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 26035.88182194 .00002728 00000-0 31284-3 0 9992
2 43485 97.8208 116.1986 0008856 189.2281 170.8773 14.86691039414559Epoch: 2026-02-04T21:09Z
TLE epoch observation values (Epoch: 2026-02-04T21:09:49.415Z)
Latitude
-0.00008°
Longitude
23.70068°
Altitude
617.426 km
Speed
7.547 km/s
True Right ascension
07h 44m 47s
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
04:37:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
611.496 km
Perigee altitude
599.127 km
Semi-major axis
6,983.448 km
Eccentricity
0.00089
Inclination
97.8208°
RAAN
116.1986°
Arg. of periapsis
189.2281°
True anomaly
170.89337°
Mean anomaly
170.8773°
Eccentric anomaly
170.88534°
Mean motion
3.7191 °/min
Orbital period
96.8 mins
BSTAR
0.00031284
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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 | 2026-02-05 05:20:58.527Z | 171.607° S | 2026-02-05 05:24:58.527Z | 223.374° SW | 43.809° | 2026-02-05 05:28:58.527Z | 343.757° N |
| 4 mins | 2026-02-05 17:08:58.527Z | 61.317° ENE | 2026-02-05 17:10:58.527Z | 95.227° ESE | 17.437° | 2026-02-05 17:12:58.527Z | 128.208° SE |
| 5 mins | 2026-02-05 18:44:58.527Z | 335.592° NNW | 2026-02-05 18:46:58.527Z | 284.691° WNW | 29.63° | 2026-02-05 18:49:58.527Z | 228.167° 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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