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 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: 18 hours ago
TLE from 18 hours ago
0 AETHER-7
1 67378U 26004R 26264.02279281 .00000981 00000-0 11703-3 0 9997
2 67378 97.8084 260.7504 0003449 148.3913 211.7511 14.86490813 37510Epoch: 2026-09-21T00:32Z
TLE epoch observation values (Epoch: 2026-09-21T00:32:49.298Z)
Latitude
0.00001°
Longitude
-107.36359°
Altitude
613.993 km
Speed
7.551 km/s
True Right ascension
17h 23m 00s
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
11:31:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
608.347 km
Perigee altitude
603.53 km
Semi-major axis
6,984.075 km
Eccentricity
0.00034
Inclination
97.8084°
RAAN
260.7504°
Arg. of periapsis
148.3913°
True anomaly
211.73031°
Mean anomaly
211.7511°
Eccentric anomaly
211.7407°
Mean motion
3.7186 °/min
Orbital period
96.81 mins
BSTAR
0.00011703
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-21 23:17:46.254Z | 133.229° SE | 2026-09-21 23:20:46.254Z | 84.498° E | 33.434° | 2026-09-21 23:24:46.254Z | 8.076° NNE |
| 4 mins | 2026-09-22 00:55:46.254Z | 241.362° WSW | 2026-09-22 00:56:46.254Z | 258.839° W | 18.854° | 2026-09-22 00:59:46.254Z | 307.592° NW |
| 7 mins | 2026-09-22 12:39:46.254Z | 17.625° NNE | 2026-09-22 12:42:46.254Z | 70.907° E | 72.696° | 2026-09-22 12:46:46.254Z | 187.245° 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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