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YAM-9, 66694

Orbit data source: Space-Track

YAM-9, 66694 is an American payload satellite in SSO that was launched on Fri, 28 Nov 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
66694, 2025-276AE
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)
2025-11-28 (4 months 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

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 YAM-9
1 66694U 25276AE  26095.45456817  .00007753  00000-0  42737-3 0  9993
2 66694  97.4245 169.7580 0008707 192.7722 167.3291 15.14229444 19344
Epoch: 2026-04-05T10:54Z
TLE epoch observation values (Epoch: 2026-04-05T10:54:34.689Z)
Latitude
-0.00002°
Longitude
172.35371°
Altitude
532.265 km
Speed
7.593 km/s
True Right ascension
11h 19m 01s
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
03:54:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
526.3 km
Perigee altitude
514.287 km
Semi-major axis
6,898.43 km
Eccentricity
0.00087
Inclination
97.4245°
RAAN
169.758°
Arg. of periapsis
192.7722°
True anomaly
167.35096°
Mean anomaly
167.3291°
Eccentric anomaly
167.34003°
Mean motion
3.78807 °/min
Orbital period
95.04 mins
BSTAR
0.00042737
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Documentation

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