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: 6 hours ago
TLE from 6 hours ago
0 YAM-10
1 64580U 25135BE 26083.55631559 .00002058 00000-0 21127-3 0 9998
2 64580 97.7616 198.6558 0001731 270.7276 89.3745 14.91481027 41240Epoch: 2026-03-24T13:21Z
TLE epoch observation values (Epoch: 2026-03-24T13:21:05.666Z)
Latitude
0.00002°
Longitude
176.34992°
Altitude
596.345 km
Speed
7.562 km/s
True Right ascension
13h 14m 37s
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
00:48:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
591.542 km
Perigee altitude
589.13 km
Semi-major axis
6,968.473 km
Eccentricity
0.00017
Inclination
97.7616°
RAAN
198.6558°
Arg. of periapsis
270.7276°
True anomaly
89.39433°
Mean anomaly
89.3745°
Eccentric anomaly
89.38442°
Mean motion
3.7311 °/min
Orbital period
96.49 mins
BSTAR
0.00021127
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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 | 2026-03-24 20:21:51.385Z | 18.266° NNE | 2026-03-24 20:24:51.385Z | 74.441° E | 43.332° | 2026-03-24 20:28:51.385Z | 186.327° SSW |
| 6 mins | 2026-03-25 07:12:51.385Z | 130.86° SE | 2026-03-25 07:14:51.385Z | 75.991° E | 34.753° | 2026-03-25 07:18:51.385Z | 1.267° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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