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 spacecraft
Bus & Motor
KEPLER GEN2B, Unknown motor
Mass
300 kg wet, 300 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 7.6 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 AETHER-8
1 67379U 26004S 26095.54915603 .00001287 00000-0 14658-3 0 9994
2 67379 97.8020 95.3125 0006031 27.5657 332.5878 14.87874035 12485Epoch: 2026-04-05T13:10Z
TLE epoch observation values (Epoch: 2026-04-05T13:10:47.080Z)
Latitude
-0.00002°
Longitude
63.76335°
Altitude
603.876 km
Speed
7.56 km/s
True Right ascension
06h 21m 15s
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
01:31:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
605.815 km
Perigee altitude
597.396 km
Semi-major axis
6,979.742 km
Eccentricity
0.0006
Inclination
97.802°
RAAN
95.3125°
Arg. of periapsis
27.5657°
True anomaly
332.55596°
Mean anomaly
332.5878°
Eccentric anomaly
332.57188°
Mean motion
3.72207 °/min
Orbital period
96.72 mins
BSTAR
0.00014658
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-04-05 23:00:54.570Z | 111.211° ESE | 2026-04-05 23:03:54.570Z | 59.929° ENE | 19.443° | 2026-04-05 23:05:54.570Z | 27.008° NE |
| 5 mins | 2026-04-06 00:36:54.570Z | 214.208° SW | 2026-04-06 00:38:54.570Z | 256.443° W | 27.082° | 2026-04-06 00:41:54.570Z | 318.204° NNW |
| 6 mins | 2026-04-06 12:21:54.570Z | 38.424° NE | 2026-04-06 12:23:54.570Z | 81.456° E | 32.75° | 2026-04-06 12:27:54.570Z | 167.589° S |
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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