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, 0.1 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 GENMAT-1
1 58276U 23174W 26175.16164094 .00008451 00000-0 25301-3 0 9999
2 58276 97.3673 252.9798 0007442 149.1018 211.0664 15.34753795146042Epoch: 2026-06-24T03:52Z
TLE epoch observation values (Epoch: 2026-06-24T03:52:45.777Z)
Latitude
-0.00005°
Longitude
-77.53375°
Altitude
469.125 km
Speed
7.629 km/s
True Right ascension
16h 51m 55s
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
19:49:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
463.684 km
Perigee altitude
453.509 km
Semi-major axis
6,836.733 km
Eccentricity
0.00074
Inclination
97.3673°
RAAN
252.9798°
Arg. of periapsis
149.1018°
True anomaly
211.02243°
Mean anomaly
211.0664°
Eccentric anomaly
211.04441°
Mean motion
3.83946 °/min
Orbital period
93.76 mins
BSTAR
0.00025301
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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 | 2026-06-25 17:59:08.931Z | 15.509° NNE | 2026-06-25 18:02:08.931Z | 51.106° ENE | 42.595° | 2026-06-25 18:05:08.931Z | 186.273° SSW |
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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