AETHER-10, 67381
Orbit data source: Space-Track
AETHER-10, 67381 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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67381 intel report (Beta)
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Identifier
Orbit
Country
CARelated business
Manufacturer
Kepler Comms
Mission
Operational spacecraft
Bus & Motor
KEPLER GEN2B, Unknown motor
Mass
300 kg wet, 300 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 7.6 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 AETHER-10
1 67381U 26004U 26095.60124895 .00001280 00000-0 14480-3 0 9995
2 67381 97.8046 95.4276 0005528 19.5958 340.5471 14.88164908 12490Epoch: 2026-04-05T14:25Z
TLE epoch observation values (Epoch: 2026-04-05T14:25:47.909Z)
Latitude
0.00008°
Longitude
45.07364°
Altitude
603.065 km
Speed
7.56 km/s
True Right ascension
06h 21m 42s
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
01:00:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
604.553 km
Perigee altitude
596.837 km
Semi-major axis
6,978.832 km
Eccentricity
0.00055
Inclination
97.8046°
RAAN
95.4276°
Arg. of periapsis
19.5958°
True anomaly
340.52599°
Mean anomaly
340.5471°
Eccentric anomaly
340.53655°
Mean motion
3.72279 °/min
Orbital period
96.7 mins
BSTAR
0.0001448
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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-10 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 | 2026-04-06 00:14:44.567Z | 187.258° SSW | 2026-04-06 00:17:44.567Z | 283.13° WNW | 38.911° | 2026-04-06 00:20:44.567Z | 336.076° NNW |
| 5 mins | 2026-04-06 12:00:44.567Z | 61.726° ENE | 2026-04-06 12:02:44.567Z | 102.513° ESE | 21.596° | 2026-04-06 12:05:44.567Z | 148.46° SSE |
| 5 mins | 2026-04-06 13:35:44.567Z | 337.49° NNW | 2026-04-06 13:37:44.567Z | 300.706° NW | 24.345° | 2026-04-06 13:40:44.567Z | 241.189° 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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