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: 12 hours ago
TLE from 12 hours ago
0 LUOJIA-1 01
1 43485U 18048B 25340.56844891 .00005224 00000-0 59896-3 0 9997
2 43485 97.8300 56.8160 0009972 41.5667 318.6305 14.86291098405592Epoch: 2025-12-06T13:38Z
TLE epoch observation values (Epoch: 2025-12-06T13:38:33.985Z)
Latitude
-0.00005°
Longitude
136.58009°
Altitude
607.341 km
Speed
7.558 km/s
True Right ascension
03h 47m 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
00:07:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
613.531 km
Perigee altitude
599.6 km
Semi-major axis
6,984.703 km
Eccentricity
0.001
Inclination
97.83°
RAAN
56.816°
Arg. of periapsis
41.5667°
True anomaly
318.55491°
Mean anomaly
318.6305°
Eccentric anomaly
318.59271°
Mean motion
3.7181 °/min
Orbital period
96.82 mins
BSTAR
0.00059896
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-07 04:20:37.246Z | 105.644° ESE | 2025-12-07 04:22:37.246Z | 70.717° E | 19.797° | 2025-12-07 04:25:37.246Z | 21.641° NNE |
| 5 mins | 2025-12-07 05:56:37.246Z | 219.894° SW | 2025-12-07 05:58:37.246Z | 267.266° W | 27.024° | 2025-12-07 06:01:37.246Z | 321.471° NNW |
| 6 mins | 2025-12-07 17:41:37.246Z | 34.523° NE | 2025-12-07 17:44:37.246Z | 107.445° ESE | 33.963° | 2025-12-07 17:47:37.246Z | 166.223° S |
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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