DECAYED

ZQ-2E R/B, 62113 (Decayed)

Orbit data source: Space-Track

ZQ-2E R/B, 62113 was space debris in LEO originally from a launch on Wed, 27 Nov 2024 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.

Not visible in the next 10 days

Iframe embed code

<iframe src="https://www.satcat.com/sats-embedded/62113?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/62113?theme=dark&initialShowStats=false

Optional Secondary NORAD IDs

Max 10 NORAD IDs; Separated by commas

Initial load time (optional)

ISO8601 Format

TLE date request (optional)

ISO8601 Format

Identifier

62113, 2024-221C

Orbit

Decayed

Last TLE update

6 months ago

Origin

Landspace (CN / PRC)

Manufacturer

Lanjian Hangtian

Mission

Decayed spacecraft

Bus & Motor

ZQ-2 ST 2, Unknown motor

Mass

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

Launch date (UTC)

2024-11-27 (7 months ago)

Launch vehicle

Unknown

Launch site

Jiuquan Satellite Launch Center, China (JSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 12 m

Radar Cross Section

35.980 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 6 months ago

0 ZQ-2E R/B
1 62113U 24221C   24359.27350825  .17063427  11656-4  23207-3 0  9999
2 62113  49.8914 275.2215 0042979 178.2700 320.2910 16.43889986  4294

Epoch: 2024-12-24T06:33Z

TLE epoch observation values (Epoch: 2024-12-24T06:33:51.112Z)

Latitude

30.72693°

Longitude

-126.37869°

Altitude

135.37 km

Speed

7.842 km/s

True Right ascension

04h 21m 28s

True Declination

30° 33' 42"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

No trajectory is available.

Visualization observer readout

No trajectory is available.

Orbital elements

Apogee altitude

184.39 km

Perigee altitude

128.221 km

Semi-major axis

6,534.442 km

Eccentricity

0.0043

Inclination

49.8914°

RAAN

275.2215°

Arg. of periapsis

178.27°

True anomaly

Unknown

Mean anomaly

320.291°

Eccentric anomaly

Unknown

Mean motion

4.10895 °/min

Orbital period

87.61 mins

BSTAR

0.00023207

Loading maneuver chart data...

Loading SW <> Apogee altitude chart data...

Loading historical data...

Other satellites on launch #221 in the year 2024 (2024-11-27 UTC)

GUANGCHUAN 01, 62111

GUANGCHUAN 02, 62112

ZQ-2E R/B Visibility

Observer location: undefined°, undefined°

This satellite is decayed

Authenticating...

Click to sort rows by Secondary header in ascending order	Click to sort rows by Secondary name header in ascending order	Click to sort rows by Country header in ascending order	Click to sort rows by Owner header in ascending order	Click to sort rows by Obj. Type header in ascending order	Click to sort rows by Miss dist. header in ascending order	Click to sort rows by Rel. speed header in ascending order	Click to sort rows by Apr. angle header in ascending order	Click to sort rows by TCA header in ascending order

Check out ZQ-2E R/B, 62113 (Decayed) on other resources

View ZQ-2E R/B, 62113 (Decayed) on Celestrak

View ZQ-2E R/B, 62113 (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.