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 26062.62742297 .00003780 00000-0 36823-3 0 9991
2 64566 97.7600 178.0510 0000645 322.6983 37.4192 14.93083042 38122Epoch: 2026-03-03T15:03Z
TLE epoch observation values (Epoch: 2026-03-03T15:03:29.344Z)
Latitude
0.00001°
Longitude
150.77497°
Altitude
591.016 km
Speed
7.565 km/s
True Right ascension
11h 52m 12s
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
02:02:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
585.795 km
Perigee altitude
584.897 km
Semi-major axis
6,963.483 km
Eccentricity
0.00006
Inclination
97.76°
RAAN
178.051°
Arg. of periapsis
322.6983°
True anomaly
37.42369°
Mean anomaly
37.4192°
Eccentric anomaly
37.42145°
Mean motion
3.73511 °/min
Orbital period
96.38 mins
BSTAR
0.00036823
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-03-04 07:16:04.447Z | 146.593° SSE | 2026-03-04 07:20:04.447Z | 49.36° ENE | 36.086° | 2026-03-04 07:23:04.447Z | 0.86° NNE |
| 6 mins | 2026-03-04 20:35:04.447Z | 8.555° NNE | 2026-03-04 20:38:04.447Z | 248.714° W | 44.293° | 2026-03-04 20:41:04.447Z | 198.428° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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