ELECTRON R/B, 64056

Orbit data source: Space-Track

ELECTRON R/B, 64056 is space debris in LEO originally from a launch on Sat, 17 May 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

Iframe embed code

<iframe src="https://www.satcat.com/sats-embedded/64056?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/64056?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

64056, 2025-104B

Orbit

LEO

Last TLE update

9 hours ago

Origin

Rocket Lab USA Inc (US)

Manufacturer

Rocket Lab

Mission

Spacecraft

Bus & Motor

ELECTRON ST2, Unknown motor

Mass

250 kg wet, ~250 kg dry

Launch date (UTC)

2025-05-17 (1 month ago)

Launch vehicle

Unknown

Launch site

Rocket Lab Launch Complex (RLLC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Large (>1 m²)

Expand to show TLE details & history

TLE from 9 hours ago

0 ELECTRON R/B
1 64056U 25104B   25169.91173214  .01435991  77886-5  16117-2 0  9995
2 64056  41.9341  95.6881 0127169 121.3968 321.6595 15.94074969  5109

Epoch: 2025-06-18T21:52Z

TLE epoch observation values (Epoch: 2025-06-18T21:52:53.656Z)

Latitude

41.61474°

Longitude

-60.44545°

Altitude

227.45 km

Speed

7.815 km/s

True Right ascension

11h 40m 39s

True Declination

41° 25' 49"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

30.22207°

Longitude

-2.51003°

Altitude

206.204 km

Speed

7.835 km/s

Apparent Right ascension

11h 36m 29s

Apparent Declination

-12° 58' 34"

Sunlit

Object is in full shadow

Visualization observer readout

Local Sidereal Time

17:56:39

Azimuth

263.111° W

Elevation

-12.109°

Doppler factor

Orbital elements

Apogee altitude

377.915 km

Perigee altitude

208.241 km

Semi-major axis

6,671.215 km

Eccentricity

0.01272

Inclination

41.9341°

RAAN

95.6881°

Arg. of periapsis

121.3968°

True anomaly

Unknown

Mean anomaly

321.6595°

Eccentric anomaly

Unknown

Mean motion

3.98323 °/min

Orbital period

90.38 mins

BSTAR

0.0016117

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Other satellites on launch #104 in the year 2025 (2025-05-17 UTC)

QPS-SAR-10, 64055

ELECTRON KICK STAGE R/B, 64057

ELECTRON R/B Visibility

Observer location: undefined°, undefined°

ELECTRON R/B is likely not visible in the next few days

Authenticating...

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Check out ELECTRON R/B, 64056 on other resources

View ELECTRON R/B, 64056 on Heavens-Above

View ELECTRON R/B, 64056 on Keep Track

View ELECTRON R/B, 64056 on Celestrak

View ELECTRON R/B, 64056 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.