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: 8 hours ago
TLE from 8 hours ago
0 AETHER-7
1 67378U 26004R 26206.60147805 .00000706 00000-0 86164-4 0 9992
2 67378 97.8026 204.3590 0003429 32.3933 327.7493 14.86348638 28982Epoch: 2026-07-25T14:26Z
TLE epoch observation values (Epoch: 2026-07-25T14:26:07.703Z)
Latitude
0.00001°
Longitude
44.51549°
Altitude
610.362 km
Speed
7.555 km/s
True Right ascension
13h 37m 26s
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
11:10:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
608.779 km
Perigee altitude
603.989 km
Semi-major axis
6,984.521 km
Eccentricity
0.00034
Inclination
97.8026°
RAAN
204.359°
Arg. of periapsis
32.3933°
True anomaly
327.72832°
Mean anomaly
327.7493°
Eccentric anomaly
327.73881°
Mean motion
3.71825 °/min
Orbital period
96.82 mins
BSTAR
0.000086164
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-07-26 00:15:49.234Z | 190.972° SSW | 2026-07-26 00:18:49.234Z | 282.752° WNW | 37.313° | 2026-07-26 00:21:49.234Z | 334.426° NNW |
| 6 mins | 2026-07-26 12:01:49.234Z | 48.711° ENE | 2026-07-26 12:03:49.234Z | 83.965° E | 23.233° | 2026-07-26 12:07:49.234Z | 152.66° SSE |
| 5 mins | 2026-07-26 13:37:49.234Z | 334.448° NNW | 2026-07-26 13:39:49.234Z | 297.936° NW | 22.878° | 2026-07-26 13:42:49.234Z | 242.895° 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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