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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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: 8 hours ago
TLE from 8 hours ago
0 LUOJIA-1 01
1 43485U 18048B 25359.95661014 .00002072 00000-0 24084-3 0 9993
2 43485 97.8271 75.9060 0008620 338.6918 21.3938 14.86401142408471Epoch: 2025-12-25T22:57Z
TLE epoch observation values (Epoch: 2025-12-25T22:57:31.116Z)
Latitude
0.00005°
Longitude
-3.17786°
Altitude
606.615 km
Speed
7.559 km/s
True Right ascension
05h 03m 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
06:11:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
612.241 km
Perigee altitude
600.2 km
Semi-major axis
6,984.357 km
Eccentricity
0.00086
Inclination
97.8271°
RAAN
75.906°
Arg. of periapsis
338.6918°
True anomaly
21.42987°
Mean anomaly
21.3938°
Eccentric anomaly
21.41183°
Mean motion
3.71838 °/min
Orbital period
96.82 mins
BSTAR
0.00024084
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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 | 2025-12-26 17:18:31.155Z | 41.951° NE | 2025-12-26 17:21:31.155Z | 88.589° E | 22.177° | 2025-12-26 17:24:31.155Z | 142.775° SSE |
| 5 mins | 2025-12-26 18:55:31.155Z | 333.674° NNW | 2025-12-26 18:57:31.155Z | 293.866° NW | 24.604° | 2025-12-26 19:00:31.155Z | 238.974° WSW |
| 4 mins | 2025-12-27 04:12:31.155Z | 95.321° ESE | 2025-12-27 04:14:31.155Z | 61.757° ENE | 16.705° | 2025-12-27 04:16:31.155Z | 30.744° NE |
| 6 mins | 2025-12-27 05:47:31.155Z | 205.069° SW | 2025-12-27 05:49:31.155Z | 249.508° W | 31.523° | 2025-12-27 05:53:31.155Z | 329.551° NNW |
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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