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: 6 hours ago
TLE from 6 hours ago
0 GENMAT-1
1 58276U 23174W 26129.18351691 .00007854 00000-0 24151-3 0 9999
2 58276 97.3672 207.0789 0005788 334.2024 25.8929 15.33938265138993Epoch: 2026-05-09T04:24Z
TLE epoch observation values (Epoch: 2026-05-09T04:24:15.861Z)
Latitude
-0.00003°
Longitude
-85.99179°
Altitude
463.623 km
Speed
7.637 km/s
True Right ascension
13h 48m 18s
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
19:01:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
464.98 km
Perigee altitude
457.063 km
Semi-major axis
6,839.159 km
Eccentricity
0.00058
Inclination
97.3672°
RAAN
207.0789°
Arg. of periapsis
334.2024°
True anomaly
25.92188°
Mean anomaly
25.8929°
Eccentric anomaly
25.90739°
Mean motion
3.83742 °/min
Orbital period
93.81 mins
BSTAR
0.00024151
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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 | 2026-05-09 17:30:22.318Z | 44.76° NE | 2026-05-09 17:32:22.318Z | 94.096° ESE | 26.263° | 2026-05-09 17:35:22.318Z | 158.627° S |
| 6 mins | 2026-05-10 05:34:22.318Z | 188.79° SSW | 2026-05-10 05:37:22.318Z | 252.796° W | 33.874° | 2026-05-10 05:40:22.318Z | 331.313° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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