DECAYED

STARLINK-1804, 46704 (Decayed)

Orbit data source: Space-Track

STARLINK-1804, 46704 was a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 18 Oct 2020 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-1804 details

Identifier	46704, 2020-073AL
Orbit	Decayed
Last TLE update	7 months ago
Origin	SpaceX/Seattle (US)
Manufacturer	SpaceX/Seattle
Mission	Decayed Commercial Communications
Bus & Motor	STARLINK, Unknown motor
Mass	260 kg wet, ~248 kg dry
Launch date (UTC)	2020-10-18 (4 years ago)
Launch vehicle	FALCON 9
Launch site	Air Force Eastern Test Range (AFETR)
Object type	Payload Rocket body Debris
Shape & HBR	Box + 1 Pan, 8.86 m
Radar Cross Section	13.562 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 7 months ago

0 STARLINK-1804
1 46704U 20073AL  24161.30844560  .34335862  12381-4  29875-2 0  9993
2 46704  53.0294 164.7593 0004460 326.4147 133.9332 16.38508121202274

Epoch: 2024-06-09T07:24Z

Definitive object data (Epoch: 2024-06-09T07:24:09.699Z)

Latitude	51.95759°
Longitude	-97.47539°
Altitude	178.002 km
Speed	7.805 km/s
True Right ascension	18h 06m 54s
True Declination	51° 46' 33"
Sunlit	Object was in full shadow 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 altitude	172.985 km
Perigee altitude	167.144 km
Semi-major axis	6,548.201 km
Eccentricity	0.000446
Inclination	53.0294°
RAAN	164.7593°
Arg. of periapsis	326.4147°
True anomaly	133.96999°
Mean anomaly	133.9332°
Eccentric anomaly	133.9516°
Mean motion	4.096 °/min
BSTAR	0.0029875
Orbital period	87.89 mins