CZ-3 DEB, 17425
Orbit data source: Space-Track
CZ-3 DEB, 17425 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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17425 intel report (Beta)
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Edit Public Description
Expand to show TLE details & history
TLE from 1 day ago
0 CZ-3 DEB
1 17425U 86010C 25215.20697597 .00003797 00000-0 80002-2 0 9992
2 17425 30.7989 238.3373 6311025 90.5507 336.9499 3.44853742292769
Epoch: 2025-08-03T04:58Z
TLE epoch observation values (Epoch: 2025-08-03T04:58:02.723Z)
Latitude
-0.00008°
Longitude
-148.17119°
Altitude
4,803.153 km
Speed
7.054 km/s
True Right ascension
15h 53m 29s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
-22.80373°
Longitude
75.89858°
Altitude
14,446.639 km
Speed
4.092 km/s
Apparent Right ascension
07h 45m 09s
Apparent Declination
-30° 48' 08"
Sunlit
Visualization observer readout
Local Sidereal Time
00:23:59
Azimuth
104.051° ESE
Elevation
-33.852°
Doppler factor
1
Orbital elements
Apogee altitude
23,812.064 km
Perigee altitude
449.815 km
Semi-major axis
18,509.077 km
Eccentricity
0.6311
Inclination
30.7989°
RAAN
238.3373°
Arg. of periapsis
90.5507°
True anomaly
269.50878°
Mean anomaly
336.9499°
Eccentric anomaly
308.74944°
Mean motion
0.86192 °/min
Orbital period
417.67 mins
BSTAR
0.0080002
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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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7 mins | 2025-08-05 05:57:28.542Z | 227.44° WSW | 2025-08-05 06:01:28.542Z | 190.915° SSW | 19.694° | 2025-08-05 06:04:28.542Z | 131.486° 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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