GEESAT 3-10, 61020
Orbit data source: Space-Track
GEESAT 3-10, 61020 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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61020 intel report (Beta)
GEESAT 3-10 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 | Medium (>0.1 m² and <1 m²) |
Expand to show TLE details & history
TLE from 9 hours ago
0 GEESAT 3-10
1 61020U 24159K 25015.14424982 .00006770 00000-0 68614-3 0 9995
2 61020 50.0007 342.0608 0018592 2.1237 357.9781 14.91747132 19612Epoch: 2025-01-15T03:27Z
Definitive object data (Epoch: 2025-01-15T03:27:43.184Z)
| Latitude | 0.00001° |
| Longitude | 175.29007° |
| Altitude | 580.083 km |
| Speed | 7.579 km/s |
| True Right ascension | 22h 48m 14s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 43.31118° |
| Longitude | -58.26351° |
| Altitude | 601.542 km |
| Speed | 7.562 km/s |
| Apparent Right ascension | 04h 02m 43s |
| Apparent Declination | 6° 03' 30" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 12:41:31 |
| Azimuth | 302.557° NW |
| Elevation | -24.799° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 606.21 km |
| Perigee altitude | 580.287 km |
| Semi-major axis | 6,971.386 km |
| Eccentricity | 0.0018592 |
| Inclination | 50.0007° |
| RAAN | 342.0608° |
| Arg. of periapsis | 2.1237° |
| True anomaly | 357.97057° |
| Mean anomaly | 357.9781° |
| Eccentric anomaly | 357.97433° |
| Mean motion | 3.72876 °/min |
| BSTAR | 0.00068614 |
| 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 3-10 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 | 2025-01-16 00:33:13.480Z | 227.225° WSW | 2025-01-16 00:36:13.480Z | 173.926° S | 43.923° | 2025-01-16 00:40:13.480Z | 58.752° ENE |
| 6 mins | 2025-01-16 02:15:13.480Z | 293.478° NW | 2025-01-16 02:17:13.480Z | 332.989° NNW | 26.261° | 2025-01-16 02:21:13.480Z | 43.008° NE |
| 5 mins | 2025-01-16 03:57:13.480Z | 325.15° NNW | 2025-01-16 03:59:13.480Z | 359.951° N | 20.173° | 2025-01-16 04:02:13.480Z | 48.852° ENE |
| 6 mins | 2025-01-16 05:38:13.480Z | 322.452° NNW | 2025-01-16 05:41:13.480Z | 28.786° NE | 31.656° | 2025-01-16 05:44:13.480Z | 86.582° E |
| 7 mins | 2025-01-16 07:19:13.480Z | 287.722° WNW | 2025-01-16 07:22:13.480Z | 209.004° SW | 36.722° | 2025-01-16 07:26:13.480Z | 146.383° SSE |
Authenticating...
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