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
Trunc Cone, 0.7 m
Radar Cross Section
0.760 m², Medium (>0.1 m² and < 1m²)
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 25301.59793118 .00005714 00000-0 56142-3 0 9990
2 59590 97.3315 321.8089 0352317 263.0850 93.0160 14.55788869 80170Epoch: 2025-10-28T14:21Z
TLE epoch observation values (Epoch: 2025-10-28T14:21:01.253Z)
Latitude
-0.00003°
Longitude
69.37055°
Altitude
731.688 km
Speed
7.478 km/s
True Right ascension
21h 27m 14s
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
00:29:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
953.358 km
Perigee altitude
454.337 km
Semi-major axis
7,081.985 km
Eccentricity
0.03523
Inclination
97.3315°
RAAN
321.8089°
Arg. of periapsis
263.085°
True anomaly
97.03504°
Mean anomaly
93.016°
Eccentric anomaly
95.02686°
Mean motion
3.64175 °/min
Orbital period
98.85 mins
BSTAR
0.00056142
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-10-29 14:01:59.762Z | 18.11° NNE | 2025-10-29 14:06:59.762Z | 81.034° E | 41.895° | 2025-10-29 14:11:59.762Z | 180.855° SSW |
| 5 mins | 2025-10-29 15:41:59.762Z | 328.227° NNW | 2025-10-29 15:43:59.762Z | 304.638° NW | 16.927° | 2025-10-29 15:46:59.762Z | 266.411° W |
| 10 mins | 2025-10-30 01:06:59.762Z | 147.712° SSE | 2025-10-30 01:10:59.762Z | 85.993° E | 40.315° | 2025-10-30 01:16:59.762Z | 356.265° N |
| 6 mins | 2025-10-30 02:46:59.762Z | 238.289° WSW | 2025-10-30 02:49:59.762Z | 277.124° WNW | 18.81° | 2025-10-30 02:52:59.762Z | 310.757° NW |
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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