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 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: 15 hours ago
TLE from 15 hours ago
0 AETHER-12
1 67383U 26004W 26094.94294350 .00001250 00000-0 14246-3 0 9994
2 67383 97.8013 94.7144 0005959 30.7184 329.4381 14.87890511 12396Epoch: 2026-04-04T22:37Z
TLE epoch observation values (Epoch: 2026-04-04T22:37:50.318Z)
Latitude
0.00005°
Longitude
-78.00074°
Altitude
603.98 km
Speed
7.559 km/s
True Right ascension
06h 18m 51s
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
19:30:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
605.713 km
Perigee altitude
597.394 km
Semi-major axis
6,979.691 km
Eccentricity
0.0006
Inclination
97.8013°
RAAN
94.7144°
Arg. of periapsis
30.7184°
True anomaly
329.40336°
Mean anomaly
329.4381°
Eccentric anomaly
329.42073°
Mean motion
3.72211 °/min
Orbital period
96.72 mins
BSTAR
0.00014246
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-04-05 13:43:36.751Z | 335.023° NNW | 2026-04-05 13:45:36.751Z | 301.926° NW | 20.676° | 2026-04-05 13:48:36.751Z | 247.867° W |
| 4 mins | 2026-04-05 23:00:36.751Z | 96.314° ESE | 2026-04-05 23:02:36.751Z | 58.634° ENE | 18.841° | 2026-04-05 23:04:36.751Z | 26.683° NE |
| 5 mins | 2026-04-06 00:35:36.751Z | 214.06° SW | 2026-04-06 00:37:36.751Z | 258.424° W | 27.898° | 2026-04-06 00:40:36.751Z | 319.76° NNW |
| 6 mins | 2026-04-06 12:20:36.751Z | 40.398° NE | 2026-04-06 12:22:36.751Z | 85.176° E | 32.24° | 2026-04-06 12:26:36.751Z | 166.945° 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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