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 26290.28393811 .00002082 00000-0 20086-3 0 9999
2 64567 97.7844 43.1878 0000170 156.6040 203.5187 14.93960779 72101Epoch: 2026-10-17T06:48Z
TLE epoch observation values (Epoch: 2026-10-17T06:48:52.252Z)
Latitude
-0.0001°
Longitude
-84.82271°
Altitude
588.753 km
Speed
7.566 km/s
True Right ascension
02h 52m 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
06:34:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
582.736 km
Perigee altitude
582.499 km
Semi-major axis
6,960.754 km
Eccentricity
0.00002
Inclination
97.7844°
RAAN
43.1878°
Arg. of periapsis
156.604°
True anomaly
203.51792°
Mean anomaly
203.5187°
Eccentric anomaly
203.51831°
Mean motion
3.73731 °/min
Orbital period
96.33 mins
BSTAR
0.00020086
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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 | 2026-10-17 20:14:06.875Z | 22.335° NNE | 2026-10-17 20:18:06.875Z | 104.758° ESE | 53.979° | 2026-10-17 20:21:06.875Z | 174.239° S |
| 5 mins | 2026-10-18 07:05:06.875Z | 114.688° SE | 2026-10-18 07:07:06.875Z | 63.34° ENE | 32.45° | 2026-10-18 07:10:06.875Z | 10.54° NNE |
| 4 mins | 2026-10-18 08:41:06.875Z | 243.352° WSW | 2026-10-18 08:42:06.875Z | 261.65° W | 18.715° | 2026-10-18 08:45:06.875Z | 309.944° 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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