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: 11 hours ago
TLE from 11 hours ago
0 GENMAT-1
1 58276U 23174W 26234.47385219 .00008349 00000-0 24283-3 0 9997
2 58276 97.3642 312.2565 0004912 317.4808 42.6055 15.35685360155142Epoch: 2026-08-22T11:22Z
TLE epoch observation values (Epoch: 2026-08-22T11:22:20.829Z)
Latitude
0.00001°
Longitude
170.88596°
Altitude
459.527 km
Speed
7.638 km/s
True Right ascension
20h 49m 01s
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
13:28:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
459.186 km
Perigee altitude
452.472 km
Semi-major axis
6,833.966 km
Eccentricity
0.00049
Inclination
97.3642°
RAAN
312.2565°
Arg. of periapsis
317.4808°
True anomaly
42.64362°
Mean anomaly
42.6055°
Eccentric anomaly
42.62456°
Mean motion
3.84179 °/min
Orbital period
93.71 mins
BSTAR
0.00024283
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-08-23 04:43:24.244Z | 120.868° SE | 2026-08-23 04:45:24.244Z | 72.341° E | 24.436° | 2026-08-23 04:47:24.244Z | 23.165° NE |
| 4 mins | 2026-08-23 17:40:24.244Z | 54.637° ENE | 2026-08-23 17:41:24.244Z | 84.28° E | 27.892° | 2026-08-23 17:44:24.244Z | 159.737° S |
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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