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OPS 5805

NORAD 12093 Payload MEO 1980-100A ● Active
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Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
3047 km
Apogee
37321 km
Inclination
63.9°
Period
718.0 min
Mean Motion
2.00543462 rev/day
TLE Epoch
2026-03-14 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude20,184 km
Orbital Velocity13,948 km/h
Velocity3.87 km/s
Orbital Period11 hours 58 minutes
Orbits / Day2.01
Eccentricity0.6453
Semi-Major Axis26,555 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)
🔗 Constellation / Groups
geo protected plus
📖 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 3,047 km and 37,321 km with an inclination of 63.9°. It travels at approximately 13,948 km/h (3.87 km/s), completing one full orbit every 11 hours 58 minutes — that’s roughly 2.01 orbits per day. Its orbital eccentricity of 0.6453 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. It is part of the Geo Protected Plus constellation group. 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 operates in Medium Earth Orbit (MEO), the region between LEO and GEO spanning roughly 2,000 to 35,786 km altitude. MEO is home to navigation constellations (GPS at ~20,200 km, Galileo at ~23,222 km, GLONASS at ~19,130 km) and some communications systems. The higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer satellites are needed for global coverage, but signal latency is higher and radiation exposure — particularly from the Van Allen belts — is a significant design challenge.
❓ Frequently Asked Questions
OPS 5805 orbits in Medium Earth Orbit (MEO) at altitudes between 3,047 km (perigee) and 37,321 km (apogee), with an average altitude of approximately 20,184 km. It completes one orbit every 11 hours 58 minutes, travelling at approximately 13,948 km/h (8,667 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.
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.
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.
OPS 5805 travels at approximately 13,948 km/h (8,667 mph) — roughly 3.87 km/s. It completes 2.01 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.
OPS 5805 is a member of the Geo Protected Plus constellation. Satellites in this group work together to provide coordinated coverage, typically in similar orbital planes at comparable altitudes. You can view all Geo Protected Plus satellites on Orbital Radar’s live tracker.