ELECTRON KICK STAGE R/B, 67616
Orbit data source: Space-Track
ELECTRON KICK STAGE R/B, 67616 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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67616 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / SKORRelated 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
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 ELECTRON KICK STAGE R/B
1 67616U 26019C 26032.79015153 .00270668 20967-4 15701-2 0 9991
2 67616 97.4061 157.8487 0205480 252.3044 105.5685 15.54465384 425Epoch: 2026-02-01T18:57Z
TLE epoch observation values (Epoch: 2026-02-01T18:57:49.092Z)
Latitude
-0°
Longitude
101.39941°
Altitude
446.889 km
Speed
7.621 km/s
True Right ascension
10h 31m 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
07:32:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
539.915 km
Perigee altitude
261.335 km
Semi-major axis
6,778.762 km
Eccentricity
0.02055
Inclination
97.4061°
RAAN
157.8487°
Arg. of periapsis
252.3044°
True anomaly
107.82062°
Mean anomaly
105.5685°
Eccentric anomaly
106.69618°
Mean motion
3.88882 °/min
Orbital period
92.57 mins
BSTAR
0.0015701
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Other satellites on launch #19 in the year 2026 (2026-01-30 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-02-02 07:27:51.592Z | 119.344° SE | 2026-02-02 07:30:51.592Z | 64.633° ENE | 20.605° | 2026-02-02 07:32:51.592Z | 26.731° NE |
| 4 mins | 2026-02-02 09:00:51.592Z | 230.816° WSW | 2026-02-02 09:01:51.592Z | 253.237° W | 22.049° | 2026-02-02 09:04:51.592Z | 314.692° NW |
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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