ELECTRON KICK STAGE R/B, 67074 (Decayed)
Orbit data source: Space-Track
ELECTRON KICK STAGE R/B, 67074 was space debris in LEO originally from a launch on Sun, 14 Dec 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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67074 intel report (Beta)
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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, 8.0 m
Radar Cross Section
0.760 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 5 months ago
TLE from 5 months ago
0 ELECTRON KICK STAGE R/B
1 67074U 25297C 26031.91160901 .15017579 26110-5 30246-3 0 9996
2 67074 97.4509 188.3072 0017883 68.7739 291.5472 16.45519813 7680Epoch: 2026-01-31T21:52Z
TLE epoch observation values (Epoch: 2026-01-31T21:52:43.018Z)
Latitude
0.00005°
Longitude
88.99915°
Altitude
150.146 km
Speed
7.819 km/s
True Right ascension
12h 33m 13s
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
07:16:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
159.633 km
Perigee altitude
136.292 km
Semi-major axis
6,526.1 km
Eccentricity
0.00179
Inclination
97.4509°
RAAN
188.3072°
Arg. of periapsis
68.7739°
True anomaly
291.35644°
Mean anomaly
291.5472°
Eccentric anomaly
291.45184°
Mean motion
4.11683 °/min
Orbital period
87.45 mins
BSTAR
0.00030246
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Other satellites on launch #297 in the year 2025 (2025-12-14 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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