CZ-4 DEB, 27806
Orbit data source: Space-Track
CZ-4 DEB, 27806 is space debris in SSO originally from a launch on Thu, 14 Oct 1999 UTC launched from the Taiyaun Space Center, China (TSC). 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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27806 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 CZ-4 DEB
1 27806U 99057MW 25293.78887882 .00000328 00000-0 13072-3 0 9999
2 27806 98.9171 314.4930 0109861 72.5339 288.7817 14.31973240248153Epoch: 2025-10-20T18:55Z
TLE epoch observation values (Epoch: 2025-10-20T18:55:59.130Z)
Latitude
0.00002°
Longitude
1.01047°
Altitude
763.504 km
Speed
7.485 km/s
True Right ascension
20h 57m 58s
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
23:51:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
860.96 km
Perigee altitude
703.63 km
Semi-major axis
7,160.432 km
Eccentricity
0.01099
Inclination
98.9171°
RAAN
314.493°
Arg. of periapsis
72.5339°
True anomaly
287.58462°
Mean anomaly
288.7817°
Eccentric anomaly
288.18368°
Mean motion
3.58207 °/min
Orbital period
100.5 mins
BSTAR
0.00013072
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Other satellites on launch #57 in the year 1999 (1999-10-14 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-4 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-10-21 13:57:08.327Z | 28.463° NE | 2025-10-21 14:01:08.327Z | 90.098° ESE | 35.676° | 2025-10-21 14:06:08.327Z | 173.265° S |
| 5 mins | 2025-10-21 15:38:08.327Z | 329.431° NNW | 2025-10-21 15:40:08.327Z | 300.478° NW | 18.894° | 2025-10-21 15:43:08.327Z | 257.681° W |
| 7 mins | 2025-10-22 01:15:08.327Z | 152.37° SSE | 2025-10-22 01:18:08.327Z | 95.635° ESE | 42.562° | 2025-10-22 01:22:08.327Z | 353.34° 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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