Showing default

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.

Loading next visibility...
Identifier
59117, 2024-043V
Orbit
SSO
Country
Flag of UnknownUnknown / SKOR
Related business
Manufacturer
CONTEC
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
2024-03-04 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 18 hours ago

TLE from 18 hours ago
0 CONTECSAT-1
1 59117U 24043V   25260.26056760  .00008939  00000-0  31360-3 0  9998
2 59117  97.5310  30.5648 0013254 123.1994 237.0519 15.29588110 85426
Epoch: 2025-09-17T06:15Z
TLE epoch observation values (Epoch: 2025-09-17T06:15:13.04Z)
Latitude
-0.00002°
Longitude
-59.6786°
Altitude
485.094 km
Speed
7.62 km/s
True Right ascension
02h 02m 15s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
16:38:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
483.083 km
Perigee altitude
464.919 km
Semi-major axis
6,852.138 km
Eccentricity
0.00133
Inclination
97.531°
RAAN
30.5648°
Arg. of periapsis
123.1994°
True anomaly
236.92456°
Mean anomaly
237.0519°
Eccentric anomaly
236.98822°
Mean motion
3.82652 °/min
Orbital period
94.08 mins
BSTAR
0.0003136
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|