CAS500-2, 69013
Orbit data source: Space-Track
CAS500-2, 69013 is a payload satellite owned by KAIST (KR) in SSO that was launched on Sun, 03 May 2026 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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69013 intel report (Beta)
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Identifier
Orbit
Country
KR / SKORRelated business
Manufacturer
SatRec Initiative
Mission
Operational Civil Technology
Bus & Motor
CAS500, Unknown motor
Mass
516 kg wet, 516 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 4 Pan, 14.5 m
Radar Cross Section
7.561 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 CAS500-2
1 69013U 26100AK 26237.64858155 .00005173 00000-0 23951-3 0 9999
2 69013 97.3797 134.1045 0010747 115.9524 244.2821 15.20496685 17363Epoch: 2026-08-25T15:33Z
TLE epoch observation values (Epoch: 2026-08-25T15:33:57.445Z)
Latitude
0.00005°
Longitude
-73.29777°
Altitude
510.65 km
Speed
7.607 km/s
True Right ascension
08h 56m 25s
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
21:34:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
508.699 km
Perigee altitude
493.912 km
Semi-major axis
6,879.442 km
Eccentricity
0.00107
Inclination
97.3797°
RAAN
134.1045°
Arg. of periapsis
115.9524°
True anomaly
244.17121°
Mean anomaly
244.2821°
Eccentric anomaly
244.22665°
Mean motion
3.80376 °/min
Orbital period
94.64 mins
BSTAR
0.00023951
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Other satellites on launch #100 in the year 2026 (2026-05-03 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.CAS500-2 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-08-26 06:19:50.209Z | 1.273° NNE | 2026-08-26 06:23:50.209Z | 254.849° W | 36.122° | 2026-08-26 06:26:50.209Z | 209.087° SW |
| 5 mins | 2026-08-26 16:58:50.209Z | 145.494° SSE | 2026-08-26 17:00:50.209Z | 85.951° E | 39.075° | 2026-08-26 17:03:50.209Z | 0.212° NNE |
| 5 mins | 2026-08-27 06:02:50.209Z | 13.162° NNE | 2026-08-27 06:04:50.209Z | 25.301° NE | 44.456° | 2026-08-27 06:07:50.209Z | 191.742° SSW |
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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