COSMOS 886 DEB, 9827 (Decayed)
Orbit data source: Space-Track
COSMOS 886 DEB, 9827 was space debris in LEO originally from a launch on Mon, 27 Dec 1976 UTC launched from the Tyuratam Missile And Space Complex (TTMTR). 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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9827 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
Unknown
Mission
Decayed 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 year ago
TLE from 1 year ago
0 COSMOS 886 DEB
1 9827U 76126AP 25103.90548526 .17786387 67332-5 45795-2 0 9993
2 9827 65.7263 320.1118 0018158 231.6194 128.3364 16.27848391401799Epoch: 2025-04-13T21:43Z
TLE epoch observation values (Epoch: 2025-04-13T21:43:53.926Z)
Latitude
-0.00002°
Longitude
151.80901°
Altitude
207.963 km
Speed
7.778 km/s
True Right ascension
21h 20m 26s
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
19:46:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
208.621 km
Perigee altitude
184.743 km
Semi-major axis
6,574.819 km
Eccentricity
0.00182
Inclination
65.7263°
RAAN
320.1118°
Arg. of periapsis
231.6194°
True anomaly
128.49938°
Mean anomaly
128.3364°
Eccentric anomaly
128.41791°
Mean motion
4.07115 °/min
Orbital period
88.43 mins
BSTAR
0.0045795
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Other satellites on launch #126 in the year 1976 (1976-12-27 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.COSMOS 886 DEB Visibility
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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. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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