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, 0.2 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 26310.16773407 .00005875 00000-0 21295-3 0 9994
2 62619 97.3964 30.0031 0006244 165.8728 194.2688 15.28732280100506Epoch: 2026-11-06T04:01Z
TLE epoch observation values (Epoch: 2026-11-06T04:01:32.223Z)
Latitude
-0°
Longitude
-75.77239°
Altitude
486.854 km
Speed
7.619 km/s
True Right ascension
02h 00m 00s
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
16:31:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
480.835 km
Perigee altitude
472.275 km
Semi-major axis
6,854.692 km
Eccentricity
0.00062
Inclination
97.3964°
RAAN
30.0031°
Arg. of periapsis
165.8728°
True anomaly
194.25118°
Mean anomaly
194.2688°
Eccentric anomaly
194.25999°
Mean motion
3.82438 °/min
Orbital period
94.13 mins
BSTAR
0.00021295
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-11-07 05:16:52.944Z | 153.846° SSE | 2026-11-07 05:19:52.944Z | 107.462° ESE | 52.236° | 2026-11-07 05:22:52.944Z | 0.368° NNE |
| 5 mins | 2026-11-07 18:17:52.944Z | 15.558° NNE | 2026-11-07 18:19:52.944Z | 35.301° NE | 67.413° | 2026-11-07 18:22:52.944Z | 188.557° SSW |
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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