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). 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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43018 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
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
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.015 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 EAGLESAT 1
1 43018U 17073F 25301.25785051 .00489658 87004-4 21091-2 0 9996
2 43018 97.5085 202.7658 0026398 294.5472 65.3046 15.84413384432399Epoch: 2025-10-28T06:11Z
TLE epoch observation values (Epoch: 2025-10-28T06:11:18.284Z)
Latitude
-0.00002°
Longitude
73.09169°
Altitude
313.803 km
Speed
7.724 km/s
True Right ascension
13h 31m 03s
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
09:00:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
332.53 km
Perigee altitude
297.194 km
Semi-major axis
6,692.999 km
Eccentricity
0.00264
Inclination
97.5085°
RAAN
202.7658°
Arg. of periapsis
294.5472°
True anomaly
65.57981°
Mean anomaly
65.3046°
Eccentric anomaly
65.44217°
Mean motion
3.9638 °/min
Orbital period
90.82 mins
BSTAR
0.0021091
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Other satellites on launch #73 in the year 2017 (2017-11-18 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.EAGLESAT 1 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-29 17:10:29.336Z | 132.072° SE | 2025-10-29 17:12:29.336Z | 77.807° E | 24.044° | 2025-10-29 17:14:29.336Z | 16.946° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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