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.
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58281 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CARelated business
Manufacturer
KEPLER/UTIAS
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
15 kg wet, 15 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.3 m
Radar Cross Section
0.109 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 AETHER-1
1 58281U 23174AB 25312.65374705 .00062468 00000-0 13852-2 0 9998
2 58281 97.4055 33.2362 0006284 220.1383 139.9402 15.43509380111597Epoch: 2025-11-08T15:41Z
TLE epoch observation values (Epoch: 2025-11-08T15:41:23.745Z)
Latitude
0.00007°
Longitude
109.80699°
Altitude
442.163 km
Speed
7.645 km/s
True Right ascension
02h 12m 56s
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
10:28:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
436.976 km
Perigee altitude
428.416 km
Semi-major axis
6,810.833 km
Eccentricity
0.00063
Inclination
97.4055°
RAAN
33.2362°
Arg. of periapsis
220.1383°
True anomaly
139.98652°
Mean anomaly
139.9402°
Eccentric anomaly
139.96336°
Mean motion
3.86138 °/min
Orbital period
93.23 mins
BSTAR
0.0013852
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Other satellites on launch #174 in the year 2023 (2023-11-11 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.AETHER-1 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-09 18:41:38.458Z | 357.161° N | 2025-11-09 18:44:38.458Z | 267.375° W | 35.055° | 2025-11-09 18:46:38.458Z | 216.559° SW |
| 4 mins | 2025-11-10 05:10:38.458Z | 131.836° SE | 2025-11-10 05:12:38.458Z | 66.78° ENE | 31.587° | 2025-11-10 05:14:38.458Z | 12.158° NNE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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