PIESAT-2 10, 62334
Orbit data source: Space-Track
PIESAT-2 10, 62334 is a payload satellite owned by Hangtian Hongtu (CN) in SSO that was launched on Mon, 16 Dec 2024 UTC via a CHANG ZHENG 2D 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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62334 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Yinhe
Mission
Operational Commercial Radar Imaging
Bus & Motor
PIESAT, Unknown motor
Mass
270 kg wet, 270 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 2.0 m
Radar Cross Section
2.315 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 PIESAT-2 10
1 62334U 24241B 26171.54211411 .00007410 00000-0 40868-3 0 9998
2 62334 97.5339 119.5654 0001860 80.5138 279.6304 15.14258064 83319Epoch: 2026-06-20T13:00Z
TLE epoch observation values (Epoch: 2026-06-20T13:00:38.659Z)
Latitude
0.00002°
Longitude
15.64907°
Altitude
526.096 km
Speed
7.6 km/s
True Right ascension
07h 58m 15s
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
07:12:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
521.494 km
Perigee altitude
518.928 km
Semi-major axis
6,898.348 km
Eccentricity
0.00019
Inclination
97.5339°
RAAN
119.5654°
Arg. of periapsis
80.5138°
True anomaly
279.60939°
Mean anomaly
279.6304°
Eccentric anomaly
279.61989°
Mean motion
3.78814 °/min
Orbital period
95.03 mins
BSTAR
0.00040868
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Other satellites on launch #241 in the year 2024 (2024-12-16 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.PIESAT-2 10 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-20 21:03:37.662Z | 195.17° SSW | 2026-06-20 21:06:37.662Z | 255.234° W | 31.002° | 2026-06-20 21:09:37.662Z | 325.992° NNW |
| 4 mins | 2026-06-21 08:38:37.662Z | 69.773° E | 2026-06-21 08:39:37.662Z | 91.5° ESE | 19.593° | 2026-06-21 08:42:37.662Z | 144.854° SSE |
| 4 mins | 2026-06-21 10:12:37.662Z | 320.371° NNW | 2026-06-21 10:13:37.662Z | 297.276° NW | 22.075° | 2026-06-21 10:16:37.662Z | 238.618° WSW |
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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