LIZZIESAT-2, 62383
Orbit data source: Space-Track
LIZZIESAT-2, 62383 is a payload satellite owned by Sidus Space (US) in LEO that was launched on Sat, 21 Dec 2024 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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62383 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Sidus Space
Mission
Operational Commercial Technology
Bus & Motor
LIZZIESAT, Unknown motor
Mass
~100 kg wet, ~100 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Oct Cyl + 8 Pan, 0.7 m
Radar Cross Section
1.008 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 LIZZIESAT-2
1 62383U 24247G 26253.49515523 .00006220 00000-0 21382-3 0 9992
2 62383 44.9908 183.7219 0001446 344.9601 15.1240 15.30966679 96045Epoch: 2026-09-10T11:53Z
TLE epoch observation values (Epoch: 2026-09-10T11:53:01.411Z)
Latitude
-0.00004°
Longitude
15.93394°
Altitude
471.968 km
Speed
7.632 km/s
True Right ascension
12h 14m 53s
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
14:21:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
475.531 km
Perigee altitude
473.549 km
Semi-major axis
6,852.677 km
Eccentricity
0.00014
Inclination
44.9908°
RAAN
183.7219°
Arg. of periapsis
344.9601°
True anomaly
15.12832°
Mean anomaly
15.124°
Eccentric anomaly
15.12616°
Mean motion
3.82607 °/min
Orbital period
94.09 mins
BSTAR
0.00021382
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Other satellites on launch #247 in the year 2024 (2024-12-21 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.LIZZIESAT-2 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 | 2026-09-10 23:03:47.279Z | 230.654° WSW | 2026-09-10 23:06:47.279Z | 127.533° SE | 61.639° | 2026-09-10 23:09:47.279Z | 71.467° E |
| 6 mins | 2026-09-11 00:42:47.279Z | 283.926° WNW | 2026-09-11 00:44:47.279Z | 327.813° NNW | 40.003° | 2026-09-11 00:48:47.279Z | 62.019° ENE |
| 5 mins | 2026-09-11 02:21:47.279Z | 304.744° NW | 2026-09-11 02:23:47.279Z | 347.448° N | 37.063° | 2026-09-11 02:26:47.279Z | 71.567° E |
| 5 mins | 2026-09-11 04:00:47.279Z | 290.754° WNW | 2026-09-11 04:02:47.279Z | 260.076° W | 73.965° | 2026-09-11 04:05:47.279Z | 119.869° SE |
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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