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: 9 hours ago
TLE from 9 hours ago
0 IRIS-F3
1 62619U 25009L 26126.17536746 .00005549 00000-0 21505-3 0 9995
2 62619 97.4041 207.3599 0008217 109.0100 251.2030 15.26527322 72417Epoch: 2026-05-06T04:12Z
TLE epoch observation values (Epoch: 2026-05-06T04:12:31.748Z)
Latitude
0.00001°
Longitude
-79.81202°
Altitude
491.124 km
Speed
7.618 km/s
True Right ascension
13h 49m 26s
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
21:22:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
488.798 km
Perigee altitude
477.522 km
Semi-major axis
6,861.297 km
Eccentricity
0.00082
Inclination
97.4041°
RAAN
207.3599°
Arg. of periapsis
109.01°
True anomaly
251.11389°
Mean anomaly
251.203°
Eccentric anomaly
251.15844°
Mean motion
3.81886 °/min
Orbital period
94.27 mins
BSTAR
0.00021505
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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 | 2026-05-06 18:56:13.618Z | 333.034° NNW | 2026-05-06 18:58:13.618Z | 284.449° WNW | 23.467° | 2026-05-06 19:00:13.618Z | 240.441° WSW |
| 5 mins | 2026-05-07 05:31:13.618Z | 173.879° S | 2026-05-07 05:33:13.618Z | 241.211° WSW | 44.343° | 2026-05-07 05:36:13.618Z | 344.542° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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