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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62617 intel report (Beta)
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Identifier
Orbit
Country
SG / SINGRelated business
Manufacturer
OrbAstro
Mission
Operational Commercial Early Warn
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
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 & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 SCOT-1 (SCOT)
1 62617U 25009J 26215.76062330 .00085327 00000-0 10202-2 0 9993
2 62617 97.3830 305.3076 0004040 145.5211 214.6309 15.60710660 86758Epoch: 2026-08-03T18:15Z
TLE epoch observation values (Epoch: 2026-08-03T18:15:17.853Z)
Latitude
0.00001°
Longitude
79.14411°
Altitude
390.998 km
Speed
7.674 km/s
True Right ascension
20h 21m 13s
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
19:53:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
385.245 km
Perigee altitude
379.783 km
Semi-major axis
6,760.651 km
Eccentricity
0.0004
Inclination
97.383°
RAAN
305.3076°
Arg. of periapsis
145.5211°
True anomaly
214.6046°
Mean anomaly
214.6309°
Eccentric anomaly
214.61775°
Mean motion
3.90445 °/min
Orbital period
92.2 mins
BSTAR
0.0010202
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Other satellites on launch #9 in the year 2025 (2025-01-14 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.SCOT-1 (SCOT) 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 | 2026-08-05 18:30:36.868Z | 33.266° NE | 2026-08-05 18:32:36.868Z | 75.57° E | 27.179° | 2026-08-05 18:35:36.868Z | 163.745° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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