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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Identifier
Orbit
Country
KR / 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, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 CONTECSAT-1
1 59117U 24043V 26265.87294336 -.00000045 00000-0 10997-5 0 9990
2 59117 97.5788 49.7893 0005007 206.1301 153.9691 15.36012063142259Epoch: 2026-09-22T20:57Z
TLE epoch observation values (Epoch: 2026-09-22T20:57:02.306Z)
Latitude
0.00006°
Longitude
93.79751°
Altitude
464.1 km
Speed
7.633 km/s
True Right ascension
03h 19m 09s
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
20:14:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
458.289 km
Perigee altitude
451.447 km
Semi-major axis
6,833.005 km
Eccentricity
0.0005
Inclination
97.5788°
RAAN
49.7893°
Arg. of periapsis
206.1301°
True anomaly
153.99427°
Mean anomaly
153.9691°
Eccentric anomaly
153.98168°
Mean motion
3.8426 °/min
Orbital period
93.69 mins
BSTAR
0.0000010997
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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 | 2026-09-23 09:35:02.970Z | 157.052° SSE | 2026-09-23 09:38:02.970Z | 81.115° E | 65.608° | 2026-09-23 09:41:02.970Z | 354.933° N |
| 5 mins | 2026-09-23 22:32:02.970Z | 16.147° NNE | 2026-09-23 22:34:02.970Z | 37.827° NE | 66.386° | 2026-09-23 22:37:02.970Z | 188.351° SSW |
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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