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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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: 8 hours ago
TLE from 8 hours ago
0 EAGLET 1
1 43790U 18099AJ 25299.67928123 .00006039 00000-0 37026-3 0 9994
2 43790 97.4593 350.4312 0013246 74.5761 285.6931 15.10437115377050Epoch: 2025-10-26T16:18Z
TLE epoch observation values (Epoch: 2025-10-26T16:18:09.898Z)
Latitude
-0.00001°
Longitude
70.59794°
Altitude
535.476 km
Speed
7.596 km/s
True Right ascension
23h 21m 43s
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
20:04:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
541 km
Perigee altitude
522.694 km
Semi-major axis
6,909.984 km
Eccentricity
0.00132
Inclination
97.4593°
RAAN
350.4312°
Arg. of periapsis
74.5761°
True anomaly
285.5469°
Mean anomaly
285.6931°
Eccentric anomaly
285.62001°
Mean motion
3.77857 °/min
Orbital period
95.27 mins
BSTAR
0.00037026
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-27 03:32:54.662Z | 167.499° S | 2025-10-27 03:36:54.662Z | 342.098° N | 43.781° | 2025-10-27 03:39:54.662Z | 347.56° N |
| 6 mins | 2025-10-27 16:42:54.662Z | 356.752° N | 2025-10-27 16:45:54.662Z | 277.652° WNW | 37.008° | 2025-10-27 16:48:54.662Z | 213.119° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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