DECAYED

Showing default

SJ-19, 61444 (Decayed)

Orbit data source: Space-Track

SJ-19, 61444 was a payload satellite owned by CASC (CN) in LEO that was launched on Fri, 27 Sep 2024 UTC via a CHANG ZHENG 2D launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

Loading next visibility...

Iframe embed code

<iframe src="https://www.satcat.com/sats-embedded/61444?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/61444?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

61444, 2024-177A

Orbit

Decayed

Last TLE update

9 months ago

Origin

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

Manufacturer

CAST

Mission

Decayed Civil Reentry Vehicle

Bus & Motor

FSW-1, Unknown motor

Mass

~0 kg wet, ~1,200 kg dry

Launch date (UTC)

2024-09-27 (9 months ago)

Launch vehicle

CHANG ZHENG 2D

Launch site

Jiuquan Satellite Launch Center, China (JSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Rounded Cone, 1.7 m

Radar Cross Section

1.836 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 9 months ago

0 SJ-19
1 61444U 24177A   24284.70845001  .00015258  00000-0  90833-4 0  9993
2 61444  41.6010  76.8644 0006944  34.8351 325.2950 15.77608314  2241

Epoch: 2024-10-10T17:00Z

TLE epoch observation values (Epoch: 2024-10-10T17:00:10.08Z)

Latitude

-0.00001°

Longitude

162.03327°

Altitude

332.999 km

Speed

7.713 km/s

True Right ascension

05h 07m 27s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

No trajectory is available.

Visualization observer readout

No trajectory is available.

Orbital elements

Apogee altitude

344.11 km

Perigee altitude

334.781 km

Semi-major axis

6,717.583 km

Eccentricity

0.00069

Inclination

41.601°

RAAN

76.8644°

Arg. of periapsis

34.8351°

True anomaly

Unknown

Mean anomaly

325.295°

Eccentric anomaly

Unknown

Mean motion

3.94206 °/min

Orbital period

91.32 mins

BSTAR

0.000090833

Loading maneuver chart data...

Loading SW <> Apogee altitude chart data...

Loading historical data...

Other satellites on launch #177 in the year 2024 (2024-09-27 UTC)

CZ-2D R/B, 61445 (Decayed)

SJ-19 DEB, 61505 (Decayed)

SJ-19 DEB, 61506 (Decayed)

SJ-19 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.
4 mins	2025-07-08 07:53:40.749Z	276.499° WNW	2025-07-08 07:55:40.749Z	231.005° WSW	35.765°	2025-07-08 07:57:40.749Z	129.155° 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 SJ-19, 61444 (Decayed) on other resources

View SJ-19, 61444 (Decayed) on Celestrak

View SJ-19, 61444 (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.