ZQ-2E R/B, 69095

Orbit data source: Space-Track

ZQ-2E R/B, 69095 is space debris in LEO originally from a launch on Wed, 13 May 2026 UTC via a ZHUQUE-2E 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.

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https://www.satcat.com/sats-embedded/69095?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

69095, 2026-105A

Orbit

LEO

Country

CN / PRC

Related business

Landspace (CN)

Manufacturer

Lanjian Hangtian

Mission

Operational spacecraft

Bus & Motor

ZQ-2 ST 2, Unknown motor

Mass

~5,000 kg wet, ~5,000 kg dry

Launch date (UTC)

2026-05-13 (1 month ago)

Launch vehicle

ZHUQUE-2E

Launch site

Jiuquan Satellite Launch Center, China (JSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 8.0 m

Radar Cross Section

Large (>1 m²)

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

TLE from 12 hours ago

0 ZQ-2E R/B
1 69095U 26105A   26168.59513014  .00096306 -57633-6  23476-3 0  9994
2 69095  88.9689 194.2117 0446413 296.8149  58.8097 15.17404330  5218

Epoch: 2026-06-17T14:16Z

TLE epoch observation values (Epoch: 2026-06-17T14:16:59.244Z)

Latitude

0.00003°

Longitude

74.11429°

Altitude

367.926 km

Speed

7.771 km/s

True Right ascension

12h 56m 50s

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

12:33:28

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

818.01 km

Perigee altitude

202.975 km

Semi-major axis

6,888.63 km

Eccentricity

0.04464

Inclination

88.9689°

RAAN

194.2117°

Arg. of periapsis

296.8149°

True anomaly

63.31119°

Mean anomaly

58.8097°

Eccentric anomaly

61.0478°

Mean motion

3.79615 °/min

Orbital period

94.83 mins

BSTAR

0.00023476

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Other satellites on launch #105 in the year 2026 (2026-05-13 UTC)

DUMMY MASS 4, 69096 (Decayed)

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ZQ-2E R/B 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	2026-06-18 03:04:38.600Z	232.684° WSW	2026-06-18 03:07:38.600Z	286.684° WNW	20.221°	2026-06-18 03:10:38.600Z	329.744° NNW
7 mins	2026-06-18 13:01:38.600Z	36.195° NE	2026-06-18 13:04:38.600Z	76.369° E	21.914°	2026-06-18 13:08:38.600Z	130.863° SE
7 mins	2026-06-18 14:36:38.600Z	337.8° N	2026-06-18 14:39:38.600Z	286.905° WNW	33.709°	2026-06-18 14:43:38.600Z	213.944° SW
4 mins	2026-06-19 01:15:38.600Z	100.695° ESE	2026-06-19 01:16:38.600Z	81.107° E	19.969°	2026-06-19 01:19:38.600Z	33.411° NE

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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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Check out ZQ-2E R/B, 69095 on other resources

View ZQ-2E R/B, 69095 on Heavens-Above

View ZQ-2E R/B, 69095 on Keep Track

View ZQ-2E R/B, 69095 on Celestrak

View ZQ-2E R/B, 69095 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-2E R/B, 69095

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: 2026-06-17T14:16:59.244Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #105 in the year 2026 (2026-05-13 UTC)

ZQ-2E R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out ZQ-2E R/B, 69095 on other resources

Documentation

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