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SEMI-1P, 66298

Orbit data source: Space-Track

SEMI-1P, 66298 is a Turkish payload satellite in LEO that was launched on Sun, 02 Nov 2025 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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Identifier
66298, 2025-248F
Orbit
LEO
Country
Flag of TRTR / TURK
Related business
Manufacturer
UNKTR
Mission
Operational Commercial Communications
Bus & Motor
CUBESAT 6U?, Unknown motor
Mass
12 kg wet, 12 kg dry
Launch date (UTC)
2025-11-02 (8 months 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: 15 hours ago

TLE from 15 hours ago
0 SEMI-1P
1 66298U 25248F   26171.20385959  .00007026  00000-0  32270-3 0  9992
2 66298  45.3808 103.5785 0012195  44.8762 315.3108 15.21045957 34994
Epoch: 2026-06-20T04:53Z
TLE epoch observation values (Epoch: 2026-06-20T04:53:33.468Z)
Latitude
-0.00005°
Longitude
121.76715°
Altitude
496.766 km
Speed
7.621 km/s
True Right ascension
06h 54m 18s
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
07:18:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
512.618 km
Perigee altitude
495.832 km
Semi-major axis
6,882.362 km
Eccentricity
0.00122
Inclination
45.3808°
RAAN
103.5785°
Arg. of periapsis
44.8762°
True anomaly
315.21242°
Mean anomaly
315.3108°
Eccentric anomaly
315.26162°
Mean motion
3.80134 °/min
Orbital period
94.7 mins
BSTAR
0.0003227
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