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 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: 21 hours ago
TLE from 21 hours ago
0 AETHER-5
1 67376U 26004P 26264.02322981 .00000371 00000-0 48702-4 0 9994
2 67376 97.8112 260.8332 0000898 162.1954 197.9293 14.85883679 37522Epoch: 2026-09-21T00:33Z
TLE epoch observation values (Epoch: 2026-09-21T00:33:27.055Z)
Latitude
-0.00003°
Longitude
-107.43854°
Altitude
614.443 km
Speed
7.552 km/s
True Right ascension
17h 23m 19s
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
14:28:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
608.47 km
Perigee altitude
607.215 km
Semi-major axis
6,985.98 km
Eccentricity
0.00009
Inclination
97.8112°
RAAN
260.8332°
Arg. of periapsis
162.1954°
True anomaly
197.92613°
Mean anomaly
197.9293°
Eccentric anomaly
197.92772°
Mean motion
3.71708 °/min
Orbital period
96.85 mins
BSTAR
0.000048702
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-21 23:18:38.979Z | 135.762° SSE | 2026-09-21 23:22:38.979Z | 62.378° ENE | 34.75° | 2026-09-21 23:25:38.979Z | 9.682° NNE |
| 4 mins | 2026-09-22 00:56:38.979Z | 236.672° WSW | 2026-09-22 00:58:38.979Z | 271.35° WNW | 18.629° | 2026-09-22 01:00:38.979Z | 303.24° NW |
| 7 mins | 2026-09-22 12:41:38.979Z | 17.547° NNE | 2026-09-22 12:44:38.979Z | 129.95° SE | 75.974° | 2026-09-22 12:48:38.979Z | 188.76° SSW |
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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