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YAM-10, 64580

Orbit data source: Space-Track

YAM-10, 64580 is an American payload satellite in SSO that was launched on Mon, 23 Jun 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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Identifier
64580, 2025-135BE
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Airbus/Toulouse
Mission
Operational Commercial Technology
Bus & Motor
ARROW, Unknown motor
Mass
~150 kg wet, ~140 kg dry
Launch date (UTC)
2025-06-23 (1 year ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Trap Box + 2 Pan, 2.3 m
Radar Cross Section
2.032 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 YAM-10
1 64580U 25135BE  26235.28170214  .00001484  00000-0  15190-3 0  9998
2 64580  97.7777 348.2279 0004445 119.2953 240.8711 14.92008018 63860
Epoch: 2026-08-23T06:45Z
TLE epoch observation values (Epoch: 2026-08-23T06:45:39.064Z)
Latitude
Longitude
-84.76487°
Altitude
596.226 km
Speed
7.561 km/s
True Right ascension
23h 12m 54s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
21:42:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.791 km
Perigee altitude
585.598 km
Semi-major axis
6,966.831 km
Eccentricity
0.00044
Inclination
97.7777°
RAAN
348.2279°
Arg. of periapsis
119.2953°
True anomaly
240.82662°
Mean anomaly
240.8711°
Eccentric anomaly
240.84886°
Mean motion
3.73242 °/min
Orbital period
96.45 mins
BSTAR
0.0001519
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Documentation

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