CZ-7 DEB, 61986 (Decayed)
Orbit data source: Space-Track
CZ-7 DEB, 61986 was space debris in LEO originally from a launch on Fri, 15 Nov 2024 UTC launched from the Wenchang Satellite Launch Center (WSC). 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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61986 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CALT
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 10 months ago
TLE from 10 months ago
0 CZ-7 DEB
1 61986U 24211D 24321.75364574 .06204315 68214-5 58898-2 0 9990
2 61986 41.6383 232.5019 0205265 189.0244 170.6889 15.80640746 164Epoch: 2024-11-16T18:05Z
TLE epoch observation values (Epoch: 2024-11-16T18:05:14.991Z)
Latitude
-0°
Longitude
-95.11318°
Altitude
464.144 km
Speed
7.559 km/s
True Right ascension
15h 30m 00s
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
06:02:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
468.564 km
Perigee altitude
193.14 km
Semi-major axis
6,708.989 km
Eccentricity
0.02053
Inclination
41.6383°
RAAN
232.5019°
Arg. of periapsis
189.0244°
True anomaly
171.06006°
Mean anomaly
170.6889°
Eccentric anomaly
170.87541°
Mean motion
3.94964 °/min
Orbital period
91.15 mins
BSTAR
0.0058898
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Other satellites on launch #211 in the year 2024 (2024-11-15 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-7 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
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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