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: 8 hours ago
TLE from 8 hours ago
0 GENMAT-1
1 58276U 23174W 26023.94493863 .00019899 00000-0 65827-3 0 9991
2 58276 97.3806 102.1927 0006884 350.1778 9.9328 15.31352334122873Epoch: 2026-01-23T22:40Z
TLE epoch observation values (Epoch: 2026-01-23T22:40:42.697Z)
Latitude
0°
Longitude
-1.26168°
Altitude
470.237 km
Speed
7.634 km/s
True Right ascension
06h 48m 46s
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
07:36:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
473.44 km
Perigee altitude
464.013 km
Semi-major axis
6,846.863 km
Eccentricity
0.00069
Inclination
97.3806°
RAAN
102.1927°
Arg. of periapsis
350.1778°
True anomaly
9.94642°
Mean anomaly
9.9328°
Eccentric anomaly
9.93961°
Mean motion
3.83094 °/min
Orbital period
93.97 mins
BSTAR
0.00065827
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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 | 2026-01-24 18:03:26.087Z | 7.638° NNE | 2026-01-24 18:06:26.087Z | 248.427° W | 43.726° | 2026-01-24 18:09:26.087Z | 198.309° SSW |
| 5 mins | 2026-01-25 04:37:26.087Z | 124.161° SE | 2026-01-25 04:39:26.087Z | 71.103° E | 27.362° | 2026-01-25 04:42:26.087Z | 9.54° 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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