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VELOX-P 2, 39438

Orbit data source: Space-Track

VELOX-P 2, 39438 is a payload satellite owned by NTU (SG) 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
39438, 2013-066Y
Orbit
SSO
Country
Flag of UnknownUnknown / SING
Related business
Manufacturer
NTU
Mission
Non-operational Amateur Technology
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1 kg wet, 1 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: 6 hours ago

TLE from 6 hours ago
0 VELOX-P 2
1 39438U 13066Y   26037.85356219  .00005776  00000-0  55665-3 0  9995
2 39438  97.8600 349.2726 0055307  55.6707 304.9728 14.92154436658395
Epoch: 2026-02-06T20:29Z
TLE epoch observation values (Epoch: 2026-02-06T20:29:07.773Z)
Latitude
0.00001°
Longitude
-94.99526°
Altitude
572.304 km
Speed
7.587 km/s
True Right ascension
23h 17m 05s
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
04:31:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
626.771 km
Perigee altitude
549.713 km
Semi-major axis
6,966.379 km
Eccentricity
0.00553
Inclination
97.86°
RAAN
349.2726°
Arg. of periapsis
55.6707°
True anomaly
304.45141°
Mean anomaly
304.9728°
Eccentric anomaly
304.71231°
Mean motion
3.73278 °/min
Orbital period
96.44 mins
BSTAR
0.00055665
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