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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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: 22 hours ago
TLE from 22 hours ago
0 LUOJIA-1 01
1 43485U 18048B 26172.54728794 .00001214 00000-0 14046-3 0 9995
2 43485 97.8097 250.6653 0010346 105.1393 255.0969 14.87296847434866Epoch: 2026-06-21T13:08Z
TLE epoch observation values (Epoch: 2026-06-21T13:08:05.678Z)
Latitude
0.00007°
Longitude
143.89564°
Altitude
611.286 km
Speed
7.553 km/s
True Right ascension
16h 42m 39s
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
21:44:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
610.636 km
Perigee altitude
596.19 km
Semi-major axis
6,981.55 km
Eccentricity
0.00103
Inclination
97.8097°
RAAN
250.6653°
Arg. of periapsis
105.1393°
True anomaly
254.98237°
Mean anomaly
255.0969°
Eccentric anomaly
255.03963°
Mean motion
3.72062 °/min
Orbital period
96.76 mins
BSTAR
0.00014046
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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 | 2026-06-22 17:10:35.255Z | 54.106° ENE | 2026-06-22 17:12:35.255Z | 86.312° E | 18.384° | 2026-06-22 17:15:35.255Z | 136.472° SSE |
| 6 mins | 2026-06-22 18:46:35.255Z | 339.383° N | 2026-06-22 18:48:35.255Z | 297.594° NW | 27.767° | 2026-06-22 18:52:35.255Z | 226.346° WSW |
| 6 mins | 2026-06-23 05:38:35.255Z | 199.043° SSW | 2026-06-23 05:40:35.255Z | 256.249° W | 36.529° | 2026-06-23 05:44:35.255Z | 335.082° 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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