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: 15 hours ago
TLE from 15 hours ago
0 CUAVA-2
1 60527U 24149BM 26264.75322065 .00008735 00000-0 23478-3 0 9990
2 60527 97.3666 346.5438 0005114 313.6807 46.4014 15.38133007117000Epoch: 2026-09-21T18:04Z
TLE epoch observation values (Epoch: 2026-09-21T18:04:38.264Z)
Latitude
0.00002°
Longitude
74.75584°
Altitude
452.338 km
Speed
7.642 km/s
True Right ascension
23h 06m 10s
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
02:01:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
452.062 km
Perigee altitude
445.079 km
Semi-major axis
6,826.707 km
Eccentricity
0.00051
Inclination
97.3666°
RAAN
346.5438°
Arg. of periapsis
313.6807°
True anomaly
46.44386°
Mean anomaly
46.4014°
Eccentric anomaly
46.42263°
Mean motion
3.84792 °/min
Orbital period
93.56 mins
BSTAR
0.00023478
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-22 18:03:48.252Z | 31.289° NE | 2026-09-22 18:06:48.252Z | 118.777° SE | 38.936° | 2026-09-22 18:08:48.252Z | 164.639° S |
| 4 mins | 2026-09-23 06:07:48.252Z | 213.783° SW | 2026-09-23 06:09:48.252Z | 275.946° WNW | 31.131° | 2026-09-23 06:11:48.252Z | 320.891° NNW |
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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