KANYINI, 60556
Orbit data source: Space-Track
KANYINI, 60556 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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60556 intel report (Beta)
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Identifier
Orbit
Country
AU / AUSRelated business
Manufacturer
INOVOR
Mission
Operational Amateur Communications
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 + 2 Pan, 0.2 m
Radar Cross Section
0.092 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 KANYINI
1 60556U 24149CS 26276.49536429 .00047527 00000-0 54805-3 0 9997
2 60556 97.3659 6.9845 0002161 192.0925 168.0282 15.61809603119369Epoch: 2026-10-03T11:53Z
TLE epoch observation values (Epoch: 2026-10-03T11:53:19.474Z)
Latitude
0.00003°
Longitude
176.45121°
Altitude
387.007 km
Speed
7.677 km/s
True Right ascension
00h 27m 56s
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
02:53:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
380.799 km
Perigee altitude
377.878 km
Semi-major axis
6,757.475 km
Eccentricity
0.00022
Inclination
97.3659°
RAAN
6.9845°
Arg. of periapsis
192.0925°
True anomaly
168.03334°
Mean anomaly
168.0282°
Eccentric anomaly
168.03077°
Mean motion
3.90721 °/min
Orbital period
92.14 mins
BSTAR
0.00054805
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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.KANYINI 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 | 2026-10-04 19:11:21.097Z | 4.265° NNE | 2026-10-04 19:14:21.097Z | 263.101° W | 59.112° | 2026-10-04 19:16:21.097Z | 206.064° SW |
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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