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DECAYED
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GNOMES-2, 48910 (Decayed)

Orbit data source: Space-Track

GNOMES-2, 48910 was a payload satellite owned by PlanetiQ (US) in LEO that was launched on Wed, 30 Jun 2021 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). Payloads include a variety of satellites, spacecraft, and rockets 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.

Next visibility unknown
No 3D visualization available: RSO Decayed
GNOMES-2 details
Identifier
48910, 2021-059AH
Orbit
Decayed
Last TLE update5 months ago
Origin
Flag of USPlanetiQ (US)
ManufacturerBlue Canyon
MissionDecayed Commercial Communications
Bus & MotorXSAT, Unknown motor
Mass~30 kg wet, ~30 kg dry
Launch date (UTC)
2021-06-30 (3 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBRBox + 2 Pan, 0.6 m
Radar Cross Section0.162 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 5 months ago
0 GNOMES-2
1 48910U 21059AH  24131.55719574  .17347472  27438-5  21614-3 0  9994
2 48910  97.5948 291.7408 0012035 255.9239 104.0727 16.49126212160263
Epoch: 2024-05-10T13:22Z
Definitive object data (Epoch: 2024-05-10T13:22:21.711Z)
Latitude-0.00007°
Longitude-137.68564°
Altitude146.812 km
Speed7.817 km/s
True Right ascension19h 26m 57s
True Declination0° 00' 00"
Sunlit
Object was in full shadow at TLE epoch
Predictive object data (real-time)
Latitude0.85168°
Longitude71.25238°
Altitude2,446.654 km
Speed69,826.665 km/s
Apparent Right ascension07h 29m 01s
Apparent Declination-20° 58' 10"
Sunlit
Object is in daylight
Predictive observer data (real-time)
Local Sidereal Time15:32:55
Azimuth272.424° WNW
Elevation-36.743°
Doppler factor1.038
Orbital elements
Apogee146.285 km
Perigee130.599 km
Semi-major axis6,516.579 km
Eccentricity0.0012035
Inclination97.5948°
RAAN291.7408°
Arg. of periapsis255.9239°
True anomaly104.20642°
Mean anomaly104.0727°
Eccentric anomaly104.13957°
Mean motion4.12585 °/min
BSTAR0.00021614
Period87.25 mins
No data available

GNOMES-2 Visibility forecast

Observer location: 39.9160978°, -105.1181434

This satellite is decayed
Span
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Max El. time (UTC)
Max El. Az.
Max El.
End time (UTC)
End Az.