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SECOR 8 (EGRS 8)

NORAD 2520 Payload MEO 1966-089B ● Active
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🛰️ Orbital Parameters
Perigee
3679 km
Apogee
3709 km
Inclination
89.9°
Period
167.7 min
Mean Motion
8.58893634 rev/day
TLE Epoch
2026-10-21 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude3,694 km
Orbital Velocity22,655 km/h
Velocity6.29 km/s
Orbital Period2 hours 48 minutes
Orbits / Day8.59
Eccentricity0.0015
Semi-Major Axis10,065 km
Est. Orbital LifetimeEffectively permanent — above atmospheric drag
🚀 Launch & Identity
Country / Operator
🇺🇸 USA ACE / GIMRADA (United States)
Launch Date
1966-10-05
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1966-089B
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
SECOR 8 (EGRS 8) is an active satellite operated by USA ACE / GIMRADA (United States), launched on 1966-10-05 from Vandenberg Space Force Base, United States on the Midas RTS-I F3 launch. After more than 60 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 3,679 km and 3,709 km with an inclination of 89.9°. It travels at approximately 22,655 km/h (6.29 km/s), completing one full orbit every 2 hours 48 minutes — that’s roughly 8.59 orbits per day. Orbital Radar tracks SECOR 8 (EGRS 8) in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
SECOR 8 (EGRS 8) orbits at an average altitude of 3,694 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 SECOR 8 (EGRS 8)’s average altitude, there are currently 8 active payloads and 4 tracked debris or rocket body fragments. This is a relatively sparse altitude band, containing less than 1% of all active satellites. With an inclination of 89.9°, SECOR 8 (EGRS 8) passes over latitudes between 89.9°N and 89.9°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 13,279 active satellites in total, of which 8 share a similar altitude band with SECOR 8 (EGRS 8).
❓ Frequently Asked Questions
SECOR 8 (EGRS 8) orbits in Medium Earth Orbit (MEO) at altitudes between 3,679 km (perigee) and 3,709 km (apogee), with an average altitude of approximately 3,694 km. It completes one orbit every 2 hours 48 minutes, travelling at approximately 22,655 km/h (14,077 mph).
SECOR 8 (EGRS 8) is operated by USA ACE / GIMRADA (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 2520. You can track SECOR 8 (EGRS 8) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
SECOR 8 (EGRS 8) was launched on 1966-10-05 from Vandenberg Space Force Base, United States, primarily used for polar and sun-synchronous orbit launches due to its southward ocean trajectory from California. View the full satellite launch log.
Yes — Orbital Radar tracks SECOR 8 (EGRS 8) (NORAD ID 2520) 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.
SECOR 8 (EGRS 8) travels at approximately 22,655 km/h (14,077 mph) — roughly 6.29 km/s. It completes 8.59 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 17 sunrises and sunsets every 24 hours.