DECAYED

ELECTRON R/B, 61794 (Decayed)

Orbit data source: Space-Track

ELECTRON R/B, 61794 was space debris in LEO originally from a launch on Tue, 05 Nov 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
ELECTRON R/B details
Identifier
61794, 2024-201C
Orbit
Decayed
Last TLE update3 weeks ago
Origin
Flag of USRocket Lab (US)
ManufacturerRocket Lab
MissionDecayed spacecraft
Bus & MotorELECTRON ST2, Unknown motor
Mass250 kg wet, ~250 kg dry
Launch date (UTC)
2024-11-05 (1 month ago)
Launch vehicleUnknown
Launch site
Rocket Lab Launch Complex (RLLC)
Object type
Payload
Rocket body
Debris
Shape & HBRUnknown
Radar Cross SectionLarge (>1 m²)

Expand to show TLE details & history

TLE from 3 weeks ago
0 ELECTRON R/B
1 61794U 24201C   24328.91290801  .28009577  23251-5  54894-3 0  9994
2 61794  97.8628 235.6162 0037199 160.1510 263.3626 16.42832349  2896
Epoch: 2024-11-23T21:54Z
Definitive object data (Epoch: 2024-11-23T21:54:35.252Z)
Latitude62.15056°
Longitude-171.45272°
Altitude171.88 km
Speed7.807 km/s
True Right ascension14h 42m 12s
True Declination61° 59' 44"
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 altitude179.407 km
Perigee altitude130.801 km
Semi-major axis6,533.241 km
Eccentricity0.0037199
Inclination97.8628°
RAAN235.6162°
Arg. of periapsis160.151°
True anomaly262.93942°
Mean anomaly263.3626°
Eccentric anomaly263.15099°
Mean motion4.11008 °/min
BSTAR0.00054894
Orbital period87.59 mins
Loading maneuver chart data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #201 in the year 2024 (2024-11-05 UTC)

ELECTRON R/B Visibility forecast

Observer location: undefined°, undefined

This satellite is decayed
Span
Click to sort rows by Start time (UTC) header in descending order
Start Az.
Max El. time (UTC)
Max El. Az.
Max El.
End time (UTC)
End Az.
|