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: 7 hours ago
TLE from 7 hours ago
0 NAPA-1
1 46320U 20061BA 25334.22479226 .00039161 00000-0 74601-3 0 9996
2 46320 97.2794 39.7424 0001846 84.4649 275.6812 15.48093165290776Epoch: 2025-11-30T05:23Z
TLE epoch observation values (Epoch: 2025-11-30T05:23:42.051Z)
Latitude
-0.00003°
Longitude
-110.52452°
Altitude
425.312 km
Speed
7.656 km/s
True Right ascension
02h 38m 58s
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
10:25:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
420.482 km
Perigee altitude
417.973 km
Semi-major axis
6,797.365 km
Eccentricity
0.00018
Inclination
97.2794°
RAAN
39.7424°
Arg. of periapsis
84.4649°
True anomaly
275.66015°
Mean anomaly
275.6812°
Eccentric anomaly
275.67067°
Mean motion
3.87286 °/min
Orbital period
92.95 mins
BSTAR
0.00074601
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-30 16:48:57.011Z | 38.83° NE | 2025-11-30 16:51:57.011Z | 108.133° ESE | 22.88° | 2025-11-30 16:53:57.011Z | 151.202° SSE |
| 4 mins | 2025-12-01 04:48:57.011Z | 196.932° SSW | 2025-12-01 04:49:57.011Z | 244.517° WSW | 39.359° | 2025-12-01 04:52:57.011Z | 338.268° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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