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: 7 hours ago
TLE from 7 hours ago
0 EAGLET 1
1 43790U 18099AJ 26308.88616442 .00003046 00000-0 17213-3 0 9998
2 43790 97.4062 354.7721 0010012 211.5393 148.5240 15.13803112433616Epoch: 2026-11-04T21:16Z
TLE epoch observation values (Epoch: 2026-11-04T21:16:04.605Z)
Latitude
-0.00002°
Longitude
-8.37513°
Altitude
533.594 km
Speed
7.593 km/s
True Right ascension
23h 39m 05s
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
00:41:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
528.497 km
Perigee altitude
514.681 km
Semi-major axis
6,899.726 km
Eccentricity
0.001
Inclination
97.4062°
RAAN
354.7721°
Arg. of periapsis
211.5393°
True anomaly
148.58384°
Mean anomaly
148.524°
Eccentric anomaly
148.55393°
Mean motion
3.787 °/min
Orbital period
95.06 mins
BSTAR
0.00017213
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-11-05 15:18:12.654Z | 51.205° ENE | 2026-11-05 15:20:12.654Z | 89.326° E | 21.981° | 2026-11-05 15:23:12.654Z | 145.124° SSE |
| 4 mins | 2026-11-05 16:53:12.654Z | 321.454° NNW | 2026-11-05 16:54:12.654Z | 299.752° NW | 22.784° | 2026-11-05 16:57:12.654Z | 241.097° WSW |
| 5 mins | 2026-11-06 03:33:12.654Z | 194.443° SSW | 2026-11-06 03:35:12.654Z | 270.957° WNW | 53.102° | 2026-11-06 03:38:12.654Z | 335.945° 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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