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: 6 hours ago
TLE from 6 hours ago
0 ARVAKER-1
1 63252U 25052AU 26220.63528448 .00001278 00000-0 12282-3 0 9990
2 63252 97.6801 110.7448 0003866 61.1972 298.9636 14.94741048 76441Epoch: 2026-08-08T15:14Z
TLE epoch observation values (Epoch: 2026-08-08T15:14:48.579Z)
Latitude
-0.00004°
Longitude
-75.10141°
Altitude
584.922 km
Speed
7.569 km/s
True Right ascension
07h 22m 58s
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
11:43:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
582.878 km
Perigee altitude
577.498 km
Semi-major axis
6,958.325 km
Eccentricity
0.00039
Inclination
97.6801°
RAAN
110.7448°
Arg. of periapsis
61.1972°
True anomaly
298.92483°
Mean anomaly
298.9636°
Eccentric anomaly
298.94422°
Mean motion
3.73926 °/min
Orbital period
96.28 mins
BSTAR
0.00012282
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-08-09 04:41:25.459Z | 54.376° ENE | 2026-08-09 04:43:25.459Z | 87.255° E | 18.098° | 2026-08-09 04:46:25.459Z | 137.356° SSE |
| 5 mins | 2026-08-09 06:17:25.459Z | 331.878° NNW | 2026-08-09 06:19:25.459Z | 281.862° WNW | 27.263° | 2026-08-09 06:22:25.459Z | 229.475° WSW |
| 6 mins | 2026-08-09 17:05:25.459Z | 191.708° SSW | 2026-08-09 17:07:25.459Z | 241.32° WSW | 37.92° | 2026-08-09 17:11:25.459Z | 336.572° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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