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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EAGLESAT 1 radio frequencies
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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: 19 hours ago
TLE from 19 hours ago
0 EAGLESAT 1
1 43018U 17073F 25260.67014922 .00116956 00000-0 12701-2 0 9991
2 43018 97.5215 159.1312 0065424 88.3928 272.4821 15.60424190426020Epoch: 2025-09-17T16:05Z
TLE epoch observation values (Epoch: 2025-09-17T16:05:00.892Z)
Latitude
-0.00006°
Longitude
-78.96528°
Altitude
387.945 km
Speed
7.678 km/s
True Right ascension
10h 36m 31s
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
03:37:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
427.584 km
Perigee altitude
339.112 km
Semi-major axis
6,761.485 km
Eccentricity
0.00654
Inclination
97.5215°
RAAN
159.1312°
Arg. of periapsis
88.3928°
True anomaly
271.73286°
Mean anomaly
272.4821°
Eccentric anomaly
272.1075°
Mean motion
3.90373 °/min
Orbital period
92.22 mins
BSTAR
0.0012701
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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 | 2025-09-18 16:51:04.695Z | 125.34° SE | 2025-09-18 16:53:04.695Z | 71.343° E | 22.63° | 2025-09-18 16:55:04.695Z | 18.666° 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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