CZ-4 DEB, 27687
Orbit data source: Space-Track
CZ-4 DEB, 27687 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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27687 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: 1 day ago
TLE from 1 day ago
0 CZ-4 DEB
1 27687U 99057MT 25304.35846966 .00000259 00000-0 96491-4 0 9990
2 27687 98.7837 337.8863 0089317 96.4731 264.6634 14.38053373220541Epoch: 2025-10-31T08:36Z
TLE epoch observation values (Epoch: 2025-10-31T08:36:11.778Z)
Latitude
-0.00005°
Longitude
168.93319°
Altitude
774.374 km
Speed
7.463 km/s
True Right ascension
22h 31m 32s
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
14:34:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
825.849 km
Perigee altitude
698.301 km
Semi-major axis
7,140.212 km
Eccentricity
0.00893
Inclination
98.7837°
RAAN
337.8863°
Arg. of periapsis
96.4731°
True anomaly
263.64545°
Mean anomaly
264.6634°
Eccentric anomaly
264.15431°
Mean motion
3.5973 °/min
Orbital period
100.08 mins
BSTAR
0.000096491
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-11-02 02:28:17.653Z | 173.367° S | 2025-11-02 02:32:17.653Z | 282.81° WNW | 43.554° | 2025-11-02 02:36:17.653Z | 341.65° N |
| 7 mins | 2025-11-02 14:38:17.653Z | 44.674° NE | 2025-11-02 14:41:17.653Z | 103.691° ESE | 29.26° | 2025-11-02 14:45:17.653Z | 162.169° S |
| 6 mins | 2025-11-02 16:17:17.653Z | 335.764° NNW | 2025-11-02 16:20:17.653Z | 285.124° WNW | 22.463° | 2025-11-02 16:23:17.653Z | 243.47° WSW |
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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