ICEYE-X30, 56947
Orbit data source: Space-Track
ICEYE-X30, 56947 is a payload satellite owned by ICEYE US (US) in SSO 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.
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56947 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
ICEYE
Mission
Operational Commercial Radar Imaging
Bus & Motor
ICEYE, Unknown motor
Mass
90 kg wet, 89 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
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 & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 ICEYE-X30
1 56947U 23084R 25334.35635826 .00063912 00000-0 92830-3 0 9999
2 56947 97.5754 113.4961 0005028 316.3178 43.7677 15.55582294137707Epoch: 2025-11-30T08:33Z
TLE epoch observation values (Epoch: 2025-11-30T08:33:09.353Z)
Latitude
-0.00007°
Longitude
-84.26425°
Altitude
401.133 km
Speed
7.671 km/s
True Right ascension
07h 33m 59s
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
01:19:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
400.793 km
Perigee altitude
393.98 km
Semi-major axis
6,775.524 km
Eccentricity
0.0005
Inclination
97.5754°
RAAN
113.4961°
Arg. of periapsis
316.3178°
True anomaly
43.80757°
Mean anomaly
43.7677°
Eccentric anomaly
43.78763°
Mean motion
3.89161 °/min
Orbital period
92.51 mins
BSTAR
0.0009283
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Other satellites on launch #84 in the year 2023 (2023-06-12 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.ICEYE-X30 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-01 09:23:19.459Z | 159.129° S | 2025-12-01 09:25:19.459Z | 120.018° SE | 42.374° | 2025-12-01 09:28:19.459Z | 352.654° N |
| 4 mins | 2025-12-01 22:10:19.459Z | 25.854° NE | 2025-12-01 22:12:19.459Z | 118.445° SE | 40.501° | 2025-12-01 22:14:19.459Z | 178.346° S |
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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