CZ-2F R/B, 61686 (Decayed)
Orbit data source: Space-Track
CZ-2F R/B, 61686 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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61686 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CALT?
Mission
Decayed spacecraft
Bus & Motor
CZ-2F, Unknown motor
Mass
5,500 kg wet, 5,500 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 7.8 m
Radar Cross Section
44.450 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 months ago
TLE from 10 months ago
0 OBJECT D
1 61686U 24194D 24312.41093039 .05262063 78099-5 37845-3 0 9990
2 61686 41.4558 285.2074 0036233 194.5499 344.2276 16.36423738 1330Epoch: 2024-11-07T09:51Z
TLE epoch observation values (Epoch: 2024-11-07T09:51:44.385Z)
Latitude
0.83222°
Longitude
-90.75832°
Altitude
151.973 km
Speed
7.831 km/s
True Right ascension
06h 57m 04s
True Declination
0° 49' 36"
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
00:51:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
201.393 km
Perigee altitude
153.886 km
Semi-major axis
6,555.777 km
Eccentricity
0.00362
Inclination
41.4558°
RAAN
285.2074°
Arg. of periapsis
194.5499°
True anomaly
344.11425°
Mean anomaly
344.2276°
Eccentric anomaly
344.17097°
Mean motion
4.0889 °/min
Orbital period
88.04 mins
BSTAR
0.00037845
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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 R/B 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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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