LING QIAO, 40136
Orbit data source: Space-Track
LING QIAO, 40136 is a payload satellite owned by Tsinghua (CN) in SSO that was launched on Thu, 04 Sep 2014 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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40136 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Tsinghua
Mission
Operational Amateur Communications
Bus & Motor
LQ, Unknown motor
Mass
135 kg wet, 135 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.0 m
Radar Cross Section
1.500 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 4 hours ago
TLE from 4 hours ago
0 LING QIAO
1 40136U 14051A 26062.91213759 -.00000018 00000-0 10031-4 0 9997
2 40136 98.7055 64.6288 0021755 119.9513 240.3832 14.30250467599954Epoch: 2026-03-03T21:53Z
TLE epoch observation values (Epoch: 2026-03-03T21:53:28.687Z)
Latitude
-0.00011°
Longitude
-65.42511°
Altitude
801.557 km
Speed
7.449 km/s
True Right ascension
04h 18m 30s
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
05:40:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
803.628 km
Perigee altitude
772.448 km
Semi-major axis
7,166.175 km
Eccentricity
0.00218
Inclination
98.7055°
RAAN
64.6288°
Arg. of periapsis
119.9513°
True anomaly
240.16677°
Mean anomaly
240.3832°
Eccentric anomaly
240.27495°
Mean motion
3.57777 °/min
Orbital period
100.62 mins
BSTAR
0.000010031
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Other satellites on launch #51 in the year 2014 (2014-09-04 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.LING QIAO 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 | 2026-03-04 11:55:19.961Z | 46.504° ENE | 2026-03-04 11:59:19.961Z | 102.603° ESE | 20.904° | 2026-03-04 12:02:19.961Z | 141.885° SSE |
| 7 mins | 2026-03-04 13:35:19.961Z | 349.255° N | 2026-03-04 13:38:19.961Z | 294.402° NW | 32.912° | 2026-03-04 13:42:19.961Z | 226.245° WSW |
| 7 mins | 2026-03-04 23:13:19.961Z | 122.623° SE | 2026-03-04 23:16:19.961Z | 75.407° E | 28.735° | 2026-03-04 23:20:19.961Z | 10.661° NNE |
| 7 mins | 2026-03-05 00:53:19.961Z | 218.662° SW | 2026-03-05 00:56:19.961Z | 268.854° W | 25.256° | 2026-03-05 01:00:19.961Z | 321.842° 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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