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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 AETHER-4
1 67375U 26004N 26263.71638750 .00000390 00000-0 50760-4 0 9990
2 67375 97.8110 260.6218 0001385 152.6199 207.5090 14.85941560 37489Epoch: 2026-09-20T17:11Z
TLE epoch observation values (Epoch: 2026-09-20T17:11:35.880Z)
Latitude
0.00004°
Longitude
3.11572°
Altitude
614.523 km
Speed
7.551 km/s
True Right ascension
17h 22m 29s
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
12:35:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
608.629 km
Perigee altitude
606.693 km
Semi-major axis
6,985.798 km
Eccentricity
0.00014
Inclination
97.811°
RAAN
260.6218°
Arg. of periapsis
152.6199°
True anomaly
207.50167°
Mean anomaly
207.509°
Eccentric anomaly
207.50534°
Mean motion
3.71723 °/min
Orbital period
96.85 mins
BSTAR
0.00005076
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-22 00:01:12.251Z | 172.605° S | 2026-09-22 00:05:12.251Z | 313.543° NW | 66.761° | 2026-09-22 00:08:12.251Z | 343.286° N |
| 4 mins | 2026-09-22 11:49:12.251Z | 65.571° ENE | 2026-09-22 11:51:12.251Z | 101.023° ESE | 18.692° | 2026-09-22 11:53:12.251Z | 132.306° SE |
| 6 mins | 2026-09-22 13:24:12.251Z | 344.298° N | 2026-09-22 13:27:12.251Z | 276.608° WNW | 33.859° | 2026-09-22 13:30:12.251Z | 226.804° 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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