GEESAT 3-10, 61020
Orbit data source: Space-Track
GEESAT 3-10, 61020 is a payload satellite owned by GeeSpace (CN) in LEO that was launched on Thu, 05 Sep 2024 UTC via a CHANG ZHENG 6 launch vehicle from the Taiyaun Space Center, China (TSC). 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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61020 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: 14 hours ago
TLE from 14 hours ago
0 GEESAT 3-10
1 61020U 24159K 26171.32696765 .00001462 00000-0 19971-3 0 9994
2 61020 50.0005 68.6669 0003751 117.4543 242.6777 14.84211637 96976Epoch: 2026-06-20T07:50Z
TLE epoch observation values (Epoch: 2026-06-20T07:50:50.004Z)
Latitude
-0.00007°
Longitude
42.41531°
Altitude
617.811 km
Speed
7.551 km/s
True Right ascension
04h 34m 40s
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
08:33:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
619.444 km
Perigee altitude
614.196 km
Semi-major axis
6,994.957 km
Eccentricity
0.00038
Inclination
50.0005°
RAAN
68.6669°
Arg. of periapsis
117.4543°
True anomaly
242.63952°
Mean anomaly
242.6777°
Eccentric anomaly
242.65861°
Mean motion
3.70993 °/min
Orbital period
97.04 mins
BSTAR
0.00019971
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Other satellites on launch #159 in the year 2024 (2024-09-05 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 3-10 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-20 22:42:24.590Z | 302.619° NW | 2026-06-20 22:45:24.590Z | 351.411° N | 22.047° | 2026-06-20 22:48:24.590Z | 40.302° NE |
| 6 mins | 2026-06-21 00:25:24.590Z | 328.092° NNW | 2026-06-21 00:27:24.590Z | 3.162° NNE | 23.44° | 2026-06-21 00:31:24.590Z | 68.811° E |
| 7 mins | 2026-06-21 02:06:24.590Z | 309.309° NW | 2026-06-21 02:09:24.590Z | 356.465° N | 42.821° | 2026-06-21 02:13:24.590Z | 115.619° SE |
| 5 mins | 2026-06-21 03:48:24.590Z | 266.24° W | 2026-06-21 03:50:24.590Z | 234.109° WSW | 19.653° | 2026-06-21 03:53:24.590Z | 185.674° SSW |
| 6 mins | 2026-06-21 19:35:24.590Z | 211.71° SW | 2026-06-21 19:38:24.590Z | 110.413° ESE | 39.165° | 2026-06-21 19:41:24.590Z | 64.707° ENE |
| 7 mins | 2026-06-21 21:16:24.590Z | 279.171° WNW | 2026-06-21 21:19:24.590Z | 337.522° N | 30.129° | 2026-06-21 21:23:24.590Z | 44.905° NE |
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 |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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