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: 6 hours ago
TLE from 6 hours ago
0 LUOJIA-1 01
1 43485U 18048B 26305.87300078 .00000460 00000-0 56413-4 0 9997
2 43485 97.7998 21.8013 0009694 36.2149 323.9722 14.87680541454682Epoch: 2026-11-01T20:57Z
TLE epoch observation values (Epoch: 2026-11-01T20:57:07.267Z)
Latitude
-0.00002°
Longitude
26.36289°
Altitude
602.746 km
Speed
7.561 km/s
True Right ascension
01h 27m 12s
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
22:27:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
608.978 km
Perigee altitude
595.444 km
Semi-major axis
6,980.348 km
Eccentricity
0.00097
Inclination
97.7998°
RAAN
21.8013°
Arg. of periapsis
36.2149°
True anomaly
323.9068°
Mean anomaly
323.9722°
Eccentric anomaly
323.93951°
Mean motion
3.72158 °/min
Orbital period
96.73 mins
BSTAR
0.000056413
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-11-02 05:08:51.129Z | 161.848° S | 2026-11-02 05:11:51.129Z | 134.708° SE | 71.215° | 2026-11-02 05:15:51.129Z | 350.455° N |
| 6 mins | 2026-11-02 18:30:51.129Z | 351.524° N | 2026-11-02 18:33:51.129Z | 267.205° W | 44.953° | 2026-11-02 18:36:51.129Z | 216.503° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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