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YAM-14, 69008

Orbit data source: Space-Track

YAM-14, 69008 is an American payload satellite in SSO that was launched on Sun, 03 May 2026 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
69008, 2026-100AE
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Airbus/Toulouse
Mission
Operational Commercial Imaging
Bus & Motor
ARROW, Unknown motor
Mass
~150 kg wet, ~140 kg dry
Launch date (UTC)
2026-05-03 (5 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, Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago
0 YAM-14
1 69008U 26100AE  26266.17660370  .00000176  00000-0  23729-4 0  9995
2 69008  97.7746 161.9238 0001438  73.1689 286.9686 14.90393955 21281
Epoch: 2026-09-23T04:14Z
TLE epoch observation values (Epoch: 2026-09-23T04:14:18.559Z)
Latitude
-0.0001°
Longitude
96.315°
Altitude
599.453 km
Speed
7.56 km/s
True Right ascension
10h 47m 41s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
04:07:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
594.73 km
Perigee altitude
592.725 km
Semi-major axis
6,971.865 km
Eccentricity
0.00014
Inclination
97.7746°
RAAN
161.9238°
Arg. of periapsis
73.1689°
True anomaly
286.95284°
Mean anomaly
286.9686°
Eccentric anomaly
286.96072°
Mean motion
3.72838 °/min
Orbital period
96.56 mins
BSTAR
0.000023729
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Documentation

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