OPS 7724
NORAD 6791
Payload
MEO
1973-056A
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MEO · NORAD 6791
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
675 km
Apogee
39668 km
Inclination
63.0°
Period
717.5 min
Mean Motion
2.00686458 rev/day
TLE Epoch
2026-10-21 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude20,172 km
Orbital Velocity13,951 km/h
Velocity3.88 km/s
Orbital Period11 hours 58 minutes
Orbits / Day2.01
Eccentricity0.7345
Semi-Major Axis26,543 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 NRO / SAFSP (United States)
Launch Date
1973-08-21
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1973-056A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
OPS 7724 is an active satellite operated by NRO / SAFSP (United States), launched on 1973-08-21 from Vandenberg Space Force Base, United States on the Jumpseat 3 launch. After more than 53 years in orbit, it is one of the longest-surviving objects in the space catalogue. It orbits in Medium Earth Orbit (MEO) at altitudes between 675 km and 39,668 km with an inclination of 63.0°. It travels at approximately 13,951 km/h (3.88 km/s), completing one full orbit every 11 hours 58 minutes — that’s roughly 2.01 orbits per day. Its orbital eccentricity of 0.7345 gives it a noticeably elliptical path, with significant altitude variation between perigee and apogee. Orbital Radar tracks OPS 7724 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 7724 orbits at an average altitude of 20,172 km in Medium Earth Orbit, the region between LEO and GEO (2,000–35,786 km). MEO’s higher altitude gives each satellite a much larger ground footprint than LEO, meaning fewer spacecraft are needed for global coverage — but signal latency is higher and radiation from the Van Allen belts is a significant design constraint. Within ±50 km of OPS 7724’s average altitude, there are currently 107 active payloads and 14 tracked debris or rocket body fragments. With an inclination of 63.0°, OPS 7724 passes over latitudes between 63.0°N and 63.0°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 13,279 active satellites in total, of which 44 share a similar altitude band with OPS 7724.
❓ Frequently Asked Questions
OPS 7724 orbits in Medium Earth Orbit (MEO) at altitudes between 675 km (perigee) and 39,668 km (apogee), with an average altitude of approximately 20,172 km. It completes one orbit every 11 hours 58 minutes, travelling at approximately 13,951 km/h (8,669 mph).
OPS 7724 is operated by NRO / SAFSP (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 6791. You can track OPS 7724 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
OPS 7724 was launched on 1973-08-21 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: effectively permanent — above atmospheric drag. View the full satellite launch log.
Yes — Orbital Radar tracks OPS 7724 (NORAD ID 6791) using the latest TLE (two-line element set) orbital data in its live tracking catalogue (see our data sources). 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 7724 travels at approximately 13,951 km/h (8,669 mph) — roughly 3.88 km/s. It completes 2.01 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 4 sunrises and sunsets every 24 hours.