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OPS 1427 (OV3-4)

NORAD 2201 Payload MEO 1966-052A ● Active
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🛰️ Orbital Parameters
Perigee
642 km
Apogee
4681 km
Inclination
40.9°
Period
142.6 min
Mean Motion
10.10119568 rev/day
TLE Epoch
2026-10-21 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude2,662 km
Orbital Velocity23,915 km/h
Velocity6.64 km/s
Orbital Period2 hours 23 minutes
Orbits / Day10.10
Eccentricity0.2236
Semi-Major Axis9,033 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 USAF OAR (United States)
Launch Date
1966-06-10
Launch Site
Wallops Flight Facility / MARS, United States
Int'l Designator
1966-052A
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
OPS 1427 (OV3-4) is an active satellite operated by USAF OAR (United States), launched on 1966-06-10 from Wallops Flight Facility / MARS, United States on the OV3-4 PHASR 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 642 km and 4,681 km with an inclination of 40.9°. It travels at approximately 23,915 km/h (6.64 km/s), completing one full orbit every 2 hours 23 minutes — that’s roughly 10.10 orbits per day. Its orbital eccentricity of 0.2236 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks OPS 1427 (OV3-4) in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
OPS 1427 (OV3-4) orbits at an average altitude of 2,662 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 1427 (OV3-4)’s average altitude, there are currently 1 active payload and 5 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 40.9°, OPS 1427 (OV3-4) passes over latitudes between 40.9°N and 40.9°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 13,279 active satellites in total.
❓ Frequently Asked Questions
OPS 1427 (OV3-4) orbits in Medium Earth Orbit (MEO) at altitudes between 642 km (perigee) and 4,681 km (apogee), with an average altitude of approximately 2,662 km. It completes one orbit every 2 hours 23 minutes, travelling at approximately 23,915 km/h (14,860 mph).
OPS 1427 (OV3-4) is operated by USAF OAR (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 2201. You can track OPS 1427 (OV3-4) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
OPS 1427 (OV3-4) was launched on 1966-06-10 from Wallops Flight Facility / MARS, United States. 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 OPS 1427 (OV3-4) (NORAD ID 2201) 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 1427 (OV3-4) travels at approximately 23,915 km/h (14,860 mph) — roughly 6.64 km/s. It completes 10.10 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 20 sunrises and sunsets every 24 hours.