OV1-2
NORAD 1613
Payload
MEO
1965-078A
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MEO · NORAD 1613
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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
396 km
Apogee
2110 km
Inclination
144.2°
Period
110.6 min
Mean Motion
13.02344286 rev/day
TLE Epoch
2026-10-21 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,253 km
Orbital Velocity26,030 km/h
Velocity7.23 km/s
Orbital Period111 minutes
Orbits / Day13.02
Eccentricity0.1124
Semi-Major Axis7,624 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇺🇸 USAF OAR (United States)
Launch Date
1965-10-05
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1965-078A
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
OV1-2 is an active satellite operated by USAF OAR (United States), launched on 1965-10-05 from Vandenberg Space Force Base, United States on the OV1-2S 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 396 km and 2,110 km with an inclination of 144.2°. It travels at approximately 26,030 km/h (7.23 km/s), completing one full orbit every 111 minutes — that’s roughly 13.02 orbits per day. Its orbital eccentricity of 0.1124 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 OV1-2 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
OV1-2 orbits at an average altitude of 1,253 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 OV1-2’s average altitude, there are currently 290 active payloads and 398 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0013, ONEWEB-0017, ONEWEB-0020. With an inclination of 144.2°, OV1-2 passes over latitudes between 144.2°N and 144.2°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 6 share a similar altitude band with OV1-2.
❓ Frequently Asked Questions
OV1-2 orbits in Medium Earth Orbit (MEO) at altitudes between 396 km (perigee) and 2,110 km (apogee), with an average altitude of approximately 1,253 km. It completes one orbit every 111 minutes, travelling at approximately 26,030 km/h (16,175 mph).
OV1-2 is operated by USAF OAR (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 1613. You can track OV1-2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
OV1-2 was launched on 1965-10-05 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: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks OV1-2 (NORAD ID 1613) 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.
OV1-2 travels at approximately 26,030 km/h (16,175 mph) — roughly 7.23 km/s. It completes 13.02 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 26 sunrises and sunsets every 24 hours.