RITE TARGET 1
NORAD 28454
Payload
LEO
2002-056F
● Active
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LEO · NORAD 28454
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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
762 km
Apogee
774 km
Inclination
98.8°
Period
100.2 min
Mean Motion
14.37104401 rev/day
TLE Epoch
2026-06-18 03:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude768 km
Orbital Velocity26,900 km/h
Velocity7.47 km/s
Orbital Period100 minutes
Orbits / Day14.37
Eccentricity0.0008
Semi-Major Axis7,139 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~25–100 years
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
2002-12-14
Launch Site
TNSTA
Int'l Designator
2002-056F
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
RITE TARGET 1 is an active satellite operated by Japan, launched on 2002-12-14 from TNSTA. With over 24 years in orbit, it has far exceeded many satellites’ design lifetimes. It orbits in Low Earth Orbit (LEO) at altitudes between 762 km and 774 km with an inclination of 98.8°. It travels at approximately 26,900 km/h (7.47 km/s), completing one full orbit every 100 minutes — that’s roughly 14.37 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 ~25–100 years. Orbital Radar tracks RITE TARGET 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
RITE TARGET 1 orbits at an average altitude of 768 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 RITE TARGET 1’s average altitude, there are currently 390 active payloads and 2,081 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0179, ONEWEB-0455. With an inclination of 98.8°, RITE TARGET 1 passes over latitudes between 98.8°N and 98.8°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 RITE TARGET 1.
❓ Frequently Asked Questions
RITE TARGET 1 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 768 km altitude. Its 98.8° 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 100 minutes, travelling at 26,900 km/h.
RITE TARGET 1 is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 28454. You can track RITE TARGET 1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
RITE TARGET 1 was launched on 2002-12-14 from TNSTA. At its current altitude, the estimated remaining orbital lifetime is: ~25–100 years. View the full satellite launch log.
Yes — Orbital Radar tracks RITE TARGET 1 (NORAD ID 28454) 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.
RITE TARGET 1 travels at approximately 26,900 km/h (16,715 mph) — roughly 7.47 km/s. It completes 14.37 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 29 sunrises and sunsets every 24 hours.