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, 0.5 m
Radar Cross Section
0.146 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 ARVAKER-1
1 63252U 25052AU 26259.92919724 .00001548 00000-0 14722-3 0 9996
2 63252 97.6732 149.1963 0000911 295.7348 64.3779 14.94857799 82319Epoch: 2026-09-16T22:18Z
TLE epoch observation values (Epoch: 2026-09-16T22:18:02.641Z)
Latitude
0.00001°
Longitude
178.81155°
Altitude
585.588 km
Speed
7.568 km/s
True Right ascension
09h 56m 47s
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
02:59:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
580.459 km
Perigee altitude
579.191 km
Semi-major axis
6,957.962 km
Eccentricity
0.00009
Inclination
97.6732°
RAAN
149.1963°
Arg. of periapsis
295.7348°
True anomaly
64.38731°
Mean anomaly
64.3779°
Eccentric anomaly
64.38261°
Mean motion
3.73956 °/min
Orbital period
96.27 mins
BSTAR
0.00014722
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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 | 2026-09-17 16:06:53.422Z | 126.158° SE | 2026-09-17 16:09:53.422Z | 62.926° ENE | 31.259° | 2026-09-17 16:12:53.422Z | 11.142° NNE |
| 4 mins | 2026-09-17 17:43:53.422Z | 244.208° WSW | 2026-09-17 17:44:53.422Z | 263.103° W | 19.304° | 2026-09-17 17:47:53.422Z | 311.422° NW |
| 7 mins | 2026-09-18 05:23:53.422Z | 21.782° NNE | 2026-09-18 05:26:53.422Z | 93.565° ESE | 63.488° | 2026-09-18 05:30:53.422Z | 182.541° SSW |
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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