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: 20 hours ago
TLE from 20 hours ago
0 BUZZZER-1
1 62609U 25009A 25294.76612068 .00006037 00000-0 28799-3 0 9991
2 62609 97.4162 12.2841 0009429 91.2643 268.9672 15.19409872 42463Epoch: 2025-10-21T18:23Z
TLE epoch observation values (Epoch: 2025-10-21T18:23:12.826Z)
Latitude
-0.00005°
Longitude
66.03129°
Altitude
510.835 km
Speed
7.608 km/s
True Right ascension
00h 49m 08s
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
09:47:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
511.08 km
Perigee altitude
498.1 km
Semi-major axis
6,882.727 km
Eccentricity
0.00094
Inclination
97.4162°
RAAN
12.2841°
Arg. of periapsis
91.2643°
True anomaly
268.85917°
Mean anomaly
268.9672°
Eccentric anomaly
268.91319°
Mean motion
3.80104 °/min
Orbital period
94.71 mins
BSTAR
0.00028799
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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 | 2025-10-22 18:40:21.932Z | 336.876° NNW | 2025-10-22 18:42:21.932Z | 274.918° WNW | 29.786° | 2025-10-22 18:45:21.932Z | 220.664° SW |
| 5 mins | 2025-10-23 05:18:21.932Z | 162.618° S | 2025-10-23 05:20:21.932Z | 20.376° NNE | 44.32° | 2025-10-23 05:23:21.932Z | 349.951° N |
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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