Kayhan Space Satcat

Watchlists

No new unread notifications...

DECAYED

ZK-1A R/B, 61909 (Decayed)

Orbit data source: Space-Track

ZK-1A R/B, 61909 was space debris in LEO originally from a launch on Mon, 11 Nov 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/61909?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/61909?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

61909, 2024-205R

Orbit

Decayed

Last TLE update

2 weeks ago

Origin

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

Manufacturer

CAS

Mission

Decayed spacecraft

Bus & Motor

Unknown

Mass

500 kg wet, 500 kg dry

Launch date (UTC)

2024-11-11 (6 months ago)

Launch vehicle

Unknown

Launch site

Jiuquan Satellite Launch Center, China (JSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 2.8 m

Radar Cross Section

8.585 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 2 weeks ago

0 ZK-1A R/B
1 61909U 24205R   25109.92697376  .17429277  26733-5  24253-3 0  9998
2 61909  97.4056 198.6236 0011765 214.7533 270.9474 16.48462880 25061

Epoch: 2025-04-19T22:14Z

Definitive object data (Epoch: 2025-04-19T22:14:50.532Z)

Latitude

53.8819°

Longitude

-153.14938°

Altitude

152.225 km

Speed

7.82 km/s

True Right ascension

01h 55m 17s

True Declination

53° 42' 10"

Sunlit

Object was in daylight at TLE epoch

Visualization observer readout

No trajectory is available.

Visualization observer readout

No trajectory is available.

Orbital elements

Apogee altitude

147.852 km

Perigee altitude

132.514 km

Semi-major axis

6,518.32 km

Eccentricity

0.0011765

Inclination

97.4056°

RAAN

198.6236°

Arg. of periapsis

214.7533°

True anomaly

270.8126°

Mean anomaly

270.9474°

Eccentric anomaly

270.88°

Mean motion

4.1242 °/min

BSTAR

0.00024253

Orbital period

87.29 mins

Loading maneuver chart data...

Loading SW <> Apogee altitude chart data...

Loading historical data...

Loading historical data...

Loading historical data...

Loading historical data...

Loading historical data...

Loading historical data...

Loading historical data...

Other satellites on launch #205 in the year 2024 (2024-11-11 UTC)

OBJECT A, 61894

OBJECT B, 61895

OBJECT C, 61896

OBJECT D, 61897

OBJECT E, 61898

OBJECT F, 61899

OBJECT G, 61900

OBJECT H, 61901

OBJECT J, 61902

OBJECT K, 61903

OBJECT L, 61904

OBJECT M, 61905

OBJECT N, 61906

OBJECT P, 61907

OBJECT Q, 61908

ZK-1A 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 ZK-1A R/B, 61909 (Decayed) on other resources

View ZK-1A R/B, 61909 (Decayed) on Celestrak

View ZK-1A R/B, 61909 (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.

|