbital Period4 hours 31 minutes
Orbits / Day5.31
Eccentricity0.5229
Semi-Major Axis13,876 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 249 km and 14,761 km with an inclination of 26.6°. It travels at approximately 19,295 km/h (5.36 km/s), completing one full orbit every 4 hours 31 minutes — that’s roughly 5.31 orbits per day. Its orbital eccentricity of 0.5229 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 operates in Medium Earth Orbit (MEO), the region between LEO and GEO spanning roughly 2,000 to 35,786 km altitude. MEO is home to navigation constellations (GPS at ~20,200 km, Galileo at ~23,222 km, GLONASS at ~19,130 km) and some communications systems. The higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer satellites are needed for global coverage, but signal latency is higher and radiation exposure — particularly from the Van Allen belts — is a significant design challenge.
❓ Frequently Asked Questions
OV2-3 orbits in Medium Earth Orbit (MEO) at altitudes between 249 km (perigee) and 14,761 km (apogee), with an average altitude of approximately 7,505 km. It completes one orbit every 4 hours 31 minutes, travelling at approximately 19,295 km/h (11,989 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.
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.
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.
OV2-3 travels at approximately 19,295 km/h (11,989 mph) — roughly 5.36 km/s. It completes 5.31 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 11 sunrises and sunsets every 24 hours.