DECAYED
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GAMA-ALPHA, 55084 (Decayed)

Orbit data source: Space-Track

GAMA-ALPHA, 55084 was a Lithuanian payload satellite in LEO that was launched on Tue, 03 Jan 2023 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.

Not visible in the next 10 days
Identifier
55084, 2023-001CD
Orbit
Decayed
Country
Flag of LTLT / LTU
Related business
Manufacturer
NanoAvionics
Mission
Decayed Commercial Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
2023-01-03 (3 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 1 Sail, 4.3 m
Radar Cross Section
0.080 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 2 months ago

TLE from 2 months ago
0 GAMA-ALPHA
1 55084U 23001CD  26015.15329531  .13047569  25563-5  23669-3 0  9991
2 55084  97.3244  99.1987 0005972 264.5748  95.4875 16.47498174169965
Epoch: 2026-01-15T03:40Z
TLE epoch observation values (Epoch: 2026-01-15T03:40:44.714Z)
Latitude
0.00002°
Longitude
-70.59863°
Altitude
149.57 km
Speed
7.816 km/s
True Right ascension
06h 36m 47s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
02:51:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
146.621 km
Perigee altitude
138.832 km
Semi-major axis
6,520.863 km
Eccentricity
0.0006
Inclination
97.3244°
RAAN
99.1987°
Arg. of periapsis
264.5748°
True anomaly
95.55562°
Mean anomaly
95.4875°
Eccentric anomaly
95.52156°
Mean motion
4.12179 °/min
Orbital period
87.34 mins
BSTAR
0.00023669
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Computing Atmospheric mass density...

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