DECAYED
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SPEI SATELLES, 56991 (Decayed)

Orbit data source: Space-Track

SPEI SATELLES, 56991 was an Italian 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.

Not visible in the next 10 days
Identifier
56991, 2023-084BT
Orbit
Decayed
Country
Flag of ITIT
Related business
Manufacturer
PolyTorino
Mission
Decayed Amateur Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
3 kg wet, 3 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
0.035 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 11 months ago

TLE from 11 months ago
0 SPEI SATELLES
1 56991U 23084BT  25093.89040148  .09884965  26180-5  77059-3 0  9992
2 56991  97.5226 233.3404 0013114 278.3259  81.6553 16.39623223101252
Epoch: 2025-04-03T21:22Z
TLE epoch observation values (Epoch: 2025-04-03T21:22:10.687Z)
Latitude
-0.00003°
Longitude
80.33913°
Altitude
168.817 km
Speed
7.806 km/s
True Right ascension
15h 33m 21s
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
19:25:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
172.197 km
Perigee altitude
155.04 km
Semi-major axis
6,541.756 km
Eccentricity
0.00131
Inclination
97.5226°
RAAN
233.3404°
Arg. of periapsis
278.3259°
True anomaly
81.80402°
Mean anomaly
81.6553°
Eccentric anomaly
81.72966°
Mean motion
4.10206 °/min
Orbital period
87.76 mins
BSTAR
0.00077059
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Computing Atmospheric mass density...

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