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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Edit Public Description
Identifier
Orbit
Country
SB / SLBRelated business
Manufacturer
GAF
Mission
Operational Amateur Technology
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 + 1 Rod, 1.5 m
Radar Cross Section
0.035 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 GOOD ANCESTOR KILAKILA
1 64528U 25135A 25311.86803147 .00014863 00000-0 70567-3 0 9990
2 64528 97.4499 64.1060 0004769 231.6677 128.4129 15.19332314 21220Epoch: 2025-11-07T20:49Z
TLE epoch observation values (Epoch: 2025-11-07T20:49:57.919Z)
Latitude
-0.00003°
Longitude
64.30885°
Altitude
512.987 km
Speed
7.606 km/s
True Right ascension
04h 16m 25s
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
06:17:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
508.108 km
Perigee altitude
501.543 km
Semi-major axis
6,882.963 km
Eccentricity
0.00048
Inclination
97.4499°
RAAN
64.106°
Arg. of periapsis
231.6677°
True anomaly
128.4557°
Mean anomaly
128.4129°
Eccentric anomaly
128.4343°
Mean motion
3.80084 °/min
Orbital period
94.72 mins
BSTAR
0.00070567
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-11-08 19:33:10.726Z | 62.311° ENE | 2025-11-08 19:35:10.726Z | 99.071° ESE | 15.392° | 2025-11-08 19:37:10.726Z | 132.352° SE |
| 4 mins | 2025-11-08 21:07:10.726Z | 331.699° NNW | 2025-11-08 21:09:10.726Z | 277.443° WNW | 25.922° | 2025-11-08 21:11:10.726Z | 235.317° WSW |
| 5 mins | 2025-11-09 07:45:10.726Z | 174.74° S | 2025-11-09 07:47:10.726Z | 305.455° NW | 43.883° | 2025-11-09 07:50:10.726Z | 344.955° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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