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: 5 hours ago
TLE from 5 hours ago
0 ARVAKER-3
1 64566U 25135AQ 26120.18759376 .00002664 00000-0 25896-3 0 9991
2 64566 97.7664 234.8724 0003298 102.5637 257.5951 14.93419743 46711Epoch: 2026-04-30T04:30Z
TLE epoch observation values (Epoch: 2026-04-30T04:30:08.100Z)
Latitude
-0.00011°
Longitude
-50.79913°
Altitude
590.82 km
Speed
7.564 km/s
True Right ascension
15h 39m 29s
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
16:39:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
586.595 km
Perigee altitude
582.003 km
Semi-major axis
6,962.436 km
Eccentricity
0.00033
Inclination
97.7664°
RAAN
234.8724°
Arg. of periapsis
102.5637°
True anomaly
257.55819°
Mean anomaly
257.5951°
Eccentric anomaly
257.57665°
Mean motion
3.73595 °/min
Orbital period
96.36 mins
BSTAR
0.00025896
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-04-30 19:33:59.791Z | 55.112° ENE | 2026-04-30 19:35:59.791Z | 88.16° E | 18.091° | 2026-04-30 19:38:59.791Z | 137.706° SSE |
| 5 mins | 2026-04-30 21:09:59.791Z | 332.725° NNW | 2026-04-30 21:11:59.791Z | 282.999° WNW | 27.528° | 2026-04-30 21:14:59.791Z | 229.681° WSW |
| 6 mins | 2026-05-01 07:57:59.791Z | 188.164° SSW | 2026-05-01 08:00:59.791Z | 264.585° W | 38.066° | 2026-05-01 08:03:59.791Z | 332.991° NNW |
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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