Showing default

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.

Loading next visibility...
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 (2 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: 15 hours ago

TLE from 15 hours ago
0 ICEYE-X34
1 58294U 23174AQ  25289.13347863  .00032973  00000-0  86221-3 0  9992
2 58294  97.4096   8.8112 0006300 315.6102  44.4637 15.38667829107935
Epoch: 2025-10-16T03:12Z
TLE epoch observation values (Epoch: 2025-10-16T03:12:12.553Z)
Latitude
-0.00009°
Longitude
-64.13867°
Altitude
450.094 km
Speed
7.644 km/s
True Right ascension
00h 35m 14s
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
12:42:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
451.289 km
Perigee altitude
442.689 km
Semi-major axis
6,825.126 km
Eccentricity
0.00063
Inclination
97.4096°
RAAN
8.8112°
Arg. of periapsis
315.6102°
True anomaly
44.5143°
Mean anomaly
44.4637°
Eccentric anomaly
44.489°
Mean motion
3.84926 °/min
Orbital period
93.52 mins
BSTAR
0.00086221
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|