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QIANFAN-39, 62240

Orbit data source: Space-Track

QIANFAN-39, 62240 is a Chinese payload satellite in LEO that was launched on Thu, 05 Dec 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/62240?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

62240, 2024-232D

Orbit

LEO

Last TLE update

12 hours ago

Origin

Shanghai Spacecom Satellite Technology Ltd (CN / PRC)

Manufacturer

SECM

Mission

Operational Commercial Communications

Bus & Motor

QIANFAN, Unknown motor

Mass

267 kg wet, ~267 kg dry

Launch date (UTC)

2024-12-05 (7 months ago)

Launch vehicle

CHANG ZHENG 6A

Launch site

Taiyaun Space Center, China (TSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box + 1 Pan, 10 m

Radar Cross Section

13.200 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 12 hours ago

0 QIANFAN-39
1 62240U 24232D   25188.88017113  .00000267  00000-0  10757-3 0  9998
2 62240  88.9945  55.4080 0014082 231.4280 128.5652 14.25219249 78908

Epoch: 2025-07-07T21:07Z

TLE epoch observation values (Epoch: 2025-07-07T21:07:26.785Z)

Latitude

-0.00004°

Longitude

172.46323°

Altitude

817.134 km

Speed

7.441 km/s

True Right ascension

03h 41m 37s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

44.65123°

Longitude

173.39394°

Altitude

824.672 km

Speed

7.44 km/s

Apparent Right ascension

06h 24m 48s

Apparent Declination

7° 17' 31"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

21:13:30

Azimuth

49.488° ENE

Elevation

-28.84°

Doppler factor

Orbital elements

Apogee altitude

814.814 km

Perigee altitude

794.584 km

Semi-major axis

7,182.836 km

Eccentricity

0.00141

Inclination

88.9945°

RAAN

55.408°

Arg. of periapsis

231.428°

True anomaly

Unknown

Mean anomaly

128.5652°

Eccentric anomaly

Unknown

Mean motion

3.56533 °/min

Orbital period

100.97 mins

BSTAR

0.00010757

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Other satellites on launch #232 in the year 2024 (2024-12-05 UTC)

QIANFAN-39 Visibility forecast

Observer location: undefined°, undefined°

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.
4 mins	2025-07-08 14:08:40.321Z	94.387° ESE	2025-07-08 14:10:40.321Z	70.542° E	13.566°	2025-07-08 14:12:40.321Z	47.688° ENE
9 mins	2025-07-08 15:46:40.321Z	189.304° SSW	2025-07-08 15:50:40.321Z	263.013° W	42.964°	2025-07-08 15:55:40.321Z	353.239° N
6 mins	2025-07-09 02:22:40.321Z	42.569° NE	2025-07-09 02:25:40.321Z	86.791° E	21.4°	2025-07-09 02:28:40.321Z	126.547° SE
8 mins	2025-07-09 04:02:40.321Z	339.788° N	2025-07-09 04:06:40.321Z	272.731° WNW	32.466°	2025-07-09 04:10:40.321Z	213.697° SW

Authenticating...

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Check out QIANFAN-39, 62240 on other resources

View QIANFAN-39, 62240 on NASA - NSSDCA Website

View QIANFAN-39, 62240 on Heavens-Above

View QIANFAN-39, 62240 on Keep Track

View QIANFAN-39, 62240 on Celestrak

View QIANFAN-39, 62240 on Gunter's Space Page

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