DECAYED
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ICEYE-X30, 56947 (Decayed)

Orbit data source: Space-Track

ICEYE-X30, 56947 was a payload satellite owned by ICEYE US (US) in LEO that was launched on Mon, 12 Jun 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
56947, 2023-084R
Orbit
Decayed
Country
Flag of USUS
Related business
Manufacturer
ICEYE
Mission
Decayed Commercial Radar Imaging
Bus & Motor
ICEYE, Unknown motor
Mass
90 kg wet, 89 kg dry
Launch date (UTC)
2023-06-12 (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: 2 months ago

TLE from 2 months ago
0 ICEYE-X30
1 56947U 23084R   26143.38323289  .14366460  26620-5  36953-3 0  9992
2 56947  97.5435 302.7258 0012790 274.1156  85.8683 16.44816394165060
Epoch: 2026-05-23T09:11Z
TLE epoch observation values (Epoch: 2026-05-23T09:11:51.321Z)
Latitude
-0.0001°
Longitude
-76.23854°
Altitude
155.683 km
Speed
7.813 km/s
True Right ascension
20h 10m 54s
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
03:05:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
158.179 km
Perigee altitude
141.48 km
Semi-major axis
6,527.966 km
Eccentricity
0.00128
Inclination
97.5435°
RAAN
302.7258°
Arg. of periapsis
274.1156°
True anomaly
86.0145°
Mean anomaly
85.8683°
Eccentric anomaly
85.9414°
Mean motion
4.11506 °/min
Orbital period
87.48 mins
BSTAR
0.00036953
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Computing Atmospheric mass density...

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