OPS 0252
NORAD 13791
Payload
LEO
1983-008A
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LEO · NORAD 13791
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Longitude
🛰️ Orbital Parameters
Perigee
447 km
Apogee
1426 km
Inclination
63.3°
Period
103.8 min
Mean Motion
13.87768618 rev/day
TLE Epoch
2026-09-16 19:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude937 km
Orbital Velocity26,588 km/h
Velocity7.39 km/s
Orbital Period104 minutes
Orbits / Day13.88
Eccentricity0.0670
Semi-Major Axis7,308 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇺🇸 NRO / NRL (United States)
Launch Date
1983-02-09
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1983-008A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
OPS 0252 is an active satellite operated by NRO / NRL (United States), launched on 1983-02-09 from Vandenberg Space Force Base, United States on the PARCAE 5 launch. With over 43 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 447 km and 1,426 km with an inclination of 63.3°. It travels at approximately 26,588 km/h (7.39 km/s), completing one full orbit every 104 minutes — that’s roughly 13.88 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 937 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 398 active payloads and 1,344 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 13,204 active satellites in total, of which 152 share a similar altitude band with OPS 0252.
❓ Frequently Asked Questions
OPS 0252 orbits in Low Earth Orbit (LEO) at altitudes between 447 km (perigee) and 1,426 km (apogee), with an average altitude of approximately 937 km. It completes one orbit every 104 minutes, travelling at approximately 26,588 km/h (16,521 mph).
OPS 0252 is operated by NRO / NRL (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 Space Force Base, United States, 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 26,588 km/h (16,521 mph) — roughly 7.39 km/s. It completes 13.88 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.