STARLINK-11650, 63312

Orbit data source: Space-Track

STARLINK-11650, 63312 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Tue, 18 Mar 2025 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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.

STARLINK-11650 will be above the set Earth location in 14 hours

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https://www.satcat.com/sats-embedded/63312?theme=dark&initialShowStats=false

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Identifier	63312, 2025-057F
Orbit	LEO
Last TLE update	4 hours ago
Origin	SPX (US)
Manufacturer	SpaceX/Seattle
Mission	Operational spacecraft
Bus & Motor	STARLINK V2M, Unknown motor
Mass	730 kg wet, ~700 kg dry
Launch date (UTC)	2025-03-18 (2 weeks ago)
Launch vehicle	FALCON 9
Launch site	Air Force Eastern Test Range (AFETR)
Object type	Payload Rocket body Debris
Shape & HBR	Unknown
Radar Cross Section	Large (>1 m²)

Expand to show TLE details & history

TLE from 4 hours ago

0 STARLINK-11650
1 63312U 25057F   25090.66668981  .00105384  00000-0  43853-3 0  9997
2 63312  43.0019 173.8102 0002181 234.4938  20.6024 15.84657857  3239

Epoch: 2025-03-31T16:00Z

Definitive object data (Epoch: 2025-03-31T16:00:01.999Z)

Latitude	-41.39897°
Longitude	-5.42649°
Altitude	328.504 km
Speed	7.712 km/s
True Right ascension	04h 15m 26s
True Declination	-41° 13' 03"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	33.54909°
Longitude	148.57079°
Altitude	319.81 km
Speed	7.721 km/s
Apparent Right ascension	13h 57m 32s
Apparent Declination	-2° 09' 09"
Sunlit	Object is in full shadow

Visualization observer readout

Local Sidereal Time	01:18:49
Azimuth	344.44° N
Elevation	-51.227°
Doppler factor	1

Orbital elements

Apogee altitude	320.742 km
Perigee altitude	317.82 km
Semi-major axis	6,697.418 km
Eccentricity	0.0002181
Inclination	43.0019°
RAAN	173.8102°
Arg. of periapsis	234.4938°
True anomaly	20.6112°
Mean anomaly	20.6024°
Eccentric anomaly	20.6068°
Mean motion	3.95988 °/min
BSTAR	0.00043853
Orbital period	90.91 mins