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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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, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 GENMAT-1
1 58276U 23174W 26313.15340867 .00015842 00000-0 43812-3 0 9995
2 58276 97.3583 30.9511 0006852 37.1915 322.9803 15.37081078167226Epoch: 2026-11-09T03:40Z
TLE epoch observation values (Epoch: 2026-11-09T03:40:54.509Z)
Latitude
0.00001°
Longitude
-72.61007°
Altitude
454.123 km
Speed
7.642 km/s
True Right ascension
02h 03m 48s
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
07:56:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
456.367 km
Perigee altitude
447.007 km
Semi-major axis
6,829.824 km
Eccentricity
0.00069
Inclination
97.3583°
RAAN
30.9511°
Arg. of periapsis
37.1915°
True anomaly
322.93299°
Mean anomaly
322.9803°
Eccentric anomaly
322.95665°
Mean motion
3.84529 °/min
Orbital period
93.62 mins
BSTAR
0.00043812
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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 | 2026-11-09 18:18:17.606Z | 7.203° NNE | 2026-11-09 18:21:17.606Z | 225.132° WSW | 63.924° | 2026-11-09 18:24:17.606Z | 197.931° SSW |
| 4 mins | 2026-11-10 04:50:17.606Z | 111.933° ESE | 2026-11-10 04:51:17.606Z | 85.413° E | 27.241° | 2026-11-10 04:54:17.606Z | 14.792° NNE |
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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