OPS 1527 (OV3-1)
NORAD 2150
Payload
MEO
1966-034A
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
329 km
Apogee
2474 km
Inclination
82.4°
Period
113.8 min
Mean Motion
12.65173197 rev/day
TLE Epoch
2026-10-21 13:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,402 km
Orbital Velocity25,780 km/h
Velocity7.16 km/s
Orbital Period114 minutes
Orbits / Day12.65
Eccentricity0.1380
Semi-Major Axis7,773 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇺🇸 USAF OAR (United States)
Launch Date
1966-04-22
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1966-034A
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
OPS 1527 (OV3-1) is an active satellite operated by USAF OAR (United States), launched on 1966-04-22 from Vandenberg Space Force Base, United States on the OV3-1 launch. After more than 60 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 329 km and 2,474 km with an inclination of 82.4°. It travels at approximately 25,780 km/h (7.16 km/s), completing one full orbit every 114 minutes — that’s roughly 12.65 orbits per day. Its orbital eccentricity of 0.1380 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 OPS 1527 (OV3-1) in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
OPS 1527 (OV3-1) orbits at an average altitude of 1,402 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 OPS 1527 (OV3-1)’s average altitude, there are currently 337 active payloads and 275 tracked debris or rocket body fragments. With an inclination of 82.4°, OPS 1527 (OV3-1) passes over latitudes between 82.4°N and 82.4°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 13,276 active satellites in total, of which 20 share a similar altitude band with OPS 1527 (OV3-1).
❓ Frequently Asked Questions
OPS 1527 (OV3-1) orbits in Medium Earth Orbit (MEO) at altitudes between 329 km (perigee) and 2,474 km (apogee), with an average altitude of approximately 1,402 km. It completes one orbit every 114 minutes, travelling at approximately 25,780 km/h (16,019 mph).
OPS 1527 (OV3-1) is operated by USAF OAR (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 2150. You can track OPS 1527 (OV3-1) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
OPS 1527 (OV3-1) was launched on 1966-04-22 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 OPS 1527 (OV3-1) (NORAD ID 2150) 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.
OPS 1527 (OV3-1) travels at approximately 25,780 km/h (16,019 mph) — roughly 7.16 km/s. It completes 12.65 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 25 sunrises and sunsets every 24 hours.