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PUCP-SAT 1, 39442

Orbit data source: Space-Track

PUCP-SAT 1, 39442 is a payload satellite owned by PUCP (PE) in SSO that was launched on Thu, 21 Nov 2013 UTC via a DNEPR launch vehicle from the Orenburg, Russia (OREN). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

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Identifier
39442, 2013-066AC
Orbit
SSO
Country
Flag of PEPE / PER
Related business
Manufacturer
PUCP
Mission
Non-operational Amateur Technology
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1.173 kg wet, 1.173 kg dry
Launch date (UTC)
2013-11-21 (12 years ago)
Launch vehicle
DNEPR
Launch site
Orenburg, Russia (OREN)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.015 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 16 hours ago

TLE from 16 hours ago
0 PUCP-SAT 1
1 39442U 13066AC  26091.94053447  .00024346  00000-0  82494-3 0  9991
2 39442  97.5789  84.4830 0014571 205.5791 154.4730 15.30458888672596
Epoch: 2026-04-01T22:34Z
TLE epoch observation values (Epoch: 2026-04-01T22:34:22.178Z)
Latitude
-0.00001°
Longitude
-84.40557°
Altitude
486.557 km
Speed
7.617 km/s
True Right ascension
05h 37m 55s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
20:05:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
481.382 km
Perigee altitude
461.421 km
Semi-major axis
6,849.539 km
Eccentricity
0.00146
Inclination
97.5789°
RAAN
84.483°
Arg. of periapsis
205.5791°
True anomaly
154.54484°
Mean anomaly
154.473°
Eccentric anomaly
154.50893°
Mean motion
3.8287 °/min
Orbital period
94.03 mins
BSTAR
0.00082494
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