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: 10 hours ago
TLE from 10 hours ago
0 LUOJIA-1 01
1 43485U 18048B 26256.30007369 .00001307 00000-0 14988-3 0 9998
2 43485 97.8051 333.0607 0008682 182.5766 177.5407 14.87545245447312Epoch: 2026-09-13T07:12Z
TLE epoch observation values (Epoch: 2026-09-13T07:12:06.366Z)
Latitude
-0.00005°
Longitude
-127.26252°
Altitude
614.702 km
Speed
7.548 km/s
True Right ascension
22h 12m 14s
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
09:54:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
608.695 km
Perigee altitude
596.574 km
Semi-major axis
6,980.772 km
Eccentricity
0.00087
Inclination
97.8051°
RAAN
333.0607°
Arg. of periapsis
182.5766°
True anomaly
177.54496°
Mean anomaly
177.5407°
Eccentric anomaly
177.54283°
Mean motion
3.72124 °/min
Orbital period
96.74 mins
BSTAR
0.00014988
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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 | 2026-09-13 17:27:28.586Z | 33.562° NE | 2026-09-13 17:31:28.586Z | 104.687° ESE | 31.322° | 2026-09-13 17:34:28.586Z | 156.928° SSE |
| 4 mins | 2026-09-13 19:05:28.586Z | 318.243° NNW | 2026-09-13 19:06:28.586Z | 299.658° NW | 20.61° | 2026-09-13 19:09:28.586Z | 248.988° W |
| 4 mins | 2026-09-14 04:21:28.586Z | 97.648° ESE | 2026-09-14 04:23:28.586Z | 57.876° ENE | 22.072° | 2026-09-14 04:25:28.586Z | 25.202° NE |
| 5 mins | 2026-09-14 05:56:28.586Z | 217.025° SW | 2026-09-14 05:58:28.586Z | 258.738° W | 29.714° | 2026-09-14 06:01:28.586Z | 317.51° 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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