CZ-3A DEB, 35556
Orbit data source: Space-Track
CZ-3A DEB, 35556 is space debris in HEO originally from a launch on Fri, 02 Feb 2007 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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35556 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 shape, 0.3 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 3 weeks ago
TLE from 3 weeks ago
0 CZ-3A DEB
1 35556U 07003Q 25271.72731594 .00010866 00000-0 48005-1 0 9998
2 35556 26.0901 353.3541 7237556 252.6015 22.3328 2.23354825 9546Epoch: 2025-09-28T17:27Z
TLE epoch observation values (Epoch: 2025-09-28T17:27:20.097Z)
Latitude
0.00024°
Longitude
83.79525°
Altitude
8,693.94 km
Speed
6.064 km/s
True Right ascension
23h 33m 28s
True Declination
0° 00' 01"
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
13:38:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,242.034 km
Perigee altitude
452.056 km
Semi-major axis
24,725.182 km
Eccentricity
0.72376
Inclination
26.0901°
RAAN
353.3541°
Arg. of periapsis
252.6015°
True anomaly
107.40513°
Mean anomaly
22.3328°
Eccentric anomaly
57.18278°
Mean motion
0.55826 °/min
Orbital period
644.86 mins
BSTAR
0.048005
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Other satellites on launch #3 in the year 2007 (2007-02-02 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.CZ-3A DEB Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 292 mins | 2025-10-22 03:28:09.219Z | 71.856° E | 2025-10-22 06:45:09.219Z | 83.065° E | 20.975° | 2025-10-22 08:20:09.219Z | 86.987° E |
| 308 mins | 2025-10-22 10:55:09.219Z | 269.257° W | 2025-10-22 12:33:09.219Z | 274.839° WNW | 21.484° | 2025-10-22 16:03:09.219Z | 288.492° WNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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