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: 1 day ago
TLE from 1 day ago
0 GENMAT-1
1 58276U 23174W 26247.43971111 .00005894 00000-0 17102-3 0 9993
2 58276 97.3624 325.2200 0004708 256.2862 103.7858 15.35896436157134Epoch: 2026-09-04T10:33Z
TLE epoch observation values (Epoch: 2026-09-04T10:33:11.039Z)
Latitude
-0.00004°
Longitude
-176.6395°
Altitude
462.141 km
Speed
7.635 km/s
True Right ascension
21h 40m 52s
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
07:09:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
458.419 km
Perigee altitude
451.985 km
Semi-major axis
6,833.339 km
Eccentricity
0.00047
Inclination
97.3624°
RAAN
325.22°
Arg. of periapsis
256.2862°
True anomaly
103.83819°
Mean anomaly
103.7858°
Eccentric anomaly
103.81199°
Mean motion
3.84232 °/min
Orbital period
93.69 mins
BSTAR
0.00017102
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-05 18:23:10.248Z | 359.734° N | 2026-09-05 18:26:10.248Z | 252.753° W | 37.813° | 2026-09-05 18:28:10.248Z | 210.363° SW |
| 5 mins | 2026-09-06 04:55:10.248Z | 129.88° SE | 2026-09-06 04:57:10.248Z | 66.875° ENE | 31.264° | 2026-09-06 05:00:10.248Z | 5.111° 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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