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: 11 hours ago
TLE from 11 hours ago
0 IRIS-F3
1 62619U 25009L 26079.95030511 .00015520 00000-0 61448-3 0 9997
2 62619 97.4077 161.5505 0005090 268.0870 91.9786 15.25509796 65367Epoch: 2026-03-20T22:48Z
TLE epoch observation values (Epoch: 2026-03-20T22:48:26.361Z)
Latitude
0.00006°
Longitude
0.96264°
Altitude
492.475 km
Speed
7.619 km/s
True Right ascension
10h 46m 12s
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
14:15:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
489.708 km
Perigee altitude
482.72 km
Semi-major axis
6,864.351 km
Eccentricity
0.00051
Inclination
97.4077°
RAAN
161.5505°
Arg. of periapsis
268.087°
True anomaly
92.03689°
Mean anomaly
91.9786°
Eccentric anomaly
92.00775°
Mean motion
3.81631 °/min
Orbital period
94.33 mins
BSTAR
0.00061448
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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 | 2026-03-21 18:15:38.746Z | 11.319° NNE | 2026-03-21 18:18:38.746Z | 211.858° SW | 44.806° | 2026-03-21 18:21:38.746Z | 193.821° SSW |
| 4 mins | 2026-03-22 04:52:38.746Z | 112.854° SE | 2026-03-22 04:53:38.746Z | 86.36° E | 26.427° | 2026-03-22 04:56:38.746Z | 14.625° 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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