ANGELS, 44876 (Decayed)
Orbit data source: Space-Track
ANGELS, 44876 was a payload satellite owned by CNES (FR) in LEO that was launched on Wed, 18 Dec 2019 UTC via a SOYUZ-ST-A launch vehicle from the French Guiana (FRGUI). 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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44876 intel report (Beta)
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Identifier
Orbit
Country
FRRelated business
Manufacturer
Hemeria
Mission
Decayed Civil Communications
Bus & Motor
CUBESAT 12U, Unknown motor
Mass
27 kg wet, 27 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.126 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 week ago
TLE from 1 week ago
0 ANGELS
1 44876U 19092D 26117.66670223 .09102593 25597-5 62771-3 0 9997
2 44876 97.3862 337.5251 0009038 257.4278 102.6011 16.40735846354431Epoch: 2026-04-27T16:00Z
TLE epoch observation values (Epoch: 2026-04-27T16:00:03.072Z)
Latitude
-0.00006°
Longitude
-118.14078°
Altitude
168.394 km
Speed
7.804 km/s
True Right ascension
22h 30m 06s
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
08:15:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
166.562 km
Perigee altitude
154.742 km
Semi-major axis
6,538.789 km
Eccentricity
0.0009
Inclination
97.3862°
RAAN
337.5251°
Arg. of periapsis
257.4278°
True anomaly
102.70215°
Mean anomaly
102.6011°
Eccentric anomaly
102.65163°
Mean motion
4.10485 °/min
Orbital period
87.7 mins
BSTAR
0.00062771
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Other satellites on launch #92 in the year 2019 (2019-12-18 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.ANGELS Visibility
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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. |
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| This satellite is decayed. |
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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