TIANHUI 1-03, 40988 (Decayed)
Orbit data source: Space-Track
TIANHUI 1-03, 40988 was a payload satellite owned by G. Cehui dili (CN) in LEO that was launched on Mon, 26 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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40988 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
DFH
Mission
Decayed Civil Imaging
Bus & Motor
CAST-2000?, Unknown motor
Mass
~1,000 kg wet, ~1,000 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.5 m
Radar Cross Section
2.045 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 3 weeks ago
TLE from 3 weeks ago
0 TIANHUI 1-03
1 40988U 15061A 25268.37930935 .09055814 26555-5 22840-3 0 9993
2 40988 97.5071 68.4308 0011155 257.2829 102.7227 16.45126035553420Epoch: 2025-09-25T09:06Z
TLE epoch observation values (Epoch: 2025-09-25T09:06:12.327Z)
Latitude
0.00004°
Longitude
-72.56185°
Altitude
157.069 km
Speed
7.811 km/s
True Right ascension
04h 33m 43s
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
03:24:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
156.289 km
Perigee altitude
141.727 km
Semi-major axis
6,527.145 km
Eccentricity
0.00112
Inclination
97.5071°
RAAN
68.4308°
Arg. of periapsis
257.2829°
True anomaly
102.84735°
Mean anomaly
102.7227°
Eccentric anomaly
102.78503°
Mean motion
4.11584 °/min
Orbital period
87.47 mins
BSTAR
0.0002284
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Other satellites on launch #61 in the year 2015 (2015-10-26 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.TIANHUI 1-03 Visibility
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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. |
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| This satellite is decayed. |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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