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OPS 1920

NORAD 2481 Payload MEO 1966-089A ● Active
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🛰️ Orbital Parameters
Perigee
3658 km
Apogee
3724 km
Inclination
89.9°
Period
167.6 min
Mean Motion
8.59257197 rev/day
TLE Epoch
2026-10-21 07:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude3,691 km
Orbital Velocity22,658 km/h
Velocity6.29 km/s
Orbital Period2 hours 48 minutes
Orbits / Day8.59
Eccentricity0.0033
Semi-Major Axis10,062 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 USAF SSD (United States)
Launch Date
1966-10-05
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1966-089A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
OPS 1920 is an active satellite operated by USAF SSD (United States), launched on 1966-10-05 from Vandenberg Space Force Base, United States on the Midas RTS-I F3 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 3,658 km and 3,724 km with an inclination of 89.9°. It travels at approximately 22,658 km/h (6.29 km/s), completing one full orbit every 2 hours 48 minutes — that’s roughly 8.59 orbits per day. Orbital Radar tracks OPS 1920 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 1920 orbits at an average altitude of 3,691 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 1920’s average altitude, there are currently 9 active payloads and 7 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 89.9°, OPS 1920 passes over latitudes between 89.9°N and 89.9°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 9 share a similar altitude band with OPS 1920.
❓ Frequently Asked Questions
OPS 1920 orbits in Medium Earth Orbit (MEO) at altitudes between 3,658 km (perigee) and 3,724 km (apogee), with an average altitude of approximately 3,691 km. It completes one orbit every 2 hours 48 minutes, travelling at approximately 22,658 km/h (14,079 mph).
OPS 1920 is operated by USAF SSD (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 2481. You can track OPS 1920 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
OPS 1920 was launched on 1966-10-05 from Vandenberg Space Force Base, United States, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. View the full satellite launch log.
Yes — Orbital Radar tracks OPS 1920 (NORAD ID 2481) 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 1920 travels at approximately 22,658 km/h (14,079 mph) — roughly 6.29 km/s. It completes 8.59 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 17 sunrises and sunsets every 24 hours.