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: 10 hours ago
TLE from 10 hours ago
0 EAGLET 1
1 43790U 18099AJ 26038.64022001 .00005755 00000-0 34013-3 0 9990
2 43790 97.4427 91.7129 0012821 75.6205 284.6448 15.11798723392752Epoch: 2026-02-07T15:21Z
TLE epoch observation values (Epoch: 2026-02-07T15:21:55.008Z)
Latitude
-0.00003°
Longitude
83.47286°
Altitude
531.563 km
Speed
7.598 km/s
True Right ascension
06h 06m 51s
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
03:24:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
536.547 km
Perigee altitude
518.839 km
Semi-major axis
6,905.83 km
Eccentricity
0.00128
Inclination
97.4427°
RAAN
91.7129°
Arg. of periapsis
75.6205°
True anomaly
284.5026°
Mean anomaly
284.6448°
Eccentric anomaly
284.5737°
Mean motion
3.78198 °/min
Orbital period
95.19 mins
BSTAR
0.00034013
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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 | 2026-02-08 02:38:16.906Z | 110.713° ESE | 2026-02-08 02:40:16.906Z | 73.286° E | 19.488° | 2026-02-08 02:43:16.906Z | 20.218° NNE |
| 4 mins | 2026-02-08 04:13:16.906Z | 231.23° WSW | 2026-02-08 04:14:16.906Z | 253.826° W | 22.12° | 2026-02-08 04:17:16.906Z | 315.105° NNW |
| 4 mins | 2026-02-08 15:47:16.906Z | 55.24° ENE | 2026-02-08 15:48:16.906Z | 81.633° E | 27.959° | 2026-02-08 15:51:16.906Z | 155.45° SSE |
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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