GEESAT 3-07, 61017
Orbit data source: Space-Track
GEESAT 3-07, 61017 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: 11 hours ago
TLE from 11 hours ago
0 GEESAT 3-07
1 61017U 24159G 26171.40163876 .00001515 00000-0 20606-3 0 9997
2 61017 49.9948 68.0449 0011335 44.1721 316.0121 14.84213617 96627Epoch: 2026-06-20T09:38Z
TLE epoch observation values (Epoch: 2026-06-20T09:38:21.588Z)
Latitude
-0.00002°
Longitude
14.83815°
Altitude
610.9 km
Speed
7.558 km/s
True Right ascension
04h 32m 10s
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
07:14:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
624.743 km
Perigee altitude
608.886 km
Semi-major axis
6,994.952 km
Eccentricity
0.00113
Inclination
49.9948°
RAAN
68.0449°
Arg. of periapsis
44.1721°
True anomaly
315.9218°
Mean anomaly
316.0121°
Eccentric anomaly
315.96696°
Mean motion
3.70993 °/min
Orbital period
97.04 mins
BSTAR
0.00020606
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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 3-07 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-20 21:10:38.655Z | 261.548° W | 2026-06-20 21:14:38.655Z | 342.152° N | 35.716° | 2026-06-20 21:18:38.655Z | 47.771° ENE |
| 5 mins | 2026-06-20 22:54:38.655Z | 318.448° NNW | 2026-06-20 22:56:38.655Z | 354.985° N | 21.263° | 2026-06-20 22:59:38.655Z | 42.542° NE |
| 6 mins | 2026-06-21 00:36:38.655Z | 329.609° NNW | 2026-06-21 00:38:38.655Z | 6.752° NNE | 24.865° | 2026-06-21 00:42:38.655Z | 73.528° E |
| 7 mins | 2026-06-21 02:17:38.655Z | 305.677° NW | 2026-06-21 02:20:38.655Z | 340.113° N | 44.736° | 2026-06-21 02:24:38.655Z | 123.144° SE |
| 7 mins | 2026-06-21 19:45:38.655Z | 224.443° SW | 2026-06-21 19:48:38.655Z | 176.916° S | 42.894° | 2026-06-21 19:52:38.655Z | 60.224° ENE |
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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