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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67481 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CAST
Mission
Civil Spaceship
Bus & Motor
SHENZHOU OM, Unknown motor
Mass
~1,842 kg wet, ~1,500 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl + 2 Pan, 14.5 m
Radar Cross Section
9.277 m²
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 SZ-20 MODULE
1 67481U 25082C 26091.22603824 .00027727 00000-0 27304-3 0 9992
2 67481 41.4778 69.0763 0008818 158.0436 202.0784 15.65294825281159Epoch: 2026-04-01T05:25Z
TLE epoch observation values (Epoch: 2026-04-01T05:25:29.703Z)
Latitude
-0.00003°
Longitude
158.11059°
Altitude
377.507 km
Speed
7.682 km/s
True Right ascension
04h 36m 18s
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
19:16:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
380.581 km
Perigee altitude
368.672 km
Semi-major axis
6,752.764 km
Eccentricity
0.00088
Inclination
41.4778°
RAAN
69.0763°
Arg. of periapsis
158.0436°
True anomaly
202.04046°
Mean anomaly
202.0784°
Eccentric anomaly
202.05943°
Mean motion
3.9113 °/min
Orbital period
92.04 mins
BSTAR
0.00027304
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Other satellites on launch #82 in the year 2025 (2025-04-24 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.SZ-20 MODULE 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-04-02 01:32:35.229Z | 194.82° SSW | 2026-04-02 01:34:35.229Z | 144.696° SSE | 20.106° | 2026-04-02 01:36:35.229Z | 100.706° ESE |
| 4 mins | 2026-04-02 03:09:35.229Z | 252.885° W | 2026-04-02 03:10:35.229Z | 232.562° WSW | 44.598° | 2026-04-02 03:13:35.229Z | 77.502° E |
| 4 mins | 2026-04-02 04:45:35.229Z | 285.648° WNW | 2026-04-02 04:47:35.229Z | 29.842° NE | 41.089° | 2026-04-02 04:49:35.229Z | 82.686° E |
| 4 mins | 2026-04-02 06:22:35.229Z | 268.332° W | 2026-04-02 06:23:35.229Z | 234.412° WSW | 38.21° | 2026-04-02 06:26:35.229Z | 121.167° SE |
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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