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 spacecraft
Bus & Motor
ARROW, Unknown motor
Mass
~150 kg wet, ~140 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 YAM-12
1 69003U 26100Z 26174.95000694 .00001184 00000-0 12703-3 0 9990
2 69003 97.7338 72.1908 0011505 56.3924 303.8391 14.90434136 7699Epoch: 2026-06-23T22:48Z
TLE epoch observation values (Epoch: 2026-06-23T22:48:00.599Z)
Latitude
0.00002°
Longitude
178.07408°
Altitude
595.158 km
Speed
7.565 km/s
True Right ascension
04h 48m 45s
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
06:02:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
601.621 km
Perigee altitude
585.579 km
Semi-major axis
6,971.737 km
Eccentricity
0.00115
Inclination
97.7338°
RAAN
72.1908°
Arg. of periapsis
56.3924°
True anomaly
303.72951°
Mean anomaly
303.8391°
Eccentric anomaly
303.78431°
Mean motion
3.72848 °/min
Orbital period
96.55 mins
BSTAR
0.00012703
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-25 05:58:22.652Z | 14.787° NNE | 2026-06-25 06:02:22.652Z | 120.853° SE | 44.532° | 2026-06-25 06:06:22.652Z | 189.763° SSW |
| 6 mins | 2026-06-25 16:50:22.652Z | 137.585° SSE | 2026-06-25 16:52:22.652Z | 87.323° E | 36.503° | 2026-06-25 16:56:22.652Z | 0.199° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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