ANGOSAT 2, 54033
Orbit data source: Space-Track
ANGOSAT 2, 54033 is a payload satellite owned by GGPEN (AO) in GEO that was launched on Wed, 12 Oct 2022 UTC via a PROTON-M/DM-3 launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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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54033 intel report (Beta)
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Identifier
Orbit
Country
AO / AGORelated business
Manufacturer
Resehetnev ISS
Mission
Operational Civil Communications
Bus & Motor
EKSPRESS-1000N, AOCS
Mass
2,150 kg wet, ~1,800 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 7.5 m
Radar Cross Section
16.987 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 ANGOSAT 2
1 54033U 22131A 26308.18505157 .00000130 00000-0 00000-0 0 9999
2 54033 0.0052 75.6778 0000803 231.1000 186.3023 1.00272631 14888Epoch: 2026-11-04T04:26Z
TLE epoch observation values (Epoch: 2026-11-04T04:26:28.455Z)
Latitude
0.01338°
Longitude
23.00084°
Altitude
35,789.197 km
Speed
3.074 km/s
True Right ascension
08h 52m 13s
True Declination
0° 00' 48"
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
12:15:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,790.814 km
Perigee altitude
35,784.042 km
Semi-major axis
42,165.565 km
Eccentricity
0.00008
Inclination
0.0052°
RAAN
75.6778°
Arg. of periapsis
231.1°
True anomaly
186.30129°
Mean anomaly
186.3023°
Eccentric anomaly
186.30179°
Mean motion
0.25067 °/min
Orbital period
1,436.14 mins
BSTAR
0
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Other satellites on launch #131 in the year 2022 (2022-10-12 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.ANGOSAT 2 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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| ANGOSAT 2 is likely not visible in the next few days. |
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54033 neighbors
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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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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