GEESAT 3-01, 61011
Orbit data source: Space-Track
GEESAT 3-01, 61011 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.
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61011 intel report (Beta)
GEESAT 3-01 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 9 hours ago |
| Origin | |
| Manufacturer | Taizhou Xingkong |
| Mission | Operational spacecraft |
| Bus & Motor | GEESAT1, Unknown motor |
| Mass | 130 kg wet, 130 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Unknown |
| Radar Cross Section | Large (>1 m²) |
Expand to show TLE details & history
TLE from 9 hours ago
0 GEESAT 3-01
1 61011U 24159A 25015.12201060 .00007343 00000-0 74345-3 0 9998
2 61011 50.0024 341.9569 0007073 57.1843 302.9779 14.91766602 19632Epoch: 2025-01-15T02:55Z
Definitive object data (Epoch: 2025-01-15T02:55:41.715Z)
| Latitude | -0.00005° |
| Longitude | -176.78584° |
| Altitude | 590.292 km |
| Speed | 7.568 km/s |
| True Right ascension | 22h 47m 49s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 10.39719° |
| Longitude | -7.31062° |
| Altitude | 593.705 km |
| Speed | 7.564 km/s |
| Apparent Right ascension | 07h 07m 51s |
| Apparent Declination | -35° 37' 12" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 12:22:45 |
| Azimuth | 235.461° WSW |
| Elevation | -14.584° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 598.118 km |
| Perigee altitude | 588.257 km |
| Semi-major axis | 6,971.325 km |
| Eccentricity | 0.0007073 |
| Inclination | 50.0024° |
| RAAN | 341.9569° |
| Arg. of periapsis | 57.1843° |
| True anomaly | 302.90988° |
| Mean anomaly | 302.9779° |
| Eccentric anomaly | 302.94389° |
| Mean motion | 3.72881 °/min |
| BSTAR | 0.00074345 |
| Orbital period | 96.55 mins |
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Other satellites on launch #159 in the year 2024 (2024-09-05 UTC)
| GEESAT 3-01, 61011 |
| GEESAT 3-02, 61012 |
| GEESAT 3-03, 61013 |
| GEESAT 3-04, 61014 |
| GEESAT 3-05, 61015 |
| GEESAT 3-06, 61016 |
| GEESAT 3-07, 61017 |
| GEESAT 3-08, 61018 |
| GEESAT 3-09, 61019 |
| GEESAT 3-10, 61020 |
GEESAT 3-01 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-01-15 23:59:30.389Z | 206.77° SW | 2025-01-16 00:03:30.389Z | 121.564° SE | 33.466° | 2025-01-16 00:06:30.389Z | 70.508° E |
| 6 mins | 2025-01-16 01:41:30.389Z | 276.552° WNW | 2025-01-16 01:43:30.389Z | 319.623° NNW | 32.455° | 2025-01-16 01:47:30.389Z | 43.831° NE |
| 5 mins | 2025-01-16 03:23:30.389Z | 318.814° NNW | 2025-01-16 03:25:30.389Z | 354.225° N | 20.25° | 2025-01-16 03:28:30.389Z | 42.823° NE |
| 5 mins | 2025-01-16 05:05:30.389Z | 335.75° NNW | 2025-01-16 05:07:30.389Z | 19.269° NNE | 25.486° | 2025-01-16 05:10:30.389Z | 72° E |
| 7 mins | 2025-01-16 06:45:30.389Z | 302.918° NW | 2025-01-16 06:48:30.389Z | 259.02° W | 44.815° | 2025-01-16 06:52:30.389Z | 127.69° SE |
Authenticating...
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