EAGLESAT 1, 43018
Orbit data source: Space-Track
EAGLESAT 1, 43018 is a payload satellite owned by Embry-Riddle (US) in SSO that was launched on Sat, 18 Nov 2017 UTC via a DELTA 7920-10C 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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43018 intel report (Beta)
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EAGLESAT 1 radio frequencies
EAGLESAT 1 details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 8 hours ago |
| Origin | |
| Manufacturer | Embry-Riddle |
| Mission | Non-operational Amateur Technology |
| Bus & Motor | CUBESAT 1U, Unknown motor |
| Mass | 1 kg wet, 1 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box, 0.1 m |
| Radar Cross Section | 0.015 m², Small (<0.1 m²) |
Expand to show TLE details & history
TLE from 8 hours ago
0 EAGLESAT 1
1 43018U 17073F 24356.92555213 .00056862 00000-0 18708-2 0 9999
2 43018 97.5657 240.7153 0132796 339.0807 20.5025 15.23148042384499Epoch: 2024-12-21T22:12Z
Definitive object data (Epoch: 2024-12-21T22:12:47.704Z)
| Latitude | 0.00004° |
| Longitude | 176.54681° |
| Altitude | 414.068 km |
| Speed | 7.71 km/s |
| True Right ascension | 16h 02m 51s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 30.72551° |
| Longitude | 172.3809° |
| Altitude | 444.628 km |
| Speed | 7.679 km/s |
| Apparent Right ascension | 16h 28m 06s |
| Apparent Declination | -3° 16' 31" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 05:18:26 |
| Azimuth | 20.514° NNE |
| Elevation | -51.628° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 584.57 km |
| Perigee altitude | 402.07 km |
| Semi-major axis | 6,871.457 km |
| Eccentricity | 0.0132796 |
| Inclination | 97.5657° |
| RAAN | 240.7153° |
| Arg. of periapsis | 339.0807° |
| True anomaly | 21.04389° |
| Mean anomaly | 20.5025° |
| Eccentric anomaly | 20.77235° |
| Mean motion | 3.81039 °/min |
| BSTAR | 0.0018708 |
| Orbital period | 94.48 mins |
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Other satellites on launch #73 in the year 2017 (2017-11-18 UTC)
| NOAA 20, 43013 |
| BUCCANEER RMM, 43014 (Decayed) |
| MIRATA, 43015 |
| MAKERSAT 0, 43016 |
| AO-91, 43017 |
| EAGLESAT 1, 43018 |
EAGLESAT 1 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 | 2024-12-23 04:44:43.544Z | 44.388° NE | 2024-12-23 04:46:43.544Z | 83.613° E | 26.849° | 2024-12-23 04:50:43.544Z | 159.238° S |
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