NUSAT-36 (ANNIE CANNON), 56190 (Decayed)
Orbit data source: Space-Track
NUSAT-36 (ANNIE CANNON), 56190 was a payload satellite owned by URUGUS S.A. (AR) in LEO that was launched on Sat, 15 Apr 2023 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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56190 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / ARGNRelated business
Manufacturer
URUGUS S.A.
Mission
Decayed Commercial Imaging
Bus & Motor
NEWSAT V, Unknown motor
Mass
41.5 kg wet, 38.5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 1.0 m
Radar Cross Section
0.542 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 months ago
TLE from 7 months ago
0 NUSAT-36 (ANNIE CANNON)
1 56190U 23054N 25101.69279641 .08896754 25673-5 67003-3 0 9992
2 56190 97.2913 12.6773 0007816 213.5058 146.5748 16.40562274112518Epoch: 2025-04-11T16:37Z
TLE epoch observation values (Epoch: 2025-04-11T16:37:37.609Z)
Latitude
-0.00011°
Longitude
-76.87655°
Altitude
171.833 km
Speed
7.801 km/s
True Right ascension
00h 50m 42s
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
10:38:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
166.22 km
Perigee altitude
155.998 km
Semi-major axis
6,539.246 km
Eccentricity
0.00078
Inclination
97.2913°
RAAN
12.6773°
Arg. of periapsis
213.5058°
True anomaly
146.6241°
Mean anomaly
146.5748°
Eccentric anomaly
146.59945°
Mean motion
4.10442 °/min
Orbital period
87.71 mins
BSTAR
0.00067003
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Other satellites on launch #54 in the year 2023 (2023-04-15 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.NUSAT-36 (ANNIE CANNON) 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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