YAM-10, 64580
Orbit data source: Space-Track
YAM-10, 64580 is an American payload satellite in SSO that was launched on Mon, 23 Jun 2025 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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64580 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Airbus/Toulouse
Mission
Operational Commercial Technology
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: 8 hours ago
TLE from 8 hours ago
0 YAM-10
1 64580U 25135BE 25340.91900103 .00004877 00000-0 47961-3 0 9992
2 64580 97.7597 92.6438 0001997 274.0154 86.0837 14.92572885 25190Epoch: 2025-12-06T22:03Z
TLE epoch observation values (Epoch: 2025-12-06T22:03:21.688Z)
Latitude
-0.00004°
Longitude
45.8636°
Altitude
592.864 km
Speed
7.564 km/s
True Right ascension
06h 10m 34s
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
04:09:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.325 km
Perigee altitude
585.543 km
Semi-major axis
6,965.071 km
Eccentricity
0.0002
Inclination
97.7597°
RAAN
92.6438°
Arg. of periapsis
274.0154°
True anomaly
86.10653°
Mean anomaly
86.0837°
Eccentric anomaly
86.09512°
Mean motion
3.73383 °/min
Orbital period
96.42 mins
BSTAR
0.00047961
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Other satellites on launch #135 in the year 2025 (2025-06-23 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-10 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-07 07:50:21.555Z | 180.239° SSW | 2025-12-07 07:53:21.555Z | 269.429° W | 41.999° | 2025-12-07 07:56:21.555Z | 338.521° N |
| 4 mins | 2025-12-07 19:34:21.555Z | 61.152° ENE | 2025-12-07 19:36:21.555Z | 97.069° ESE | 18.359° | 2025-12-07 19:38:21.555Z | 131.101° SE |
| 6 mins | 2025-12-07 21:09:21.555Z | 340.833° N | 2025-12-07 21:11:21.555Z | 301.062° NW | 27.302° | 2025-12-07 21:15:21.555Z | 226.949° WSW |
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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