DECAYED

CZ-3B R/B, 60328 (Decayed)

Orbit data source: Space-Track

CZ-3B R/B, 60328 was space debris originally from a launch on Thu, 01 Aug 2024 UTC launched from the Xichang Space Center, China (XSC). 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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Identifier
60328, 2024-135B
Orbit
Decayed
Country
Flag of CNCN / PRC
Related business
Manufacturer
CALT
Mission
Decayed spacecraft
Bus & Motor
CZ-3A STAGE 3, Unknown motor
Mass
~2,800 kg wet, ~2,800 kg dry
Launch date (UTC)
2024-08-01 (1 year ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 5 months ago

TLE from 5 months ago
0 CZ-3B R/B
1 60328U 24135B   25093.99565336  .00000580 -37028-5  00000+0 0  9997
2 60328  26.8591  19.9287 4420718  29.5119  23.1088  6.91815698  6912
Epoch: 2025-04-03T23:53Z
TLE epoch observation values (Epoch: 2025-04-03T23:53:44.45Z)
Latitude
26.97496°
Longitude
-82.26251°
Altitude
1,263.105 km
Speed
8.374 km/s
True Right ascension
07h 14m 55s
True Declination
26° 50' 43"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
16:50:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
10,404.669 km
Perigee altitude
115.022 km
Semi-major axis
11,637.982 km
Eccentricity
0.44207
Inclination
26.8591°
RAAN
19.9287°
Arg. of periapsis
29.5119°
True anomaly
59.4085°
Mean anomaly
23.1088°
Eccentric anomaly
39.07426°
Mean motion
1.72873 °/min
Orbital period
208.25 mins
BSTAR
0
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Other satellites on launch #135 in the year 2024 (2024-08-01 UTC)

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