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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Identifier
Orbit
Country
NO / NORRelated business
Manufacturer
NanoAvionics
Mission
Operational Commercial Sigint
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: 7 hours ago
TLE from 7 hours ago
0 ARVAKER-3
1 64566U 25135AQ 26163.87030699 .00002680 00000-0 25930-3 0 9991
2 64566 97.7723 278.0443 0001251 19.1070 341.0196 14.93601259 53236Epoch: 2026-06-12T20:53Z
TLE epoch observation values (Epoch: 2026-06-12T20:53:14.523Z)
Latitude
-0.00009°
Longitude
63.54025°
Altitude
588.937 km
Speed
7.566 km/s
True Right ascension
18h 32m 10s
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
13:59:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
584.606 km
Perigee altitude
582.864 km
Semi-major axis
6,961.872 km
Eccentricity
0.00013
Inclination
97.7723°
RAAN
278.0443°
Arg. of periapsis
19.107°
True anomaly
341.01494°
Mean anomaly
341.0196°
Eccentric anomaly
341.01727°
Mean motion
3.73641 °/min
Orbital period
96.35 mins
BSTAR
0.0002593
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-13 06:41:45.678Z | 102.691° ESE | 2026-06-13 06:43:45.678Z | 67.36° ENE | 18.635° | 2026-06-13 06:45:45.678Z | 32.133° NE |
| 5 mins | 2026-06-13 08:16:45.678Z | 212.642° SW | 2026-06-13 08:18:45.678Z | 256.143° W | 27.651° | 2026-06-13 08:21:45.678Z | 319.429° NNW |
| 6 mins | 2026-06-13 19:58:45.678Z | 37.996° NE | 2026-06-13 20:01:45.678Z | 106.281° ESE | 30.302° | 2026-06-13 20:04:45.678Z | 161.814° 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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