LUOJIA-1 01, 43485
Orbit data source: Space-Track
LUOJIA-1 01, 43485 is a payload satellite owned by Wuhan daxue (CN) in SSO that was launched on Sat, 02 Jun 2018 UTC via a CHANG ZHENG 2D launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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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43485 intel report (Beta)
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LUOJIA-1 01 radio frequencies
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Wuhan daxue
Mission
Operational Amateur Imaging
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, 10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 0.3 m
Radar Cross Section
0.092 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 LUOJIA-1 01
1 43485U 18048B 25258.55102787 .00002343 00000-0 27667-3 0 9995
2 43485 97.8367 336.0643 0008065 308.4361 51.6129 14.85629700393411Epoch: 2025-09-15T13:13Z
TLE epoch observation values (Epoch: 2025-09-15T13:13:28.807Z)
Latitude
-0.00012°
Longitude
142.94023°
Altitude
611.143 km
Speed
7.556 km/s
True Right ascension
22h 24m 15s
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
15:10:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
614.275 km
Perigee altitude
603.006 km
Semi-major axis
6,986.778 km
Eccentricity
0.00081
Inclination
97.8367°
RAAN
336.0643°
Arg. of periapsis
308.4361°
True anomaly
51.68539°
Mean anomaly
51.6129°
Eccentric anomaly
51.64914°
Mean motion
3.71645 °/min
Orbital period
96.87 mins
BSTAR
0.00027667
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Other satellites on launch #48 in the year 2018 (2018-06-02 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.LUOJIA-1 01 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-16 05:31:46.029Z | 186.885° SSW | 2025-09-16 05:33:46.029Z | 239.075° WSW | 40.608° | 2025-09-16 05:37:46.029Z | 338.76° N |
| 4 mins | 2025-09-16 17:18:46.029Z | 64.398° ENE | 2025-09-16 17:20:46.029Z | 104.886° ESE | 21.159° | 2025-09-16 17:22:46.029Z | 138.535° SSE |
| 6 mins | 2025-09-16 18:53:46.029Z | 338.524° N | 2025-09-16 18:55:46.029Z | 301.919° NW | 25.158° | 2025-09-16 18:59:46.029Z | 231.849° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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