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VELOX 1, 40057

Orbit data source: Space-Track

VELOX 1, 40057 is a payload satellite owned by NTU (SG) in SSO that was launched on Mon, 30 Jun 2014 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.

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Identifier
40057, 2014-034E
Orbit
SSO
Last TLE update
3 hours ago
Origin
Manufacturer
NTU
Mission
Non-operational Amateur Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4.25 kg wet, 4.25 kg dry
Launch date (UTC)
2014-06-30 (11 years ago)
Launch vehicle
PSLV
Launch site
Sirharikota (SRI)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 4 Pan, 0.34 m
Radar Cross Section
0.092 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 3 hours ago
0 VELOX 1
1 40057U 14034E   25129.54739278  .00005523  00000-0  53889-3 0  9993
2 40057  98.2984   7.4054 0008898 149.1997 210.9745 14.92847024586289
Epoch: 2025-05-09T13:08Z
Definitive object data (Epoch: 2025-05-09T13:08:14.736Z)
Latitude
0.00005°
Longitude
-57.25797°
Altitude
597.408 km
Speed
7.558 km/s
True Right ascension
00h 29m 37s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at TLE epoch
Visualization TLE readout
Latitude
50.197°
Longitude
-67.13242°
Altitude
597.928 km
Speed
7.565 km/s
Apparent Right ascension
16h 55m 42s
Apparent Declination
46° 25' 53"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
00:45:23
Azimuth
321.144° NNW
Elevation
12.795°
Doppler factor
1
Orbital elements
Apogee altitude
592.302 km
Perigee altitude
579.909 km
Semi-major axis
6,964.243 km
Eccentricity
0.0008898
Inclination
98.2984°
RAAN
7.4054°
Arg. of periapsis
149.1997°
True anomaly
210.92207°
Mean anomaly
210.9745°
Eccentric anomaly
210.94828°
Mean motion
3.7345 °/min
BSTAR
0.00053889
Orbital period
96.4 mins
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Other satellites on launch #34 in the year 2014 (2014-06-30 UTC)

VELOX 1 Visibility forecast

Observer location: undefined°, undefined°

Span
Click to sort rows by Start time (UTC) header in descending order
Start Az.
Max El. time (UTC)
Max El. Az.
Max El.
End time (UTC)
End Az.
6 mins2025-05-10 04:11:53.392Z39.278° NE2025-05-10 04:14:53.392Z107.68° ESE29.778°2025-05-10 04:17:53.392Z162.216° S
5 mins2025-05-10 15:01:53.392Z111.831° ESE2025-05-10 15:03:53.392Z73.669° E23.008°2025-05-10 15:06:53.392Z18.589° NNE
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