PICOSAT 4
NORAD 26092
Payload
LEO
2000-004K
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LEO · NORAD 26092
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
707 km
Apogee
751 km
Inclination
100.2°
Period
99.4 min
Mean Motion
14.48937245 rev/day
TLE Epoch
2026-09-17 01:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude729 km
Orbital Velocity26,974 km/h
Velocity7.49 km/s
Orbital Period99 minutes
Orbits / Day14.49
Eccentricity0.0031
Semi-Major Axis7,100 km
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇺🇸 SCU (United States)
Launch Date
2000-01-27
Launch Site
Vandenberg Space Force Base, United States
Int'l Designator
2000-004K
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
PICOSAT 4 is an active satellite operated by SCU (United States), launched on 2000-01-27 from Vandenberg Space Force Base, United States on the JAWSAT launch. With over 26 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 707 km and 751 km with an inclination of 100.2°. It travels at approximately 26,974 km/h (7.49 km/s), completing one full orbit every 99 minutes — that’s roughly 14.49 orbits per day. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~25–100 years. Orbital Radar tracks PICOSAT 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
PICOSAT 4 orbits at an average altitude of 729 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 PICOSAT 4’s average altitude, there are currently 410 active payloads and 1,981 tracked debris or rocket body fragments — notable neighbours include TERRA, AQUA, ONEWEB-0179. With an inclination of 100.2°, PICOSAT 4 passes over latitudes between 100.2°N and 100.2°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 13,204 active satellites in total, of which 173 share a similar altitude band with PICOSAT 4.
❓ Frequently Asked Questions
PICOSAT 4 orbits in Low Earth Orbit (LEO) at altitudes between 707 km (perigee) and 751 km (apogee), with an average altitude of approximately 729 km. It completes one orbit every 99 minutes, travelling at approximately 26,974 km/h (16,761 mph).
PICOSAT 4 is operated by SCU (United States). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 26092. You can track PICOSAT 4 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
PICOSAT 4 was launched on 2000-01-27 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 PICOSAT 4 (NORAD ID 26092) 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.
PICOSAT 4 travels at approximately 26,974 km/h (16,761 mph) — roughly 7.49 km/s. It completes 14.49 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.