ELECTRON KICK STAGE R/B, 62928
Orbit data source: Space-Track
ELECTRON KICK STAGE R/B, 62928 is space debris in SSO originally from a launch on Sat, 08 Feb 2025 UTC via an ELECTRON launch vehicle 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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62928 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Rocket Lab
Mission
Spacecraft
Bus & Motor
KICK STAGE, CURIE
Mass
~50 kg wet, ~50 kg dry
Launch date (UTC)
Launch vehicle
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: 18 hours ago
TLE from 18 hours ago
0 ELECTRON KICK STAGE R/B
1 62928U 25028A 25259.09665272 .00002768 00000-0 30749-3 0 9993
2 62928 97.9305 314.8629 0041704 32.5148 327.8624 14.87403864 32578Epoch: 2025-09-16T02:19Z
TLE epoch observation values (Epoch: 2025-09-16T02:19:10.795Z)
Latitude
0.00002°
Longitude
-75.22394°
Altitude
584.447 km
Speed
7.581 km/s
True Right ascension
20h 59m 27s
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
12:37:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
632.197 km
Perigee altitude
573.969 km
Semi-major axis
6,981.22 km
Eccentricity
0.00417
Inclination
97.9305°
RAAN
314.8629°
Arg. of periapsis
32.5148°
True anomaly
327.60706°
Mean anomaly
327.8624°
Eccentric anomaly
327.73484°
Mean motion
3.72088 °/min
Orbital period
96.75 mins
BSTAR
0.00030749
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Other satellites on launch #28 in the year 2025 (2025-02-08 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 forecast
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-09-17 02:42:19.258Z | 94.368° ESE | 2025-09-17 02:44:19.258Z | 62.102° ENE | 14.76° | 2025-09-17 02:46:19.258Z | 31.698° NE |
| 6 mins | 2025-09-17 04:17:19.258Z | 201.795° SSW | 2025-09-17 04:19:19.258Z | 249.576° W | 32.896° | 2025-09-17 04:23:19.258Z | 331.717° NNW |
| 6 mins | 2025-09-17 16:02:19.258Z | 44.316° NE | 2025-09-17 16:05:19.258Z | 106.956° ESE | 26.625° | 2025-09-17 16:08:19.258Z | 156.176° SSE |
| 4 mins | 2025-09-17 17:39:19.258Z | 317.374° NNW | 2025-09-17 17:40:19.258Z | 297.938° NW | 20.582° | 2025-09-17 17:43:19.258Z | 246.956° WSW |
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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