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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Edit Public Description
Identifier
Orbit
Country
NO / NORRelated business
Manufacturer
NanoAvionics
Mission
Operational Commercial Imaging
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: 15 hours ago
TLE from 15 hours ago
0 ARVAKER-1
1 63252U 25052AU 25287.26805689 .00003661 00000-0 35706-3 0 9990
2 63252 97.7088 178.3370 0002276 4.7137 355.4104 14.93051464 31897Epoch: 2025-10-14T06:26Z
TLE epoch observation values (Epoch: 2025-10-14T06:26:00.115Z)
Latitude
0.00002°
Longitude
58.77759°
Altitude
589.891 km
Speed
7.566 km/s
True Right ascension
11h 53m 20s
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
15:55:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.027 km
Perigee altitude
583.857 km
Semi-major axis
6,963.579 km
Eccentricity
0.00023
Inclination
97.7088°
RAAN
178.337°
Arg. of periapsis
4.7137°
True anomaly
355.40831°
Mean anomaly
355.4104°
Eccentric anomaly
355.40936°
Mean motion
3.73503 °/min
Orbital period
96.38 mins
BSTAR
0.00035706
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-10-15 05:30:39.624Z | 19.309° NNE | 2025-10-15 05:34:39.624Z | 104.06° ESE | 41.705° | 2025-10-15 05:38:39.624Z | 182.552° SSW |
| 5 mins | 2025-10-15 16:21:39.624Z | 126.169° SE | 2025-10-15 16:23:39.624Z | 78.729° E | 31.112° | 2025-10-15 16:26:39.624Z | 11.293° NNE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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