Showing default

ARVAKER-2, 64567

Orbit data source: Space-Track

ARVAKER-2, 64567 is a payload satellite owned by NSC (NO) in SSO that was launched on Mon, 23 Jun 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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
64567, 2025-135AR
Orbit
SSO
Country
Flag of NONO / NOR
Related business
Manufacturer
NanoAvionics
Mission
Operational Commercial Imaging
Bus & Motor
MP42, Unknown motor
Mass
~100 kg wet, ~100 kg dry
Launch date (UTC)
2025-06-23 (5 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.146 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 ARVAKER-2
1 64567U 25135AR  25340.89019402  .00004874  00000-0  48217-3 0  9999
2 64567  97.7613  92.5526 0000927 173.9990 186.1240 14.92333173 25182
Epoch: 2025-12-06T21:21Z
TLE epoch observation values (Epoch: 2025-12-06T21:21:52.763Z)
Latitude
-0.00005°
Longitude
56.17132°
Altitude
594.348 km
Speed
7.562 km/s
True Right ascension
06h 10m 12s
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
04:13:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.327 km
Perigee altitude
587.035 km
Semi-major axis
6,965.818 km
Eccentricity
0.00009
Inclination
97.7613°
RAAN
92.5526°
Arg. of periapsis
173.999°
True anomaly
186.12287°
Mean anomaly
186.124°
Eccentric anomaly
186.12343°
Mean motion
3.73323 °/min
Orbital period
96.43 mins
BSTAR
0.00048217
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
|