CZ-2C DEB, 40290
Orbit data source: Space-Track
CZ-2C DEB, 40290 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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40290 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: 12 hours ago
TLE from 12 hours ago
0 CZ-2C DEB
1 40290U 14066E 25306.45547491 .00016313 00000-0 16569-2 0 9990
2 40290 97.9180 276.3752 0048567 221.8383 137.9118 14.90016256586104Epoch: 2025-11-02T10:55Z
TLE epoch observation values (Epoch: 2025-11-02T10:55:53.032Z)
Latitude
-0.00003°
Longitude
70.43328°
Altitude
626.142 km
Speed
7.532 km/s
True Right ascension
18h 25m 30s
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
18:57:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
628.779 km
Perigee altitude
561.047 km
Semi-major axis
6,973.05 km
Eccentricity
0.00486
Inclination
97.918°
RAAN
276.3752°
Arg. of periapsis
221.8383°
True anomaly
138.28316°
Mean anomaly
137.9118°
Eccentric anomaly
138.09765°
Mean motion
3.72743 °/min
Orbital period
96.58 mins
BSTAR
0.0016569
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-03 10:05:29.338Z | 54.142° ENE | 2025-11-03 10:07:29.338Z | 86.642° E | 18.317° | 2025-11-03 10:10:29.338Z | 137.165° SSE |
| 5 mins | 2025-11-03 11:41:29.338Z | 336.767° NNW | 2025-11-03 11:43:29.338Z | 291.752° WNW | 27.583° | 2025-11-03 11:46:29.338Z | 232.638° WSW |
| 6 mins | 2025-11-03 22:31:29.338Z | 194.317° SSW | 2025-11-03 22:34:29.338Z | 283.618° WNW | 36.201° | 2025-11-03 22:37:29.338Z | 332.995° NNW |
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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