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RIGIDSPHERE 2 (LCS 4)

NORAD 5398 Payload LEO 1971-067E ● Active
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🛰️ Orbital Parameters
Perigee
722 km
Apogee
808 km
Inclination
87.6°
Period
100.1 min
Mean Motion
14.37986028 rev/day
TLE Epoch
2026-10-21 13:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude765 km
Orbital Velocity26,906 km/h
Velocity7.47 km/s
Orbital Period100 minutes
Orbits / Day14.38
Eccentricity0.0060
Semi-Major Axis7,136 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇺🇸 US Army / MIT-LL (United States)
Launch Date
1971-08-07
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
1971-067E
Object Type
Payload
RCS Size
Large (>1 m²)
📖 About This Object
RIGIDSPHERE 2 (LCS 4) is an active satellite operated by US Army / MIT-LL (United States), launched on 1971-08-07 from Vandenberg Space Force Base, United States on the OAR-901 launch. After more than 55 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 722 km and 808 km with an inclination of 87.6°. It travels at approximately 26,906 km/h (7.47 km/s), completing one full orbit every 100 minutes — that’s roughly 14.38 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. Orbital Radar tracks RIGIDSPHERE 2 (LCS 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
RIGIDSPHERE 2 (LCS 4) orbits at an average altitude of 765 km in the mid-LEO band, where atmospheric drag is minimal but radiation exposure remains manageable. Objects at this altitude persist for decades to centuries, making debris mitigation critical. This regime is popular for remote sensing constellations and scientific instruments that need stable, long-duration orbits. Within ±50 km of RIGIDSPHERE 2 (LCS 4)’s average altitude, there are currently 431 active payloads and 2,276 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0455. With an inclination of 87.6°, RIGIDSPHERE 2 (LCS 4) passes over latitudes between 87.6°N and 87.6°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 184 share a similar altitude band with RIGIDSPHERE 2 (LCS 4).
❓ Frequently Asked Questions
RIGIDSPHERE 2 (LCS 4) orbits in Low Earth Orbit (LEO) at altitudes between 722 km (perigee) and 808 km (apogee), with an average altitude of approximately 765 km. It completes one orbit every 100 minutes, travelling at approximately 26,906 km/h (16,718 mph).
RIGIDSPHERE 2 (LCS 4) is operated by US Army / MIT-LL (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 5398. You can track RIGIDSPHERE 2 (LCS 4) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
RIGIDSPHERE 2 (LCS 4) was launched on 1971-08-07 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: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks RIGIDSPHERE 2 (LCS 4) (NORAD ID 5398) 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.
RIGIDSPHERE 2 (LCS 4) travels at approximately 26,906 km/h (16,718 mph) — roughly 7.47 km/s. It completes 14.38 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.