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CUBESAT XI-IV (CO-57)

NORAD 27848 Payload LEO 2003-031J ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
806 km
Apogee
821 km
Inclination
98.7°
Period
101.2 min
Mean Motion
14.23566913 rev/day
TLE Epoch
2026-03-17 10:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude814 km
Orbital Velocity26,815 km/h
Velocity7.45 km/s
Orbital Period101 minutes
Orbits / Day14.24
Eccentricity0.0010
Semi-Major Axis7,185 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
2003-06-30
Launch Site
PKMTR
Int'l Designator
2003-031J
Object Type
Payload
RCS Size
Small (<0.1 m²)
🔗 Constellation / Groups
cubesatamateurengineering
📖 About This Object
CUBESAT XI-IV (CO-57) is an active satellite operated by Japan, launched on 2003-06-30 from PKMTR. With over 23 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 806 km and 821 km with an inclination of 98.7°. It travels at approximately 26,815 km/h (7.45 km/s), completing one full orbit every 101 minutes — that’s roughly 14.24 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. It is part of the Cubesat constellation group. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. Orbital Radar tracks CUBESAT XI-IV (CO-57) in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
CUBESAT XI-IV (CO-57) operates in a sun-synchronous orbit (SSO), a special subset of LEO where the orbital plane precesses to keep a constant angle relative to the Sun. This means the satellite crosses any given latitude at approximately the same local solar time on every pass, providing consistent lighting conditions — essential for Earth observation, weather monitoring and environmental science. SSO orbits typically sit between 600 and 800 km altitude with inclinations near 97–99°.
🔗 CubeSat

This is a CubeSat — a class of miniaturised satellite built to standardised dimensions (1U = 10×10×10 cm, ~1.3 kg). CubeSats have democratised space access, enabling universities, startups and research institutions to deploy orbital experiments at a fraction of traditional satellite costs. They are used for technology demonstration, Earth observation, communications and scientific research.

❓ Frequently Asked Questions
CUBESAT XI-IV (CO-57) is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 814 km altitude. Its 98.7° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 101 minutes, travelling at 26,815 km/h.
CUBESAT XI-IV (CO-57) is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 27848. You can track CUBESAT XI-IV (CO-57) in real time on Orbital Radar’s live tracker.
CUBESAT XI-IV (CO-57) was launched on 2003-06-30 from PKMTR. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years.
Yes — Orbital Radar tracks CUBESAT XI-IV (CO-57) (NORAD ID 27848) 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.
CUBESAT XI-IV (CO-57) travels at approximately 26,815 km/h (16,662 mph) — roughly 7.45 km/s. It completes 14.24 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 28 sunrises and sunsets every 24 hours.
CUBESAT XI-IV (CO-57) is a member of the Cubesat constellation. Satellites in this group work together to provide coordinated coverage, typically in similar orbital planes at comparable altitudes. You can view all Cubesat satellites on Orbital Radar’s live tracker.