LILIUM-1, 58467
Orbit data source: Space-Track
LILIUM-1, 58467 is a Taiwanese payload satellite in SSO that was launched on Fri, 01 Dec 2023 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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58467 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
TW / TWNRelated business
Manufacturer
NCKU
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 LILIUM-1
1 58467U 23185F 25306.54077822 .00047399 00000-0 96440-3 0 9998
2 58467 97.3602 16.8608 0006389 291.9516 68.1054 15.46118854107114Epoch: 2025-11-02T12:58Z
TLE epoch observation values (Epoch: 2025-11-02T12:58:43.238Z)
Latitude
-0.00001°
Longitude
140.12561°
Altitude
429.6 km
Speed
7.655 km/s
True Right ascension
01h 07m 26s
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
23:56:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
429.368 km
Perigee altitude
420.675 km
Semi-major axis
6,803.159 km
Eccentricity
0.00064
Inclination
97.3602°
RAAN
16.8608°
Arg. of periapsis
291.9516°
True anomaly
68.17335°
Mean anomaly
68.1054°
Eccentric anomaly
68.13937°
Mean motion
3.86792 °/min
Orbital period
93.07 mins
BSTAR
0.0009644
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Other satellites on launch #185 in the year 2023 (2023-12-01 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.LILIUM-1 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-03 04:38:34.452Z | 151.15° SSE | 2025-11-03 04:41:34.452Z | 48.777° ENE | 37.732° | 2025-11-03 04:43:34.452Z | 1.593° NNE |
| 5 mins | 2025-11-03 17:30:34.452Z | 27.21° NE | 2025-11-03 17:32:34.452Z | 108.75° ESE | 40.029° | 2025-11-03 17:35:34.452Z | 180.255° SSW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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