ARVAKER-2, 64567
Orbit data source: Space-Track
ARVAKER-2, 64567 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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64567 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-2
1 64567U 25135AR 25293.94757106 .00005669 00000-0 56624-3 0 9996
2 64567 97.7585 46.3192 0002248 60.9330 299.2114 14.91882166 18185Epoch: 2025-10-20T22:44Z
TLE epoch observation values (Epoch: 2025-10-20T22:44:30.139Z)
Latitude
-0.00001°
Longitude
35.55105°
Altitude
594.344 km
Speed
7.563 km/s
True Right ascension
03h 05m 16s
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
01:26:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.652 km
Perigee altitude
587.52 km
Semi-major axis
6,967.223 km
Eccentricity
0.00022
Inclination
97.7585°
RAAN
46.3192°
Arg. of periapsis
60.933°
True anomaly
299.18891°
Mean anomaly
299.2114°
Eccentric anomaly
299.20016°
Mean motion
3.7321 °/min
Orbital period
96.46 mins
BSTAR
0.00056624
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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-2 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 | 2025-10-21 06:55:20.623Z | 129.238° SE | 2025-10-21 06:58:20.623Z | 82.941° E | 25.2° | 2025-10-21 07:02:20.623Z | 10.764° NNE |
| 5 mins | 2025-10-21 08:32:20.623Z | 228.16° WSW | 2025-10-21 08:34:20.623Z | 264.975° W | 20.033° | 2025-10-21 08:37:20.623Z | 313.998° NW |
| 6 mins | 2025-10-21 20:15:20.623Z | 28.937° NE | 2025-10-21 20:17:20.623Z | 79.499° E | 39.797° | 2025-10-21 20:21:20.623Z | 179.251° 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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