GNOMES-1, 46266
Orbit data source: Space-Track
GNOMES-1, 46266 is a payload satellite owned by PlanetiQ (US) in SSO that was launched on Sun, 30 Aug 2020 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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46266 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Blue Canyon
Mission
Operational Commercial Meteo Radio Occ.
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, Unknown HBR
Radar Cross Section
0.162 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 GNOMES-1
1 46266U 20059B 25355.13241093 .00002865 00000-0 24011-3 0 9995
2 46266 97.8060 200.2074 0003319 176.0596 184.0654 14.99210827288909Epoch: 2025-12-21T03:10Z
TLE epoch observation values (Epoch: 2025-12-21T03:10:40.304Z)
Latitude
0.00004°
Longitude
62.59021°
Altitude
574.684 km
Speed
7.572 km/s
True Right ascension
13h 20m 49s
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
08:22:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
568.649 km
Perigee altitude
564.039 km
Semi-major axis
6,944.481 km
Eccentricity
0.00033
Inclination
97.806°
RAAN
200.2074°
Arg. of periapsis
176.0596°
True anomaly
184.0627°
Mean anomaly
184.0654°
Eccentric anomaly
184.06405°
Mean motion
3.75045 °/min
Orbital period
95.99 mins
BSTAR
0.00024011
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Other satellites on launch #59 in the year 2020 (2020-08-30 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-1 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 | 2025-12-21 12:56:51.699Z | 105.151° ESE | 2025-12-21 12:58:51.699Z | 69.714° E | 18.822° | 2025-12-21 13:01:51.699Z | 21.029° NNE |
| 5 mins | 2025-12-21 14:31:51.699Z | 216.98° SW | 2025-12-21 14:33:51.699Z | 263.431° W | 26.616° | 2025-12-21 14:36:51.699Z | 320.983° NNW |
| 5 mins | 2025-12-22 02:11:51.699Z | 49.08° ENE | 2025-12-22 02:13:51.699Z | 100.489° ESE | 29.026° | 2025-12-22 02:16:51.699Z | 159.393° S |
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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