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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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, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 ARCSAT-1
1 52161U 22033E 26264.79847065 .00009948 00000-0 14544-3 0 9992
2 52161 97.2734 358.6489 0004552 182.2262 177.8974 15.55815565250715Epoch: 2026-09-21T19:09Z
TLE epoch observation values (Epoch: 2026-09-21T19:09:47.864Z)
Latitude
0.00006°
Longitude
70.52633°
Altitude
406.009 km
Speed
7.665 km/s
True Right ascension
23h 54m 35s
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
21:56:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
399.779 km
Perigee altitude
393.612 km
Semi-major axis
6,774.832 km
Eccentricity
0.00046
Inclination
97.2734°
RAAN
358.6489°
Arg. of periapsis
182.2262°
True anomaly
177.89931°
Mean anomaly
177.8974°
Eccentric anomaly
177.89836°
Mean motion
3.8922 °/min
Orbital period
92.49 mins
BSTAR
0.00014544
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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 | 2026-09-22 06:06:25.644Z | 141.929° SSE | 2026-09-22 06:08:25.644Z | 89.105° E | 41.337° | 2026-09-22 06:11:25.644Z | 3.54° NNE |
| 4 mins | 2026-09-22 18:53:25.644Z | 39.431° NE | 2026-09-22 18:55:25.644Z | 111.966° ESE | 37.44° | 2026-09-22 18:57:25.644Z | 164.183° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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