GEESAT 4-10, 65128
Orbit data source: Space-Track
GEESAT 4-10, 65128 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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65128 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, 1.0 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 4-10
1 65128U 25170K 25283.41081472 .00003517 00000-0 41435-3 0 9990
2 65128 49.9921 252.8799 0032146 188.2728 171.7685 14.86677113 9336Epoch: 2025-10-10T09:51Z
TLE epoch observation values (Epoch: 2025-10-10T09:51:34.391Z)
Latitude
-0.00006°
Longitude
85.72951°
Altitude
631.098 km
Speed
7.532 km/s
True Right ascension
16h 51m 31s
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
19:03:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
631.548 km
Perigee altitude
586.626 km
Semi-major axis
6,987.224 km
Eccentricity
0.00321
Inclination
49.9921°
RAAN
252.8799°
Arg. of periapsis
188.2728°
True anomaly
171.82103°
Mean anomaly
171.7685°
Eccentric anomaly
171.79479°
Mean motion
3.71609 °/min
Orbital period
96.88 mins
BSTAR
0.00041435
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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 4-10 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-11 02:14:06.569Z | 269.101° W | 2025-10-11 02:17:06.569Z | 320.515° NNW | 33.002° | 2025-10-11 02:21:06.569Z | 43.573° NE |
| 5 mins | 2025-10-11 03:57:06.569Z | 314.462° NW | 2025-10-11 03:59:06.569Z | 346.695° N | 20.722° | 2025-10-11 04:02:06.569Z | 38.708° NE |
| 6 mins | 2025-10-11 05:39:06.569Z | 325.96° NNW | 2025-10-11 05:42:06.569Z | 25.86° NE | 26.13° | 2025-10-11 05:45:06.569Z | 74.849° E |
| 7 mins | 2025-10-11 07:20:06.569Z | 301.971° NW | 2025-10-11 07:23:06.569Z | 263.358° W | 44.395° | 2025-10-11 07:27:06.569Z | 129.349° SE |
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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