GOOD ANCESTOR KILAKILA, 64528
Orbit data source: Space-Track
GOOD ANCESTOR KILAKILA, 64528 is a Solomon Islander payload satellite in SSO that was launched on Mon, 23 Jun 2025 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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64528 intel report (Beta)
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Identifier
Orbit
Country
SB / SLBRelated business
Manufacturer
GAF
Mission
Operational Amateur Communications
Bus & Motor
CUBESAT 2U, Unknown motor
Mass
2 kg wet, 2 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.025 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 GOOD ANCESTOR KILAKILA
1 64528U 25135A 26234.86089944 .00007414 00000-0 30030-3 0 9991
2 64528 97.4679 349.8475 0003604 324.9048 35.1952 15.24960746 65046Epoch: 2026-08-22T20:39Z
TLE epoch observation values (Epoch: 2026-08-22T20:39:41.711Z)
Latitude
-0°
Longitude
68.75847°
Altitude
491.975 km
Speed
7.62 km/s
True Right ascension
23h 19m 23s
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
23:04:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
490.34 km
Perigee altitude
485.391 km
Semi-major axis
6,866.002 km
Eccentricity
0.00036
Inclination
97.4679°
RAAN
349.8475°
Arg. of periapsis
324.9048°
True anomaly
35.21901°
Mean anomaly
35.1952°
Eccentric anomaly
35.20711°
Mean motion
3.81494 °/min
Orbital period
94.37 mins
BSTAR
0.0003003
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Other satellites on launch #135 in the year 2025 (2025-06-23 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.GOOD ANCESTOR KILAKILA 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-08-24 20:28:01.412Z | 19.049° NNE | 2026-08-24 20:31:01.412Z | 94.849° ESE | 42.518° | 2026-08-24 20:34:01.412Z | 182.75° SSW |
| 4 mins | 2026-08-25 07:05:01.412Z | 112.364° ESE | 2026-08-25 07:07:01.412Z | 67.145° ENE | 21.842° | 2026-08-25 07:09:01.412Z | 25.064° NE |
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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