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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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
442 km
Apogee
1434 km
Inclination
63.3°
Period
103.8 min
Mean Motion
13.87324836 rev/day
TLE Epoch
2026-06-18 13:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude938 km
Orbital Velocity26,585 km/h
Velocity7.38 km/s
Orbital Period104 minutes
Orbits / Day13.87
Eccentricity0.0679
Semi-Major Axis7,309 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 442 km and 1,434 km with an inclination of 63.3°. It travels at approximately 26,585 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 at an average altitude of 938 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of OPS 0252’s average altitude, there are currently 306 active payloads and 1,123 tracked debris or rocket body fragments. With an inclination of 63.3°, OPS 0252 passes over latitudes between 63.3°N and 63.3°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 12,339 active satellites in total, of which 89 share a similar altitude band with OPS 0252.
❓ Frequently Asked Questions
OPS 0252 orbits in Low Earth Orbit (LEO) at altitudes between 442 km (perigee) and 1,434 km (apogee), with an average altitude of approximately 938 km. It completes one orbit every 104 minutes, travelling at approximately 26,585 km/h (16,519 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 or browse all operators in the operator directory.
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. View the full satellite launch log.
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. You can also browse the satellite directory to find other tracked objects.
OPS 0252 travels at approximately 26,585 km/h (16,519 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.