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: 16 hours ago
TLE from 16 hours ago
0 EAGLESAT 1
1 43018U 17073F 25243.26883666 .00123266 00000-0 15566-2 0 9990
2 43018 97.5246 140.7403 0070099 149.3970 211.1404 15.56181154423311Epoch: 2025-08-31T06:27Z
TLE epoch observation values (Epoch: 2025-08-31T06:27:07.487Z)
Latitude
0.00007°
Longitude
64.26789°
Altitude
442.615 km
Speed
7.623 km/s
True Right ascension
09h 22m 57s
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
14:08:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
443.128 km
Perigee altitude
348.161 km
Semi-major axis
6,773.781 km
Eccentricity
0.00701
Inclination
97.5246°
RAAN
140.7403°
Arg. of periapsis
149.397°
True anomaly
210.72809°
Mean anomaly
211.1404°
Eccentric anomaly
210.93394°
Mean motion
3.89311 °/min
Orbital period
92.47 mins
BSTAR
0.0015566
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Other satellites on launch #73 in the year 2017 (2017-11-18 UTC)
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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-01 06:09:03.439Z | 10.834° NNE | 2025-09-01 06:12:03.439Z | 205.001° SW | 42.42° | 2025-09-01 06:14:03.439Z | 194.842° SSW |
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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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Authenticating...
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