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
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, 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 25289.16865125 .00008316 00000-0 28436-3 0 9994
2 58299 97.4111 7.4308 0006584 306.6204 53.4431 15.30504608107857Epoch: 2025-10-16T04:02Z
TLE epoch observation values (Epoch: 2025-10-16T04:02:51.468Z)
Latitude
0.00003°
Longitude
-78.2159°
Altitude
474.724 km
Speed
7.63 km/s
True Right ascension
00h 29m 43s
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
12:47:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
475.767 km
Perigee altitude
466.748 km
Semi-major axis
6,849.395 km
Eccentricity
0.00066
Inclination
97.4111°
RAAN
7.4308°
Arg. of periapsis
306.6204°
True anomaly
53.50373°
Mean anomaly
53.4431°
Eccentric anomaly
53.47341°
Mean motion
3.82882 °/min
Orbital period
94.02 mins
BSTAR
0.00028436
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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 | 2025-10-16 18:43:28.770Z | 349.338° N | 2025-10-16 18:46:28.770Z | 280.556° WNW | 28.255° | 2025-10-16 18:48:28.770Z | 231.988° WSW |
| 5 mins | 2025-10-17 05:17:28.770Z | 159.261° S | 2025-10-17 05:19:28.770Z | 123.133° SE | 42.838° | 2025-10-17 05:22:28.770Z | 353.003° N |
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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