Showing default

AAC-AIS-SAT-1, 55107

Orbit data source: Space-Track

AAC-AIS-SAT-1, 55107 is a payload satellite owned by AAC ClydeSpace (UK) in SSO that was launched on Tue, 03 Jan 2023 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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
55107, 2023-001DC
Orbit
SSO
Country
Flag of UKUK
Related business
Manufacturer
AAC ClydeSpace
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
2023-01-03 (4 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 1.0 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 AAC-AIS-SAT-1
1 55107U 23001DC  26255.26364815  .00002600  00000-0  25722-3 0  9998
2 55107  97.9142 332.5007 0008958 359.9605   0.1611 14.92753911191270
Epoch: 2026-09-12T06:19Z
TLE epoch observation values (Epoch: 2026-09-12T06:19:39.200Z)
Latitude
-0.00006°
Longitude
-113.68778°
Altitude
586.149 km
Speed
7.571 km/s
True Right ascension
22h 10m 00s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
13:12:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
592.616 km
Perigee altitude
580.139 km
Semi-major axis
6,964.515 km
Eccentricity
0.0009
Inclination
97.9142°
RAAN
332.5007°
Arg. of periapsis
359.9605°
True anomaly
0.16139°
Mean anomaly
0.1611°
Eccentric anomaly
0.16124°
Mean motion
3.73428 °/min
Orbital period
96.4 mins
BSTAR
0.00025722
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|