ELECTRON R/B, 68099 (Decayed)
Orbit data source: Space-Track
ELECTRON R/B, 68099 was space debris in LEO originally from a launch on Thu, 05 Mar 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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68099 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Rocket Lab
Mission
Decayed spacecraft
Bus & Motor
KICK STAGE, CURIE
Mass
40 kg wet, ~40 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 8.0 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 2 months ago
TLE from 2 months ago
0 ELECTRON R/B
1 68099U 26043B 26072.01391444 .12248352 90084-5 58475-3 0 9995
2 68099 42.0046 51.9802 0052977 313.8573 45.7931 16.35030976 1128Epoch: 2026-03-13T00:20Z
TLE epoch observation values (Epoch: 2026-03-13T00:20:02.207Z)
Latitude
0.00001°
Longitude
-123.68452°
Altitude
154.581 km
Speed
7.83 km/s
True Right ascension
03h 27m 55s
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
06:48:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
216.014 km
Perigee altitude
146.514 km
Semi-major axis
6,559.401 km
Eccentricity
0.0053
Inclination
42.0046°
RAAN
51.9802°
Arg. of periapsis
313.8573°
True anomaly
46.23028°
Mean anomaly
45.7931°
Eccentric anomaly
46.01149°
Mean motion
4.08552 °/min
Orbital period
88.12 mins
BSTAR
0.00058475
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Other satellites on launch #43 in the year 2026 (2026-03-05 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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