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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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, 0.2 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 EAGLET 1
1 43790U 18099AJ 26295.59959169 .00003907 00000-0 22022-3 0 9997
2 43790 97.4095 341.8541 0009256 263.8258 96.1920 15.13733787431607Epoch: 2026-10-22T14:23Z
TLE epoch observation values (Epoch: 2026-10-22T14:23:24.722Z)
Latitude
0.00007°
Longitude
94.96891°
Altitude
528.602 km
Speed
7.598 km/s
True Right ascension
22h 47m 24s
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
03:21:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
528.186 km
Perigee altitude
515.413 km
Semi-major axis
6,899.937 km
Eccentricity
0.00093
Inclination
97.4095°
RAAN
341.8541°
Arg. of periapsis
263.8258°
True anomaly
96.29743°
Mean anomaly
96.192°
Eccentric anomaly
96.24472°
Mean motion
3.78683 °/min
Orbital period
95.07 mins
BSTAR
0.00022022
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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 | 2026-10-23 16:19:34.410Z | 3.225° NNE | 2026-10-23 16:23:34.410Z | 260.145° W | 54.9° | 2026-10-23 16:26:34.410Z | 207.41° SW |
| 5 mins | 2026-10-24 03:01:34.410Z | 144.096° SSE | 2026-10-24 03:03:34.410Z | 74.154° E | 56.581° | 2026-10-24 03:06:34.410Z | 359.459° N |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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