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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Iframe URL

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 (8 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)

Expand to show TLE details & history
Last TLE update: 7 hours ago

TLE from 7 hours ago

0 CZ-2D DEB
1 44612U 17060E   26095.50862475  .00006192  00000-0  58589-3 0  9996
2 44612  97.5928 101.8177 0009880 349.0450  11.0553 14.93956132456030

Epoch: 2026-04-05T12:12Z

TLE epoch observation values (Epoch: 2026-04-05T12:12:25.178Z)

Latitude

-0.00009°

Longitude

84.89977°

Altitude

581.911 km

Speed

7.573 km/s

True Right ascension

06h 47m 16s

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

01:09:57

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

589.501 km

Perigee altitude

575.746 km

Semi-major axis

6,960.76 km

Eccentricity

0.00099

Inclination

97.5928°

RAAN

101.8177°

Arg. of periapsis

349.045°

True anomaly

11.07704°

Mean anomaly

11.0553°

Eccentric anomaly

11.06617°

Mean motion

3.7373 °/min

Orbital period

96.33 mins

BSTAR

0.00058589

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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.
6 mins	2026-04-05 23:36:01.485Z	121.333° SE	2026-04-05 23:39:01.485Z	69.255° E	22.75°	2026-04-05 23:42:01.485Z	17.459° NNE
4 mins	2026-04-06 01:13:01.485Z	235.071° WSW	2026-04-06 01:14:01.485Z	256.319° W	22.155°	2026-04-06 01:17:01.485Z	313.159° NW
6 mins	2026-04-06 12:54:01.485Z	30.476° NE	2026-04-06 12:57:01.485Z	115.058° SE	36.805°	2026-04-06 13:00:01.485Z	172.156° S

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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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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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: 7 hours ago

TLE from 7 hours ago

TLE epoch observation values (Epoch: 2026-04-05T12:12:25.178Z)

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: 7 hours ago