CZ-3B DEB, 40159
Orbit data source: Space-Track
CZ-3B DEB, 40159 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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40159 intel report (Beta)
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Edit Public Description
Expand to show TLE details & history
TLE from 8 months ago
0 CZ-3B DEB
1 40159U 10042L 24325.99769251 .00000611 00000-0 10706-2 0 9994
2 40159 26.4157 225.0517 7121019 284.9312 11.7108 2.42561861105603
Epoch: 2024-11-20T23:56Z
TLE epoch observation values (Epoch: 2024-11-20T23:56:40.632Z)
Latitude
0.00057°
Longitude
165.44648°
Altitude
3,398.304 km
Speed
8.031 km/s
True Right ascension
15h 00m 24s
True Declination
0° 00' 02"
Sunlit
Visualization orbit readout
Latitude
-26.54714°
Longitude
-19.90306°
Altitude
32,841.984 km
Speed
1.81 km/s
Apparent Right ascension
02h 22m 28s
Apparent Declination
-28° 50' 26"
Sunlit
Visualization observer readout
Local Sidereal Time
12:18:06
Azimuth
283.829° WNW
Elevation
-62.234°
Doppler factor
1
Orbital elements
Apogee altitude
33,688.943 km
Perigee altitude
359.334 km
Semi-major axis
23,402.275 km
Eccentricity
0.7121
Inclination
26.4157°
RAAN
225.0517°
Arg. of periapsis
284.9312°
True anomaly
75.56779°
Mean anomaly
11.7108°
Eccentric anomaly
35.27049°
Mean motion
0.60626 °/min
Orbital period
593.81 mins
BSTAR
0.0010706
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Other satellites on launch #42 in the year 2010 (2010-09-04 UTC)
CZ-3B DEB Visibility forecast
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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10 mins | 2025-07-19 03:47:28.994Z | 215.067° SW | 2025-07-19 03:50:28.994Z | 171.715° S | 18.582° | 2025-07-19 03:57:28.994Z | 130.284° SE |
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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