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: 15 hours ago
TLE from 15 hours ago
0 GNOMES-1
1 46266U 20059B 25302.53056916 .00004684 00000-0 39403-3 0 9991
2 46266 97.8115 147.5182 0006351 48.0193 312.1570 14.98738354281029Epoch: 2025-10-29T12:44Z
TLE epoch observation values (Epoch: 2025-10-29T12:44:01.175Z)
Latitude
0.00003°
Longitude
-81.58908°
Altitude
570.882 km
Speed
7.577 km/s
True Right ascension
09h 50m 04s
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
23:26:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.217 km
Perigee altitude
563.394 km
Semi-major axis
6,945.942 km
Eccentricity
0.00064
Inclination
97.8115°
RAAN
147.5182°
Arg. of periapsis
48.0193°
True anomaly
312.10302°
Mean anomaly
312.157°
Eccentric anomaly
312.13001°
Mean motion
3.74927 °/min
Orbital period
96.02 mins
BSTAR
0.00039403
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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 | 2025-10-30 12:54:47.408Z | 115.845° SE | 2025-10-30 12:57:47.408Z | 65.886° ENE | 19.526° | 2025-10-30 12:59:47.408Z | 29.555° NE |
| 5 mins | 2025-10-30 14:30:47.408Z | 220.924° SW | 2025-10-30 14:32:47.408Z | 267.604° W | 25.268° | 2025-10-30 14:35:47.408Z | 321.16° NNW |
| 5 mins | 2025-10-31 02:10:47.408Z | 46.656° ENE | 2025-10-31 02:12:47.408Z | 99.039° ESE | 30.506° | 2025-10-31 02:15:47.408Z | 160.949° 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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