ICEYE-X26, 56961
Orbit data source: Space-Track
ICEYE-X26, 56961 is 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). Payloads include a variety of satellites, spacecraft, and rockets 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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56961 intel report (Beta)
ICEYE-X26 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 1 day ago |
| Origin | |
| 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 | Payload Rocket body Debris |
| Shape & HBR | Box + 1 Pan, 3.25 m |
| Radar Cross Section | 0.825 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 1 day ago
0 ICEYE-X26
1 56961U 23084AF 24337.59545583 .00041194 00000-0 13415-2 0 9992
2 56961 97.5491 98.5028 0002352 151.8297 208.3072 15.31724881 81866Epoch: 2024-12-02T14:17Z
Definitive object data (Epoch: 2024-12-02T14:17:27.383Z)
| Latitude | -0.00001° |
| Longitude | 172.22165° |
| Altitude | 475.187 km |
| Speed | 7.627 km/s |
| True Right ascension | 06h 34m 00s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | -43.002° |
| Longitude | -179.5952° |
| Altitude | 488.596 km |
| Speed | 7.618 km/s |
| Apparent Right ascension | 04h 53m 48s |
| Apparent Declination | -46° 36' 11" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 14:36:51 |
| Azimuth | 243.487° WSW |
| Elevation | -64.406° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 469.232 km |
| Perigee altitude | 466.012 km |
| Semi-major axis | 6,845.759 km |
| Eccentricity | 0.0002352 |
| Inclination | 97.5491° |
| RAAN | 98.5028° |
| Arg. of periapsis | 151.8297° |
| True anomaly | 208.29442° |
| Mean anomaly | 208.3072° |
| Eccentric anomaly | 208.30081° |
| Mean motion | 3.83187 °/min |
| BSTAR | 0.0013415 |
| Orbital period | 93.95 mins |
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Other satellites on launch #84 in the year 2023 (2023-06-12 UTC)
ICEYE-X26 Visibility forecast
Observer location: undefined°, undefined
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 | 2024-12-03 20:39:18.731Z | 42.071° NE | 2024-12-03 20:41:18.731Z | 90.651° ESE | 27.596° | 2024-12-03 20:44:18.731Z | 160.037° S |
| 4 mins | 2024-12-04 08:46:18.731Z | 216.95° SW | 2024-12-04 08:47:18.731Z | 250.619° W | 30.836° | 2024-12-04 08:50:18.731Z | 327.269° NNW |
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