ULTP, 45605 (Decayed)

Orbit data source: Space-Track

ULTP, 45605 was a payload satellite owned by Lynk (US) in LEO that was launched on Sat, 15 Feb 2020 UTC via an FALCON 9 launch vehicle from the Wallops Island (WLPIS). 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

ULTP details

Identifier	45605, 2020-011D
Orbit	Decayed
Last TLE update	9 months ago
Origin	Lynk (US)
Manufacturer	Lynk
Mission	Decayed Commercial Communications
Bus & Motor	CUBESAT 6U, Unknown motor
Mass	~8 kg wet, ~8 kg dry
Launch date (UTC)	2020-02-15 (5 years ago)
Launch vehicle	FALCON 9
Launch site	Wallops Island (WLPIS)
Object type	Payload Rocket body Debris
Shape & HBR	Box, Unknown HBR
Radar Cross Section	0.080 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 9 months ago

0 ULTP
1 45605U 20011D   24092.15627178  .12698457  12626-4  23983-3 0  9999
2 45605  51.6088  89.4431 0002221 304.0209  56.0609 16.47421305218431

Epoch: 2024-04-01T03:45Z

Definitive object data (Epoch: 2024-04-01T03:45:01.881Z)

Latitude	-0.00007°
Longitude	-156.81536°
Altitude	146.095 km
Speed	7.82 km/s
True Right ascension	05h 57m 46s
True Declination	0° 00' 00"
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 altitude	148.118 km
Perigee altitude	145.22 km
Semi-major axis	6,524.806 km
Eccentricity	0.0002221
Inclination	51.6088°
RAAN	89.4431°
Arg. of periapsis	304.0209°
True anomaly	56.08202°
Mean anomaly	56.0609°
Eccentric anomaly	56.07146°
Mean motion	4.11805 °/min
BSTAR	0.00023983
Orbital period	87.42 mins