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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.

Not visible in the next 10 days
Identifier
48963, 2021-059CN
Orbit
SSO
Country
Flag of UnknownUnknown / THAI
Related business
Manufacturer
ISIS BV
Mission
Operational Defense Imaging
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, 10 kg dry
Launch date (UTC)
2021-06-30 (4 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 8 hours ago

TLE from 8 hours ago
0 NAPA-2
1 48963U 21059CN  25308.80362534  .00033699  00000-0  50731-3 0  9995
2 48963  97.6854 120.6382 0005491  69.4629 290.7213 15.54742936242589
Epoch: 2025-11-04T19:17Z
TLE epoch observation values (Epoch: 2025-11-04T19:17:13.229Z)
Latitude
-0.00001°
Longitude
147.04768°
Altitude
404.713 km
Speed
7.669 km/s
True Right ascension
08h 02m 33s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
23:06:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
403.554 km
Perigee altitude
396.11 km
Semi-major axis
6,777.969 km
Eccentricity
0.00055
Inclination
97.6854°
RAAN
120.6382°
Arg. of periapsis
69.4629°
True anomaly
290.66243°
Mean anomaly
290.7213°
Eccentric anomaly
290.69187°
Mean motion
3.8895 °/min
Orbital period
92.56 mins
BSTAR
0.00050731
Loading maneuver chart data...
Computing Atmospheric mass density...

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