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: 10 hours ago
TLE from 10 hours ago
0 YAM-10
1 64580U 25135BE 25293.85217666 .00005057 00000-0 50062-3 0 9994
2 64580 97.7568 46.2725 0004560 79.5593 280.6140 14.92281535 18174Epoch: 2025-10-20T20:27Z
TLE epoch observation values (Epoch: 2025-10-20T20:27:08.063Z)
Latitude
0°
Longitude
69.94036°
Altitude
593.282 km
Speed
7.564 km/s
True Right ascension
03h 05m 05s
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
01:26:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.018 km
Perigee altitude
584.665 km
Semi-major axis
6,965.978 km
Eccentricity
0.00046
Inclination
97.7568°
RAAN
46.2725°
Arg. of periapsis
79.5593°
True anomaly
280.56263°
Mean anomaly
280.614°
Eccentric anomaly
280.58832°
Mean motion
3.7331 °/min
Orbital period
96.43 mins
BSTAR
0.00050062
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-21 07:50:20.136Z | 178.902° S | 2025-10-21 07:53:20.136Z | 230.039° WSW | 41.08° | 2025-10-21 07:57:20.136Z | 340.066° N |
| 4 mins | 2025-10-21 19:35:20.136Z | 67.681° E | 2025-10-21 19:36:20.136Z | 85.885° E | 18.315° | 2025-10-21 19:39:20.136Z | 136.727° SSE |
| 5 mins | 2025-10-21 21:10:20.136Z | 335.101° NNW | 2025-10-21 21:12:20.136Z | 288.574° WNW | 27.44° | 2025-10-21 21:15:20.136Z | 231.67° 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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