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SERT 2

NORAD 4327 Payload LEO 1970-009A ● Active
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🛰️ Orbital Parameters
Perigee
1037 km
Apogee
1043 km
Inclination
99.3°
Period
106.0 min
Mean Motion
13.58748585 rev/day
TLE Epoch
2026-10-21 13:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude1,040 km
Orbital Velocity26,402 km/h
Velocity7.33 km/s
Orbital Period106 minutes
Orbits / Day13.59
Eccentricity0.0004
Semi-Major Axis7,411 km
Est. Orbital Lifetime~500–1,000 years
🚀 Launch & Identity
Country / Operator
🇺🇸 NASA LeRC (United States)
Launch Date
1970-02-04
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1970-009A
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
SERT 2 is an active satellite operated by NASA LeRC (United States), launched on 1970-02-04 from Vandenberg Space Force Base, United States on the SERT 2 launch. After more than 56 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 1,037 km and 1,043 km with an inclination of 99.3°. It travels at approximately 26,402 km/h (7.33 km/s), completing one full orbit every 106 minutes — that’s roughly 13.59 orbits per day. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~500–1,000 years. Orbital Radar tracks SERT 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
SERT 2 orbits at an average altitude of 1,040 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 SERT 2’s average altitude, there are currently 333 active payloads and 689 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0041. With an inclination of 99.3°, SERT 2 passes over latitudes between 99.3°N and 99.3°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 13,276 active satellites in total, of which 40 share a similar altitude band with SERT 2.
❓ Frequently Asked Questions
SERT 2 orbits in Low Earth Orbit (LEO) at altitudes between 1,037 km (perigee) and 1,043 km (apogee), with an average altitude of approximately 1,040 km. It completes one orbit every 106 minutes, travelling at approximately 26,402 km/h (16,405 mph).
SERT 2 is operated by NASA LeRC (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 4327. You can track SERT 2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
SERT 2 was launched on 1970-02-04 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: ~500–1,000 years. View the full satellite launch log.
Yes — Orbital Radar tracks SERT 2 (NORAD ID 4327) 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.
SERT 2 travels at approximately 26,402 km/h (16,405 mph) — roughly 7.33 km/s. It completes 13.59 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 27 sunrises and sunsets every 24 hours.