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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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: 12 hours ago
TLE from 12 hours ago
0 GNOMES-3
1 52158U 22033B 25286.94026353 .00003579 00000-0 43922-3 0 9993
2 52158 97.8474 2.5637 0012141 54.9447 305.2904 14.83662852190803Epoch: 2025-10-13T22:33Z
TLE epoch observation values (Epoch: 2025-10-13T22:33:58.768Z)
Latitude
-0.00007°
Longitude
1.33301°
Altitude
615.913 km
Speed
7.554 km/s
True Right ascension
00h 10m 15s
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
04:54:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
623.31 km
Perigee altitude
606.33 km
Semi-major axis
6,992.957 km
Eccentricity
0.00121
Inclination
97.8474°
RAAN
2.5637°
Arg. of periapsis
54.9447°
True anomaly
305.17674°
Mean anomaly
305.2904°
Eccentric anomaly
305.23358°
Mean motion
3.71152 °/min
Orbital period
97 mins
BSTAR
0.00043922
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-14 16:58:08.110Z | 59.478° ENE | 2025-10-14 17:00:08.110Z | 89.925° E | 15.785° | 2025-10-14 17:02:08.110Z | 121.784° SE |
| 6 mins | 2025-10-14 18:34:08.110Z | 345.548° N | 2025-10-14 18:36:08.110Z | 302.322° NW | 32.263° | 2025-10-14 18:40:08.110Z | 220.808° SW |
| 6 mins | 2025-10-15 05:27:08.110Z | 186.014° SSW | 2025-10-15 05:30:08.110Z | 278.616° WNW | 39.664° | 2025-10-15 05:33:08.110Z | 336.003° NNW |
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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