YAM-8, 63254
Orbit data source: Space-Track
YAM-8, 63254 is a payload satellite owned by Loft Orbital (US) in SSO that was launched on Sat, 15 Mar 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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63254 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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 YAM-8
1 63254U 25052AW 25334.68119205 .00007437 00000-0 46708-3 0 9992
2 63254 97.7091 229.8567 0003230 120.0206 240.1343 15.09561378 39298Epoch: 2025-11-30T16:20Z
TLE epoch observation values (Epoch: 2025-11-30T16:20:54.993Z)
Latitude
-0.00004°
Longitude
-85.16399°
Altitude
541.72 km
Speed
7.591 km/s
True Right ascension
15h 19m 25s
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
01:16:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
536.765 km
Perigee altitude
532.299 km
Semi-major axis
6,912.669 km
Eccentricity
0.00032
Inclination
97.7091°
RAAN
229.8567°
Arg. of periapsis
120.0206°
True anomaly
240.10221°
Mean anomaly
240.1343°
Eccentric anomaly
240.11825°
Mean motion
3.77637 °/min
Orbital period
95.33 mins
BSTAR
0.00046708
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Other satellites on launch #52 in the year 2025 (2025-03-15 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-8 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 | 2025-12-01 05:38:34.742Z | 29.609° NE | 2025-12-01 05:41:34.742Z | 91.009° ESE | 33.566° | 2025-12-01 05:44:34.742Z | 165.824° S |
| 4 mins | 2025-12-01 16:22:34.742Z | 100.711° ESE | 2025-12-01 16:24:34.742Z | 58.083° ENE | 19.646° | 2025-12-01 16:26:34.742Z | 23.761° NE |
| 5 mins | 2025-12-01 17:56:34.742Z | 223.073° SW | 2025-12-01 17:58:34.742Z | 267.592° W | 22.852° | 2025-12-01 18:01:34.742Z | 320.005° 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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