OPS 5805
NORAD 12093
Payload
MEO
1980-100A
● Active
CONNECTING…
MEO · NORAD 12093
NOW PASSING OVER
Calculating position…
—
Altitude (km)
—
Speed (km/s)
—
Latitude
—
Longitude
🛰️ Orbital Parameters
Perigee
3110 km
Apogee
37277 km
Inclination
63.9°
Period
718.4 min
Mean Motion
2.00436833 rev/day
TLE Epoch
2026-06-17 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude20,194 km
Orbital Velocity13,945 km/h
Velocity3.87 km/s
Orbital Period11 hours 58 minutes
Orbits / Day2.00
Eccentricity0.6431
Semi-Major Axis26,565 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1980-12-13
Launch Site
Vandenberg SFB, California
Int'l Designator
1980-100A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
OPS 5805 is an active satellite operated by United States, launched on 1980-12-13 from Vandenberg SFB, California. With over 46 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Medium Earth Orbit (MEO) at altitudes between 3,110 km and 37,277 km with an inclination of 63.9°. It travels at approximately 13,945 km/h (3.87 km/s), completing one full orbit every 11 hours 58 minutes — that’s roughly 2.00 orbits per day. Its orbital eccentricity of 0.6431 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 20,194 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 103 active payloads and 14 tracked debris or rocket body fragments — notable neighbours include GPS BIIR-5 (PRN 22), GPS BIIR-8 (PRN 16), GPS BIIR-11 (PRN 19). 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 12,360 active satellites in total, of which 43 share a similar altitude band with OPS 5805.
❓ Frequently Asked Questions
OPS 5805 orbits in Medium Earth Orbit (MEO) at altitudes between 3,110 km (perigee) and 37,277 km (apogee), with an average altitude of approximately 20,194 km. It completes one orbit every 11 hours 58 minutes, travelling at approximately 13,945 km/h (8,665 mph).
OPS 5805 is operated by 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 SFB, California, 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) data from Space-Track and CelesTrak. 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 13,945 km/h (8,665 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.