DECAYED

ZQ-3 R/B, 66877 (Decayed)

Orbit data source: Space-Track

ZQ-3 R/B, 66877 was space debris in LEO originally from a launch on Wed, 03 Dec 2025 UTC via a ZHUQUE-3 launch vehicle 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

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Iframe URL

https://www.satcat.com/sats-embedded/66877?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

66877, 2025-282A

Orbit

Decayed

Country

CN / PRC

Related business

Landspace (CN)

Manufacturer

Lanjian Hangtian

Mission

Decayed Commercial Technology

Bus & Motor

ZQ-3 ST 2, Unknown motor

Mass

~7,500 kg wet, ~3,500 kg dry

Launch date (UTC)

2025-12-03 (2 months ago)

Launch vehicle

ZHUQUE-3

Launch site

Jiuquan Satellite Launch Center, China (JSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 8.0 m

Radar Cross Section

59.199 m²

Expand to show TLE details & history
Last TLE update: 5 days ago

TLE from 5 days ago

0 ZQ-3 R/B
1 66877U 25282A   26030.41870987  .24115767  12625-4  14011-3 0  9991
2 66877  56.9292 214.3380 0083208 311.3925  48.0041 16.43522473  8782

Epoch: 2026-01-30T10:02Z

TLE epoch observation values (Epoch: 2026-01-30T10:02:56.532Z)

Latitude

0.00001°

Longitude

-66.05488°

Altitude

121.68 km

Speed

7.856 km/s

True Right ascension

14h 17m 21s

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

02:36:51

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

210.463 km

Perigee altitude

101.723 km

Semi-major axis

6,534.23 km

Eccentricity

0.00832

Inclination

56.9292°

RAAN

214.338°

Arg. of periapsis

311.3925°

True anomaly

48.71768°

Mean anomaly

48.0041°

Eccentric anomaly

48.36039°

Mean motion

4.10915 °/min

Orbital period

87.61 mins

BSTAR

0.00014011

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Other satellites on launch #282 in the year 2025 (2025-12-03 UTC)

No other RSOs were in this launch

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ZQ-3 R/B Visibility

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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.
This satellite is decayed.

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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Check out ZQ-3 R/B, 66877 (Decayed) on other resources

View ZQ-3 R/B, 66877 (Decayed) on Celestrak

View ZQ-3 R/B, 66877 (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.

ZQ-3 R/B, 66877 (Decayed)

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 5 days ago

TLE from 5 days ago

TLE epoch observation values (Epoch: 2026-01-30T10:02:56.532Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #282 in the year 2025 (2025-12-03 UTC)

ZQ-3 R/B Visibility

Co-orbital & Co-planar RSOs

Check out ZQ-3 R/B, 66877 (Decayed) on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 5 days ago