QUICK3, 64558
Orbit data source: Space-Track
QUICK3, 64558 is a Lithuanian 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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64558 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
LT / LTURelated business
Manufacturer
NANAV/JENAU
Mission
Operational Commercial Com/MetRO
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
5 kg wet, 5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.045 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 QUICK3
1 64558U 25135AG 25328.29964823 .00014879 00000-0 67660-3 0 9994
2 64558 97.4618 80.6140 0006522 152.8758 207.2819 15.20815163 23641Epoch: 2025-11-24T07:11Z
TLE epoch observation values (Epoch: 2025-11-24T07:11:29.607Z)
Latitude
-0.00003°
Longitude
-90.76096°
Altitude
510.461 km
Speed
7.606 km/s
True Right ascension
05h 22m 27s
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
14:00:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.834 km
Perigee altitude
495.861 km
Semi-major axis
6,878.485 km
Eccentricity
0.00065
Inclination
97.4618°
RAAN
80.614°
Arg. of periapsis
152.8758°
True anomaly
207.24767°
Mean anomaly
207.2819°
Eccentric anomaly
207.26478°
Mean motion
3.80456 °/min
Orbital period
94.62 mins
BSTAR
0.0006766
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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.QUICK3 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-24 20:22:48.753Z | 16.963° NNE | 2025-11-24 20:25:48.753Z | 51.533° ENE | 41.194° | 2025-11-24 20:29:48.753Z | 185.789° SSW |
| 5 mins | 2025-11-25 07:01:48.753Z | 116.843° SE | 2025-11-25 07:03:48.753Z | 71.116° E | 24.053° | 2025-11-25 07:06:48.753Z | 13.989° NNE |
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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