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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.

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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: 8 hours ago

TLE from 8 hours ago
0 SCOT-1 (SCOT)
1 62617U 25009J   26126.48569809  .00049261  00000-0  88662-3 0  9999
2 62617  97.3846 213.1948 0003957 113.6806 246.4861 15.49666467 72888
Epoch: 2026-05-06T11:39Z
TLE epoch observation values (Epoch: 2026-05-06T11:39:24.314Z)
Latitude
-0.00004°
Longitude
173.99799°
Altitude
421.906 km
Speed
7.657 km/s
True Right ascension
14h 12m 46s
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
03:09:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
417.314 km
Perigee altitude
411.939 km
Semi-major axis
6,792.763 km
Eccentricity
0.0004
Inclination
97.3846°
RAAN
213.1948°
Arg. of periapsis
113.6806°
True anomaly
246.44453°
Mean anomaly
246.4861°
Eccentric anomaly
246.46531°
Mean motion
3.8768 °/min
Orbital period
92.86 mins
BSTAR
0.00088662
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