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: 6 hours ago
TLE from 6 hours ago
0 ARVAKER-2
1 64567U 25135AR 26260.27682749 .00001857 00000-0 18016-3 0 9995
2 64567 97.7811 13.4660 0002075 51.2547 308.8858 14.93861107 67622Epoch: 2026-09-17T06:38Z
TLE epoch observation values (Epoch: 2026-09-17T06:38:37.895Z)
Latitude
-0.00001°
Longitude
-82.40828°
Altitude
588.047 km
Speed
7.567 km/s
True Right ascension
00h 53m 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
05:13:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
584.371 km
Perigee altitude
581.483 km
Semi-major axis
6,961.064 km
Eccentricity
0.00021
Inclination
97.7811°
RAAN
13.466°
Arg. of periapsis
51.2547°
True anomaly
308.86729°
Mean anomaly
308.8858°
Eccentric anomaly
308.87654°
Mean motion
3.73706 °/min
Orbital period
96.33 mins
BSTAR
0.00018016
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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 | 2026-09-17 20:03:58.773Z | 27.123° NE | 2026-09-17 20:07:58.773Z | 100.892° ESE | 41.276° | 2026-09-17 20:10:58.773Z | 164.792° S |
| 5 mins | 2026-09-18 06:54:58.773Z | 109.25° ESE | 2026-09-18 06:56:58.773Z | 67.086° ENE | 25.937° | 2026-09-18 06:59:58.773Z | 15.913° NNE |
| 5 mins | 2026-09-18 08:29:58.773Z | 221.645° SW | 2026-09-18 08:31:58.773Z | 258.465° W | 23.606° | 2026-09-18 08:34:58.773Z | 313.188° 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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