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Home Library Satellite Directory OPS 8701

OPS 8701

NORAD 13086 Payload GEO 1982-019A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
36365 km
Apogee
36396 km
Inclination
9.3°
Period
1466.5 min
Mean Motion
0.98190148 rev/day
TLE Epoch
2026-06-19 14:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude36,381 km
Orbital Velocity10,992 km/h
Velocity3.05 km/s
Orbital Period24.4 hours
Orbits / Day0.98
Eccentricity0.0004
Semi-Major Axis42,752 km
Est. Orbital LifetimePermanent — geostationary orbit, no atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1982-03-06
Launch Site
Cape Canaveral, Florida
Int'l Designator
1982-019A
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
OPS 8701 is an active satellite operated by United States, launched on 1982-03-06 from Cape Canaveral, Florida. With over 44 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Geostationary Orbit (GEO) at altitudes between 36,365 km and 36,396 km with an inclination of 9.3°. It travels at approximately 10,992 km/h (3.05 km/s), completing one full orbit every 24.4 hours — that’s roughly 0.98 orbits per day. At geostationary altitude, there is no meaningful atmospheric drag — this object will remain in orbit indefinitely unless actively deorbited. Orbital Radar tracks OPS 8701 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 8701 occupies geostationary orbit at approximately 35,786 km above the equator, where its orbital period matches the Earth’s 24-hour rotation. From the ground, it appears to hover over a fixed point — ideal for broadcast television, weather monitoring and wideband communications. With an inclination of 9.3°, it traces a small figure-of-eight pattern relative to the equator rather than remaining perfectly stationary, which can indicate aging stationkeeping fuel or a deliberate inclined-orbit strategy. Within ±50 km of OPS 8701’s average altitude, there are currently 28 active payloads and 16 tracked debris or rocket body fragments. United States operates approximately 12,360 active satellites in total, of which 5 share a similar altitude band with OPS 8701.
❓ Frequently Asked Questions
OPS 8701 orbits at approximately 36,381 km altitude, where the orbital period matches the Earth’s 24-hour rotation. This means it stays above the same point on the equator at all times. Its actual speed is still 10,992 km/h — it just keeps pace with the ground below. With an inclination of 9.3°, it actually traces a small figure-of-eight pattern rather than remaining perfectly fixed. Learn more about geostationary orbits.
OPS 8701 is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 13086. You can track OPS 8701 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
OPS 8701 was launched on 1982-03-06 from Cape Canaveral, Florida, one of the busiest launch facilities in the world, operated by NASA and the U.S. Space Force on Florida’s Atlantic coast. View the full satellite launch log.
Yes — Orbital Radar tracks OPS 8701 (NORAD ID 13086) 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 8701 travels at approximately 10,992 km/h (6,830 mph) — roughly 3.05 km/s. Despite this high speed, it appears stationary from the ground because it matches the Earth’s rotation. Geostationary satellites are actually slower than LEO satellites because orbital velocity decreases with altitude.