GEESAT 3-02, 61012
Orbit data source: Space-Track
GEESAT 3-02, 61012 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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61012 intel report (Beta)
GEESAT 3-02 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 3-02
1 61012U 24159B 25015.11461476 .00006644 00000-0 67521-3 0 9998
2 61012 49.9955 342.5514 0008028 91.2992 268.8869 14.91748974 19626Epoch: 2025-01-15T02:45Z
Definitive object data (Epoch: 2025-01-15T02:45:02.715Z)
| Latitude | -0.00004° |
| Longitude | -173.52155° |
| Altitude | 593.141 km |
| Speed | 7.565 km/s |
| True Right ascension | 22h 50m 12s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -46.50412° |
| Longitude | 123.04822° |
| Altitude | 613.35 km |
| Speed | 7.55 km/s |
| Apparent Right ascension | 21h 42m 43s |
| Apparent Declination | -53° 31' 33" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 12:45:06 |
| Azimuth | 129.48° SE |
| Elevation | -56.617° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 598.84 km |
| Perigee altitude | 587.647 km |
| Semi-major axis | 6,971.381 km |
| Eccentricity | 0.0008028 |
| Inclination | 49.9955° |
| RAAN | 342.5514° |
| Arg. of periapsis | 91.2992° |
| True anomaly | 268.79493° |
| Mean anomaly | 268.8869° |
| Eccentric anomaly | 268.84091° |
| Mean motion | 3.72876 °/min |
| BSTAR | 0.00067521 |
| 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 3-02 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 23:48:47.914Z | 195.438° SSW | 2025-01-15 23:51:47.914Z | 140.81° SSE | 28.876° | 2025-01-15 23:55:47.914Z | 72.06° E |
| 7 mins | 2025-01-16 01:29:47.914Z | 264.794° W | 2025-01-16 01:32:47.914Z | 339.373° N | 36.448° | 2025-01-16 01:36:47.914Z | 48.066° ENE |
| 4 mins | 2025-01-16 03:12:47.914Z | 324.963° NNW | 2025-01-16 03:13:47.914Z | 343.806° N | 20.522° | 2025-01-16 03:16:47.914Z | 36.807° NE |
| 5 mins | 2025-01-16 04:53:47.914Z | 329.865° NNW | 2025-01-16 04:55:47.914Z | 7.072° NNE | 23.541° | 2025-01-16 04:58:47.914Z | 63.189° ENE |
| 6 mins | 2025-01-16 06:34:47.914Z | 308.83° NW | 2025-01-16 06:37:47.914Z | 87.611° E | 43.261° | 2025-01-16 06:40:47.914Z | 119.058° SE |
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