Showing default

SCOT-1 (SCOT), 62617

Orbit data source: Space-Track

SCOT-1 (SCOT), 62617 is a Singaporean payload satellite in SSO that was launched on Tue, 14 Jan 2025 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
62617, 2025-009J
Orbit
SSO
Country
Flag of SGSG / SING
Related business
Manufacturer
OrbAstro
Mission
Operational Commercial Early Warn
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
2025-01-14 (1 year ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 19 hours ago

TLE from 19 hours ago
0 SCOT-1 (SCOT)
1 62617U 25009J   26171.23433100  .00054191  00000-0  82117-3 0  9993
2 62617  97.3857 259.1799 0003386 259.7913 100.2959 15.54469278 79824
Epoch: 2026-06-20T05:37Z
TLE epoch observation values (Epoch: 2026-06-20T05:37:26.198Z)
Latitude
-0.00002°
Longitude
-93.63114°
Altitude
407.245 km
Speed
7.666 km/s
True Right ascension
17h 16m 43s
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
11:43:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
402.91 km
Perigee altitude
398.32 km
Semi-major axis
6,778.752 km
Eccentricity
0.00034
Inclination
97.3857°
RAAN
259.1799°
Arg. of periapsis
259.7913°
True anomaly
100.33407°
Mean anomaly
100.2959°
Eccentric anomaly
100.31499°
Mean motion
3.88883 °/min
Orbital period
92.57 mins
BSTAR
0.00082117
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
|