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, 0.1 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 25260.71357987 .00003215 00000-0 15672-3 0 9996
2 62609 97.4188 338.8500 0007459 198.3504 161.7463 15.19015428 37299Epoch: 2025-09-17T17:07Z
TLE epoch observation values (Epoch: 2025-09-17T17:07:33.3Z)
Latitude
0°
Longitude
85.07567°
Altitude
516.783 km
Speed
7.602 km/s
True Right ascension
22h 35m 23s
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
13:03:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.917 km
Perigee altitude
500.648 km
Semi-major axis
6,883.92 km
Eccentricity
0.00075
Inclination
97.4188°
RAAN
338.85°
Arg. of periapsis
198.3504°
True anomaly
161.77305°
Mean anomaly
161.7463°
Eccentric anomaly
161.75968°
Mean motion
3.80005 °/min
Orbital period
94.74 mins
BSTAR
0.00015672
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-19 05:37:32.004Z | 189.81° SSW | 2025-09-19 05:39:32.004Z | 245.326° WSW | 38.408° | 2025-09-19 05:42:32.004Z | 334.414° NNW |
| 5 mins | 2025-09-19 18:42:32.004Z | 340.363° N | 2025-09-19 18:44:32.004Z | 288.228° WNW | 29.06° | 2025-09-19 18:47:32.004Z | 224.718° SW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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