CZ-3B R/B, 41022
Orbit data source: Space-Track
CZ-3B R/B, 41022 is space debris in HEO originally from a launch on Tue, 03 Nov 2015 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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41022 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, 6.2 m
Radar Cross Section
32.704 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 CZ-3B R/B
1 41022U 15063B 26171.35473797 .00038765 00000-0 14881-2 0 9999
2 41022 26.7558 191.0220 6150735 96.3490 332.4522 3.88364634109025Epoch: 2026-06-20T08:30Z
TLE epoch observation values (Epoch: 2026-06-20T08:30:49.360Z)
Latitude
-0.00006°
Longitude
154.76834°
Altitude
5,006.539 km
Speed
6.834 km/s
True Right ascension
12h 44m 10s
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
21:31:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
21,239.989 km
Perigee altitude
204.194 km
Semi-major axis
17,100.228 km
Eccentricity
0.61507
Inclination
26.7558°
RAAN
191.022°
Arg. of periapsis
96.349°
True anomaly
263.73597°
Mean anomaly
332.4522°
Eccentric anomaly
302.84455°
Mean motion
0.9706 °/min
Orbital period
370.9 mins
BSTAR
0.0014881
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Other satellites on launch #63 in the year 2015 (2015-11-03 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. |
|---|---|---|---|---|---|---|---|
| 118 mins | 2026-06-22 19:43:54.033Z | 171.39° S | 2026-06-22 21:08:54.033Z | 161.135° S | 11.226° | 2026-06-22 21:41:54.033Z | 149.941° SSE |
| 9 mins | 2026-06-23 04:38:54.033Z | 221.971° SW | 2026-06-23 04:44:54.033Z | 195.309° SSW | 16.132° | 2026-06-23 04:47:54.033Z | 163.586° 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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