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OPS 8781

NORAD 10502 Payload LEO 1977-112A ● Active
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Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
526 km
Apogee
1210 km
Inclination
63.3°
Period
102.3 min
Mean Motion
14.07354102 rev/day
TLE Epoch
2026-05-08 13:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude868 km
Orbital Velocity26,714 km/h
Velocity7.42 km/s
Orbital Period102 minutes
Orbits / Day14.07
Eccentricity0.0472
Semi-Major Axis7,239 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1977-12-08
Launch Site
Vandenberg SFB, California
Int'l Designator
1977-112A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
OPS 8781 is an active satellite operated by United States, launched on 1977-12-08 from Vandenberg SFB, California. With over 49 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 526 km and 1,210 km with an inclination of 63.3°. It travels at approximately 26,714 km/h (7.42 km/s), completing one full orbit every 102 minutes — that’s roughly 14.07 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. Orbital Radar tracks OPS 8781 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 8781 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 8781 orbits in Low Earth Orbit (LEO) at altitudes between 526 km (perigee) and 1,210 km (apogee), with an average altitude of approximately 868 km. It completes one orbit every 102 minutes, travelling at approximately 26,714 km/h (16,599 mph).
OPS 8781 is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 10502. You can track OPS 8781 in real time on Orbital Radar’s live tracker.
OPS 8781 was launched on 1977-12-08 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 8781 (NORAD ID 10502) 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 8781 travels at approximately 26,714 km/h (16,599 mph) — roughly 7.42 km/s. It completes 14.07 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.
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