GEESAT 4-09, 65127
Orbit data source: Space-Track
GEESAT 4-09, 65127 is a payload satellite owned by GeeSpace (CN) in LEO that was launched on Fri, 08 Aug 2025 UTC via a JIELONG-3 launch vehicle from the Yellow Sea Launch Area, China (YSLA). Payload-class satellites include a variety of spacecraft 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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65127 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
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
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 GEESAT 4-09
1 65127U 25170J 25283.41171065 .00000685 00000-0 18750-3 0 9994
2 65127 49.9923 258.6472 0021676 173.5635 186.5574 14.57958355 9259Epoch: 2025-10-10T09:52Z
TLE epoch observation values (Epoch: 2025-10-10T09:52:51.800Z)
Latitude
-0.00005°
Longitude
91.17339°
Altitude
715.552 km
Speed
7.491 km/s
True Right ascension
17h 14m 35s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
19:12:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
715.869 km
Perigee altitude
685.181 km
Semi-major axis
7,078.662 km
Eccentricity
0.00217
Inclination
49.9923°
RAAN
258.6472°
Arg. of periapsis
173.5635°
True anomaly
186.52911°
Mean anomaly
186.5574°
Eccentric anomaly
186.54325°
Mean motion
3.64432 °/min
Orbital period
98.78 mins
BSTAR
0.0001875
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Other satellites on launch #170 in the year 2025 (2025-08-08 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.GEESAT 4-09 Visibility forecast
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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 | 2025-10-11 00:53:08.448Z | 184.254° SSW | 2025-10-11 00:55:08.448Z | 125.487° SE | 34.955° | 2025-10-11 00:59:08.448Z | 67.578° E |
| 7 mins | 2025-10-11 02:35:08.448Z | 271.592° WNW | 2025-10-11 02:38:08.448Z | 337.504° N | 35.848° | 2025-10-11 02:42:08.448Z | 46.045° ENE |
| 7 mins | 2025-10-11 04:19:08.448Z | 308.169° NW | 2025-10-11 04:22:08.448Z | 354.2° N | 23.394° | 2025-10-11 04:26:08.448Z | 50.926° ENE |
| 7 mins | 2025-10-11 06:03:08.448Z | 319.579° NNW | 2025-10-11 06:06:08.448Z | 6.995° NNE | 28.592° | 2025-10-11 06:10:08.448Z | 76.904° E |
| 7 mins | 2025-10-11 07:47:08.448Z | 300.344° NW | 2025-10-11 07:50:08.448Z | 221.092° SW | 44.488° | 2025-10-11 07:54:08.448Z | 131.384° SE |
| 6 mins | 2025-10-11 23:52:08.448Z | 176.789° S | 2025-10-11 23:55:08.448Z | 131.857° SE | 22.453° | 2025-10-11 23:58:08.448Z | 86.896° E |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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