ELECTRON KICK STAGE R/B, 59590
Orbit data source: Space-Track
ELECTRON KICK STAGE R/B, 59590 is space debris in SSO originally from a launch on Tue, 23 Apr 2024 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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59590 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated 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
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 ELECTRON KICK STAGE R/B
1 59590U 24077D 25258.21954793 .00008193 00000-0 79660-3 0 9992
2 59590 97.3373 283.5915 0357181 40.9959 321.7511 14.55144520 73861Epoch: 2025-09-15T05:16Z
TLE epoch observation values (Epoch: 2025-09-15T05:16:08.941Z)
Latitude
0.00002°
Longitude
-149.8731°
Altitude
516.68 km
Speed
7.709 km/s
True Right ascension
18h 54m 21s
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
12:57:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
958.97 km
Perigee altitude
452.91 km
Semi-major axis
7,084.077 km
Eccentricity
0.03572
Inclination
97.3373°
RAAN
283.5915°
Arg. of periapsis
40.9959°
True anomaly
319.1262°
Mean anomaly
321.7511°
Eccentric anomaly
320.44793°
Mean motion
3.64014 °/min
Orbital period
98.9 mins
BSTAR
0.0007966
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Other satellites on launch #77 in the year 2024 (2024-04-23 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 | 2025-09-16 01:12:45.024Z | 125.567° SE | 2025-09-16 01:14:45.024Z | 84.469° E | 23.368° | 2025-09-16 01:17:45.024Z | 15.677° NNE |
| 8 mins | 2025-09-16 14:49:45.024Z | 3.249° NNE | 2025-09-16 14:52:45.024Z | 301.158° NW | 43.028° | 2025-09-16 14:57:45.024Z | 202.211° SSW |
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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