DECAYED

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.

Not visible in the next 10 days
Identifier
61445, 2024-177B
Orbit
Decayed
Last TLE update
5 months ago
Origin
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)
2024-09-27 (7 months ago)
Launch vehicle
Unknown
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Sail, 8.9 m
Radar Cross Section
27.824 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 5 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  6994
Epoch: 2024-11-10T05:25Z
Definitive object data (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
Object was in full shadow at TLE epoch
Visualization observer readout
Visualization observer readout
Orbital elements
Apogee altitude
178.633 km
Perigee altitude
168.768 km
Semi-major axis
6,551.838 km
Eccentricity
0.0007529
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
BSTAR
0.00067146
Orbital period
87.96 mins
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Other satellites on launch #177 in the year 2024 (2024-09-27 UTC)

CZ-2D R/B Visibility forecast

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