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NANOSAT(1)

NORAD 28493 Payload LEO 2004-049B ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
627 km
Apogee
631 km
Inclination
98.2°
Period
97.3 min
Mean Motion
14.80163884 rev/day
TLE Epoch
2026-06-19 19:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude629 km
Orbital Velocity27,166 km/h
Velocity7.55 km/s
Orbital Period97 minutes
Orbits / Day14.80
Eccentricity0.0003
Semi-Major Axis7,000 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇪🇸 Instituto Nacional de Técnia Aeroespacial (INTA) (Spain)
Launch Date
2004-12-18
Launch Site
Guiana Space Centre, Kourou
Int'l Designator
2004-049B
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
NANOSAT(1) is an active satellite operated by Instituto Nacional de Técnia Aeroespacial (INTA) (Spain), launched on 2004-12-18 from Guiana Space Centre, Kourou. With over 22 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 627 km and 631 km with an inclination of 98.2°. It travels at approximately 27,166 km/h (7.55 km/s), completing one full orbit every 97 minutes — that’s roughly 14.80 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. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~10–25 years. Orbital Radar tracks NANOSAT(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
NANOSAT(1) orbits at an average altitude of 629 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 NANOSAT(1)’s average altitude, there are currently 785 active payloads and 833 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050. With an inclination of 98.2°, NANOSAT(1) passes over latitudes between 98.2°N and 98.2°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. Spain operates approximately 53 active satellites in total, of which 7 share a similar altitude band with NANOSAT(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
NANOSAT(1) is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 629 km altitude. Its 98.2° 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 97 minutes, travelling at 27,166 km/h.
NANOSAT(1) is operated by Instituto Nacional de Técnia Aeroespacial (INTA) (Spain). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 28493. You can track NANOSAT(1) in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
NANOSAT(1) was launched on 2004-12-18 from Guiana Space Centre, Kourou, the European spaceport in French Guiana, chosen for its equatorial location which provides an energy-efficient boost for orbital insertions. At its current altitude, the estimated remaining orbital lifetime is: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks NANOSAT(1) (NORAD ID 28493) 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.
NANOSAT(1) travels at approximately 27,166 km/h (16,880 mph) — roughly 7.55 km/s. It completes 14.80 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.