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SZ-20 MODULE, 67481

Orbit data source: Space-Track

SZ-20 MODULE, 67481 is a payload satellite owned by ZZHGB (CN) in LEO that was launched on Thu, 24 Apr 2025 UTC launched 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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Identifier
67481, 2025-082C
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
CAST
Mission
Spacecraft
Bus & Motor
SHENZHOU OM, Unknown motor
Mass
~1,842 kg wet, ~1,500 kg dry
Launch date (UTC)
2025-04-24 (10 months ago)
Launch vehicle
Unknown
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 SZ-20 MODULE
1 67481U 25082C   26042.24751114  .00027909  00000-0  30508-3 0  9998
2 67481  41.4802   8.5083 0007222 155.9859 204.1318 15.62660831273487
Epoch: 2026-02-11T05:56Z
TLE epoch observation values (Epoch: 2026-02-11T05:56:24.962Z)
Latitude
-0.00006°
Longitude
138.08787°
Altitude
384.029 km
Speed
7.679 km/s
True Right ascension
00h 34m 01s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
19:42:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
387.09 km
Perigee altitude
377.325 km
Semi-major axis
6,760.344 km
Eccentricity
0.00072
Inclination
41.4802°
RAAN
8.5083°
Arg. of periapsis
155.9859°
True anomaly
204.09799°
Mean anomaly
204.1318°
Eccentric anomaly
204.11489°
Mean motion
3.90472 °/min
Orbital period
92.2 mins
BSTAR
0.00030508
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Other satellites on launch #82 in the year 2025 (2025-04-24 UTC)

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