PIESAT-2 09, 62333
Orbit data source: Space-Track
PIESAT-2 09, 62333 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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62333 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
320 kg wet, 320 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: 9 hours ago
TLE from 9 hours ago
0 PIESAT-2 09
1 62333U 24241A 26171.52282248 .00007321 00000-0 40423-3 0 9999
2 62333 97.5301 119.1565 0002475 94.2064 265.9451 15.14224457 83306Epoch: 2026-06-20T12:32Z
TLE epoch observation values (Epoch: 2026-06-20T12:32:51.862Z)
Latitude
0.00004°
Longitude
22.20417°
Altitude
526.534 km
Speed
7.6 km/s
True Right ascension
07h 56m 37s
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
08:33:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
522.02 km
Perigee altitude
518.606 km
Semi-major axis
6,898.45 km
Eccentricity
0.00025
Inclination
97.5301°
RAAN
119.1565°
Arg. of periapsis
94.2064°
True anomaly
265.91681°
Mean anomaly
265.9451°
Eccentric anomaly
265.93096°
Mean motion
3.78805 °/min
Orbital period
95.04 mins
BSTAR
0.00040423
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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 09 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 | 2026-06-21 09:43:09.714Z | 359.959° N | 2026-06-21 09:46:09.714Z | 308.451° NW | 36.315° | 2026-06-21 09:50:09.714Z | 210.508° SW |
| 6 mins | 2026-06-21 20:24:09.714Z | 154.664° SSE | 2026-06-21 20:27:09.714Z | 37.325° NE | 41.044° | 2026-06-21 20:30:09.714Z | 354.504° N |
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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