CZ-2D DEB, 44612

Orbit data source: Space-Track

CZ-2D DEB, 44612 is space debris in SSO originally from a launch on Mon, 09 Oct 2017 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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https://www.satcat.com/sats-embedded/44612?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

44612, 2017-060E

Orbit

SSO

Country

CN / PRC

Related business

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

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2017-10-09 (9 years ago)

Launch vehicle

Unknown

Launch site

Jiuquan Satellite Launch Center, China (JSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.1 m

Radar Cross Section

Small (<0.1 m²)

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Last TLE update: 12 hours ago

TLE from 12 hours ago

0 CZ-2D DEB
1 44612U 17060E   26128.72710927  .00002768  00000-0  26330-3 0  9995
2 44612  97.5906 133.9332 0009305 219.6868 140.3673 14.94199394460991

Epoch: 2026-05-08T17:27Z

TLE epoch observation values (Epoch: 2026-05-08T17:27:02.240Z)

Latitude

-0°

Longitude

5.61912°

Altitude

592.902 km

Speed

7.561 km/s

True Right ascension

08h 55m 43s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

13:49:28

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

588.343 km

Perigee altitude

575.391 km

Semi-major axis

6,960.004 km

Eccentricity

0.00093

Inclination

97.5906°

RAAN

133.9332°

Arg. of periapsis

219.6868°

True anomaly

140.43525°

Mean anomaly

140.3673°

Eccentric anomaly

140.40128°

Mean motion

3.73791 °/min

Orbital period

96.31 mins

BSTAR

0.0002633

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Other satellites on launch #60 in the year 2017 (2017-10-09 UTC)

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CZ-2D DEB Visibility forecast

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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.
7 mins	2026-05-09 13:17:43.272Z	8.637° NNE	2026-05-09 13:21:43.272Z	258.774° W	44.024°	2026-05-09 13:24:43.272Z	199.691° SSW
6 mins	2026-05-10 00:07:43.272Z	148.964° SSE	2026-05-10 00:10:43.272Z	39.717° NE	39.557°	2026-05-10 00:13:43.272Z	356.774° N

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Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

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Check out CZ-2D DEB, 44612 on other resources

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View CZ-2D DEB, 44612 on Celestrak

View CZ-2D DEB, 44612 on Gunter's Space Page

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CZ-2D DEB, 44612

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 12 hours ago

TLE from 12 hours ago

TLE epoch observation values (Epoch: 2026-05-08T17:27:02.240Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #60 in the year 2017 (2017-10-09 UTC)

CZ-2D DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-2D DEB, 44612 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 12 hours ago