DECAYED

ELECTRON R/B, 59882 (Decayed)

Orbit data source: Space-Track

ELECTRON R/B, 59882 was space debris in LEO originally from a launch on Sat, 25 May 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/59882?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/59882?theme=dark&initialShowStats=false

Optional Secondary NORAD IDs

Max 10 NORAD IDs; Separated by commas

Initial load time (optional)

ISO8601 Format

TLE date request (optional)

ISO8601 Format

Identifier

59882, 2024-099B

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)

2024-05-25 (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 59882U 24099B   24162.35253499  .26591496  21862-5  37978-3 0  9994
2 59882  97.4512  21.7750 0027981 183.1273 235.1261 16.46282928  2545

Epoch: 2024-06-10T08:27Z

TLE epoch observation values (Epoch: 2024-06-10T08:27:39.023Z)

Latitude

57.33377°

Longitude

-16.02835°

Altitude

169.334 km

Speed

7.804 km/s

True Right ascension

00h 40m 17s

True Declination

57° 09' 48"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

No trajectory is available.

Visualization observer readout

No trajectory is available.

Orbital elements

Apogee altitude

164.199 km

Perigee altitude

127.689 km

Semi-major axis

6,524.081 km

Eccentricity

0.0028

Inclination

97.4512°

RAAN

21.775°

Arg. of periapsis

183.1273°

True anomaly

Unknown

Mean anomaly

235.1261°

Eccentric anomaly

Unknown

Mean motion

4.11874 °/min

Orbital period

87.41 mins

BSTAR

0.00037978

Loading maneuver chart data...

Loading SW <> Apogee altitude chart data...

Loading historical data...

Other satellites on launch #99 in the year 2024 (2024-05-25 UTC)

PREFIRE-2, 59881

ELECTRON KICK STAGE R/B, 59883

ELECTRON R/B Visibility

Observer location: undefined°, undefined°

This satellite is decayed

Authenticating...

Click to sort rows by Secondary header in ascending order	Click to sort rows by Secondary name header in ascending order	Click to sort rows by Country header in ascending order	Click to sort rows by Owner header in ascending order	Click to sort rows by Obj. Type header in ascending order	Click to sort rows by Miss dist. header in ascending order	Click to sort rows by Rel. speed header in ascending order	Click to sort rows by Apr. angle header in ascending order	Click to sort rows by TCA header in ascending order

Check out ELECTRON R/B, 59882 (Decayed) on other resources

View ELECTRON R/B, 59882 (Decayed) on Celestrak

View ELECTRON R/B, 59882 (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.