CZ-2C DEB, 40288
Orbit data source: Space-Track
CZ-2C DEB, 40288 is space debris in SSO originally from a launch on Mon, 27 Oct 2014 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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40288 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CALT
Mission
Spacecraft
Bus & Motor
Unknown
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cone, 0.1 m
Radar Cross Section
0.025 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 CZ-2C DEB
1 40288U 14066C 25348.31536208 .00002365 00000-0 79071-3 0 9992
2 40288 97.9495 118.7804 0159810 37.8424 323.3870 14.31264628577785Epoch: 2025-12-14T07:34Z
TLE epoch observation values (Epoch: 2025-12-14T07:34:07.283Z)
Latitude
0.00004°
Longitude
-77.97999°
Altitude
699.187 km
Speed
7.554 km/s
True Right ascension
07h 55m 07s
True Declination
0° 00' 00"
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
21:13:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
899.082 km
Perigee altitude
670.146 km
Semi-major axis
7,162.751 km
Eccentricity
0.01598
Inclination
97.9495°
RAAN
118.7804°
Arg. of periapsis
37.8424°
True anomaly
322.27709°
Mean anomaly
323.387°
Eccentric anomaly
322.83383°
Mean motion
3.58033 °/min
Orbital period
100.55 mins
BSTAR
0.00079071
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Other satellites on launch #66 in the year 2014 (2014-10-27 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-2C DEB Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-14 23:14:45.729Z | 321.768° NNW | 2025-12-14 23:16:45.729Z | 296.912° NW | 14.451° | 2025-12-14 23:18:45.729Z | 272.512° WNW |
| 7 mins | 2025-12-15 08:51:45.729Z | 165.673° S | 2025-12-15 08:54:45.729Z | 161.186° S | 44.426° | 2025-12-15 08:58:45.729Z | 347.703° N |
| 8 mins | 2025-12-15 21:03:45.729Z | 36.837° NE | 2025-12-15 21:07:45.729Z | 105.32° ESE | 31° | 2025-12-15 21:11:45.729Z | 160.866° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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