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: 10 hours ago
TLE from 10 hours ago
0 YAM-10
1 64580U 25135BE 26178.27335926 .00001947 00000-0 19834-3 0 9999
2 64580 97.7739 291.9855 0002331 346.0592 14.0562 14.91845716 55367Epoch: 2026-06-27T06:33Z
TLE epoch observation values (Epoch: 2026-06-27T06:33:38.240Z)
Latitude
-0°
Longitude
-81.81371°
Altitude
593.646 km
Speed
7.564 km/s
True Right ascension
19h 27m 56s
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
04:20:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.824 km
Perigee altitude
587.576 km
Semi-major axis
6,967.337 km
Eccentricity
0.00023
Inclination
97.7739°
RAAN
291.9855°
Arg. of periapsis
346.0592°
True anomaly
14.06269°
Mean anomaly
14.0562°
Eccentric anomaly
14.05944°
Mean motion
3.73201 °/min
Orbital period
96.46 mins
BSTAR
0.00019834
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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 | 2026-06-27 20:00:07.950Z | 28.081° NE | 2026-06-27 20:04:07.950Z | 102.836° ESE | 32.682° | 2026-06-27 20:07:07.950Z | 163.968° S |
| 5 mins | 2026-06-28 06:52:07.950Z | 106.707° ESE | 2026-06-28 06:54:07.950Z | 63.323° ENE | 23.449° | 2026-06-28 06:57:07.950Z | 14.737° NNE |
| 5 mins | 2026-06-28 08:27:07.950Z | 221.849° SW | 2026-06-28 08:29:07.950Z | 259.005° W | 22.031° | 2026-06-28 08:32:07.950Z | 313.533° NW |
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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