CZ-2D R/B, 62728 (Decayed)
Orbit data source: Space-Track
CZ-2D R/B, 62728 was space debris in LEO originally from a launch on Fri, 17 Jan 2025 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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62728 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
BWYIC
Mission
Decayed spacecraft
Bus & Motor
CZ-2 STAGE 2, Unknown motor
Mass
4,006 kg wet, 4,006 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 3.0 m
Radar Cross Section
27.824 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 months ago
TLE from 2 months ago
0 CZ-2D R/B
1 62728U 25012D 26174.22670545 .15643967 25556-5 49150-3 0 9997
2 62728 97.3833 262.4850 0016970 266.2463 93.6898 16.43206175 80162Epoch: 2026-06-23T05:26Z
TLE epoch observation values (Epoch: 2026-06-23T05:26:27.350Z)
Latitude
-0.00003°
Longitude
-90.53026°
Altitude
161.276 km
Speed
7.809 km/s
True Right ascension
17h 29m 56s
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
02:43:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
165.175 km
Perigee altitude
143.005 km
Semi-major axis
6,532.227 km
Eccentricity
0.0017
Inclination
97.3833°
RAAN
262.485°
Arg. of periapsis
266.2463°
True anomaly
93.88383°
Mean anomaly
93.6898°
Eccentric anomaly
93.78682°
Mean motion
4.11104 °/min
Orbital period
87.57 mins
BSTAR
0.0004915
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Other satellites on launch #12 in the year 2025 (2025-01-17 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-2D 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
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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