GEESAT 3-09, 61019
Orbit data source: Space-Track
GEESAT 3-09, 61019 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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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: 10 hours ago
TLE from 10 hours ago
0 GEESAT 3-09
1 61019U 24159J 26171.42427649 .00001565 00000-0 21171-3 0 9995
2 61019 49.9986 67.6853 0022204 71.9019 288.4336 14.84219565 97258Epoch: 2026-06-20T10:10Z
TLE epoch observation values (Epoch: 2026-06-20T10:10:57.488Z)
Latitude
-0.00001°
Longitude
6.30666°
Altitude
611.701 km
Speed
7.557 km/s
True Right ascension
04h 30m 44s
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
07:13:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
632.327 km
Perigee altitude
601.264 km
Semi-major axis
6,994.932 km
Eccentricity
0.00222
Inclination
49.9986°
RAAN
67.6853°
Arg. of periapsis
71.9019°
True anomaly
288.192°
Mean anomaly
288.4336°
Eccentric anomaly
288.31282°
Mean motion
3.70995 °/min
Orbital period
97.04 mins
BSTAR
0.00021171
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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 3-09 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 | 2026-06-20 21:45:30.436Z | 281.356° WNW | 2026-06-20 21:48:30.436Z | 333.661° NNW | 27.894° | 2026-06-20 21:52:30.436Z | 43.569° NE |
| 4 mins | 2026-06-20 23:29:30.436Z | 332.489° NNW | 2026-06-20 23:31:30.436Z | 10.459° NNE | 20.129° | 2026-06-20 23:33:30.436Z | 42.779° NE |
| 6 mins | 2026-06-21 01:10:30.436Z | 323.385° NNW | 2026-06-21 01:13:30.436Z | 28.44° NE | 30.609° | 2026-06-21 01:16:30.436Z | 84.166° E |
| 7 mins | 2026-06-21 02:51:30.436Z | 292.938° NW | 2026-06-21 02:54:30.436Z | 236.197° WSW | 38.533° | 2026-06-21 02:58:30.436Z | 145.2° SSE |
| 4 mins | 2026-06-21 18:40:30.436Z | 161.457° S | 2026-06-21 18:42:30.436Z | 123.001° SE | 20.494° | 2026-06-21 18:44:30.436Z | 90.832° ESE |
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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