CZ-3B DEB, 42473
Orbit data source: Space-Track
CZ-3B DEB, 42473 is space debris in HEO originally from a launch on Mon, 19 Dec 2011 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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42473 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
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 CZ-3B DEB
1 42473U 11077AN 25257.96171354 -.00000157 00000-0 00000-0 0 9997
2 42473 23.0045 113.2321 7175017 16.8150 358.2696 1.69234915 58437Epoch: 2025-09-14T23:04Z
TLE epoch observation values (Epoch: 2025-09-14T23:04:52.049Z)
Latitude
0.0001°
Longitude
132.89133°
Altitude
2,174.983 km
Speed
8.933 km/s
True Right ascension
07h 33m 07s
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
23:07:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
44,714.143 km
Perigee altitude
2,025.629 km
Semi-major axis
29,748.023 km
Eccentricity
0.7175
Inclination
23.0045°
RAAN
113.2321°
Arg. of periapsis
16.815°
True anomaly
345.04008°
Mean anomaly
358.2696°
Eccentric anomaly
353.90385°
Mean motion
0.42302 °/min
Orbital period
851.03 mins
BSTAR
0
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Other satellites on launch #77 in the year 2011 (2011-12-19 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-3B 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. |
|---|---|---|---|---|---|---|---|
| 21 mins | 2025-09-16 06:25:46.692Z | 258.199° W | 2025-09-16 06:25:46.692Z | 258.199° W | 11.835° | 2025-09-16 06:46:46.692Z | 258.411° W |
| 40 mins | 2025-09-16 17:46:46.692Z | 205.824° SW | 2025-09-16 17:54:46.692Z | 150.174° SSE | 28.812° | 2025-09-16 18:26:46.692Z | 89.795° E |
| 459 mins | 2025-09-16 22:46:46.692Z | 108.293° ESE | 2025-09-17 03:21:46.692Z | 152.775° SSE | 23.77° | 2025-09-17 06:25:46.692Z | 164.145° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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