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: 5 hours ago
TLE from 5 hours ago
0 LUOJIA-1 01
1 43485U 18048B 25310.87676919 .00003994 00000-0 46217-3 0 9997
2 43485 97.8325 27.5805 0010338 128.0146 232.2004 14.86044626401182Epoch: 2025-11-06T21:02Z
TLE epoch observation values (Epoch: 2025-11-06T21:02:32.858Z)
Latitude
-0.00003°
Longitude
25.6148°
Altitude
617.774 km
Speed
7.548 km/s
True Right ascension
01h 50m 19s
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
21:57:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
614.56 km
Perigee altitude
600.117 km
Semi-major axis
6,985.476 km
Eccentricity
0.00103
Inclination
97.8325°
RAAN
27.5805°
Arg. of periapsis
128.0146°
True anomaly
232.10687°
Mean anomaly
232.2004°
Eccentric anomaly
232.15363°
Mean motion
3.71748 °/min
Orbital period
96.84 mins
BSTAR
0.00046217
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-11-07 05:14:11.802Z | 165.539° S | 2025-11-07 05:18:11.802Z | 92.368° ESE | 44.982° | 2025-11-07 05:22:11.802Z | 348.085° N |
| 5 mins | 2025-11-07 18:38:11.802Z | 342.322° N | 2025-11-07 18:40:11.802Z | 287.473° WNW | 33.592° | 2025-11-07 18:43:11.802Z | 222.895° SW |
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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