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: 23 hours ago
TLE from 23 hours ago
0 EAGLET 1
1 43790U 18099AJ 26235.57008068 .00003140 00000-0 17931-3 0 9994
2 43790 97.4182 283.4528 0012673 110.2979 249.9616 15.13374370422522Epoch: 2026-08-23T13:40Z
TLE epoch observation values (Epoch: 2026-08-23T13:40:54.970Z)
Latitude
-0.00001°
Longitude
106.35952°
Altitude
532.008 km
Speed
7.595 km/s
True Right ascension
18h 53m 48s
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
04:05:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
531.639 km
Perigee altitude
514.148 km
Semi-major axis
6,901.03 km
Eccentricity
0.00127
Inclination
97.4182°
RAAN
283.4528°
Arg. of periapsis
110.2979°
True anomaly
249.82524°
Mean anomaly
249.9616°
Eccentric anomaly
249.89341°
Mean motion
3.78593 °/min
Orbital period
95.09 mins
BSTAR
0.00017931
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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 | 2026-08-24 15:38:18.274Z | 32.711° NE | 2026-08-24 15:41:18.274Z | 93.03° ESE | 29.749° | 2026-08-24 15:44:18.274Z | 160.744° S |
| 5 mins | 2026-08-25 03:54:18.274Z | 212.876° SW | 2026-08-25 03:56:18.274Z | 262.099° W | 27.344° | 2026-08-25 03:59:18.274Z | 323.628° NNW |
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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