AETHER-8, 67379
Orbit data source: Space-Track
AETHER-8, 67379 is a payload satellite owned by Kepler Comms (CA) in SSO that was launched on Sun, 11 Jan 2026 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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67379 intel report (Beta)
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Identifier
Orbit
Country
CARelated business
Manufacturer
Kepler Comms
Mission
Operational Commercial Communications
Bus & Motor
KEPLER GEN2B, Unknown motor
Mass
300 kg wet, 300 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 7.6 m
Radar Cross Section
4.448 m²
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 AETHER-8
1 67379U 26004S 26146.59715413 .00000379 00000-0 49155-4 0 9995
2 67379 97.8013 145.5242 0000860 199.1357 160.9827 14.86285237 20072Epoch: 2026-05-26T14:19Z
TLE epoch observation values (Epoch: 2026-05-26T14:19:54.116Z)
Latitude
0.00001°
Longitude
46.3804°
Altitude
613.156 km
Speed
7.552 km/s
True Right ascension
09h 42m 05s
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
09:02:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
607.183 km
Perigee altitude
605.982 km
Semi-major axis
6,984.72 km
Eccentricity
0.00009
Inclination
97.8013°
RAAN
145.5242°
Arg. of periapsis
199.1357°
True anomaly
160.98591°
Mean anomaly
160.9827°
Eccentric anomaly
160.98431°
Mean motion
3.71809 °/min
Orbital period
96.82 mins
BSTAR
0.000049155
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Other satellites on launch #4 in the year 2026 (2026-01-11 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-8 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-05-27 00:08:37.040Z | 178.133° S | 2026-05-27 00:12:37.040Z | 287.045° WNW | 41.235° | 2026-05-27 00:15:37.040Z | 338.823° N |
| 4 mins | 2026-05-27 11:56:37.040Z | 64.408° ENE | 2026-05-27 11:58:37.040Z | 103.403° ESE | 20.046° | 2026-05-27 12:00:37.040Z | 136.604° SSE |
| 6 mins | 2026-05-27 13:31:37.040Z | 339.876° N | 2026-05-27 13:33:37.040Z | 302.844° NW | 25.888° | 2026-05-27 13:37:37.040Z | 230.364° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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