DECAYED

CZ-2F R/B, 59592 (Decayed)

Orbit data source: Space-Track

CZ-2F R/B, 59592 was space debris in LEO originally from a launch on Thu, 25 Apr 2024 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). 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.

Not visible in the next 10 days
Identifier
59592, 2024-078B
Orbit
Decayed
Last TLE update
1 year ago
Origin
Manufacturer
CALT?
Mission
Decayed spacecraft
Bus & Motor
CZ-2F, Unknown motor
Mass
5,500 kg wet, 5,500 kg dry
Launch date (UTC)
2024-04-25 (1 year ago)
Launch vehicle
Unknown
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history

TLE from 1 year ago
0 CZ-2F R/B
1 59592U 24078B   24127.30767977  .08931474  79814-5  16603-3 0  9992
2 59592  41.4578 333.6383 0024816 223.5914 301.6033 16.44858434  1742
Epoch: 2024-05-06T07:23Z
TLE epoch observation values (Epoch: 2024-05-06T07:23:03.532Z)
Latitude
9.90358°
Longitude
166.89423°
Altitude
143.283 km
Speed
7.828 km/s
True Right ascension
09h 29m 13s
True Declination
9° 50' 24"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Visualization observer readout
Orbital elements
Apogee altitude
171.438 km
Perigee altitude
139.011 km
Semi-major axis
6,533.361 km
Eccentricity
0.00248
Inclination
41.4578°
RAAN
333.6383°
Arg. of periapsis
223.5914°
True anomaly
Unknown
Mean anomaly
301.6033°
Eccentric anomaly
Unknown
Mean motion
4.10997 °/min
Orbital period
87.59 mins
BSTAR
0.00016603
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CZ-2F R/B Visibility

Observer location: undefined°, undefined°

This satellite is decayed
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