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CUBESAT XI-V

NORAD 28895 Payload LEO 2005-043F ● Active
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🛰️ Orbital Parameters
Perigee
643 km
Apogee
664 km
Inclination
98.3°
Period
97.8 min
Mean Motion
14.72355170 rev/day
TLE Epoch
2026-03-17 20:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude654 km
Orbital Velocity27,118 km/h
Velocity7.53 km/s
Orbital Period98 minutes
Orbits / Day14.72
Eccentricity0.0015
Semi-Major Axis7,025 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
2005-10-27
Launch Site
PKMTR
Int'l Designator
2005-043F
Object Type
Payload
RCS Size
Small (<0.1 m²)
🔗 Constellation / Groups
cubesatamateur
📖 About This Object
CUBESAT XI-V is an active satellite operated by Japan, launched on 2005-10-27 from PKMTR. With over 21 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 643 km and 664 km with an inclination of 98.3°. It travels at approximately 27,118 km/h (7.53 km/s), completing one full orbit every 98 minutes — that’s roughly 14.72 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 ~10–25 years. Orbital Radar tracks CUBESAT XI-V 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-V 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-V is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 654 km altitude. Its 98.3° 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 98 minutes, travelling at 27,118 km/h.
CUBESAT XI-V is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 28895. You can track CUBESAT XI-V in real time on Orbital Radar’s live tracker.
CUBESAT XI-V was launched on 2005-10-27 from PKMTR. At its current altitude, the estimated remaining orbital lifetime is: ~10–25 years.
Yes — Orbital Radar tracks CUBESAT XI-V (NORAD ID 28895) 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-V travels at approximately 27,118 km/h (16,851 mph) — roughly 7.53 km/s. It completes 14.72 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.
CUBESAT XI-V 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.