ELECTRON KICK STAGE R/B, 44496 (Decayed)
Orbit data source: Space-Track
ELECTRON KICK STAGE R/B, 44496 was space debris in LEO originally from a launch on Mon, 19 Aug 2019 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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44496 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Rocket Lab
Mission
Decayed spacecraft
Bus & Motor
KICK STAGE, CURIE
Mass
50 kg wet, 50 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Trunc Cone, 0.7 m
Radar Cross Section
0.760 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 months ago
TLE from 9 months ago
0 ELECTRON KICK STAGE R/B
1 44496U 19054B 25043.51783917 .17988936 10669-4 87007-3 0 9993
2 44496 44.9741 125.2899 0004346 336.0185 153.8598 16.42987145304392Epoch: 2025-02-12T12:25Z
TLE epoch observation values (Epoch: 2025-02-12T12:25:41.304Z)
Latitude
32.96162°
Longitude
-64.12776°
Altitude
161.671 km
Speed
7.813 km/s
True Right ascension
17h 40m 24s
True Declination
32° 47' 26"
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
05:11:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
162.403 km
Perigee altitude
156.721 km
Semi-major axis
6,537.699 km
Eccentricity
0.00043
Inclination
44.9741°
RAAN
125.2899°
Arg. of periapsis
336.0185°
True anomaly
153.88173°
Mean anomaly
153.8598°
Eccentric anomaly
153.87077°
Mean motion
4.10588 °/min
Orbital period
87.68 mins
BSTAR
0.00087007
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Other satellites on launch #54 in the year 2019 (2019-08-19 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ELECTRON KICK STAGE R/B Visibility
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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. |
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| This satellite is decayed. |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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