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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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-2
1 64567U 25135AR 26178.55164095 .00001901 00000-0 18551-3 0 9997
2 64567 97.7750 292.5937 0000156 51.0988 309.0245 14.93594759 55420Epoch: 2026-06-27T13:14Z
TLE epoch observation values (Epoch: 2026-06-27T13:14:21.778Z)
Latitude
-0.00006°
Longitude
178.3388°
Altitude
589.713 km
Speed
7.565 km/s
True Right ascension
19h 30m 22s
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
05:15:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
583.864 km
Perigee altitude
583.646 km
Semi-major axis
6,961.892 km
Eccentricity
0.00002
Inclination
97.775°
RAAN
292.5937°
Arg. of periapsis
51.0988°
True anomaly
309.02311°
Mean anomaly
309.0245°
Eccentric anomaly
309.02381°
Mean motion
3.73639 °/min
Orbital period
96.35 mins
BSTAR
0.00018551
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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 | 2026-06-27 20:14:20.793Z | 23.151° NE | 2026-06-27 20:17:20.793Z | 71.41° E | 38.533° | 2026-06-27 20:21:20.793Z | 177.886° S |
| 6 mins | 2026-06-28 07:04:20.793Z | 126.174° SE | 2026-06-28 07:06:20.793Z | 86.622° E | 28.595° | 2026-06-28 07:10:20.793Z | 7.713° NNE |
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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