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: 23 hours ago
TLE from 23 hours ago
0 AETHER-3
1 67374U 26004M 26263.93453935 .00000392 00000-0 49761-4 0 9994
2 67374 97.8032 261.0015 0005247 94.3270 265.8546 14.86982087 37533Epoch: 2026-09-20T22:25Z
TLE epoch observation values (Epoch: 2026-09-20T22:25:44.199Z)
Latitude
-0.00001°
Longitude
-75.25426°
Altitude
610.672 km
Speed
7.554 km/s
True Right ascension
17h 24m 00s
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
14:28:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
608.062 km
Perigee altitude
600.735 km
Semi-major axis
6,982.536 km
Eccentricity
0.00052
Inclination
97.8032°
RAAN
261.0015°
Arg. of periapsis
94.327°
True anomaly
265.79463°
Mean anomaly
265.8546°
Eccentric anomaly
265.82462°
Mean motion
3.71983 °/min
Orbital period
96.78 mins
BSTAR
0.000049761
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-09-21 22:48:54.577Z | 100.046° ESE | 2026-09-21 22:50:54.577Z | 70.069° E | 16.285° | 2026-09-21 22:52:54.577Z | 37.842° NE |
| 6 mins | 2026-09-22 00:23:54.577Z | 197.617° SSW | 2026-09-22 00:26:54.577Z | 271.017° WNW | 41.72° | 2026-09-22 00:29:54.577Z | 328.693° NNW |
| 6 mins | 2026-09-22 12:09:54.577Z | 45.633° ENE | 2026-09-22 12:11:54.577Z | 84.807° E | 30.698° | 2026-09-22 12:15:54.577Z | 158.859° S |
| 5 mins | 2026-09-22 13:45:54.577Z | 329.195° NNW | 2026-09-22 13:47:54.577Z | 294.069° NW | 21.168° | 2026-09-22 13:50:54.577Z | 245.881° WSW |
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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