CZ-7 DEB, 61985 (Decayed)
Orbit data source: Space-Track
CZ-7 DEB, 61985 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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61985 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
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 10 months ago
TLE from 10 months ago
0 CZ-7 DEB
1 61985U 24211C 24322.12276153 .11069787 67666-5 62994-2 0 9996
2 61985 41.3258 230.1136 0138930 163.0962 197.4583 15.99971003 226Epoch: 2024-11-17T02:56Z
TLE epoch observation values (Epoch: 2024-11-17T02:56:46.596Z)
Latitude
-0.00004°
Longitude
129.25297°
Altitude
362.342 km
Speed
7.643 km/s
True Right ascension
15h 20m 27s
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
05:59:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
369.251 km
Perigee altitude
184.338 km
Semi-major axis
6,654.932 km
Eccentricity
0.01389
Inclination
41.3258°
RAAN
230.1136°
Arg. of periapsis
163.0962°
True anomaly
196.98847°
Mean anomaly
197.4583°
Eccentric anomaly
197.22261°
Mean motion
3.99786 °/min
Orbital period
90.05 mins
BSTAR
0.0062994
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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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