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: 1 day ago
TLE from 1 day ago
0 ARVAKER-2
1 64567U 25135AR 25312.86051219 .00006045 00000-0 60081-3 0 9992
2 64567 97.7596 64.9397 0001044 29.9329 330.1950 14.92051512 21008Epoch: 2025-11-08T20:39Z
TLE epoch observation values (Epoch: 2025-11-08T20:39:08.253Z)
Latitude
0.00005°
Longitude
66.87124°
Altitude
593.95 km
Speed
7.563 km/s
True Right ascension
04h 19m 45s
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
18:22:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.285 km
Perigee altitude
587.831 km
Semi-major axis
6,966.695 km
Eccentricity
0.0001
Inclination
97.7596°
RAAN
64.9397°
Arg. of periapsis
29.9329°
True anomaly
330.18905°
Mean anomaly
330.195°
Eccentric anomaly
330.19203°
Mean motion
3.73253 °/min
Orbital period
96.45 mins
BSTAR
0.00060081
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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 | 2025-11-10 06:36:32.627Z | 104.779° ESE | 2025-11-10 06:38:32.627Z | 73.516° E | 17.061° | 2025-11-10 06:41:32.627Z | 25.597° NE |
| 6 mins | 2025-11-10 08:11:32.627Z | 204.18° SW | 2025-11-10 08:14:32.627Z | 274.796° WNW | 29.757° | 2025-11-10 08:17:32.627Z | 326.661° NNW |
| 5 mins | 2025-11-10 19:55:32.627Z | 50.886° ENE | 2025-11-10 19:57:32.627Z | 101.153° ESE | 28.736° | 2025-11-10 20:00:32.627Z | 158.024° S |
| 4 mins | 2025-11-10 21:31:32.627Z | 314.928° NW | 2025-11-10 21:32:32.627Z | 296.391° NW | 18.16° | 2025-11-10 21:35:32.627Z | 248.58° W |
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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