GEESAT 2-03, 58907
Orbit data source: Space-Track
GEESAT 2-03, 58907 is a payload satellite owned by GeeSpace (CN) in LEO that was launched on Fri, 02 Feb 2024 UTC via a CHANG ZHENG 2C launch vehicle from the Xichang Space Center, China (XSC). 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.
Focus sentinelFocus sentinel
Request partner network tasking
Focus sentinelFocus sentinel
Embed this page
Focus sentinelFocus sentinel
58907 intel report (Beta)
Focus sentinelFocus sentinel
Edit Public Description
Focus sentinelFocus sentinel
Edit Sat Name
Focus sentinelFocus sentinel
Create New Watchlist
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: 2 days ago
TLE from 2 days ago
0 GEESAT 2-03
1 58907U 24023C 26171.38392579 .00001744 00000-0 17130-3 0 9994
2 58907 50.0027 309.1363 0005839 48.6385 311.5060 14.97102096129804Epoch: 2026-06-20T09:12Z
TLE epoch observation values (Epoch: 2026-06-20T09:12:51.188Z)
Latitude
-0.00004°
Longitude
-97.67635°
Altitude
573.714 km
Speed
7.577 km/s
True Right ascension
20h 36m 32s
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
21:40:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
580.679 km
Perigee altitude
572.557 km
Semi-major axis
6,954.755 km
Eccentricity
0.00058
Inclination
50.0027°
RAAN
309.1363°
Arg. of periapsis
48.6385°
True anomaly
311.45587°
Mean anomaly
311.506°
Eccentric anomaly
311.48094°
Mean motion
3.74214 °/min
Orbital period
96.2 mins
BSTAR
0.0001713
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #23 in the year 2024 (2024-02-02 UTC)
Did you know?
You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.GEESAT 2-03 Visibility forecast
Loading observer location...
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 | 2026-06-22 11:02:38.423Z | 201.2° SSW | 2026-06-22 11:05:38.423Z | 139.296° SSE | 32.398° | 2026-06-22 11:08:38.423Z | 74.743° E |
| 6 mins | 2026-06-22 12:43:38.423Z | 273.782° WNW | 2026-06-22 12:45:38.423Z | 316.056° NNW | 32.762° | 2026-06-22 12:49:38.423Z | 44.016° NE |
| 4 mins | 2026-06-22 14:25:38.423Z | 322.725° NNW | 2026-06-22 14:27:38.423Z | 0.609° NNE | 19.81° | 2026-06-22 14:29:38.423Z | 34.816° NE |
| 5 mins | 2026-06-22 16:06:38.423Z | 331.587° NNW | 2026-06-22 16:08:38.423Z | 11.257° NNE | 24.312° | 2026-06-22 16:11:38.423Z | 67.667° E |
| 7 mins | 2026-06-22 17:46:38.423Z | 304.761° NW | 2026-06-22 17:49:38.423Z | 339.405° N | 44.97° | 2026-06-22 17:53:38.423Z | 124.777° SE |
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 descending order |
|---|
CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
Authenticating...
Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
|---|