LILACSAT 2
NORAD 40908
Payload
LEO
2015-049K
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LEO · NORAD 40908
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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
407 km
Apogee
416 km
Inclination
97.5°
Period
92.8 min
Mean Motion
15.51731803 rev/day
TLE Epoch
2026-06-26 05:00:00 UTC
📐 Computed Orbital Characteristics
Avg. Altitude412 km
Orbital Velocity27,598 km/h
Velocity7.67 km/s
Orbital Period93 minutes
Orbits / Day15.52
Eccentricity0.0007
Semi-Major Axis6,783 km
Orbit ClassSun-Synchronous (SSO)
Est. Orbital Lifetime~1–3 years
🚀 Launch & Identity
Country / Operator
🇨🇳 Harbin Institute/China Amateur Satellite - CAMSAT (China)
Launch Date
2015-09-19
Launch Site
Taiyuan, China
Int'l Designator
2015-049K
Object Type
Payload
RCS Size
Medium (0.1–1 m²)
📖 About This Object
LILACSAT 2 is an active satellite operated by Harbin Institute/China Amateur Satellite - CAMSAT (China), launched on 2015-09-19 from Taiyuan, China on the Cluster launch. After 11 years in orbit, it continues to be tracked by global surveillance networks. It orbits in Low Earth Orbit (LEO) at altitudes between 407 km and 416 km with an inclination of 97.5°. It travels at approximately 27,598 km/h (7.67 km/s), completing one full orbit every 93 minutes — that’s roughly 15.52 orbits per day. Its near-polar, sun-synchronous orbit means it passes over any given point on Earth at approximately the same local solar time, ideal for consistent Earth observation lighting conditions. 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 LILACSAT 2 in real time using the latest two-line element set (TLE) data, providing live position, altitude, speed and orbital path updated continuously.
🌍 Orbit Context
LILACSAT 2 orbits at an average altitude of 412 km in a sun-synchronous orbit (SSO), a specialised subset of LEO where the orbital plane precesses to maintain a constant angle relative to the Sun. This provides consistent lighting conditions on every pass — essential for Earth observation, weather monitoring and environmental science. Within ±50 km of LILACSAT 2’s average altitude, there are currently 831 active payloads and 113 tracked debris or rocket body fragments — notable neighbours include STARLINK-1008, STARLINK-1012, STARLINK-1020. With an inclination of 97.5°, LILACSAT 2 passes over latitudes between 97.5°N and 97.5°S, providing near-global coverage including the polar regions. Polar and near-polar orbits are used for reconnaissance, weather monitoring and Earth-observation missions that need to image every part of the planet. China operates approximately 1,221 active satellites in total, of which 52 share a similar altitude band with LILACSAT 2.
❓ Frequently Asked Questions
LILACSAT 2 is in a sun-synchronous orbit (SSO), a specialised form of LEO at approximately 412 km altitude. Its 97.5° inclination causes the orbital plane to precess at exactly the rate of the Earth’s revolution around the Sun, so the satellite crosses each latitude at a consistent local solar time. It completes one orbit every 93 minutes, travelling at 27,598 km/h.
LILACSAT 2 is operated by Harbin Institute/China Amateur Satellite - CAMSAT (China). It is catalogued by the U.S. Space Surveillance Network under NORAD ID 40908. You can track LILACSAT 2 in real time on Orbital Radar’s live tracker or browse all operators in the operator directory.
LILACSAT 2 was launched on 2015-09-19 from Taiyuan, China. At its current altitude, the estimated remaining orbital lifetime is: ~1–3 years. View the full satellite launch log.
Yes — Orbital Radar tracks LILACSAT 2 (NORAD ID 40908) 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.
LILACSAT 2 travels at approximately 27,598 km/h (17,149 mph) — roughly 7.67 km/s. It completes 15.52 orbits per day, meaning the crew or instruments aboard (if any) would experience approximately 31 sunrises and sunsets every 24 hours.