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 26175.17891167 .00002073 00000-0 19684-3 0 9996
2 63252 97.6871 66.2345 0002531 155.9070 204.2270 14.94584553 69653Epoch: 2026-06-24T04:17Z
TLE epoch observation values (Epoch: 2026-06-24T04:17:37.968Z)
Latitude
0.00006°
Longitude
89.48645°
Altitude
588.317 km
Speed
7.565 km/s
True Right ascension
04h 24m 56s
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
21:54:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
582.436 km
Perigee altitude
578.913 km
Semi-major axis
6,958.811 km
Eccentricity
0.00025
Inclination
97.6871°
RAAN
66.2345°
Arg. of periapsis
155.907°
True anomaly
204.2151°
Mean anomaly
204.227°
Eccentric anomaly
204.22105°
Mean motion
3.73887 °/min
Orbital period
96.29 mins
BSTAR
0.00019684
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-24 15:42:21.132Z | 97.952° ESE | 2026-06-24 15:44:21.132Z | 65.763° ENE | 15.673° | 2026-06-24 15:46:21.132Z | 33.855° NE |
| 5 mins | 2026-06-24 17:17:21.132Z | 207.113° SW | 2026-06-24 17:19:21.132Z | 260.089° W | 32.354° | 2026-06-24 17:22:21.132Z | 325.936° NNW |
| 5 mins | 2026-06-25 04:59:21.132Z | 50.166° ENE | 2026-06-25 05:01:21.132Z | 93.479° ESE | 25.924° | 2026-06-25 05:04:21.132Z | 152.021° SSE |
| 4 mins | 2026-06-25 06:35:21.132Z | 318.175° NNW | 2026-06-25 06:36:21.132Z | 298.776° NW | 19.61° | 2026-06-25 06:39:21.132Z | 246.826° WSW |
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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