GNOMES-3, 52158
Orbit data source: Space-Track
GNOMES-3, 52158 is a payload satellite owned by PlanetiQ (US) in SSO that was launched on Fri, 01 Apr 2022 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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52158 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: 11 hours ago
TLE from 11 hours ago
0 GNOMES-3
1 52158U 22033B 26099.43944193 .00002128 00000-0 25648-3 0 9995
2 52158 97.8244 176.9846 0011096 181.3256 178.7931 14.84835346217137Epoch: 2026-04-09T10:32Z
TLE epoch observation values (Epoch: 2026-04-09T10:32:47.782Z)
Latitude
-0.00007°
Longitude
-178.90192°
Altitude
624.892 km
Speed
7.542 km/s
True Right ascension
11h 47m 56s
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
03:53:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
618.889 km
Perigee altitude
603.378 km
Semi-major axis
6,989.271 km
Eccentricity
0.00111
Inclination
97.8244°
RAAN
176.9846°
Arg. of periapsis
181.3256°
True anomaly
178.79577°
Mean anomaly
178.7931°
Eccentric anomaly
178.79444°
Mean motion
3.71446 °/min
Orbital period
96.92 mins
BSTAR
0.00025648
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Other satellites on launch #33 in the year 2022 (2022-04-01 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-3 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 | 2026-04-10 04:28:11.985Z | 131.007° SE | 2026-04-10 04:31:11.985Z | 84.235° E | 27.31° | 2026-04-10 04:35:11.985Z | 9.788° NNE |
| 4 mins | 2026-04-10 06:06:11.985Z | 237.893° WSW | 2026-04-10 06:08:11.985Z | 275.622° WNW | 19.25° | 2026-04-10 06:10:11.985Z | 307.314° NW |
| 7 mins | 2026-04-10 17:51:11.985Z | 19.935° NNE | 2026-04-10 17:54:11.985Z | 91.579° ESE | 43.11° | 2026-04-10 17:58:11.985Z | 185.153° SSW |
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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