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PUCP-SAT 1

NORAD 39442 Payload LEO 2013-066AC ● Active
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Altitude (km)
Speed (km/s)
Latitude
Longitude
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🛰️ Orbital Parameters
Perigee
457 km
Apogee
474 km
Inclination
97.6°
Period
93.9 min
Mean Motion
15.33362551 rev/day
TLE Epoch
2026-06-18 22:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude466 km
Orbital Velocity27,489 km/h
Velocity7.64 km/s
Orbital Period94 minutes
Orbits / Day15.33
Eccentricity0.0012
Semi-Major Axis6,837 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
PER
Launch Date
2013-11-21
Launch Site
OREN
Int'l Designator
2013-066AC
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
PUCP-SAT 1 is an active satellite operated by PER, launched on 2013-11-21 from OREN. After 13 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 457 km and 474 km with an inclination of 97.6°. It travels at approximately 27,489 km/h (7.64 km/s), completing one full orbit every 94 minutes — that’s roughly 15.33 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 ~1–3 years. Orbital Radar tracks PUCP-SAT 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
PUCP-SAT 1 orbits at an average altitude of 466 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 PUCP-SAT 1’s average altitude, there are currently 8,006 active payloads and 179 tracked debris or rocket body fragments — notable neighbours include STARLINK-1008, STARLINK-1017, STARLINK-1039. This makes it one of the more crowded altitude bands, containing roughly 46% of all active satellites. With an inclination of 97.6°, PUCP-SAT 1 passes over latitudes between 97.6°N and 97.6°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. PER operates approximately 2 active satellites in total.
❓ Frequently Asked Questions
PUCP-SAT 1 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 466 km altitude. Its 97.6° 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 94 minutes, travelling at 27,489 km/h.
PUCP-SAT 1 is operated by PER. It is catalogued by the U.S. Space Surveillance Network under NORAD ID 39442. You can track PUCP-SAT 1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
PUCP-SAT 1 was launched on 2013-11-21 from OREN. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks PUCP-SAT 1 (NORAD ID 39442) 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.
PUCP-SAT 1 travels at approximately 27,489 km/h (17,081 mph) — roughly 7.64 km/s. It completes 15.33 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.