BEIDOU 3 M28, 58654
Orbit data source: Space-Track
BEIDOU 3 M28, 58654 is a payload satellite owned by CNSA (CN) in MEO that was launched on Tue, 26 Dec 2023 UTC via a CHANG ZHENG 3B/YZ-1 launch vehicle from the Xichang Space Center, China (XSC). 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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58654 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CAST
Mission
Operational Defense Navigation
Bus & Motor
BD-3M, Unknown motor
Mass
1,014 kg wet, ~850 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 5.0 m
Radar Cross Section
8.984 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 BEIDOU 3 M28
1 58654U 23207A 26172.05798505 -.00000081 00000-0 00000+0 0 9998
2 58654 55.7561 62.1723 0003138 350.0414 9.9905 1.86229753 16914Epoch: 2026-06-21T01:23Z
TLE epoch observation values (Epoch: 2026-06-21T01:23:29.908Z)
Latitude
0.00005°
Longitude
132.04932°
Altitude
21,519.848 km
Speed
3.781 km/s
True Right ascension
04h 08m 45s
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
21:30:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
21,536.911 km
Perigee altitude
21,519.397 km
Semi-major axis
27,906.291 km
Eccentricity
0.00031
Inclination
55.7561°
RAAN
62.1723°
Arg. of periapsis
350.0414°
True anomaly
9.99674°
Mean anomaly
9.9905°
Eccentric anomaly
9.99362°
Mean motion
0.46558 °/min
Orbital period
773.24 mins
BSTAR
0
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Other satellites on launch #207 in the year 2023 (2023-12-26 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.BEIDOU 3 M28 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. |
|---|---|---|---|---|---|---|---|
| 345 mins | 2026-06-22 14:55:54.711Z | 166.643° S | 2026-06-22 17:40:54.711Z | 96.088° ESE | 42.895° | 2026-06-22 20:40:54.711Z | 56.759° ENE |
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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