AETHER-9, 67380
Orbit data source: Space-Track
AETHER-9, 67380 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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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: 13 hours ago
TLE from 13 hours ago
0 AETHER-9
1 67380U 26004T 26264.27771679 .00000402 00000-0 52188-4 0 9996
2 67380 97.8073 261.0221 0001546 151.2778 208.8523 14.85916398 37553Epoch: 2026-09-21T06:39Z
TLE epoch observation values (Epoch: 2026-09-21T06:39:54.730Z)
Latitude
-0.00001°
Longitude
160.88421°
Altitude
614.69 km
Speed
7.551 km/s
True Right ascension
17h 24m 05s
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
12:36:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
608.82 km
Perigee altitude
606.66 km
Semi-major axis
6,985.877 km
Eccentricity
0.00015
Inclination
97.8073°
RAAN
261.0221°
Arg. of periapsis
151.2778°
True anomaly
208.84375°
Mean anomaly
208.8523°
Eccentric anomaly
208.84803°
Mean motion
3.71716 °/min
Orbital period
96.85 mins
BSTAR
0.000052188
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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-9 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 | 2026-09-21 22:59:01.569Z | 107.213° ESE | 2026-09-21 23:01:01.569Z | 73.534° E | 21.361° | 2026-09-21 23:04:01.569Z | 23.267° NE |
| 5 mins | 2026-09-22 00:35:01.569Z | 217.5° SW | 2026-09-22 00:37:01.569Z | 262.717° W | 31.37° | 2026-09-22 00:40:01.569Z | 320.058° NNW |
| 6 mins | 2026-09-22 12:21:01.569Z | 40.14° NE | 2026-09-22 12:23:01.569Z | 90.454° ESE | 42.967° | 2026-09-22 12:27:01.569Z | 169.995° 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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