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: 10 hours ago
TLE from 10 hours ago
0 IRIS-F3
1 62619U 25009L 25335.20911265 .00006488 00000-0 28511-3 0 9990
2 62619 97.4245 53.0571 0005367 309.2438 50.8321 15.22234395 48656Epoch: 2025-12-01T05:01Z
TLE epoch observation values (Epoch: 2025-12-01T05:01:07.332Z)
Latitude
-0.0001°
Longitude
-92.53534°
Altitude
499.865 km
Speed
7.616 km/s
True Right ascension
03h 32m 13s
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
12:51:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
499.756 km
Perigee altitude
492.377 km
Semi-major axis
6,874.203 km
Eccentricity
0.00054
Inclination
97.4245°
RAAN
53.0571°
Arg. of periapsis
309.2438°
True anomaly
50.8798°
Mean anomaly
50.8321°
Eccentric anomaly
50.85595°
Mean motion
3.80811 °/min
Orbital period
94.54 mins
BSTAR
0.00028511
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Other satellites on launch #9 in the year 2025 (2025-01-14 UTC)
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.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 | 2025-12-01 18:12:24.590Z | 13.212° NNE | 2025-12-01 18:15:24.590Z | 180.022° SSW | 43.921° | 2025-12-01 18:18:24.590Z | 191.677° SSW |
| 4 mins | 2025-12-02 04:50:24.590Z | 115.658° SE | 2025-12-02 04:52:24.590Z | 58.711° ENE | 26.408° | 2025-12-02 04:54:24.590Z | 17.012° NNE |
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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