CUTE-1
NORAD 27844
Payload
LEO
2003-031E
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LEO · NORAD 27844
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Altitude (km)
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Longitude
🛰️ Orbital Parameters
Perigee
804 km
Apogee
818 km
Inclination
98.7°
Period
101.1 min
Mean Motion
14.24336816 rev/day
TLE Epoch
2026-06-19 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude811 km
Orbital Velocity26,819 km/h
Velocity7.45 km/s
Orbital Period101 minutes
Orbits / Day14.24
Eccentricity0.0010
Semi-Major Axis7,182 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
2003-031E
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
CUTE-1 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 804 km and 818 km with an inclination of 98.7°. It travels at approximately 26,819 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. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~100–500 years. Orbital Radar tracks CUTE-1 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
CUTE-1 orbits at an average altitude of 811 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 CUTE-1’s average altitude, there are currently 433 active payloads and 2,312 tracked debris or rocket body fragments — notable neighbours include NOAA 20, ONEWEB-0179, ONEWEB-0455. With an inclination of 98.7°, CUTE-1 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 CUTE-1.
🔗 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
CUTE-1 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 811 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 26,819 km/h.
CUTE-1 is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 27844. You can track CUTE-1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
CUTE-1 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 CUTE-1 (NORAD ID 27844) 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.
CUTE-1 travels at approximately 26,819 km/h (16,665 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.