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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40057 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / SINGRelated business
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)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 4 Pan, 0.2 m
Radar Cross Section
0.092 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 VELOX 1
1 40057U 14034E 25300.97839469 .00008419 00000-0 77977-3 0 9995
2 40057 98.2712 188.0384 0007035 331.3516 28.7315 14.94752486611875Epoch: 2025-10-27T23:28Z
TLE epoch observation values (Epoch: 2025-10-27T23:28:53.301Z)
Latitude
-0.00005°
Longitude
159.24384°
Altitude
581.877 km
Speed
7.572 km/s
True Right ascension
12h 32m 09s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
03:58:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
585.075 km
Perigee altitude
575.284 km
Semi-major axis
6,958.316 km
Eccentricity
0.0007
Inclination
98.2712°
RAAN
188.0384°
Arg. of periapsis
331.3516°
True anomaly
28.77028°
Mean anomaly
28.7315°
Eccentric anomaly
28.75089°
Mean motion
3.73927 °/min
Orbital period
96.28 mins
BSTAR
0.00077977
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Other satellites on launch #34 in the year 2014 (2014-06-30 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.VELOX 1 Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-28 15:41:53.469Z | 112.083° ESE | 2025-10-28 15:44:53.469Z | 58.768° ENE | 19.849° | 2025-10-28 15:46:53.469Z | 25.118° NE |
| 5 mins | 2025-10-28 17:17:53.469Z | 222.213° SW | 2025-10-28 17:19:53.469Z | 269.83° W | 25.536° | 2025-10-28 17:22:53.469Z | 321.256° NNW |
| 6 mins | 2025-10-29 04:58:53.469Z | 38.549° NE | 2025-10-29 05:01:53.469Z | 105.852° ESE | 30.203° | 2025-10-29 05:04:53.469Z | 162.005° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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