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: 21 hours ago
TLE from 21 hours ago
0 BUZZZER-1
1 62609U 25009A 25260.18658574 .00003102 00000-0 15138-3 0 9995
2 62609 97.4187 338.3326 0007406 200.4256 159.6683 15.19011487 37213Epoch: 2025-09-17T04:28Z
TLE epoch observation values (Epoch: 2025-09-17T04:28:41.007Z)
Latitude
-0.0001°
Longitude
-85.20439°
Altitude
516.7 km
Speed
7.603 km/s
True Right ascension
22h 33m 19s
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
17:55:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.893 km
Perigee altitude
500.696 km
Semi-major axis
6,883.932 km
Eccentricity
0.00074
Inclination
97.4187°
RAAN
338.3326°
Arg. of periapsis
200.4256°
True anomaly
159.69776°
Mean anomaly
159.6683°
Eccentric anomaly
159.68303°
Mean motion
3.80004 °/min
Orbital period
94.74 mins
BSTAR
0.00015138
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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 | 2025-09-18 04:20:56.993Z | 104.038° ESE | 2025-09-18 04:22:56.993Z | 70.329° E | 15.396° | 2025-09-18 04:24:56.993Z | 34.895° NE |
| 5 mins | 2025-09-18 05:54:56.993Z | 215.216° SW | 2025-09-18 05:56:56.993Z | 269.882° W | 27.594° | 2025-09-18 05:59:56.993Z | 326.196° NNW |
| 4 mins | 2025-09-18 17:25:56.993Z | 59.167° ENE | 2025-09-18 17:27:56.993Z | 104.317° ESE | 20.487° | 2025-09-18 17:29:56.993Z | 141.928° SSE |
| 4 mins | 2025-09-18 18:59:56.993Z | 322.32° NNW | 2025-09-18 19:00:56.993Z | 301.38° NW | 19.712° | 2025-09-18 19:03:56.993Z | 242.747° WSW |
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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