GNOMES-4, 58462
Orbit data source: Space-Track
GNOMES-4, 58462 is a payload satellite owned by PlanetiQ (US) in SSO that was launched on Fri, 01 Dec 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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58462 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Blue Canyon
Mission
Operational Commercial Communications
Bus & Motor
XSAT, Unknown motor
Mass
~30 kg wet, ~30 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.3 m
Radar Cross Section
0.162 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 GNOMES-4
1 58462U 23185A 26208.28587850 .00003629 00000-0 28836-3 0 9995
2 58462 97.4822 263.9738 0008737 177.1903 182.9372 15.01027682145307Epoch: 2026-07-27T06:51Z
TLE epoch observation values (Epoch: 2026-07-27T06:51:39.902Z)
Latitude
-0.00004°
Longitude
-143.91409°
Altitude
572.847 km
Speed
7.571 km/s
True Right ascension
17h 35m 53s
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
02:03:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
566.783 km
Perigee altitude
554.658 km
Semi-major axis
6,938.857 km
Eccentricity
0.00087
Inclination
97.4822°
RAAN
263.9738°
Arg. of periapsis
177.1903°
True anomaly
182.93208°
Mean anomaly
182.9372°
Eccentric anomaly
182.93464°
Mean motion
3.75501 °/min
Orbital period
95.87 mins
BSTAR
0.00028836
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Other satellites on launch #185 in the year 2023 (2023-12-01 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.GNOMES-4 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 | 2026-07-27 17:02:10.095Z | 350.767° N | 2026-07-27 17:04:10.095Z | 305.499° NW | 34.894° | 2026-07-27 17:08:10.095Z | 213.97° SW |
| 6 mins | 2026-07-28 03:48:10.095Z | 165.732° S | 2026-07-28 03:50:10.095Z | 152.621° SSE | 44.711° | 2026-07-28 03:54:10.095Z | 348.552° N |
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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