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.
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61794 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Rocket Lab
Mission
Decayed spacecraft
Bus & Motor
ELECTRON ST2, Unknown motor
Mass
250 kg wet, ~250 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, Unknown HBR
Radar Cross Section
2.827 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 months ago
TLE from 9 months 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 2896Epoch: 2024-11-23T21:54Z
TLE epoch observation values (Epoch: 2024-11-23T21:54:35.252Z)
Latitude
62.15056°
Longitude
-171.45272°
Altitude
171.88 km
Speed
7.807 km/s
True Right ascension
14h 42m 12s
True Declination
61° 59' 44"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
05:57:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
179.407 km
Perigee altitude
130.801 km
Semi-major axis
6,533.241 km
Eccentricity
0.00372
Inclination
97.8628°
RAAN
235.6162°
Arg. of periapsis
160.151°
True anomaly
262.93942°
Mean anomaly
263.3626°
Eccentric anomaly
263.15099°
Mean motion
4.11008 °/min
Orbital period
87.59 mins
BSTAR
0.00054894
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Other satellites on launch #201 in the year 2024 (2024-11-05 UTC)
ELECTRON R/B Visibility
Observer location: undefined°, undefined°
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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Authenticating...
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