CZ-2D R/B, 61445 (Decayed)
Orbit data source: Space-Track
CZ-2D R/B, 61445 was space debris in LEO originally from a launch on Fri, 27 Sep 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.
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61445 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
BWYIC
Mission
Decayed spacecraft
Bus & Motor
CZ-2 STAGE 2, Unknown motor
Mass
4,006 kg wet, 4,006 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl + 1 Sail, 4.5 m
Radar Cross Section
27.824 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 months ago
TLE from 10 months ago
0 CZ-2D R/B
1 61445U 24177B 24315.22634495 .07484936 79825-5 67146-3 0 9995
2 61445 41.3775 239.1072 0007529 234.7996 251.2891 16.37905997 6994Epoch: 2024-11-10T05:25Z
TLE epoch observation values (Epoch: 2024-11-10T05:25:56.203Z)
Latitude
32.45712°
Longitude
-118.12239°
Altitude
173.711 km
Speed
7.806 km/s
True Right ascension
00h 52m 55s
True Declination
32° 17' 16"
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
09:35:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
178.633 km
Perigee altitude
168.768 km
Semi-major axis
6,551.838 km
Eccentricity
0.00075
Inclination
41.3775°
RAAN
239.1072°
Arg. of periapsis
234.7996°
True anomaly
251.20741°
Mean anomaly
251.2891°
Eccentric anomaly
251.24825°
Mean motion
4.09259 °/min
Orbital period
87.96 mins
BSTAR
0.00067146
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Other satellites on launch #177 in the year 2024 (2024-09-27 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-2D 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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