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 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: 13 hours ago
TLE from 13 hours ago
0 AETHER-5
1 67376U 26004P 26095.00766017 .00003249 00000-0 36034-3 0 9997
2 67376 97.8038 94.8081 0005903 25.8246 334.3264 14.87939583 12410Epoch: 2026-04-05T00:11Z
TLE epoch observation values (Epoch: 2026-04-05T00:11:01.838Z)
Latitude
-0.00005°
Longitude
-101.26881°
Altitude
603.694 km
Speed
7.56 km/s
True Right ascension
06h 19m 13s
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
19:27:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
605.52 km
Perigee altitude
597.28 km
Semi-major axis
6,979.537 km
Eccentricity
0.00059
Inclination
97.8038°
RAAN
94.8081°
Arg. of periapsis
25.8246°
True anomaly
334.29707°
Mean anomaly
334.3264°
Eccentric anomaly
334.31174°
Mean motion
3.72223 °/min
Orbital period
96.72 mins
BSTAR
0.00036034
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-04-05 13:39:55.494Z | 337.352° NNW | 2026-04-05 13:42:55.494Z | 280.886° WNW | 22.292° | 2026-04-05 13:44:55.494Z | 246.223° WSW |
| 4 mins | 2026-04-05 22:56:55.494Z | 95.256° ESE | 2026-04-05 22:58:55.494Z | 59.769° ENE | 17.515° | 2026-04-05 23:00:55.494Z | 28.518° NE |
| 6 mins | 2026-04-06 00:31:55.494Z | 210.274° SW | 2026-04-06 00:33:55.494Z | 256.861° W | 29.972° | 2026-04-06 00:37:55.494Z | 329.206° NNW |
| 6 mins | 2026-04-06 12:16:55.494Z | 43.127° NE | 2026-04-06 12:18:55.494Z | 86.262° E | 30.129° | 2026-04-06 12:22:55.494Z | 163.85° S |
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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