FOX-1, 40967
Orbit data source: Space-Track
FOX-1, 40967 is a payload satellite owned by AMSAT-NA (US) in LEO that was launched on Thu, 08 Oct 2015 UTC via an ATLAS V 401 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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40967 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
AMSAT-NA
Mission
Operational Amateur Com/Tech
Bus & Motor
CUBESAT 1U, Unknown motor
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.015 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 FOX-1
1 40967U 15058D 26015.10372328 .00001296 00000-0 12981-3 0 9997
2 40967 64.7747 34.3515 0131785 117.0122 244.4515 14.89917186 90753Epoch: 2026-01-15T02:29Z
TLE epoch observation values (Epoch: 2026-01-15T02:29:21.691Z)
Latitude
-0.00002°
Longitude
-117.55104°
Altitude
640.834 km
Speed
7.516 km/s
True Right ascension
02h 17m 24s
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
12:03:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
688.68 km
Perigee altitude
504.843 km
Semi-major axis
6,974.899 km
Eccentricity
0.01318
Inclination
64.7747°
RAAN
34.3515°
Arg. of periapsis
117.0122°
True anomaly
243.09876°
Mean anomaly
244.4515°
Eccentric anomaly
243.77416°
Mean motion
3.72594 °/min
Orbital period
96.62 mins
BSTAR
0.00012981
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Other satellites on launch #58 in the year 2015 (2015-10-08 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.FOX-1 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 | 2026-01-15 12:43:25.926Z | 298.046° NW | 2026-01-15 12:46:25.926Z | 235.589° WSW | 23.523° | 2026-01-15 12:48:25.926Z | 196.803° SSW |
| 6 mins | 2026-01-16 02:48:25.926Z | 206.034° SW | 2026-01-16 02:51:25.926Z | 69.893° E | 44.193° | 2026-01-16 02:54:25.926Z | 34.427° NE |
| 5 mins | 2026-01-16 11:15:25.926Z | 353.773° N | 2026-01-16 11:17:25.926Z | 55.66° ENE | 34.763° | 2026-01-16 11:20:25.926Z | 124.208° SE |
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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