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: 6 hours ago
TLE from 6 hours ago
0 GNOMES-4
1 58462U 23185A 26002.94359294 .00007695 00000-0 63045-3 0 9997
2 58462 97.5203 65.9395 0011219 123.3342 236.8958 14.99496625114510Epoch: 2026-01-02T22:38Z
TLE epoch observation values (Epoch: 2026-01-02T22:38:46.430Z)
Latitude
0.00007°
Longitude
-16.33052°
Altitude
575.773 km
Speed
7.57 km/s
True Right ascension
04h 23m 45s
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
04:42:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
573.239 km
Perigee altitude
557.659 km
Semi-major axis
6,943.586 km
Eccentricity
0.00112
Inclination
97.5203°
RAAN
65.9395°
Arg. of periapsis
123.3342°
True anomaly
236.78819°
Mean anomaly
236.8958°
Eccentric anomaly
236.84199°
Mean motion
3.75118 °/min
Orbital period
95.97 mins
BSTAR
0.00063045
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-01-03 05:11:37.158Z | 238.064° WSW | 2026-01-03 05:13:37.158Z | 270.682° WNW | 14.709° | 2026-01-03 05:15:37.158Z | 301.673° NW |
| 6 mins | 2026-01-03 16:50:37.158Z | 18.366° NNE | 2026-01-03 16:52:37.158Z | 46.382° ENE | 42.461° | 2026-01-03 16:56:37.158Z | 187.413° SSW |
| 5 mins | 2026-01-04 03:37:37.158Z | 125.974° SE | 2026-01-04 03:39:37.158Z | 69.775° E | 32.264° | 2026-01-04 03:42:37.158Z | 7.825° 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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