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: 11 hours ago
TLE from 11 hours ago
0 LIZZIESAT-2
1 62383U 24247G 26036.71613447 .00014698 00000-0 54489-3 0 9992
2 62383 44.9908 290.6494 0003053 150.9366 209.1687 15.27558485 62857Epoch: 2026-02-05T17:11Z
TLE epoch observation values (Epoch: 2026-02-05T17:11:14.018Z)
Latitude
-0.00003°
Longitude
-103.02341°
Altitude
484.94 km
Speed
7.624 km/s
True Right ascension
19h 22m 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
06:43:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.82 km
Perigee altitude
482.629 km
Semi-major axis
6,862.861 km
Eccentricity
0.00031
Inclination
44.9908°
RAAN
290.6494°
Arg. of periapsis
150.9366°
True anomaly
209.15165°
Mean anomaly
209.1687°
Eccentric anomaly
209.16018°
Mean motion
3.81756 °/min
Orbital period
94.3 mins
BSTAR
0.00054489
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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 | 2026-02-06 20:05:13.711Z | 226.355° WSW | 2026-02-06 20:08:13.711Z | 115.896° SE | 38.761° | 2026-02-06 20:11:13.711Z | 72.209° E |
| 6 mins | 2026-02-06 21:44:13.711Z | 282.23° WNW | 2026-02-06 21:46:13.711Z | 327.171° NNW | 33.797° | 2026-02-06 21:50:13.711Z | 62.289° ENE |
| 5 mins | 2026-02-06 23:24:13.711Z | 314.502° NW | 2026-02-06 23:26:13.711Z | 21.574° NNE | 31.742° | 2026-02-06 23:29:13.711Z | 76.92° E |
| 6 mins | 2026-02-07 01:02:13.711Z | 292.004° WNW | 2026-02-07 01:05:13.711Z | 136.762° SSE | 43.692° | 2026-02-07 01:08:13.711Z | 117.732° 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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