DECAYED
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AYRIS-1, 56988 (Decayed)

Orbit data source: Space-Track

AYRIS-1, 56988 was a payload satellite owned by NanoAvionics (IL) 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.

Not visible in the next 10 days
Identifier
56988, 2023-084BJ
Orbit
Decayed
Country
Flag of UnknownUnknown / ISRA
Related business
Manufacturer
NanoAvionics
Mission
Decayed Commercial Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, 10 kg dry
Launch date (UTC)
2023-06-12 (3 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.080 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 9 months ago

TLE from 9 months ago
0 AYRIS-1
1 56988U 23084BJ  25128.80145654  .13050227  26838-5  40001-3 0  9994
2 56988  97.5281 268.6279 0010943 246.8767 113.1382 16.44145250106566
Epoch: 2025-05-08T19:14Z
TLE epoch observation values (Epoch: 2025-05-08T19:14:05.845Z)
Latitude
0.00007°
Longitude
113.2368°
Altitude
160.868 km
Speed
7.808 km/s
True Right ascension
17h 54m 30s
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
04:15:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
158.752 km
Perigee altitude
144.461 km
Semi-major axis
6,529.744 km
Eccentricity
0.00109
Inclination
97.5281°
RAAN
268.6279°
Arg. of periapsis
246.8767°
True anomaly
113.25345°
Mean anomaly
113.1382°
Eccentric anomaly
113.19583°
Mean motion
4.11338 °/min
Orbital period
87.52 mins
BSTAR
0.00040001
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Computing Atmospheric mass density...

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