LINGQIAO VIDEO B, 40960
Orbit data source: Space-Track
LINGQIAO VIDEO B, 40960 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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40960 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
HARB/CIOMP
Mission
Operational Commercial Imaging
Bus & Motor
JL-1, Unknown motor
Mass
95 kg wet, 95 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.0 m
Radar Cross Section
2.000 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 LINGQIAO VIDEO B
1 40960U 15057C 26283.93680170 .00000385 00000-0 60561-4 0 9990
2 40960 97.6690 274.2322 0015360 252.1715 107.7821 14.77624109592540Epoch: 2026-10-10T22:28Z
TLE epoch observation values (Epoch: 2026-10-10T22:28:59.666Z)
Latitude
-0.00004°
Longitude
-82.55318°
Altitude
643.165 km
Speed
7.535 km/s
True Right ascension
18h 16m 55s
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
03:36:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
644.638 km
Perigee altitude
623.097 km
Semi-major axis
7,012.005 km
Eccentricity
0.00154
Inclination
97.669°
RAAN
274.2322°
Arg. of periapsis
252.1715°
True anomaly
107.94961°
Mean anomaly
107.7821°
Eccentric anomaly
107.86586°
Mean motion
3.69641 °/min
Orbital period
97.39 mins
BSTAR
0.000060561
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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.LINGQIAO VIDEO B 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 | 2026-10-11 12:03:24.968Z | 22.689° NE | 2026-10-11 12:07:24.968Z | 113.961° SE | 56.133° | 2026-10-11 12:11:24.968Z | 178.921° S |
| 6 mins | 2026-10-11 23:00:24.968Z | 131.617° SE | 2026-10-11 23:03:24.968Z | 57.302° ENE | 40.439° | 2026-10-11 23:06:24.968Z | 6.545° NNE |
| 4 mins | 2026-10-12 00:38:24.968Z | 247.586° W | 2026-10-12 00:39:24.968Z | 263.774° W | 17.23° | 2026-10-12 00:42:24.968Z | 307.417° NW |
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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