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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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Iframe embed code

<iframe src="https://www.satcat.com/sats-embedded/62617?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/62617?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

62617, 2025-009J

Orbit

SSO

Country

SG / 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 (2 years 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: 14 hours ago

TLE from 14 hours ago

0 SCOT-1 (SCOT)
1 62617U 25009J   26262.00619988  .00105573  00000-0  90856-3 0  9999
2 62617  97.3783 353.6889 0003031 266.0916  94.0000 15.68978107 93984

Epoch: 2026-09-19T00:08Z

TLE epoch observation values (Epoch: 2026-09-19T00:08:55.669Z)

Latitude

0.00005°

Longitude

-6.46399°

Altitude

365.122 km

Speed

7.69 km/s

True Right ascension

23h 34m 45s

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

06:37:34

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

360.764 km

Perigee altitude

356.68 km

Semi-major axis

6,736.859 km

Eccentricity

0.0003

Inclination

97.3783°

RAAN

353.6889°

Arg. of periapsis

266.0916°

True anomaly

94.03465°

Mean anomaly

94°

Eccentric anomaly

94.01732°

Mean motion

3.92516 °/min

Orbital period

91.72 mins

BSTAR

0.00090856

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Other satellites on launch #9 in the year 2025 (2025-01-14 UTC)

FLOCK 4G 7, 62624

OBJECT CN, 62693 (Decayed)

PAUSAT-1, 62653

OBJECT DM, 63002 (Decayed)

PIONEER-02, 62662 (Decayed)

FLOCK 4G 27, 62641

HYPE, 62687 (Decayed)

HYDRA-T, 62692 (Decayed)

OBJECT DP, 63004 (Decayed)

OBJECT BR, 62672

OBJECT F, 62614 (Decayed)

Did you know?

You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.

Click here to try in Sandbox

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	2026-09-19 19:04:07.602Z	13.687° NNE	2026-09-19 19:06:07.602Z	22.347° NNE	57.452°	2026-09-19 19:09:07.602Z	190.407° SSW

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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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Check out SCOT-1 (SCOT), 62617 on other resources

View SCOT-1 (SCOT), 62617 on NASA - NSSDCA Website

View SCOT-1 (SCOT), 62617 on Heavens-Above

View SCOT-1 (SCOT), 62617 on Keep Track

View SCOT-1 (SCOT), 62617 on Celestrak

View SCOT-1 (SCOT), 62617 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

Documentation

Go to standalone docs website

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