GEESAT 3-06, 61016
Orbit data source: Space-Track
GEESAT 3-06, 61016 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 3-06
1 61016U 24159F 26171.40930079 .00001561 00000-0 21143-3 0 9991
2 61016 49.9990 68.4061 0016507 89.2738 271.0092 14.84216769 97248Epoch: 2026-06-20T09:49Z
TLE epoch observation values (Epoch: 2026-06-20T09:49:23.588Z)
Latitude
-0°
Longitude
12.43348°
Altitude
616.405 km
Speed
7.552 km/s
True Right ascension
04h 33m 37s
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
07:14:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
628.351 km
Perigee altitude
605.257 km
Semi-major axis
6,994.941 km
Eccentricity
0.00165
Inclination
49.999°
RAAN
68.4061°
Arg. of periapsis
89.2738°
True anomaly
270.82007°
Mean anomaly
271.0092°
Eccentric anomaly
270.91463°
Mean motion
3.70994 °/min
Orbital period
97.04 mins
BSTAR
0.00021143
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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 3-06 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 21:22:07.389Z | 266.114° W | 2026-06-20 21:26:07.389Z | 341.507° N | 33.289° | 2026-06-20 21:30:07.389Z | 46.797° ENE |
| 5 mins | 2026-06-20 23:06:07.389Z | 319.704° NNW | 2026-06-20 23:08:07.389Z | 355.246° N | 20.73° | 2026-06-20 23:11:07.389Z | 43.33° NE |
| 6 mins | 2026-06-21 00:48:07.389Z | 329.066° NNW | 2026-06-21 00:50:07.389Z | 6.816° NNE | 25.909° | 2026-06-21 00:54:07.389Z | 76.782° E |
| 7 mins | 2026-06-21 02:29:07.389Z | 302.026° NW | 2026-06-21 02:32:07.389Z | 247.554° W | 44.663° | 2026-06-21 02:36:07.389Z | 129.101° SE |
| 7 mins | 2026-06-21 19:57:07.389Z | 231.282° WSW | 2026-06-21 20:00:07.389Z | 207.042° SW | 44.252° | 2026-06-21 20:04:07.389Z | 57.194° 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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