AETHER-6, 67377
Orbit data source: Space-Track
AETHER-6, 67377 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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67377 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: 13 hours ago
TLE from 13 hours ago
0 AETHER-6
1 67377U 26004Q 26264.27014079 .00000365 00000-0 48037-4 0 9992
2 67377 97.8111 261.1302 0000712 162.0796 198.0445 14.85860028 37558Epoch: 2026-09-21T06:29Z
TLE epoch observation values (Epoch: 2026-09-21T06:29:00.164Z)
Latitude
0.00003°
Longitude
163.72713°
Altitude
614.393 km
Speed
7.552 km/s
True Right ascension
17h 24m 31s
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
12:35:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
608.414 km
Perigee altitude
607.419 km
Semi-major axis
6,986.054 km
Eccentricity
0.00007
Inclination
97.8111°
RAAN
261.1302°
Arg. of periapsis
162.0796°
True anomaly
198.04197°
Mean anomaly
198.0445°
Eccentric anomaly
198.04324°
Mean motion
3.71702 °/min
Orbital period
96.85 mins
BSTAR
0.000048037
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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-6 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 22:48:42.460Z | 96.55° ESE | 2026-09-21 22:50:42.460Z | 65.063° ENE | 16.694° | 2026-09-21 22:52:42.460Z | 33.981° NE |
| 6 mins | 2026-09-22 00:23:42.460Z | 200.073° SSW | 2026-09-22 00:26:42.460Z | 279.192° WNW | 40.452° | 2026-09-22 00:29:42.460Z | 329.816° NNW |
| 6 mins | 2026-09-22 12:09:42.460Z | 41.472° NE | 2026-09-22 12:12:42.460Z | 104.162° ESE | 32.085° | 2026-09-22 12:15:42.460Z | 157.019° SSE |
| 4 mins | 2026-09-22 13:46:42.460Z | 320.071° NNW | 2026-09-22 13:47:42.460Z | 302.081° NW | 20.529° | 2026-09-22 13:50:42.460Z | 250.736° W |
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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