LIZZIESAT, 59132
Orbit data source: Space-Track
LIZZIESAT, 59132 is a payload satellite owned by Sidus Space (US) in SSO that was launched on Mon, 04 Mar 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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59132 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
1 59132U 24043AL 25259.88287259 .00004892 00000-0 20186-3 0 9998
2 59132 97.5279 28.1205 0012602 123.3311 236.9134 15.24450106 85250Epoch: 2025-09-16T21:11Z
TLE epoch observation values (Epoch: 2025-09-16T21:11:20.191Z)
Latitude
-0.0001°
Longitude
74.21959°
Altitude
500.265 km
Speed
7.612 km/s
True Right ascension
01h 52m 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
20:50:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
498.057 km
Perigee altitude
480.748 km
Semi-major axis
6,867.539 km
Eccentricity
0.00126
Inclination
97.5279°
RAAN
28.1205°
Arg. of periapsis
123.3311°
True anomaly
236.79251°
Mean anomaly
236.9134°
Eccentric anomaly
236.85295°
Mean motion
3.81366 °/min
Orbital period
94.4 mins
BSTAR
0.00020186
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Other satellites on launch #43 in the year 2024 (2024-03-04 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 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-18 07:59:35.805Z | 119.8° SE | 2025-09-18 08:01:35.805Z | 79.805° E | 22.475° | 2025-09-18 08:04:35.805Z | 17.555° NNE |
| 5 mins | 2025-09-18 21:01:35.805Z | 41.551° NE | 2025-09-18 21:03:35.805Z | 89.986° E | 28.461° | 2025-09-18 21:06:35.805Z | 160.28° S |
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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