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: 18 hours ago
TLE from 18 hours ago
0 YAM-12
1 69003U 26100Z 26237.51954694 .00001242 00000-0 13301-3 0 9990
2 69003 97.7791 133.6830 0001650 79.1449 280.9955 14.90459089 17016Epoch: 2026-08-25T12:28Z
TLE epoch observation values (Epoch: 2026-08-25T12:28:08.855Z)
Latitude
0.00001°
Longitude
-27.13963°
Altitude
599.323 km
Speed
7.56 km/s
True Right ascension
08h 54m 43s
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
21:34:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
594.675 km
Perigee altitude
592.374 km
Semi-major axis
6,971.662 km
Eccentricity
0.00017
Inclination
97.7791°
RAAN
133.683°
Arg. of periapsis
79.1449°
True anomaly
280.97694°
Mean anomaly
280.9955°
Eccentric anomaly
280.98622°
Mean motion
3.72854 °/min
Orbital period
96.55 mins
BSTAR
0.00013301
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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 | 2026-08-26 06:44:50.083Z | 349.575° N | 2026-08-26 06:48:50.083Z | 278.191° WNW | 25.498° | 2026-08-26 06:51:50.083Z | 231.073° WSW |
| 5 mins | 2026-08-26 17:36:50.083Z | 202.694° SW | 2026-08-26 17:38:50.083Z | 260.807° W | 35.164° | 2026-08-26 17:41:50.083Z | 328.812° NNW |
| 5 mins | 2026-08-27 05:20:50.083Z | 53.595° ENE | 2026-08-27 05:22:50.083Z | 96.364° ESE | 24.846° | 2026-08-27 05:25:50.083Z | 150.773° SSE |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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