ELECTRON KICK STAGE R/B, 63026 (Decayed)
Orbit data source: Space-Track
ELECTRON KICK STAGE R/B, 63026 was space debris in LEO originally from a launch on Tue, 18 Feb 2025 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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63026 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, 1.0 m
Radar Cross Section
0.760 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 4 months ago
TLE from 4 months ago
0 ELECTRON KICK STAGE R/B
1 63026U 25033A 26054.55654025 .12448917 10728-4 13458-2 0 9990
2 63026 58.9629 23.9658 0003520 239.3970 235.6002 16.36810450 57334Epoch: 2026-02-23T13:21Z
TLE epoch observation values (Epoch: 2026-02-23T13:21:25.077Z)
Latitude
51.11066°
Longitude
162.28222°
Altitude
182.259 km
Speed
7.802 km/s
True Right ascension
10h 24m 20s
True Declination
50° 55' 40"
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
07:18:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
175.931 km
Perigee altitude
171.318 km
Semi-major axis
6,551.761 km
Eccentricity
0.00035
Inclination
58.9629°
RAAN
23.9658°
Arg. of periapsis
239.397°
True anomaly
235.56693°
Mean anomaly
235.6002°
Eccentric anomaly
235.58356°
Mean motion
4.09266 °/min
Orbital period
87.96 mins
BSTAR
0.0013458
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Other satellites on launch #33 in the year 2025 (2025-02-18 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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