DECAYED

CZ-2F R/B, 63633 (Decayed)

Orbit data source: Space-Track

CZ-2F R/B, 63633 was space debris in LEO originally from a launch on Thu, 24 Apr 2025 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). 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.

Not visible in the next 10 days

Iframe embed code

<iframe src="https://www.satcat.com/sats-embedded/63633?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/63633?theme=dark&initialShowStats=false

Optional Secondary NORAD IDs

Max 10 NORAD IDs; Separated by commas

Initial load time (optional)

ISO8601 Format

TLE date request (optional)

ISO8601 Format

Identifier

63633, 2025-082B

Orbit

Decayed

Last TLE update

3 weeks ago

Origin

Unknown

Manufacturer

Unknown

Mission

Decayed spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2025-04-24 (4 weeks ago)

Launch vehicle

Unknown

Launch site

Jiuquan Satellite Launch Center, China (JSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Large (>1 m²)

Expand to show TLE details & history

TLE from 3 weeks ago

0 CZ-2F R/B
1 63633U 25082B   25122.79872868  .12669141  78614-5  34580-3 0  9999
2 63633  41.4570 292.5240 0026111 206.6050 247.2406 16.42622166  1314

Epoch: 2025-05-02T19:10Z

TLE epoch observation values (Epoch: 2025-05-02T19:10:10.157Z)

Latitude

41.52272°

Longitude

-121.20485°

Altitude

168.009 km

Speed

7.808 km/s

True Right ascension

01h 49m 09s

True Declination

41° 20' 12"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

No trajectory is available.

Visualization observer readout

No trajectory is available.

Orbital elements

Apogee altitude

178.223 km

Perigee altitude

144.074 km

Semi-major axis

6,539.286 km

Eccentricity

0.00261

Inclination

41.457°

RAAN

292.524°

Arg. of periapsis

206.605°

True anomaly

Unknown

Mean anomaly

247.2406°

Eccentric anomaly

Unknown

Mean motion

4.10438 °/min

Orbital period

87.71 mins

BSTAR

0.0003458

Loading maneuver chart data...

Loading SW <> Apogee altitude chart data...

Loading historical data...

Other satellites on launch #82 in the year 2025 (2025-04-24 UTC)

SZ-20, 63632

CZ-2F R/B Visibility

Observer location: undefined°, undefined°

This satellite is decayed

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-2F R/B, 63633 (Decayed) on other resources

View CZ-2F R/B, 63633 (Decayed) on Celestrak

View CZ-2F R/B, 63633 (Decayed) on Gunter's Space Page

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