CZ-3 DEB, 25936
Orbit data source: Space-Track
CZ-3 DEB, 25936 is space debris in HEO originally from a launch on Sat, 01 Feb 1986 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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25936 intel report (Beta)
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Edit Public Description
Expand to show TLE details & history
TLE from 22 hours ago
0 CZ-3 DEB
1 25936U 86010D 25215.52603471 .00008341 00000-0 13414-1 0 9993
2 25936 30.8302 15.4241 6551534 65.1291 347.7869 3.14784087 12620
Epoch: 2025-08-03T12:37Z
TLE epoch observation values (Epoch: 2025-08-03T12:37:29.398Z)
Latitude
-0.00008°
Longitude
-126.30449°
Altitude
2,421.53 km
Speed
8.386 km/s
True Right ascension
01h 01m 39s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
-28.07862°
Longitude
170.06184°
Altitude
13,747.78 km
Speed
4.399 km/s
Apparent Right ascension
19h 46m 51s
Apparent Declination
-41° 04' 60"
Sunlit
Visualization observer readout
Local Sidereal Time
00:28:47
Azimuth
226.867° WSW
Elevation
-13.211°
Doppler factor
1
Orbital elements
Apogee altitude
26,178.136 km
Perigee altitude
404.872 km
Semi-major axis
19,669.641 km
Eccentricity
0.65515
Inclination
30.8302°
RAAN
15.4241°
Arg. of periapsis
65.1291°
True anomaly
295.32515°
Mean anomaly
347.7869°
Eccentric anomaly
327.7642°
Mean motion
0.78677 °/min
Orbital period
457.57 mins
BSTAR
0.013414
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Other satellites on launch #10 in the year 1986 (1986-02-01 UTC)
CZ-3 DEB 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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32 mins | 2025-08-04 19:31:15.876Z | 242.365° WSW | 2025-08-04 19:36:15.876Z | 178.796° S | 31.745° | 2025-08-04 20:03:15.876Z | 123.817° 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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