Showing default

VELOX C1, 41166

Orbit data source: Space-Track

VELOX C1, 41166 is a payload satellite owned by NTU (SG) in LEO that was launched on Wed, 16 Dec 2015 UTC via a PSLV launch vehicle from the Sirharikota (SRI). 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.

Not visible in the next 10 days
Identifier
41166, 2015-077A
Orbit
LEO
Country
Flag of SGSG / SING
Related business
Manufacturer
NTU
Mission
Operational Amateur Meteo Radio Occ.
Bus & Motor
VELOX-C, Unknown motor
Mass
123 kg wet, 123 kg dry
Launch date (UTC)
2015-12-16 (11 years ago)
Launch vehicle
PSLV
Launch site
Sirharikota (SRI)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.348 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 5 hours ago

TLE from 5 hours ago
0 VELOX C1
1 41166U 15077A   26296.15801557  .00029345  00000-0  40134-3 0  9993
2 41166  14.9815 169.5742 0004497 316.2864  43.7106 15.55070383602642
Epoch: 2026-10-23T03:47Z
TLE epoch observation values (Epoch: 2026-10-23T03:47:32.545Z)
Latitude
-0.00001°
Longitude
81.10598°
Altitude
396.945 km
Speed
7.677 km/s
True Right ascension
11h 18m 17s
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
04:09:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
410.852 km
Perigee altitude
404.749 km
Semi-major axis
6,785.938 km
Eccentricity
0.00045
Inclination
14.9815°
RAAN
169.5742°
Arg. of periapsis
316.2864°
True anomaly
43.74622°
Mean anomaly
43.7106°
Eccentric anomaly
43.72841°
Mean motion
3.88265 °/min
Orbital period
92.72 mins
BSTAR
0.00040134
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|