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: 5 hours ago
TLE from 5 hours ago
0 YAM-10
1 64580U 25135BE 26260.29642316 .00001136 00000-0 11734-3 0 9998
2 64580 97.7802 12.9205 0004288 62.0232 298.1421 14.92076173 67598Epoch: 2026-09-17T07:06Z
TLE epoch observation values (Epoch: 2026-09-17T07:06:50.961Z)
Latitude
0.00006°
Longitude
-90.02754°
Altitude
593.095 km
Speed
7.564 km/s
True Right ascension
00h 51m 40s
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
05:12:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.47 km
Perigee altitude
585.495 km
Semi-major axis
6,966.619 km
Eccentricity
0.00043
Inclination
97.7802°
RAAN
12.9205°
Arg. of periapsis
62.0232°
True anomaly
298.09876°
Mean anomaly
298.1421°
Eccentric anomaly
298.12043°
Mean motion
3.73259 °/min
Orbital period
96.45 mins
BSTAR
0.00011734
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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 | 2026-09-17 20:32:59.438Z | 10.338° NNE | 2026-09-17 20:36:59.438Z | 234.107° WSW | 78.364° | 2026-09-17 20:39:59.438Z | 197.1° SSW |
| 6 mins | 2026-09-18 07:23:59.438Z | 146.991° SSE | 2026-09-18 07:25:59.438Z | 99.934° ESE | 57.331° | 2026-09-18 07:29:59.438Z | 356.464° N |
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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