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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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: 12 hours ago
TLE from 12 hours ago
0 YAM-10
1 64580U 25135BE 26133.06406508 .00001275 00000-0 13232-3 0 9992
2 64580 97.7688 247.4154 0004629 105.5707 254.6023 14.91687253 48621Epoch: 2026-05-13T01:32Z
TLE epoch observation values (Epoch: 2026-05-13T01:32:15.222Z)
Latitude
-0.00004°
Longitude
-6.47748°
Altitude
596.574 km
Speed
7.561 km/s
True Right ascension
16h 29m 39s
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
22:05:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
592.919 km
Perigee altitude
586.468 km
Semi-major axis
6,967.831 km
Eccentricity
0.00046
Inclination
97.7688°
RAAN
247.4154°
Arg. of periapsis
105.5707°
True anomaly
254.55117°
Mean anomaly
254.6023°
Eccentric anomaly
254.57673°
Mean motion
3.73161 °/min
Orbital period
96.47 mins
BSTAR
0.00013232
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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 | 2026-05-13 19:49:47.879Z | 42.433° NE | 2026-05-13 19:52:47.879Z | 103.239° ESE | 26.085° | 2026-05-13 19:55:47.879Z | 155.206° SSE |
| 4 mins | 2026-05-13 21:26:47.879Z | 315.202° NNW | 2026-05-13 21:27:47.879Z | 295.27° NW | 19.912° | 2026-05-13 21:30:47.879Z | 245.315° WSW |
| 4 mins | 2026-05-14 06:40:47.879Z | 100.806° ESE | 2026-05-14 06:42:47.879Z | 64.692° ENE | 18.742° | 2026-05-14 06:44:47.879Z | 30.429° NE |
| 5 mins | 2026-05-14 08:15:47.879Z | 212.893° SW | 2026-05-14 08:17:47.879Z | 256.505° W | 27.775° | 2026-05-14 08:20:47.879Z | 319.466° NNW |
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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