ELECTRON R/B, 100562 (Decayed)
Orbit data source: Space-Track
ELECTRON R/B, 100562 was space debris in LEO originally from a launch on Wed, 02 Sep 2026 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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100562 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, 8.0 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 weeks ago
TLE from 2 weeks ago
0 ELECTRON R/B
1 A0562U 26201B 26283.10918319 .12248089 47787-5 54545-3 0 9995
2 A0562 38.0195 184.2564 0038796 258.3867 101.2583 16.38126418 5930Epoch: 2026-10-10T02:37Z
TLE epoch observation values (Epoch: 2026-10-10T02:37:13.427Z)
Latitude
0.00001°
Longitude
126.22943°
Altitude
175.035 km
Speed
7.801 km/s
True Right ascension
12h 17m 01s
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
04:42:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
199.113 km
Perigee altitude
148.276 km
Semi-major axis
6,551.831 km
Eccentricity
0.00388
Inclination
38.0195°
RAAN
184.2564°
Arg. of periapsis
258.3867°
True anomaly
101.6939°
Mean anomaly
101.2583°
Eccentric anomaly
101.47614°
Mean motion
4.0926 °/min
Orbital period
87.96 mins
BSTAR
0.00054545
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Other satellites on launch #201 in the year 2026 (2026-09-02 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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