CZ-3B DEB, 40815
Orbit data source: Space-Track
CZ-3B DEB, 40815 is space debris in HEO originally from a launch on Sat, 04 Sep 2010 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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40815 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Last TLE update
20 hours ago
Origin
Manufacturer
CALT
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & history
TLE from 20 hours ago
0 CZ-3B DEB
1 40815U 10042Y 25199.13566152 .00000083 00000-0 26694-2 0 9990
2 40815 25.5208 224.0476 7402588 64.8286 352.1223 1.91031581 394Epoch: 2025-07-18T03:15Z
TLE epoch observation values (Epoch: 2025-07-18T03:15:21.155Z)
Latitude
-0.00007°
Longitude
-120.96779°
Altitude
3,018.091 km
Speed
8.385 km/s
True Right ascension
14h 56m 14s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
-24.09369°
Longitude
128.28263°
Altitude
40,628.683 km
Speed
1.56 km/s
Apparent Right ascension
07h 07m 56s
Apparent Declination
-29° 19' 36"
Sunlit
Visualization observer readout
Local Sidereal Time
12:07:28
Azimuth
238.214° WSW
Elevation
-8.041°
Doppler factor
1
Orbital elements
Apogee altitude
41,375.468 km
Perigee altitude
749.296 km
Semi-major axis
27,440.519 km
Eccentricity
0.74026
Inclination
25.5208°
RAAN
224.0476°
Arg. of periapsis
64.8286°
True anomaly
295.51702°
Mean anomaly
352.1223°
Eccentric anomaly
332.61028°
Mean motion
0.47748 °/min
Orbital period
753.96 mins
BSTAR
0.0026694
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Other satellites on launch #42 in the year 2010 (2010-09-04 UTC)
CZ-3B DEB Visibility
Observer location: undefined°, undefined°
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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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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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Authenticating...
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