LILACSAT 2, 40908
Orbit data source: Space-Track
LILACSAT 2, 40908 is a payload satellite owned by Harbin (CN) in SSO that was launched on Sat, 19 Sep 2015 UTC via a CHANG ZHENG 6 launch vehicle from the Taiyaun Space Center, China (TSC). 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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40908 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Harbin
Mission
Operational Amateur Com/Tech
Bus & Motor
CAS-3H, Unknown motor
Mass
11 kg wet, 11 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.060 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 LILACSAT 2
1 40908U 15049K 25338.76749535 .00028277 00000-0 61290-3 0 9994
2 40908 97.4915 3.9065 0006471 230.0961 129.9718 15.44367126565675Epoch: 2025-12-04T18:25Z
TLE epoch observation values (Epoch: 2025-12-04T18:25:11.598Z)
Latitude
-0.00009°
Longitude
13.78897°
Altitude
439.193 km
Speed
7.647 km/s
True Right ascension
00h 15m 37s
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
06:48:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
434.581 km
Perigee altitude
425.77 km
Semi-major axis
6,808.312 km
Eccentricity
0.00065
Inclination
97.4915°
RAAN
3.9065°
Arg. of periapsis
230.0961°
True anomaly
130.0286°
Mean anomaly
129.9718°
Eccentric anomaly
130.0002°
Mean motion
3.86353 °/min
Orbital period
93.18 mins
BSTAR
0.0006129
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Other satellites on launch #49 in the year 2015 (2015-09-19 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.LILACSAT 2 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-05 15:12:11.230Z | 339.93° N | 2025-12-05 15:14:11.230Z | 277.329° WNW | 28.457° | 2025-12-05 15:16:11.230Z | 228.031° WSW |
| 4 mins | 2025-12-06 01:40:11.230Z | 142.245° SSE | 2025-12-06 01:42:11.230Z | 45.794° ENE | 37.403° | 2025-12-06 01:44:11.230Z | 1.372° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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