Skip to content
Home › Library › Satellite Directory › SECOR 4 (EGRS 4)

SECOR 4 (EGRS 4)

NORAD 1315 Payload LEO 1965-027B ● Active
CONNECTING… LEO · NORAD 1315
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
1268 km
Apogee
1314 km
Inclination
90.3°
Period
111.4 min
Mean Motion
12.92669475 rev/day
TLE Epoch
2026-10-21 04:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,291 km
Orbital Velocity25,966 km/h
Velocity7.21 km/s
Orbital Period111 minutes
Orbits / Day12.93
Eccentricity0.0030
Semi-Major Axis7,662 km
Est. Orbital LifetimeThousands of years
🚀 Launch & Identity
Country / Operator
🇺🇸 USA ACE / GIMRADA (United States)
Launch Date
1965-04-03
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1965-027B
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
SECOR 4 (EGRS 4) is an active satellite operated by USA ACE / GIMRADA (United States), launched on 1965-04-03 from Vandenberg Space Force Base, United States on the SNAP-10A FS-4 launch. After more than 61 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 1,268 km and 1,314 km with an inclination of 90.3°. It travels at approximately 25,966 km/h (7.21 km/s), completing one full orbit every 111 minutes — that’s roughly 12.93 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is thousands of years. Orbital Radar tracks SECOR 4 (EGRS 4) 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 4 (EGRS 4) orbits at an average altitude of 1,291 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 SECOR 4 (EGRS 4)’s average altitude, there are currently 24 active payloads and 394 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 90.3°, SECOR 4 (EGRS 4) passes over latitudes between 90.3°N and 90.3°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 9 share a similar altitude band with SECOR 4 (EGRS 4).
❓ Frequently Asked Questions
SECOR 4 (EGRS 4) orbits in Low Earth Orbit (LEO) at altitudes between 1,268 km (perigee) and 1,314 km (apogee), with an average altitude of approximately 1,291 km. It completes one orbit every 111 minutes, travelling at approximately 25,966 km/h (16,134 mph).
SECOR 4 (EGRS 4) is operated by USA ACE / GIMRADA (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 1315. You can track SECOR 4 (EGRS 4) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
SECOR 4 (EGRS 4) was launched on 1965-04-03 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 SECOR 4 (EGRS 4) (NORAD ID 1315) 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 4 (EGRS 4) travels at approximately 25,966 km/h (16,134 mph) — roughly 7.21 km/s. It completes 12.93 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 26 sunrises and sunsets every 24 hours.