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: 1 day ago
TLE from 1 day ago
0 EAGLET 1
1 43790U 18099AJ 25312.59691125 .00007938 00000-0 48316-3 0 9993
2 43790 97.4571 3.0150 0012477 34.7126 325.4916 15.10611482379009Epoch: 2025-11-08T14:19Z
TLE epoch observation values (Epoch: 2025-11-08T14:19:33.131Z)
Latitude
0.00004°
Longitude
100.1027°
Altitude
530.305 km
Speed
7.602 km/s
True Right ascension
00h 12m 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
21:05:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
539.935 km
Perigee altitude
522.694 km
Semi-major axis
6,909.452 km
Eccentricity
0.00125
Inclination
97.4571°
RAAN
3.015°
Arg. of periapsis
34.7126°
True anomaly
325.4105°
Mean anomaly
325.4916°
Eccentric anomaly
325.45106°
Mean motion
3.77901 °/min
Orbital period
95.26 mins
BSTAR
0.00048316
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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 | 2025-11-10 03:01:38.166Z | 134.109° SE | 2025-11-10 03:04:38.166Z | 65.128° ENE | 29.835° | 2025-11-10 03:07:38.166Z | 7.916° NNE |
| 5 mins | 2025-11-10 16:11:38.166Z | 27.732° NE | 2025-11-10 16:13:38.166Z | 111.155° ESE | 41.582° | 2025-11-10 16:16:38.166Z | 180.496° SSW |
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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