BUZZZER-1, 62609
Orbit data source: Space-Track
BUZZZER-1, 62609 is a payload satellite owned by Unseen Labs (FR) in SSO that was launched on Tue, 14 Jan 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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62609 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
FRRelated business
Manufacturer
Unseen Labs
Mission
Operational Commercial Sigint
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.3 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 BUZZZER-1
1 62609U 25009A 25324.66196910 .00003377 00000-0 16100-3 0 9994
2 62609 97.4139 41.6433 0007585 357.6723 2.4476 15.19752999 47008Epoch: 2025-11-20T15:53Z
TLE epoch observation values (Epoch: 2025-11-20T15:53:14.130Z)
Latitude
0.00006°
Longitude
103.41828°
Altitude
504.458 km
Speed
7.615 km/s
True Right ascension
02h 46m 34s
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
17:03:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
508.773 km
Perigee altitude
498.333 km
Semi-major axis
6,881.69 km
Eccentricity
0.00076
Inclination
97.4139°
RAAN
41.6433°
Arg. of periapsis
357.6723°
True anomaly
2.45132°
Mean anomaly
2.4476°
Eccentric anomaly
2.44946°
Mean motion
3.8019 °/min
Orbital period
94.69 mins
BSTAR
0.000161
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Other satellites on launch #9 in the year 2025 (2025-01-14 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.BUZZZER-1 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 | 2025-11-22 04:23:10.585Z | 106.472° ESE | 2025-11-22 04:25:10.585Z | 71.605° E | 16.243° | 2025-11-22 04:27:10.585Z | 34.396° NE |
| 5 mins | 2025-11-22 05:57:10.585Z | 217.853° SW | 2025-11-22 05:59:10.585Z | 268.972° W | 25.397° | 2025-11-22 06:02:10.585Z | 324.371° NNW |
| 4 mins | 2025-11-22 17:28:10.585Z | 63.574° ENE | 2025-11-22 17:29:10.585Z | 86.916° E | 22.138° | 2025-11-22 17:32:10.585Z | 147.81° SSE |
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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