GEESAT 3-06, 61016
Orbit data source: Space-Track
GEESAT 3-06, 61016 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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61016 intel report (Beta)
GEESAT 3-06 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 10 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 10 hours ago
0 GEESAT 3-06
1 61016U 24159F 25015.09231971 .00006862 00000-0 69534-3 0 9992
2 61016 50.0003 342.4744 0013397 350.3971 9.6713 14.91786172 19599Epoch: 2025-01-15T02:12Z
Definitive object data (Epoch: 2025-01-15T02:12:56.422Z)
| Latitude | -0.00003° |
| Longitude | -165.55034° |
| Altitude | 583.707 km |
| Speed | 7.575 km/s |
| True Right ascension | 22h 49m 53s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 8.39148° |
| Longitude | -160.37576° |
| Altitude | 583.368 km |
| Speed | 7.575 km/s |
| Apparent Right ascension | 23h 45m 33s |
| Apparent Declination | -14° 47' 28" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 12:34:53 |
| Azimuth | 26.721° NE |
| Elevation | -62.656° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 602.466 km |
| Perigee altitude | 583.788 km |
| Semi-major axis | 6,971.264 km |
| Eccentricity | 0.0013397 |
| Inclination | 50.0003° |
| RAAN | 342.4744° |
| Arg. of periapsis | 350.3971° |
| True anomaly | 9.69713° |
| Mean anomaly | 9.6713° |
| Eccentric anomaly | 9.68421° |
| Mean motion | 3.72886 °/min |
| BSTAR | 0.00069534 |
| Orbital period | 96.54 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 3-06 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-01-15 23:16:36.611Z | 164.338° S | 2025-01-15 23:18:36.611Z | 131.385° SE | 17.74° | 2025-01-15 23:21:36.611Z | 87.057° E |
| 6 mins | 2025-01-16 00:56:36.611Z | 244.487° WSW | 2025-01-16 00:58:36.611Z | 276.255° WNW | 42.978° | 2025-01-16 01:02:36.611Z | 52.569° ENE |
| 5 mins | 2025-01-16 02:38:36.611Z | 310.359° NW | 2025-01-16 02:40:36.611Z | 352.53° N | 23.498° | 2025-01-16 02:43:36.611Z | 40.535° NE |
| 5 mins | 2025-01-16 04:20:36.611Z | 336.67° NNW | 2025-01-16 04:22:36.611Z | 15.776° NNE | 20.881° | 2025-01-16 04:25:36.611Z | 59.578° ENE |
| 7 mins | 2025-01-16 06:00:36.611Z | 316.463° NNW | 2025-01-16 06:03:36.611Z | 18.927° NNE | 37.015° | 2025-01-16 06:07:36.611Z | 101.54° ESE |
| 6 mins | 2025-01-16 07:41:36.611Z | 280.212° WNW | 2025-01-16 07:44:36.611Z | 220.512° SW | 28.558° | 2025-01-16 07:47:36.611Z | 165.967° S |
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