NAPA-1, 46320
Orbit data source: Space-Track
NAPA-1, 46320 is a payload satellite owned by RTAF (TH) in LEO that was launched on Thu, 03 Sep 2020 UTC via a VEGA launch vehicle from the French Guiana (FRGUI). 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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46320 intel report (Beta)
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Identifier
Orbit
Country
TH / THAIRelated business
Manufacturer
ISIS BV
Mission
Decayed Defense Imaging
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, 10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 NAPA-1
1 46320U 20061BA 26306.03458208 .14783012 24884-5 17213-3 0 9995
2 46320 97.2106 27.7167 0012801 262.9372 97.0478 16.49487913343541Epoch: 2026-11-02T00:49Z
TLE epoch observation values (Epoch: 2026-11-02T00:49:47.891Z)
Latitude
0.00003°
Longitude
-26.05024°
Altitude
144.989 km
Speed
7.818 km/s
True Right ascension
01h 50m 52s
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
02:49:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
145.812 km
Perigee altitude
129.131 km
Semi-major axis
6,515.608 km
Eccentricity
0.00128
Inclination
97.2106°
RAAN
27.7167°
Arg. of periapsis
262.9372°
True anomaly
97.19335°
Mean anomaly
97.0478°
Eccentric anomaly
97.12058°
Mean motion
4.12677 °/min
Orbital period
87.24 mins
BSTAR
0.00017213
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Other satellites on launch #61 in the year 2020 (2020-09-03 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.NAPA-1 Visibility
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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. |
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| NAPA-1 is likely not visible in the next few days. |
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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