CZ-2D DEB, 44606

Orbit data source: Space-Track

CZ-2D DEB, 44606 is space debris in SSO originally from a launch on Fri, 11 Nov 2016 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.

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Iframe URL

https://www.satcat.com/sats-embedded/44606?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

44606, 2016-068F

Orbit

SSO

Last TLE update

4 hours ago

Origin

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

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2016-11-11 (9 years ago)

Launch vehicle

Unknown

Launch site

Jiuquan Satellite Launch Center, China (JSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history

TLE from 4 hours ago

0 CZ-2D DEB
1 44606U 16068F   25182.22760868  .00000486  00000-0  32922-3 0  9997
2 44606  98.4421 284.9000 0225976 100.9267 261.7408 13.92497459437587

Epoch: 2025-07-01T05:27Z

TLE epoch observation values (Epoch: 2025-07-01T05:27:45.389Z)

Latitude

-0.00002°

Longitude

-76.5652°

Altitude

950.107 km

Speed

7.363 km/s

True Right ascension

18h 59m 36s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

-32.81889°

Longitude

98.13964°

Altitude

992.255 km

Speed

7.324 km/s

Apparent Right ascension

07h 54m 52s

Apparent Declination

-37° 57' 09"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

21:32:48

Azimuth

91.967° ESE

Elevation

-70.916°

Doppler factor

Orbital elements

Apogee altitude

1,081.927 km

Perigee altitude

752.218 km

Semi-major axis

7,295.21 km

Eccentricity

0.0226

Inclination

98.4421°

RAAN

284.9°

Arg. of periapsis

100.9267°

True anomaly

Unknown

Mean anomaly

261.7408°

Eccentric anomaly

Unknown

Mean motion

3.48326 °/min

Orbital period

103.35 mins

BSTAR

0.00032922

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Other satellites on launch #68 in the year 2016 (2016-11-11 UTC)

YUNHAI 1, 41857

CZ-2D R/B, 41858

CZ-2D DEB, 44603

CZ-2D DEB, 44604 (Decayed)

CZ-2D DEB, 44605

CZ-2D DEB, 44607

CZ-2D DEB 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.
10 mins	2025-07-01 19:49:26.715Z	11.369° NNE	2025-07-01 19:54:26.715Z	253.955° W	44.72°	2025-07-01 19:59:26.715Z	197.64° SSW
6 mins	2025-07-02 05:46:26.715Z	102.908° ESE	2025-07-02 05:48:26.715Z	73.996° E	22.224°	2025-07-02 05:52:26.715Z	17.955° NNE
8 mins	2025-07-02 07:27:26.715Z	201.248° SSW	2025-07-02 07:30:26.715Z	249.704° W	32.844°	2025-07-02 07:35:26.715Z	329.828° NNW

Authenticating...

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Check out CZ-2D DEB, 44606 on other resources

View CZ-2D DEB, 44606 on Heavens-Above

View CZ-2D DEB, 44606 on Keep Track

View CZ-2D DEB, 44606 on Celestrak

View CZ-2D DEB, 44606 on Gunter's Space Page

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