OPS 5805
NORAD 12093
Payload
MEO
1980-100A
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MEO · NORAD 12093
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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
3170 km
Apogee
37254 km
Inclination
63.9°
Period
719.2 min
Mean Motion
2.00228364 rev/day
TLE Epoch
2026-11-01 18:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude20,212 km
Orbital Velocity13,940 km/h
Velocity3.87 km/s
Orbital Period11 hours 59 minutes
Orbits / Day2.00
Eccentricity0.6411
Semi-Major Axis26,583 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 NRO / SAFSP (United States)
Launch Date
1980-12-13
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1980-100A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
OPS 5805 is an active satellite operated by NRO / SAFSP (United States), launched on 1980-12-13 from Vandenberg Space Force Base, United States on the SDS 4 launch. With over 46 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 3,170 km and 37,254 km with an inclination of 63.9°. It travels at approximately 13,940 km/h (3.87 km/s), completing one full orbit every 11 hours 59 minutes — that’s roughly 2.00 orbits per day. Its orbital eccentricity of 0.6411 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks OPS 5805 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 5805 orbits at an average altitude of 20,212 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 5805’s average altitude, there are currently 96 active payloads and 14 tracked debris or rocket body fragments. With an inclination of 63.9°, OPS 5805 passes over latitudes between 63.9°N and 63.9°S, covering most populated land masses in both hemispheres. This mid-inclination band balances global coverage with efficient launch energy requirements. United States operates approximately 13,342 active satellites in total, of which 44 share a similar altitude band with OPS 5805.
❓ Frequently Asked Questions
OPS 5805 orbits in Medium Earth Orbit (MEO) at altitudes between 3,170 km (perigee) and 37,254 km (apogee), with an average altitude of approximately 20,212 km. It completes one orbit every 11 hours 59 minutes, travelling at approximately 13,940 km/h (8,662 mph).
OPS 5805 is operated by NRO / SAFSP (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 12093. You can track OPS 5805 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
OPS 5805 was launched on 1980-12-13 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 5805 (NORAD ID 12093) 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 5805 travels at approximately 13,940 km/h (8,662 mph) — roughly 3.87 km/s. It completes 2.00 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.