Skip to content
Home Library Satellite Directory OPS 8314 (2)

OPS 8314 (2)

NORAD 6822 Payload LEO 1972-079C ● Active
CONNECTING… LEO · NORAD 6822
NOW PASSING OVER
Calculating position…
Altitude (km)
Speed (km/s)
Latitude
Longitude
Real-time tracking powered by Orbital Radar
ORBITAL RADAR · LIVE GROUND TRACK
🌍 Track on 3D Globe
🛰️ Orbital Parameters
Perigee
1419 km
Apogee
1463 km
Inclination
95.6°
Period
114.7 min
Mean Motion
12.55632526 rev/day
TLE Epoch
2026-09-15 17:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,441 km
Orbital Velocity25,715 km/h
Velocity7.14 km/s
Orbital Period115 minutes
Orbits / Day12.56
Eccentricity0.0028
Semi-Major Axis7,812 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1972-10-10
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1972-079C
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
OPS 8314 (2) is an active satellite operated by United States, launched on 1972-10-10 from Vandenberg Space Force Base, United States on the HEXAGON SV-4 launch. After more than 54 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Low Earth Orbit (LEO) at altitudes between 1,419 km and 1,463 km with an inclination of 95.6°. It travels at approximately 25,715 km/h (7.14 km/s), completing one full orbit every 115 minutes — that’s roughly 12.56 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. Orbital Radar tracks OPS 8314 (2) 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 8314 (2) orbits at an average altitude of 1,441 km in the uppermost reaches of Low Earth Orbit. At this altitude, orbital decay is effectively zero without active deorbiting, and coverage footprints are significantly larger than lower LEO, though at the cost of higher latency. Within ±50 km of OPS 8314 (2)’s average altitude, there are currently 511 active payloads and 312 tracked debris or rocket body fragments. With an inclination of 95.6°, OPS 8314 (2) passes over latitudes between 95.6°N and 95.6°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. United States operates approximately 13,206 active satellites in total, of which 18 share a similar altitude band with OPS 8314 (2).
❓ Frequently Asked Questions
OPS 8314 (2) orbits in Low Earth Orbit (LEO) at altitudes between 1,419 km (perigee) and 1,463 km (apogee), with an average altitude of approximately 1,441 km. It completes one orbit every 115 minutes, travelling at approximately 25,715 km/h (15,979 mph).
OPS 8314 (2) is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 6822. You can track OPS 8314 (2) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
OPS 8314 (2) was launched on 1972-10-10 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: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks OPS 8314 (2) (NORAD ID 6822) 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 8314 (2) travels at approximately 25,715 km/h (15,979 mph) — roughly 7.14 km/s. It completes 12.56 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 25 sunrises and sunsets every 24 hours.