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: 6 hours ago
TLE from 6 hours ago
0 ARVAKER-3
1 64566U 25135AQ 25312.18822737 .00005303 00000-0 52733-3 0 9998
2 64566 97.7584 64.2626 0001120 4.3758 355.7470 14.92085366 20902Epoch: 2025-11-08T04:31Z
TLE epoch observation values (Epoch: 2025-11-08T04:31:02.844Z)
Latitude
-0.00009°
Longitude
-51.12066°
Altitude
593.698 km
Speed
7.563 km/s
True Right ascension
04h 17m 03s
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
06:32:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.233 km
Perigee altitude
587.672 km
Semi-major axis
6,966.59 km
Eccentricity
0.00011
Inclination
97.7584°
RAAN
64.2626°
Arg. of periapsis
4.3758°
True anomaly
355.74605°
Mean anomaly
355.747°
Eccentric anomaly
355.74652°
Mean motion
3.73261 °/min
Orbital period
96.45 mins
BSTAR
0.00052733
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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 | 2025-11-08 19:35:14.752Z | 48.857° ENE | 2025-11-08 19:38:14.752Z | 99.019° ESE | 19.216° | 2025-11-08 19:40:14.752Z | 133.398° SE |
| 5 mins | 2025-11-08 21:11:14.752Z | 338.903° N | 2025-11-08 21:13:14.752Z | 298.885° NW | 26.421° | 2025-11-08 21:16:14.752Z | 236.31° WSW |
| 6 mins | 2025-11-09 08:01:14.752Z | 199.134° SSW | 2025-11-09 08:03:14.752Z | 258.882° W | 36.597° | 2025-11-09 08:07:14.752Z | 335.65° 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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