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: 11 hours ago
TLE from 11 hours ago
0 GENMAT-1
1 58276U 23174W 26080.96056139 .00016322 00000-0 51530-3 0 9991
2 58276 97.3711 158.9899 0008255 130.5946 229.6015 15.32884739131601Epoch: 2026-03-21T23:03Z
TLE epoch observation values (Epoch: 2026-03-21T23:03:12.504Z)
Latitude
-0.00007°
Longitude
-6.28597°
Altitude
473.985 km
Speed
7.627 km/s
True Right ascension
10h 35m 57s
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
14:48:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
469.806 km
Perigee altitude
458.509 km
Semi-major axis
6,842.295 km
Eccentricity
0.00083
Inclination
97.3711°
RAAN
158.9899°
Arg. of periapsis
130.5946°
True anomaly
229.52951°
Mean anomaly
229.6015°
Eccentric anomaly
229.5655°
Mean motion
3.83478 °/min
Orbital period
93.88 mins
BSTAR
0.0005153
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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 | 2026-03-22 18:24:31.474Z | 353.609° N | 2026-03-22 18:27:31.474Z | 276.987° WNW | 32.177° | 2026-03-22 18:30:31.474Z | 216.423° SW |
| 5 mins | 2026-03-23 04:57:31.474Z | 149.031° SSE | 2026-03-23 04:59:31.474Z | 102.531° ESE | 38.406° | 2026-03-23 05:02:31.474Z | 359.998° N |
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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