LQSAT, 40958
Orbit data source: Space-Track
LQSAT, 40958 is a payload satellite owned by Changguang WJ (CN) in SSO that was launched on Wed, 07 Oct 2015 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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40958 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
HARB/CIOMP
Mission
Non-operational Commercial Imaging
Bus & Motor
JL-1, Unknown motor
Mass
50 kg wet, 50 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.320 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 LQSAT
1 40958U 15057A 26172.47396014 .00000519 00000-0 80804-4 0 9995
2 40958 97.6685 165.6370 0015376 258.0033 101.9455 14.76787685575944Epoch: 2026-06-21T11:22Z
TLE epoch observation values (Epoch: 2026-06-21T11:22:30.156Z)
Latitude
0.00005°
Longitude
85.33763°
Altitude
644.756 km
Speed
7.534 km/s
True Right ascension
11h 02m 32s
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
21:35:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
647.303 km
Perigee altitude
625.731 km
Semi-major axis
7,014.654 km
Eccentricity
0.00154
Inclination
97.6685°
RAAN
165.637°
Arg. of periapsis
258.0033°
True anomaly
102.11781°
Mean anomaly
101.9455°
Eccentric anomaly
102.03166°
Mean motion
3.69431 °/min
Orbital period
97.45 mins
BSTAR
0.000080804
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Other satellites on launch #57 in the year 2015 (2015-10-07 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.LQSAT 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-22 12:19:38.557Z | 15.094° NNE | 2026-06-22 12:23:38.557Z | 52.104° ENE | 43.475° | 2026-06-22 12:27:38.557Z | 187.808° SSW |
| 7 mins | 2026-06-22 23:16:38.557Z | 149.357° SSE | 2026-06-22 23:20:38.557Z | 46.792° ENE | 38.751° | 2026-06-22 23:23:38.557Z | 359.298° N |
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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