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: 10 hours ago
TLE from 10 hours ago
0 GNOMES-4
1 58462U 23185A 26263.61090594 .00001826 00000-0 14628-3 0 9998
2 58462 97.4728 317.2380 0010807 10.1830 349.9611 15.01293793153605Epoch: 2026-09-20T14:39Z
TLE epoch observation values (Epoch: 2026-09-20T14:39:42.273Z)
Latitude
-0.00008°
Longitude
97.80926°
Altitude
558.581 km
Speed
7.586 km/s
True Right ascension
21h 08m 57s
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
18:03:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
567.397 km
Perigee altitude
552.401 km
Semi-major axis
6,938.036 km
Eccentricity
0.00108
Inclination
97.4728°
RAAN
317.238°
Arg. of periapsis
10.183°
True anomaly
349.93948°
Mean anomaly
349.9611°
Eccentric anomaly
349.95029°
Mean motion
3.75568 °/min
Orbital period
95.85 mins
BSTAR
0.00014628
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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 | 2026-09-21 03:34:32.051Z | 159.644° S | 2026-09-21 03:38:32.051Z | 44.652° NE | 68.957° | 2026-09-21 03:41:32.051Z | 353.59° N |
| 6 mins | 2026-09-21 16:49:32.051Z | 359.06° N | 2026-09-21 16:52:32.051Z | 271.723° WNW | 56.315° | 2026-09-21 16:55:32.051Z | 209.419° 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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