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 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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62928 intel report (Beta)
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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
Unknown
Launch site
Object type
Shape & HBR
Trunc Cone, 0.9 m
Radar Cross Section
0.760 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 ELECTRON KICK STAGE R/B
1 62928U 25028A 26091.16481793 .00002984 00000-0 31897-3 0 9995
2 62928 97.8965 151.6055 0041335 103.0091 257.5746 14.88910976 61888Epoch: 2026-04-01T03:57Z
TLE epoch observation values (Epoch: 2026-04-01T03:57:20.269Z)
Latitude
0.00003°
Longitude
-97.26053°
Altitude
610.693 km
Speed
7.55 km/s
True Right ascension
10h 06m 25s
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
15:49:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
627.203 km
Perigee altitude
569.528 km
Semi-major axis
6,976.503 km
Eccentricity
0.00413
Inclination
97.8965°
RAAN
151.6055°
Arg. of periapsis
103.0091°
True anomaly
257.11255°
Mean anomaly
257.5746°
Eccentric anomaly
257.34352°
Mean motion
3.72466 °/min
Orbital period
96.65 mins
BSTAR
0.00031897
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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 | 2026-04-01 15:50:51.681Z | 65.362° ENE | 2026-04-01 15:52:51.681Z | 99.479° ESE | 15.715° | 2026-04-01 15:54:51.681Z | 130.259° SE |
| 6 mins | 2026-04-01 17:25:51.681Z | 345.447° N | 2026-04-01 17:28:51.681Z | 271.658° WNW | 29.495° | 2026-04-01 17:31:51.681Z | 223.517° SW |
| 6 mins | 2026-04-02 04:16:51.681Z | 186.827° SSW | 2026-04-02 04:19:51.681Z | 277.817° WNW | 38.896° | 2026-04-02 04:22:51.681Z | 335.476° NNW |
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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