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 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-6
1 67377U 26004Q 26095.60325712 .00003870 00000-0 42630-3 0 9996
2 67377 97.8039 95.4189 0005238 19.5645 340.5771 14.88113513 12490Epoch: 2026-04-05T14:28Z
TLE epoch observation values (Epoch: 2026-04-05T14:28:41.415Z)
Latitude
-0.00007°
Longitude
44.34004°
Altitude
603.416 km
Speed
7.56 km/s
True Right ascension
06h 21m 40s
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
00:59:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
604.511 km
Perigee altitude
597.2 km
Semi-major axis
6,978.993 km
Eccentricity
0.00052
Inclination
97.8039°
RAAN
95.4189°
Arg. of periapsis
19.5645°
True anomaly
340.55713°
Mean anomaly
340.5771°
Eccentric anomaly
340.56712°
Mean motion
3.72267 °/min
Orbital period
96.7 mins
BSTAR
0.0004263
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-04-06 00:17:56.290Z | 193.17° SSW | 2026-04-06 00:19:56.290Z | 242.682° WSW | 37.599° | 2026-04-06 00:23:56.290Z | 335.641° NNW |
| 5 mins | 2026-04-06 12:02:56.290Z | 50.227° ENE | 2026-04-06 12:04:56.290Z | 86.234° E | 22.865° | 2026-04-06 12:07:56.290Z | 143.443° SSE |
| 5 mins | 2026-04-06 13:38:56.290Z | 332.295° NNW | 2026-04-06 13:40:56.290Z | 293.22° NW | 23.321° | 2026-04-06 13:43:56.290Z | 240.184° 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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