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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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
GWCG
Mission
Operational Commercial Navigation
Bus & Motor
GPS100, Unknown motor
Mass
130 kg wet, 130 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.833 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 4 days ago
TLE from 4 days ago
0 GEESAT 4-05
1 65123U 25170E 26155.29507250 .00001728 00000-0 24285-3 0 9993
2 65123 49.9936 188.1794 0008349 271.6400 88.3582 14.82095231 45133Epoch: 2026-06-04T07:04Z
TLE epoch observation values (Epoch: 2026-06-04T07:04:54.264Z)
Latitude
0.00006°
Longitude
-170.78804°
Altitude
623.099 km
Speed
7.549 km/s
True Right ascension
12h 32m 43s
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
10:51:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
629.323 km
Perigee altitude
617.631 km
Semi-major axis
7,001.614 km
Eccentricity
0.00083
Inclination
49.9936°
RAAN
188.1794°
Arg. of periapsis
271.64°
True anomaly
88.45384°
Mean anomaly
88.3582°
Eccentric anomaly
88.40602°
Mean motion
3.70464 °/min
Orbital period
97.18 mins
BSTAR
0.00024285
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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 | 2026-06-08 03:28:55.441Z | 209.002° SW | 2026-06-08 03:32:55.441Z | 126.648° SE | 35.704° | 2026-06-08 03:36:55.441Z | 65.876° ENE |
| 7 mins | 2026-06-08 05:10:55.441Z | 270.946° WNW | 2026-06-08 05:13:55.441Z | 325.719° NNW | 32.995° | 2026-06-08 05:17:55.441Z | 44.116° NE |
| 5 mins | 2026-06-08 06:54:55.441Z | 325.778° NNW | 2026-06-08 06:56:55.441Z | 3.157° NNE | 21.222° | 2026-06-08 06:59:55.441Z | 47.095° ENE |
| 6 mins | 2026-06-08 08:36:55.441Z | 331.628° NNW | 2026-06-08 08:38:55.441Z | 12.184° NNE | 27.307° | 2026-06-08 08:42:55.441Z | 79.152° E |
| 7 mins | 2026-06-08 10:17:55.441Z | 300.651° NW | 2026-06-08 10:20:55.441Z | 230.274° WSW | 44.417° | 2026-06-08 10:24:55.441Z | 131.089° 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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