ARVAKER-1, 63252
Orbit data source: Space-Track
ARVAKER-1, 63252 is a payload satellite owned by NSC (NO) in SSO that was launched on Sat, 15 Mar 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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63252 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, 0.8 m
Radar Cross Section
0.146 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 ARVAKER-1
1 63252U 25052AU 26072.26332271 .00002594 00000-0 24764-3 0 9991
2 63252 97.6988 325.4001 0002866 142.6127 217.5293 14.94158729 54285Epoch: 2026-03-13T06:19Z
TLE epoch observation values (Epoch: 2026-03-13T06:19:11.082Z)
Latitude
-0.00001°
Longitude
59.70256°
Altitude
589.615 km
Speed
7.564 km/s
True Right ascension
21h 41m 36s
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
04:32:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
583.993 km
Perigee altitude
580.003 km
Semi-major axis
6,960.135 km
Eccentricity
0.00029
Inclination
97.6988°
RAAN
325.4001°
Arg. of periapsis
142.6127°
True anomaly
217.5093°
Mean anomaly
217.5293°
Eccentric anomaly
217.5193°
Mean motion
3.73781 °/min
Orbital period
96.31 mins
BSTAR
0.00024764
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Other satellites on launch #52 in the year 2025 (2025-03-15 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-1 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 | 2026-03-14 05:23:36.521Z | 24.756° NE | 2026-03-14 05:26:36.521Z | 86.422° E | 38.956° | 2026-03-14 05:30:36.521Z | 177.824° S |
| 5 mins | 2026-03-14 16:13:36.521Z | 118.833° SE | 2026-03-14 16:15:36.521Z | 71.338° E | 28.337° | 2026-03-14 16:18:36.521Z | 12.552° NNE |
| 4 mins | 2026-03-14 17:49:36.521Z | 239.424° WSW | 2026-03-14 17:50:36.521Z | 256.944° W | 17.371° | 2026-03-14 17:53:36.521Z | 307.202° 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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