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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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: 2 days ago
TLE from 2 days ago
0 YAM-8
1 63254U 25052AW 26305.46538300 .00003065 00000-0 20327-3 0 9990
2 63254 97.6808 207.3994 0002467 80.2257 279.9249 15.08018011 89988Epoch: 2026-11-01T11:10Z
TLE epoch observation values (Epoch: 2026-11-01T11:10:09.091Z)
Latitude
-0.00004°
Longitude
-0.89484°
Altitude
545.029 km
Speed
7.59 km/s
True Right ascension
13h 49m 35s
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
01:37:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
540.957 km
Perigee altitude
537.544 km
Semi-major axis
6,917.388 km
Eccentricity
0.00025
Inclination
97.6808°
RAAN
207.3994°
Arg. of periapsis
80.2257°
True anomaly
279.89705°
Mean anomaly
279.9249°
Eccentric anomaly
279.91098°
Mean motion
3.77251 °/min
Orbital period
95.43 mins
BSTAR
0.00020327
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-11-03 06:43:00.399Z | 4.457° NNE | 2026-11-03 06:47:00.399Z | 272.323° WNW | 58.893° | 2026-11-03 06:50:00.399Z | 207.69° SW |
| 6 mins | 2026-11-03 17:27:00.399Z | 152.396° SSE | 2026-11-03 17:30:00.399Z | 41.428° NE | 59.041° | 2026-11-03 17:33:00.399Z | 355.447° N |
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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