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: 11 hours ago
TLE from 11 hours ago
0 ARVAKER-1
1 63252U 25052AU 26129.65038218 .00001847 00000-0 17670-3 0 9999
2 63252 97.6917 21.6367 0002805 24.8558 335.2797 14.94415020 62858Epoch: 2026-05-09T15:36Z
TLE epoch observation values (Epoch: 2026-05-09T15:36:33.020Z)
Latitude
-0.00002°
Longitude
-79.96565°
Altitude
585.462 km
Speed
7.569 km/s
True Right ascension
01h 26m 32s
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
11:14:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
583.154 km
Perigee altitude
579.249 km
Semi-major axis
6,959.338 km
Eccentricity
0.00028
Inclination
97.6917°
RAAN
21.6367°
Arg. of periapsis
24.8558°
True anomaly
335.26625°
Mean anomaly
335.2797°
Eccentric anomaly
335.27298°
Mean motion
3.73845 °/min
Orbital period
96.3 mins
BSTAR
0.0001767
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-05-10 05:02:37.186Z | 38.752° NE | 2026-05-10 05:05:37.186Z | 97.909° ESE | 27.659° | 2026-05-10 05:08:37.186Z | 155.782° SSE |
| 4 mins | 2026-05-10 06:39:37.186Z | 314.669° NW | 2026-05-10 06:40:37.186Z | 295.555° NW | 18.644° | 2026-05-10 06:43:37.186Z | 247.05° WSW |
| 4 mins | 2026-05-10 15:52:37.186Z | 101.585° ESE | 2026-05-10 15:54:37.186Z | 64.778° ENE | 18.952° | 2026-05-10 15:56:37.186Z | 30.037° NE |
| 5 mins | 2026-05-10 17:27:37.186Z | 216.069° SW | 2026-05-10 17:29:37.186Z | 261.542° W | 27.035° | 2026-05-10 17:32:37.186Z | 320.519° 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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