Showing default

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.

Loading next visibility...
Identifier
52161, 2022-033E
Orbit
SSO
Country
Flag of NONO / NOR
Related business
Manufacturer
GOMSpace
Mission
Operational Defense Communications
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
2022-04-01 (4 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.080 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 ARCSAT-1
1 52161U 22033E   25286.92266202  .00016092  00000-0  32722-3 0  9994
2 52161  97.2866  11.7295 0005640  29.3834 330.7732 15.46362208197553
Epoch: 2025-10-13T22:08Z
TLE epoch observation values (Epoch: 2025-10-13T22:08:37.998Z)
Latitude
-0.00001°
Longitude
16.85269°
Altitude
427.158 km
Speed
7.657 km/s
True Right ascension
00h 46m 55s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
04:48:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
428.141 km
Perigee altitude
420.468 km
Semi-major axis
6,802.441 km
Eccentricity
0.00056
Inclination
97.2866°
RAAN
11.7295°
Arg. of periapsis
29.3834°
True anomaly
330.74162°
Mean anomaly
330.7732°
Eccentric anomaly
330.75741°
Mean motion
3.86853 °/min
Orbital period
93.06 mins
BSTAR
0.00032722
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|