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: 7 hours ago
TLE from 7 hours ago
0 ARVAKER-2
1 64567U 25135AR 26133.26083523 .00001403 00000-0 13900-3 0 9992
2 64567 97.7698 247.8176 0002770 83.9963 276.1572 14.93411777 48663Epoch: 2026-05-13T06:15Z
TLE epoch observation values (Epoch: 2026-05-13T06:15:36.163Z)
Latitude
-0.00007°
Longitude
-77.10647°
Altitude
590.144 km
Speed
7.565 km/s
True Right ascension
16h 31m 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
22:06:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
586.253 km
Perigee altitude
582.395 km
Semi-major axis
6,962.461 km
Eccentricity
0.00028
Inclination
97.7698°
RAAN
247.8176°
Arg. of periapsis
83.9963°
True anomaly
276.12564°
Mean anomaly
276.1572°
Eccentric anomaly
276.14142°
Mean motion
3.73593 °/min
Orbital period
96.36 mins
BSTAR
0.000139
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-05-13 19:42:42.202Z | 48.796° ENE | 2026-05-13 19:45:42.202Z | 106.009° ESE | 21.664° | 2026-05-13 19:47:42.202Z | 140.979° SSE |
| 5 mins | 2026-05-13 21:18:42.202Z | 330.579° NNW | 2026-05-13 21:20:42.202Z | 288.839° WNW | 23.393° | 2026-05-13 21:23:42.202Z | 237.402° WSW |
| 6 mins | 2026-05-14 08:07:42.202Z | 204.77° SW | 2026-05-14 08:09:42.202Z | 255.974° W | 32.857° | 2026-05-14 08:13:42.202Z | 332.169° 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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