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ICEYE-X34, 58294

Orbit data source: Space-Track

ICEYE-X34, 58294 is a payload satellite owned by ICEYE US (US) in SSO that was launched on Sat, 11 Nov 2023 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
58294, 2023-174AQ
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
ICEYE
Mission
Operational Commercial Radar Imaging
Bus & Motor
ICEYE, Unknown motor
Mass
90 kg wet, 89 kg dry
Launch date (UTC)
2023-11-11 (3 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 1 Pan, 1.6 m
Radar Cross Section
0.825 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 ICEYE-X34
1 58294U 23174AQ  26234.24534437  .00360111  00000-0  13913-2 0  9995
2 58294  97.3806 329.4827 0006640 240.9168 119.1438 15.86345946156138
Epoch: 2026-08-22T05:53Z
TLE epoch observation values (Epoch: 2026-08-22T05:53:17.753Z)
Latitude
-0.00007°
Longitude
-89.39978°
Altitude
317.884 km
Speed
7.716 km/s
True Right ascension
21h 57m 55s
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
09:34:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
313.855 km
Perigee altitude
304.974 km
Semi-major axis
6,687.551 km
Eccentricity
0.00066
Inclination
97.3806°
RAAN
329.4827°
Arg. of periapsis
240.9168°
True anomaly
119.21023°
Mean anomaly
119.1438°
Eccentric anomaly
119.17702°
Mean motion
3.96865 °/min
Orbital period
90.71 mins
BSTAR
0.0013913
Loading maneuver chart data...
Computing Atmospheric mass density...

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