NAPA-2, 48963
Orbit data source: Space-Track
NAPA-2, 48963 is a payload satellite owned by RTAF (TH) in SSO that was launched on Wed, 30 Jun 2021 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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48963 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, 0.1 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 NAPA-2
1 48963U 21059CN 25355.77626606 .00046879 00000-0 58573-3 0 9992
2 48963 97.6831 171.2597 0003734 258.6437 101.4399 15.59706297249890Epoch: 2025-12-21T18:37Z
TLE epoch observation values (Epoch: 2025-12-21T18:37:49.387Z)
Latitude
-0.00006°
Longitude
161.22007°
Altitude
392.144 km
Speed
7.675 km/s
True Right ascension
11h 25m 02s
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
05:51:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
387.957 km
Perigee altitude
382.906 km
Semi-major axis
6,763.569 km
Eccentricity
0.00037
Inclination
97.6831°
RAAN
171.2597°
Arg. of periapsis
258.6437°
True anomaly
101.48183°
Mean anomaly
101.4399°
Eccentric anomaly
101.46087°
Mean motion
3.90193 °/min
Orbital period
92.26 mins
BSTAR
0.00058573
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Other satellites on launch #59 in the year 2021 (2021-06-30 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-2 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 | 2025-12-22 11:42:18.571Z | 149.172° SSE | 2025-12-22 11:44:18.571Z | 94.167° ESE | 37.987° | 2025-12-22 11:47:18.571Z | 358.11° N |
| 4 mins | 2025-12-23 00:27:18.571Z | 37.915° NE | 2025-12-23 00:29:18.571Z | 111.2° ESE | 32.022° | 2025-12-23 00:31:18.571Z | 165.933° S |
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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