GEESAT 3-03, 61013
Orbit data source: Space-Track
GEESAT 3-03, 61013 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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61013 intel report (Beta)
GEESAT 3-03 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 18 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 18 hours ago
0 GEESAT 3-03
1 61013U 24159C 25014.73462428 .00006905 00000-0 70050-3 0 9995
2 61013 49.9950 343.0976 0006069 18.4303 341.6857 14.91770907 19617Epoch: 2025-01-14T17:37Z
Definitive object data (Epoch: 2025-01-14T17:37:51.537Z)
| Latitude | -0.00008° |
| Longitude | -35.80427° |
| Altitude | 588.943 km |
| Speed | 7.569 km/s |
| True Right ascension | 22h 52m 23s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 10.08973° |
| Longitude | 132.04869° |
| Altitude | 595.657 km |
| Speed | 7.562 km/s |
| Apparent Right ascension | 07h 02m 31s |
| Apparent Declination | -32° 48' 57" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 12:43:51 |
| Azimuth | 241.251° WSW |
| Elevation | -17.176° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 597.406 km |
| Perigee altitude | 588.945 km |
| Semi-major axis | 6,971.312 km |
| Eccentricity | 0.0006069 |
| Inclination | 49.995° |
| RAAN | 343.0976° |
| Arg. of periapsis | 18.4303° |
| True anomaly | 341.66383° |
| Mean anomaly | 341.6857° |
| Eccentric anomaly | 341.67477° |
| Mean motion | 3.72882 °/min |
| BSTAR | 0.0007005 |
| 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 3-03 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 | 2025-01-16 00:22:33.241Z | 218.543° SW | 2025-01-16 00:24:33.241Z | 179.03° S | 41.364° | 2025-01-16 00:28:33.241Z | 61.64° ENE |
| 6 mins | 2025-01-16 02:03:33.241Z | 287.96° WNW | 2025-01-16 02:06:33.241Z | 354.512° N | 27.337° | 2025-01-16 02:09:33.241Z | 41.804° NE |
| 5 mins | 2025-01-16 03:45:33.241Z | 321.728° NNW | 2025-01-16 03:47:33.241Z | 355.381° N | 19.966° | 2025-01-16 03:50:33.241Z | 45.538° ENE |
| 6 mins | 2025-01-16 05:27:33.241Z | 332.857° NNW | 2025-01-16 05:29:33.241Z | 21.096° NNE | 29.94° | 2025-01-16 05:33:33.241Z | 88.506° E |
| 7 mins | 2025-01-16 07:07:33.241Z | 292.622° NW | 2025-01-16 07:10:33.241Z | 219.538° SW | 39.708° | 2025-01-16 07:14:33.241Z | 142.472° SSE |
Authenticating...
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