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 26149.51901729 .00000279 00000-0 12472-3 0 9998
2 40136 98.7050 151.2993 0019870 225.9664 133.9882 14.30268178612333Epoch: 2026-05-29T12:27Z
TLE epoch observation values (Epoch: 2026-05-29T12:27:23.093Z)
Latitude
-0.00003°
Longitude
77.40485°
Altitude
803.673 km
Speed
7.446 km/s
True Right ascension
10h 05m 11s
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
02:23:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
802.218 km
Perigee altitude
773.74 km
Semi-major axis
7,166.116 km
Eccentricity
0.00199
Inclination
98.705°
RAAN
151.2993°
Arg. of periapsis
225.9664°
True anomaly
134.15174°
Mean anomaly
133.9882°
Eccentric anomaly
134.07°
Mean motion
3.57781 °/min
Orbital period
100.62 mins
BSTAR
0.00012472
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-05-29 22:42:19.927Z | 92.232° ESE | 2026-05-29 22:44:19.927Z | 67.79° E | 15.704° | 2026-05-29 22:47:19.927Z | 30.029° NE |
| 8 mins | 2026-05-30 00:20:19.927Z | 181.068° SSW | 2026-05-30 00:23:19.927Z | 234.234° WSW | 41.733° | 2026-05-30 00:28:19.927Z | 339.18° N |
| 8 mins | 2026-05-30 12:33:19.927Z | 30.837° NE | 2026-05-30 12:37:19.927Z | 105.823° ESE | 36.094° | 2026-05-30 12:41:19.927Z | 170.18° S |
| 5 mins | 2026-05-30 14:14:19.927Z | 325.215° NNW | 2026-05-30 14:16:19.927Z | 295.179° NW | 19.972° | 2026-05-30 14:19:19.927Z | 254.583° W |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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