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: 8 hours ago
TLE from 8 hours ago
0 AETHER-4
1 67375U 26004N 26206.62214156 .00000720 00000-0 87876-4 0 9992
2 67375 97.8058 204.5545 0003032 91.9395 268.2168 14.86296125 29004Epoch: 2026-07-25T14:55Z
TLE epoch observation values (Epoch: 2026-07-25T14:55:53.030Z)
Latitude
-0.00003°
Longitude
37.25176°
Altitude
612.62 km
Speed
7.553 km/s
True Right ascension
13h 38m 13s
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
11:54:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
608.667 km
Perigee altitude
604.431 km
Semi-major axis
6,984.686 km
Eccentricity
0.0003
Inclination
97.8058°
RAAN
204.5545°
Arg. of periapsis
91.9395°
True anomaly
268.18207°
Mean anomaly
268.2168°
Eccentric anomaly
268.19944°
Mean motion
3.71812 °/min
Orbital period
96.82 mins
BSTAR
0.000087876
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-07-25 23:09:16.270Z | 120.474° SE | 2026-07-25 23:12:16.270Z | 66.185° ENE | 23.981° | 2026-07-25 23:15:16.270Z | 15.838° NNE |
| 5 mins | 2026-07-26 00:46:16.270Z | 229.774° WSW | 2026-07-26 00:48:16.270Z | 271.338° WNW | 22.396° | 2026-07-26 00:51:16.270Z | 318.466° NNW |
| 6 mins | 2026-07-26 12:31:16.270Z | 28.503° NE | 2026-07-26 12:34:16.270Z | 122.679° SE | 38.733° | 2026-07-26 12:37:16.270Z | 176.085° 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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