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: 19 hours ago
TLE from 19 hours ago
0 YAM-8
1 63254U 25052AW 25287.67050342 .00007894 00000-0 50796-3 0 9993
2 63254 97.7101 182.6140 0001725 353.6533 6.4673 15.08656238 32209Epoch: 2025-10-14T16:05Z
TLE epoch observation values (Epoch: 2025-10-14T16:05:31.495Z)
Latitude
-0.00002°
Longitude
-82.22282°
Altitude
542.185 km
Speed
7.592 km/s
True Right ascension
12h 10m 27s
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
05:49:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
538.492 km
Perigee altitude
536.106 km
Semi-major axis
6,915.436 km
Eccentricity
0.00017
Inclination
97.7101°
RAAN
182.614°
Arg. of periapsis
353.6533°
True anomaly
6.46953°
Mean anomaly
6.4673°
Eccentric anomaly
6.46841°
Mean motion
3.7741 °/min
Orbital period
95.39 mins
BSTAR
0.00050796
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-15 16:07:36.222Z | 103.419° ESE | 2025-10-15 16:09:36.222Z | 70.526° E | 15.835° | 2025-10-15 16:11:36.222Z | 35.477° NE |
| 5 mins | 2025-10-15 17:41:36.222Z | 205.725° SW | 2025-10-15 17:43:36.222Z | 247.558° W | 28.302° | 2025-10-15 17:46:36.222Z | 320.348° NNW |
| 5 mins | 2025-10-16 05:17:36.222Z | 53.216° ENE | 2025-10-16 05:19:36.222Z | 96.208° ESE | 23.037° | 2025-10-16 05:22:36.222Z | 150.839° SSE |
| 4 mins | 2025-10-16 06:52:36.222Z | 320.346° NNW | 2025-10-16 06:53:36.222Z | 299.881° NW | 19.907° | 2025-10-16 06:56:36.222Z | 244.403° WSW |
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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