CZ-2F DEB, 61685 (Decayed)
Orbit data source: Space-Track
CZ-2F DEB, 61685 was space debris in LEO originally from a launch on Tue, 29 Oct 2024 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). 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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61685 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
1 kg wet, 1 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cone, 0.1 m
Radar Cross Section
0.025 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 11 months ago
TLE from 11 months ago
0 OBJECT C
1 61685U 24194C 24304.53447202 .10360189 69059-5 81270-2 0 9998
2 61685 41.5666 336.9773 0196838 141.4270 221.5742 15.84571849 104Epoch: 2024-10-30T12:49Z
TLE epoch observation values (Epoch: 2024-10-30T12:49:38.382Z)
Latitude
0.96583°
Longitude
106.32003°
Altitude
416.715 km
Speed
7.606 km/s
True Right ascension
22h 32m 14s
True Declination
0° 57' 35"
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
10:57:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
451.611 km
Perigee altitude
187.93 km
Semi-major axis
6,697.908 km
Eccentricity
0.01968
Inclination
41.5666°
RAAN
336.9773°
Arg. of periapsis
141.427°
True anomaly
220.10464°
Mean anomaly
221.5742°
Eccentric anomaly
220.83673°
Mean motion
3.95945 °/min
Orbital period
90.92 mins
BSTAR
0.008127
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Other satellites on launch #194 in the year 2024 (2024-10-29 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-2F 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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