PIESAT-2 12, 62336
Orbit data source: Space-Track
PIESAT-2 12, 62336 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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62336 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: 8 hours ago
TLE from 8 hours ago
0 PIESAT-2 12
1 62336U 24241D 26171.50576192 .00006312 00000-0 34982-3 0 9996
2 62336 97.5239 118.9510 0001664 95.1301 265.0121 15.14147455 83306Epoch: 2026-06-20T12:08Z
TLE epoch observation values (Epoch: 2026-06-20T12:08:17.829Z)
Latitude
-0°
Longitude
28.1573°
Altitude
526.747 km
Speed
7.6 km/s
True Right ascension
07h 55m 48s
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
07:12:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
521.695 km
Perigee altitude
519.399 km
Semi-major axis
6,898.684 km
Eccentricity
0.00017
Inclination
97.5239°
RAAN
118.951°
Arg. of periapsis
95.1301°
True anomaly
264.9931°
Mean anomaly
265.0121°
Eccentric anomaly
265.0026°
Mean motion
3.78786 °/min
Orbital period
95.04 mins
BSTAR
0.00034982
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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 12 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 | 2026-06-21 09:19:32.402Z | 15.866° NNE | 2026-06-21 09:22:32.402Z | 144.382° SSE | 44.071° | 2026-06-21 09:25:32.402Z | 188.606° SSW |
| 5 mins | 2026-06-21 20:00:32.402Z | 123.855° SE | 2026-06-21 20:02:32.402Z | 75.094° E | 28.303° | 2026-06-21 20:05:32.402Z | 11.399° NNE |
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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