DECAYED

STARLINK-5693, 55482 (Decayed)

Orbit data source: Space-Track

STARLINK-5693, 55482 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Thu, 02 Feb 2023 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.

Not visible in the next 10 days
STARLINK-5693 details
Identifier
55482, 2023-015AK
Orbit
Decayed
Last TLE update3 weeks ago
Origin
Flag of USSpaceX/Seattle (US)
ManufacturerSpaceX/Seattle
MissionDecayed Commercial Communications
Bus & MotorSTARLINK, Unknown motor
Mass305 kg wet, ~290 kg dry
Launch date (UTC)
2023-02-02 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBRBox + 1 Pan, 8.86 m
Radar Cross Section13.562 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 3 weeks ago
0 STARLINK-5693
1 55482U 23015AK  25029.05860583  .25797387  95571-5  21671-3 0  9998
2 55482  42.9852 348.1107 0008572 274.4437 140.4065 16.51422629109898
Epoch: 2025-01-29T01:24Z
Definitive object data (Epoch: 2025-01-29T01:24:23.543Z)
Latitude34.04691°
Longitude-115.42331°
Altitude141.107 km
Speed7.824 km/s
True Right ascension02h 16m 55s
True Declination33° 52' 21"
Sunlit
Object was in daylight at TLE epoch
Visualization observer readout
Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.
Visualization observer readout
Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.
Orbital elements
Apogee altitude143.229 km
Perigee altitude132.058 km
Semi-major axis6,515.78 km
Eccentricity0.0008572
Inclination42.9852°
RAAN348.1107°
Arg. of periapsis274.4437°
True anomaly140.46905°
Mean anomaly140.4065°
Eccentric anomaly140.43778°
Mean motion4.12661 °/min
BSTAR0.00021671
Orbital period87.24 mins
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STARLINK-5693 Visibility forecast

Observer location: undefined°, undefined

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