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REX 2

NORAD 23814 Payload LEO 1996-014A ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
790 km
Apogee
824 km
Inclination
90.0°
Period
101.0 min
Mean Motion
14.25362895 rev/day
TLE Epoch
2026-06-19 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude807 km
Orbital Velocity26,827 km/h
Velocity7.45 km/s
Orbital Period101 minutes
Orbits / Day14.25
Eccentricity0.0024
Semi-Major Axis7,178 km
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇺🇸 United States
Launch Date
1996-03-09
Launch Site
Vandenberg SFB, California
Int'l Designator
1996-014A
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
REX 2 is an active satellite operated by United States, launched on 1996-03-09 from Vandenberg SFB, California. With over 30 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 790 km and 824 km with an inclination of 90.0°. It travels at approximately 26,827 km/h (7.45 km/s), completing one full orbit every 101 minutes — that’s roughly 14.25 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. Orbital Radar tracks REX 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
REX 2 orbits at an average altitude of 807 km in the upper LEO band, where atmospheric drag is negligible and objects can persist for centuries to millennia. This altitude is used by broadband constellations like OneWeb and by scientific missions requiring stable orbits far from the densest debris bands. Within ±50 km of REX 2’s average altitude, there are currently 439 active payloads and 2,299 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 90.0°, REX 2 passes over latitudes between 90.0°N and 90.0°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 12,360 active satellites in total, of which 151 share a similar altitude band with REX 2.
❓ Frequently Asked Questions
REX 2 orbits in Low Earth Orbit (LEO) at altitudes between 790 km (perigee) and 824 km (apogee), with an average altitude of approximately 807 km. It completes one orbit every 101 minutes, travelling at approximately 26,827 km/h (16,669 mph).
REX 2 is operated by United States. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 23814. You can track REX 2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
REX 2 was launched on 1996-03-09 from Vandenberg SFB, California, 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: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks REX 2 (NORAD ID 23814) 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.
REX 2 travels at approximately 26,827 km/h (16,669 mph) — roughly 7.45 km/s. It completes 14.25 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.