GENMAT-1, 58276
Orbit data source: Space-Track
GENMAT-1, 58276 is a payload satellite owned by GenMat (US) in SSO that was launched on Sat, 11 Nov 2023 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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58276 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
GenMat
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
8.8 kg wet, 8.8 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 GENMAT-1
1 58276U 23174W 25335.20588196 .00014739 00000-0 51209-3 0 9996
2 58276 97.3899 48.7247 0007890 160.7750 199.3790 15.29819891114655Epoch: 2025-12-01T04:56Z
TLE epoch observation values (Epoch: 2025-12-01T04:56:28.201Z)
Latitude
0.00002°
Longitude
-95.70152°
Altitude
484.558 km
Speed
7.62 km/s
True Right ascension
03h 14m 53s
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
12:41:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
478.708 km
Perigee altitude
467.897 km
Semi-major axis
6,851.439 km
Eccentricity
0.00079
Inclination
97.3899°
RAAN
48.7247°
Arg. of periapsis
160.775°
True anomaly
199.34903°
Mean anomaly
199.379°
Eccentric anomaly
199.36401°
Mean motion
3.82711 °/min
Orbital period
94.07 mins
BSTAR
0.00051209
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Other satellites on launch #174 in the year 2023 (2023-11-11 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.GENMAT-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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-01 18:03:07.696Z | 6.877° NNE | 2025-12-01 18:06:07.696Z | 321.656° NNW | 42.336° | 2025-12-01 18:09:07.696Z | 201.523° SSW |
| 5 mins | 2025-12-02 04:38:07.696Z | 128.494° SE | 2025-12-02 04:40:07.696Z | 75.795° E | 29.489° | 2025-12-02 04:43:07.696Z | 8.786° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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