AETHER-7, 67378
Orbit data source: Space-Track
AETHER-7, 67378 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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67378 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: 6 hours ago
TLE from 6 hours ago
0 AETHER-7
1 67378U 26004R 26095.54983336 .00001309 00000-0 14903-3 0 9999
2 67378 97.8014 95.3064 0005689 32.2587 327.8977 14.87859999 12481Epoch: 2026-04-05T13:11Z
TLE epoch observation values (Epoch: 2026-04-05T13:11:45.602Z)
Latitude
0.00004°
Longitude
63.51273°
Altitude
604.293 km
Speed
7.559 km/s
True Right ascension
06h 21m 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
00:59:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
605.62 km
Perigee altitude
597.678 km
Semi-major axis
6,979.786 km
Eccentricity
0.00057
Inclination
97.8014°
RAAN
95.3064°
Arg. of periapsis
32.2587°
True anomaly
327.86303°
Mean anomaly
327.8977°
Eccentric anomaly
327.88037°
Mean motion
3.72203 °/min
Orbital period
96.72 mins
BSTAR
0.00014903
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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-7 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 23:02:01.045Z | 110.22° ESE | 2026-04-05 23:04:01.045Z | 77.791° E | 19.707° | 2026-04-05 23:07:01.045Z | 25.001° NE |
| 5 mins | 2026-04-06 00:38:01.045Z | 216.87° SW | 2026-04-06 00:40:01.045Z | 260.46° W | 26.67° | 2026-04-06 00:43:01.045Z | 318.975° NNW |
| 6 mins | 2026-04-06 12:23:01.045Z | 39.051° NE | 2026-04-06 12:25:01.045Z | 85.97° E | 33.683° | 2026-04-06 12:29:01.045Z | 169.161° 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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