CZ-2D DEB, 31409
Orbit data source: Space-Track
CZ-2D DEB, 31409 is space debris in SSO originally from a launch on Tue, 05 Jul 2005 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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31409 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 CZ-2D DEB
1 31409U 05024J 25241.83507889 .00042970 00000-0 56381-3 0 9998
2 31409 97.1861 274.1487 0007156 122.6878 237.5069 15.58399772 88281
Epoch: 2025-08-29T20:02Z
TLE epoch observation values (Epoch: 2025-08-29T20:02:30.816Z)
Latitude
-0.00005°
Longitude
-4.75772°
Altitude
398.042 km
Speed
7.67 km/s
True Right ascension
18h 16m 35s
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
12:48:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
394.036 km
Perigee altitude
384.351 km
Semi-major axis
6,767.33 km
Eccentricity
0.00072
Inclination
97.1861°
RAAN
274.1487°
Arg. of periapsis
122.6878°
True anomaly
237.43777°
Mean anomaly
237.5069°
Eccentric anomaly
237.47233°
Mean motion
3.89868 °/min
Orbital period
92.34 mins
BSTAR
0.00056381
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Other satellites on launch #24 in the year 2005 (2005-07-05 UTC)
CZ-2D 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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5 mins | 2025-09-01 02:06:07.992Z | 155.324° SSE | 2025-09-01 02:09:07.992Z | 60.944° ENE | 39.862° | 2025-09-01 02:11:07.992Z | 0.228° 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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