CUAVA-2, 60527
Orbit data source: Space-Track
CUAVA-2, 60527 is an Australian payload satellite in SSO that was launched on Fri, 16 Aug 2024 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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60527 intel report (Beta)
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Identifier
Orbit
Country
AU / AUSRelated business
Manufacturer
USYD/UNSW
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, 10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 CUAVA-2
1 60527U 24149BM 26219.78634397 .00006365 00000-0 17655-3 0 9994
2 60527 97.3702 301.4274 0008158 107.4620 252.7517 15.37252797110091Epoch: 2026-08-07T18:52Z
TLE epoch observation values (Epoch: 2026-08-07T18:52:20.119Z)
Latitude
-0.00005°
Longitude
62.03654°
Altitude
459.009 km
Speed
7.636 km/s
True Right ascension
20h 05m 42s
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
21:50:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
456.75 km
Perigee altitude
445.607 km
Semi-major axis
6,829.316 km
Eccentricity
0.00082
Inclination
97.3702°
RAAN
301.4274°
Arg. of periapsis
107.462°
True anomaly
252.66245°
Mean anomaly
252.7517°
Eccentric anomaly
252.70707°
Mean motion
3.84572 °/min
Orbital period
93.61 mins
BSTAR
0.00017655
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Other satellites on launch #149 in the year 2024 (2024-08-16 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.CUAVA-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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-08-08 18:52:50.219Z | 333.452° NNW | 2026-08-08 18:53:50.219Z | 305.072° NW | 27.901° | 2026-08-08 18:56:50.219Z | 225.377° WSW |
| 5 mins | 2026-08-09 05:22:50.219Z | 151.899° SSE | 2026-08-09 05:24:50.219Z | 99.174° ESE | 40.443° | 2026-08-09 05:27:50.219Z | 357.272° N |
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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