Showing default

AETHER-1, 58281

Orbit data source: Space-Track

AETHER-1, 58281 is a payload satellite owned by Kepler Comms (CA) in SSO that was launched on Sat, 11 Nov 2023 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
58281, 2023-174AB
Orbit
SSO
Country
Flag of CACA
Related business
Manufacturer
KEPLER/UTIAS
Mission
Operational Commercial Communications
Bus & Motor
AETHER, Unknown motor
Mass
125 kg wet, 125 kg dry
Launch date (UTC)
2023-11-11 (3 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 3.6 m
Radar Cross Section
0.583 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 AETHER-1
1 58281U 23174AB  26175.23665512  .00297122  00000-0  10532-2 0  9998
2 58281  97.3769 270.1251 0004729 232.6182 127.4660 15.88272766147078
Epoch: 2026-06-24T05:40Z
TLE epoch observation values (Epoch: 2026-06-24T05:40:47.002Z)
Latitude
Longitude
-87.4675°
Altitude
312.233 km
Speed
7.72 km/s
True Right ascension
18h 00m 30s
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
16:59:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
307.159 km
Perigee altitude
300.839 km
Semi-major axis
6,682.136 km
Eccentricity
0.00047
Inclination
97.3769°
RAAN
270.1251°
Arg. of periapsis
232.6182°
True anomaly
127.509°
Mean anomaly
127.466°
Eccentric anomaly
127.4875°
Mean motion
3.97347 °/min
Orbital period
90.6 mins
BSTAR
0.0010532
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|