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: 16 hours ago
TLE from 16 hours ago
0 BUZZZER-1
1 62609U 25009A 25311.16360705 .00005112 00000-0 24324-3 0 9996
2 62609 97.4146 28.3863 0008776 42.3363 317.8547 15.19573694 44952Epoch: 2025-11-07T03:55Z
TLE epoch observation values (Epoch: 2025-11-07T03:55:35.649Z)
Latitude
-0.00007°
Longitude
-77.12374°
Altitude
505.739 km
Speed
7.614 km/s
True Right ascension
01h 53m 32s
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
16:28:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.135 km
Perigee altitude
498.055 km
Semi-major axis
6,882.232 km
Eccentricity
0.00088
Inclination
97.4146°
RAAN
28.3863°
Arg. of periapsis
42.3363°
True anomaly
317.78716°
Mean anomaly
317.8547°
Eccentric anomaly
317.82094°
Mean motion
3.80145 °/min
Orbital period
94.7 mins
BSTAR
0.00024324
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-08 05:20:07.931Z | 167.767° S | 2025-11-08 05:23:07.931Z | 177.537° S | 44.501° | 2025-11-08 05:26:07.931Z | 347.377° N |
| 5 mins | 2025-11-08 18:26:07.931Z | 351.481° N | 2025-11-08 18:28:07.931Z | 267.042° W | 38.881° | 2025-11-08 18:31:07.931Z | 208.354° 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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