BRO-16, 62654
Orbit data source: Space-Track
BRO-16, 62654 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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62654 intel report (Beta)
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Identifier
Orbit
Country
FRRelated business
Manufacturer
GOMSpace
Mission
Operational Commercial Sigint
Bus & Motor
CUBESAT 8U, Unknown motor
Mass
15 kg wet, ~15 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.100 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 BRO-16
1 62654U 25009AX 26287.48749076 .00004653 00000-0 19111-3 0 9993
2 62654 97.3976 6.5051 0000927 176.8261 183.2983 15.24691517 96978Epoch: 2026-10-14T11:41Z
TLE epoch observation values (Epoch: 2026-10-14T11:41:59.201Z)
Latitude
-0.00001°
Longitude
167.97193°
Altitude
495.445 km
Speed
7.617 km/s
True Right ascension
00h 26m 01s
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
03:14:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
489.308 km
Perigee altitude
488.035 km
Semi-major axis
6,866.808 km
Eccentricity
0.00009
Inclination
97.3976°
RAAN
6.5051°
Arg. of periapsis
176.8261°
True anomaly
183.29769°
Mean anomaly
183.2983°
Eccentric anomaly
183.29799°
Mean motion
3.81426 °/min
Orbital period
94.38 mins
BSTAR
0.00019111
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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.BRO-16 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-10-15 18:10:45.857Z | 14.879° NNE | 2026-10-15 18:14:45.857Z | 164.22° S | 64.114° | 2026-10-15 18:17:45.857Z | 188.309° SSW |
| 4 mins | 2026-10-16 04:48:45.857Z | 107.97° ESE | 2026-10-16 04:49:45.857Z | 83.844° E | 25.859° | 2026-10-16 04:52:45.857Z | 17.841° NNE |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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