DECAYED

CZ-2F R/B, 61686 (Decayed)

Orbit data source: Space-Track

CZ-2F R/B, 61686 was space debris in LEO originally from a launch on Tue, 29 Oct 2024 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/61686?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/61686?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

61686, 2024-194D

Orbit

Decayed

Last TLE update

6 months ago

Origin

China Aerospace Science and Technology Corporation (CASC) (CN / PRC)

Manufacturer

CALT?

Mission

Decayed spacecraft

Bus & Motor

CZ-2F, Unknown motor

Mass

5,500 kg wet, 5,500 kg dry

Launch date (UTC)

2024-10-29 (6 months ago)

Launch vehicle

Unknown

Launch site

Jiuquan Satellite Launch Center, China (JSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 15.5 m

Radar Cross Section

44.450 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 6 months ago

0 OBJECT D
1 61686U 24194D   24312.41093039  .05262063  78099-5  37845-3 0  9990
2 61686  41.4558 285.2074 0036233 194.5499 344.2276 16.36423738  1330

Epoch: 2024-11-07T09:51Z

Definitive object data (Epoch: 2024-11-07T09:51:44.385Z)

Latitude

0.83222°

Longitude

-90.75832°

Altitude

151.973 km

Speed

7.831 km/s

True Right ascension

06h 57m 04s

True Declination

0° 49' 36"

Sunlit

Object was in full shadow at TLE epoch

Visualization observer readout

No trajectory is available.

Visualization observer readout

No trajectory is available.

Orbital elements

Apogee altitude

201.393 km

Perigee altitude

153.886 km

Semi-major axis

6,555.777 km

Eccentricity

0.0036233

Inclination

41.4558°

RAAN

285.2074°

Arg. of periapsis

194.5499°

True anomaly

344.11425°

Mean anomaly

344.2276°

Eccentric anomaly

344.17097°

Mean motion

4.0889 °/min

BSTAR

0.00037845

Orbital period

88.04 mins

Loading maneuver chart data...

Loading SW <> Apogee altitude chart data...

Loading historical data...

Other satellites on launch #194 in the year 2024 (2024-10-29 UTC)

SZ-19, 61683 (Decayed)

CZ-2F DEB, 61684 (Decayed)

CZ-2F DEB, 61685 (Decayed)

SZ-19 DEB, 63801

CZ-2F R/B Visibility forecast

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, 61686 (Decayed) on other resources

View CZ-2F R/B, 61686 (Decayed) on Celestrak

View CZ-2F R/B, 61686 (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.