VELOX C1
NORAD 41166
Payload
LEO
2015-077A
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LEO · NORAD 41166
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Altitude (km)
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Speed (km/s)
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Latitude
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Longitude
🛰️ Orbital Parameters
Perigee
414 km
Apogee
420 km
Inclination
15.0°
Period
92.9 min
Mean Motion
15.49890130 rev/day
TLE Epoch
2026-06-19 00:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude417 km
Orbital Velocity27,587 km/h
Velocity7.66 km/s
Orbital Period93 minutes
Orbits / Day15.50
Eccentricity0.0004
Semi-Major Axis6,788 km
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
Nanyang Technological University (Singapore)
Launch Date
2015-12-16
Launch Site
SRI
Int'l Designator
2015-077A
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
VELOX C1 is an active satellite operated by Nanyang Technological University (Singapore), launched on 2015-12-16 from SRI. After 11 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 414 km and 420 km with an inclination of 15.0°. It travels at approximately 27,587 km/h (7.66 km/s), completing one full orbit every 93 minutes — that’s roughly 15.50 orbits per day. Its near-circular orbit (eccentricity close to zero) means it maintains a very consistent altitude throughout each revolution. At its current altitude, the estimated orbital lifetime before atmospheric re-entry is ~1–3 years. Orbital Radar tracks VELOX C1 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
VELOX C1 orbits at an average altitude of 417 km in the core of Low Earth Orbit, the most heavily utilised altitude band. The balance of moderate drag (limiting debris accumulation) and short signal path (enabling low-latency links and high-resolution imaging) makes this regime the default for most commercial and government missions. Within ±50 km of VELOX C1’s average altitude, there are currently 2,606 active payloads and 119 tracked debris or rocket body fragments — notable neighbours include STARLINK-1008, STARLINK-1012, STARLINK-1020. This makes it one of the more crowded altitude bands, containing roughly 15% of all active satellites. With an inclination of 15.0°, VELOX C1 passes over latitudes between 15.0°N and 15.0°S, concentrating coverage over equatorial and near-equatorial regions. Low-inclination orbits maximise revisit rates over specific tropical zones. Singapore operates approximately 14 active satellites in total, of which 2 share a similar altitude band with VELOX C1.
❓ Frequently Asked Questions
VELOX C1 orbits in Low Earth Orbit (LEO) at altitudes between 414 km (perigee) and 420 km (apogee), with an average altitude of approximately 417 km. It completes one orbit every 93 minutes, travelling at approximately 27,587 km/h (17,142 mph).
VELOX C1 is operated by Nanyang Technological University (Singapore). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 41166. You can track VELOX C1 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
VELOX C1 was launched on 2015-12-16 from SRI. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks VELOX C1 (NORAD ID 41166) using the latest TLE (two-line element set) data from Space-Track and CelesTrak. Open the live tracker to see its current position, altitude, speed and orbital path updated in real time. You can also browse the satellite directory to find other tracked objects.
VELOX C1 travels at approximately 27,587 km/h (17,142 mph) — roughly 7.66 km/s. It completes 15.50 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.