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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 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

8 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 8 hours ago

0 GEESAT 2-04
1 58908U 24023D   25184.16445654  .00000693  00000-0  85610-4 0  9998
2 58908  49.9918 172.7040 0006308 112.4232 247.7379 14.94912285 77070

Epoch: 2025-07-03T03:56Z

TLE epoch observation values (Epoch: 2025-07-03T03:56:49.045Z)

Latitude

-0.00005°

Longitude

-167.93553°

Altitude

584.857 km

Speed

7.568 km/s

True Right ascension

11h 30m 48s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-38.67577°

Longitude

148.60652°

Altitude

599.228 km

Speed

7.558 km/s

Apparent Right ascension

09h 58m 39s

Apparent Declination

-41° 08' 39"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

23:30:04

Azimuth

101.474° ESE

Elevation

-72.635°

Doppler factor

Orbital elements

Apogee altitude

587.8 km

Perigee altitude

579.017 km

Semi-major axis

6,961.545 km

Eccentricity

0.00063

Inclination

49.9918°

RAAN

172.704°

Arg. of periapsis

112.4232°

True anomaly

Unknown

Mean anomaly

247.7379°

Eccentric anomaly

Unknown

Mean motion

3.73667 °/min

Orbital period

96.34 mins

BSTAR

0.00008561

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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.
5 mins	2025-07-04 00:57:32.054Z	174.984° S	2025-07-04 01:00:32.054Z	123.966° SE	19.498°	2025-07-04 01:02:32.054Z	91.643° ESE
7 mins	2025-07-04 02:37:32.054Z	248.177° W	2025-07-04 02:40:32.054Z	345.512° N	42.751°	2025-07-04 02:44:32.054Z	52.088° ENE
5 mins	2025-07-04 04:19:32.054Z	308.497° NW	2025-07-04 04:21:32.054Z	347.606° N	22.558°	2025-07-04 04:24:32.054Z	38.657° NE
5 mins	2025-07-04 06:01:32.054Z	336.772° NNW	2025-07-04 06:03:32.054Z	16.402° NNE	20.845°	2025-07-04 06:06:32.054Z	61.194° ENE
7 mins	2025-07-04 07:41:32.054Z	316.377° NNW	2025-07-04 07:44:32.054Z	32.274° NE	38.482°	2025-07-04 07:48:32.054Z	105.745° ESE
6 mins	2025-07-04 09:22:32.054Z	272.687° WNW	2025-07-04 09:24:32.054Z	234.376° WSW	25.44°	2025-07-04 09:28:32.054Z	165.482° S

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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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