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: 4 hours ago
TLE from 4 hours ago
0 GNOMES-4
1 58462U 23185A 26254.81287772 .00002208 00000-0 17610-3 0 9995
2 58462 97.4745 308.7717 0011638 36.8892 323.3131 15.01257455152280Epoch: 2026-09-11T19:30Z
TLE epoch observation values (Epoch: 2026-09-11T19:30:32.635Z)
Latitude
-0.00001°
Longitude
25.30487°
Altitude
559.605 km
Speed
7.585 km/s
True Right ascension
20h 35m 05s
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
15:29:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
568.086 km
Perigee altitude
551.937 km
Semi-major axis
6,938.148 km
Eccentricity
0.00116
Inclination
97.4745°
RAAN
308.7717°
Arg. of periapsis
36.8892°
True anomaly
323.23333°
Mean anomaly
323.3131°
Eccentric anomaly
323.27322°
Mean motion
3.75559 °/min
Orbital period
95.86 mins
BSTAR
0.0001761
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-12 03:37:41.911Z | 161.166° S | 2026-09-12 03:40:41.911Z | 134.937° SE | 64.803° | 2026-09-12 03:44:41.911Z | 351.801° N |
| 6 mins | 2026-09-12 16:52:41.911Z | 355.763° N | 2026-09-12 16:55:41.911Z | 257.859° W | 50.083° | 2026-09-12 16:58:41.911Z | 210.213° SW |
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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