VELOX 2, 41171 (Decayed)
Orbit data source: Space-Track
VELOX 2, 41171 was 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.
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41171 intel report (Beta)
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VELOX 2 radio frequencies
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 VELOX 2
1 41171U 15077F 24200.22842821 .01761728 20491-2 21891-2 0 9994
2 41171 14.9815 159.0057 0006929 222.3342 137.6457 16.06834981476786
Epoch: 2024-07-18T05:28Z
TLE epoch observation values (Epoch: 2024-07-18T05:28:56.197Z)
Latitude
-0.00001°
Longitude
140.24991°
Altitude
256.074 km
Speed
7.755 km/s
True Right ascension
10h 36m 01s
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
15:03:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
266.122 km
Perigee altitude
256.921 km
Semi-major axis
6,639.659 km
Eccentricity
0.00069
Inclination
14.9815°
RAAN
159.0057°
Arg. of periapsis
222.3342°
True anomaly
137.69916°
Mean anomaly
137.6457°
Eccentric anomaly
137.67243°
Mean motion
4.01166 °/min
Orbital period
89.74 mins
BSTAR
0.0021891
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Other satellites on launch #77 in the year 2015 (2015-12-16 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 2 Visibility
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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. |
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This satellite is decayed. |
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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