PROITERES
NORAD 38756
Payload
LEO
2012-047B
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LEO · NORAD 38756
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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
613 km
Apogee
630 km
Inclination
98.2°
Period
97.1 min
Mean Motion
14.82502484 rev/day
TLE Epoch
2026-06-19 06:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude622 km
Orbital Velocity27,180 km/h
Velocity7.55 km/s
Orbital Period97 minutes
Orbits / Day14.83
Eccentricity0.0012
Semi-Major Axis6,993 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~10–25 years
🚀 Launch & Identity
Country / Operator
🇯🇵 Japan
Launch Date
2012-09-09
Launch Site
SRI
Int'l Designator
2012-047B
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
PROITERES is an active satellite operated by Japan, launched on 2012-09-09 from SRI. After 14 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 613 km and 630 km with an inclination of 98.2°. It travels at approximately 27,180 km/h (7.55 km/s), completing one full orbit every 97 minutes — that’s roughly 14.83 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 ~10–25 years. Orbital Radar tracks PROITERES in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
PROITERES orbits at an average altitude of 622 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 PROITERES’s average altitude, there are currently 1,528 active payloads and 784 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-3090, STARLINK-3077. This makes it one of the more crowded altitude bands, containing roughly 8.8% of all active satellites. With an inclination of 98.2°, PROITERES 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. Japan operates approximately 189 active satellites in total, of which 27 share a similar altitude band with PROITERES.
❓ Frequently Asked Questions
PROITERES is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 622 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 27,180 km/h.
PROITERES is operated by Japan. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 38756. You can track PROITERES in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
PROITERES was launched on 2012-09-09 from SRI. At its current altitude, the estimated remaining orbital lifetime is: ~10–25 years. View the full satellite launch log.
Yes — Orbital Radar tracks PROITERES (NORAD ID 38756) 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.
PROITERES travels at approximately 27,180 km/h (16,889 mph) — roughly 7.55 km/s. It completes 14.83 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.