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 26083.54180507 .00003215 00000-0 31332-3 0 9999
2 64567 97.7628 198.7134 0001149 160.3921 199.7343 14.93172998 41249Epoch: 2026-03-24T13:00Z
TLE epoch observation values (Epoch: 2026-03-24T13:00:11.958Z)
Latitude
0.00001°
Longitude
-178.3544°
Altitude
591.846 km
Speed
7.564 km/s
True Right ascension
13h 14m 51s
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
00:47:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
585.867 km
Perigee altitude
584.266 km
Semi-major axis
6,963.204 km
Eccentricity
0.00011
Inclination
97.7628°
RAAN
198.7134°
Arg. of periapsis
160.3921°
True anomaly
199.72985°
Mean anomaly
199.7343°
Eccentric anomaly
199.73208°
Mean motion
3.73533 °/min
Orbital period
96.38 mins
BSTAR
0.00031332
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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 | 2026-03-24 20:00:14.415Z | 29.696° NE | 2026-03-24 20:04:14.415Z | 112.226° ESE | 31.756° | 2026-03-24 20:07:14.415Z | 165.301° S |
| 5 mins | 2026-03-25 06:51:14.415Z | 108.76° ESE | 2026-03-25 06:53:14.415Z | 67.874° E | 22.946° | 2026-03-25 06:56:14.415Z | 16.833° NNE |
| 5 mins | 2026-03-25 08:26:14.415Z | 219.747° SW | 2026-03-25 08:28:14.415Z | 256.523° W | 22.426° | 2026-03-25 08:31:14.415Z | 313.116° NW |
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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