YAM-12, 69003
Orbit data source: Space-Track
YAM-12, 69003 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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69003 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: 5 hours ago
TLE from 5 hours ago
0 YAM-12
1 69003U 26100Z 26317.81296530 .00001672 00000-0 17712-3 0 9997
2 69003 97.7719 212.7178 0001195 82.3524 277.7830 14.90446300 28979Epoch: 2026-11-13T19:30Z
TLE epoch observation values (Epoch: 2026-11-13T19:30:40.201Z)
Latitude
-0.00002°
Longitude
-132.87643°
Altitude
599.47 km
Speed
7.56 km/s
True Right ascension
14h 10m 52s
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
21:25:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
594.397 km
Perigee altitude
592.731 km
Semi-major axis
6,971.701 km
Eccentricity
0.00012
Inclination
97.7719°
RAAN
212.7178°
Arg. of periapsis
82.3524°
True anomaly
277.76943°
Mean anomaly
277.783°
Eccentric anomaly
277.77622°
Mean motion
3.72851 °/min
Orbital period
96.55 mins
BSTAR
0.00017712
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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-12 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 05:44:46.066Z | 23.045° NE | 2026-11-14 05:48:46.066Z | 124.029° SE | 53.325° | 2026-11-14 05:51:46.066Z | 176.487° S |
| 5 mins | 2026-11-14 16:36:46.066Z | 119.729° SE | 2026-11-14 16:38:46.066Z | 69.582° E | 35.067° | 2026-11-14 16:41:46.066Z | 10.982° NNE |
| 4 mins | 2026-11-14 18:12:46.066Z | 237.738° WSW | 2026-11-14 18:14:46.066Z | 272.521° WNW | 17.871° | 2026-11-14 18:16:46.066Z | 303.965° 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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