GEESAT 3-04, 61014
Orbit data source: Space-Track
GEESAT 3-04, 61014 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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 GEESAT 3-04
1 61014U 24159D 26171.48069417 .00001647 00000-0 22639-3 0 9992
2 61014 49.9998 338.8457 0002708 94.3059 265.8189 14.83289482 98495Epoch: 2026-06-20T11:32Z
TLE epoch observation values (Epoch: 2026-06-20T11:32:11.976Z)
Latitude
0.00002°
Longitude
-102.89889°
Altitude
619.643 km
Speed
7.55 km/s
True Right ascension
22h 35m 22s
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
07:12:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
621.613 km
Perigee altitude
617.823 km
Semi-major axis
6,997.855 km
Eccentricity
0.00027
Inclination
49.9998°
RAAN
338.8457°
Arg. of periapsis
94.3059°
True anomaly
265.78795°
Mean anomaly
265.8189°
Eccentric anomaly
265.80343°
Mean motion
3.70762 °/min
Orbital period
97.1 mins
BSTAR
0.00022639
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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 3-04 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 21:46:57.866Z | 280.018° WNW | 2026-06-20 21:49:57.866Z | 236.86° WSW | 22.551° | 2026-06-20 21:53:57.866Z | 172.906° S |
| 7 mins | 2026-06-21 13:34:57.866Z | 209.492° SW | 2026-06-21 13:37:57.866Z | 150.312° SSE | 37.311° | 2026-06-21 13:41:57.866Z | 66.481° ENE |
| 6 mins | 2026-06-21 15:16:57.866Z | 277.691° WNW | 2026-06-21 15:19:57.866Z | 345.817° N | 31.816° | 2026-06-21 15:22:57.866Z | 40.746° NE |
| 5 mins | 2026-06-21 16:59:57.866Z | 321.286° NNW | 2026-06-21 17:01:57.866Z | 356.41° N | 20.927° | 2026-06-21 17:04:57.866Z | 44.36° NE |
| 6 mins | 2026-06-21 18:41:57.866Z | 328.12° NNW | 2026-06-21 18:43:57.866Z | 5.677° NNE | 27.243° | 2026-06-21 18:47:57.866Z | 78.983° 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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