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: 7 hours ago
TLE from 7 hours ago
0 LUOJIA-1 01
1 43485U 18048B 26125.78668179 .00001963 00000-0 22447-3 0 9994
2 43485 97.8102 204.6591 0007438 259.1455 100.8925 14.87130369427913Epoch: 2026-05-05T18:52Z
TLE epoch observation values (Epoch: 2026-05-05T18:52:49.306Z)
Latitude
0.00005°
Longitude
57.79713°
Altitude
610.927 km
Speed
7.553 km/s
True Right ascension
13h 38m 38s
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
10:11:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
609.128 km
Perigee altitude
598.741 km
Semi-major axis
6,982.071 km
Eccentricity
0.00074
Inclination
97.8102°
RAAN
204.6591°
Arg. of periapsis
259.1455°
True anomaly
100.97618°
Mean anomaly
100.8925°
Eccentric anomaly
100.93434°
Mean motion
3.7202 °/min
Orbital period
96.77 mins
BSTAR
0.00022447
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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 | 2026-05-06 04:42:31.529Z | 132.572° SE | 2026-05-06 04:45:31.529Z | 69.376° E | 31.321° | 2026-05-06 04:48:31.529Z | 9.759° NNE |
| 6 mins | 2026-05-06 18:04:31.529Z | 16.666° NNE | 2026-05-06 18:06:31.529Z | 38.619° NE | 43.512° | 2026-05-06 18:10:31.529Z | 189.972° SSW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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