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, 0.1 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 CONTECSAT-1
1 59117U 24043V 26175.31825037 .00008882 00000-0 24945-3 0 9999
2 59117 97.5647 316.5374 0009820 202.4169 157.6647 15.36739412128340Epoch: 2026-06-24T07:38Z
TLE epoch observation values (Epoch: 2026-06-24T07:38:16.831Z)
Latitude
-0.00005°
Longitude
-70.50991°
Altitude
465.077 km
Speed
7.63 km/s
True Right ascension
21h 06m 08s
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
06:50:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
459.417 km
Perigee altitude
446.001 km
Semi-major axis
6,830.846 km
Eccentricity
0.00098
Inclination
97.5647°
RAAN
316.5374°
Arg. of periapsis
202.4169°
True anomaly
157.70742°
Mean anomaly
157.6647°
Eccentric anomaly
157.68606°
Mean motion
3.84443 °/min
Orbital period
93.64 mins
BSTAR
0.00024945
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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 | 2026-06-24 22:16:09.981Z | 15.885° NNE | 2026-06-24 22:18:09.981Z | 35.178° NE | 42.154° | 2026-06-24 22:21:09.981Z | 188.521° SSW |
| 4 mins | 2026-06-25 08:48:09.981Z | 105.887° ESE | 2026-06-25 08:49:09.981Z | 82.517° E | 21.061° | 2026-06-25 08:52:09.981Z | 18.58° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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