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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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, 3.6 m
Radar Cross Section
0.583 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 AETHER-2
1 58299U 23174AV 26234.17354524 .00005208 00000-0 15466-3 0 9998
2 58299 97.3874 317.5710 0005075 273.4036 86.6627 15.35224721155355Epoch: 2026-08-22T04:09Z
TLE epoch observation values (Epoch: 2026-08-22T04:09:54.308Z)
Latitude
-0.00002°
Longitude
-75.39303°
Altitude
463.164 km
Speed
7.635 km/s
True Right ascension
21h 10m 17s
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
08:44:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
460.667 km
Perigee altitude
453.729 km
Semi-major axis
6,835.335 km
Eccentricity
0.00051
Inclination
97.3874°
RAAN
317.571°
Arg. of periapsis
273.4036°
True anomaly
86.72076°
Mean anomaly
86.6627°
Eccentric anomaly
86.69173°
Mean motion
3.84064 °/min
Orbital period
93.73 mins
BSTAR
0.00015466
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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 | 2026-08-22 18:48:28.661Z | 355.477° N | 2026-08-22 18:50:28.661Z | 308.278° NW | 36.223° | 2026-08-22 18:53:28.661Z | 212.872° SW |
| 5 mins | 2026-08-23 05:20:28.661Z | 135.038° SSE | 2026-08-23 05:22:28.661Z | 68.667° E | 34.006° | 2026-08-23 05:25:28.661Z | 3.067° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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