DECAYED

CZ-2F DEB, 59595 (Decayed)

Orbit data source: Space-Track

CZ-2F DEB, 59595 was space debris in LEO originally from a launch on Thu, 25 Apr 2024 UTC via a Proton-K launch vehicle 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
59595, 2024-078E
Orbit
Decayed
Last TLE update
1 year ago
Origin
Manufacturer
CALT?
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
2024-04-25 (1 year ago)
Launch vehicle
Proton-K
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
RCS unknown

Expand to show TLE details & history

TLE from 1 year ago
0 CZ-2F DEB
1 59595U 24078E   24117.85336774  .13837883  68135-5  88539-2 0  9996
2 59595  41.2954  36.8973 0161439 124.3929 237.3200 15.94157667   211
Epoch: 2024-04-26T20:28Z
TLE epoch observation values (Epoch: 2024-04-26T20:28:50.972Z)
Latitude
0.05851°
Longitude
-125.57769°
Altitude
349.566 km
Speed
7.667 km/s
True Right ascension
02h 27m 51s
True Declination
0° 03' 29"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Visualization observer readout
Orbital elements
Apogee altitude
400.655 km
Perigee altitude
185.26 km
Semi-major axis
6,671.095 km
Eccentricity
0.01614
Inclination
41.2954°
RAAN
36.8973°
Arg. of periapsis
124.3929°
True anomaly
Unknown
Mean anomaly
237.32°
Eccentric anomaly
Unknown
Mean motion
3.98334 °/min
Orbital period
90.38 mins
BSTAR
0.0088539
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CZ-2F DEB Visibility

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