AETHER-11, 67382
Orbit data source: Space-Track
AETHER-11, 67382 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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67382 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: 5 hours ago
TLE from 5 hours ago
0 AETHER-11
1 67382U 26004V 26095.60002055 .00001301 00000-0 14707-3 0 9995
2 67382 97.8041 95.4194 0004939 19.1406 340.9995 14.88168214 12493Epoch: 2026-04-05T14:24Z
TLE epoch observation values (Epoch: 2026-04-05T14:24:01.775Z)
Latitude
-0.00006°
Longitude
45.50889°
Altitude
603.434 km
Speed
7.56 km/s
True Right ascension
06h 21m 40s
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
00:59:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
604.132 km
Perigee altitude
597.238 km
Semi-major axis
6,978.822 km
Eccentricity
0.00049
Inclination
97.8041°
RAAN
95.4194°
Arg. of periapsis
19.1406°
True anomaly
340.98106°
Mean anomaly
340.9995°
Eccentric anomaly
340.99028°
Mean motion
3.7228 °/min
Orbital period
96.7 mins
BSTAR
0.00014707
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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-11 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 | 2026-04-06 00:12:56.202Z | 184.94° SSW | 2026-04-06 00:15:56.202Z | 281.877° WNW | 39.989° | 2026-04-06 00:18:56.202Z | 336.975° NNW |
| 5 mins | 2026-04-06 11:58:56.202Z | 61.637° ENE | 2026-04-06 12:00:56.202Z | 101.043° ESE | 20.865° | 2026-04-06 12:03:56.202Z | 146.858° SSE |
| 6 mins | 2026-04-06 13:33:56.202Z | 339.05° N | 2026-04-06 13:35:56.202Z | 302.519° NW | 25.006° | 2026-04-06 13:39:56.202Z | 231.523° 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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