AETHER-12, 67383
Orbit data source: Space-Track
AETHER-12, 67383 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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67383 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: 15 hours ago
TLE from 15 hours ago
0 AETHER-12
1 67383U 26004W 26206.25826297 .00000695 00000-0 84923-4 0 9996
2 67383 97.8028 204.0387 0003895 25.6073 334.5334 14.86332352 28939Epoch: 2026-07-25T06:11Z
TLE epoch observation values (Epoch: 2026-07-25T06:11:53.920Z)
Latitude
-0.00012°
Longitude
168.09092°
Altitude
609.982 km
Speed
7.556 km/s
True Right ascension
13h 36m 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
10:26:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
609.156 km
Perigee altitude
603.715 km
Semi-major axis
6,984.572 km
Eccentricity
0.00039
Inclination
97.8028°
RAAN
204.0387°
Arg. of periapsis
25.6073°
True anomaly
334.5142°
Mean anomaly
334.5334°
Eccentric anomaly
334.5238°
Mean motion
3.71821 °/min
Orbital period
96.82 mins
BSTAR
0.000084923
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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-12 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 | 2026-07-26 00:05:50.564Z | 177.625° S | 2026-07-26 00:08:50.564Z | 244.46° WSW | 42.722° | 2026-07-26 00:12:50.564Z | 341.603° N |
| 5 mins | 2026-07-26 11:52:50.564Z | 58.714° ENE | 2026-07-26 11:54:50.564Z | 94.077° ESE | 19.43° | 2026-07-26 11:57:50.564Z | 141.352° SSE |
| 5 mins | 2026-07-26 13:28:50.564Z | 333.921° NNW | 2026-07-26 13:30:50.564Z | 287.632° WNW | 27.552° | 2026-07-26 13:33:50.564Z | 232.281° 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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