KITSAT 3, 25756
Orbit data source: Space-Track
KITSAT 3, 25756 is a payload satellite owned by KAIST (KR) in SSO that was launched on Wed, 26 May 1999 UTC via a PSLV launch vehicle from the Sirharikota (SRI). 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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25756 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / SKORRelated business
Manufacturer
KAIST
Mission
Non-operational Civil Imaging
Bus & Motor
SI-200, Unknown motor
Mass
110 kg wet, 110 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.8 m
Radar Cross Section
0.780 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 KITSAT 3
1 25756U 99029A 25259.57653872 .00000232 00000-0 64527-4 0 9995
2 25756 98.6492 280.8959 0013708 24.6392 335.5457 14.55578235395229Epoch: 2025-09-16T13:50Z
TLE epoch observation values (Epoch: 2025-09-16T13:50:12.945Z)
Latitude
0.00004°
Longitude
77.5771°
Altitude
701.611 km
Speed
7.51 km/s
True Right ascension
18h 43m 35s
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
14:01:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
714.305 km
Perigee altitude
694.887 km
Semi-major axis
7,082.733 km
Eccentricity
0.00137
Inclination
98.6492°
RAAN
280.8959°
Arg. of periapsis
24.6392°
True anomaly
335.48057°
Mean anomaly
335.5457°
Eccentric anomaly
335.51315°
Mean motion
3.64118 °/min
Orbital period
98.87 mins
BSTAR
0.000064527
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Other satellites on launch #29 in the year 1999 (1999-05-26 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.KITSAT 3 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-09-17 01:30:35.107Z | 167.416° S | 2025-09-17 01:34:35.107Z | 330.995° NNW | 43.875° | 2025-09-17 01:38:35.107Z | 345.471° N |
| 6 mins | 2025-09-17 13:32:35.107Z | 57.169° ENE | 2025-09-17 13:34:35.107Z | 90.754° ESE | 22.422° | 2025-09-17 13:38:35.107Z | 149.142° SSE |
| 7 mins | 2025-09-17 15:09:35.107Z | 346.123° N | 2025-09-17 15:12:35.107Z | 292.277° WNW | 29.053° | 2025-09-17 15:16:35.107Z | 229.291° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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