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SOCRATES

NORAD 39768 Payload LEO 2014-029C ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
579 km
Apogee
587 km
Inclination
97.9°
Period
96.3 min
Mean Motion
14.94789642 rev/day
TLE Epoch
2026-06-19 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude583 km
Orbital Velocity27,255 km/h
Velocity7.57 km/s
Orbital Period96 minutes
Orbits / Day14.95
Eccentricity0.0006
Semi-Major Axis6,954 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~3–10 years
🚀 Launch & Identity
Country / Operator
🇯🇵 National Institute of Information and Communications Technology (JPN) (Japan)
Launch Date
2014-05-24
Launch Site
TNSTA
Int'l Designator
2014-029C
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
SOCRATES is an active satellite operated by National Institute of Information and Communications Technology (JPN) (Japan), launched on 2014-05-24 from TNSTA. After 12 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 579 km and 587 km with an inclination of 97.9°. It travels at approximately 27,255 km/h (7.57 km/s), completing one full orbit every 96 minutes — that’s roughly 14.95 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 ~3–10 years. Orbital Radar tracks SOCRATES in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
SOCRATES orbits at an average altitude of 583 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 SOCRATES’s average altitude, there are currently 3,257 active payloads and 572 tracked debris or rocket body fragments — notable neighbours include ONEWEB-0050, STARLINK-3005, STARLINK-3090. This makes it one of the more crowded altitude bands, containing roughly 18.7% of all active satellites. With an inclination of 97.9°, SOCRATES passes over latitudes between 97.9°N and 97.9°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 41 share a similar altitude band with SOCRATES.
❓ Frequently Asked Questions
SOCRATES is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 583 km altitude. Its 97.9° 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 96 minutes, travelling at 27,255 km/h.
SOCRATES is operated by National Institute of Information and Communications Technology (JPN) (Japan). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 39768. You can track SOCRATES in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
SOCRATES was launched on 2014-05-24 from TNSTA. At its current altitude, the estimated remaining orbital lifetime is: ~3–10 years. View the full satellite launch log.
Yes — Orbital Radar tracks SOCRATES (NORAD ID 39768) 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.
SOCRATES travels at approximately 27,255 km/h (16,936 mph) — roughly 7.57 km/s. It completes 14.95 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 30 sunrises and sunsets every 24 hours.