ELECTRON KICK STAGE R/B, 45111 (Decayed)
Orbit data source: Space-Track
ELECTRON KICK STAGE R/B, 45111 was space debris in LEO originally from a launch on Fri, 31 Jan 2020 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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45111 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Rocket Lab
Mission
Decayed spacecraft
Bus & Motor
KICK STAGE, CURIE
Mass
40 kg wet, 40 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: 2 months ago
TLE from 2 months ago
0 ELECTRON KICK STAGE R/B
1 45111U 20007B 26080.51063610 .18034427 44838-5 32898-3 0 9993
2 45111 69.9345 145.7422 0008771 277.9257 82.0982 16.47056642103854Epoch: 2026-03-21T12:15Z
TLE epoch observation values (Epoch: 2026-03-21T12:15:18.959Z)
Latitude
0.00005°
Longitude
142.88292°
Altitude
148.893 km
Speed
7.818 km/s
True Right ascension
09h 42m 58s
True Declination
0° 00' 00"
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
23:26:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
150.641 km
Perigee altitude
139.198 km
Semi-major axis
6,523.057 km
Eccentricity
0.00088
Inclination
69.9345°
RAAN
145.7422°
Arg. of periapsis
277.9257°
True anomaly
82.19777°
Mean anomaly
82.0982°
Eccentric anomaly
82.14798°
Mean motion
4.11971 °/min
Orbital period
87.38 mins
BSTAR
0.00032898
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Other satellites on launch #7 in the year 2020 (2020-01-31 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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