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: 13 hours ago
TLE from 13 hours ago
0 GNOMES-3
1 52158U 22033B 26042.15286176 .00002623 00000-0 31706-3 0 9994
2 52158 97.8336 120.7155 0011128 23.5867 336.5855 14.84528801208639Epoch: 2026-02-11T03:40Z
TLE epoch observation values (Epoch: 2026-02-11T03:40:07.256Z)
Latitude
-0.00007°
Longitude
-75.53779°
Altitude
610.954 km
Speed
7.558 km/s
True Right ascension
08h 02m 51s
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
18:41:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
619.876 km
Perigee altitude
604.318 km
Semi-major axis
6,990.234 km
Eccentricity
0.00111
Inclination
97.8336°
RAAN
120.7155°
Arg. of periapsis
23.5867°
True anomaly
336.53476°
Mean anomaly
336.5855°
Eccentric anomaly
336.56014°
Mean motion
3.71369 °/min
Orbital period
96.94 mins
BSTAR
0.00031706
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-02-11 17:11:21.648Z | 42.777° NE | 2026-02-11 17:14:21.648Z | 90.181° ESE | 22.166° | 2026-02-11 17:17:21.648Z | 143.231° SSE |
| 5 mins | 2026-02-11 18:48:21.648Z | 334.494° NNW | 2026-02-11 18:50:21.648Z | 295.17° NW | 24.804° | 2026-02-11 18:53:21.648Z | 239.306° WSW |
| 4 mins | 2026-02-12 04:06:21.648Z | 92.306° ESE | 2026-02-12 04:08:21.648Z | 57.708° ENE | 16.71° | 2026-02-12 04:10:21.648Z | 27.961° NE |
| 6 mins | 2026-02-12 05:41:21.648Z | 206.875° SW | 2026-02-12 05:43:21.648Z | 253.292° W | 31.41° | 2026-02-12 05:47:21.648Z | 329.831° 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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