NAPA-1, 46320
Orbit data source: Space-Track
NAPA-1, 46320 is a payload satellite owned by RTAF (TH) in SSO 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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Edit Public Description
Identifier
Orbit
Country
Unknown / THAIRelated business
Manufacturer
ISIS BV
Mission
Operational 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, Unknown HBR
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 NAPA-1
1 46320U 20061BA 25287.95952434 .00030131 00000-0 63913-3 0 9992
2 46320 97.2859 353.2551 0001657 132.8436 227.2952 15.45009929283621Epoch: 2025-10-14T23:01Z
TLE epoch observation values (Epoch: 2025-10-14T23:01:42.902Z)
Latitude
-0.0001°
Longitude
-15.91411°
Altitude
435.242 km
Speed
7.65 km/s
True Right ascension
23h 33m 01s
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
10:42:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
429.404 km
Perigee altitude
427.148 km
Semi-major axis
6,806.413 km
Eccentricity
0.00017
Inclination
97.2859°
RAAN
353.2551°
Arg. of periapsis
132.8436°
True anomaly
227.28125°
Mean anomaly
227.2952°
Eccentric anomaly
227.28822°
Mean motion
3.86514 °/min
Orbital period
93.14 mins
BSTAR
0.00063913
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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 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 | 2025-10-15 16:42:05.019Z | 49.54° ENE | 2025-10-15 16:44:05.019Z | 96.477° ESE | 21.326° | 2025-10-15 16:46:05.019Z | 143.071° SSE |
| 5 mins | 2025-10-16 04:42:05.019Z | 182.969° SSW | 2025-10-16 04:44:05.019Z | 268.224° W | 41.499° | 2025-10-16 04:47:05.019Z | 341.018° N |
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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