Showing default

GEESAT 3-04, 61014

Orbit data source: Space-Track

GEESAT 3-04, 61014 is a payload satellite owned by GeeSpace (CN) in LEO that was launched on Thu, 05 Sep 2024 UTC via a CHANG ZHENG 6 launch vehicle from the Taiyaun Space Center, China (TSC). Payloads include a variety of satellites, spacecraft, and rockets 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.

Loading next visibility...

GEESAT 3-04 details

Identifier	61014, 2024-159D
Orbit	LEO
Last TLE update	17 hours ago
Origin	GeeSpace (CN / PRC)
Manufacturer	Taizhou Xingkong
Mission	Operational spacecraft
Bus & Motor	GEESAT1, Unknown motor
Mass	130 kg wet, 130 kg dry
Launch date (UTC)	2024-09-05 (4 months ago)
Launch vehicle	CHANG ZHENG 6
Launch site	Taiyaun Space Center, China (TSC)
Object type	Payload Rocket body Debris
Shape & HBR	Unknown
Radar Cross Section	Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history

TLE from 17 hours ago

0 GEESAT 3-04
1 61014U 24159D   25014.77281457  .00078776  00000-0  11970-2 0  9991
2 61014  50.0007 304.4735 0018174  21.1275 339.0440 15.53637068 20123

Epoch: 2025-01-14T18:32Z

Definitive object data (Epoch: 2025-01-14T18:32:51.178Z)

Latitude	-0°
Longitude	-88.21445°
Altitude	395.168 km
Speed	7.681 km/s
True Right ascension	20h 17m 53s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	4.80361°
Longitude	-87.85184°
Altitude	394.143 km
Speed	7.682 km/s
Apparent Right ascension	21h 56m 02s
Apparent Declination	-18° 58' 22"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	12:13:24
Azimuth	64.744° ENE
Elevation	-53.853°
Doppler factor	1

Orbital elements

Apogee altitude	419.23 km
Perigee altitude	394.568 km
Semi-major axis	6,785.036 km
Eccentricity	0.0018174
Inclination	50.0007°
RAAN	304.4735°
Arg. of periapsis	21.1275°
True anomaly	338.96936°
Mean anomaly	339.044°
Eccentric anomaly	339.00669°
Mean motion	3.88343 °/min
BSTAR	0.001197
Orbital period	92.7 mins

Loading maneuver chart data...

Loading historical data...

Other satellites on launch #159 in the year 2024 (2024-09-05 UTC)

GEESAT 3-04 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.
4 mins	2025-01-15 20:57:10.978Z	173.376° S	2025-01-15 20:59:10.978Z	131.11° SE	16.509°	2025-01-15 21:01:10.978Z	91.327° ESE
4 mins	2025-01-15 22:34:10.978Z	268.024° W	2025-01-15 22:35:10.978Z	309.036° NW	37.481°	2025-01-15 22:38:10.978Z	46.224° ENE
4 mins	2025-01-16 03:26:10.978Z	336.688° NNW	2025-01-16 03:27:10.978Z	12.168° NNE	31.98°	2025-01-16 03:30:10.978Z	96.853° ESE

Authenticating...

Click to sort rows by NORAD ID header in ascending order	Click to sort rows by Common 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 GEESAT 3-04, 61014 on other resources

View GEESAT 3-04, 61014 on NASA - NSSDCA Website

View GEESAT 3-04, 61014 on Heavens-Above

View GEESAT 3-04, 61014 on Keep Track

View GEESAT 3-04, 61014 on Celestrak

View GEESAT 3-04, 61014 on Gunter's Space Page

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