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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69008 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Airbus/Toulouse
Mission
Operational Commercial Imaging
Bus & Motor
ARROW, Unknown motor
Mass
~150 kg wet, ~140 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Trap Box + 2 Pan, 2.3 m
Radar Cross Section
2.032 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 YAM-14
1 69008U 26100AE 26317.53559602 .00001807 00000-0 19086-3 0 9999
2 69008 97.7717 212.4654 0001631 95.5322 264.6082 14.90482190 28932Epoch: 2026-11-13T12:51Z
TLE epoch observation values (Epoch: 2026-11-13T12:51:15.496Z)
Latitude
-0.00001°
Longitude
-33.0025°
Altitude
599.578 km
Speed
7.56 km/s
True Right ascension
14h 09m 51s
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
21:09:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
594.589 km
Perigee altitude
592.315 km
Semi-major axis
6,971.589 km
Eccentricity
0.00016
Inclination
97.7717°
RAAN
212.4654°
Arg. of periapsis
95.5322°
True anomaly
264.58959°
Mean anomaly
264.6082°
Eccentric anomaly
264.5989°
Mean motion
3.7286 °/min
Orbital period
96.55 mins
BSTAR
0.00019086
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Other satellites on launch #100 in the year 2026 (2026-05-03 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.YAM-14 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 | 2026-11-14 05:32:18.423Z | 31.22° NE | 2026-11-14 05:35:18.423Z | 81.96° E | 37.89° | 2026-11-14 05:39:18.423Z | 165.99° S |
| 5 mins | 2026-11-14 16:24:18.423Z | 107.987° ESE | 2026-11-14 16:26:18.423Z | 66.193° ENE | 25.777° | 2026-11-14 16:29:18.423Z | 16.08° NNE |
| 5 mins | 2026-11-14 17:59:18.423Z | 219.029° SW | 2026-11-14 18:01:18.423Z | 254.341° W | 24.205° | 2026-11-14 18:04:18.423Z | 311.548° NW |
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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