AETHER-4, 67375
Orbit data source: Space-Track
AETHER-4, 67375 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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67375 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: 1 day ago
TLE from 1 day ago
0 AETHER-4
1 67375U 26004N 26145.76480515 .00000634 00000-0 74763-4 0 9998
2 67375 97.8036 144.8038 0004751 178.0917 182.0319 14.88162234 19969Epoch: 2026-05-25T18:21Z
TLE epoch observation values (Epoch: 2026-05-25T18:21:19.164Z)
Latitude
-0.00002°
Longitude
-13.87396°
Altitude
610.029 km
Speed
7.552 km/s
True Right ascension
09h 39m 12s
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
11:09:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
604.019 km
Perigee altitude
597.388 km
Semi-major axis
6,978.84 km
Eccentricity
0.00048
Inclination
97.8036°
RAAN
144.8038°
Arg. of periapsis
178.0917°
True anomaly
182.02997°
Mean anomaly
182.0319°
Eccentric anomaly
182.03094°
Mean motion
3.72279 °/min
Orbital period
96.7 mins
BSTAR
0.000074763
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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-4 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 | 2026-05-27 12:52:16.930Z | 10.342° NNE | 2026-05-27 12:56:16.930Z | 261.262° W | 44.677° | 2026-05-27 13:00:16.930Z | 196.743° SSW |
| 6 mins | 2026-05-27 23:45:16.930Z | 148.715° SSE | 2026-05-27 23:47:16.930Z | 91.803° ESE | 41.799° | 2026-05-27 23:51:16.930Z | 354.769° N |
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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