GEESAT 3-08, 61018
Orbit data source: Space-Track
GEESAT 3-08, 61018 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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61018 intel report (Beta)
GEESAT 3-08 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 3-08
1 61018U 24159H 25015.09978742 .00006901 00000-0 70065-3 0 9993
2 61018 50.0062 341.8603 0005374 347.5641 12.5167 14.91742283 19604Epoch: 2025-01-15T02:23Z
Definitive object data (Epoch: 2025-01-15T02:23:41.633Z)
| Latitude | -0.00003° |
| Longitude | -168.86018° |
| Altitude | 589.393 km |
| Speed | 7.569 km/s |
| True Right ascension | 22h 47m 26s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -46.40506° |
| Longitude | 128.11403° |
| Altitude | 606.065 km |
| Speed | 7.557 km/s |
| Apparent Right ascension | 21h 31m 15s |
| Apparent Declination | -52° 16' 12" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 12:23:48 |
| Azimuth | 127.415° SE |
| Elevation | -58.209° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 597.009 km |
| Perigee altitude | 589.516 km |
| Semi-major axis | 6,971.4 km |
| Eccentricity | 0.0005374 |
| Inclination | 50.0062° |
| RAAN | 341.8603° |
| Arg. of periapsis | 347.5641° |
| True anomaly | 12.53005° |
| Mean anomaly | 12.5167° |
| Eccentric anomaly | 12.52338° |
| Mean motion | 3.72875 °/min |
| BSTAR | 0.00070065 |
| 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 3-08 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 23:26:33.904Z | 185.744° SSW | 2025-01-15 23:29:33.904Z | 140.711° SSE | 21.952° | 2025-01-15 23:32:33.904Z | 87.194° E |
| 7 mins | 2025-01-16 01:07:33.904Z | 252.746° W | 2025-01-16 01:10:33.904Z | 339.745° N | 41.399° | 2025-01-16 01:14:33.904Z | 50.728° ENE |
| 5 mins | 2025-01-16 02:49:33.904Z | 306.625° NW | 2025-01-16 02:51:33.904Z | 342.04° N | 22.114° | 2025-01-16 02:54:33.904Z | 35.836° NE |
| 5 mins | 2025-01-16 04:31:33.904Z | 329.735° NNW | 2025-01-16 04:33:33.904Z | 5.93° NNE | 21.944° | 2025-01-16 04:36:33.904Z | 57.869° ENE |
| 6 mins | 2025-01-16 06:12:33.904Z | 316.045° NNW | 2025-01-16 06:15:33.904Z | 52.159° ENE | 39.991° | 2025-01-16 06:18:33.904Z | 106.914° ESE |
| 5 mins | 2025-01-16 07:53:33.904Z | 268.91° W | 2025-01-16 07:55:33.904Z | 231.939° WSW | 23.463° | 2025-01-16 07:58:33.904Z | 177.614° S |
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