CZ-7 DEB, 61987 (Decayed)
Orbit data source: Space-Track
CZ-7 DEB, 61987 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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61987 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 61987U 24211E 24321.11989614 .04777669 69678-5 55935-2 0 9998
2 61987 41.8022 236.3926 0222688 178.1516 182.0204 15.74500383 67Epoch: 2024-11-16T02:52Z
TLE epoch observation values (Epoch: 2024-11-16T02:52:39.026Z)
Latitude
0.00002°
Longitude
137.55205°
Altitude
495.314 km
Speed
7.534 km/s
True Right ascension
15h 45m 34s
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
06:01:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
498.033 km
Perigee altitude
198.456 km
Semi-major axis
6,726.381 km
Eccentricity
0.02227
Inclination
41.8022°
RAAN
236.3926°
Arg. of periapsis
178.1516°
True anomaly
181.93287°
Mean anomaly
182.0204°
Eccentric anomaly
181.9764°
Mean motion
3.93433 °/min
Orbital period
91.5 mins
BSTAR
0.0055935
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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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