DECAYED
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AII-DELTA, 56987 (Decayed)

Orbit data source: Space-Track

AII-DELTA, 56987 was a Lithuanian payload satellite in LEO that was launched on Mon, 12 Jun 2023 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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Identifier
56987, 2023-084BH
Orbit
Decayed
Country
Flag of LTLT / LTU
Related business
Manufacturer
NanoAvionics US
Mission
Decayed Commercial Sigint
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
2023-06-12 (3 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.3 m
Radar Cross Section
0.104 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 1 year ago

TLE from 1 year ago
0 AII-DELTA
1 56987U 23084BH  25024.48994909  .16331298  26821-5  26144-3 0  9994
2 56987  97.4923 162.3956 0009408 257.0751 102.9501 16.47863696 90633
Epoch: 2025-01-24T11:45Z
TLE epoch observation values (Epoch: 2025-01-24T11:45:31.601Z)
Latitude
-0.00009°
Longitude
-138.03843°
Altitude
149.607 km
Speed
7.816 km/s
True Right ascension
10h 49m 34s
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
07:20:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
147.903 km
Perigee altitude
135.635 km
Semi-major axis
6,519.906 km
Eccentricity
0.00094
Inclination
97.4923°
RAAN
162.3956°
Arg. of periapsis
257.0751°
True anomaly
103.05514°
Mean anomaly
102.9501°
Eccentric anomaly
103.00262°
Mean motion
4.12269 °/min
Orbital period
87.32 mins
BSTAR
0.00026144
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