OPS 0252
NORAD 13791
Payload
LEO
1983-008A
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LEO · NORAD 13791
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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
440 km
Apogee
1439 km
Inclination
63.3°
Period
103.8 min
Mean Motion
13.86987602 rev/day
TLE Epoch
2026-05-08 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude940 km
Orbital Velocity26,583 km/h
Velocity7.38 km/s
Orbital Period104 minutes
Orbits / Day13.87
Eccentricity0.0683
Semi-Major Axis7,311 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1983-02-09
Launch Site
Vandenberg SFB, California
Int'l Designator
1983-008A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
OPS 0252 is an active satellite operated by United States, launched on 1983-02-09 from Vandenberg SFB, California. With over 43 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 440 km and 1,439 km with an inclination of 63.3°. It travels at approximately 26,583 km/h (7.38 km/s), completing one full orbit every 104 minutes — that’s roughly 13.87 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. Orbital Radar tracks OPS 0252 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 0252 orbits in the most densely populated region of Low Earth Orbit, between roughly 300 and 600 km altitude. This band is home to the International Space Station, most Earth observation satellites, and the bulk of the Starlink constellation. Objects here experience measurable atmospheric drag, which gradually lowers their orbit over months to years and eventually causes re-entry. The relatively short signal path makes this altitude ideal for low-latency communications and high-resolution imaging.
❓ Frequently Asked Questions
OPS 0252 orbits in Low Earth Orbit (LEO) at altitudes between 440 km (perigee) and 1,439 km (apogee), with an average altitude of approximately 940 km. It completes one orbit every 104 minutes, travelling at approximately 26,583 km/h (16,518 mph).
OPS 0252 is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 13791. You can track OPS 0252 in real time on Orbital Radar’s live tracker.
OPS 0252 was launched on 1983-02-09 from Vandenberg SFB, California, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years.
Yes — Orbital Radar tracks OPS 0252 (NORAD ID 13791) 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 0252 travels at approximately 26,583 km/h (16,518 mph) — roughly 7.38 km/s. It completes 13.87 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.