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: 5 hours ago
TLE from 5 hours ago
0 CZ-2C DEB
1 40288U 14066C 25304.26721166 .00005564 00000-0 18495-2 0 9993
2 40288 97.9478 78.4398 0162107 169.4133 191.0533 14.30847958571487Epoch: 2025-10-31T06:24Z
TLE epoch observation values (Epoch: 2025-10-31T06:24:47.087Z)
Latitude
-0.00003°
Longitude
-57.57049°
Altitude
905.97 km
Speed
7.34 km/s
True Right ascension
05h 13m 45s
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
06:48:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
902.141 km
Perigee altitude
669.87 km
Semi-major axis
7,164.143 km
Eccentricity
0.01621
Inclination
97.9478°
RAAN
78.4398°
Arg. of periapsis
169.4133°
True anomaly
190.70411°
Mean anomaly
191.0533°
Eccentric anomaly
190.87802°
Mean motion
3.57929 °/min
Orbital period
100.58 mins
BSTAR
0.0018495
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-10-31 22:06:08.310Z | 7.864° NNE | 2025-10-31 22:10:08.310Z | 282.41° WNW | 43.835° | 2025-10-31 22:14:08.310Z | 201.235° SSW |
| 5 mins | 2025-11-01 07:46:08.310Z | 91.706° ESE | 2025-11-01 07:48:08.310Z | 65.988° ENE | 17.752° | 2025-11-01 07:51:08.310Z | 28.425° NE |
| 9 mins | 2025-11-01 09:23:08.310Z | 182.748° SSW | 2025-11-01 09:27:08.310Z | 249.74° W | 41.102° | 2025-11-01 09:32:08.310Z | 338.696° N |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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