CONTECSAT-1, 59117
Orbit data source: Space-Track
CONTECSAT-1, 59117 is a payload satellite owned by CONTEC (KR) in SSO that was launched on Mon, 04 Mar 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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59117 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / SKORRelated business
Manufacturer
CONTEC
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 CONTECSAT-1
1 59117U 24043V 25359.73063554 .00012415 00000-0 39683-3 0 9998
2 59117 97.5409 131.6385 0012332 129.4478 230.7857 15.32517654100644Epoch: 2025-12-25T17:32Z
TLE epoch observation values (Epoch: 2025-12-25T17:32:06.910Z)
Latitude
-0.00001°
Longitude
134.12823°
Altitude
476.752 km
Speed
7.624 km/s
True Right ascension
08h 46m 33s
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
22:08:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
473.698 km
Perigee altitude
456.819 km
Semi-major axis
6,843.396 km
Eccentricity
0.00123
Inclination
97.5409°
RAAN
131.6385°
Arg. of periapsis
129.4478°
True anomaly
230.67632°
Mean anomaly
230.7857°
Eccentric anomaly
230.731°
Mean motion
3.83386 °/min
Orbital period
93.9 mins
BSTAR
0.00039683
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Other satellites on launch #43 in the year 2024 (2024-03-04 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.CONTECSAT-1 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-26 09:20:19.841Z | 191.426° SSW | 2025-12-26 09:22:19.841Z | 240.029° WSW | 35.208° | 2025-12-26 09:25:19.841Z | 331.724° NNW |
| 5 mins | 2025-12-26 22:18:19.841Z | 347.72° N | 2025-12-26 22:20:19.841Z | 298.898° NW | 30.569° | 2025-12-26 22:23:19.841Z | 221.609° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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