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 26264.78017383 .00000993 00000-0 12151-3 0 9992
2 52158 97.8159 339.3428 0010951 14.6596 345.4934 14.85366645241671Epoch: 2026-09-21T18:43Z
TLE epoch observation values (Epoch: 2026-09-21T18:43:27.018Z)
Latitude
-0.00011°
Longitude
57.82515°
Altitude
608.054 km
Speed
7.559 km/s
True Right ascension
22h 37m 22s
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
21:56:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
617.117 km
Perigee altitude
601.813 km
Semi-major axis
6,987.602 km
Eccentricity
0.0011
Inclination
97.8159°
RAAN
339.3428°
Arg. of periapsis
14.6596°
True anomaly
345.46192°
Mean anomaly
345.4934°
Eccentric anomaly
345.47767°
Mean motion
3.71579 °/min
Orbital period
96.88 mins
BSTAR
0.00012151
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-22 06:10:26.123Z | 230.13° WSW | 2026-09-22 06:12:26.123Z | 260.184° W | 16.851° | 2026-09-22 06:15:26.123Z | 306.46° NW |
| 7 mins | 2026-09-22 17:56:26.123Z | 14.714° NNE | 2026-09-22 17:59:26.123Z | 171.79° S | 76.495° | 2026-09-22 18:03:26.123Z | 191.822° SSW |
| 4 mins | 2026-09-23 04:48:26.123Z | 148.434° SSE | 2026-09-23 04:51:26.123Z | 83.446° E | 56.009° | 2026-09-23 04:52:26.123Z | 29.639° NE |
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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