EAGLET 1, 43790
Orbit data source: Space-Track
EAGLET 1, 43790 is a payload satellite owned by OHB-I (IT) in SSO that was launched on Mon, 03 Dec 2018 UTC via an FALCON 9 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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43790 intel report (Beta)
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EAGLET 1 radio frequencies
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Edit Public Description
Identifier
Orbit
Country
ITRelated business
Manufacturer
OHB-I
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5 kg wet, 5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 EAGLET 1
1 43790U 18099AJ 25260.05539589 .00003830 00000-0 24024-3 0 9998
2 43790 97.4668 311.8282 0011342 200.2968 159.7812 15.09851818371075Epoch: 2025-09-17T01:19Z
TLE epoch observation values (Epoch: 2025-09-17T01:19:46.204Z)
Latitude
-0.00006°
Longitude
-64.35115°
Altitude
547.089 km
Speed
7.584 km/s
True Right ascension
20h 47m 18s
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
13:55:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
541.474 km
Perigee altitude
525.795 km
Semi-major axis
6,911.771 km
Eccentricity
0.00113
Inclination
97.4668°
RAAN
311.8282°
Arg. of periapsis
200.2968°
True anomaly
159.82606°
Mean anomaly
159.7812°
Eccentric anomaly
159.80364°
Mean motion
3.77711 °/min
Orbital period
95.31 mins
BSTAR
0.00024024
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Other satellites on launch #99 in the year 2018 (2018-12-03 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.EAGLET 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-18 02:54:52.384Z | 128.606° SE | 2025-09-18 02:57:52.384Z | 73.04° E | 25.521° | 2025-09-18 03:00:52.384Z | 14.629° NNE |
| 4 mins | 2025-09-18 04:30:52.384Z | 236.354° WSW | 2025-09-18 04:32:52.384Z | 275.401° WNW | 17.639° | 2025-09-18 04:34:52.384Z | 308.319° NW |
| 6 mins | 2025-09-18 16:04:52.384Z | 30.718° NE | 2025-09-18 16:07:52.384Z | 123.929° SE | 35.222° | 2025-09-18 16:10:52.384Z | 173.711° S |
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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