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 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: 19 hours ago
TLE from 19 hours ago
0 AETHER-10
1 67381U 26004U 26263.97834322 .00000382 00000-0 49848-4 0 9994
2 67381 97.8115 260.9094 0001054 163.6454 196.4796 14.85920614 37515Epoch: 2026-09-20T23:28Z
TLE epoch observation values (Epoch: 2026-09-20T23:28:48.854Z)
Latitude
0.00003°
Longitude
-91.15893°
Altitude
614.436 km
Speed
7.551 km/s
True Right ascension
17h 23m 38s
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
11:33:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
608.463 km
Perigee altitude
606.99 km
Semi-major axis
6,985.864 km
Eccentricity
0.00011
Inclination
97.8115°
RAAN
260.9094°
Arg. of periapsis
163.6454°
True anomaly
196.47617°
Mean anomaly
196.4796°
Eccentric anomaly
196.47789°
Mean motion
3.71717 °/min
Orbital period
96.85 mins
BSTAR
0.000049848
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-21 23:50:31.522Z | 162.51° S | 2026-09-21 23:54:31.522Z | 20.947° NNE | 74.516° | 2026-09-21 23:57:31.522Z | 350.437° N |
| 6 mins | 2026-09-22 13:13:31.522Z | 352.774° N | 2026-09-22 13:16:31.522Z | 279.851° WNW | 45.094° | 2026-09-22 13:19:31.522Z | 219.248° SW |
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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