OPS-SAT, 44878 (Decayed)
Orbit data source: Space-Track
OPS-SAT, 44878 was a payload satellite owned by ESA (ESA) 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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44878 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
ESARelated business
Manufacturer
TUG/GOMSP
Mission
Decayed Civil Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
7 kg wet, 7 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.3 m
Radar Cross Section
0.048 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 OPS-SAT
1 44878U 19092F 24143.84045348 .17176592 26004-5 26698-3 0 9991
2 44878 97.4081 350.0941 0014332 258.8962 101.0730 16.47500343246598Epoch: 2024-05-22T20:10Z
TLE epoch observation values (Epoch: 2024-05-22T20:10:15.18Z)
Latitude
-0.00003°
Longitude
166.58791°
Altitude
150.996 km
Speed
7.814 km/s
True Right ascension
23h 20m 22s
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
11:44:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
152.07 km
Perigee altitude
133.379 km
Semi-major axis
6,520.861 km
Eccentricity
0.00143
Inclination
97.4081°
RAAN
350.0941°
Arg. of periapsis
258.8962°
True anomaly
101.23412°
Mean anomaly
101.073°
Eccentric anomaly
101.15357°
Mean motion
4.12179 °/min
Orbital period
87.34 mins
BSTAR
0.00026698
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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.OPS-SAT 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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