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: 2 days ago
TLE from 2 days ago
0 LUOJIA-1 01
1 43485U 18048B 25306.50000613 .00003250 00000-0 37756-3 0 9997
2 43485 97.8330 23.2710 0010130 140.9230 219.2719 14.86012503400538Epoch: 2025-11-02T12:00Z
TLE epoch observation values (Epoch: 2025-11-02T12:00:00.529Z)
Latitude
-0.00003°
Longitude
161.25395°
Altitude
618.926 km
Speed
7.546 km/s
True Right ascension
01h 33m 05s
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
19:57:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
614.516 km
Perigee altitude
600.363 km
Semi-major axis
6,985.576 km
Eccentricity
0.00101
Inclination
97.833°
RAAN
23.271°
Arg. of periapsis
140.923°
True anomaly
219.19849°
Mean anomaly
219.2719°
Eccentric anomaly
219.23519°
Mean motion
3.7174 °/min
Orbital period
96.84 mins
BSTAR
0.00037756
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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 | 2025-11-04 04:31:56.878Z | 129.148° SE | 2025-11-04 04:35:56.878Z | 59.938° ENE | 25.374° | 2025-11-04 04:38:56.878Z | 12.397° NNE |
| 4 mins | 2025-11-04 06:09:56.878Z | 235.16° WSW | 2025-11-04 06:11:56.878Z | 275.443° WNW | 20.703° | 2025-11-04 06:13:56.878Z | 308.699° NW |
| 6 mins | 2025-11-04 17:54:56.878Z | 26.267° NE | 2025-11-04 17:57:56.878Z | 133.619° SE | 39.783° | 2025-11-04 18:00:56.878Z | 179.707° 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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