DECAYED
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IRIS-F1, 59110 (Decayed)

Orbit data source: Space-Track

IRIS-F1, 59110 was a Taiwanese payload satellite in LEO that was launched on Mon, 04 Mar 2024 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.

Not visible in the next 10 days
Identifier
59110, 2024-043N
Orbit
Decayed
Country
Flag of TWTW / TWN
Related business
Manufacturer
Satoro
Mission
Decayed Amateur Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
2024-03-04 (2 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 9 months ago

TLE from 9 months ago
0 IRIS-F1
1 59110U 24043N   25322.52934150  .10443978  25836-5  10229-2 0  9993
2 59110  97.4892 105.7479 0010883 276.8555  83.1505 16.38182243 95811
Epoch: 2025-11-18T12:42Z
TLE epoch observation values (Epoch: 2025-11-18T12:42:15.105Z)
Latitude
-0.00002°
Longitude
-142.62915°
Altitude
173.046 km
Speed
7.803 km/s
True Right ascension
07h 02m 59s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
15:53:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
174.58 km
Perigee altitude
160.333 km
Semi-major axis
6,545.593 km
Eccentricity
0.00109
Inclination
97.4892°
RAAN
105.7479°
Arg. of periapsis
276.8555°
True anomaly
83.27434°
Mean anomaly
83.1505°
Eccentric anomaly
83.21242°
Mean motion
4.09845 °/min
Orbital period
87.84 mins
BSTAR
0.0010229
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Computing Atmospheric mass density...

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