SQX-1 R/B, 64963
Orbit data source: Space-Track
SQX-1 R/B, 64963 is space debris in SSO 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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Edit Public Description
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 SQX-1 R/B
1 64963U 25160B 25241.22950743 .00077230 38596-5 43032-3 0 9998
2 64963 97.4365 317.4758 0160121 238.4467 120.1072 15.63404277 4853
Epoch: 2025-08-29T05:30Z
TLE epoch observation values (Epoch: 2025-08-29T05:30:29.441Z)
Latitude
-0.00012°
Longitude
-102.82801°
Altitude
436.537 km
Speed
7.618 km/s
True Right ascension
21h 09m 54s
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
12:26:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
482.868 km
Perigee altitude
266.613 km
Semi-major axis
6,752.877 km
Eccentricity
0.01601
Inclination
97.4365°
RAAN
317.4758°
Arg. of periapsis
238.4467°
True anomaly
121.67853°
Mean anomaly
120.1072°
Eccentric anomaly
120.89446°
Mean motion
3.9112 °/min
Orbital period
92.04 mins
BSTAR
0.00043032
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Other satellites on launch #160 in the year 2025 (2025-07-29 UTC)
SQX-1 R/B Visibility forecast
Observer location: undefined°, undefined°
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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6 mins | 2025-08-30 04:41:03.807Z | 134.505° SE | 2025-08-30 04:44:03.807Z | 67.157° ENE | 28.397° | 2025-08-30 04:47:03.807Z | 8.382° NNE |
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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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