BEIDOU 3M25, 61186
Orbit data source: Space-Track
BEIDOU 3M25, 61186 is a payload satellite owned by CNSA (CN) in MEO that was launched on Thu, 19 Sep 2024 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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61186 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
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 BEIDOU 3M25
1 61186U 24168B 26170.87388850 -.00000088 00000-0 00000-0 0 9993
2 61186 54.4707 302.1484 0003007 300.7544 238.5226 1.86230002 11839Epoch: 2026-06-19T20:58Z
TLE epoch observation values (Epoch: 2026-06-19T20:58:23.966Z)
Latitude
0.5686°
Longitude
-100.97062°
Altitude
21,532.736 km
Speed
3.779 km/s
True Right ascension
08h 06m 54s
True Declination
0° 34' 04"
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
07:24:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
21,536.57 km
Perigee altitude
21,519.787 km
Semi-major axis
27,906.316 km
Eccentricity
0.0003
Inclination
54.4707°
RAAN
302.1484°
Arg. of periapsis
300.7544°
True anomaly
238.49322°
Mean anomaly
238.5226°
Eccentric anomaly
238.50791°
Mean motion
0.46557 °/min
Orbital period
773.24 mins
BSTAR
0
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Other satellites on launch #168 in the year 2024 (2024-09-19 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 3M25 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. |
|---|---|---|---|---|---|---|---|
| 202 mins | 2026-06-20 20:28:37.890Z | 297.401° NW | 2026-06-20 21:10:37.890Z | 266.98° W | 40.794° | 2026-06-20 23:50:37.890Z | 201.024° SSW |
| 200 mins | 2026-06-21 05:15:37.890Z | 109.796° ESE | 2026-06-21 06:57:37.890Z | 69.609° E | 24.747° | 2026-06-21 08:35:37.890Z | 37.622° NE |
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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