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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Edit Public Description
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: 1 day ago
TLE from 1 day ago
0 LIZZIESAT-2
1 62383U 24247G 25346.10657716 .00013004 00000-0 50192-3 0 9992
2 62383 44.9884 233.9474 0002339 151.4670 208.6340 15.26314341 54354Epoch: 2025-12-12T02:33Z
TLE epoch observation values (Epoch: 2025-12-12T02:33:28.266Z)
Latitude
-0.00008°
Longitude
114.52659°
Altitude
488.248 km
Speed
7.622 km/s
True Right ascension
15h 35m 47s
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
05:23:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
490.058 km
Perigee altitude
486.846 km
Semi-major axis
6,866.589 km
Eccentricity
0.00023
Inclination
44.9884°
RAAN
233.9474°
Arg. of periapsis
151.467°
True anomaly
208.62116°
Mean anomaly
208.634°
Eccentric anomaly
208.62758°
Mean motion
3.81445 °/min
Orbital period
94.38 mins
BSTAR
0.00050192
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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 | 2025-12-13 19:36:11.269Z | 225.326° WSW | 2025-12-13 19:39:11.269Z | 155.365° SSE | 38.841° | 2025-12-13 19:42:11.269Z | 75.739° E |
| 5 mins | 2025-12-13 21:16:11.269Z | 284.241° WNW | 2025-12-13 21:18:11.269Z | 346.731° N | 35.786° | 2025-12-13 21:21:11.269Z | 58.989° ENE |
| 5 mins | 2025-12-13 22:55:11.269Z | 305.12° NW | 2025-12-13 22:57:11.269Z | 351.847° N | 31.44° | 2025-12-13 23:00:11.269Z | 70.431° E |
| 6 mins | 2025-12-14 00:34:11.269Z | 293.532° NW | 2025-12-14 00:36:11.269Z | 292.948° NW | 42.678° | 2025-12-14 00:40:11.269Z | 114.864° 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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