Showing default

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.

Loading next visibility...
Identifier
63254, 2025-052AW
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Airbus/Toulouse
Mission
Operational Commercial Technology
Bus & Motor
ARROW, Unknown motor
Mass
~150 kg wet, ~140 kg dry
Launch date (UTC)
2025-03-15 (1 year ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Trap Box + 2 Pan, 2.3 m
Radar Cross Section
2.032 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 5 hours ago

TLE from 5 hours ago
0 YAM-8
1 63254U 25052AW  26166.97784992  .00003977  00000-0  23674-3 0  9991
2 63254  97.6948  68.4500 0002204 162.5381 197.5925 15.11812097 69088
Epoch: 2026-06-15T23:28Z
TLE epoch observation values (Epoch: 2026-06-15T23:28:06.233Z)
Latitude
-0°
Longitude
172.16754°
Altitude
535.196 km
Speed
7.594 km/s
True Right ascension
04h 33m 48s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
14:48:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
529.185 km
Perigee altitude
526.141 km
Semi-major axis
6,905.8 km
Eccentricity
0.00022
Inclination
97.6948°
RAAN
68.45°
Arg. of periapsis
162.5381°
True anomaly
197.58487°
Mean anomaly
197.5925°
Eccentric anomaly
197.58868°
Mean motion
3.78201 °/min
Orbital period
95.19 mins
BSTAR
0.00023674
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|