GEESAT 3-09, 61019
Orbit data source: Space-Track
GEESAT 3-09, 61019 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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61019 intel report (Beta)
GEESAT 3-09 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 3-09
1 61019U 24159J 25015.10696657 .00006853 00000-0 69557-3 0 9998
2 61019 49.9986 341.8065 0006987 44.4976 315.6526 14.91762977 19602Epoch: 2025-01-15T02:34Z
Definitive object data (Epoch: 2025-01-15T02:34:01.911Z)
| Latitude | -0.00002° |
| Longitude | -171.50554° |
| Altitude | 589.503 km |
| Speed | 7.569 km/s |
| True Right ascension | 22h 47m 13s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -46.59707° |
| Longitude | 68.64256° |
| Altitude | 612.388 km |
| Speed | 7.551 km/s |
| Apparent Right ascension | 19h 42m 10s |
| Apparent Declination | -71° 47' 41" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 12:23:48 |
| Azimuth | 156.009° SSE |
| Elevation | -43.621° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 598.07 km |
| Perigee altitude | 588.329 km |
| Semi-major axis | 6,971.337 km |
| Eccentricity | 0.0006987 |
| Inclination | 49.9986° |
| RAAN | 341.8065° |
| Arg. of periapsis | 44.4976° |
| True anomaly | 315.5966° |
| Mean anomaly | 315.6526° |
| Eccentric anomaly | 315.6246° |
| Mean motion | 3.7288 °/min |
| BSTAR | 0.00069557 |
| 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 3-09 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 | 2025-01-15 23:37:34.061Z | 189.411° SSW | 2025-01-15 23:40:34.061Z | 135.987° SSE | 25.819° | 2025-01-15 23:43:34.061Z | 81.092° E |
| 6 mins | 2025-01-16 01:18:34.061Z | 261.066° W | 2025-01-16 01:21:34.061Z | 349.708° N | 38.174° | 2025-01-16 01:24:34.061Z | 45.781° ENE |
| 5 mins | 2025-01-16 03:00:34.061Z | 311.45° NW | 2025-01-16 03:02:34.061Z | 347.154° N | 21.283° | 2025-01-16 03:05:34.061Z | 38.425° NE |
| 5 mins | 2025-01-16 04:42:34.061Z | 332.523° NNW | 2025-01-16 04:44:34.061Z | 11.059° NNE | 22.865° | 2025-01-16 04:47:34.061Z | 62.775° ENE |
| 6 mins | 2025-01-16 06:23:34.061Z | 313.132° NW | 2025-01-16 06:25:34.061Z | 350.984° N | 41.749° | 2025-01-16 06:29:34.061Z | 114.2° SE |
| 5 mins | 2025-01-16 08:04:34.061Z | 261.728° W | 2025-01-16 08:06:34.061Z | 225.975° WSW | 19.901° | 2025-01-16 08:09:34.061Z | 180.255° SSW |
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