CZ-2D DEB, 35273
Orbit data source: Space-Track
CZ-2D DEB, 35273 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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35273 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 CZ-2D DEB
1 35273U 05024M 25243.34895826 .00069744 00000-0 65850-3 0 9999
2 35273 97.1700 275.4070 0007063 92.3223 267.8846 15.66784309132992Epoch: 2025-08-31T08:22Z
TLE epoch observation values (Epoch: 2025-08-31T08:22:29.993Z)
Latitude
-0.00011°
Longitude
170.01186°
Altitude
371.452 km
Speed
7.687 km/s
True Right ascension
18h 21m 37s
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
12:48:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
369.768 km
Perigee altitude
360.243 km
Semi-major axis
6,743.143 km
Eccentricity
0.00071
Inclination
97.17°
RAAN
275.407°
Arg. of periapsis
92.3223°
True anomaly
267.80372°
Mean anomaly
267.8846°
Eccentric anomaly
267.84416°
Mean motion
3.91967 °/min
Orbital period
91.84 mins
BSTAR
0.0006585
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Other satellites on launch #24 in the year 2005 (2005-07-05 UTC)
CZ-2D DEB Visibility
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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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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Authenticating...
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