IRIS-F3, 62619
Orbit data source: Space-Track
IRIS-F3, 62619 is a payload satellite owned by NCKU (TW) 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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62619 intel report (Beta)
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Identifier
Orbit
Country
TW / TWNRelated business
Manufacturer
NCKU
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 IRIS-F3
1 62619U 25009L 26171.20064477 .00004897 00000-0 18717-3 0 9992
2 62619 97.4043 252.0177 0005223 323.0020 37.0858 15.27068574 79281Epoch: 2026-06-20T04:48Z
TLE epoch observation values (Epoch: 2026-06-20T04:48:55.708Z)
Latitude
-0.00002°
Longitude
-88.63309°
Altitude
484.822 km
Speed
7.624 km/s
True Right ascension
16h 48m 04s
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
07:24:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.12 km
Perigee altitude
477.954 km
Semi-major axis
6,859.674 km
Eccentricity
0.00052
Inclination
97.4043°
RAAN
252.0177°
Arg. of periapsis
323.002°
True anomaly
37.12191°
Mean anomaly
37.0858°
Eccentric anomaly
37.10385°
Mean motion
3.82022 °/min
Orbital period
94.24 mins
BSTAR
0.00018717
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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.IRIS-F3 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-21 04:33:25.137Z | 109.003° ESE | 2026-06-21 04:35:25.137Z | 73.312° E | 16.618° | 2026-06-21 04:37:25.137Z | 34.228° NE |
| 4 mins | 2026-06-21 06:07:25.137Z | 226.261° WSW | 2026-06-21 06:08:25.137Z | 250.249° W | 22.915° | 2026-06-21 06:11:25.137Z | 317.149° NNW |
| 4 mins | 2026-06-21 17:34:25.137Z | 57.303° ENE | 2026-06-21 17:36:25.137Z | 103.746° ESE | 20.886° | 2026-06-21 17:38:25.137Z | 142.95° SSE |
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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