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USA 294, 45110

Orbit data source: McCants

USA 294, 45110 is a payload satellite owned by NRO (US) in LEO that was launched on Fri, 31 Jan 2020 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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

USA 294 details

Identifier	45110, 2020-007A
Orbit	LEO
Last TLE update	1 year ago
Origin	NRO (US)
Manufacturer	HARRL3?
Mission	Operational Defense Technology
Bus & Motor	NRO UNK SMALL, Unknown motor
Mass	~150 kg wet, ~150 kg dry
Launch date (UTC)	2020-01-31 (5 years ago)
Launch vehicle	ELECTRON
Launch site	Rocket Lab Launch Complex (RLLC)
Object type	Payload Rocket body Debris
Shape & HBR	Box + 2 Pan, Unknown HBR
Radar Cross Section	2.045 m²

Expand to show TLE details & history

TLE from 1 year ago

USA 294
1 45110U 20007A   23232.80903846 0.00110000  00000-0  32750-2 0    04
2 45110  69.9913 111.5649 0009740 159.9373 200.0626 15.34502222    06

Epoch: 2023-08-20T19:25Z

Definitive object data (Epoch: 2023-08-20T19:25:00.922Z)

Latitude	-0.14763°
Longitude	-148.61571°
Altitude	471.141 km
Speed	7.627 km/s
True Right ascension	07h 26m 02s
True Declination	0° 08' 48"
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	466.976 km
Perigee altitude	453.655 km
Semi-major axis	6,838.453 km
Eccentricity	0.000974
Inclination	69.9913°
RAAN	111.5649°
Arg. of periapsis	159.9373°
True anomaly	200.02436°
Mean anomaly	200.0626°
Eccentric anomaly	200.04347°
Mean motion	3.83801 °/min
BSTAR	0.003275
Orbital period	93.8 mins