AETHER-3, 67374
Orbit data source: Space-Track
AETHER-3, 67374 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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67374 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: 20 hours ago
TLE from 20 hours ago
0 AETHER-3
1 67374U 26004M 26206.01852552 .00000793 00000-0 92423-4 0 9996
2 67374 97.7999 204.0225 0003812 26.1224 334.0184 14.87965145 28929Epoch: 2026-07-25T00:26Z
TLE epoch observation values (Epoch: 2026-07-25T00:26:40.604Z)
Latitude
-0.00008°
Longitude
-105.3835°
Altitude
604.937 km
Speed
7.558 km/s
True Right ascension
13h 36m 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
09:24:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
603.981 km
Perigee altitude
598.659 km
Semi-major axis
6,979.457 km
Eccentricity
0.00038
Inclination
97.7999°
RAAN
204.0225°
Arg. of periapsis
26.1224°
True anomaly
333.99926°
Mean anomaly
334.0184°
Eccentric anomaly
334.00883°
Mean motion
3.72229 °/min
Orbital period
96.71 mins
BSTAR
0.000092423
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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-3 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 23:11:05.431Z | 120.696° SE | 2026-07-25 23:14:05.431Z | 63.976° ENE | 24.406° | 2026-07-25 23:17:05.431Z | 14.437° NNE |
| 4 mins | 2026-07-26 00:48:05.431Z | 233.623° WSW | 2026-07-26 00:50:05.431Z | 275.355° WNW | 21.351° | 2026-07-26 00:52:05.431Z | 309.506° NW |
| 6 mins | 2026-07-26 12:32:05.431Z | 27.722° NE | 2026-07-26 12:35:05.431Z | 121.388° SE | 39.155° | 2026-07-26 12:38:05.431Z | 176.515° 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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