AETHER-5, 67376
Orbit data source: Space-Track
AETHER-5, 67376 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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67376 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: 20 hours ago
TLE from 20 hours ago
0 AETHER-5
1 67376U 26004P 26145.93083818 .00000510 00000-0 63992-4 0 9998
2 67376 97.8021 144.8879 0003178 179.8216 180.3002 14.86340031 19983Epoch: 2026-05-25T22:20Z
TLE epoch observation values (Epoch: 2026-05-25T22:20:24.418Z)
Latitude
0.00003°
Longitude
-73.7254°
Altitude
614.637 km
Speed
7.551 km/s
True Right ascension
09h 39m 33s
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
03:35:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
608.631 km
Perigee altitude
604.191 km
Semi-major axis
6,984.548 km
Eccentricity
0.00032
Inclination
97.8021°
RAAN
144.8879°
Arg. of periapsis
179.8216°
True anomaly
180.30001°
Mean anomaly
180.3002°
Eccentric anomaly
180.3001°
Mean motion
3.71823 °/min
Orbital period
96.82 mins
BSTAR
0.000063992
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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-5 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 | 2026-05-26 22:44:42.481Z | 93.065° ESE | 2026-05-26 22:46:42.481Z | 63.27° ENE | 14.047° | 2026-05-26 22:48:42.481Z | 34.216° NE |
| 6 mins | 2026-05-27 00:19:42.481Z | 195.411° SSW | 2026-05-27 00:21:42.481Z | 241.765° WSW | 36.264° | 2026-05-27 00:25:42.481Z | 333.934° NNW |
| 5 mins | 2026-05-27 12:05:42.481Z | 49.706° ENE | 2026-05-27 12:07:42.481Z | 88.094° E | 24.588° | 2026-05-27 12:10:42.481Z | 146.88° SSE |
| 5 mins | 2026-05-27 13:41:42.481Z | 330.882° NNW | 2026-05-27 13:43:42.481Z | 293.401° NW | 21.906° | 2026-05-27 13:46:42.481Z | 242.46° 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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