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: 11 hours ago
TLE from 11 hours ago
0 AETHER-9
1 67380U 26004T 26206.44000349 .00002550 00000-0 29607-3 0 9995
2 67380 97.8024 204.2543 0003069 88.9124 271.2443 14.86251524 28962Epoch: 2026-07-25T10:33Z
TLE epoch observation values (Epoch: 2026-07-25T10:33:36.301Z)
Latitude
-0.00005°
Longitude
102.70079°
Altitude
612.647 km
Speed
7.553 km/s
True Right ascension
13h 37m 01s
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
10:27:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
608.832 km
Perigee altitude
604.545 km
Semi-major axis
6,984.825 km
Eccentricity
0.00031
Inclination
97.8024°
RAAN
204.2543°
Arg. of periapsis
88.9124°
True anomaly
271.20914°
Mean anomaly
271.2443°
Eccentric anomaly
271.22672°
Mean motion
3.718 °/min
Orbital period
96.83 mins
BSTAR
0.00029607
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-07-25 23:36:15.135Z | 150.818° SSE | 2026-07-25 23:40:15.135Z | 74.314° E | 39.263° | 2026-07-25 23:44:15.135Z | 357.336° N |
| 7 mins | 2026-07-26 12:59:15.135Z | 3.74° NNE | 2026-07-26 13:02:15.135Z | 277.316° WNW | 42.64° | 2026-07-26 13:06:15.135Z | 202.979° SW |
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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