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: 13 hours ago
TLE from 13 hours ago
0 YAM-10
1 64580U 25135BE 25311.88905102 .00004033 00000-0 39953-3 0 9996
2 64580 97.7588 64.0375 0003761 32.9205 327.2248 14.92375277 20863Epoch: 2025-11-07T21:20Z
TLE epoch observation values (Epoch: 2025-11-07T21:20:14.008Z)
Latitude
0.00003°
Longitude
56.65259°
Altitude
591.37 km
Speed
7.566 km/s
True Right ascension
04h 16m 08s
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
06:48:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.169 km
Perigee altitude
584.93 km
Semi-major axis
6,965.687 km
Eccentricity
0.00038
Inclination
97.7588°
RAAN
64.0375°
Arg. of periapsis
32.9205°
True anomaly
327.20146°
Mean anomaly
327.2248°
Eccentric anomaly
327.21313°
Mean motion
3.73334 °/min
Orbital period
96.43 mins
BSTAR
0.00039953
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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 | 2025-11-08 20:26:03.645Z | 15.246° NNE | 2025-11-08 20:29:03.645Z | 44.96° NE | 43.821° | 2025-11-08 20:33:03.645Z | 189.79° SSW |
| 6 mins | 2025-11-09 07:16:03.645Z | 141.58° SSE | 2025-11-09 07:19:03.645Z | 62.911° ENE | 36.486° | 2025-11-09 07:22:03.645Z | 2.79° NNE |
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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