CZ-3B R/B, 62486
Orbit data source: Space-Track
CZ-3B R/B, 62486 is space debris in HEO originally from a launch on Mon, 06 Jan 2025 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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62486 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CALT
Mission
Spacecraft
Bus & Motor
CZ-3A STAGE 3, Unknown motor
Mass
~2,800 kg wet, ~2,800 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl + 1 Nozzle, 3.3 m
Radar Cross Section
32.704 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 5 days ago
TLE from 5 days ago
0 CZ-3B R/B
1 62486U 25002B 26127.21586110 .00592864 -18624-6 60714-3 0 9990
2 62486 28.4387 116.4050 5726424 287.4393 19.9846 4.61600671 9279Epoch: 2026-05-07T05:10Z
TLE epoch observation values (Epoch: 2026-05-07T05:10:50.399Z)
Latitude
-0.00023°
Longitude
173.61836°
Altitude
2,359.247 km
Speed
8.067 km/s
True Right ascension
07h 45m 34s
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
22:42:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
17,589.201 km
Perigee altitude
134.866 km
Semi-major axis
15,240.17 km
Eccentricity
0.57264
Inclination
28.4387°
RAAN
116.405°
Arg. of periapsis
287.4393°
True anomaly
72.5814°
Mean anomaly
19.9846°
Eccentric anomaly
41.89334°
Mean motion
1.15361 °/min
Orbital period
312.06 mins
BSTAR
0.00060714
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Other satellites on launch #2 in the year 2025 (2025-01-06 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 R/B 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. |
|---|---|---|---|---|---|---|---|
| 182 mins | 2026-05-13 00:32:58.556Z | 200.58° SSW | 2026-05-13 00:54:58.556Z | 130.873° SE | 36.004° | 2026-05-13 03:34:58.556Z | 86.44° E |
| 231 mins | 2026-05-13 06:02:58.556Z | 267.362° W | 2026-05-13 07:59:58.556Z | 220.896° SW | 42.028° | 2026-05-13 09:53:58.556Z | 147.751° SSE |
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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