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GEESAT 2-04, 58908

Orbit data source: Space-Track

GEESAT 2-04, 58908 is a payload satellite owned by GeeSpace (CN) in LEO that was launched on Fri, 02 Feb 2024 UTC via a CHANG ZHENG 2C launch vehicle from the Xichang Space Center, China (XSC). 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 src="https://www.satcat.com/sats-embedded/58908?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/58908?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

58908, 2024-023D

Orbit

LEO

Last TLE update

4 hours ago

Origin

GeeSpace (CN / PRC)

Manufacturer

Taizhou Xingkong

Mission

Operational Commercial Navigation

Bus & Motor

GEESAT1, Unknown motor

Mass

130 kg wet, 130 kg dry

Launch date (UTC)

2024-02-02 (1 year ago)

Launch vehicle

CHANG ZHENG 2C

Launch site

Xichang Space Center, China (XSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box + 2 Pan, 2 m

Radar Cross Section

0.833 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 4 hours ago

0 GEESAT 2-04
1 58908U 24023D   25123.53100732  .00003196  00000-0  31440-3 0  9999
2 58908  49.9914  98.6669 0006804 239.5772 120.4498 14.94616388 68007

Epoch: 2025-05-03T12:44Z

Definitive object data (Epoch: 2025-05-03T12:44:39.032Z)

Latitude

-0.00008°

Longitude

45.83226°

Altitude

586.512 km

Speed

7.567 km/s

True Right ascension

06h 34m 40s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

-5.85973°

Longitude

-130.04802°

Altitude

582.182 km

Speed

7.572 km/s

Apparent Right ascension

16h 24m 29s

Apparent Declination

-30° 16' 46"

Sunlit

Object is in full shadow

Visualization observer readout

Local Sidereal Time

00:34:14

Azimuth

262.998° W

Elevation

-42.75°

Doppler factor

Orbital elements

Apogee altitude

589.064 km

Perigee altitude

579.59 km

Semi-major axis

6,962.464 km

Eccentricity

0.0006804

Inclination

49.9914°

RAAN

98.6669°

Arg. of periapsis

239.5772°

True anomaly

120.51699°

Mean anomaly

120.4498°

Eccentric anomaly

120.4834°

Mean motion

3.73593 °/min

BSTAR

0.0003144

Orbital period

96.36 mins

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Other satellites on launch #23 in the year 2024 (2024-02-02 UTC)

GEESAT 2-04 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.
6 mins	2025-05-04 00:07:21.651Z	179.667° S	2025-05-04 00:10:21.651Z	134.883° SE	19.407°	2025-05-04 00:13:21.651Z	87.233° E
6 mins	2025-05-04 01:48:21.651Z	248.794° W	2025-05-04 01:50:21.651Z	287.594° WNW	42.171°	2025-05-04 01:54:21.651Z	51.228° ENE
6 mins	2025-05-04 03:29:21.651Z	300.507° NW	2025-05-04 03:32:21.651Z	356.772° N	22.7°	2025-05-04 03:35:21.651Z	42.211° NE
5 mins	2025-05-04 05:11:21.651Z	327.76° NNW	2025-05-04 05:13:21.651Z	2.803° NNE	21.119°	2025-05-04 05:16:21.651Z	54.633° ENE
6 mins	2025-05-04 06:52:21.651Z	319.186° NNW	2025-05-04 06:55:21.651Z	49.636° ENE	37.403°	2025-05-04 06:58:21.651Z	102.159° ESE
5 mins	2025-05-04 08:33:21.651Z	269.311° W	2025-05-04 08:35:21.651Z	226.411° WSW	26.474°	2025-05-04 08:38:21.651Z	170.275° S

Authenticating...

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Check out GEESAT 2-04, 58908 on other resources

View GEESAT 2-04, 58908 on NASA - NSSDCA Website

View GEESAT 2-04, 58908 on Heavens-Above

View GEESAT 2-04, 58908 on Keep Track

View GEESAT 2-04, 58908 on Celestrak

View GEESAT 2-04, 58908 on Gunter's Space Page

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