ARCSAT-1, 52161
Orbit data source: Space-Track
ARCSAT-1, 52161 is a payload satellite owned by NDRE (NO) in SSO that was launched on Fri, 01 Apr 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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52161 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
NO / NORRelated business
Manufacturer
GOMSpace
Mission
Operational Defense Communications
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.080 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 ARCSAT-1
1 52161U 22033E 25348.80937010 .00010412 00000-0 19797-3 0 9999
2 52161 97.2835 74.0316 0006204 134.7071 225.4687 15.48416070207129Epoch: 2025-12-14T19:25Z
TLE epoch observation values (Epoch: 2025-12-14T19:25:29.576Z)
Latitude
0.00006°
Longitude
58.9414°
Altitude
427.452 km
Speed
7.653 km/s
True Right ascension
04h 56m 07s
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
19:04:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
422.498 km
Perigee altitude
414.065 km
Semi-major axis
6,796.419 km
Eccentricity
0.00062
Inclination
97.2835°
RAAN
74.0316°
Arg. of periapsis
134.7071°
True anomaly
225.41805°
Mean anomaly
225.4687°
Eccentric anomaly
225.44337°
Mean motion
3.87367 °/min
Orbital period
92.94 mins
BSTAR
0.00019797
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Other satellites on launch #33 in the year 2022 (2022-04-01 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.ARCSAT-1 Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-16 05:40:48.507Z | 150.235° SSE | 2025-12-16 05:43:48.507Z | 40.428° NE | 36.172° | 2025-12-16 05:45:48.507Z | 1.045° NNE |
| 4 mins | 2025-12-16 18:31:48.507Z | 31.227° NE | 2025-12-16 18:33:48.507Z | 131.674° SE | 37.506° | 2025-12-16 18:35:48.507Z | 175.891° S |
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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