GEESAT 3-05, 61015
Orbit data source: Space-Track
GEESAT 3-05, 61015 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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61015 intel report (Beta)
GEESAT 3-05 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 3-05
1 61015U 24159E 25015.12904564 .00008453 00000-0 85237-3 0 9996
2 61015 50.0051 342.0317 0008266 315.7202 44.3078 14.91745112 19616Epoch: 2025-01-15T03:05Z
Definitive object data (Epoch: 2025-01-15T03:05:49.543Z)
| Latitude | 0° |
| Longitude | -179.25055° |
| Altitude | 588.92 km |
| Speed | 7.569 km/s |
| True Right ascension | 22h 48m 07s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 7.24308° |
| Longitude | -7.05924° |
| Altitude | 597.182 km |
| Speed | 7.56 km/s |
| Apparent Right ascension | 07h 21m 28s |
| Apparent Declination | -38° 44' 22" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 12:34:05 |
| Azimuth | 232.646° WSW |
| Elevation | -16.186° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 599.017 km |
| Perigee altitude | 587.492 km |
| Semi-major axis | 6,971.391 km |
| Eccentricity | 0.0008266 |
| Inclination | 50.0051° |
| RAAN | 342.0317° |
| Arg. of periapsis | 315.7202° |
| True anomaly | 44.37401° |
| Mean anomaly | 44.3078° |
| Eccentric anomaly | 44.3409° |
| Mean motion | 3.72876 °/min |
| BSTAR | 0.00085237 |
| 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 3-05 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-01-16 00:09:49.271Z | 214.168° SW | 2025-01-16 00:13:49.271Z | 130.19° SE | 37.96° | 2025-01-16 00:17:49.271Z | 64.162° ENE |
| 6 mins | 2025-01-16 01:51:49.271Z | 278.44° WNW | 2025-01-16 01:54:49.271Z | 345.257° N | 30.776° | 2025-01-16 01:57:49.271Z | 40.469° NE |
| 4 mins | 2025-01-16 03:34:49.271Z | 330.012° NNW | 2025-01-16 03:35:49.271Z | 348.124° N | 19.932° | 2025-01-16 03:38:49.271Z | 40.09° NE |
| 6 mins | 2025-01-16 05:15:49.271Z | 330.175° NNW | 2025-01-16 05:17:49.271Z | 10.548° NNE | 27.143° | 2025-01-16 05:21:49.271Z | 80.757° E |
| 6 mins | 2025-01-16 06:56:49.271Z | 296.861° NW | 2025-01-16 06:58:49.271Z | 261.803° W | 42.455° | 2025-01-16 07:02:49.271Z | 134.431° SE |
Authenticating...
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