GEESAT 3-02, 61012
Orbit data source: Space-Track
GEESAT 3-02, 61012 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 3-02
1 61012U 24159B 26171.43204016 .00001546 00000-0 20959-3 0 9992
2 61012 49.9952 68.2691 0018962 68.0978 292.1974 14.84216354 97273Epoch: 2026-06-20T10:22Z
TLE epoch observation values (Epoch: 2026-06-20T10:22:08.269Z)
Latitude
-0.00006°
Longitude
4.08784°
Altitude
611.602 km
Speed
7.557 km/s
True Right ascension
04h 33m 04s
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
07:15:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
630.07 km
Perigee altitude
603.542 km
Semi-major axis
6,994.943 km
Eccentricity
0.0019
Inclination
49.9952°
RAAN
68.2691°
Arg. of periapsis
68.0978°
True anomaly
291.99604°
Mean anomaly
292.1974°
Eccentric anomaly
292.09674°
Mean motion
3.70994 °/min
Orbital period
97.04 mins
BSTAR
0.00020959
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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 3-02 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 21:58:01.025Z | 293.905° NW | 2026-06-20 22:00:01.025Z | 332.264° NNW | 26.274° | 2026-06-20 22:04:01.025Z | 42.601° NE |
| 5 mins | 2026-06-20 23:41:01.025Z | 331.522° NNW | 2026-06-20 23:43:01.025Z | 8.891° NNE | 20.549° | 2026-06-20 23:46:01.025Z | 53.498° ENE |
| 7 mins | 2026-06-21 01:22:01.025Z | 321.163° NNW | 2026-06-21 01:25:01.025Z | 26.088° NE | 32.79° | 2026-06-21 01:29:01.025Z | 93.835° ESE |
| 6 mins | 2026-06-21 03:04:01.025Z | 282.167° WNW | 2026-06-21 03:06:01.025Z | 235.982° WSW | 35.207° | 2026-06-21 03:10:01.025Z | 151.2° SSE |
| 6 mins | 2026-06-21 18:51:01.025Z | 180.065° SSW | 2026-06-21 18:54:01.025Z | 123.089° SE | 23.472° | 2026-06-21 18:57:01.025Z | 78.863° E |
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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