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). Payloads include a variety of satellites, spacecraft, and rockets 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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CONTECSAT-1 radio frequencies
CONTECSAT-1 details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 8 hours ago |
| Origin | |
| 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 | Payload Rocket body Debris |
| Shape & HBR | Box, 0.3 m |
| Radar Cross Section | 0.080 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 8 hours ago
0 CONTECSAT-1
1 59117U 24043V 25015.07175518 .00010877 00000-0 45362-3 0 9999
2 59117 97.5007 143.6592 0012425 269.8366 90.1448 15.23796074 48009Epoch: 2025-01-15T01:43Z
Definitive object data (Epoch: 2025-01-15T01:43:19.647Z)
| Latitude | 0.00006° |
| Longitude | 3.05797° |
| Altitude | 497.528 km |
| Speed | 7.616 km/s |
| True Right ascension | 09h 34m 38s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | 8.10416° |
| Longitude | 2.31942° |
| Altitude | 498.194 km |
| Speed | 7.615 km/s |
| Apparent Right ascension | 07h 47m 04s |
| Apparent Declination | -54° 13' 31" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 10:18:10 |
| Azimuth | 201.294° SSW |
| Elevation | -9.566° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 499.903 km |
| Perigee altitude | 482.832 km |
| Semi-major axis | 6,869.505 km |
| Eccentricity | 0.0012425 |
| Inclination | 97.5007° |
| RAAN | 143.6592° |
| Arg. of periapsis | 269.8366° |
| True anomaly | 90.28718° |
| Mean anomaly | 90.1448° |
| Eccentric anomaly | 90.21599° |
| Mean motion | 3.81202 °/min |
| BSTAR | 0.00045362 |
| Orbital period | 94.44 mins |
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Other satellites on launch #43 in the year 2024 (2024-03-04 UTC)
CONTECSAT-1 Visibility forecast
Observer location: undefined°, undefined
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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-01-15 21:11:15.999Z | 15.971° NNE | 2025-01-15 21:15:15.999Z | 154.421° SSE | 41.925° | 2025-01-15 21:18:15.999Z | 186.846° SSW |
| 4 mins | 2025-01-16 07:49:15.999Z | 114.388° SE | 2025-01-16 07:51:15.999Z | 65.875° ENE | 23.963° | 2025-01-16 07:53:15.999Z | 22.626° NE |
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