USA 320, 51075 (Decayed)
Orbit data source: Space-Track
USA 320, 51075 was a payload satellite owned by NRO (US) in LEO that was launched on Thu, 13 Jan 2022 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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51075 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
SPXS?
Mission
Decayed Defense Sigint
Bus & Motor
STARLINK?, Unknown motor
Mass
300 kg wet, ~280 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 4.5 m
Radar Cross Section
11.087 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 months ago
TLE from 10 months ago
0 USA 320
1 51075U 22002CV 24333.48886079 .11094112 25414-5 23303-2 0 9992
2 51075 97.3686 41.8129 0006037 233.9118 260.4753 16.30954062159623Epoch: 2024-11-28T11:43Z
TLE epoch observation values (Epoch: 2024-11-28T11:43:57.572Z)
Latitude
45.3026°
Longitude
-14.58002°
Altitude
197.656 km
Speed
7.792 km/s
True Right ascension
15h 17m 07s
True Declination
45° 06' 58"
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
21:05:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
190.758 km
Perigee altitude
182.832 km
Semi-major axis
6,564.932 km
Eccentricity
0.0006
Inclination
97.3686°
RAAN
41.8129°
Arg. of periapsis
233.9118°
True anomaly
260.40708°
Mean anomaly
260.4753°
Eccentric anomaly
260.44119°
Mean motion
4.08035 °/min
Orbital period
88.23 mins
BSTAR
0.0023303
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Other satellites on launch #2 in the year 2022 (2022-01-13 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.USA 320 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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