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DECAYED

STARLINK-31915, 59796 (Decayed)

Orbit data source: Space-Track

STARLINK-31915, 59796 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sat, 18 May 2024 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
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STARLINK-31915 details
Identifier
59796, 2024-093Q
Orbit
Decayed
Last TLE update5 months ago
Origin
Flag of USSpaceX/Seattle (US)
ManufacturerSpaceX/Seattle
MissionDecayed spacecraft
Bus & MotorSTARLINK V2M, Unknown motor
Mass800 kg wet, ~750 kg dry
Launch date (UTC)
2024-05-18 (5 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBRUnknown
Radar Cross SectionLarge (>1 m²)

Expand to show TLE details & history

TLE from 5 months ago
0 STARLINK-31915
1 59796U 24093Q   24155.76002328  .26324036  92744-5  35200-2 0  9998
2 59796  42.9880 275.4664 0006477 337.3134 139.2662 16.34370322  3868
Epoch: 2024-06-03T18:14Z
Definitive object data (Epoch: 2024-06-03T18:14:26.011Z)
Latitude37.70356°
Longitude-126.3726°
Altitude185.964 km
Speed7.799 km/s
True Right ascension02h 39m 42s
True Declination37° 31' 22"
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
Apogee187.107 km
Perigee178.608 km
Semi-major axis6,560.995 km
Eccentricity0.0006477
Inclination42.988°
RAAN275.4664°
Arg. of periapsis337.3134°
True anomaly139.3146°
Mean anomaly139.2662°
Eccentric anomaly139.2904°
Mean motion4.08403 °/min
BSTAR0.00352
Period88.15 mins
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STARLINK-31915 Visibility forecast

Observer location: undefined°, undefined

This satellite is decayed
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Start Az.
Max El. time (UTC)
Max El. Az.
Max El.
End time (UTC)
End Az.
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