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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Identifier
Orbit
Country
LT / LTURelated business
Manufacturer
NANAV/JENAU
Mission
Operational Amateur Technology
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 + 1 Rod, 1.5 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 QUICK3
1 64558U 25135AG 26071.79109372 .00017391 00000-0 70445-3 0 9992
2 64558 97.4616 188.3697 0006429 135.5393 224.6362 15.24713552 40155Epoch: 2026-03-12T18:59Z
TLE epoch observation values (Epoch: 2026-03-12T18:59:10.497Z)
Latitude
0.00003°
Longitude
93.14004°
Altitude
497.886 km
Speed
7.614 km/s
True Right ascension
12h 33m 28s
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
11:57:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
493.022 km
Perigee altitude
484.193 km
Semi-major axis
6,866.745 km
Eccentricity
0.00064
Inclination
97.4616°
RAAN
188.3697°
Arg. of periapsis
135.5393°
True anomaly
224.58447°
Mean anomaly
224.6362°
Eccentric anomaly
224.61033°
Mean motion
3.81432 °/min
Orbital period
94.38 mins
BSTAR
0.00070445
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-03-13 07:42:22.644Z | 165.635° S | 2026-03-13 07:45:22.644Z | 157.834° S | 43.027° | 2026-03-13 07:48:22.644Z | 349.12° N |
| 5 mins | 2026-03-13 20:45:22.644Z | 1.709° NNE | 2026-03-13 20:47:22.644Z | 318.572° NNW | 40.748° | 2026-03-13 20:50:22.644Z | 205.319° SW |
| 5 mins | 2026-03-14 07:21:22.644Z | 136.156° SSE | 2026-03-14 07:23:22.644Z | 84.432° E | 33.314° | 2026-03-14 07:26:22.644Z | 6.324° NNE |
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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