DECAYED

ELECTRON R/B, 59589 (Decayed)

Orbit data source: Space-Track

ELECTRON R/B, 59589 was space debris in LEO originally from a launch on Tue, 23 Apr 2024 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/59589?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/59589?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

59589, 2024-077C

Orbit

Decayed

Last TLE update

1 year ago

Origin

Rocket Lab USA Inc (US)

Manufacturer

Rocket Lab

Mission

Decayed spacecraft

Bus & Motor

ELECTRON ST2, Unknown motor

Mass

250 kg wet, ~250 kg dry

Launch date (UTC)

2024-04-23 (1 year 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 1 year ago

0 ELECTRON R/B
1 59589U 24077C   24120.11832866  .25703934  18435-5  42399-3 0  9999
2 59589  97.3717 201.4229 0049442 202.9026 244.9909 16.41921092   828

Epoch: 2024-04-29T02:50Z

Definitive object data (Epoch: 2024-04-29T02:50:23.596Z)

Latitude

82.22266°

Longitude

-129.09537°

Altitude

188.031 km

Speed

7.792 km/s

True Right ascension

08h 44m 15s

True Declination

82° 10' 21"

Sunlit

Object was in daylight at TLE epoch

Visualization observer readout

No trajectory is available.

Visualization observer readout

No trajectory is available.

Orbital elements

Apogee altitude

189.814 km

Perigee altitude

125.187 km

Semi-major axis

6,535.638 km

Eccentricity

0.0049442

Inclination

97.3717°

RAAN

201.4229°

Arg. of periapsis

202.9026°

True anomaly

244.4788°

Mean anomaly

244.9909°

Eccentric anomaly

244.73472°

Mean motion

4.10782 °/min

BSTAR

0.00042399

Orbital period

87.64 mins

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Other satellites on launch #77 in the year 2024 (2024-04-23 UTC)

NEONSAT-1, 59587

ACS 3, 59588

ELECTRON KICK STAGE R/B, 59590

ELECTRON R/B Visibility forecast

Observer location: undefined°, undefined°

This satellite is decayed

Authenticating...

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Check out ELECTRON R/B, 59589 (Decayed) on other resources

View ELECTRON R/B, 59589 (Decayed) on Celestrak

View ELECTRON R/B, 59589 (Decayed) on Gunter's Space Page

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