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: 9 hours ago
TLE from 9 hours ago
0 CONTECSAT-1
1 59117U 24043V 25299.49645731 .00012016 00000-0 40554-3 0 9993
2 59117 97.5376 70.3609 0011484 351.7088 8.3961 15.30786265 91423Epoch: 2025-10-26T11:54Z
TLE epoch observation values (Epoch: 2025-10-26T11:54:53.911Z)
Latitude
-0.00003°
Longitude
-143.47554°
Altitude
468.781 km
Speed
7.636 km/s
True Right ascension
04h 41m 26s
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
16:02:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
478.287 km
Perigee altitude
462.557 km
Semi-major axis
6,848.559 km
Eccentricity
0.00115
Inclination
97.5376°
RAAN
70.3609°
Arg. of periapsis
351.7088°
True anomaly
8.41534°
Mean anomaly
8.3961°
Eccentric anomaly
8.40572°
Mean motion
3.82952 °/min
Orbital period
94.01 mins
BSTAR
0.00040554
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-26 21:53:25.447Z | 4.05° NNE | 2025-10-26 21:56:25.447Z | 243.736° WSW | 40.969° | 2025-10-26 21:59:25.447Z | 202.023° SSW |
| 5 mins | 2025-10-27 08:27:25.447Z | 129.841° SE | 2025-10-27 08:29:25.447Z | 72.528° E | 30.71° | 2025-10-27 08:32:25.447Z | 6.554° NNE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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