GAOFEN 8, 40701
Orbit data source: Space-Track
GAOFEN 8, 40701 is a payload satellite owned by PLA GAD (CN) in SSO that was launched on Fri, 26 Jun 2015 UTC via a CHANG ZHENG 4B launch vehicle from the Taiyaun Space Center, China (TSC). 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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40701 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CAST
Mission
Operational Defense Imaging
Bus & Motor
YW-5?, Unknown motor
Mass
~2,400 kg wet, ~2,400 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 4.0 m
Radar Cross Section
9.231 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 GAOFEN 8
1 40701U 15030A 25261.00219557 .00011214 00000-0 33469-3 0 9993
2 40701 97.6944 75.2215 0012564 89.5835 270.6847 15.34733105569546Epoch: 2025-09-18T00:03Z
TLE epoch observation values (Epoch: 2025-09-18T00:03:09.697Z)
Latitude
-0°
Longitude
77.26105°
Altitude
464.723 km
Speed
7.634 km/s
True Right ascension
05h 00m 53s
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
01:32:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
467.262 km
Perigee altitude
450.082 km
Semi-major axis
6,836.809 km
Eccentricity
0.00126
Inclination
97.6944°
RAAN
75.2215°
Arg. of periapsis
89.5835°
True anomaly
270.54073°
Mean anomaly
270.6847°
Eccentric anomaly
270.61272°
Mean motion
3.8394 °/min
Orbital period
93.76 mins
BSTAR
0.00033469
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Other satellites on launch #30 in the year 2015 (2015-06-26 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.GAOFEN 8 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 | 2025-09-18 11:08:37.782Z | 129.12° SE | 2025-09-18 11:11:37.782Z | 61.648° ENE | 24.427° | 2025-09-18 11:13:37.782Z | 18.157° NNE |
| 4 mins | 2025-09-19 00:06:37.782Z | 54.153° ENE | 2025-09-19 00:07:37.782Z | 81.851° E | 26.596° | 2025-09-19 00:10:37.782Z | 158.123° S |
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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