DECAYED

CZ-2F DEB, 59594 (Decayed)

Orbit data source: Space-Track

CZ-2F DEB, 59594 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
59594, 2024-078D
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
Unknown
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 59594U 24078D   24119.06132642  .38721847  72850-5  24546-2 0  9994
2 59594  41.5973  28.4800 0063503 152.0982 294.6586 16.31592083   377
Epoch: 2024-04-28T01:28Z
TLE epoch observation values (Epoch: 2024-04-28T01:28:18.602Z)
Latitude
41.64314°
Longitude
-125.34043°
Altitude
173.674 km
Speed
7.818 km/s
True Right ascension
07h 33m 01s
True Declination
41° 27' 26"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Visualization observer readout
Orbital elements
Apogee altitude
232.255 km
Perigee altitude
148.829 km
Semi-major axis
6,568.679 km
Eccentricity
0.00635
Inclination
41.5973°
RAAN
28.48°
Arg. of periapsis
152.0982°
True anomaly
Unknown
Mean anomaly
294.6586°
Eccentric anomaly
Unknown
Mean motion
4.07686 °/min
Orbital period
88.3 mins
BSTAR
0.0024546
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CZ-2F DEB Visibility

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