ELECTRON R/B, 63028 (Decayed)
Orbit data source: Space-Track
ELECTRON R/B, 63028 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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63028 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Rocket Lab
Mission
Decayed spacecraft
Bus & Motor
ELECTRON ST2, Unknown motor
Mass
250 kg wet, ~250 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, Unknown HBR
Radar Cross Section
2.827 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 ELECTRON R/B
1 63028U 25033C 25057.01430395 .25107025 10876-4 30531-3 0 9999
2 63028 58.9964 75.2812 0052966 270.2695 186.1265 16.43070160 1127Epoch: 2025-02-26T00:20Z
TLE epoch observation values (Epoch: 2025-02-26T00:20:35.861Z)
Latitude
58.56478°
Longitude
16.1929°
Altitude
200.371 km
Speed
7.772 km/s
True Right ascension
11h 49m 48s
True Declination
58° 23' 55"
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
07:17:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
191.579 km
Perigee altitude
122.351 km
Semi-major axis
6,535.102 km
Eccentricity
0.0053
Inclination
58.9964°
RAAN
75.2812°
Arg. of periapsis
270.2695°
True anomaly
186.06215°
Mean anomaly
186.1265°
Eccentric anomaly
186.09428°
Mean motion
4.10832 °/min
Orbital period
87.63 mins
BSTAR
0.00030531
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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 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
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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