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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 AETHER-8
1 67379U 26004S 26264.28512277 .00000355 00000-0 46783-4 0 9993
2 67379 97.8089 261.0388 0000874 166.1672 193.9568 14.85898637 37551Epoch: 2026-09-21T06:50Z
TLE epoch observation values (Epoch: 2026-09-21T06:50:34.607Z)
Latitude
0.00004°
Longitude
158.22745°
Altitude
614.392 km
Speed
7.552 km/s
True Right ascension
17h 24m 09s
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
11:33:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
608.406 km
Perigee altitude
607.185 km
Semi-major axis
6,985.933 km
Eccentricity
0.00009
Inclination
97.8089°
RAAN
261.0388°
Arg. of periapsis
166.1672°
True anomaly
193.95438°
Mean anomaly
193.9568°
Eccentric anomaly
193.95559°
Mean motion
3.71712 °/min
Orbital period
96.85 mins
BSTAR
0.000046783
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-21 23:08:57.377Z | 120.729° SE | 2026-09-21 23:11:57.377Z | 65.205° ENE | 27.288° | 2026-09-21 23:14:57.377Z | 15.138° NNE |
| 5 mins | 2026-09-22 00:45:57.377Z | 230.642° WSW | 2026-09-22 00:47:57.377Z | 271.498° WNW | 23.99° | 2026-09-22 00:50:57.377Z | 318.054° NNW |
| 7 mins | 2026-09-22 12:30:57.377Z | 25.945° NE | 2026-09-22 12:33:57.377Z | 109.697° ESE | 57.662° | 2026-09-22 12:37:57.377Z | 180.037° SSW |
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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