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: 10 hours ago
TLE from 10 hours ago
0 GNOMES-3
1 52158U 22033B 26170.73088867 .00001402 00000-0 17017-3 0 9990
2 52158 97.8233 246.9941 0009752 320.6894 39.3612 14.85092643227710Epoch: 2026-06-19T17:32Z
TLE epoch observation values (Epoch: 2026-06-19T17:32:28.781Z)
Latitude
-0.00001°
Longitude
75.91852°
Altitude
611.056 km
Speed
7.557 km/s
True Right ascension
16h 27m 58s
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
14:08:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
617.141 km
Perigee altitude
603.511 km
Semi-major axis
6,988.463 km
Eccentricity
0.00098
Inclination
97.8233°
RAAN
246.9941°
Arg. of periapsis
320.6894°
True anomaly
39.43214°
Mean anomaly
39.3612°
Eccentric anomaly
39.39666°
Mean motion
3.7151 °/min
Orbital period
96.9 mins
BSTAR
0.00017017
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-20 04:58:38.602Z | 159.603° S | 2026-06-20 05:02:38.602Z | 65.178° ENE | 43.803° | 2026-06-20 05:06:38.602Z | 351.7° N |
| 6 mins | 2026-06-20 18:22:38.602Z | 352.544° N | 2026-06-20 18:25:38.602Z | 262.739° W | 36.222° | 2026-06-20 18:28:38.602Z | 214.508° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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