CZ-2F DEB, 61684 (Decayed)
Orbit data source: Space-Track
CZ-2F DEB, 61684 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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61684 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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 months ago
TLE from 10 months ago
0 CZ-2F DEB
1 61684U 24194B 24327.96353995 .00465987 65563-5 48903-3 0 9998
2 61684 41.3237 193.5705 0257846 294.4302 62.9836 15.68300172 3788Epoch: 2024-11-22T23:07Z
TLE epoch observation values (Epoch: 2024-11-22T23:07:29.851Z)
Latitude
-0.00008°
Longitude
144.27265°
Altitude
288.015 km
Speed
7.78 km/s
True Right ascension
12h 54m 16s
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
00:27:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
539.927 km
Perigee altitude
192.136 km
Semi-major axis
6,744.168 km
Eccentricity
0.02578
Inclination
41.3237°
RAAN
193.5705°
Arg. of periapsis
294.4302°
True anomaly
65.65399°
Mean anomaly
62.9836°
Eccentric anomaly
64.31497°
Mean motion
3.91878 °/min
Orbital period
91.87 mins
BSTAR
0.00048903
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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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