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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Edit Public Description
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: 9 hours ago
TLE from 9 hours ago
0 GENMAT-1
1 58276U 23174W 25290.11859027 .00017551 00000-0 63556-3 0 9993
2 58276 97.3943 3.9334 0007050 339.5421 20.5536 15.28431646107768Epoch: 2025-10-17T02:50Z
TLE epoch observation values (Epoch: 2025-10-17T02:50:46.199Z)
Latitude
0.00005°
Longitude
-64.62765°
Altitude
479.074 km
Speed
7.629 km/s
True Right ascension
00h 15m 44s
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
06:59:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
482.287 km
Perigee altitude
472.621 km
Semi-major axis
6,855.591 km
Eccentricity
0.00071
Inclination
97.3943°
RAAN
3.9334°
Arg. of periapsis
339.5421°
True anomaly
20.58199°
Mean anomaly
20.5536°
Eccentric anomaly
20.56779°
Mean motion
3.82363 °/min
Orbital period
94.15 mins
BSTAR
0.00063556
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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 | 2025-10-17 17:33:23.722Z | 30.841° NE | 2025-10-17 17:36:23.722Z | 119.908° SE | 33.535° | 2025-10-17 17:38:23.722Z | 165.626° S |
| 4 mins | 2025-10-18 05:42:23.722Z | 227.888° WSW | 2025-10-18 05:43:23.722Z | 255.409° W | 24.895° | 2025-10-18 05:46:23.722Z | 321.247° NNW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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