CATSAT, 60246
Orbit data source: Space-Track
CATSAT, 60246 is a payload satellite owned by U. Arizona (US) in SSO that was launched on Thu, 04 Jul 2024 UTC via an FIREFLY ALPHA 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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60246 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
U. Arizona
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
12 kg wet, ~12 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + Inf Sphere + 1 Pan, 0.4 m
Radar Cross Section
0.050 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 CATSAT
1 60246U 24125J 26265.12483549 .00102417 00000-0 73819-3 0 9995
2 60246 97.1937 119.7766 0015310 170.9306 189.2238 15.73091574122559Epoch: 2026-09-22T02:59Z
TLE epoch observation values (Epoch: 2026-09-22T02:59:45.786Z)
Latitude
-0.00001°
Longitude
73.84102°
Altitude
363.406 km
Speed
7.685 km/s
True Right ascension
07h 59m 06s
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
05:10:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
357.25 km
Perigee altitude
336.657 km
Semi-major axis
6,725.091 km
Eccentricity
0.00153
Inclination
97.1937°
RAAN
119.7766°
Arg. of periapsis
170.9306°
True anomaly
189.19573°
Mean anomaly
189.2238°
Eccentric anomaly
189.20976°
Mean motion
3.93546 °/min
Orbital period
91.48 mins
BSTAR
0.00073819
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Other satellites on launch #125 in the year 2024 (2024-07-04 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.CATSAT Visibility
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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. |
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| CATSAT is likely not visible in the next few days. |
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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