GEESAT 4-05, 65123
Orbit data source: Space-Track
GEESAT 4-05, 65123 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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65123 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: 16 hours ago
TLE from 16 hours ago
0 GEESAT 4-05
1 65123U 25170E 25283.36588729 .00003631 00000-0 42885-3 0 9993
2 65123 49.9909 253.3300 0020573 168.5200 191.6212 14.86684352 9327Epoch: 2025-10-10T08:46Z
TLE epoch observation values (Epoch: 2025-10-10T08:46:52.661Z)
Latitude
-0.00008°
Longitude
102.39775°
Altitude
622.927 km
Speed
7.541 km/s
True Right ascension
16h 53m 19s
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
19:08:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
623.44 km
Perigee altitude
594.69 km
Semi-major axis
6,987.202 km
Eccentricity
0.00206
Inclination
49.9909°
RAAN
253.33°
Arg. of periapsis
168.52°
True anomaly
191.57383°
Mean anomaly
191.6212°
Eccentric anomaly
191.5975°
Mean motion
3.71611 °/min
Orbital period
96.88 mins
BSTAR
0.00042885
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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 4-05 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-10-11 01:05:31.766Z | 228.944° WSW | 2025-10-11 01:09:31.766Z | 167.999° S | 44.27° | 2025-10-11 01:13:31.766Z | 58.46° ENE |
| 6 mins | 2025-10-11 02:48:31.766Z | 290.317° WNW | 2025-10-11 02:51:31.766Z | 351.203° N | 26.725° | 2025-10-11 02:54:31.766Z | 40.388° NE |
| 5 mins | 2025-10-11 04:31:31.766Z | 329.618° NNW | 2025-10-11 04:33:31.766Z | 6.29° NNE | 20.64° | 2025-10-11 04:36:31.766Z | 52.137° ENE |
| 7 mins | 2025-10-11 06:12:31.766Z | 321.719° NNW | 2025-10-11 06:15:31.766Z | 27.492° NE | 32.324° | 2025-10-11 06:19:31.766Z | 93.504° ESE |
| 7 mins | 2025-10-11 07:53:31.766Z | 289.233° WNW | 2025-10-11 07:56:31.766Z | 227.047° WSW | 35.959° | 2025-10-11 08:00:31.766Z | 149.213° SSE |
| 6 mins | 2025-10-11 23:39:31.766Z | 179.021° S | 2025-10-11 23:42:31.766Z | 125.02° SE | 22.908° | 2025-10-11 23:45:31.766Z | 80.504° E |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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