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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Edit Public Description
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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 KANYINI
1 60556U 24149CS 25286.91996305 .00028798 00000-0 84435-3 0 9998
2 60556 97.3978 5.1211 0002782 72.0017 288.1529 15.35145645 64513Epoch: 2025-10-13T22:04Z
TLE epoch observation values (Epoch: 2025-10-13T22:04:44.807Z)
Latitude
-0.00006°
Longitude
11.21858°
Altitude
463.007 km
Speed
7.635 km/s
True Right ascension
00h 20m 29s
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
10:35:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
459.335 km
Perigee altitude
455.532 km
Semi-major axis
6,835.57 km
Eccentricity
0.00028
Inclination
97.3978°
RAAN
5.1211°
Arg. of periapsis
72.0017°
True anomaly
288.1226°
Mean anomaly
288.1529°
Eccentric anomaly
288.13775°
Mean motion
3.84044 °/min
Orbital period
93.74 mins
BSTAR
0.00084435
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-14 17:25:48.377Z | 53.77° ENE | 2025-10-14 17:27:48.377Z | 94.782° ESE | 18.342° | 2025-10-14 17:29:48.377Z | 135.992° SSE |
| 4 mins | 2025-10-15 05:30:48.377Z | 180.9° SSW | 2025-10-15 05:32:48.377Z | 310.832° NW | 40.967° | 2025-10-15 05:34:48.377Z | 341.098° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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