CZ-3C DEB, 40177
Orbit data source: Space-Track
CZ-3C DEB, 40177 is space debris in HEO originally from a launch on Sun, 31 Oct 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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40177 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 CZ-3C DEB
1 40177U 10057AF 24222.22662896 .00001864 00000-0 20836-1 0 9994
2 40177 17.6309 314.2845 7214565 223.2477 49.5393 2.21111368 91436
Epoch: 2024-08-09T05:26Z
TLE epoch observation values (Epoch: 2024-08-09T05:26:20.742Z)
Latitude
0.00026°
Longitude
-85.45207°
Altitude
18,835.457 km
Speed
3.95 km/s
True Right ascension
20h 57m 21s
True Declination
0° 00' 01"
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
16:50:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,473.852 km
Perigee altitude
555.609 km
Semi-major axis
24,892.868 km
Eccentricity
0.72146
Inclination
17.6309°
RAAN
314.2845°
Arg. of periapsis
223.2477°
True anomaly
136.77467°
Mean anomaly
49.5393°
Eccentric anomaly
90.87094°
Mean motion
0.55263 °/min
Orbital period
651.44 mins
BSTAR
0.020836
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Other satellites on launch #57 in the year 2010 (2010-10-31 UTC)
CZ-3C 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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308 mins | 2025-08-31 12:34:02.171Z | 129.779° SE | 2025-08-31 16:27:02.171Z | 143.895° SSE | 22.511° | 2025-08-31 17:42:02.171Z | 118.629° 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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Authenticating...
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