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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Edit Public Description
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
0.800 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 IRIS-F3
1 62619U 25009L 25286.48826048 .00013440 00000-0 59892-3 0 9991
2 62619 97.4272 4.9669 0008369 108.8297 251.3848 15.21519228 41240Epoch: 2025-10-13T11:43Z
TLE epoch observation values (Epoch: 2025-10-13T11:43:05.705Z)
Latitude
0.00005°
Longitude
166.9028°
Altitude
506.192 km
Speed
7.61 km/s
True Right ascension
00h 19m 52s
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
18:50:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.977 km
Perigee altitude
492.467 km
Semi-major axis
6,876.359 km
Eccentricity
0.00084
Inclination
97.4272°
RAAN
4.9669°
Arg. of periapsis
108.8297°
True anomaly
251.29395°
Mean anomaly
251.3848°
Eccentric anomaly
251.33937°
Mean motion
3.80632 °/min
Orbital period
94.58 mins
BSTAR
0.00059892
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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 | 2025-10-14 05:12:55.454Z | 154.082° SSE | 2025-10-14 05:15:55.454Z | 38.015° NE | 40.347° | 2025-10-14 05:18:55.454Z | 354.971° N |
| 5 mins | 2025-10-14 18:16:55.454Z | 8.834° NNE | 2025-10-14 18:18:55.454Z | 328.275° NNW | 44.501° | 2025-10-14 18:21:55.454Z | 196.224° SSW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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