CUBESAT XI 4
NORAD 27848
Payload
LEO
2003-031J
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LEO · NORAD 27848
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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
807 km
Apogee
820 km
Inclination
98.7°
Period
101.2 min
Mean Motion
14.23622052 rev/day
TLE Epoch
2026-06-19 23:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude814 km
Orbital Velocity26,815 km/h
Velocity7.45 km/s
Orbital Period101 minutes
Orbits / Day14.24
Eccentricity0.0009
Semi-Major Axis7,185 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~100–500 years
🚀 Launch & Identity
Country / Operator
🇯🇵 Department of Astronautics, University of Tokyo (Japan)
Launch Date
2003-06-30
Launch Site
PKMTR
Int'l Designator
2003-031J
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
🔗 Constellation / Groups
cubesat
📖 About This Object
CUBESAT XI 4 is an active satellite operated by Department of Astronautics, University of Tokyo (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 807 km and 820 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. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. 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 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
CUBESAT XI 4 orbits at an average altitude of 814 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of CUBESAT XI 4’s average altitude, there are currently 419 active payloads and 2,319 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 98.7°, CUBESAT XI 4 passes over latitudes between 98.7°N and 98.7°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. Japan operates approximately 189 active satellites in total, of which 9 share a similar altitude band with CUBESAT XI 4.
🔗 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 4 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 4 is operated by Department of Astronautics, University of Tokyo (Japan). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 27848. You can track CUBESAT XI 4 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
CUBESAT XI 4 was launched on 2003-06-30 from PKMTR. At its current altitude, the estimated remaining orbital lifetime is: ~100–500 years. View the full satellite launch log.
Yes — Orbital Radar tracks CUBESAT XI 4 (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. You can also browse the satellite directory to find other tracked objects.
CUBESAT XI 4 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 4 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.