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.
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61504 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated 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)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl + 1 Nozzle, 6.2 m
Radar Cross Section
32.704 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 months ago
TLE from 7 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 4899Epoch: 2025-02-28T14:05Z
TLE epoch observation values (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
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
06:33:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,569.882 km
Perigee altitude
85.965 km
Semi-major axis
7,206.06 km
Eccentricity
0.10296
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
Orbital period
101.46 mins
BSTAR
0.0012668
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Other satellites on launch #181 in the year 2024 (2024-10-10 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.CZ-3B R/B Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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