ICEYE-X7, 46496
Orbit data source: Space-Track
ICEYE-X7, 46496 is a payload satellite owned by ICEYE (FI) in SSO that was launched on Mon, 28 Sep 2020 UTC via a SOYUZ-2-1B launch vehicle from the Plesetsk Missile And Space Complex (PKMTR). 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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46496 intel report (Beta)
ICEYE-X7 details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 6 hours ago |
| Origin | |
| Manufacturer | ICEYE |
| Mission | Operational Commercial Radar Imaging |
| Bus & Motor | ICEYE, Unknown motor |
| Mass | 80 kg wet, 80 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 | 1.837 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 6 hours ago
0 ICEYE-X7
1 46496U 20068L 24361.28794701 .00017070 00000-0 89308-3 0 9995
2 46496 97.6907 300.9964 0012746 49.6747 310.5597 15.15846231232864Epoch: 2024-12-26T06:54Z
Definitive object data (Epoch: 2024-12-26T06:54:38.621Z)
| Latitude | 0.00002° |
| Longitude | 102.06598° |
| Altitude | 515.776 km |
| Speed | 7.609 km/s |
| True Right ascension | 20h 03m 59s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -65.26716° |
| Longitude | 119.27183° |
| Altitude | 546.954 km |
| Speed | 7.585 km/s |
| Apparent Right ascension | 23h 10m 57s |
| Apparent Declination | -55° 05' 58" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 12:18:57 |
| Azimuth | 148.962° SSE |
| Elevation | -71.071° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 524.181 km |
| Perigee altitude | 506.608 km |
| Semi-major axis | 6,893.531 km |
| Eccentricity | 0.0012746 |
| Inclination | 97.6907° |
| RAAN | 300.9964° |
| Arg. of periapsis | 49.6747° |
| True anomaly | 310.44862° |
| Mean anomaly | 310.5597° |
| Eccentric anomaly | 310.50417° |
| Mean motion | 3.79211 °/min |
| BSTAR | 0.00089308 |
| Orbital period | 94.93 mins |
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Other satellites on launch #68 in the year 2020 (2020-09-28 UTC)
ICEYE-X7 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2024-12-26 19:43:21.304Z | 132.944° SE | 2024-12-26 19:46:21.304Z | 63.005° ENE | 28.884° | 2024-12-26 19:49:21.304Z | 7.488° NNE |
| 5 mins | 2024-12-27 08:50:21.304Z | 31.352° NE | 2024-12-27 08:52:21.304Z | 92.132° ESE | 38.442° | 2024-12-27 08:55:21.304Z | 174.559° S |
Authenticating...
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