AETHER-2, 58299
Orbit data source: Space-Track
AETHER-2, 58299 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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58299 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CARelated business
Manufacturer
KEPLER/UTIAS
Mission
Operational Commercial Communications
Bus & Motor
AETHER, Unknown motor
Mass
125 kg wet, 125 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.583 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 AETHER-2
1 58299U 23174AV 26022.95741847 .00009265 00000-0 29774-3 0 9991
2 58299 97.4008 106.1369 0006491 317.6058 42.4681 15.32475387122970Epoch: 2026-01-22T22:58Z
TLE epoch observation values (Epoch: 2026-01-22T22:58:40.955Z)
Latitude
-0.00012°
Longitude
-0.83686°
Altitude
468.259 km
Speed
7.634 km/s
True Right ascension
07h 04m 32s
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
19:40:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
469.821 km
Perigee altitude
460.936 km
Semi-major axis
6,843.516 km
Eccentricity
0.00065
Inclination
97.4008°
RAAN
106.1369°
Arg. of periapsis
317.6058°
True anomaly
42.51835°
Mean anomaly
42.4681°
Eccentric anomaly
42.49322°
Mean motion
3.83375 °/min
Orbital period
93.9 mins
BSTAR
0.00029774
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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-2 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 | 2026-01-24 04:53:49.613Z | 125.601° SE | 2026-01-24 04:55:49.613Z | 81.825° E | 25.274° | 2026-01-24 04:58:49.613Z | 13.905° NNE |
| 4 mins | 2026-01-24 17:52:49.613Z | 54.621° ENE | 2026-01-24 17:53:49.613Z | 87.61° E | 30.334° | 2026-01-24 17:56:49.613Z | 163.304° S |
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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