ELECTRON R/B, 67615
Orbit data source: Space-Track
ELECTRON R/B, 67615 is space debris in SSO originally from a launch on Fri, 30 Jan 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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67615 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Rocket Lab
Mission
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
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 ELECTRON R/B
1 67615U 26019B 26040.01816560 .03850825 21454-5 15569-2 0 9992
2 67615 97.4250 165.8463 0133302 191.5521 168.2695 16.05693345 1575Epoch: 2026-02-09T00:26Z
TLE epoch observation values (Epoch: 2026-02-09T00:26:09.507Z)
Latitude
-0.00005°
Longitude
20.18768°
Altitude
348.58 km
Speed
7.649 km/s
True Right ascension
11h 03m 23s
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
11:18:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
343.965 km
Perigee altitude
167.108 km
Semi-major axis
6,633.674 km
Eccentricity
0.01333
Inclination
97.425°
RAAN
165.8463°
Arg. of periapsis
191.5521°
True anomaly
168.57507°
Mean anomaly
168.2695°
Eccentric anomaly
168.42278°
Mean motion
4.01709 °/min
Orbital period
89.62 mins
BSTAR
0.0015569
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Other satellites on launch #19 in the year 2026 (2026-01-30 UTC)
Did you know?
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. |
|---|---|---|---|---|---|---|---|
| ELECTRON R/B is likely not visible in the next few days. |
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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