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
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 AETHER-12
1 67383U 26004W 26146.61071228 .00000628 00000-0 77395-4 0 9996
2 67383 97.8006 145.5006 0003575 170.3968 189.7317 14.86306067 20070Epoch: 2026-05-26T14:39Z
TLE epoch observation values (Epoch: 2026-05-26T14:39:25.540Z)
Latitude
-0.00002°
Longitude
41.46251°
Altitude
614.985 km
Speed
7.55 km/s
True Right ascension
09h 42m 00s
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
04:33:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
609.014 km
Perigee altitude
604.02 km
Semi-major axis
6,984.654 km
Eccentricity
0.00036
Inclination
97.8006°
RAAN
145.5006°
Arg. of periapsis
170.3968°
True anomaly
189.72478°
Mean anomaly
189.7317°
Eccentric anomaly
189.72824°
Mean motion
3.71814 °/min
Orbital period
96.82 mins
BSTAR
0.000077395
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-05-26 22:54:08.010Z | 97.774° ESE | 2026-05-26 22:56:08.010Z | 64.339° ENE | 17.29° | 2026-05-26 22:58:08.010Z | 32.165° NE |
| 6 mins | 2026-05-27 00:29:08.010Z | 204.606° SW | 2026-05-27 00:31:08.010Z | 245.06° WSW | 30.548° | 2026-05-27 00:35:08.010Z | 327.955° NNW |
| 6 mins | 2026-05-27 12:15:08.010Z | 42.457° NE | 2026-05-27 12:17:08.010Z | 82.923° E | 29.347° | 2026-05-27 12:21:08.010Z | 162.329° S |
| 4 mins | 2026-05-27 13:52:08.010Z | 313.282° NW | 2026-05-27 13:53:08.010Z | 295.038° NW | 18.008° | 2026-05-27 13:56:08.010Z | 248.949° W |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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