SQX-1 R/B, 64963 (Decayed)
Orbit data source: Space-Track
SQX-1 R/B, 64963 was space debris in LEO originally from a launch on Tue, 29 Jul 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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64963 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Sanjiang
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
~200 kg wet, ~200 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 8.0 m
Radar Cross Section
2.853 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 months ago
TLE from 6 months ago
0 SQX-1 R/B
1 64963U 25160B 25359.95492091 .15153986 25956-5 13436-3 0 9995
2 64963 97.3985 86.0586 0016541 74.1290 286.1837 16.50959454 23642Epoch: 2025-12-25T22:55Z
TLE epoch observation values (Epoch: 2025-12-25T22:55:05.166Z)
Latitude
-0.00003°
Longitude
7.58454°
Altitude
137.088 km
Speed
7.826 km/s
True Right ascension
05h 44m 14s
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
07:23:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
144.375 km
Perigee altitude
122.832 km
Semi-major axis
6,511.741 km
Eccentricity
0.00165
Inclination
97.3985°
RAAN
86.0586°
Arg. of periapsis
74.129°
True anomaly
286.00156°
Mean anomaly
286.1837°
Eccentric anomaly
286.09264°
Mean motion
4.13045 °/min
Orbital period
87.16 mins
BSTAR
0.00013436
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Other satellites on launch #160 in the year 2025 (2025-07-29 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.SQX-1 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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