CZ-3B R/B, 63362

Orbit data source: Space-Track

CZ-3B R/B, 63362 is space debris in HEO originally from a launch on Wed, 26 Mar 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.

Loading next visibility...

Iframe embed code

<iframe src="https://www.satcat.com/sats-embedded/63362?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/63362?theme=dark&initialShowStats=false

Initial load time (optional)

TLE date request (optional)

Identifier	63362, 2025-062B
Orbit	HEO
Last TLE update	20 hours ago
Origin	CASC (CN / PRC)
Manufacturer	CALT
Mission	Spacecraft
Bus & Motor	CZ-3A STAGE 3, Unknown motor
Mass	~2,800 kg wet, ~2,800 kg dry
Launch date (UTC)	2025-03-26 (6 days ago)
Launch vehicle	Unknown
Launch site	Xichang Space Center, China (XSC)
Object type	Payload Rocket body Debris
Shape & HBR	Unknown
Radar Cross Section	Large (>1 m²)

Expand to show TLE details & history

TLE from 20 hours ago

0 CZ-3B R/B
1 63362U 25062B   25090.10438154  .00095078  93736-6  19867-2 0  9993
2 63362  27.1025  59.1159 7245824 181.3107 174.5793  2.37314134   118

Epoch: 2025-03-31T02:30Z

Definitive object data (Epoch: 2025-03-31T02:30:18.565Z)

Latitude	-0.00003°
Longitude	-167.19973°
Altitude	34,540.649 km
Speed	1.641 km/s
True Right ascension	03h 56m 24s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	0.23278°
Longitude	-167.07848°
Altitude	34,517.858 km
Speed	1.642 km/s
Apparent Right ascension	03h 53m 38s
Apparent Declination	-6° 11' 09"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	04:20:53
Azimuth	189.355° SSW
Elevation	43.471°
Doppler factor	1

Orbital elements

Apogee altitude	34,573.856 km
Perigee altitude	161.939 km
Semi-major axis	23,746.034 km
Eccentricity	0.7245824
Inclination	27.1025°
RAAN	59.1159°
Arg. of periapsis	181.3107°
True anomaly	178.74337°
Mean anomaly	174.5793°
Eccentric anomaly	176.85614°
Mean motion	0.59314 °/min
BSTAR	0.0019867
Orbital period	606.94 mins

Loading maneuver chart data...

Loading historical data...

Other satellites on launch #62 in the year 2025 (2025-03-26 UTC)

TIANLIAN-2 04, 63361

CZ-3B R/B Visibility forecast

Observer location: undefined°, undefined°

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.
296 mins	2025-03-31 22:43:08.901Z	189.351° SSW	2025-04-01 03:19:08.901Z	185.919° SSW	42.276°	2025-04-01 03:39:08.901Z	107.528° ESE
304 mins	2025-04-01 17:39:08.901Z	114.064° SE	2025-04-01 22:24:08.901Z	120.983° SE	34.748°	2025-04-01 22:43:08.901Z	116.195° SE

Authenticating...

Click to sort rows by Secondary header in ascending order	Click to sort rows by Secondary name header in ascending order	Click to sort rows by Country header in ascending order	Click to sort rows by Owner header in ascending order	Click to sort rows by Obj. Type header in ascending order	Click to sort rows by Miss dist. header in ascending order	Click to sort rows by Rel. speed header in ascending order	Click to sort rows by Apr. angle header in ascending order	Click to sort rows by TCA header in ascending order

Check out CZ-3B R/B, 63362 on other resources

View CZ-3B R/B, 63362 on Heavens-Above

View CZ-3B R/B, 63362 on Keep Track

View CZ-3B R/B, 63362 on Celestrak

View CZ-3B R/B, 63362 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.