VELOX C1
Satellite information VELOX C1 - VELOX-CI
| Spacetrack Directory Name | VELOX C1 |
| Alternative name | VELOX-CI |
| Follow VELOX C1 | VELOX C1 Tracker |
| Pass predictions VELOX C1 | Pass predictions VELOX C1 |
| Orbit launches |
2015-12-16 (10 years ago)
|
| Days in orbit | 3977 |
| Country/organisation of origin | Singapur (SING) |
| Starting point | SRILR (Satish Dhawan Space Centre, India) |
| WWW | Here |
| Perigee | 528 km |
| Apogee | 543 km |
| Orbit slope (inclination) | 14.98° |
| Laps per day | 16 |
| Orbit | LEO (Equatorial) |
| Height VELOX C1 | 420.47 km |
Additional information VELOX C1
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). Payloads include a variety of satellites, spacecraft, and rockets 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.
satellite VELOX C1 Date of exalting 16.12.2015y. Average height of ISS VELOX C1 hundred 420.47 km. Average velocity VELOX C1 is 27584.38 km/h. Inclination VELOX C1 satellite 14.98°.TLE
Average velocity VELOX C1
Average inclination VELOX C1
Mean right ascension of the ascending node (RAAN) VELOX C1
Mean argument of perigee VELOX C1
Mean semi-major axis of the orbit VELOX C1
Mean orbital eccentricity VELOX C1
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