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, 2.3 m
Radar Cross Section
7.561 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 CAS500-2
1 69013U 26100AK 26254.69553051 .00004050 00000-0 18969-3 0 9996
2 69013 97.3762 150.7847 0011234 75.8592 284.3891 15.20219217 19953Epoch: 2026-09-11T16:41Z
TLE epoch observation values (Epoch: 2026-09-11T16:41:33.836Z)
Latitude
0.00001°
Longitude
-90.32148°
Altitude
506.356 km
Speed
7.612 km/s
True Right ascension
10h 03m 08s
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
09:16:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.872 km
Perigee altitude
494.414 km
Semi-major axis
6,880.28 km
Eccentricity
0.00112
Inclination
97.3762°
RAAN
150.7847°
Arg. of periapsis
75.8592°
True anomaly
284.26436°
Mean anomaly
284.3891°
Eccentric anomaly
284.32674°
Mean motion
3.80307 °/min
Orbital period
94.66 mins
BSTAR
0.00018969
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-12 18:05:40.335Z | 220.298° SW | 2026-09-12 18:08:40.335Z | 274.839° WNW | 18.201° | 2026-09-12 18:10:40.335Z | 309.201° NW |
| 5 mins | 2026-09-13 05:36:40.335Z | 43.551° NE | 2026-09-13 05:38:40.335Z | 104.308° ESE | 37.81° | 2026-09-13 05:41:40.335Z | 165.9° 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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