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: 17 hours ago
TLE from 17 hours ago
0 GOOD ANCESTOR KILAKILA
1 64528U 25135A 25327.86944562 .00011548 00000-0 54190-3 0 9995
2 64528 97.4507 79.8966 0005551 171.9844 188.1481 15.19796119 23650Epoch: 2025-11-23T20:52Z
TLE epoch observation values (Epoch: 2025-11-23T20:52:00.101Z)
Latitude
0.00001°
Longitude
63.8186°
Altitude
513.329 km
Speed
7.605 km/s
True Right ascension
05h 19m 35s
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
10:48:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.244 km
Perigee altitude
499.604 km
Semi-major axis
6,881.561 km
Eccentricity
0.00056
Inclination
97.4507°
RAAN
79.8966°
Arg. of periapsis
171.9844°
True anomaly
188.13909°
Mean anomaly
188.1481°
Eccentric anomaly
188.14359°
Mean motion
3.80201 °/min
Orbital period
94.69 mins
BSTAR
0.0005419
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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 | 2025-11-24 19:34:19.439Z | 55.443° ENE | 2025-11-24 19:36:19.439Z | 90.182° ESE | 15.908° | 2025-11-24 19:38:19.439Z | 127.197° SE |
| 5 mins | 2025-11-24 21:08:19.439Z | 337.112° NNW | 2025-11-24 21:10:19.439Z | 290.706° WNW | 25.308° | 2025-11-24 21:13:19.439Z | 230.525° WSW |
| 5 mins | 2025-11-25 07:46:19.439Z | 175.881° S | 2025-11-25 07:48:19.439Z | 255.438° W | 44.11° | 2025-11-25 07:51:19.439Z | 343.579° 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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