ARVAKER-3, 64566
Orbit data source: Space-Track
ARVAKER-3, 64566 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.
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64566 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
NO / NORRelated business
Manufacturer
NanoAvionics
Mission
Operational Commercial Imaging
Bus & Motor
MP42, Unknown motor
Mass
~100 kg wet, ~100 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
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 & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 ARVAKER-3
1 64566U 25135AQ 25293.94646727 .00005773 00000-0 57584-3 0 9993
2 64566 97.7573 46.3045 0002485 51.0704 309.0736 14.91927928 18183Epoch: 2025-10-20T22:42Z
TLE epoch observation values (Epoch: 2025-10-20T22:42:54.772Z)
Latitude
-0.00001°
Longitude
35.9348°
Altitude
593.875 km
Speed
7.564 km/s
True Right ascension
03h 05m 13s
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
01:28:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.674 km
Perigee altitude
587.212 km
Semi-major axis
6,967.08 km
Eccentricity
0.00025
Inclination
97.7573°
RAAN
46.3045°
Arg. of periapsis
51.0704°
True anomaly
309.05149°
Mean anomaly
309.0736°
Eccentric anomaly
309.06254°
Mean motion
3.73222 °/min
Orbital period
96.46 mins
BSTAR
0.00057584
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Other satellites on launch #135 in the year 2025 (2025-06-23 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.ARVAKER-3 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-21 06:53:53.345Z | 127.17° SE | 2025-10-21 06:56:53.345Z | 79.088° E | 24.695° | 2025-10-21 06:59:53.345Z | 19.05° NNE |
| 5 mins | 2025-10-21 08:30:53.345Z | 229.217° WSW | 2025-10-21 08:32:53.345Z | 267.95° W | 20.679° | 2025-10-21 08:35:53.345Z | 316.024° NNW |
| 6 mins | 2025-10-21 20:13:53.345Z | 31.867° NE | 2025-10-21 20:15:53.345Z | 90.971° ESE | 39.433° | 2025-10-21 20:19:53.345Z | 178.426° 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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