ELECTRON R/B, 63360

Orbit data source: Space-Track

ELECTRON R/B, 63360 is space debris in SSO originally from an American launch on Wed, 26 Mar 2025 UTC launched from the Rocket Lab Launch Complex (RLLC). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

Not visible in the next 10 days

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Identifier	63360, 2025-061K
Orbit	SSO
Last TLE update	7 hours ago
Origin	US
Manufacturer	Unknown
Mission	Spacecraft
Bus & Motor	Unknown
Mass	Unknown
Launch date (UTC)	2025-03-26 (1 week ago)
Launch vehicle	Unknown
Launch site	Rocket Lab Launch Complex (RLLC)
Object type	Payload Rocket body Debris
Shape & HBR	Unknown
Radar Cross Section	Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history

TLE from 7 hours ago

0 ELECTRON R/B
1 63360U 25061K   25091.87334475  .03581798  22058-5  12926-2 0  9995
2 63360  97.4909  69.1671 0157161 204.7002 214.2059 16.01878041   980

Epoch: 2025-04-01T20:57Z

Definitive object data (Epoch: 2025-04-01T20:57:36.986Z)

Latitude	57.24372°
Longitude	-87.4318°
Altitude	365.822 km
Speed	7.645 km/s
True Right ascension	03h 49m 45s
True Declination	57° 04' 40"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	15.56644°
Longitude	-77.45066°
Altitude	364.248 km
Speed	7.635 km/s
Apparent Right ascension	01h 50m 44s
Apparent Declination	-16° 39' 38"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	Unknown
Azimuth	277.444° WNW
Elevation	-35.005°
Doppler factor	1

Orbital elements

Apogee altitude	370.499 km
Perigee altitude	161.657 km
Semi-major axis	6,644.215 km
Eccentricity	0.0157161
Inclination	97.4909°
RAAN	69.1671°
Arg. of periapsis	204.7002°
True anomaly	213.20972°
Mean anomaly	214.2059°
Eccentric anomaly	213.7062°
Mean motion	4.00754 °/min
BSTAR	0.0012926
Orbital period	89.83 mins