CZ-3B R/B, 64471
Orbit data source: Space-Track
CZ-3B R/B, 64471 is space debris in HEO originally from a launch on Fri, 20 Jun 2025 UTC launched from the Xichang Space Center, China (XSC). 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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64471 intel report (Beta)
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Edit Public Description
Expand to show TLE details & history
TLE from 2 days ago
0 CZ-3B R/B
1 64471U 25132B 25198.46528958 .00020018 00000-0 21875-2 0 9993
2 64471 27.7615 85.1583 7324403 195.9977 114.0999 2.24815000 625
Epoch: 2025-07-17T11:10Z
TLE epoch observation values (Epoch: 2025-07-17T11:10:01.019Z)
Latitude
0.00016°
Longitude
-17.84067°
Altitude
32,184.556 km
Speed
2.116 km/s
True Right ascension
05h 40m 46s
True Declination
0° 00' 01"
Sunlit
Visualization orbit readout
Latitude
12.36834°
Longitude
5.99421°
Altitude
34,502.83 km
Speed
1.818 km/s
Apparent Right ascension
07h 32m 35s
Apparent Declination
6° 05' 40"
Sunlit
Visualization observer readout
Local Sidereal Time
21:55:53
Azimuth
44.189° NE
Elevation
-33.382°
Doppler factor
1
Orbital elements
Apogee altitude
36,271.075 km
Perigee altitude
208.647 km
Semi-major axis
24,617.998 km
Eccentricity
0.73244
Inclination
27.7615°
RAAN
85.1583°
Arg. of periapsis
195.9977°
True anomaly
164.01888°
Mean anomaly
114.0999°
Eccentric anomaly
140.68736°
Mean motion
0.56191 °/min
Orbital period
640.68 mins
BSTAR
0.0021875
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Other satellites on launch #132 in the year 2025 (2025-06-20 UTC)
CZ-3B 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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574 mins | 2025-07-19 13:59:41.895Z | 178.39° S | 2025-07-19 23:14:41.895Z | 192.876° SSW | 42.709° | 2025-07-19 23:33:41.895Z | 116.194° SE |
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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