DECAYED

CZ-3B R/B, 61504 (Decayed)

Orbit data source: Space-Track

CZ-3B R/B, 61504 was space debris in LEO originally from a launch on Thu, 10 Oct 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.

Not visible in the next 10 days
Identifier
61504, 2024-181B
Orbit
Decayed
Last TLE update
2 months ago
Origin
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)
2024-10-10 (7 months ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Nozzle, 12.38 m
Radar Cross Section
32.704 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 2 months ago
0 CZ-3B R/B
1 61504U 24181B   25059.58702788  .99999999  27309-5  12668-2 0  9991
2 61504  28.1094  84.9567 1029631  45.9705  84.2595 14.20467468  4899
Epoch: 2025-02-28T14:05Z
Definitive object data (Epoch: 2025-02-28T14:05:19.208Z)
Latitude
16.91607°
Longitude
-139.51526°
Altitude
823.494 km
Speed
7.444 km/s
True Right ascension
15h 21m 50s
True Declination
16° 49' 17"
Sunlit
Object was in daylight at TLE epoch
Visualization observer readout
Visualization observer readout
Orbital elements
Apogee altitude
1,569.882 km
Perigee altitude
85.965 km
Semi-major axis
7,206.06 km
Eccentricity
0.1029631
Inclination
28.1094°
RAAN
84.9567°
Arg. of periapsis
45.9705°
True anomaly
96.06779°
Mean anomaly
84.2595°
Eccentric anomaly
90.15883°
Mean motion
3.5481 °/min
BSTAR
0.0012668
Orbital period
101.46 mins
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Other satellites on launch #181 in the year 2024 (2024-10-10 UTC)

CZ-3B R/B Visibility forecast

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This satellite is decayed
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