OV1-4
NORAD 2121
Payload
LEO
1966-025A
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LEO · NORAD 2121
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Altitude (km)
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Longitude
🛰️ Orbital Parameters
Perigee
877 km
Apogee
999 km
Inclination
144.5°
Period
103.8 min
Mean Motion
13.87339117 rev/day
TLE Epoch
2026-10-21 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude938 km
Orbital Velocity26,585 km/h
Velocity7.38 km/s
Orbital Period104 minutes
Orbits / Day13.87
Eccentricity0.0083
Semi-Major Axis7,309 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇺🇸 USAF OAR (United States)
Launch Date
1966-03-30
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1966-025A
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
OV1-4 is an active satellite operated by USAF OAR (United States), launched on 1966-03-30 from Vandenberg Space Force Base, United States on the OV1-4S 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 877 km and 999 km with an inclination of 144.5°. It travels at approximately 26,585 km/h (7.38 km/s), completing one full orbit every 104 minutes — that’s roughly 13.87 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. Orbital Radar tracks OV1-4 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
OV1-4 orbits at an average altitude of 938 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 OV1-4’s average altitude, there are currently 444 active payloads and 1,371 tracked debris or rocket body fragments. With an inclination of 144.5°, OV1-4 passes over latitudes between 144.5°N and 144.5°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 173 share a similar altitude band with OV1-4.
❓ Frequently Asked Questions
OV1-4 orbits in Low Earth Orbit (LEO) at altitudes between 877 km (perigee) and 999 km (apogee), with an average altitude of approximately 938 km. It completes one orbit every 104 minutes, travelling at approximately 26,585 km/h (16,519 mph).
OV1-4 is operated by USAF OAR (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 2121. You can track OV1-4 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
OV1-4 was launched on 1966-03-30 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: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks OV1-4 (NORAD ID 2121) 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.
OV1-4 travels at approximately 26,585 km/h (16,519 mph) — roughly 7.38 km/s. It completes 13.87 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.