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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Edit Public Description
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: 9 hours ago
TLE from 9 hours ago
0 ANGOSAT 2
1 54033U 22131A 26039.34194346 .00000142 00000-0 00000+0 0 9994
2 54033 0.0170 188.2068 0000554 262.7336 193.5792 1.00272690 12186Epoch: 2026-02-08T08:12Z
TLE epoch observation values (Epoch: 2026-02-08T08:12:23.914Z)
Latitude
0.01099°
Longitude
22.99365°
Altitude
35,788.101 km
Speed
3.075 km/s
True Right ascension
18h 58m 10s
True Declination
0° 00' 40"
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
19:50:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,789.748 km
Perigee altitude
35,785.076 km
Semi-major axis
42,165.549 km
Eccentricity
0.00006
Inclination
0.017°
RAAN
188.2068°
Arg. of periapsis
262.7336°
True anomaly
193.57771°
Mean anomaly
193.5792°
Eccentric anomaly
193.57845°
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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