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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Edit Public Description
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: 15 hours ago
TLE from 15 hours ago
0 GNOMES-4
1 58462U 23185A 25306.53612876 .00004403 00000-0 37013-3 0 9996
2 58462 97.5303 6.6499 0011070 345.3932 14.6970 14.98738032105318Epoch: 2025-11-02T12:52Z
TLE epoch observation values (Epoch: 2025-11-02T12:52:01.524Z)
Latitude
-0.00002°
Longitude
131.5931°
Altitude
566.41 km
Speed
7.582 km/s
True Right ascension
00h 26m 35s
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
00:01:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
575.483 km
Perigee altitude
560.105 km
Semi-major axis
6,945.931 km
Eccentricity
0.00111
Inclination
97.5303°
RAAN
6.6499°
Arg. of periapsis
345.3932°
True anomaly
14.72923°
Mean anomaly
14.697°
Eccentric anomaly
14.71311°
Mean motion
3.74928 °/min
Orbital period
96.02 mins
BSTAR
0.00037013
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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 | 2025-11-03 05:00:50.143Z | 215.39° SW | 2025-11-03 05:03:50.143Z | 266.963° W | 20.611° | 2025-11-03 05:06:50.143Z | 316.56° NNW |
| 5 mins | 2025-11-03 16:41:50.143Z | 35.587° NE | 2025-11-03 16:43:50.143Z | 97.109° ESE | 37.591° | 2025-11-03 16:46:50.143Z | 171.131° S |
| 5 mins | 2025-11-04 03:28:50.143Z | 112.358° ESE | 2025-11-04 03:30:50.143Z | 67.272° ENE | 24.748° | 2025-11-04 03:33:50.143Z | 14.378° 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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