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SECOR 5 (EGRS 5)

NORAD 1506 Payload MEO 1965-063A ● Active
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🛰️ Orbital Parameters
Perigee
1136 km
Apogee
2419 km
Inclination
69.2°
Period
122.2 min
Mean Motion
11.78694325 rev/day
TLE Epoch
2026-10-21 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,778 km
Orbital Velocity25,179 km/h
Velocity6.99 km/s
Orbital Period2 hours 2 minutes
Orbits / Day11.79
Eccentricity0.0787
Semi-Major Axis8,149 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇺🇸 USA ACE / GIMRADA (United States)
Launch Date
1965-08-10
Launch Site
Wallops Flight Facility / MARS, United States
Int'l Designator
1965-063A
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
SECOR 5 (EGRS 5) is an active satellite operated by USA ACE / GIMRADA (United States), launched on 1965-08-10 from Wallops Flight Facility / MARS, United States on the Secor Type I S/N 2 launch. After more than 61 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 1,136 km and 2,419 km with an inclination of 69.2°. It travels at approximately 25,179 km/h (6.99 km/s), completing one full orbit every 2 hours 2 minutes — that’s roughly 11.79 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. Orbital Radar tracks SECOR 5 (EGRS 5) 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 5 (EGRS 5) orbits at an average altitude of 1,778 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 5 (EGRS 5)’s average altitude, there are currently 7 active payloads and 40 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 69.2°, SECOR 5 (EGRS 5) passes over latitudes between 69.2°N and 69.2°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 2 share a similar altitude band with SECOR 5 (EGRS 5).
❓ Frequently Asked Questions
SECOR 5 (EGRS 5) orbits in Medium Earth Orbit (MEO) at altitudes between 1,136 km (perigee) and 2,419 km (apogee), with an average altitude of approximately 1,778 km. It completes one orbit every 2 hours 2 minutes, travelling at approximately 25,179 km/h (15,645 mph).
SECOR 5 (EGRS 5) is operated by USA ACE / GIMRADA (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 1506. You can track SECOR 5 (EGRS 5) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
SECOR 5 (EGRS 5) was launched on 1965-08-10 from Wallops Flight Facility / MARS, United States. At its current altitude, the estimated remaining orbital lifetime is: thousands of years. View the full satellite launch log.
Yes — Orbital Radar tracks SECOR 5 (EGRS 5) (NORAD ID 1506) 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 5 (EGRS 5) travels at approximately 25,179 km/h (15,645 mph) — roughly 6.99 km/s. It completes 11.79 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 24 sunrises and sunsets every 24 hours.