CZ-3C DEB, 48544
Orbit data source: Space-Track
CZ-3C DEB, 48544 is space debris in HEO originally from a launch on Sun, 31 Oct 2010 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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48544 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CALT
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-3C DEB
1 48544U 10057BP 26245.03056744 .00001063 00000-0 72178-3 0 9994
2 48544 20.4098 139.3194 4837577 253.8490 49.3792 5.73523973233266Epoch: 2026-09-02T00:44Z
TLE epoch observation values (Epoch: 2026-09-02T00:44:01.026Z)
Latitude
0.00008°
Longitude
147.14841°
Altitude
5,298.206 km
Speed
6.168 km/s
True Right ascension
09h 17m 21s
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
04:06:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
13,189.194 km
Perigee altitude
429.905 km
Semi-major axis
13,187.686 km
Eccentricity
0.48376
Inclination
20.4098°
RAAN
139.3194°
Arg. of periapsis
253.849°
True anomaly
106.20161°
Mean anomaly
49.3792°
Eccentric anomaly
76.30891°
Mean motion
1.43315 °/min
Orbital period
251.2 mins
BSTAR
0.00072178
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Other satellites on launch #57 in the year 2010 (2010-10-31 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-3C 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. |
|---|---|---|---|---|---|---|---|
| 64 mins | 2026-09-23 15:21:35.787Z | 178.163° S | 2026-09-23 15:35:35.787Z | 129.674° SE | 26.1° | 2026-09-23 16:25:35.787Z | 88.34° E |
| 161 mins | 2026-09-23 19:44:35.787Z | 244.55° WSW | 2026-09-23 20:32:35.787Z | 175.367° S | 59.978° | 2026-09-23 22:25:35.787Z | 117.801° SE |
| 144 mins | 2026-09-24 00:37:35.787Z | 270.513° WNW | 2026-09-24 02:09:35.787Z | 229.663° WSW | 34.112° | 2026-09-24 03:01:35.787Z | 171.77° S |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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