CZ-3C DEB, 42467
Orbit data source: Space-Track
CZ-3C DEB, 42467 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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42467 intel report (Beta)
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Edit Public Description
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, 0.2 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 CZ-3C DEB
1 42467U 10057BG 25298.54975956 .00017562 00000-0 10622-1 0 9995
2 42467 20.1321 52.5319 4510648 149.2416 247.5057 6.29491520226260Epoch: 2025-10-25T13:11Z
TLE epoch observation values (Epoch: 2025-10-25T13:11:39.225Z)
Latitude
0.00005°
Longitude
-179.56988°
Altitude
9,737.454 km
Speed
4.16 km/s
True Right ascension
03h 30m 05s
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
02:45:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
11,606.698 km
Perigee altitude
425.494 km
Semi-major axis
12,394.233 km
Eccentricity
0.45106
Inclination
20.1321°
RAAN
52.5319°
Arg. of periapsis
149.2416°
True anomaly
210.78715°
Mean anomaly
247.5057°
Eccentric anomaly
228.2304°
Mean motion
1.57295 °/min
Orbital period
228.87 mins
BSTAR
0.010622
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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. |
|---|---|---|---|---|---|---|---|
| 92 mins | 2025-10-26 07:26:14.655Z | 206.016° SW | 2025-10-26 08:30:14.655Z | 164.954° S | 28.608° | 2025-10-26 08:58:14.655Z | 112.575° SE |
| 40 mins | 2025-10-26 12:22:14.655Z | 243.712° WSW | 2025-10-26 12:53:14.655Z | 191.617° SSW | 29.273° | 2025-10-26 13:02:14.655Z | 131.032° SE |
| 95 mins | 2025-10-27 05:51:14.655Z | 199.015° SSW | 2025-10-27 07:06:14.655Z | 155.768° SSE | 25.518° | 2025-10-27 07:26:14.655Z | 134.449° SE |
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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