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QIANFAN-4, 60382

Orbit data source: Space-Track

QIANFAN-4, 60382 is a Chinese payload satellite in LEO that was launched on Tue, 06 Aug 2024 UTC via a CHANG ZHENG 6A launch vehicle from the Taiyaun Space Center, China (TSC). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

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Iframe URL

https://www.satcat.com/sats-embedded/60382?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60382, 2024-140D

Orbit

LEO

Country

CN / PRC

Related business

Shanghai Spacecom Satellite Technology Ltd (CN)

Manufacturer

SECM

Mission

Operational Commercial Communications

Bus & Motor

QIANFAN, Unknown motor

Mass

267 kg wet, ~267 kg dry

Launch date (UTC)

2024-08-06 (2 years ago)

Launch vehicle

CHANG ZHENG 6A

Launch site

Taiyaun Space Center, China (TSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box + 1 Pan, 5.0 m

Radar Cross Section

13.200 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 6 hours ago

TLE from 6 hours ago

0 QIANFAN-4
1 60382U 24140D   26054.13948667  .00000105  00000-0  14367-3 0  9991
2 60382  88.9737 291.6681 0012878 348.7373  11.3488 13.50998061 77211

Epoch: 2026-02-23T03:20Z

TLE epoch observation values (Epoch: 2026-02-23T03:20:51.648Z)

Latitude

-0.00001°

Longitude

88.41525°

Altitude

1,062.138 km

Speed

7.325 km/s

True Right ascension

19h 26m 40s

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

12:54:38

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,075.226 km

Perigee altitude

1,056.054 km

Semi-major axis

7,443.777 km

Eccentricity

0.00129

Inclination

88.9737°

RAAN

291.6681°

Arg. of periapsis

348.7373°

True anomaly

11.37789°

Mean anomaly

11.3488°

Eccentric anomaly

11.36334°

Mean motion

3.37951 °/min

Orbital period

106.52 mins

BSTAR

0.00014367

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Other satellites on launch #140 in the year 2024 (2024-08-06 UTC)

CZ-6A DEB, 61341 (Decayed)

CZ-6A DEB, 60889

CZ-6A DEB, 60756 (Decayed)

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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.

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QIANFAN-4 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.
12 mins	2026-02-23 15:52:55.253Z	166.312° S	2026-02-23 15:58:55.253Z	103.902° ESE	42.647°	2026-02-23 16:04:55.253Z	5.612° NNE
6 mins	2026-02-23 17:43:55.253Z	256.938° W	2026-02-23 17:45:55.253Z	278.215° WNW	17.501°	2026-02-23 17:49:55.253Z	319.281° NNW
10 mins	2026-02-24 03:03:55.253Z	26.267° NE	2026-02-24 03:08:55.253Z	87.729° E	28.431°	2026-02-24 03:13:55.253Z	141.952° SSE
10 mins	2026-02-24 04:50:55.253Z	336.872° NNW	2026-02-24 04:54:55.253Z	284.573° WNW	32.289°	2026-02-24 05:00:55.253Z	214.868° SW

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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 QIANFAN-4, 60382 on other resources

View QIANFAN-4, 60382 on NASA - NSSDCA Website

View QIANFAN-4, 60382 on Heavens-Above

View QIANFAN-4, 60382 on Keep Track

View QIANFAN-4, 60382 on Celestrak

View QIANFAN-4, 60382 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

QIANFAN-4, 60382

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 6 hours ago

TLE from 6 hours ago

TLE epoch observation values (Epoch: 2026-02-23T03:20:51.648Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #140 in the year 2024 (2024-08-06 UTC)

QIANFAN-4 Visibility forecast

Co-orbital & Co-planar RSOs

Check out QIANFAN-4, 60382 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 6 hours ago